TCDS A-759

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