# TCDS A-759: American Champion Aircraft Corp. - Type: Type certificate data sheet - Status: Current - Holder: American Champion Aircraft Corp. - Revision: 73 - Revised: February 9, 2011 - Product: Aircraft, Small Airplane - Certification basis: Part 23, Part 36, CAR 4a, CAR 8 - Registered aircraft: 5,582, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/a3/89/a3893108540fde3ff3e89d9dab0537c3211414936079e879e7c45c4bf34f3293 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/2B3FA1C355E95F9A862578380053D423.0001 - Page: https://openairdocs.org/tcds/A-759 ## Models (22) As the data sheet lists them. - 7KC - S7EC - 7GCBA - 7FC - S7CCM - 7JC - 7EC - 7GCA - 7KCAB - 7GC - 7ACA - 7CCM (Army L-16B) - 7GCAA - 7HC - 7GCBC - 7AC - 7ECA - S7AC - S7DC - 7BCM (Army L-16A) - 7DC - 7GCB ## What the data sheet says Some pages are OCR from the scanned FAA data sheet. OCR can misread letters and numbers. ```text Page No. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 Rev. No. 70 65 65 65 65 65 65 65 65 65 71 68 70 67 73 73 66 71 73 70 Page No. 21 22 23 24 25 26 27 28 29 30 31 32 33 34 Rev No. 73 69 66 69 73 69 66 66 66 66 66 67 73 70 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A-759 Revision 73 American Champion (Bellanca) (Champion) 7AC (Aeronca) 7ACA 7EC 7GCB S7AC S7EC 7GCBA (L-16A) 7BCM 7ECA 7GCBC (L-16B) 7CCM 7FC 7HC S7CCM 7GC 7JC 7DC 7GCA 7KC S7DC 7GCAA 7KCAB February 9, 2011 AIRCRAFT SPECIFICATION NO. A-759 Type Certificate Holder: American Champion Aircraft Corp. P. O. Box 37 Rochester, WI 53167 Type Certificate Holder Record: Aeronca Ai rcraft Corporation transferred TC A-759 to Champion Aircraft Corporation on July 19, 1954 Champion Aircraft Corporation transferred TC A-759 to Bellanca Aircraft Corporation on March 15, 1971 Bellanca Aircraft Corporation transferred TC A-759 to Champion Aircraft Company, Inc. on November 1, 1982 Champion Aircraft Company, Inc. transferred TC A-759 to Tetelestai, Inc. on October 11, 1988 Tetelestai transferred TC A-759 to FRA Enterprises, Inc. on December 27, 1988 FRA Enterprises, Inc. transferred TC A-759 to American Champion Aircraft Corp.on May 30, 1989 I - Model 7AC, 2 PCLM (Normal Category), Approved October 18, 1945 (See NOTE 4 for optional engines and conversions to other models) Engine Continental A-65-8 (see item 115 for Lycoming O-235-C) Fuel 73 minimum grade aviation gasoline Engine Limits For all operations, 2300 r.p.m. (65 hp.) Airspeed Limits Level flight or clim b 95 m.p.h. (83 knots) True Ind. Glide or dive 129 m.p.h. (112 knots) True Ind. Propeller Limits Static rpm at maximum permissible throttle setting: (For fixed pitch Not over 2250, not under 1960. No additional tolerance permitted. wood propeller) Diameter: not over 72 in., not under 70 in. C.G. Range (+10.9) to (+21.5) Empty wt. C.G. Range (+14.1) to (+17.9) standard arrangement (+14.1) to (+15.0) when item 106(a) installed. When empty weight C.G. falls within the range given, it is not necessary to compute critical fore and aft C.G. positions. This range valid for standard arrangement only. Maximum Weight 1220 lb. No. of Seats 2 (1 at +11.5, 1 at +42) Maximum Baggage 40 lbs. at +64. See NOTE 2 for baggage placard. Fuel Capacity 13 gal. at -15. Oil Capacity 4 qt. at -33. A-759 Page 2 of 37 Control Surface Movements Elevator Up 25 o Down 15.5 o Elevator Trim Tab Up 20 o Down 34.5 o Ailerons Up 28.5 o Down 18 o Rudder Right 24 o Left 25 o Serial Nos. Eligible 7AC-1 and up. Required Equipment Items 1, 101, 102, 201, 202. II - Model S7AC, 2 PCSM (Normal Category), Approved February 27, 1947 (Same as 7AC except for float installation) Engine Continental A-65-8 Fuel 80 minimum grade aviation gasoline Engine Limits For all operations, 2300 r.p.m. (65 hp.) Airspeed Limits Level flight or clim b 90 m.p.h. (78 knots) True Ind. Glide or dive 121 m.p.h. (105 knots) True Ind. Propeller Limits Static rpm at maximum permissible throttle setting: (For fixed pitch Not over 2200, not under 1960. No additional tolerance permitted. propeller) Diameter: not over 76 in., not under 70 in. C.G. Range (+10.9) to (+19.5) Empty wt. C.G. Range (+13.6) to (+15.7) not valid when item 106(a) installed. When empty weight C.G. falls within this range, it is not necessary to compute critical fore and aft C.G. positions. This range valid for standard arrangement only. Maximum Weight 1320 lb. No. of Seats 2 (1 at +11.5, 1 at +42) Maximum Baggage 40 lbs. at +64. See NOTE 2 for baggage placard. Fuel Capacity 13 gal. at -15. Oil Capacity 4 qt. at -33. Control Surface Movements Elevator Up 25 o Down 15.5 o Elevator Trim Tab Up 20 o Down 34.5 o Ailerons Up 28.5 o Down 18 o Rudder Right 24 o Left 25 o Serial Nos. Eligible 7AC-1 and up. Required Equipment Items 1, 101, 102, 204(a) or (b), 205(a), 205(c) III - Model 7BCM (Army L-16A), 2 PCLM (N ormal Category), Approved September 16, 1947 Same as 7AC except for powerplant installation. See NOTE 4 for conversion from Model 7AC. Engine Continental C-85-8, -8F, -8J or -8FJ Fuel 80 minimum grade aviation gasoline Engine Limits For all operations, 2575 r.p.m. (85 hp.) Airspeed Limits Level flight or clim b 95 m.p.h. (83 knots) True Ind. Glide or dive 129 m.p.h. (112 knots) True Ind. Propeller Limits Static rpm at maximum permissible throttle setting: (For fixed pitch Not over 2450, not under 2200. No additional tolerance permitted. wood propeller) Diameter: not over 72 in., not under 70 in. C.G. Range (+10.4) to (+19.7) Empty wt. C.G. Range (+13.2) to (+15.5) valid only for standard arrangement. When empty weight C.G. falls within this range, it is not necessary to compute critical fore and aft C.G. positions. Maximum Weight 1220 lb. No. of Seats 2 (1 at +11.5, 1 at +42). Placard: "Solo from front seat only." Maximum Baggage 50 lbs. at +64. A-759 Page 3 of 37 Fuel Capacity 13 gal. at -15. Oil Capacity 4 qt. at -33. Control Surface Movements Elevator Up 27 o Down 21.5 o Elevator Trim Tab Up 20 o Down 34.5 o Ailerons Up 28.5 o Down 18 o Rudder Right 24 o Left 25 o Serial Nos. Eligible 7BCM-1 and up. Also, see NOTE 5 for military S/N's eligible. Required Equipment Carburetor engine: 1, 102, 105, 201, 202. (Items) Injector engine: 1, 110, 201, 202. IV - Model 7CCM (Army L-16B), 2 PCLM (Normal Category), Approved July 12, 1948 Same as 7BCM except for powerplant installati on, increased fin area, auxiliary fuel wing tank and fuselage member changed. See NOTE 4 for conversion from Model 7AC. Engine Continental C90-8F or C90-8FJ Fuel 80 minimum grade aviation gasoline Engine Limits For all operations, 2475 r.p.m. (90 hp.) Airspeed Limits Level flight or clim b 100 m.p.h. ( 87 knots) True Ind. Glide or dive 135 m.p.h. (117 knots) True Ind. Propeller Limits Static rpm at maximum permissible throttle setting: (For fixed pitch Not over 2410, not under 2170. No additional tolerance permitted. wood propeller) Diameter: not over 72 in., not under 70 in. C.G. Range (+16.8) to (+20.0) at 1300 lb. (+10.0) to (+20.0) at 1087 lb. or less Straight line variation between points given. Empty wt. C.G. Range None Maximum Weight 1300 lb. May be increased to 1350 lb. when "Long Stroke Oleo Landing Gear", Aeronca P/N 3-665, installed and placar d, "Intentional spinning prohibited when baggage carried", Aeronca P/N 1-2929, installed on instrument panel. C.G. range at 1350 lb. is as follows: (+16.8) to (+20.4) at 1350 lb. (+10.0) to (+20.4) at 1087 lb. or less Straight line variation between points given. No. of Seats 2 (1 at +11.5, 1 at +42). Placard: "Solo from front seat only." Maximum Baggage 50 lbs. at +64. Fuel Capacity 18.5 gal. (13 gal. at -15, 5.5 gal. at +24). Oil Capacity 5 qt. at -33. Control Surface Movements Elevator Up 24 o Down 24 o Elevator Trim Tab Up 17.5 o Down 37.5 o Ailerons Up 28.5 o Down 18 o Rudder Right 25 o Left 25 o Serial Nos. Eligible 7CCM-1 and up. Also, see NOTE 5 for military S/N's eligible. Required Equipment With Continental C 90-8F engine: 1, 102, 105, 106, 109, 201, 202. (Items) With Continental C90-8FJ engine: 1, 106, 110, 201, 202. V - Model 7DC, 2 PCLM (Normal Category), Approved July 12, 1948 Same as 7CCM except for powerplant installation. See NOTE 4 for conversion from Model 7AC. Engine Continental C-85-8, -8F, -8J, or -8FJ Fuel 80 minimum grade aviation gasoline Engine Limits For all operations, 2575 r.p.m. (85 hp.) Airspeed Limits Level flight or clim b 100 m.p.h. ( 87 knots) True Ind. Glide or dive 135 m.p.h. (117 knots) True Ind. Propeller Limits Static rpm at maximum permissible throttle setting: (For fixed pitch Not over 2465, not under 2300. No additional tolerance permitted. wood propeller) Diameter: not over 72 in., not under 70 in. A-759 Page 4 of 37 C.G. Range (+16.8) to (+20.0) at 1300 lb. (+10.0) to (+20.0) at 1087 lb. or less Straight line variation between points given. Empty wt. C.G. Range None Maximum Weight 1300 lb. May be increased to 1350 lb. when "Long Stroke Oleo Landing Gear", Aeronca P/N 3-665, installed and placar d, "Intentional spinning prohibited when baggage carried", Aeronca P/N 1-2929, installed on instrument panel. C.G. range at 1350 lb. is as follows: (+16.8) to (+20.4) at 1350 lb. (+10.0) to (+20.4) at 1087 lb. or less Straight line variation between points given. No. of Seats 2 (1 at +11.5, 1 at +42). Placard: "Solo from front seat only." Maximum Baggage 50 lbs. at +64. Fuel Capacity 18.5 gal. (13 gal. at -15, 5.5 gal. at +24). Oil Capacity 5 qt. at -33. Control Surface Movements Elevator Up 24 o Down 24 o Elevator Trim Tab Up 17.5 o Down 37.5 o Ailerons Up 28.5 o Down 18 o Rudder Right 25 o Left 25 o Serial Nos. Eligible 7DC-1 and up. Required Equipment With carburetor engine: 1, 102, 105, 201, 202. (Items) With injector engine: 1, 110, 201, 202. VI - Model S7DC, 2 PCSM (Normal Category), Approved September 22, 1948 Same as 7DC except for increase in maximum we ight, float and auxiliary ventral fin installation. Engine Continental C-85-8F Fuel 80 minimum grade aviation gasoline Engine Limits For all operations, 2575 r.p.m. (85 hp.) Airspeed Limits Level flight or climb 95 m.p.h. ( 83 knots) True Ind. Glide or dive 129 m.p.h. (112 knots) True Ind. Propeller Limits Static rpm at maximum permissible throttle setting: (For fixed pitch Not over 2440, not under 2290. No additional tolerance permitted. wood propeller) Diameter: not over 72 in., not under 70 in. C.G. Range (+16.8) to (+20.3) at 1400 lb. (+10.4) to (+20.3) at 1189 lb. or less Straight line variation between points given. Empty wt. C.G. Range None Maximum Weight 1400 lb. No. of Seats 2 (1 at +11.5, 1 at +43). Placard: "Solo from front seat only." Maximum Baggage 50 lbs. at +64. Fuel Capacity 18.5 gal. (13 gal. at -15, 5.5 gal. at +24). Oil Capacity 5 qt. at -33. Control Surface Movements Elevator Up 27 o Down 21.5 o Elevator Trim Tab Up 17.5 o Down 37.5 o Ailerons Up 28.5 o Down 18 o Rudder Right 25 o Left 25 o Serial Nos. Eligible 7DC-1 and up. Required Equipment Items 1, 102, 105, 204(b), 205(a), 205(c). A-759 Page 5 of 37 VII - Model S7CCM, 2 PCSM (Normal Category), Approved March 15, 1949 Same as 7CCM except for increase in maximum we ight, float and auxiliary ventral fin linstallation. Engine Continental C90-8F or C90-8FJ Fuel 80 minimum grade aviation gasoline Engine Limits For all operations, 2475 r.p.m. (90 hp.) Airspeed Limits Level flight or climb 95 m.p.h. ( 83 knots) True Ind. Glide or dive 129 m.p.h. (112 knots) True Ind. Propeller Limits Static rpm at maximum permissible throttle setting: (For fixed pitch Not over 2410, not under 2170. No additional tolerance permitted. wood propeller) Diameter: not over 72 in., not under 70 in. C.G. Range (+16.8) to (+20.3) at 1400 lb. (+10.4) to (+20.3) at 1189 lb. or less Straight line variation between points given. Empty wt. C.G. Range None Maximum Weight 1400 lb. No. of Seats 2 (1 at +11.5, 1 at +42). Placard: "Solo from front seat only." Maximum Baggage 50 lbs. at +64. Fuel Capacity 18.5 gal. (13 gal. at -15, 5.5 gal. at +24). Oil Capacity 5 qt. at -33. Control Surface Movements Elevator Up 24 o Down 24 o Elevator Trim Tab Up 17.5 o Down 37.5 o Ailerons Up 28.5 o Down 18 o Rudder Right 25 o Left 25 o Serial Nos. Eligible 7CCM-1 and up. Also, see NOTE 5 for military S/N's eligible. Required Equipment With Continental C90-8F engine: 1, 102, 105, 106, 109, 204(b), 205(a), 205(c). (Items) With Continental C90-8FJ engine: 1, 106, 110, 204(b), 205(a), 205(c). VIII - Model 7EC, 2 PCLM (Normal Category), Approved November 30, 1949 See Note 8 for conversion from Model 7JC. See Note 16 for alternate engine and weight configuration. Engine Continental C90-12F or C90-12FJ Fuel 80 minimum grade aviation gasoline Engine Limits For all operations, 2475 r.p.m. (90 hp.) Airspeed Limits Level flight or clim b 100 m.p.h. ( 87 knots) True Ind. Glide or dive 135 m.p.h. (117 knots) True Ind. Propeller Limits Static rpm at maximum permissible throttle setting: (For fixed pitch Not over 2350, not under 2125. No additional tolerance permitted. wood propeller) Diameter: not over 72 in., not under 70 in. C.G. Range (+15.0) to (+19.2) at 1450 lb. (+10.2) to (+19.2) at 1190 lb. or less Straight line variation between points given. Placard: "Intentional spi nning prohibited when carrying baggage." Empty wt. C.G. Range None Maximum Weight 1450 lb. 1300 lb. (If lower end landing gear oleo strut aaembl y, Aeronca dwg. 3-433, is installed). C.G. range at 1300 lb. is as follows: (+16.8) to (+19.2) at 1300 lb. (+10.2) to (+19.2) at 1100 lb. or less Straight line variation between points given. 1500 lb. (S/N's 7EC-705 and up eligible) C.G. range at 1500 lb. is as follows: (+15.0) to (+19.2) at 1500 lb. (+10.2) to (+19.2) at 1190 lb. or less Straight line variation between points given. No. of Seats 2 (1 at +11.5, 1 at +42). Placard: "Solo from front seat only." Maximum Baggage 50 lbs. at +64. A-759 Page 6 of 37 Fuel Capacity 18.5 gal. (13 gal. at -15, 5.5 gal. at +24). See item 116 for optional fuel systems. Oil Capacity 5 qt. at -33. Control Surface Movements Elevator Up 24 o Down 24 o Elevator Trim Tab Up 17.5 o Down 37.5 o Ailerons Up 28.5 o Down 18 o Rudder Right 25 o Left 25 o Serial Nos. Eligible 1 and up. Required Equipment With Continental C90-12F engine: 1, 102, 105, 109, 201, 202. (Items) With Continental C90-12FJ engine: 1, 106, 110, 201, 202. IX - Model S7EC, 2 PCSM (Normal Category), Approved May 12, 1950 Same as 7EC except for increase in maximum we ight, float and auxiliary ventral fin linstallation. Engine Continental C90-12F or C90-12FJ Fuel 80 minimum grade aviation gasoline Engine Limits For all operations, 2475 r.p.m. (90 hp.) Airspeed Limits Level flight or climb 95 m.p.h. ( 83 knots) True Ind. Glide or dive 129 m.p.h. (112 knots) True Ind. C.G. Range (+15.0) to (+18.6) at 1474 lb. (+10.4) to (+18.6) at 1258 lb. or less Straight line variation between points given. Placard: "Intentional spi nning prohibited when carrying baggage." Empty wt. C.G. Range None Maximum Weight 1474 lb. No. of Seats 2 (1 at +11.5, 1 at +42). Placard: "Solo from front seat only." Maximum Baggage 50 lbs. at +64. Fuel Capacity 18.5 gal. (13 gal. at -15, 5.5 gal. at +24). See item 116 for optional fuel systems. Oil Capacity 5 qt. at -33. Control Surface Movements Elevator Up 24 o Down 24 o Elevator Trim Tab Up 17.5 o Down 37.5 o Ailerons Up 28.5 o Down 18 o Rudder Right 25 o Left 25 o Serial Nos. Eligible 1 and up. Required Equipment With Continental C90-12F engine: 6, 102, 105, 106, 109, 112, 204(b), 205(a). (Items) With Continental C90-12FJ engine: 6, 106, 110, 112, 204(b), 205(a). X - Model 7FC, 2 PCLM (Normal Category), Approved March 27, 1957 See Note 7 for conversion to Wide Track Main Gear Engine Continental C90-12F or C90-12FJ Fuel 80 minimum grade aviation gasoline Engine Limits For all operations, 2475 r.p.m. (90 hp.) Airspeed Limits Level flight or clim b 100 m.p.h. ( 87 knots) True Ind. Glide or dive 135 m.p.h. (117 knots) True Ind. Propeller Limits Static rpm at maximum permissible throttle setting: (For fixed pitch Not over 2350, not under 2125. No additional tolerance permitted. wood propeller) Diameter: not over 72 in., not under 70 in. C.G. Range (+15.0) to (+17.2) at 1450 lb. (+10.2) to (+17.2) at 1190 lb. or less Straight line variation between points given. Placard: "Intentional spi nning prohibited when carrying baggage." Empty wt. C.G. Range None A-759 Page 7 of 37 Maximum Weight 1450 lb. (S/N's 7FC-2 thru 7FC-405) 1500 lb. (S/N's 7FC-406 and up when Champion 7-1159 Wide Track Main Gear installed. S/N's 7FC-347 thru 7FC-405 eligible for 1500 lb. maximum weight when modified in accordance with Cham pion Service Letters Nos. 45 and 46) C.G. range at 1500 lb. is as follows: (+15.0) to (+18.5) at 1500 lb. (+10.2) to (+18.5) at 1190 lb. or less Straight line variation between points given. No. of Seats 2 (1 at +11.5, 1 at +42). Placard: "Solo from front seat only." Maximum Baggage 50 lbs. at +64. Fuel Capacity 26 gal. (two 13 gal. wing tanks +24) Oil Capacity 5 qt. at -35. Control Surface Movements Elevator Up 24 o Down 24 o Elevator Trim Tab Up 17.5 o Down 37.5 o (1500 lb. max. wt. only) Elevator Trim Tab Up 17.5 o Down 44 o Ailerons Up 28.5 o Down 18 o Rudder Right 25 o Left 25 o Serial Nos. Eligible 2 and up. Required Equipment With Continental C90-12F engine: 1, 102, 103, 105, 116, 201(b) or (d). (Items) (201(e) and 210(b) also required for 1500 lb. maximum weight). With Continental C90-12FJ engine: 1, 110, 116, 201(b) or (d). (201(e) and 210(b) also required for 1500 lb. maximum weight). XI - Model 7GC, 2 PCL-SM (Normal Category), Approved October 3, 1958 Model 7GC is generally similar to 7EC except for modified fuselage structure as required for increase in gross weight and installation of Lycoming O-290-D2B engine and revised fuel system. Engine Lycoming O-290-D2B Fuel 80 minimum grade aviation gasoline Engine Limits Takeoff (one minute) 2800 r.p.m. (140 hp.) Maximum continuous 2600 r.p.m. (135 hp.) Airspeed Limits Landplane: Level flight or climb 120 m.p.h. (104 knots) True Ind. Glide or dive 162 m.p.h. (141 knots) True Ind. Seaplane with item 204(c) installed: Level flight or climb 120 m.p.h. (104 knots) True Ind. Glide or dive 137 m.p.h. (119 knots) True Ind. C.G. Range Landplane: (+14.2) to (+17.7) at 1650 lb. (+10.2) to (+17.7) at 1230 lb. or less Seaplane: (+14.45) to (+17.7) at 1732 lb. (+11.9) to (+17.7) at 1450 lb. or less Straight line variation between points given. Empty wt. C.G. Range None Maximum Weight Landplane: 1650 lb. Seaplane: 1732 lb. No. of Seats 2 (1 at +12, 1 at +42). Maximum Baggage 50 lbs. at +64.5 Fuel Capacity 39 gal. at +24.5 Oil Capacity 8 qt. at -36 Control Surface Movements Elevator Up 24 o Down 24 o Elevator Trim Tab Up 17.5 o Down 37.5 o Ailerons Up 27.5 o Down 19 o Rudder Right 25 o Left 25 o Serial Nos. Eligible 2 and up. Required Equipment Landplane: 11(a), 102(c) or (d), 118(a) or (b), 119, 120(a) or (b), 201(b), 202(f). (Items) Seaplane: 11(a), 102(c) or (d), 118(a) or (b), 119, 120(a) or (b), 204(c), 205(a), 205(c) A-759 Page 8 of 37 XII - Model 7HC, 3 PCL-SM (Normal Category), Approved August 6, 1959 Model 7HC is generally similar to the 7GC except for modified fuselage structure as required for additional rear seat capacity, tricycle type gear and control wheel type system in front seat. See NOTE 9 for conversion to Wide Track Main Gear. Engine Lycoming O-290-D2B Fuel 80 minimum grade aviation gasoline Engine Limits Takeoff (one minute) 2800 r.p.m. (140 hp.) Maximum continuous 2600 r.p.m. (135 hp.) Airspeed Limits Landplane: Level flight or climb 120 m.p.h. (104 knots) True Ind. Glide or dive 162 m.p.h. (141 knots) True Ind. Seaplane with item 204(c) installed: Level flight or climb 120 m.p.h. (104 knots) True Ind. Glide or dive 137 m.p.h. (119 knots) True Ind. C.G. Range Landplane: (+14.2) to (+17.7) at 1650 lb. (+10.4) to (+17.7) at 1250 lb. or less Seaplane: (+14.45) to (+17.7) at 1732 lb. (+11.9) to (+17.7) at 1450 lb. or less Straight line variation between points given. Empty wt. C.G. Range None Maximum Weight Landplane: 1650 lb. Seaplane: 1732 lb. No. of Seats 3 (front adjustable from +13.5 to +14.5, rear adjustable from +44 to +51). Maximum Baggage 50 lbs. at +64.5 Fuel Capacity 39 gal. at +24.5 Oil Capacity 8 qt. at -36 Control Surface Movements Elevator Up 24 o Down 24 o Elevator Trim Tab Up 17.5 o Down 37.5 o Ailerons Up 27.5 o Down 19 o Rudder Right 25 o Left 25 o Serial Nos. Eligible 2 and up. Required Equipment Landplane: (S/N's 7HC-1 thru 7 HC-32), 11(a), 102(c) or (d), 118(a) or (b), 119, (Items) 120(a) or (b), 201(b), 209 (see NOTE 9). (S/N's 7HC-33 and up), 11(a), 102( c) or (d), 118(a) or (b), 119, 120(a), 201(e), 209, 210(b) Seaplane: 11(a), 102(c) or (d), 118(a) or (b), 119, 120(a) or (b), 204(c), 205(a), 205(c). XIII - Model 7GCA, 2 PCLM (Normal Category), Approved November 17, 1959 Model 7GCA is generally similar to the 7GC except for modifications as required for installation of Lycoming O-320-A2B engine) Engine Lycoming O-320-A2B Fuel 80/87 minimum grade aviation gasoline Engine Limits For all operations, 2700 r.p.m. (150 hp.) Airspeed Limits Level flight or c limb 120 m.p.h. (104 knots) True Ind. Glide or dive 162 m.p.h. (141 knots) True Ind. C.G. Range (+14.2) to (+17.7) at 1650 lb. (+10.2) to (+17.7) at 1230 lb. or less Straight line variation between points given. Empty wt. C.G. Range None Maximum Weight 1650 lb. No. of Seats 2 (front adjustable from +13.5 to +14.5, rear at +44) Maximum Baggage 50 lbs. at +64.5 Fuel Capacity 39 gal. at +24.5 Oil Capacity 8 qt. at -36 A-759 Page 9 of 37 Control Surface Movements Elevator Up 24 o Down 24 o Elevator Trim Tab Up 17.5 o Down 37.5 o Ailerons Up 27.5 o Down 19 o Rudder Right 25 o Left 25 o Serial Nos. Eligible 120 and up. Required Equipment Items 11(b), 102(c) or (d), 118(a) or (b), 119, 120(a) or (b), 201(a) or (b), 202(f) XIV - Model 7JC, 2 PCLM (Normal Category), Approved February 24, 1960 Model 7JC is generally similar to the 7EC except for modified fuselage structure as required for installation of tricycle gear with single gear a ft. See Note 8 for conversion to Model 7EC. Engine Continental C90-12F Fuel 80/87 minimum grade aviation gasoline Engine Limits For all operations, 2475 r.p.m. (90 hp.) Airspeed Limits Level flight or clim b 100 m.p.h. ( 87 knots) True Ind. Glide or dive 135 m.p.h. (117 knots) True Ind. Propeller Limits Static rpm at maximum permissible throttle setting: (For fixed pitch Not over 2350, not under 2125. No additional tolerance permitted. wood propeller) Diameter: not over 72 in., not under 70 in. C.G. Range (+15.5) to (+19.2) at 1450 lb. (+11.3) to (+19.2) at 1200 lb. or less Straight line variation between points given. Empty wt. C.G. Range None Maximum Weight 1450 lb. No. of Seats 2 (front adjustable from +11.3 to +13.3, rear at +39.7) Maximum Baggage 50 lbs. at +64. Fuel Capacity 26 gal. (two 13 gal. wing tanks at +24) Oil Capacity 5 qt. at -35. Control Surface Movements Elevator Up 24 o Down 24 o Elevator Trim Tab Up 17.5 o Down 37.5 o Ailerons Up 28.5 o Down 18 o Rudder Right 25 o Left 25 o Serial Nos. Eligible 1 and up. Required Equipment Items 1, 102(b), 103(b), 105, 116, 201(b), 211 XV - Model 7GCB, 2 PCL-SM (Normal Category), Approved April 28, 1960 For operation in the acrobatic category, see NOTES 2(b)(12) and 10. Model 7GCB is generally similar to the 7GCA except for modified wing and fuselage structure as required for addition of wing flaps, increased wing area and increased rear seat weight limit. Engine Lycoming O-320-A2B Fuel 80/87 minimum grade aviation gasoline Engine Limits For all operations 2700 r.p.m. (150 hp.) Airspeed Limits Landplane: Level flight or climb 120 m.p.h. (104 knots) True Ind. Glide or dive 162 m.p.h. (141 knots) True Ind. Flaps extended 90 m.p.h. ( 78 knots) True Ind. Seaplane with item 204(c) installed: Level flight or climb 120 m.p.h. (104 knots) True Ind. Glide or dive 137 m.p.h. (119 knots) True Ind. Flaps extended 90 m.p.h. ( 78 knots) True Ind. C.G. Range Landplane: (+15.0) to (+19.2) at 1650 lb. (+12.26) to (+19.2) at 1325 lb. or less Seaplane: (+16.2) to (+19.2) at 1732 lb. (+13.0) to (+19.2) at 1500 lb. or less When performing acrobatic maneuvers, the C.G. range shall be limited to: (+15.0) to (+17.1) at 1650 lb. (+12.26) to (+17.1) at 1325 lb. or less A-759 Page 10 of 37 With increased flap travel (Champi on Installation dwg. No. 7-1131) and installation of horizontal tail surface per Champion dwg. No. 4-1410, 4-1411 and 4-1412: Landplane: (+14.2) to (+19.2) at 1732 lb. (+10.5) to (+19.2) at 1325 lb. or less When performing acrobatic maneuvers, the C.G. range shall be limited to: (+14.2) to (+17.1) at 1650 lb. (+10.5) to (+17.1) at 1325 lb. or less Straight line variation between points given. Empty wt. C.G. Range None Maximum Weight Landplane: 1650 lb. Seaplane: 1732 lb. No. of Seats 2 (front adjustable from +13.5 to +14.5, rear fixed seat at +42.5, or rear adjustable from +44 to +51). (This rear seat limit is 250 lb.) Maximum Baggage 50 lbs. at +64.5 Fuel Capacity 39 gal. at +24.5 Oil Capacity 8 qt. at -36 Control Surface Movements Elevator Up 28 o Down 24 o Elevator Trim Tab Up 17.5 o Down 44 o Ailerons Up 27.5 o Down 19 o Flaps Up 0 o Down 21 o (with flap control system installed per Champion dwg. 7-1131 and horizontal tail surfaces per Champion dwg. 4-1410, 4-1411, 4-1412) Up 0 o Down 35 o Rudder Right 25 o Left 25 o Serial Nos. Eligible 1 and up. Required Equipment Landplane: 11(b), 102(d) , 118(b), 119, 120(b), 201(a) or (b), 202 (Items) Seaplane: 11(b), 102(d), 118(b), 119, 120(b), 204(c), 205(a) and (c) or (c) and (d) XVI - Model 7KC, 2 PCLM (Normal Category), Approved January 10, 1961 Model 7KC is generally similar to the 7GCA exc ept for modifications as required for reduced wing area, minor fairing, cabin interior c hanges and controls in front seat only) Engine Lycoming O-320-A2B Fuel 80/87 minimum grade aviation gasoline Engine Limits For all operations, 2700 r.p.m. (150 hp.) Airspeed Limits Level flight or c limb 120 m.p.h. (104 knots) True Ind. Glide or dive 162 m.p.h. (141 knots) True Ind. C.G. Range (+14.2) to (+18.6) at 1650 lb. (+11.9) to (+18.6) at 1406 lb. or less Straight line variation between points given. Empty wt. C.G. Range None Maximum Weight 1650 lb. No. of Seats 2 (front adjustable from +12.6 to +13.8, rear adjustable from +41.8 to +43) Maximum Baggage 50 lbs. at +64.5 Fuel Capacity 39 gal. at +24.5 Oil Capacity 8 qt. at -36 Control Surface Movements Elevator Up 28 o Down 24 o Elevator Trim Tab Up 17.5 o Down 44 o Ailerons Up 27.5 o Down 19 o Rudder Right 25 o Left 25 o Serial Nos. Eligible 1 and up. Required Equipment Items 11(b), 102(d) , 118(b), 119, 120(b), 201(a) or (b), 202 A-759 Page 11 of 37 A-759 Page 12 of 37 XVII - Model 7GCBA, 2 PCLM (Restricted Agricu ltural Category Only), Approved February 2, 1962 Engine Lycoming O-320-A2B Fuel 80/87 minimum grade aviation gasoline Engine Limits For all operations, 2700 r.p.m. (150 hp.) Airspeed Limits Level flight or c limb 115 m.p.h. (100 knots) True Ind. Glide or dive 121 m.p.h. (105 knots) True Ind. Flaps extended 90 m.p.h. ( 78 knots) True Ind. C.G. Range (+15.0) to (+22.5) at 2400 lb. (+10.5) to (+22.5) at 1325 lb. or less Straight line variation between points given. Empty wt. C.G. Range None Maximum Weight 2400 lb. Any increase in maximum weight to be determined in accordance with CAM 8.10-3(e) No. of Seats 1 at +12 Maximum Baggage None Hopper Load Maximum structural compliance wi th CAM 8 is 900 lb. (see NOTE 2(e)). Fuel Capacity 39 gal. at +24.5 Oil Capacity 8 qt. at -36 Control Surface Movements Elevator Up 28 o Down 24 o Elevator Trim Tab Up 17.5 o Down 44 o Ailerons Up 27.5 o Down 19 o Flaps Up 0 o Down 21 o Rudder Right 25 o Left 25 o Serial Nos. Eligible 1 and up. Required Equipment Items 11(b), 102(d), 118(b), 119, 120(b), 201(b), 202 and 620(a), (b), (c) or (d) XVIII - Model 7ECA, 2 PCL-SM (Normal or Acrobatic Category), Approved August 5, 1964 For operation in the Acrobatic Category, see NO TES 2(b)(13) and 10. Model 7ECA is generally similar to the 7GC except for modifications required for installation of the approved engines and modified vertical tail assembly, windshield contour , rear seat windows and wide track main gear. See Item 621 for applicable horizontal tail surfaces. See NO TE 15 concerning optional C.G. range and maximum weight. Engine Continental O-200-A (see Ite m 122, 124 and 125 for optional engines) Fuel 80/87 minimum grade aviation gasoline Engine Limits For all operations, 2750 r.p.m. (100 hp.) Airspeed Limits Landplane: Level flight or climb 120 m.p.h. (104 knots) True Ind. Glide or dive 162 m.p.h. (141 knots) True Ind. Seaplane with Item 204(c) installed: Level flight or climb 114 m.p.h. ( 99 knots) True Ind. Glide or dive 137 m.p.h. (119 knots) True Ind. C.G. Range Landplane: (+14.2) to (+19.2) at 1650 lb. (+10.2) to (+19.2) at 1325 lb. or less When performing acrobatic maneuvers, the C.G. range shall be limited to: (+14.2) to (+17.3) at 1650 lb. (+10.5) to (+17.3) at 1325 lb. or less Seaplane: (+14.2) to (+19.2) at 1732 lb. (+10.5) to (+19.2) at 1407 lb. or less Straight line variation between points given. (See NOTE 15 for optional CG Range) Empty wt. C.G. Range None Maximum Weight Landplane: 1650 lb. (S ee NOTE 15 for optional weight) Seaplane: 1732 lb. No. of Seats 2 (1 at +12, 1 at +42) 2 (1 at +11 to +14 with Item 404(n), 1 at +43 with Item 404(o) or (p)) Maximum Baggage 100 lbs. at +69 A-759 Page 13 of 37 Fuel Capacity 39 gal. at +24.5 (Item 119) 36 gal. at +24.5 (Item 123(a)) (see NOTE 1 for Weight of Unusable fuel) Oil Capacity 6 qt. at -44 Control Surface Movements Elevator Up 24 o Down 24 o Elevator Trim Tab Up 17.5 o Down 37.5 o Ailerons Up 27.5 o Down 19 o Rudder Right 25 o Left 25 o Serial Nos. Eligible 1 thru 722, 725, 723-70, 724-70, 726-70 thru 785-70, 786-71 thru 792-71, 794-71 thru 812-71, 793-72, 813-72 thru 888-72, 889-73 thru 984-73, 985-74 thru 1059-74, 1060-75 thru 1125-75, 1126-76 thru 1180-76, 1181-77 thru 1223-77, 1224-78 thru 1278-78, 1279-79 thru 1328-79, 1329-80 thru 1352-80, 1353-84, 1355-95 and up. Required Equipment Landplane: 15(a), 102(e), 103(e) or (i), 117(d), 116 or 119 or 123(a), 201(d) or (Items) (h) or (i) or (l), 202 Seaplane: 15(a), 102(e), 103(e) or (i), 117(d), 116 or 119 or 123(a), 204(c), 205(a) or 205(d). XIX - Model 7GCAA, 2 PCLM (Normal or Acrobatic Category), Approved July 30, 1965 For operation in the Acrobatic Category, see NO TES 2(b)(13) and 10. Model 7GCAA is generally similar to the 7ECA except for the installati on of the Model 7GCB engine mount and engine, revised cowling and minor equipment and trim changes. S ee NOTE 15 concerning optional C.G. range and maximum weight. Engine Lycoming O-320-A2B or O-320-C2B or O-320-A2D (see Item 125 and 126 for optional engines) Fuel 80/87 minimum grade aviation gasoline Engine Limits For all operations, 2700 r.p.m. (150 hp.) Airspeed Limits Level flight or c limb 120 m.p.h. (104 knots) True Ind. Glide or dive 162 m.p.h. (141 knots) True Ind. C.G. Range (+14.2) to (+18.2) at 1650 lb. (+10.5) to (+18.2) at 1325 lb. or less When performing acrobatic maneuvers, the C.G. range shall be limited to: (+14.2) to (+16.0) at 1650 lb. (+10.5) to (+16.0) at 1325 lb. or less Straight line variation between points given. (See NOTE 15 for optional CG Range) Empty wt. C.G. Range None Maximum Weight 1650 lb. (See NOTE 15 for optional weight) No. of Seats 2 (1 at +12, 1 at +42) 2 (1 at +11 to +14 with Item 404(n), 1 at +43 with Item 404(o) or (p)) Maximum Baggage 100 lbs. at +69 Fuel Capacity 39 gal. at +24.5 (Item 119) 36 gal. at +24.5 (Item 123(a)) (see NOTE 1 for Weight of Unusable fuel) Oil Capacity 8 qt. at -36 Control Surface Movements Elevator Up 28 o Down 24 o (with Items 404(d) (e) installed) Up 24 o Down 24 o Elevator Trim Tab Up 17.5 o Down 44 o Ailerons Up 27.5 o Down 19 o Rudder Right 25 o Left 25 o Serial Nos. Eligible 1 thru 198, 200 thru 204, 276, 205-70 thru 229-70, 199-71, 203-71, 231-72 thru 242-72, 244-72 thru 251-72, 243-73, 252-73 thru 275-73, 277-73 thru 279-73, 280-74 thru 304-74, 305-75 thru 323-75, 324-76 thru 334-76, 335-77 thru 348-77, 349-78 thru 370-78, 371-79 thru 389-79, 390-80 thru 396-80, 400-97 and up. Required Equipment Items 16(a) or 20(a), 102(i) or (j), 103(f), (h) or (i), 117(e), 118(c), 119 or 123(a), 201(d) or (h) or (i) or (l), 202 A-759 Page 14 of 37 A-759 Page 15 of 37 XX - Model 7GCBC, 2 PCL-SM (Normal or Ac robatic Category), Approved December 3, 1965 Model 7GCBC is generally similar to the 7GCAA exc ept for the installation of the Model 7GCB wings, wingstruts, and flap system. See Item 621 for applicable horizontal tail surfaces See NOTE 10 for Acrobatic Operation. See NOTE 13 for optional C. G. ranges and maximum weights. Engine Lycoming O-320-A2B or O-320-C2B or O-320-A2D (see Items 122, 125, 126, and 127 for optional engines) Fuel 80/87 minimum grade aviation gasoline Engine Limits For all operations, 2700 r.p.m. (150 hp.) (See NOTE 11 for additional limitations) Airspeed Limits Landplane: Level flight or climb 120 m.p.h. (104 knots) True Ind. Glide or dive 162 m.p.h. (141 knots) True Ind. Flaps extended 90 m.p.h. ( 78 knots) True Ind. Seaplane with Item 204(c) installed: Level flight or climb 114 m.p.h. ( 99 knots) CAS Glide or dive 137 m.p.h. (119 knots) CAS Flaps extended 90 m.p.h. ( 78 knots) CAS Seaplane with Item 204(d) installed: Level flight or climb 110 m.p.h. ( 92 knots) CAS Glide or dive 148 m.p.h. (128 knots) CAS Flaps extended 90 m.p.h. ( 78 knots) CAS C.G. Range Landplane: (+14.2) to (+19.2) at 1650 lb. (+10.5) to (+19.2) at 1325 lb. or less When performing acrobatic maneuvers, the C.G. range shall be limited to: (+14.2) to (+16.3) at 1650 lb. (+10.5) to (+16.3) at 1350 lb. or less Seaplane with Item 204(c) installed:: (+14.8) to (+19.2) at 1732 lb. (+11.5) to (+19.2) at 1500 lb. or less Seaplane with Item 204(d) installed:: (+13.8) to (+18.4) at 1800 lb. (+11.5) to (+18.4) at 1590 lb. or less Skiplane with Item 203(k) installed:: (+14.2) to (+16.8) at 1650 lb. (+10.5) to (+16.8) at 1325 lb. or less Skiplane with Item 203(l) installed:: (+14.2) to (+19.2) at 1650 lb. (+10.5) to (+19.2) at 1325 lb. or less Straight line variation between points given. (See NOTE 13 for optional CG Range) Empty wt. C.G. Range None Maximum Weight Landplane - Skiplane: 1650 lb . (See NOTE 13 for optional weight) Seaplane with Item 204(c): 1732 lb. Seaplane with Item 204(d): 1800 lb. No. of Seats 2 (1 at +12, 1 at +42) 2 (1 at +11 to +14 with Item 404(n), 1 at +43 with Item 404(o) or (p)) Maximum Baggage 100 lbs. at +69 Fuel Capacity 39 gal. at +24.5 (Item 119) 36 gal. at +24.5 (Item 123(a)) (see NOTE 1 for Weight of Unusable fuel) Oil Capacity 8 qt. at -36 Control Surface Elevator Up 28 o Down 24 o Movements with Item 404(d) and (e) Up 24 o Down 24 o Elevator Trim Tab Up 17.5 o Down 44 o Seaplane with Item 204(c) Up 12 o Down 44 o Ailerons Up 27.5 o Down 19 o Flaps Up 0 o Down 35 o Rudder Right 25 o Left 25 o Serial Nos. Eligible 1 thru 201, 205, 207, 202-70, 203-70, 204-70, 206-70, 208-70 thru 294-70, 295-71 thru 318-71, 319-72 thru 330-72, 332-72 thru 416-72, 331-73, 417-73 thru 603-73, 604-74 thru 773-74, 774-75 thru 886-75, 887-76 thru 956-76, 957-77 thru 1005-77, 1006-78 thru 1065-78, 1066-79 thru 1177-79, 1178-80 thru 1214-80, 1200-94 and up. A-759 Page 16 of 37 Required Equipment Landplane: 16(a) or 20(a), 102(f) or (j), 103(f), (h) or (i), 117(e), 118(c), 119 or (Items) 123(a), 201(d) or (h) or (i) or (l), 202 Seaplane: 16(a) or 18(a) or 19(a), 102( f) or (j), 103(f), (h) or (i), 117(e), 118(c), 119 or 123(a), 204(c) or (d), 205(d). Skiplane: 16(a) or 20(a), 102(f) or (j ), 103(f), (h) or (i), 117(e), 118(c), 119 or 123(a), 203(k) or (l). XXI - Model 7KCAB, 2 PCLM (Normal or Ac robatic Category), Approved December 21, 1966 For operation in the Acrobatic Category, see NO TES 2(b)(15) and 10. Model 7KCAB is generally similar to the 7GCAA except for the installation of fuel injected engine, revised fuel system and modified oil system for limited inverted operati on. See Item 621 for applicable horizontal tail surfaces. See NOTE 15 concerning optional C.G. range and maximum weight. Engine Lycoming IO-320-E2A or IO-320-E2B or AEIO-320-E2B (IO-320-E2A and -E2B must be modified per STC SE7CE) Fuel 80/87 minimum grade aviation gasoline Engine Limits For all operations, 2700 r.p.m. (150 hp.) Airspeed Limits Level flight or c limb 120 m.p.h. (104 knots) True Ind. Glide or dive 162 m.p.h. (141 knots) True Ind. C.G. Range (+14.2) to (+18.2) at 1650 lb. (+10.5) to (+18.2) at 1325 lb. or less When performing acrobatic maneuvers, the C.G. range shall be limited to: (+14.2) to (+16.0) at 1650 lb. (+10.5) to (+16.0) at 1325 lb. or less Straight line variation between points given. (See NOTE 15 for optional CG Range) Empty wt. C.G. Range None Maximum Weight 1650 lb. (See NOTE 15 for optional weight) No. of Seats 2 (1 at +12, 1 at +42) 2 (1 at +11 to +14 with Item 404(n), 1 at +43 with Item 404(o) or (p)) Maximum Baggage 100 lbs. at +69 Fuel Capacity 39 gal. at +24.5 (Item 119) 36 gal. at +24.5 (Item 123(a)) (see NOTE 1 for Weight of Unusable fuel) Oil Capacity 8 qt. at -36 Control Surface Elevator Up 28 o Down 24 o Movements Elevator Trim Tab Up 17.5 o Down 44 o Ailerons Up 27.5 o Down 19 o Rudder Right 25 o Left 25 o Serial Nos. Eligible 1 thru 208, 210 thru 226, 270, 271, 209-70, 227-70 thru 257-70, 266-70 thru 269-70, 272-70 thru 287-72, 258-71 thru 265-71, 288-71 thru 290-71, 291-72 thru 335-72, 336-73 thru 404-73, 405-74 thru 486-74, 487-75 thru 550-75, 551-76 thru 597-76, 598-77 thru 617-77. Required Equipment Items 16(a) or 20(a), 102(h) or (k), 103(f), (h) or (i), 117(g), 118(d), 119 or 123(a), 201(d) or (h) or (i) or (l), 202 XXII - Model 7ACA, 2 PCLM (Normal Category), Approved April 30, 1971 Engine Franklin 2A-120A or 2A-120B Fuel 100/120 minimum grade aviation gasoline Engine Limits For all operations, 3200 r.p.m. (60 hp.) Airspeed Limits Level flight or clim b 95 m.p.h. (83 knots) True Ind. Glide or dive 129 m.p.h. (112 knots) True Ind. Propeller Limits See Item 21 - Propeller and Propeller Accessories (For fixed pitch wood propeller) Diameter: not over 60 in., not under 58.5 in. C.G. Range (+10.9) to (+21.5) Empty wt. C.G. Range None Maximum Weight 1220 lb. A-759 Page 17 of 37 No. of Seats 2 (1 at +11.5, 1 at +42) Maximum Baggage 40 lbs. at +64. See NOTE 2(a)(4) for baggage placard. Fuel Capacity 13 gal. at -15. Oil Capacity 2.5 qt. at -46. Control Surface Elevator Up 25 o Down 15.5 o Movements Elevator Trim Tab Up 20 o Down 34.5 o Ailerons Up 28.5 o Down 18 o Rudder Right 24 o Left 25 o Serial Nos. Eligible 1-71 thru 23-71, 25-71 thru 28-71, 24-72, 29-72 thru 69-72, 70-73 and up. Required Equipment Items 21(a) or (b), 201(j) , (k) or (m), 202(b) or (c), 102(i), 103(g) Specifications Pertinent to All Models Datum Wing leading edge. Leveling Means Any portion of the cabin floor to level laterally and longitudinally. (Also see NOTE 6) Certification Basis 1) Part 4(a) of the Civil Ai r Regulations effective as amended to April 7, 1950, except paragraph 4a.532(m) (for all models except 7GCBA). 2) Paragraphs 23.25 and 23.959 of the Federal Aviation Regulations dated February 1, 1965 for Models 7ECA, 7GCAA, 7GCBC, and 7KCAB. 3) Part 8.10(b) of the Civil Air R egulations effective October 11, 1950 (Model 7GCBA); and FAR 36, appendix G for the Models 7ECA (with Lycoming O-235-K2C engine), 7GCAA, 7GCBC (S/N 1198-80 and up), and 7KCAB. 4) In addition to the Part 4a certific ation basis contained in first paragraph above, the model 7EC certification basis fo r serial numbers 1000-2006 & up includes the additional regulations below: FAR 23.961; 23.971; 23.1351 as amended by Amendment 23-6. FAR 23.21; 23.23; 23.25; 23.29; 23.45; 23.49; 23.51; 23.53; 23.63; 23.65; 23.69; 23.71; 23.73; 23.75; 23.77; 23.141; 23.143; 23.145; 23.147; 23.153; 23.155; 23.157; 23.161; 23.171; 23.173, 23.175; 23.177; 23.179; 23.181; 23.201; 23.203; 23.207; 23.221; 23.231; 23.233; 23.235; 23.251; 23.477; 23.479; 23.481; 23.483; 23.485; 23.493; 23.497; 23.901; 23.903; 23.905; 23.907; 23.925; 23.943; 23.951; 23.955; 23.957; 23.959; 23.963; 23.965; 23.967; 23.969; 23.973; 23.975; 23.977; 23.993; 23.995, 23.997; 23.999; 23.1041; 23.1043; 23.1047; 23.1123; 23.1301; 23.1303; 23.1305; 23.1321; 23.1323; 23.1325; 23.1327; 23.1337; 23.1353; 23.1357; 23.1359; 23.1361; 23.1365; 23.1367; 23.1381; 23.1385; 23.1387; 23.1389; 23.1391; 23.1393; 23.1395; 23.1397; 23.1401; 23.1431; 23.1529; 23.1581; 23.1583; 23.1585; 23.1587; 23.1589 as amended by Amendment 23-55. FAR 36 dated December 1, 1969, as amended by amendments 36-1 through 36-28. (for model 7EC S/N 1000-2006 & up) 5) In addition to the Part 4a certific ation basis contained in the first paragraph above and the Part 23 / Part 36 certific ation basis contained in the fourth papragraph above; the model 7EC certificat ion basis for thos e airplanes equipped with Teledyne Continental Motors model O-200-D engines; serial numbers 1029- 2009 & up includes the additi onal regulations below: FAR 23.1501; 23.1521; 23.1541; 23.1549; 23.1583 as amended by Amendment 23- 59. (For model 7EC equipped with TCM model O-200-D engine S/N 1029-2009 & up) 6) The certification basis for model 7GCBC, for acrobatic maneuvers, effective with serial number 1360 and up, and with engine option item 126; includes the certification basis contained in first two paragraphs above. In addition, the certification basis includes the regulations below: FAR 23.321, 23.331; 23.335, 23.369, 23.391, 23.395, 23.397, 23.399, 23.405, 23.407, 23.409, 23.415, 23.421, 23.423, 23.425, 23.427, 23.411, 23.443, 23.445, 23.457, 23.471, 23.473, 23.477, 23.479, 23.481, 23.483, 23.485, 23.493, 23.497 as amended by Amendment 23-6. FAR 23.21; 23.23; 23.25; 23.29; 23.45; 23.49; 23.51; 23.53; 23.63; 23.65; 23.69; 23.71; 23.73; 23.75; 23.77; 23.141; 23.143; 23.145; 23.147; 23.153; 23.155; 23.157; 23.161; 23.171; 23.173, 23.175; 23.177; 23.179; 23.181; 23.201; 23.203; 23.207; 23.221; 23.231; 23.233; 23.235; 23.251; 23.925; 23.1041; 23.1043; 23.1047; 23.1529; 23.1581; 23.1583; 23.1585; 23.1587; 23.1589 as amended by Amendment 23-55. FAR 36 dated December 1, 1969, as amended by amendments 36-1 through 36-28. A-759 Page 18 of 37 7) The certification basis for model 7GCB C, in the Normal category, effective with serial number 1360 and up, and with engi ne options item 126 and 127; includes the certification basis in the paragraph abov e with the exception of regulations 4a.75, 4a.76, and 4a.79 through 4a.93. In addition, the certification basis includes regulations: FAR 23.333, 23.337, 23.341, 23.345, 23.347, 23.349, 23.351 as amended by amendment 23-6. Approved Type Certificate No. 759 issued October 18, 1945. Production Basis American Champion Aircra ft Production Limitation Record 333CE, dated July 21, 1997. Production authorized Aug. 30, 1994 (7GCBC), Dec. 26, 1995 (7ECA), July 21, 1997 (7GCAA), and March 26, 2007 (7EC S/N 1000-2006 & up) Equipment A plus (+) or minus (-) sign preceding the weight of an optional item indicates the net weight change when that item is installed. Approval for the installation of all items of equipment listed herein has been obtained by the aircraft manufacturer except those items preceded by an asteri sk (*). This symbol denotes that approval has been obtained by someone other than the aircraft manufacturer. An item so marked may not have been manufactured under an FAA monitored or approved quality control system; and, theref ore, conformity must be determined if the item is not identified by a Form FAA-186, PMA, or other evidence of FAA production approval. Propeller and Propeller Accessories 1. Wood Propellers - fixed pitch Models 7AC, 7BCM, 7CCM, 7DC Models 7EC,7FC, 7JC 10 lb. (-52) (-54) (a) Sensenich 72C-44 (Models 7AC and S7AC) Sensenich 72CK (Model 7BCM) Sensenich 72CK-44, -45, -46 (Models 7DC, S7DC) Sensenich 72GK-48, -49, -50 (Models 7CCM, 7EC, S7CCM, 7FC, 7JC) (b) Flottorp 72A50, 52 (Models 7CCM, S7CCM, 7EC, 7FC, 7JC) (c) Any other approved fixed pitch wood pr opeller which is eligible for the engine power and speed and which meets the diameter and static r.p.m. limits specified under "Propeller Limi ts" for the pertinent model. 2. McCauley 1A90 with following limits: 26 lb. (-52) (a) (7AC and S7AC) Static r.p.m. at maximum permissible throttle setting: Not over 2250 (for 7AC), 2200 (for S7AC), not under 2100 (for 7AC or S7AC). No additional tolerance permitted. Diameter: not over 71 in., not under 69.5 in. (b) (7BCM only) Static r.p.m. at maximum permissible throttle setting: Not over 2450, not under 2350. No additional tolerance permitted. Diameter: not over 71 in., not under 69.5 in. (c) (7DC only) Static r.p.m. at maximum permissible throttle setting: Not over 2465, not under 2300. No additional tolerance permitted. Diameter: not over 71 in., not under 69.5 in. (d) (S7DC only) Static r.p.m. at maximum permissible throttle setting: Not over 2440, not under 2290. No additional tolerance permitted. Diameter: not over 74 in., not under 69.5 in. 3. Omitted. 4. Spinner (a) (Aeronca dwg. 4-710 and 4-711) Models 7EC and 7FC 7AC, 7BCM, 7CCM, 7DC 1 lb. 1 lb. (-61) (-49) (b) (Champion dwg. 4-10012) 7EC and 7FC 1 lb. (-61) (c) (Champion dwg. 4-1028) 7EC, 7FC, 7JC 7GC, 7HC, 7GCA, 7GCB, 7KC 2 lb. 2 lb. (-57) (-59) (d) (Champion dwg. 7-1252) 7ECA (with CMC O-200-A engine) 4 lb. (-61) (e) (Champion dwg. 3-1397) 7GCAA, 7GCBC, 7KCAB 4 lb. (-61) (f) (Champion dwg. 3-1408) 7ECA, 7GCBC (with Lycoming O-235-C1 engine) 4 lb. (-61) (g) (Champion dwg. 3-1618) 7ECA (with Lycoming O-235-K2C engine) 4 lb. (-61) 5. Hartzell ground adjustable propeller Hb Model HA-12U Blades 7414 to 6814 or 7214M to 6814M. Eligible at diameter and static r.p.m. limits shown for fixed pitch wood. 18 lb. (-52) 6. McCauley 1B90CM with following limitations: Models 7AC, 7BCM, 7CCM, 7DC Models 7EC,7FC, 7JC 21 lb. (-52) (-54) A-759 Page 19 of 37 (a) (Models 7CCM, S7CCM) Static r.p.m. at maximum permissible throttle setting: Not over 2410, not under 2150. No additional tolerance permitted. Diameter: not over 73 in., not under 71.5 in. (b) (Models 7EC, 7FC, 7JC) Static r.p.m. at maximum permissible throttle setting: Not over 2350, not under 2150. No additional tolerance permitted. Diameter: not over 73 in., not under 71.5 in. (c) (Model S7EC) Static r.p.m. at maximum permissible throttle setting: Not over 2400, not under 2300. No additional tolerance permitted. Diameter: not over 73 in., not under 71.5 in. (d) (Model 7AC) Static r.p.m. at maximum permissible throttle setting: Not over 2250, not under 2100. Diameter: not over 74 in., not under 72.5 in. (e) (Models 7BCM, 7DC) Static r.p.m. at maximum permissible throttle setting: Not over 2450, not under 2200. Diameter: not over 71 in., not under 69.5 in. 7. Koppers Aeromatic F200/00-72D Parts List Assembly No. 4324 revised February 21, 1949 (eligible on Models 7AC, S7AC with A-65 engine only). Low pitch setting at 24 in. sta.: 13.5 o Static r.p.m. at maximum permissible throttle setting: Not over 2300, not under 2200. No additional tolerance permitted. Diameter: not over 72 in., not under 70.5 in. When this propeller is installed, insta llation and operation must be accomplished in accordance with Kopper's "Installation and Operating Limitations No. 22A." 31 lb. (-52) 8. Sensenich M76AK-2 metal propeller with following limitations: Models 7AC, 7BCM, 7CCM, 7DC Models 7EC,7FC, 7JC 23 lb. (-52) (-54) (a) (Models 7CCM, S7CCM) Static r.p.m. at maximum permissible throttle setting: Not over 2410, not under 2150. No additional tolerance permitted. Diameter: not over 74 in., not under 72.5 in. (b) (Models 7EC, 7FC, 7JC) Static r.p.m. at maximum permissible throttle setting: Not over 2350, not under 2150. No additional tolerance permitted. Diameter: not over 74 in., not under 72.5 in. (c) (Model S7EC) Static r.p.m. at maximum permissible throttle setting: Not over 2400, not under 2300. No additional tolerance permitted. Diameter: not over 74 in., not under 72.5 in. (d) (Models 7AC, 7BCM, 7DC) Static r.p.m. and diameter limits same as for fixed pitch wood propeller under applicable. 9. Flottorp controllable, R002 or R003 series hub, blades R003-233-72 (Model 7AC only). Pitch at 28.5 in. sta.: low 12.5 o, high 19.0 o Static r.p.m. at maximum permissible throttle setting: Not over 2250, not under 2150. No additional tolerance permitted. Diameter: not over 72 in., not under 70.5 in. 29 lb. (-52) *10. Senenich fixed pitch metal 21 lb. (-52) (a) M74CK (Models 7AC, S7AC) Static r.p.m. at maximum permissible throttle setting: Not over 2250, not under 1960. Diameter: not over 74 in., not under 72 in. (b) M74CK-2 (Model 7BCM) Static r.p.m. at maximum permissible throttle setting: Not over 2450, not under 2200. Diameter: not over 72 in., not under 70 in. 11. Sensenich M74DM 30 lb. (-57) (a) Models 7GC, 7HC Static r.p.m. at maximum permissible throttle setting: Not over 2500, not under 2300. No additional tolerance permitted. Diameter: not over 74 in., not under 72.5 in. (b) Models 7GCA, 7GCB, 7GCBA, 7KC Static r.p.m. at maximum permissible throttle setting: Not over 2610, not under 2300. No additional tolerance permitted. Diameter: not over 74 in., not under 72.5 in. (8.00-6 tires required when using this propeller on 7GCBA) 12. McCauley 1A170GM74 33 lb. (-57) A-759 Page 20 of 37 (a) Models 7GC, 7HC, 7GCA, 7GCB, 7GCBA, 7KC Static r.p.m. at maximum permissible throttle setting: (No additional tolerance permitted). (Models 7GC, 7HC) not over 2500, not under 2300 (Models 7GCA, 7GCB, 7GCBA) not over 2610, not under 2300 (Model 7KC) not over 2600, not under 2125 Diameter: not over 74 in., not under 72.5 in. (8.00-6 tires required when using this propeller on 7GCBA) A-759 Page 21 of 37 13. McCauley 1A170GM76 34 lb. (-57) (a) Models 7GC, 7HC, 7GCA Static r.p.m. at maximum permissible throttle setting: (No additional tolerance permitted). (Models 7GC, 7HC) not over 2500, not under 2300 (Model 7GCA) not over 2610, not under 2300 Diameter: not over 76 in., not under 74.5 in. (7.00-6 tires required when using this propeller on 7GC and 7GCA) 14. McCauley 1C172MCM74 33 lb. (-57) (a) Models 7GCB, 7GCBA, 7KC Static r.p.m. at maximum permissible throttle setting: (No additional tolerance permitted). (Models 7GCB, 7GCBA) not over 2610, not under 2300 (Model 7KC) not over 2600, not under 2125 Diameter: not over 74 in., not under 72.5 in. (8.00-6 tires required when using this propeller on 7GCBA) 15. McCauley 1A100ACM69 24 lb. (-58) (a) Models 7ECA with Continental O-200-A engine Static r.p.m. at maximum permissible throttle setting: (No additional tolerance permitted). Not over 2600, not under 2400 Diameter: not over 69 in., not under 67.5 in. 16. McCauley 1C172AGM72 35 lb. (-58) (a) Models 7GCAA, 7GCBC, 7KCAB, S7GCBC Static r.p.m. at maximum permissible throttle setting: (No additional tolerance permitted). (Models 7GCAA, 7GCBC) not over 2640, not under 2300 (Model 7KCAB) not over 2540, not under 2300 (Model S7GCBC ith Item 204(d) installed) not over 2550, not under 2450 (Model 7KCAB with Bendix fuel inje ctor flow setting #2524723-1) not over 2500, not under 2300 Diameter: not over 72 in., not under 70.5 in. 17. McCauley 1C90ALM72 or McCauley 1C90CLM72 28 lb. (-58) (a) Models 7ECA and 7GCBC with Lycoming O-235-C1 engine Static r.p.m. at maximum permissible throttle setting: (No additional tolerance permitted). Not over 2425, not under 2225 Diameter: not over 72 in., not under 70.5 in. 18. McCauley 1A175GMA80 33 lb. (-58) (a) Model S7GCBC with Item 204(d) installed and O-320 Lycoming engine Static r.p.m. at maximum permissible throttle setting: (No additional tolerance permitted). Not over 2560, not under 2460 Diameter: not over 80 in., not under 78.5 in. 19. McCauley 1A172AGM76 35 lb. (-58) (a) Model S7GCBC with Item 204(d) installed and O-320 Lycoming engine Static r.p.m. at maximum permissible throttle setting: (No additional tolerance permitted). Not over 2550, not under 2450 Diameter: not over 76 in., not under 74.5 in. 20. Sensenich 74DM6S8-1 37 lb. (-58) (a) Models 7ECA, 7GCAA, 7GCBC, 7KCAB Static r.p.m. at maximum permissible throttle setting: (No additional tolerance permitted). (Model 7GCBC with Item 204(d) installed and with O-320 Lycoming engine) not over 2550, not under 2450 Diameter: not over 74 in., not under 72 in. (Models 7ECA, 7GCAA, 7GCBC, 7KCAB) eligible for use only on aircraft equipped with narrow lower end section steel spring gear P/N 7-1404, extended steel gear P/N 4-2038, or aluminum gear P/N 4-2035. (Model 7ECA) eligible only for aircraft equipped with Item 125 (Models 7ECA, 7GCAA, 7GCBC) not over 2640, not under 2300 (Model 7KCAB) not over 2540, not under 2300 (Model 7KCAB with Bendix fuel inje ctor flow setting #2524723-1) not over 2500, not under 2300 Diameter: not over 73 in., not under 72 in. 21. Sensenich W60GM Wood Propeller 10 lb. (-58) (a) Model 7ACA with Franklin 2A-120B engine Static r.p.m. at maximum permissible throttle setting: (No additional tolerance permitted). Not over 3050, not under 2750 Diameter: not over 60 in., not under 58.5 in. A-759 Page 22 of 37 (b) Model 7ACA with Franklin 2A-120A engine Static r.p.m. at maximum permissible throttle setting: (No additional tolerance permitted). Not over 3050, not under 2850 Diameter: not over 60 in., not under 58.5 in. 22. Sensenich 72CKS8-0 28 lb. (-58) (a) Models 7ECA with Lycoming O-235-K2C engine Static r.p.m. at maximum permissible throttle setting: (No additional tolerance permitted). Not over 2530, not under 2215 Diameter: not over 72 in., not under 70.0 in. 23. Sensenich 76EM8S8-0 41 lb. (-58) (a) Model 7GCBC with Superior O-360-A3A2 or Lycoming O-360-C4P engine Static r.p.m. at maximum permissible throttle setting: (No additional tolerance permitted). Not over 2550, not under 2350 Diameter: not over 76.25 in., not under 76 in. 24. MT 188 R 135-4G 18 lb. (-58) (a) Model 7GCAA with O-360 Superior engine Static r.p.m. at maximum permissible throttle setting: (No additional tolerance permitted). Not over 2500, not under 2300 Diameter: not over 74 in., ±.2 in. 25. Sensenich W69EK-48 10 lb. (-54) (a) Model 7EC with O-200-A or O-200-D Continental engine Static r.p.m. at maximum permissible throttle setting: (No additional tolerance permitted). Not over 2500, not under 2300 Diameter: not over 69 in., ±.1 in. Engine and Engine Accessories - Fuel and Oil Systems 101. Carburetor air heater (7AC, S7AC, 7DC and S7DC) 2 lb. (-42) 102. Carburetor or injector air scoop (a) Models 7AC, 7BCM, 7CCM, 7DC (Aeronca dwg. 4-601) 2 lb. (-47) (b) Models 7EC, 7FC, 7JC (Champion dw g. 4-877-3 with Marvel - Schebler carburetor, Champion dwg. 4-877-4) (c) Models 7GC, 7GCA, and 7HC (Champion dwg. 4-1031) 3 lb. (-37) (d) Models 7GC, 7GCA, 7GCB, 7GCBA, 7HC, 7KC (Champion dwg. 4-1099) 4 lb. (-44) (e) Model 7ECA with Continental O-200- A engine (Champion dwg. 4-1377) 1 lb. (-45) (f) Models 7GCAA, 7GCBC (Champion dwg. 4-1637) 1 lb. (-33) (g) Models 7ECA and 7GCBC with Lycoming O-235-C1 engine (Champion dwg. 4-1435) 1 lb. (-33) (h) Model 7KCAB (Champion dwg. 4-1454) 1 lb. (-33) (i) Model 7ACA (Champion dwg. 4-1563) 1 lb. (-48) (j) Models 7ECA, 7GCAA, 7GCBC (Champion dwg. 4-1637 box and 3-1535 cover) 1 lb. (-33) (k) Model 7KCAB (Champion dwg. 4-1637 box and 3-1544 cover) 1 lb. (-33) (l) Models 7GCAA, 7GCBC (Champion dwg. 4-1637-1 box and 3-1562 cover) 1 lb. (-33) 103. Carburetor or Injector Air Filter (a) Models 7AC, 7BCM, 7CCM, 7DC (Aeronca Dwg. 2-849) 1 lb. (-47) (b) Models 7EC, 7FC, 7JC (Aeronca Dwg. 2-849) 1 lb. (-49) (c) Models 7GC, 7GCA, and 7HC (P/N 120086 Air Maze) 1 lb. (-46) (d) Models 7GC, 7GCA, 7GCB, 7GCBA, 7HC, 7KC (Fram P/N CA161PL) 2 lb. (-45) (e) Model 7ECA with Continental O-200-A engine (Air Maze P/N 13203) 1 lb. (-53) (f) Models 7ECA, 7GCBC, 7GCAA, 7KCAB (Fram P/N CA121PL or AC P/N 6486786 or 5648075) 1 lb. (-37) (g) Model 7ACA (Air Maze P/N 13203) 1 lb. (-52) (h) Models 7ECA, 7GCAA, 7GCBC, 7KC AB (Donaldson P/N P10-4145) 1 lb. (-45) (i) Models 7ECA, 7GCAA, 7GCBC, 7KC AB (Brackett P/N BA-8110) 1 lb. (-45) 104. McDowell starter (Aeronca dwg. S-7) 9 lb. (-50) 105. Hanlon and Wilson mufflers and heaters (a) Models 7AC, 7BCM, 7CCM, and 7DC (dwg. 7-557) Note: Weight of exhaust stack removed to permit this installation, 4 lb., Model 7AC only. 13 lb. (-40) (b) Models 7EC, 7FC, 7JC (dwg. 7-1056) 13 lb. (-42) 106. Auxiliary fuel tank (5.5 gal. capacity) (a) Models 7AC, S7AC (Aeronca dwg. 7-565A) 11 lb. (+58) (b) Models 7AC, S7AC, 7BCM, 7CCM, S7CCM, 7DC, S7DC, 7EC, S7EC (dwg. 7-1001, 7-796) (weight per tank) Note: Left and right tanks eligible. When two tanks are installed, placard (dwg. 1-3510) is required. 8 lb. (+19) 107. Exhaust muffler, Ryan Aeronautical Co. Dwg. 54209 (7AC, S7AC) 2 lb. (-40) *108. Oil filter - Fram PB-5, Kit No. 510, Fram Installation Dwg. 61522 or 62399. Weight includes 1 qt. of oil. (Eligible on all 7 series aircraft.) 4 lb. (-26) A-759 Page 23 of 37 109. Carburetor restricted air filter assembly, Champion dwg. 2-957 1 lb. (a) Models 7CCM, 7DC Model 7EC Note: 2-957 restricted filter assembly required on Model 7EC with auxiliary wing tank fuel system installed. (-47) (-49) (b) Unrestricted air filter assembly ( Champion dwg. 2-849) (Used with 7-10002 fuel system. See item 116) Models 7EC, 7FC, 7JC 1 lb. (-49) 110. Injector airscoop and filter assemb ly for injector type engine 4 lb. (-47) 111. Starters (a) Delco-Remy No. 1109656, 12V, Models 7EC, 7FC, 7JC 16 lb. (-28) (b) Delco-Remy No. 1109657 starter and No. DR1464 starter solenoid. Models 7ECA (with Lycoming O-235-C1 engine), 7GC, 7GCA, 7GCAA, 7GCB, 7GCBA, 7GCBC, 7HC, 7KC, 7KCAB 18 lb. (-46) (c) Deleted September 12, 1961 (inc luded in Items 111(b) and 308(d)). (d) Delco-Remy No. 1109656, 12V, Model 7ECA wi th Continental O-200-A engine. 16 lb. (-32) (e) Prestolite P/N MZ-4204, Models 7ECA (with Lycoming O-235-C1 or O-235-K2C engine), 7GCAA, 7GCBC, 7KCAB 18 lb. (-46) (f) Prestolite P/N MZ-4203, Model 7ACA (w ith Franklin 2A-120A engine), 15 lb. (-38) (g) Sky-Tec P/N 149-12LS, Models 7GCAA, 7GCBC, 7KCAB 10 lb. (-46) (h) Sky-Tec P/N 122-12PM, Models 7ECA (with Lycoming O-235 engine) 10 lb. (-46) (i) Teledyne Continental P/N 655551, Model 7EC (with Continental O-200-A or O-200D) 11 lb. (-31) 112. Oil capaity calibration plate installed on firewall for Model S7EC (Aeronca dwg. 1-3517). No wt. change *113. Davis exhaust silencer Model D-65-2 in stalled per Davis Silencer Co. dwg. 650 (7AC, S7AC when Items 105 or 107 are not installed). 3 lb. (-39) *114. Wright winter shutters, installed per Wright Instln, Instructions No. 1 dated 12-24-49, issued by Wright Fl ying Service, Williston, ND 2 lb. (-26) *115. Lycoming O-235-C and -C1 engines eligible when installed per STC SA3-372. Engine and propeller combinations and limits as specified on STC and addendum pages, as amended 27 November 1970 or later amendments. 116. 26 Gallon Fuel System. Champion Instln. dwg. 7-1102 and 7-10002, Models 7FC, 7JC and 7ECA. (Models eligible when installed per Champion Kit 192: 7A, 7B, 7C, 7D, 7E) Placard (Champion dwg. 1-8825) required on Model 7A. 30 lb. (+20) 117. Mixture Control installation (a) Models 7EC, 7FC, 7JC (Champion dwg. 4-1013) 1 lb. (-5) (b) Models 7GC, 7HC, (Champion dwg. 7-1088) 1 lb. (-10) (c) Models 7GCA, 7GCB, 7GCBA, 7KC (Champion dwg. 7-1114) 1 lb. (-10) (d) Model 7ECA with CMC O-200-A engine (Champion dwg. 7-1252) 1 lb. (-22) (e) Models 7GCBC (with Lycoming O-320 engine), 7GCAA (Champion dwg. 7-1289) 1 lb. (-10) (f) Models 7GCBC (with Lycoming O- 235-C1 engine), 7ECA (Champion dwg. 7-1300) 1 lb. (-10) (g) Model 7KCAB (Champion instln. dwg. 7-1302) 1 lb. (-10) (h) Model 7ACA (Champion instln. dwg. 7-1445) 1 lb. (-15) (i) Models 7ECA (with Lycoming O-235-K2 C engine), (Champion Installation dwg. 7-1530) 1 lb. (-10) (j) Modesl 7GCAA, 7GCBC (with S uperior O-360-A3A2 engine), (Champion Installation dwg. 7-1581) 1 lb. (-10) 118. Oil Cooler (a) Models 7GC, 7GCA, 7HC (Champion P/N 3-1086-1) 8 lb. (-26) (b) Models 7GC, 7GCA, 7GCB, 7GCBA, 7HC, 7KC (Champion P/N 3-1114-1) 4 lb. (-28) (c) Models 7GCAA, 7GCBC (with Lycoming O-320 engine) (Champion Instln. dwg. 7-1289) 3 lb. (-29) (d) Models 7KCAB (Champion Instln. dwg. 7-1302) 3 lb. (-29) (e) Models 7ECA (with Lycoming O-235-K2 C engine) (Champion Instalation dwg. 7-1530) 3 lb. (-29) (f) Model 7EC (with TCM O-200-D) (Champion Installation dwg. 7-1612) 3 lb. (-33) 119. 39 Gallon Fuel System Models 7ECA, 7GC, 7GCA, 7GCAA, 7GCB, 7GCBA, 7GCBC, 7HC, 7KC (Champion instln. dwg. 7-1099, 7-1102) Model 7KCAB (Champion instln. dwg. 7-1099, 7-1314) Models 7ECA, 7GCAA, 7GCBC, 7KCAB (Champion instln. dwg. 7-1328) 32 lb. 42 lb. 40 lb. (+20) (+20) (+19) 120. Exhaust mufflers and heaters (a) For use with Item 102(c) carburetor air scoop (Champion instln. dwg. 7-1086) Models 7GC, 7GCA, 7HC 15 lb. (-36) (b) For use with Item 102(d) carburetor air scoop (Champion instln. dwg. 7-1133) Models 7GC, 7GCA, 7GCB, 7GCBA, 7HC, 7KC 15 lb. (-36) (c) For use with Item 102(f) carburetor air scoop (Champion instln. dwg. 7-1289) Models 7GCAA, 7GCBC 15 lb. (-36) (d) For use with Item 102(g) carburetor air scoop (Champion instln. dwg. 7-1300) Model 7ECA (with Lycoming O-235-C1 engine) 14 lb. (-36) (e) For use with Item 102(h) carburetor air scoop (Champion instln. dwg. 7-1302) Model 7KCAB 14 lb. (-36) A-759 Page 24 of 37 (f) For use with Item 102(j) carburetor air scoop (Champion P/N 7-1466-2 or 7-1483-2 and Inst. Dwg. 7-1300 Model 7ECA with Lycoming O-235-C1 engine 15 lb. (-42) (g) For use with Item 102(j) carburetor air scoop (Champion P/N 7-1466-1 or 7-1483-1 and Inst. Dwg. 7-1289) Models 7GCAA, 7GCBC 15 lb. (-42) (h) For use with Item 102(k) Injector air scoop (Champion P/N 7-1466-1 or 7-1483-1 and Inst. Dwg. 7-1314 Model 7KCAB 15 lb. (-42) (i) For use with Item 102(j) carburetor air scoop (Champion P/N 7-1483-2 and Inst. Dwg. 7-1530 Model 7ECA with Lycoming O-235-K2C engine 15 lb. (-42) 121. Vacuum pump (a) Airborne Mechanisms dry vacuum pum p, Model 10-113-A1 (Champion instln. dwg. 7-1104) Models 7GC, 7GCA, 7GCB, 7GCBA, 7HC, 7KC 3 lb. (-28) (b) Airborne Mechanisms dry vacuum pum p, Model 113A5 (Champion instln. dwg. 7-1275) Model 7ECA with Continental O-200-A engine 5 lb. (-43) (c) Airborne Mechanisms dry vacuum pump, Model 113A5 or 200CC (Champion instln. dwg. 7-1125) Models 7ECA, (with Lycoming O-235-C1 or O-235-K2C engine), 7GC, 7GCA, 7GCAA, 7GCB, 7GCBA, 7GCBC, 7HC, 7KC, 7KCAB 5 lb. (-28) 122. Lycoming O-235-C1 or O-235-C2C (Models 7ECA, 7GCBC) installed per Champion instln. dwg. 7-1300 Fuel: 80 minimum grade aviation gasoline Engine limits for all operations: 2800 r.p.m. (115 h.p.) Oil capacity: 6 qt. at -36 Control surface Elevator trim tab Up 10 o Down 44 o (Model 7GCBC only) Required equip. Landplane: 17(a), 102(g) or (j), 103(f) or (h), 117(f), 116 or 119 or 123(a), 201(d) or (h) or (i) or (l), 202. Seaplane: 17(a), 102(g) or (j), 103(f) or (h), 117(f), 116 or 119 or 123(a), 204(c), 205(a) or 205(d) 123. Fuel System (a) 36 Gallon Fuel System Champion instln. dwg. 7-1456, 7-1476 Models 7ECA, 7GCAA, 7GCBC Champion instln. dwg. 7-1456, 7-1314 Models 7KCAB 39 lb. 41 lb. (+20) (+19) 124. Lycoming O-235-K2C engine (Model 7ECA) Installed per Champion Dwg. 7-1530 Fuel 100 minimum grade aviation gasoline Engine limits Take-Off 2800 r.p.m. (118 h.p.) Maximum Continuous 2700 r.p.m. (115 h.p.) Oil capacity 6 qt. at -36 Required equip. Landplane: 22(a), 102(j), 103(h)(i), 117(i), 123(a), 201(i)(l), 202(g). 125. Lycoming O-320-B2B engine (Models 7ECA, 7GCAA, 7GCBC) Installed per Champion Dwg. 7-1289. Requires aircraft to be outfitted per Note 13 (7GCBC) or Note 15 (7ECA, 7GCAA) Fuel 100 minimum grade aviation gasoline Engine limits Maximum Continuous 2700 r.p.m. (160 h.p.) Oil capacity 8 qt. at –36 Required equip. Landplane: 20(a), 102(f), 103( i), 117(e), 123(a), 201(i)(l), 202(g). Modifications per Champion dwg. 11-1029 (7ECA only). Original Equipment Serial Numbers: 400-97 and up (7GCAA) 1200-94 and up (7GCBC) 126. Superior O-360-A3A2 engine (Model 7GCBC, 7GCAA) Installed per Champion Dwg. 7-1581. Requires aircraft to be outfitted per Note 13 (7GCBC) or Note 15 (7GCAA). Fuel 91 octane minimum gaso line (no alcohol content) Engine limits Maximum Continuous 2700 r.p.m. (180 h.p.) Oil capacity 8 qt. at -36 Required equip.7GCBC Landplane:23(a), 102(l) , 103(i), 117(j), 123( a), 201(n), 202(g) Required equip.7GCAA Landplane:23(a), 102(l) , 103(i), 117(j), 123( a), 201(i), 202(g) Original Equipment Eligible Serial Numbers: 1360-2004 and up (7GCBC) 497-2005 and up (7GCAA) 127. Lycoming O-360-C4P engine (Model 7GCBC) Installed per Champion Dwg. 7-1581. Requires aircraft to be outfitted per Note 13 (7GCBC). Fuel 91 octane minimum gaso line (no alcohol content) Engine limits Maximum Continuous 2700 r.p.m. (180 h.p.) Oil capacity 8 qt. at -36 Required equip.7GCBC Landplane:23(a), 102(l) , 103(i), 117(j), 123(a) , 201(n), 202(g) Original Equipment Eligible Serial Numbers: 1459-2011 and up (7GCBC) A-759 Page 25 of 37 Landing Gear and Floats 201. Main landing gear wheels (a) 6.00-6 wheels with brakes (Goodyear model L6MBD, wheel assembly 511413M, Brake assembly 511254-A) with: 6.00-6, 2 or 4-ply tires (Model 7AC only) 6.00-6, 4-ply tires or 7.00-6, 4-ply tire s (all models except 7FC, 7GCBA, 7HC) 35 lb. 35 lb. (0) (0) (b) 6.00-6 wheels with brakes (Cleveland Model 6.00DMB-3, wheel assembly C-38500-HM with mechanical brake asse mbly C-7000, or wheel assembly C-38500-H with hydraulic brake assembly C-2000-H with: 6.00-6, 2 or 4-ply tires (Model 7AC only) 6.00-6, 4-ply tires 7.00-6, 4-ply tires 8.00-6, 4-ply tires Models 7AC thru 7EC, 7GC, 7GCA, 7GCB, 7JC, 7KC Model 7GCBA, 8.00-6, 4-ply tire only Models 7FC, 7HC 32 lb. 32 lb. 39 lb. 42 lb. (0) (0) (+26) (c) 6.00-6 Goodyear Model CL6HBM (cross-wind) wheel and brake assembly 266AX36 or wheel assembly 9530526RH and 9530525LH, brake assembly 9530368RH and 9530369LH with: 6.00-6, 2 or 4-ply tires (Model 7AC only) 6.00-6, 4-ply tires or 7.00-6, 4-ply tires (Installation Aeronca dwg. 7-1000) (Models 7AC thru 7EC only) 52 lb. (0) (d) Cleveland hydraulic wheel and brake assembly 20-16 (Champion installation dwg. 7-1159 - Oleo type gear) with: 6.00-6, 4-ply tires (Model 7FC) 7.00-6, 4-ply tires (Model 7FC) 7.00-6, 4-ply tires (Model 7ECA with CMC O-200-A engine) 6.00-6, 4-ply tires (Model 7ECA with CMC O-200-A engine) Eligible when P/N 2-1655 Oleo Taxi Spring installed. 7.00-6, 6-ply tires (Model 7ECA with Lycoming O-235-C1 engine, 7GCAA, 7GCBC and 7KCAB), with Oleo Taxi Springs (P/N 2-1655 ) installed. 32 lb. 35 lb. 35 lb. 32 lb. 37 lb. (+26) (+26) (0) (0) (0) (e) 4-1139 axle assembly (Champion instln. dwg. 7-1159) Model 7FC (see NOTE 7) Model 7HC (see NOTE 9) 13 lb. (+26) (f) Goodrich wheel and brake instln. (P/N 3-1086 and 2-883) Wide trake main gear (Champion dwg. 7-1176) with 6.00-6, 4-ply tires 7.00-6, 4-ply tires 8.00-6, 4-ply tires (Models 7FC and 7HC) 38 lb. 45 lb. 48 lb. (+26) (g) Goodrich wheel and brake instln. (P/N 3-1086 and 2-883) (Champion dwg. 7-1177) with 6.00-6, 4-ply tires 7.00-6, 4-ply tires 8.00-6, 4-ply tires (Models 7EC, 7GC, 7GCA, 7GCB, 7JC, 7KC) (Model 7GCBA, 8.00-6, 4-ply tires only) 38 lb. 45 lb. 48 lb. (0) (0) (h) Cleveland wheel and brake assemblies (20-16) Champion Instln dwg. 7-1307, 7-1291 Spring Steel Gear 7.00-6, 6-ply tires 8.00-6, 4-ply tires (Models 7ECA, 7GCAA, 7GCBC, 7KCAB) 32 lb. 35 lb. (0) (0) (i) Cleveland wheel and brake assemblies ( 20-16) Champion Instln dwg. 7-1307, 7-1404 or 4-2038 Spring Steel Gear 4-2035 Spring Aluminum Gear (Installation dwg 7-1559) 6.00-6, 4-ply or 6-ply tires 7.00-6, 4-ply or 6-ply tires 8.00-6, 4-ply tires (Models 7ECA, 7GCAA, 7GCBC, 7KCAB) 29 lb. 32 lb. 35 lb. (0) (0) (0) (j) Cleveland wheel and brake assemblies (40-78B) Champion Instln dwg. 7-1440, 7-1441 Spring Steel Gear 5.00-5, 4-ply tires 5.00-5, 6-ply tires (Model 7ACA) 23 lb. 25 lb. (0) (0) (k) Cleveland wheel and brake assemblies (20-16) Champion Instln dwg. 7-1440, 7-1441-1 Spring Steel Gear 6.00-6, 4 or 6-ply tires (Model 7ACA) 29 lb. (0) (l) McCauley wheel and brake assemblies (D-30039-1) Champion Instln dwg. 7-1307, 7-1404 Spring Steel Gear 6.00-6, 4-ply or 6-ply tires 7.00-6, 4-ply or 6-ply tires 8.00-6, 4-ply tires (Models 7ECA, 7GCAA, 7GCBC, 7KCAB) 29 lb. 32 lb. 35 lb. (0) (0) (0) A-759 Page 26 of 37 (m) McCauley wheel and brake assemblies (D-30039-1) Champion Instln dwg. 7-1440, 7-1441 Spring Steel Gear 6.00-6, 4-ply or 6-ply tires (Models 7ACA) 29 lb. (0) (n) Cleveland wheel and brake assemblies (20-16) Champion Instln dwg. 7-1559, 4-2035 Spring Aluminum Gear 8.00-6, 4-ply tires (Model 7GCBC with Superior O-360-A3A2 Engine) 35 lb. (0) (o) Cleveland wheel and brake assemblies (20-16) Champion Instln dwg. 7-1589, 4-2045 Spring Aluminum Gear 6.00-6, 4-ply tires (Model 7EC wi th Continental O-200-A Engine) 29 lb. (0) 202. Tail wheel assemblies (Models 7AC, 7BC, 7CCM, 7DC, 7EC, 7ECA, 7GC, 7GCA, 7GCAA, 7GCB, 7GCBA, 7GCBC, 7KC, 7KCAB, 7ACA, except as noted) (a) 6 x 200 steerable Scott Aviation Model 3000 7 lb. (+186) (b) Maule Models SFS-12, SS-12 or SAFS-12 6 lb. (+186) (c) Steerable, Scott Model 3-24B 7 lb. (+186) (d) Imperial Model B-100 6 lb. (+186) (e) Lang (formerly Decker) steerable Model D-501A 7 lb. (+186) (f) Maule SFS-1-2 (Champion instln. dwg. 4-1042) (Model 7GC only) 6 lb. (+197) (g) Scott (Avox) 3200 or ABI-3200 (Champion instln. dwg. 4-1080) 8 lb. (+190.5) (h) Maule pneumatic SFS-1-2P8 (Champion instln. dwg. 3-486) 8 lb. (+190.5) (i) Maule pneumatic SFS-1-2P8 (Champion instln. dwg. 4-1423) 8 lb. (+191) 203. Skis (Models 7AC, 7BCM, 7CCM, 7 DC, 7EC, 7GC, except as noted) (a) Federal A-1500 (Federal instln. dwg. 11R241) 37 lb. (0) (b) Federal CA1850-6 (Federal instln. dwg. 11R241) 48 lb. (0) (c) Federal A-2000-A (Federal instln. dwg. 11R241) 49 lb. (0) (d) Federal A-2000 (Federal instln. dwg. 11R241) 41 lb. (0) (e) Federal A-1850 (Federal instln. dwg. 11R241) 38 lb. (0) (f) Federal A-1500-A (Federal instln. dwg. 11R241) 39 lb. (0) (g) Federal Model AWB-1500 wheel skis when installed in accordance with Federal Instal. Dwg. 11R471. Placard required on ski position selector box: "SKI CONTROL" "UP-NEUTRAL-DOWN" 75 lb. Retracted (-6) Extended (-3.5) (h) Federal Model AWB-1500A wheel skis when installed in accordance with Federal Instal. Dwg. 11R471. Placard required on ski position selector box: "SKI CONTROL" "UP-NEUTRAL-DOWN" 84 lb. Retracted (-6) Extended (-3.5) (i) Federal Model C-2200 wheel-ski co mbination (Champion instln. dwg. 7-1076) (Models 7EC, 7GC only) Main skis and hydraulic components with LDR bottoms Main skis and hydraulic components with aluminum bottoms 106 lb. Retracted (-13) 96 lb. Retracted (-14) Extended (-5) Extended (-5) (j) Federal Model AWT-2500 tail ski (Cham pion instln. dwg. 3-1101) (Models 7EC, 7GC only) 7 lb. (+186) (k) FluiDyne Model A-2000-A (Champion instln. dwg. 7-1281) (Models 7ECA, 7GCAA, 7GCBC) Main skis only. 38 lb. (-6) (l) FluiDyne Model A-2000A (Champion inst ln. dwg. 7-1321) Model 7GCBC with Lycoming O-320 engine and spring steel gear installed. Main skis only. (Models 7GCAA, 7KCAB, 7ECA) 44 lb. (-5) 204. Floats - Seaplane (a) Edo 60-1320 including water rudder (Model S7AC only) 168 lb. (+16) (b) Edo 92-1400 including water rudder (Models S7AC thru S7EC) 169 lb. (+16) (c) Pee-Kay 1800 (Champion dwg. 7-1118) (Models 7GC, 7GCB, 7GCBC with Lycoming O-320 engine, 7ECA, 7HC). Model 7HC eligible only on aircraft with Champion dwg. 3-1135 fuselage fittings installed at Champion factory). 198 lb. (+19) (d) Edo 89A2000 floats including double water rudders Model 7GCBC with Lycoming O-320 engi ne and fitted for steel spring gear. 270 lb. (+16) 205. Auxiliary fins - Seaplane (a) Auxiliary Dorsal Fins (Champion P/N 4-634, Installation Dwg. 3-1067). Two required for EDO 60-1320, Model S7AC, EDO 92-1400 Floats on Models S7AC, S7CCM, S7DC, S7EC and for Pee-Kay 1800 Floats on Models 7ECA, 7GCA and 7HC Four required for Pee-Kay 1800 Floats on Models 7GCB 3 lb. 6 lb. (+170) (+170) (b) Deleted (c) Ventral Fin (Champion P/N4-6587) (Cham pion Installation Dwg. 4-909) Required for Models S7AC, S7CCM and S7DC on EDO 92-1400 Floats and Models 7GC, 7GCB and 7HC on Pee-Kay 1800 Floats 4 lb. (+171) (d) Auxiliary Dorsal Fins (Champion P/N 4-1458, instln. dwg. 3-1418) (used with stabilizer, Champion P/N 4-1413) Two required for Pee-Kay 1800 Floats on Model 7ECA Four required for Pee-Kay 1800 Floats on Models 7GCB and 7GCBC Four required for Edo 89A2000 floats on Model 7GCBC with Lycoming O-320 engine 3 lb. 6 lb. 6 lb. (+170) (+170) (+170) A-759 Page 27 of 37 206. Wheel pants (a) Models 7AC, 7BCM, 7CCM, 7DC (dwg. 7-606) 6 lb. (0) (b) Model 7EC (dwg. 7-1060) 6 lb. (0) (c) Models 7FC, 7HC (dwg. 7-10006) 6 lb. (+26) (d) Models 7EC, 7GC, 7GCA, 7GCB, 7JC (dwg. 7-10006) 6 lb. (0) (e) Model 7FC (nose wheel only, dwg. 4-1006) 6 lb. (-31) (f) Model 7HC (nose wheel only, dwg. 7-1112) 3 lb. (-31) (g) Model 7JC (aft gear only, dwg. 7-1128) 3 lb. (+80) (h) Model 7FC (main wheels, dwg. 7-1141) 14 lb. (+26) (i) Model 7FC (nose wheel, dwg. 7-1154) 2 lb. (-29) (j) Models 7ECA, 7GCAA, 7GCB, 7GCBA, 7G CBC,, 7KC, 7KCAB (dwg. 7-1141) 14 lb. (0) (k) Models 7ECA, 7GCAA, 7GCBC,, 7KCAB (Champion instln. dwg. 4-1474) 14 lb. (0) 207. Parking brake (a) Models 7AC, 7BCM, 7DC, 7EC, 7FC, 7GC, 7GCA, 7GCB, 7HC, 7JC (Champion dwg. 7-443) 2 lb. (-10) (b) Models 7EC, 7FC, 7GC, 7GCA, (Champion dwg. 4-1023) 1 lb. (-8) (c) Models 7EC, 7FC, 7GC, 7GCA, 7HC, 7JC (Champion dwg. 4-1023) 1 lb. (-7) (d) Models 7ECA, 7GCAA, 7GCBC, 7KCAB (Champion dwg. 4-1370) 2 lb. (-16) (e) Models 7ECA, 7GCAA, 7GCBC, 7KCAB, 7ACA (Champion dwg. 4-1557) 1 lb. (-14) (f) Models 7ECA, 7GCAA, 7GCBC, 7KCAB, 7ACA (Champion dwg. 4-1624) 1 lb. (-14) *208. Wheel fenders - Consolidair Model 17 (Consolidair dwg. 0036) Models 7AC thru 7EC only 10 lb. (0) 209. Nose landing gear installation (Champion dwg. 7-1073) Models 7FC and 7HC (a) 5.00-5 Cleveland wheel and 5.00-5, Ty pe III, 4-ply rating tires 9 lb. (-31) 210. Hydraulic brake installation (a) Champion dwg. 7-1078 (Model 7EC only) (w t. increase over mechanical) 2 lb. (+10) (b) Scott hydraulic brake installation (Champion dwg. 4-1091) Models 7EC, 7FC, 7GC, 7GCA, 7GCB, 7JC, 7KC 3 lb. (+10) (c) Scott hydraulic brake instln. (Champi on dwg. 4-1122) Model 7KC 3 lb. (-18) (d) Cleveland hydraulic brake instln. (Champion dwg. 4-1370) Models 7ECA, 7GCAA, 7GCBC, 7KCAB 3 lb. (-6) (e) Hydraulic brake instln. - Heel - (Champion dwg. 4-1557, 7-1307) Models 7ECA, 7GCAA, 7GCBC, 7KCAB, 7ACA 2 lb. (-10) (f) Hydraulic brake instln. - Toe - (Champion dwg. 4-1624, 7-1307) Models 7ECA, 7GCAA, 7GCBC, 7KCAB, 7ACA 2 lb. (-10) 211. Aft landing gear (Champion instln. dwg. 7-1126) Model 7JC (a) 5.00-5 Cleveland wheel and 5.00-5, Ty pe III, 4-ply rating tires 9 lb. (+80) Electrical Equipment 304. (a) Battery, 6V, Reading (Models 7AC thru S7EC only) 12 lb. (+57) (b) Battery box (Models 7AC thru S7EC only) 2 lb. (+57) 305. Position lights (a) Models 7AC, 7BCM, 7CCM, 7DC (dwg. 7-545) 2 lb. (+24) (b) Models 7EC, 7FC (dwg. 7-1065) 3 lb. (+20) (c) Models 7GC, 7GCA, 7GCB, 7GCB C, 7HC (dwg. 7-1101) 1 lb. (+90) (d) Models 7EC, 7FC, 7JC (dwg. 7-1085) 1 lb. (+90) (e) Model 7KC (dwg. 7-1149) 1 lb. (+90) (f) Model 7GCBA (dwg. 7-1163) 1 lb. (+90) (g) Models 7ECA, 7GCAA, 7KCAB (dwg. 7-1320, 7-1051) 1 lb. (+90) (h) Model 7ACA (dwg. 7-439, 7-1051) 3 lb. (+20) 306. Generator, wing-driven, Champion 8 amp. 8 lb. ( +9) 307. Battery (a) Willard AW-12-25 (Model 7EC only) 24 lb. (+54) (b) Bowers BA-25, 12V Model 7EC only Models 7FC, 7JC Models 7GC, 7GCA (with cables), 7HC 24 lb. 24 lb. 28 lb. (+54) (-27) (+79.5) (c) Exide AC-60, 33 a. hr.; AC-66, 33 a. hr.; AC-78, 35 a. hr. 12V manifold vented Models 7GC, 7GCA, 7GCB, 7HC (Champion instln. dwg. 4-1066) Model 7KC (Champion dwg. 7-1149) 27 lb. (+79) (d) Exide AC-54 manifold vented, 12V 24 a. hr. (Champion instln. dwg. 4-1108) Models 7EC, 7FC, 7JC Model 7ECA with CMC O-200-A engine (instln. dwg. 7-1252) Model 7ECA and 7GCBC with Lycoming O-235-C1 engine (instln. dwg. 7-1300) 22 lb. 22 lb. 23 lb. (-27) (-27) (-26) (e) Exide AC-54 manifold vented, 12V 24 a. hr. (Champion instln. dwg. 3-1191) (Model 7EC) 22 lb. (+54) (f) Exide AC-54 manifold vented, 12V 24 a. hr. (Champion instln. dwg. 4-1167) (Model 7GCBA) 22 lb. (-27) (g) Exide AC-66 manifold vented, 12V 33 a. hr. (Champion instln. dwg. 7-1293) Models 7GCAA, 7GCBC, 7KCAB 33 lb. (+82) (h) Rebat S25, 12V 25 a. hr. (Champion instln. dwg. 7-1300) Models 7ECA, 7GCBC (with Lycoming engine O-235-C1) 23 lb. (-26) A-759 Page 28 of 37 (i) Rebat R35, 12V 35 a. hr. (Champion instln. dwg. 4-1469) Models 7GCAA, 7GCBC, 7KCAB 33 lb. (+82) (j) Gill 6GCAB-11, 12V 35 a. hr. (Champion instln. dwg. 4-1509) Models 7GCAA, 7GCBC, 7KCAB 33 lb. (+82) (k) Gill 6-GCAB-9, 12V 25 a. hr. (Champion instln. dwg. 7-1300) Models 7ECA, 7GCBC with Lycoming O-235-C1 engine 23 lb. (-26) (l) Exide AC-78, 12V 35 a. hr. (Champi on instln. dwg. 4-1545) Models 7GCAA, 7GCBC, 7KCAB 33 lb. (+82) (m) Sonotone CA-24A, 12V 25 a. hr. (Champion instln. dwg. 4-1578) Models 7GCAA, 7GCBC, 7KCAB 30 lb. (+82) (n) Rebat S25M, 12V 25 a. hr. (Champion instln. dwg. 4-1588) Model 7ACA 21 lb. (+55) (o) Rebat R35, 12V 35 a. hr. with battery box (Champion instln. dwg. 4-1599) Models 7GCAA, 7GCBC, 7KCAB 35 lb. (+82) (p) Gill PS6-11, 12V 35 a. hr. with battery box (Champion instln. dwg. 4-1599) Models 7GCAA, 7GCBC, 7KCAB 35 lb. (+82) (q) Gill PS6-9, 12V 25 a. hr. (Champion instln. dwg. 7-1300) Models 7ECA, 7GCBC (with Lycoming O-235-C1 engine) 23 lb. (-26) (r) Rebat S25, 12V 25 a. hr. (Champion instln. dwg. 7-1530) Model 7ECA (with Lycoming O-235-K2C engine) 23 lb. (-26) (s) Gill PS6-9, 12V 25 a. hr. (Champion instln. dwg. 7-1530) Model 7ECA (with Lycoming O-235-K2C engine) 23 lb. (-26) (t) American Champion 11-0817, 12V 31a. hr. with battery box (Champion instln dwg 4-1599) Models 7GCAA, 7GCBC, and 7KCAB 23 lb. (+82) (u) Concorde RG25, 12V 25 a. hr. with battery box (Champion instln dwg 4-1599) Models 7GCAA, 7GCBC, and 7KCAB 23 lb. (+82) (v) Concorde RG25, 12V 25 a. hr. (Cham pion instln. dwg. 7-1530) Model 7ECA (with Lycoming O-235-K2C engine) 23 lb. (-26) (w) Hawker 0769-4005, 12V 15 a hr. (Champion instln. Dwg. 7-1582) Model 7EC (with Continental O-200-A or O-200-D engine) 15 lb. (-25) 308. Generator or Alternator (a) Generator, voltage regulator, 12V 20 a., Delco-Remy 1101890 and 118736 Models 7EC, 7FC, 7JC 11 lb. (-28) (b) Generator, voltage regulator, 12V 35 a., Delco-Remy 1101898 and 1118704 Models 7EC, 7FC, 7JC 16 lb. (-28) (c) Generator, voltage regulator, 12V 20 a., Delco-Remy 1101899 and 1119226 Models 7ECA with Lycoming O-235-C1 engine, 7GC, 7GCA, 7GCAA, 7GCB, 7GCBA, 7GCBC, 7HC, 7KC, 7KCAB 12 lb. (-45) (d) Generator, voltage regulator, 12V 35 a., Delco-Remy 1101900 and 1118704 Models 7ECA (with Lycoming O-235-C1 engine), 7GC, 7GCA, 7GCAA, 7GCB, 7GCBA, 7GCBC, 7HC, 7KC, 7KCAB 18 lb. (-46) (e) Generator, voltage regulator, 12V 20 a., Delco-Remy 1101890 and 1118736 Model 7ECA 12 lb. (-32) (f) Generator, voltage regulator, 12V 35 a., Delco-Remy 1101898 and 1119220 Models 7ECA with Continental O-200-A engine 18 lb. (-31) (g) Alternator and voltage regulator, 12V 40 a., Prestolite Alternator P/N ALE 6406 (Model 7ECA with Lycoming O-235-C1 engine) and Prestolite Alternator P/N ALE 8406 (Models 7GCAA, 7GCBC, 7K CAB), Prestolite Voltage Regulator P/N VSF 72-1 or VSF 7202 or VSF 7203 12 lb. (-50) (h) Alternator and voltage regulator, 12V 35 a., Motorola RA12N451 and Integral R3-1 regulator - Model 7ACA 8 lb. (-41) (i) Alternator and voltage regulator, 12V 60 a., Prestolite Alternator P/N ALY8403 or ALY-8420 (Model 7ECA with Lycoming O-235-C1 engine, 7GCAA, 7GCBC, 7KCAB). Prestolite Voltage Regulator P/N VSF 7203. 12 lb. (-50) (j) Alternator and voltage regulator, 12V 60 a., Prestolite Alternator P/N ALY8420 G (#2 Field Terminal Grounded) Models 7ECA (with Lycoming O-235-C1 or O-235-K2C engine), 7GCAA, 7GCBC, 7KC AB. Prestolite Voltage Regulator P/N FVR 3224. 12 lb. (-50) 309. Deleted - included in Item 305 310. Landing light (a) Fixed light (dwg. 7-1065) Models 7EC, 7FC only 2 lb. (+7) (b) Retractable light (dwg. 4-10009) Models 7EC, 7FC only 5 lb. (+13) (c) Leading edge landing light (dwg. 4-1001) Models 7EC, 7FC, 7GC, 7GCA, 7GCB, 7GCBA, 7HC, 7JC 2 lb. (+4) (d) Nose bowl landing lights (Champion instln. dwg. 7-1149) Model 7KC only 2 lb. (-55) (e) Nose bowl mounted 100W bulb (Champion instln. dwg. 7-1274) Model 7ECA with CMC O-200-A engine 1 lb. (-22) (f) Nose bowl mounted 100W bulb (Champion instln. dwg. 7-1288) Models 7ECA with Lycoming O-235-C1 engine, 7GCAA, 7 GCBC, 7KCAB 1 lb. (-53) (g) Nose bowl mounted 100W bulb (Champion instln. dwg. 4-1558) Model 7ACA 1 lb. (-53) (h) Nose bowl mounted 100W bulb (Champion instln. dwg. 7-1475) Models 7ECA, 7GCAA, 7GCBC, 7KCAB 1 lb. (-53) 311. Stall warning equipment installation (a) (Champion dwg. 7-1065) Models 7EC, 7FC, 7JC 1 lb. (-4) (b) (Champion dwg. 7-1101) Models 7GC, 7GCA, 7GCB, 7HC 1 lb. (-2) (c) (Champion dwg. 7-1138) Model 7KC 1 lb. (-2) A-759 Page 29 of 37 (d) (Champion dwg. 7-1163) Model 7GCBA 1 lb. (-2) (e) (Champion dwg. 4-1401) Models 7ECA, 7GCAA, 7GCBC, 7KCAB, 7EC 1 lb. (-2) 312. Radio Equipment (a) Narco VHT-3 Superhomer radio instln. (Champion dwg. 3-1063) Models 7EC, 7FC, 7GC, 7GCA, 7GCB, 7GCBA (Champion dwg. 7-1103) Models 7EC, 7FC, 7GC, 7GCA, 7GCB, 7GCBA, 7HC, 7JC (Champion dwg. 7-1167) Model 7KC Cabin speaker instln. (optional) 13 lb. 1 lb. (-8) (+13) 313. Rotating beacon (a) (Champion dwg. 4-1020) Models 7EC, 7ECA, 7FC, 7GCA, 7GCAA, 7GCB, 7GCBA, 7GCBC, 7HC, 7JC, 7KCAB 2 lb. (+18 0) (b) (Champion dwg. 7-1149) Model 7KC 3 lb. (+18 2) (c) (Champion dwg. 4-1513) Models 7ACA, 7E CA, 7GCAA, 7GCBC, 7KCAB 2 lb. (+62) 314. Strobe Light (a) Delta Model 7000 per Champion dwg. 4-1512 Models 7ECA, 7GCAA, 7GCBC 4 lb. (+24) (b) Whelen A429 Wing Tip Strobe Lights (C hampion instln. dwg. 3-1512) Models 7ECA, 7GCAA, 7GCBC, 7KCAB 4 lb. (-4) (c) Aeroflash P/N 156-0003 Models 7ECA , 7GCAA, 7KCAB, 7GCBC, 7EC per Champion dwg. 3-1668 4 lb. (+24) Interior Equipment 401. Adjustable front seat cushion and belt (a) (Champion dwg. 7-453) Models 7EC, 7FC, 7GC, 7GCA, 7HC, 7JC 14 lb. (+17) (b) (Champion dwg. 7-1147) Model 7KC 32 lb. (+14) 402. Cargo rack replacing rear seat, cushion and belt 5 lb. (+40) 403. Cabin heater 2 lb. (-36) 404. Seats (a) Wide rear seat, dwg. 7-1067, cushions and belt, Models 7EC, 7ECA, 7FC, 7GC, 7GCA, 7GCAA, 7GCB, 7GCBC, 7JC, 7KCAB, 7ACA 18 lb. (+46) (b) Adjustable rear seat, Champion instln., dwg. 4-1056, Models 7GCB, 7HC 20 lb. (+48) (c) Adjustable rear seat, Champion inst ln., dwg. 7-1147, Model 7KC 33 lb. (+45) (d) Adjustable hinged front seat, Champion dwg. 7-1261, Models 7ECA, 7GCAA, 7GCBC 13 lb. (+16) (e) Adjustable hinged rear seat, Champion dwg. 7-1261, Models 7ECA, 7GCAA, 7GCBC 13 lb. (+46) (f) Parachute seat with seat pack parac hute and cushions, front (Champion instln. dwg. 7-1279) Models 7ECA, 7GCAA, 7GCBC, 7KCAB 33 lb. (+15) (g) Parachute seat with seat pack parac hute and cushions, rear (Champion instln. dwg. 7-1279) Models 7ECA, 7GCAA, 7GCBC, 7KCAB 33 lb. (+45) (h) Parachute seat instln. with cushi ons, without seat pack parachutes - front (Champion dwg. 4-1403-10) Models 7ECA, 7GCAA, 7GCBC, 7KCAB 13 lb. (+16) (i) Parachute seat instln. with cushi ons, without seat pack parachutes - rear (Champion dwg. 4-1403-10) Models 7ECA, 7GCAA, 7GCBC, 7KCAB 13 lb. (+46) (j) Front seat installation (Champion dwg. 4-1403-11) Models 7ECA, 7GCAA, 7GCBC, 7KCAB, 7ACA 11 lb. (+16) (k) Rear seat installation (Champion dwg. 4-1403-11) Models 7ECA, 7GCAA, 7GCBC, 7KCAB, 7ACA 11 lb. (+46) (l) Front seat installation (Champion dw g. 4-1642) Models 7ECA, 7GCAA, 7GCBC, 7KCAB 11 lb. (+16) (m) Rear seat installation (Champion dw g. 4-1642) Models 7ECA, 7GCAA, 7GCBC, 7KCAB 11 lb. (+46) (n) Adjustable front seat installati on (Champion Drawing 7-1499) Models 7ECA, 7GCAA, 7GCBC, 7KCAB 15 lb. (+16) (o) Rear seat installation (Champion Drawing 4-1708) Models 7ECA, 7GCAA, 7GCBC, 7KCAB 13 lb. (+47) (p) Wide Rear Seat Installation (Champi on Drawing 4-1709) Models 7ECA, 7GCAA, 7GCBC, 7KCAB 18 lb. (+47) 405. Soundingproofing (side panels, headlining and firewall) Models 7EC, 7JC Model 7FC only Models 7GC, 7GCA, 7GCB, 7HC 4 lb. 5 lb. 4 lb. (+22) (+10) (+24) 406. Alternate interior (includes uphol stery, floormat and baggage compartment lid) (Champion instln. dwg. 7-10003) Models 7EC, 7JC Model 7FC Models 7GC, 7GCA, 7GCB, 7HC (minus baggage compartment lid) 12 lb. 15 lb. 12 lb. (+21) (+28) (+36) 407. Fire extinguisher (a) (Champion instln. dwg. 7-442) Models 7AC, 7BCM, 7CCM, 7DC 7 lb. (+20) (b) (Champion instln. dwg. 7-10004) Models 7EC, 7FC, 7GC, 7GCA, 7GCB, 7HC, 7JC 7 lb. (+20) (c) (Champion instln. dwg. 7-1262 or 7-1293) Models 7ECA, 7GCAA, 7GCBC, 7KCAB 5 lb. (+23) (d) (Champion instln. dwg. 7-1444) Model 7ACA 5 lb. (+23) A-759 Page 30 of 37 408. Rear Seat Heater (a) (Champion instln. dwg. 7-1293) Models 7ECA, 7GCAA, 7GCBC, 7KCAB 2 lb. (-9) (b) (Champion instln. dwg. 7-1478) Models 7ECA, 7GCAA, 7GCBC, 7KCAB 2 lb. (-9) 409. Emergency Locator Transmitter (a) SHARC 7 Emergency Locator Transmi tter (Champion Inst. Drawing 3-1504) Models 7ECA, 7GCAA, 7GCBC, 7KCAB 2 lb. (+79) (b) SHARC 7 Emergency Locator Transmi tter (Champion Inst. Drawing 3-1506) Model 7ACA 2 lb. (+62) (c) Larago Emergency Locator Transmitte r (Champion Inst. Drawing 3-1590) Models 7ECA, 7GCAA, 7GCBC, 7KCAB 3 lb. (+68) (d) Ameri-King AK-450 or ACK Technologi es E-01 Emergency Locator Transmitter (Champion Inst. Drawing 3-1689), Models 7ECA, 7GCAA, 7GCBC, 7KCAB, 7EC 2.5 lb (+68) Miscellaneous (not listed above) 601. Deluxe finish 12 lb. (+55) 602. Step (fuselage) 1 lb. (+19) 603. Special windows (Aeronca dwg. 7-576) 7 lb. (+50) *604. Crop spraying instln., Aero Spray King Model A2 or A2-49 (Instln. per Ong dwg. A2-200 or A200-49 submitted by Ong Airc raft Corp., P.O. Box 214, Kansas City, MO) Eligble for certification in Standar d and/or Restricted classification. (See NOTE 3.) (Models 7AC thru 7EC only) (a) Aero Spray King Model A2 66 lb. (+37.5) (b) Aero Spray King Model A2-49 71 lb. (+39) 605. Aerial Insecticiding, Inc., "Portable Spray Equipment Model AI-7AC" installed per instln. instructions and instln. dwg. 7AC-2 and 7AC-3 furnished with kit. Eligible for certification in Standard classifi cation. Models 7AC thru 7EC only 40 lb. (+13) *606. Crop sprayer instln. (Models 7AC thru 7EC only) Pipestone Aviation Services installed per Pipestone Aviation Servic es, Pipestone, MN, dwg. and instln. instructions dated March 3, 1949. (Eligible for certification in Standard classification). 67 lb. (+17) *607. Crop sprayer instln. (Models 7AC thru 7EC only) Svedy-Sorensen Sprayer installed per Svedy-Sorensen, Worthington, MN, dwg. and instln. instructions dated March 10, 1949. (Eligible for certification in Standard classification). 56 lb. (+17) *608. Crop sprayer instln. (Models 7AC thru 7EC only) Sprayer installed per Broyhill Company, Dakota City, NE, dwg. BC-7DC-1. All propeller limits listed for each Model apply to this installation except M odel 7AC and 7CCM static r.p.m. limits for wood propeller which should be as follows: Static r.p.m. at maximum permissible throttle setting: (Model 7AC) not over 2250, not under 2150; (Model 7BCM) not over 2450, not under 2300. Eligible for certification in Standard or Restricted classification (See NOTE 3.). Placards required: In full view of pilot: "All acrobatics including spins prohibited when spray rig installed." On spray tank: "Allowable weight tank contents to be determined from weight and balance. Do not exceed 280 lb." 71 lb. (+28) *609. Crop sprayer instln. (Models 7AC thru 7EC only) Oda Spray and Equipment Co., Inc. installed per Oda dwg. H-300 and H301. Certification and operation limitations same as item 608 except as noted below: Placards on tank: "Allowable weight t ank contents to be determined from weight and balance. Do not exceed 260 lb." 77 lb. (+9) *610. Crop sprayer instln. (Models 7AC thru 7EC) Frye Mfg. Co. Model 112 (Instln. per Frye Aerial Spray Kit instructions for Ae ronca 7 series). Certification and operation limitations same as item 608. Disposable spray fluid. 32 lb. (+4) (+33.5) *611. Crop sprayer instln. (Models 7AC thru 7EC) Aero Spray King, Jr. Model SA-10 installed per Ong Aircraft Corp. instln. instructions and dwg. SA-1000. Certification and operation limitations same as item 608 except as noted below: Placards on tank: "Allowable weight t ank contents to be determined from weight and balance. Do not exceed 193 lb." Disposable spray fluid. 54 lb. (+19) (+40) *612. Crop sprayer installation. (Models 7AC thru 7EC only) Martin Sprayer, Model B, installed per Martin Sprayer Mfg. Co., Inc., Monmouth, IL, instln. instructions dated March 3, 1949. Eligible for certificati on in Standard and/or Restricted classification (See NOTE 3.) except Model 7AC, having w ood propeller, is limited to certification in Standard classification only. Placards required: In full view of pilot: "All acrobatics including spins prohibited when spray equipment installed." On spray tank: "Allowable weight tank contents to be determined from weight and balance. Do not exceed 395 lb." Disposable spray fluid. 45 lb. (+29) (+37) A-759 Page 31 of 37 *613. Crop sprayer instln. Svedy-S orensen Model 9 Combination Seeder, Duster and High or Low Gallonage Sprayer and Model 11 High or Low Gallonage Sprayer installed per Svedy-Sorensen Worthington, MN, instln. instructions dated April 1, 1950. Eligible for certification in Standard and/or Restricted classifica tion (see NOTE 3) except Model 7AC is limited to certification in Standard classification only. All propeller limits apply with the exception of those listed below: Static r.p.m. at maximum permissible throttle setting : Model 9 Seeder, Duster and Low Gallonage Sprayer and Model 11 Low Gallonage Sprayer: Fixed Pitch Wood Propellers Model 7AC Model 7EC Not over 2250 2350 Not under 2050 2200 Fixed Pitch Metal Propellers Model 7EC Not over 2350 Not under 2200 Model 9 and 11 High Gallonage Sprayer: Fixed Pitch Wood Propellers Model 7AC Model 7GC Not over 2250 2350 Not under 2200 2275 Fixed Pitch Metal Propellers Model 7AC Model 7EC Not over 2250 2350 Not under 2175 2250 Placards: In full view of pilot: "All acrobatics including spins prohibited ." On spray tank: "Allowable weight tank contents to be determined from weight and balance. Do not exceed 450 lb." LOW GAL. 60 lb. HIGH GAL. 84 lb. DUSTER AND 47 lb. (+19) (+16) SEEDER (+33) *614. Crop sprayer instln. consisting of items (a) and (b) below: (a) Crop Sprayer instln., Independent Crop Dusting, Inc., Campbell, CA, two-unit Rotary Spray Kit, when installed per Independent Crop Dusting, Inc., instructions for instln. of two Series 700 Rotors dated February 1, 1950. Eligible for certification in Standard and/or Restrict ed Classification (see NOTE 3) except Model 7AC with wood propeller is limited to certification in Standard Classification only. (Kit does not include tank). (b) Sprayer tank for approved sprayer instln. when installed per Independent Crop Dusting, Inc., "Mounting Kit A-700-1" instructions and dwg. dated July 31, 1950.. Placards required: In full view of pilot: "All acrobatics including spins prohibited." On spray tank: "Maximum tank load to be determined from weight and balance. Do not exceed 264 lb." 25 lb. 30 lb. (+34) (+36) *615. Crop sprayer instln., Svedy-Sorensen s eat tank sprayer installed per Svedy- Sorensen dwg. 16 and installation instructions dated November 2, 1951. 59 lb. (+21) 616. Fiberglass wing tip modification (C hampion dwg. 7-1085) Models 7AC, 7BCM, 7CCM, 7DC, 7EC, 7FC. No wt. change 617. Sorensen sprayer unit per Champion dwg. 7-1113. (Models 7GC and 7GCA only). Eligible for certification under regulati ons of CAR 8 and CAM 8 only. Maximum gross weight 7GC, 2100 lb., 7GCA, 2150. Placards required: In full view of pilot: "All acrobatics including spins prohibited." "Restricted Category speed limitations: Maximum level speed 92 m.p.h., never exceed speed 123 m.p.h." On spray tanks: "Allowable weight of tank contents to be determined from weight and balance. Do not exceed 810 lb." 125 lb. (+7.5) 618. Clamp-on dorsal fin, Models 7AC and 7B CM (Aeronca dwg. 4-678) 3 lb. (+148) 619. Sorensen sprayer unit per Champion dwg. 7-1113. (Models 7GCAA, 7GCB, 7GCBC). Eligible for certification under regulations of CAR 8 and CAM 8 only. Maximum gross weight 2325 lb. Placards required: In full view of pilot: "All acrobatics including spins prohibited." "Restricted Category Speed Limitations: Maximum level speed 115 m.p.h., never exceed speed 121 m.p.h." On spray tanks: "Allowable weight of tank contents to be determined from weight and balance. Do not exceed 810 lb." 128 lb. (+7) 620. Champion combination sprayer- duster unit (Model 7GCBA only) (a) Hopper instln. only per Champion Installation dwg. 4-1167, 4-1182, 4-1194, 7-1163, 7-1169, 7-1172, 7-1178. 101 lb. (+33) A-759 Page 32 of 37 (b) Hopper and duster unit only per Champion instln. dwg. 4-1167, 4-1182, 4-1194, 7-1163, 7-1169, 7-1172, 7-1178. 172 lb. (+30.5) (c) Hopper and sprayer unit only per Champion instln. dwg. 4-1167, 4-1182, 4-1194, 7-1163, 7-1169, 7-1172, 7-1178. 197 lb. (+22.5) (d) Hopper and duster-sprayer unit combination complete per Champion instln. dwg. 4-1167, 4-1182, 4-1194, 7-1163, 7-1169, 7-1172, 7-1178. 239 lb. (+22.5) 621. Horizontal Tail Surfaces Model Applicability Model 4-867 Stab. 4-869 4-870 Elev. 4-1413 Stab. 4-1414 4-1415 Elev. 4-1481 Stab. 4-1482 4-1483 Elev. 4-1481 Stab. 4-1671 4-1700 Elev. 7ECA x x x x Seaplane x x x x Skiplane x x x x 7GCAA x x x Skiplane x x x 7GCB x x 7GCBA x x 7GCBC x x x Seaplane x* x** x Skiplane x x x 7KCAB x x x 7ACA x *With Pee Kay 1800 Floats **With Edo 89-2000 Floats Other models approved with 4-867 Stab. and 4-870 Elev. only. 4-1414-5 and 4-1415-5 Elev. are alternates for 4-1414 and 4-1415 Elev. 622. Tow Hitch Installation Tow Hitch instln. per Champion dwg.7-1143 Models 7ECA, 7GCAA, 7GCB, 7GCBC, 7KCAB 4 lb. (+111) 623. Metal Belly Skin Instln. per Bellanca dwg. 4-1579 Models 7ECA, 7GCAA, 7GCBC, 7KCAB 14 lb. (+66) NOTE 1. Current weight and balance report includi ng list of equipment included in certificated empty weight and loading instructions when necessary mu st be provided for each aircraft at the time of original certification. The certificated empty weight and C.G. location must include unusable fuel of 6 lb. at (+15) in. on Models 7ECA, 7GCAA, 7GCBC, 7KCAB with items 119 or 123(a) Fuel tanks installed. NOTE 2. The following placards shall be displayed: (a) Baggage Compartment: (1) (Models 7AC and S7AC) "Maximum baggage - 40 lb. solo front, 20 lb. solo rear." (2) (Models 7EC, 7FC, 7GC, 7GCA, 7GCB, 7HC, 7JC, 7KC) "Maximum baggage 50 lb." (3) (Models 7ECA, 7GCAA, 7GCBC, 7KCAB) "Maximum baggage 100 lb." (4) (Model 7ACA) "Maximum baggage 40 lb." (b) In front and clear view of pilot: (1) (Model 7BCM) "Do not exceed 95 m.p.h. TIAS in level flight at any time." "Solo from front seat only." (2) (Model S7AC with item 106) "Solo from front seat only." (3) (Models 7CCM and 7DC) "Do not exceed 100 m.p.h. TIAS in level flight." "Do not exceed 135 m.p.h. TIAS." "Solo from front seat only." "Intentional spinning pr ohibited when carrying baggage." "Avoid abrupt throttle operation." (For t hose models equipped with carburetor engine only.) (4) (Models S7CCM, S7DC) "Do not exceed 129 m.p.h. TIAS." "Solo from front seat only." "Avoid abrupt throttle operation." (For t hose models equipped with carburetor engine only.) (5) (Models 7EC and 7FC) "Intentional spinning pr ohibited when carrying baggage." (6) (Models 7GC, 7GCA) "Solo from front seat only." "Intentional spinning prohibited." (7) (Model 7HC) "Solo from front seat only." "Intentional spinning prohibited." "Refer to loading schedule for loading information." A-759 Page 33 of 37 (8) (Model 7JC) "Occupy front seat when flying solo." (9) (Model 7KC) "Intentional spinning prohibited." (10) (Models 7ECA, 7GC, 7GCB, 7GCBC, 7HC) In addition to the above applicable plac ards, the following is required when Item 204(c) is installed: "For seaplane use, do not exceed 137 m.p.h." "Intentional spinning prohibited." (11) (Model 7GCBA) "All acrobatics including spins prohibited." (12) (Model 7GCB) "Occupy front seat when flying solo." "Refer to loading schedule for loading information." "Do not exceed 135 MPH IAS during negative G condition." "Landplane approved for only following acrobatic maneuvers: Maneuver Entry Speed (IAS) m.p.h. Knots Chandelle, Lazy Eight 120 104 Barrel or Slow Roll 120 104 Immelmann 145 126 Loop or Clover Leaf 140 122 Split S 80 70 Snap Roll 85 74 Hammerhead Turn 140 122 Cuban Eight 145 126 Spin Slow Deceleration Do not exceed +5.0 or -2.0 G load factor. Do not exceed 135 m.p.h. IAS during negative G condition. Do not perform acrobatics in tur bulent air. Caution: Negative G will cause loss of oil and oil pressure. Use of flaps dur ing acrobatics prohibited. To recover from spin, use full opposite rudder and neutralize elevator. (13) (Model 7ECA, 7GCAA) "Occupy front seat when flying solo." "Do not exceed 135 m.p.h. during negative G condition." "Landplane approved for only following acrobatic maneuvers: Maneuver Entry Speed (IAS) m.p.h. Knots Chandelle, Lazy Eight 120 104 Barrel or Slow Roll 120 104 Immelmann 145 126 Loop or Clover Leaf 140 122 Split S 80 70 Snap Roll 85 74 Hammerhead Turn 140 122 Cuban Eight 145 126 Spin Slow Deceleration Do not exceed +5.0 or -2.0 G load factor. Do not exceed 135 m.p.h. IAS during negative G condition. Do not perform acrobatics in tur bulent air. Caution: Negative G will cause loss of oil and oil pressure. To recover from spin, use full opposite rudder and neutralize elevator. (14) (Model 7GCBC) "Occupy front seat when flying solo." "Do not exceed 135 m.p.h. IAS during negative G condition." "Landplane approved for only following acrobatic maneuvers: Maneuver Entry Speed (IAS) m.p.h. Knots Chandelle, Lazy Eight 120 104 Barrel or Slow Roll 120 104 Immelmann 145 126 Loop or Clover Leaf 140 122 Split S 80 70 Snap Roll 85 74 Hammerhead Turn 140 122 Cuban Eight 145 126 Spin Slow Deceleration Do not exceed +5.0 or -2.0 G load factor. Do not exceed 135 m.p.h. IAS during negative G condition. Do not perform acrobatics in tur bulent air. Caution: Negative G will cause loss of oil and oil pressure. Use of flaps dur ing acrobatics prohibited. To recover from spin, use full opposite rudder and neutralize elevator. A-759 Page 34 of 37 (15) (Model 7KCAB) with IO-320-E2A or IO-320-E2B (Modified per STC SE7CE) "Occupy front seat when flying solo." "Do not exceed 135 m.p.h. IAS during negative G condition." "Landplane approved for only following acrobatic maneuvers: Maneuver Entry Speed (IAS) m.p.h. Knots Chandelle, Lazy Eight 120 104 Barrel or Slow Roll 120 104 Immelmann 145 126 Loop or Clover Leaf 140 122 Split S 80 70 Snap Roll 85 74 Hammerhead Turn 140 122 Cuban Eight 145 126 Spin Slow Deceleration Level Inverted Flight 120 104 135 m.p.h. (117 KTS) IAS Max Do not exceed +5.0 or -2.0 G load factor. Do not exceed 135 m.p.h. IAS during negative G condition. Do not perform acrobatics in turbul ent air. Inverted flight limited to 2 min. Monitor oil press. while inverted to insure minimum of 60 psi. To recover from spin, use full opposite rudder and neutralize elevator. (Model 7KCAB with AEIO-320-E2B) "Occupy front seat when flying solo." "Do not exceed 135 m.p.h. IAS during negative G condition." "Landplane approved for only following acrobatic maneuvers: Maneuver Entry Speed (IAS) m.p.h. Knots Chandelle, Lazy Eight 120 104 Barrel or Slow Roll 120 104 Immelmann 145 126 Loop or Clover Leaf 140 122 Split S 80 70 Snap Roll 85 74 Hammerhead Turn 140 122 Cuban Eight 145 126 Spin Slow Deceleration Level Inverted Flight 120 104 135 m.p.h. (117 KTS) IAS Max Do not exceed +5.0 or -2.0 G load factor. Do not exceed 135 m.p.h. IAS during negative G condition. Do not perform acrobatics in tur bulent air. 2 min. of inverted fuel normally available. Momentary oil pressure interrupti ons are normal. To recover from spin, use full opposite rudder and neutralize elevator. (16) (Model 7GCBC with O-320-A2B Lyco ming engine and item 204(d) installed) "For Seaplane use: Acrobatics including spins prohibited. Maximum glide or dive speed 148 m.p.h. (128 knots) CAS Maximum level speed 110 m.p.h. ( 95 knots) CAS Maximum flaps extended speed 90 m.p.h. ( 78 knots) CAS" (17) (Model 7ACA) "Do not exceed 129 TIAS." "Occupy front seat when flying solo." (c) On left side of fuselage, next to rear seat: (1) (Model 7HC) "Maximum rear seat load, 250 lb. Remove rear stick with two occupants." (2) (Model 7GCB) (When usi ng adjustable rear seat) "Maximum rear seat load, 250 lb. Remove rear stick with two occupants." (d) On cabin door rear window: (1) (Model 7GCBA) "Restricted." (e) On top of hopper in plain view of ground crew filling the hopper: (1) (Model 7GCBA) "Maximum hopper load 900 lb." NOTE 3. Mandatory inspection times for strut atta ch fitting 3-1692 (7ECA, 7GCAA, 7GCBC, and 7KCAB) on metal spar winged aircraft must be inspected in accordance with American Champion Aircraft Airworthiness Limitations, dated May 9, 1996 or later FAA approved revision. A-759 Page 35 of 37 NOTE 4. All Model 7AC airplanes are eligible with the engine installations listed under Sections III, IV, V and VIII, when accomplished in accordance with the following Champion Service Letters: No. 13 7AC to 7BCM No. 14 7AC to 7DC No. 15 7AC to 7CCM No. 56 7AC to 7EC All Model 7EC airplanes are eligible with the engine installations listed under Section IX when accomplished in accordance with the following Champion Service Letters: No. 60 7EC to 7GC When making this conversion, the nameplate in t he airplane must be restamped with the proper model designation and the letters "CONV" added. The airplane serial number should not be changed. NOTE 5. Military S/N AAF 47-788 thru AAF 47-1296 e ligible as 7BCM. Military S/N AAF 48-424 thru AAF 48-524 eligible as 7CCM. The nameplate in the airplane must be stamped with the proper model designation. S/N 47-788 thru 47-1296 eligible as 7CCM if converted in accordance with Aeronca Service Letter No. 15. NOTE 6. (a) On aircraft S/N 7EC-732 thru 773-397 thru 472, 7GC-171, 7GCB-17 thru 194, 7HC-30 thru 39, 7JC-18 thru 25, 7KC-1 thru 4, level as follows: level aircraft laterally and longitudinally using the three leveling lugs projec ting through the left hand front floorboard. (b) On aircraft S/N's 7EC-774, 7ECA-1 and up, 7GC-172, 7GCA-172, 7GCAA-1 and up, 7GCB-195, 7GCBA-1, 7GCBC-1 and up, 7JC-26, 7KC-4, 7KCAB-1 and up, level as follows: drop plumb line from wing leading edge so that top oleo retaining bolt center line is 1/4 inch forward of wing leading edge. (c) On aircraft S/N's 7FC-473 and up, 7HC-40 and up, level as follows: drop plumb line from wing leading edge and measure 10-5/16 inches to aft face of front wing strut lug. (d) Models 7ECA, 7GCAA, 7GCBC, 7KCAB, 7ACA - Aircraft with spring steel gear installed, level as follows: drop plumb line from wing leading edge so that it is 10.19 inches forward of front face of fuselage wing strut fittings. NOTE 7. S/N's 7FC-2 thru 7FC-430 of model 7FC are eligible for item 201(e) wide track main gear when modified per Champion Service Letter No. 45. NOTE 8. All 7JC aircraft are eligible for conver sion to model 7EC at 1500 lb. maximum weight when modified per Champion Service Letter No. 49. NOTE 9. S/N's 7HC-1 thru 7HC-32 of model 7HC are eligible for item 201(e) wide track main gear when modified per Champion Service Letter No. 50. NOTE 10. Model 7GCB eligible for acrobatic maneuv ers listed in NOTE 2(b)( 12), Model 7ECA and 7GCAA eligible for acrobatic maneuvers listed in NOTE 2(b)(13), Model 7GCBC eligible for acrobatic maneuvers listed in NOTE 2(b)(14), and Model 7K CAB eligible for acrobatic maneuvers listed in NOTE 2(b)(15) when Quick Release Door is installed per Champion dwg. 4-1203. As a replacement item on acrobatic categor y 7ECA, 7GCAA, 7GCB, 7GCBC, 7KCAB aircraft, the following metal-to-metal type seat belts should be installed inlieu of metal-to-fabric cam type buckle seat belts to preclude inadv ertent release during acrobatics: 1. Rubert Parachute Company, Model 65 (or 82) 2. Cummings and Sander Model CS 9700-AC-50 3. Equivalent TSO approved bel t with metal-to-metal buckle NOTE 11. In order to comply with the requirement s of Part 36 of the Federal Aviation Regulations, revised engine limits have been established for the M odel 7GCBC seaplane (S/N 1198-80 and up). The revised limits are: Engine limits: Maximum normal operating, 2500 r.p.m. (118 hp.) For all other operations, 2700 r.p.m. (150 hp.) A-759 Page 36 of 37 NOTE 12. Effective March 1, 1979, each Model 7ECA , 7GCAA, and 7GCBC airplane contains as FAA Approved Airplane Flight Manual which is par t of the required equipment. The AFM must remain in the airplane during aircraft operations. Airplane Flight Manuals are requi red for the following airplanes: Model Beginning Serial Number 7ECA 1295-79 7GCAA 378-79 7GCBC 1108-79 Only 1110-79 Any 7GCBC retrofit with 7-1545 wings NOTE 13. The following changes apply to 7GCBC airc raft built in 1994 and later (all with 7-1545 wings). C.G. Range and Maximum Weight changes apply to any 7GCBC that retrofits with 7-1545 wings except for airplanes with optional engine item 122. C.G. Range: Landplane: (+14.2) to (+19.2) at 1800 lb. (+10.5) to (+19.2) at 1325 lb. or less When performing acrobatic maneuvers, the C.G. range shall be limited to: (+14.2) to (+16.3) at 1800 lb. (+10.5) to (+16.3) at 1350 lb. or less Straight line variation between points given. Maximum Weight, Landplane: 1800 lb. Serial Nos. Eligible 1200-94 thru 1202-94, 1203-95 and up For Serial Nos. 1360-2004 and up with opti onal engine item 126 or 127; when performing acrobatic maneuvers (see Note 10) the airpl ane must be loaded as shown above. The airplane may otherwise be operated in the Normal category as shown below. C.G. Range Landplane: (+15.4) to (+19.2) at 1950 lb. (+10.5) to (+19.2) at 1325 lb. or less Straight line variation between points given. Maximum Weight, Landplane 1950 lb. Required Equipment Item 126 or 127 NOTE 14. Aircraft having sprayer or duster installati ons which are listed in th is specification as being eligible for certification and were certificated in the restricted category prior to October 11, 1950, may continue to be operated with the following additional limitations: Models Models Models 7AC & 7BCM 7CCM & 7DC 7EC (a) Maximum takeoff weight (lb.) 1300 1430 1595 Maximum landing weight (lb.) 1340 1340 1450 Maneuvering speed m.p.h. True Ind. (at max. wt.) 89 95 97 (b) The following placard must be in full view of the pilot: "Maneuvering speed at maximum weight not to exceed (see NOTE 3(a)) m.p.h. - Intentional spins prohibited." The C.G. range restricted certification is the same as that listed for each model in standard category except the restricted maximum weight value is substituted in lieu of the standard maximum weight. All original certification in the restricted category after October 11, 1950, must be in accordance with CAR 8 and CAM 8. A-759 Page 37 of 37 NOTE 15. The following changes apply to 7ECA and 7GCAA aircraft built in 1995 and later (all with 7-1566 wing frames). C.G. Range and Maximum Weight changes also apply to any 7ECA, 7GCAA, or 7KCAB that retrofits with 7-1566 wing frames or 7-1567 covered wing frames. C.G. Range: Landplane: (+14.2) to (+19.2) at 1750 lb. (+10.5) to (+19.2) at 1325 lb. or less When performing acrobatic maneuvers, the C.G. range shall be limited to: (+14.2) to (+16.3) at 1750 lb. (+10.5) to (+16.3) at 1325 lb. or less Straight line variation between points given. Maximum Weight Landplane: 1750 lb. Serial Nos. Eligible 7ECA: 1355-95 and up 7GCAA: 400-97 and up NOTE 16. The following changes apply to 7EC aircraft built in 2006 and later Engine Continental O-200-A or O-200-D Fuel 80 minimum grade aviation gasoline (O-200-A) 100LL minimum grade aviation gasoline (O-200-D) Engine Limits For all operations, 2750 r.p.m. (100 hp.) Airspeed Limits Level flight or c limb 100 m.p.h. (87 knots) True Ind. Glide or dive 135 m.p.h. (117 knots) True Ind. C.G. Range Normal Category: (+14.0) to (+19.2) at 1320 lb. (+11.0) to (+19.2) at 1100 lb. or less Utility Category: (+14.0) to (+18.2) at 1320 lb. (+11.0) to (+18.2) at 1100 lb. or less Straight line variation between points given. Empty wt. C.G. Range None Maximum Weight 1320 lb. No. of Seats 2 (1 at +11.5, 1 at +43) 2 (1 at +11 to +14 with item 404(n), 1 at +43) Maximum Baggage 100 lbs. at +69 Fuel Capacity 18 gal. At +24.5 Oil Capacity 6 qt. at –35 (O-200-A) 5 qt at –35 (O-200-D) Control Surface Movements Elevator Up 24 o Down 24 o Elevator Trim Tab Up 17.5 o Down 37.5 o Ailerons Up 28.5 o Down 18 o Rudder Right 25 o Left 25 o Serial Nos. Eligible 1000-2006 and up Required Equipment Items 25, 111(i), 118(f), 201(o), 202(g), 307(w), 311(e), 409(d) -- END -- ``` ## ADs (35, in force first) - [AD 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI or SA02658SE). Effective Mar 21, 2022 - [AD 2010-13-10](https://openairdocs.org/ad/2010-13-10): Propeller governors · American Champion 7GCAA, DA 40, A36 and 1 more. Effective Aug 5, 2010 - [AD 2009-22-02](https://openairdocs.org/ad/2009-22-02): Rear seat back hinge area and excessive elongation of the rear seat hinge bolt hole · American Champion 7ECA, 7GCAA, 7GCBC and 3 more. Effective Dec 3, 2009 - [AD 2006-12-07](https://openairdocs.org/ad/2006-12-07): ECi cylinder assemblies · Aerostar AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 386 more. Effective Jul 11, 2006 - [AD 2006-03-08](https://openairdocs.org/ad/2006-03-08): Vacuum pumps · Aero Advantage 14-19, 14-19-2, 14-19-3 and 299 more. Effective Mar 10, 2006 - [AD 2005-24-10](https://openairdocs.org/ad/2005-24-10): Pilot's Operating Handbook (POH) limitation · American Champion 7AC, 7ACA, 7BCM (Army L-16A) and 21 more. Effective Jan 17, 2006 - [AD 2000-25-02 R1](https://openairdocs.org/ad/2000-25-02-R1): Wood Spars · American Champion 11AC, 11BC, 11CC and 27 more. Effective Jul 13, 2001 - [AD 96-18-02](https://openairdocs.org/ad/96-18-02): Wing Strut Attach Fittings · American Champion 7ECA, 7GCAA, 7GCBC and 3 more. Effective Sep 20, 1996 - [AD 96-09-06](https://openairdocs.org/ad/96-09-06): Air Filter Assemblies · Maule Aerospace Technology 7ACA, 7ECA, 7FC and 180 more. Effective Jun 7, 1996 - [AD 89-18-06](https://openairdocs.org/ad/89-18-06): Front Folding Seats · American Champion 7ECA, 7GCAA, 7GCBC and 3 more. Effective Sep 21, 1989 - [AD 80-25-07 R1](https://openairdocs.org/ad/80-25-07-R1): Oil Coolers · American Champion 7ECA, 7GCAA, 7GCBC and 39 more. Effective Sep 24, 1981 - [AD 81-16-04](https://openairdocs.org/ad/81-16-04): Competition Harness Installation · American Champion 7ECA, 7GCAA, 7GCBC and 2 more. Effective Jul 28, 1981 - [AD 80-21-06](https://openairdocs.org/ad/80-21-06): Muffler Core and Body Assembly · American Champion 7ECA, 7GC, 7GCA and 8 more. Effective Oct 16, 1980 - [AD 47-20-01](https://openairdocs.org/ad/47-20-01): Gascolator Bowl Cleaning · American Champion 11AC, 7AC and 7BCM (Army L-16A). Effective Mar 18, 1980 - [AD 79-22-01](https://openairdocs.org/ad/79-22-01): Exhaust System · American Champion 7ECA, 8GCBC and 8KCAB. Effective Oct 29, 1979 - [AD 79-07-02](https://openairdocs.org/ad/79-07-02): Batteries · Aircraft Parts & Development A, A-2, A-3 and 149 more. Effective Apr 3, 1979 - [AD 77-22-05](https://openairdocs.org/ad/77-22-05): Operating Limitations · American Champion 7ECA, 7GC, 7GCA and 5 more. Effective Nov 7, 1977 - [AD 76-22-01](https://openairdocs.org/ad/76-22-01): Adjustable Front Seat · American Champion 7ECA, 7GCAA, 7GCBC and 3 more. Effective Nov 2, 1976 - [AD 75-17-16](https://openairdocs.org/ad/75-17-16): Engine Power Loss · American Champion 7ECA, 7GCAA, 7GCBC and 3 more. Effective Aug 12, 1975 - [AD 72-20-06](https://openairdocs.org/ad/72-20-06): Aerobatic Flight Placard · American Champion 7ECA, 7GCAA, 7GCBC and 2 more. Effective Oct 5, 1972 - [AD 72-18-03](https://openairdocs.org/ad/72-18-03): Corrosion of Rudder and Elevator Cables · American Champion 7GCAA, 7GCBC, 7KCAB and 1 more. Effective Sep 1, 1972 - [AD 71-20-04](https://openairdocs.org/ad/71-20-04): Lower Fuselage Longeron · American Champion 7ECA, 7GCAA, 7GCBC and 1 more. Effective Sep 30, 1971 - [AD 67-03-02](https://openairdocs.org/ad/67-03-02): Fuel Shutoff Valve Bracket · American Champion 7ECA, 7GCAA, 7GCB and 1 more. Effective Jan 18, 1967 - [AD 64-04-03](https://openairdocs.org/ad/64-04-03): Air Door Hinge · American Champion 7GC, 7GCA, 7GCB and 3 more. Effective Mar 9, 1964 - [AD 47-20-02](https://openairdocs.org/ad/47-20-02): Oleo Piston · American Champion 11AC and 7AC - [AD 47-30-01](https://openairdocs.org/ad/47-30-01): Lift Strut Wing Attach Fittings · American Champion 11AC and 7AC - [AD 47-30-05](https://openairdocs.org/ad/47-30-05): Exhaust Stack Inspection · American Champion 11AC and 7AC - [AD 48-04-02](https://openairdocs.org/ad/48-04-02): Wing Rib Rework · American Champion 11AC, 11BC and 7AC - [AD 48-08-02](https://openairdocs.org/ad/48-08-02): Cleveland Wheels · American Champion 11AC, 11BC, 11CC and 33 more - [AD 48-39-01](https://openairdocs.org/ad/48-39-01): Control Stick Rework · American Champion 7AC, 7ACA, 7BCM (Army L-16A) and 19 more - [AD 49-11-02](https://openairdocs.org/ad/49-11-02): Wing Attach Fitting · American Champion 11AC, 11BC, 11CC and 4 more - [AD 56-04-01](https://openairdocs.org/ad/56-04-01): Control Stick Socket Castings · American Champion 7EC - [AD 57-20-01](https://openairdocs.org/ad/57-20-01): Fireproof Steering Link Boot · American Champion 7FC - [AD 2000-25-02](https://openairdocs.org/ad/2000-25-02) (historical): Wood Wing Spars · American Champion 11AC, 11BC, 11CC and 15 more. Effective Jan 19, 2001 - [AD 96-03-11](https://openairdocs.org/ad/96-03-11) (historical): Wing Front Strut Fittings · American Champion 7ECA, 7GCBC, 8GCBC and 1 more. Effective Feb 26, 1996 ## Registered aircraft by registry model (OpenAirDocs) - [Aeronca 7AC](https://openairdocs.org/model/aeronca-7ac): 1,878 aircraft (registry code 2110102) - [Bellanca 7GCBC](https://openairdocs.org/model/bellanca-7gcbc): 487 aircraft (registry code 1220601) - [Champion 7ECA](https://openairdocs.org/model/champion-7eca): 419 aircraft (registry code 21101NN) - [Bellanca 7ECA](https://openairdocs.org/model/bellanca-7eca): 347 aircraft (registry code 1220460) - [American Champion 7GCBC](https://openairdocs.org/model/american-champion-7gcbc): 232 aircraft (registry code 21101PL) - [Bellanca 7KCAB](https://openairdocs.org/model/bellanca-7kcab): 230 aircraft (registry code 1220701) - [Aeronca 7BCM](https://openairdocs.org/model/aeronca-7bcm): 175 aircraft (registry code 2110106) - [Champion 7FC](https://openairdocs.org/model/champion-7fc): 164 aircraft (registry code 21101NX) - [Champion 7EC](https://openairdocs.org/model/champion-7ec): 157 aircraft (registry code 21101NM) - [Champion 7KCAB](https://openairdocs.org/model/champion-7kcab): 151 aircraft (registry code 21101P3) - [Champion 7AC](https://openairdocs.org/model/champion-7ac): 144 aircraft (registry code 21101MA) - [Champion 7GCBC](https://openairdocs.org/model/champion-7gcbc): 144 aircraft (registry code 21101PK) - [Aeronca 7DC](https://openairdocs.org/model/aeronca-7dc): 121 aircraft (registry code 2110116) - [American Champion 7GCAA](https://openairdocs.org/model/american-champion-7gcaa): 119 aircraft (registry code 2121002) - [Bellanca 7GCAA](https://openairdocs.org/model/bellanca-7gcaa): 118 aircraft (registry code 1220501) - [Champion 7GCAA](https://openairdocs.org/model/champion-7gcaa): 114 aircraft (registry code 21101N8) - [Aeronca 7CCM](https://openairdocs.org/model/aeronca-7ccm): 91 aircraft (registry code 2110110) - [Champion AERONCA 7AC](https://openairdocs.org/model/champion-aeronca-7ac): 58 aircraft (registry code 2110140) - [Champion 7GCB](https://openairdocs.org/model/champion-7gcb): 55 aircraft (registry code 21101PC) - [Aeronca 7EC](https://openairdocs.org/model/aeronca-7ec): 52 aircraft (registry code 2110120) - [Bellanca 7ACA](https://openairdocs.org/model/bellanca-7aca): 44 aircraft (registry code 1220438) - [American Champion 7EC](https://openairdocs.org/model/american-champion-7ec): 38 aircraft (registry codes 2120001, 2120002, 2120004) - [American Champion 7ECA](https://openairdocs.org/model/american-champion-7eca): 38 aircraft (registry code 2120003) - [Champion 7GC](https://openairdocs.org/model/champion-7gc): 37 aircraft (registry code 21101N2) - [Champion 7CCM](https://openairdocs.org/model/champion-7ccm): 20 aircraft (registry code 21101MW) - [Champion 7BCM](https://openairdocs.org/model/champion-7bcm): 19 aircraft (registry code 21101ML) - [Champion AERONCA 7FC](https://openairdocs.org/model/champion-aeronca-7fc): 18 aircraft (registry code 2110162) - [Champion AERONCA 7BCM](https://openairdocs.org/model/champion-aeronca-7bcm): 17 aircraft (registry code 2110144) - [Champion AERONCA 7EC](https://openairdocs.org/model/champion-aeronca-7ec): 14 aircraft (registry code 2110158) - [Champion 7HC](https://openairdocs.org/model/champion-7hc): 8 aircraft (registry code 21101PN) - [Champion 7DC](https://openairdocs.org/model/champion-7dc): 7 aircraft (registry code 21101NB) - [Champion AERONCA 7DC](https://openairdocs.org/model/champion-aeronca-7dc): 7 aircraft (registry code 2110154) - [Champion AERONCA 7GC](https://openairdocs.org/model/champion-aeronca-7gc): 7 aircraft (registry code 2110164) - [Champion AERONCA 7CCM](https://openairdocs.org/model/champion-aeronca-7ccm): 6 aircraft (registry code 2110148) - [Aeronca 7FC](https://openairdocs.org/model/aeronca-7fc): 5 aircraft (registry code 2110124) - [Champion 7JC](https://openairdocs.org/model/champion-7jc): 4 aircraft (registry code 21101PT) - [Aeronca 7EC CONV](https://openairdocs.org/model/aeronca-7ec-conv): 3 aircraft (registry code 2110113) - [Aeronca S7AC](https://openairdocs.org/model/aeronca-s7ac): 3 aircraft (registry code 2110104) - [Aeronca S7CCM](https://openairdocs.org/model/aeronca-s7ccm): 3 aircraft (registry code 2110114) - [Champion 7EC(CONV)](https://openairdocs.org/model/champion-7ec-conv): 3 aircraft (registry code 21101NL) - [Champion AERONCA 7GCB](https://openairdocs.org/model/champion-aeronca-7gcb): 3 aircraft (registry code 2110168) - [Champion AERONCA 7HC](https://openairdocs.org/model/champion-aeronca-7hc): 3 aircraft (registry code 2110172) - [Aeronca 7GC](https://openairdocs.org/model/aeronca-7gc): 2 aircraft (registry code 2110126) - [American Champion 7AC](https://openairdocs.org/model/american-champion-7ac): 2 aircraft (registry code 2120005) - [Champion 7GCA](https://openairdocs.org/model/champion-7gca): 2 aircraft (registry code 21101N7) - [Champion 7GCBA](https://openairdocs.org/model/champion-7gcba): 2 aircraft (registry code 21101PH) - [Aeronca 7GCB](https://openairdocs.org/model/aeronca-7gcb): 1 aircraft (registry code 2110130) - [Aeronca 7GCBC](https://openairdocs.org/model/aeronca-7gcbc): 1 aircraft (registry code 2110133) - [Aeronca CHAMPION 7BCM](https://openairdocs.org/model/aeronca-champion-7bcm): 1 aircraft (registry code 0190151) - [Aeronca S7DC](https://openairdocs.org/model/aeronca-s7dc): 1 aircraft (registry code 2110118) All 82: https://openairdocs.org/tcds/A-759/aircraft.md ## STCs approved under this data sheet (299, first 50) - [STC SA01233SE](https://openairdocs.org/stc/SA01233SE): Fabrication and installation of Alaskan Bushwheel LLC tail wheel and fork assembly. ABI, LLC - [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).. Garmin International Inc. - [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.. TCW Technologies, LLC - [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC - [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC - [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC - [STC SA02636SE](https://openairdocs.org/stc/SA02636SE): Installation of Garmin GPS 175 Navigation System and GNX 375 Navigation System with ADS-B In/Out Transponder.. Garmin International Inc. - [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc. - [STC SA800EA](https://openairdocs.org/stc/SA800EA): Installation of Whelen Anti-Collision, Position, or Anti-Collision/Position Light System, and applicable associated power supplies. Whelen Aerospace Technologies - [STC SA00079NY](https://openairdocs.org/stc/SA00079NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K008 on single and multi engine fixed wing light aircraft incorporating Teledyne Continental reciprocating engines of 450 horsepower or less.. Airwolf Filter Corporation - [STC SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc. - [STC SA33CE](https://openairdocs.org/stc/SA33CE): If Champion Part Number 7-480 door is installed, remove two of AN 380-2-2 cotter pins and two of AN 393-3 flat head pins as necessarry to remove one door. If American Champion Part Number 7-1265 door is installed, remove quick release pins to remove one door. Weight change --10lb at +21.06 arm. National Aeronca Association - [STC SA00081NY](https://openairdocs.org/stc/SA00081NY): Installation of Iceman Aviation Supplies, Inc. Carburetor Ice Detector.. Alcor LLC - [STC SA04046CH PAGE 1](https://openairdocs.org/stc/SA04046CH%20PAGE%201): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc. - [STC SA7965SW](https://openairdocs.org/stc/SA7965SW): Application of fabric and polyurethane finishing system.. Shady Aviation LLC - [STC SA01240SE](https://openairdocs.org/stc/SA01240SE): Installation of secondary voltage indication system. Visual Instruments LLC - [STC SA2699CE](https://openairdocs.org/stc/SA2699CE): Installation of aileron spades.. Rainbow Flying Services - [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd. - [STC SA02594SE](https://openairdocs.org/stc/SA02594SE): SkyView HDX Instrumentation and Autopilot System manufactured. Dynon Avionics - [STC SA01757WI](https://openairdocs.org/stc/SA01757WI): To allow the use of UL91 or UL94 (minimum) grade aviation fuel. Swift Fuels LLC - [STC SA03898NY](https://openairdocs.org/stc/SA03898NY): Installation and maintenance of ORATEX covering and coating material. Aircraft Design & Certification Ltd - [STC SA4503NM](https://openairdocs.org/stc/SA4503NM): Remove original cloth covering and install Ceconite covering. Ceconite Division of Poly-Fiber Inc. - [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc. - [STC SA01899WI](https://openairdocs.org/stc/SA01899WI): Installation of Garmin G3X Touch Electronic Flight Instrument System. Garmin International Inc. - [STC SA02576AK](https://openairdocs.org/stc/SA02576AK): Installation of Cleveland and ABI, LLC Wheel and Brake Kits. ABI LLC - [STC SA11137SC](https://openairdocs.org/stc/SA11137SC): Installation of Plane-Power ALT-FLX alternator. Hartzell Engine Technologies, LLC - [STC SA3-214](https://openairdocs.org/stc/SA3-214): Installation of Wipaire Skis Model3000 main skis and Model 1000 tail ski.. F.Atlee Dodge Aircraft Services - [STC SA3-361](https://openairdocs.org/stc/SA3-361): Installation of Wipaire Skis Model C-2200 main and Model CTF-2200 tail wheel skis.. F.Atlee Dodge Aircraft Services - [STC SA3-362](https://openairdocs.org/stc/SA3-362): Installation of Wipaire Skis Model C-2200 main and Model CTF-2200 tail wheel skis.. F.Atlee Dodge Aircraft Services - [STC SA3-368](https://openairdocs.org/stc/SA3-368): Installation of Wipaire Skis Model A2000A main wheel replacement ski.. F.Atlee Dodge Aircraft Services - [STC SA3-424](https://openairdocs.org/stc/SA3-424): Installation of Wiparie Skis Model CTF-2200 (Acft Skis) (FluiDyne) (Federal) tail ski on airplanes equipped with Scott Model 3000 tail wheel.. F.Atlee Dodge Aircraft Services - [STC SA3-628](https://openairdocs.org/stc/SA3-628): Installation of Wipaire Skis Model3000 main and Model 1000 nose skis.. F.Atlee Dodge Aircraft Services - [STC SA02987CH](https://openairdocs.org/stc/SA02987CH): Installation of the Electroair Electronic Ignition System. Electroair Acquisition Corporation - [STC SA04776NY](https://openairdocs.org/stc/SA04776NY): The HIPEC Covering and Finishing System must be performed and maintained. HIPEC Aircraft Coatings Inc. - [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC - [STC SA02153AK](https://openairdocs.org/stc/SA02153AK): Installation of Burl's Aircraft Rebuild Magnum I tail wheel Penetration ski. Burl's Aircraft Rebuild LLC - [STC SA03819NY](https://openairdocs.org/stc/SA03819NY): Installation and maintenance of Oratex 6000 Covering and Coating System. Lanitz-Prena Folien Factory GmbH - [STC SA01015SE](https://openairdocs.org/stc/SA01015SE): Installation of eligible Alaska Bushwheel, Inc. wheels and TSO-C62d tires. ABI LLC - [STC SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc. - [STC SA02553AK](https://openairdocs.org/stc/SA02553AK): Fabrication and installation of a Tail Wheel Anti-Shimmy Dampener. Keller Engineering Group LLC - [STC SA11174SC PAGE 1](https://openairdocs.org/stc/SA11174SC%20PAGE%201): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King) - [STC SA1151NW](https://openairdocs.org/stc/SA1151NW): Installation of the Flight Grip Model 135 Control Stick Grip. Air Products & Parts LLC - [STC SA10822SC](https://openairdocs.org/stc/SA10822SC): Installation of EFD1000 Primary Flight Display. Aspen Avionics Inc. - [STC SA220SO](https://openairdocs.org/stc/SA220SO): Tow bar, release mechanism, and safety tow link.. Fliegen Works Inc. d/b/a Pacific Aerial Tow Hooks - [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation - [STC SA00410BO](https://openairdocs.org/stc/SA00410BO): Installation of an AV-30-C Multi-Mode Indicator. uAvionix Corporation - [STC SA01831WI](https://openairdocs.org/stc/SA01831WI): To allow the use of UL91 (minimum) grade aviation fuel. Petersen Aviation Inc - [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation - [STC SA04205CH](https://openairdocs.org/stc/SA04205CH): Installation of Engines and propellers. C William Pancake Jr - [STC SA04301CH](https://openairdocs.org/stc/SA04301CH): Attachment of fabric covering and wing leading edge. C William Pancake Jr All 299: https://openairdocs.org/tcds/A-759/stcs.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.