TCDS A-796

Page No. 1 2 3 4 5 Rev. No. 14 14 14 14 14 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A-796 Revision 14 AMERICAN CHAMPION (Bellanca) (Trytek) (Aeronca) 11CC S11CC August 1, 1991 AIRCRAFT SPECIATION NO. A-796 Type Certificate Holder: American Champion Aircraft Corporation P.O. Box 37 Rochester, WI 53167 I. Model 11CC, 2 PCLM (Normal Category), 2 PCLM (Utility Category), approved May 10, 1948 Engine Continental C-85-8F Fuel 80 minimum octane aviation gasoline Engine Limits For all operations, 2575 r.p.m. (85 hp) Airspeed Limits (CAS) Maneuvering 90 m.p.h. (normal) 94 m.p.h. (utility) Maximum structural cruising 100 m.p.h. (normal) 100 m.p.h. (utility) Never exceed 126 m.p.h. (normal) 135 m.p.h. (utility) Propeller Limits Static rpm at maximum permissible throttle setting: (with Item 1(a)) Not over 2465, not under 2300. No additional tolerance permitted. Diameter: not more than 72 in., not less than 70 in. C.G. Range Normal Category (+14.3) to (+22.0) Utility Category (+14.3) to (+19.7) Empty Wt. C.G. Range (+15.5) to (+16.5). Usable only where operation of airplane is to be confined to Normal Category. For operation in Utility Category, full computations are necessary. Range given is not valid for non-standard arrangements. Maximum Weight 1350 lbs. (normal); 1290 lbs. (utility) No. of Seats 2 (adjustable from +21.5 to +25.5) Maximum Baggage 70 lbs. (+48.5) Fuel Capacity 22 gal. - Main 15 gal. (-6), Auxiliary 8 gal. (+60) Oil Capacity 4.5 qt. (-32) Control Surface Movements Elevator Up 24° Down 26° Elevator trim tab Up 14° Down 44.5° Ailerons Up 28.5° Down 18° Rudder Right 28° Left 28° Serial Nos. Eligible 11CC-1 and up. Required Equipment: Landplane: Items 1(a), 101, 102, 106, 201, 202, 203, and 401(a) Sailplane: Items 1(a), 101, 102, 106, 209, and 401(a) and 401(c) A-796 2 II. Model S11CC, 2 PCSM (Normal Category), 2 PCSM (Utility Category), approved October 29, 1948 Engine Continental C-85-8F Fuel 80 minimum octane aviation gasoline Engine limits For all operations, 2575 r.p.m. (85 hp) Airspeed Limits (CAS) Maneuvering 85 m.p.h. (normal) 90 m.p.h. (utility) Maximum structural cruising 90 m.p.h. (normal) 90 m.p.h. (utility) Never exceed 113 m.p.h. (normal) 121 m.p.h. (utility) Propeller Limits Static rpm at maximum permissible throttle setting: Not over 2465, not under 2300. No additional tolerance permitted. Diameter: not over 72 in., not under 70 in. C.G. Range (Normal Category) Forward limit (+14.6) at 1216 lbs. Straight line to (+16.2) at 1400 lbs. Rear limit (+21.8) at 1400 lbs. (Utility Category) Forward limit (+14.6) at 1216 lbs. Straight line to (+16.2) at 1400 lbs. Rear limit (+20.6) at 1400 lbs. 14 15 16 17 18 19 20 21 22 23 900 1000 1100 1200 1300 1400 1500 Front Limit Rear Limit Utility Cat. Rear Limit Normal Cat. LBS. INCHES Emtpy Wt. C.G. Range None Maximum Weight 1400 lb. (normal and utility) No. of Seats 2 adjustable (+21.5 to +25.5) Maximum Baggage 70 lbs. (+48.5) Fuel Capacity 23 gal. - Main 15 gal. (-6), Auxiliary 8 gal. (+60) Oil Capacity 4.5 qt. (-32) Control Surface Movements Elevator Up 24° Down 26° Elevator trim tab Up 14° Down 44.5° Ailerons Up 28.5° Down 18° Rudder Right 28° Left 28° Serial nos. eligible 11CC-1 and up Required equipment Items 1(a), 101, 102, 106, 206, 207, and 401(b) 3 A-796 SPECIFICATIONS PERTINENT TO ALL MODELS Datum Leading edge of wing Leveling Means Any portion of the cabin floor to level laterally and longitudinally. Certification Basis Type Certificate No. 796 (CAR 3, Normal and Utility Categories) Production Basis None. Prior to original certification, an FAA representative must perform a detailed inspection for workmanship, materials, and conformity with the approved technical data, and a check of the flight characteristics. Export Eligibility Eligible for export to all countries subject to the provisions of MCP 2-4. EQUIPMENT A plus (+) or minus (-) sign preceding the weight of an optional item indicates the net weight change between that item and the equivalent required item. Approval for the installation of all items of equipment listed herein has be en obtained by the aircraft manufacturer except those items preceded by an asterisk (*). The asterisk denotes that approval has been obtained by someone other than the aircraft manufacturer. An item marked with an asterisk may not have been manufactured under an FAA monitored or approved quality control system; and, therefore, conformity must be determined if the item is not identified by a Form ACA-186, PMA, or other evidence of FAA production approval. Propeller and Propeller Accessories 1. Propeller (a) Sensenich 72GK44, 72GK45, 72GK46, or any fixed pitch wood propeller eligible for 11 lb. (-44) the engine speed and power and which meets the diameter and static r.p.m. limits specified under "Propeller Limits." (b) McCauley 1A90 with following limits: 22 lb. (-44) 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. 2. Propeller spinner (Aeronca Dwg. 4-710 and 4-711) 1 lb. (-45) *3. Propeller - Sensenich M74CK-2, fixed pitch metal 21 lb. (-44) Static rpm at maximum permissible throttle setting - Not over 2465, not under 2300 No additional tolerance permitted. Diameter: Not over 72 in., not under 70 in. Applicable Airplane Flight Manual shall be revised by the Modifer and approved by the FAA Engineering and Manufacturing Division to reflect this installation change. Engine and Engine Accessories - Fuel and Oil Systems 101. Carburetor air heater (Aeronca Dwg. 7-557) 1 lb. (-32) 102. Carburetor air scoop (Aeronca Dwg. 4-601) 21 lbs. (38) 103. Carburetor air filter (Aeronca Dwg. 2-849) 1 lb. (-38) 104. Cabin heater (Aeronca Dwg. 3-503 and 7-557) 2 lb. (-25) 105. Starter - (MacDowell (Aeronca Dwg. 7-600) 9 lb. (-39) 106. Mufflers - Hanlon and Wilson (Aeronca Dwg. 7-557) 13 lbs. (-32) *107. Oil filter - Fram PB-5, Kit No. 510, Fram Installation Dwg. 61522 (Weight includes 1 qt. of oil) 4 lb. (-21) *108. Flight winter shutters, installed in accordance with Wright Installation Instructions No. 1, dated December 24, 1949, issued by Wright Flying Service, Williston, ND 2 lb. (-26) A-796 4 Landing Gear and Floats 201. Two main wheel - brake assemblies, 6.00-6, Type III (a) Goodyear Model L6MBD 20 lbs. (0) Wheel Assembly No. 511413-M Brake Assembly No. 511254-A (b) Cleveland Model 6.00DMB 17 lbs. (0) Wheel Assembly No. C-38500 Brake Assembly NO. C-7000 202. (a) Two main wheel 4-ply-rating tires, 6.00-6 17 lbs. (0) (b) Two main wheel 4-ply-rating tires, 7.00-6 203. Tail wheel assemblies (a) Scott Model 3000, 6x2.00, steerable with leaf spring 11 lb. (+181) (b) Scott Model 3-24B with leaf spring 11 lb. (+181) (c) Maule Model SFS-1-2 with leaf spring 10 lb. (+181) (d) Maule Model SS-1-2 with leaf spring 10 lb. (+181) (e) Decker steerable Model D-501 7 lb. (+181) 204. Wheel pants (Aeronca Dwg. 7-606) 6 lb. (-0) 205. Parking brake (Aeronca Dwg. 7-527) 1 lb. (-1) 206. Edo 92-1400 float installation 167 lbs. (+19) 207. Auxiliary ventral fin (Aeronca Dwg. 4-657) 4 lb. (+161) *208. Consolidair Model 17 wheel fenders (Consolidair Installation Dwg. No. 0036) 10 lb. (0) *209. Skis (a) Federal A-1500A (Federal Installation Dwg. 11R241) 39 lb. (0) (b) Federal A-1500 (Federal Installation Dwg. 11R241) 37 lb. (0) (c) Federal CA 1850-6 (Federal Installation Dwg. 11R241) 48 lb. (0) (d) Federal A-2000 (Federal Installation Dwg. 11R241) 41 lb. (0) (e) Federal A-2000A (Federal Installatin Dwg. 11R241) 49 lbs. (0) (f) Federal A-1850 (Federal Installation Dwg. 11R241) 38 lbs. (0) Interior Equipment 401. (a) (For 11CC Landplane) FAA Approved Airplane Flight Manual dated May 10, 1948 (b) (For S11CC Landplane) FAA Approved Airplane Flight Manual dated October 29, 1948 (c) FAA Approved Skiplane Supplement to Airplane Flight Manual dated January 25, 1949. In lieu of this item, the following skiplane performance information may be appended to the Performance Section of Item 401(a): TAKEOFF DISTANCE AND LANDING DISTANCE - Under the most favorable conditions of smooth packed snow at temperatures approximating 32°F, the skiplane takeoff distance is approximately 10% greater than that shown for the landplane and the skiplane landing distance is approximately 20% greater than that shown for the landplane. In estimating takeoff and landing distance for other conditions, caution should be exercised in that lower temperatures or other snow conditions will usually increase the takeoff distances and either decrease or increase the landing distances. NORMAL RATE OF CLIMB - Reduce rate of climb values of landplane by approximately 10%. STALLING SPEED (POWER OFF) - Stalling speeds for skiplane same as shown for landplane. NOTE 1. Current weight and balance report including list of equipment included in certificated weight empty, and loading instructions when necessary, must be in each aircraft at the time of original certification and at all times thereafter (except in the case of air carrier operators having an aproved weight control system). 5 A-796 NOTE 2. The following placards must be displayed in front of and in clear view of the pilot: (a) "This airplane must be operated as a normal or utility category airplane in compliance with the limitation in the FAA Approved Airplane Flight Manual. All markings and placards on this airplane apply to its operation as normal category airplane. For utility category operations, refer to Airplane Flight Manual. No aerobatics maneuvers (including spins) are approved for Normal Category operations." (b) "Auxiliary Fuel Tank - Drain in level flight when main tank is half full. Close valve when drained." ....END....