DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A21CE

Transcription

1 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A2CE A2CE Revision American Champion (Bellanca) (Champion) August 25, 997 This data sheet, which is part of Type Certificate No. A2CE, prescribes conditions and limitations under which the product for the which type certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations. Type Certificate Holder: American Champion Aircraft Corp. P. O. Box 37 Rochester, WI 5367 I - Model, 2 PCLM (Normal and Acrobatic Category), Approved October 6, 970 Lycoming IO-320-EA or IO-320-EB or AEIO-320-EB or AEIO-320-E2B (IO-320-EA and IO-320-EB must be modified per STC SE7CE) (See NOTE 5 for optional engine and applicable limitations) 80/87 minimum grade aviation gasoline For all operations, 2700 r.p.m. (50 hp.) (See NOTE 7 for additional limitations) Propeller Limits. (a) Hartzell HC-C2YL-4/C or HC-C2YL-4F/FC or HC-C2YL-4BF/FC (Eligible with all engines except AEIO-320-E2B) Diameter: not over 72 in., not under 70 in. Pitch setting at 30 in. sta.: low o, high 20 o (b) Hartzell spinner ass'y (c) Hartzell propeller governor F6-3A or F6-3 or Woodward D Sensenich 74DM6S8-0 (Eligible with AEIO-320-E2B only) not over 2450, not under 2200 no additional tolerance permitted Diameter: not over 74 in., not under 73 in. Airspeed Limits (CAS) Never exceed 80 mph (56 knots) 60 mph (39 knots) Normal Category 2 mph (05 knots) Acrobatic Category 30 mph (3 knots) C. G. Range Normal Category (+3.5) to (+2.0) at 800 lbs. (+.5) to (+2.0) at 550 lbs. or less Acrobatic Category (+3.5) to (+8.5) at 800 lbs. (+.5) to (+8.5) at 550 lbs. or less Empty wt. C. G. Range None Maximum Weight 800 lbs. Normal Category 800 lbs. Acrobatic Category No. of Seats 2 ( at +4, at +44) 2 ( at +4, at +45) when Front Adjustable Seat is installed. Maximum Baggage 00 lbs. (+7) (Normal Category Only) Capacity Wing tanks: 40.0 gal. (+26) Inverted header tank:.5 gal. (-3) See NOTE for unusable fuel Page No Rev. No.

2 A2CE Rev. -2- Oil Capacity 0 qt. (-34) See NOTE for undrainable oil Control Surface Movements Elevator Up 30 o Down 30 o Elevator Trim Tab Up 9.5 o Down 44 o Ailerons Up 20 o Down 20 o Rudder Right 30 o Left 30 o Serial Nos. Eligible 3-70, 4-7, 6-7, 5-72, 7-72 thru 53-72, thru 9-73, thru 6-74, thru 28-75, , 22-75, 29-76, thru , thru , thru , thru , thru , , and up. II - Model, 2 PCLM-SM (Normal Category), Approved April 30, PCLM, (Restricted Category), Approved May 4, 975 Propeller Limits Lycoming O-360-C2A, C2E, CA, CE, or CG 9/96 minimum grade aviation gasoline 00/30 may be used 00% of the time. For all other operations, 2700 r.p.m. (80 hp.) (See NOTE 6 for additional limitations). Propeller (Landplane Only) McCauley A200HFA80 (Fixed Pitch) Not over 2350, not under 200 (for Restricted Category aircraft utilized for chemical dispensing operations - not over 2360, not under 2260) No additional tolerance permitted Diameter: Not over 80 in., not under 79 in. Caution: Avoid operation between 700 and 200 rpm during descending flight. 2. Propeller (Landplane Only) (a) Hartzell HC-C2YR-BF/F7666A (Constant Speed) or Hartzell HC-C2YK-BF/F7666A (Constant Speed) Diameter: Not over 76 in., not under 72 in. Pitch setting at 30 in. sta.: low 2 o, high 29 o (b) Hartzell spinner ass'y (c) Woodward Propeller Governor B20776 (replacement for B2068) Woodward Propeller Governor T2076 (for O-360-CG only) Placard Required: "AVOID CONTINUOUS OPER." 3. Propeller (Landplane Only) (a) Hartzell HC-C3YR-RF/F7282 (Constant Speed) Diameter: Not over 72 in., not under 70 in. Pitch setting at 30 in. sta.: low 9.2 ± 0. o, high 30.5 ± 0.5 o (b) Hartzell spinner ass'y 82A2295-P (c) Woodward Propeller Governor B20776 (replacement for B2068) Woodward Propeller Governor T2076 (for O-360-CG only) Placard Required: "AVOID CONTINUOUS OPER. BELOW 5 IN M.P." 4. Propeller (Seaplane Only, equipped with EDO floats) McCauley A200HFA80 (Fixed Pitch) Not over 2400, not under 2260 No additional tolerance permitted Diameter: Not over 80 in., not under 79 in. Placard Required: "AVOID OPERATION BETWEEN 700 and 200 RPM DURING DESCENDING FLIGHT." Airspeed Limits (CAS) Landplane: Normal Category Never exceed 62 mph (4 knots) 30 mph (3 knots) 5 mph (00 knots) 00 mph ( 87 knots)

3 A2CE -3- Rev. Restricted Category Maximum Operating Speed Airspeed Limits (CAS) Seaplane (with EDO floats): (Continued) Normal Category Never exceed 20 mph (04 knots) 2 mph ( 97 knots) 00 mph ( 87 knots) 48 mph (29 knots) 20 mph (04 knots) 5 mph (00 knots) 00 mph ( 87 knots) C. G. Range Landplane: Normal Category and Restricted Category (Ferry operation only - see approved AFMS) (+4.2) to (+9.2) at 250 lbs. (+0.5) to (+9.2) at 450 lbs. or less Empty wt. C. G. Range None Restricted Category (utilized for dispensing operations) (+7.0) to (+9.2) at 2600 lbs. (+0.5) to (+9.2) at 650 lbs. or less Seaplane (with EDO floats): Normal Category (+4.2) to (+8.2) at 250 lbs. (+0.5) to (+8.2) at 675 lbs. or less Maximum Weight Normal Category Landplane and Seaplane, (and Restricted Category Ferry configuration): 250 lbs. Restricted Category (utilized for chemical dispensing operations): 2600 lbs. No. of Seats 2 ( at +2, at +42) 2 ( at +2, at +43) when Front Adjustable Seat is installed. Maximum Baggage Capacity 00 lbs. (+69) (Note: No baggage permissible on Restricted Category aircraft during chemical dispensing operations). Landplane: 36 gal. or 72 gal. (two 8 gal. or 36 gal. tanks in wings at ) See NOTE for data on unusable fuel. Seaplane: 36 gal. (two 8 gal. tanks in wings at ) See NOTE for data on unusable fuel. Oil Capacity 8 qt. (with fixed pitch propeller), or 0 qt. (with constant speed propeller), at (-36). See NOTE for undrainable oil Control Surface Movements Elevator Up 29 o Down 26 o Elevator Trim Tab Up 9.5 o Down 45 o Ailerons Up 27.5 o Down 9 o Rudder Right 25 o Left 25 o Flaps Up 0 o Down 28 o Serial Nos. Eligible Normal Category: -74 thru 9-74, thru 87-75, thru , thru , thru , thru , thru , , , , , 36-9 and up. Restricted Category: 29-75, and up.

4 A2CE Rev. -4- Data Pertinent to All Models Datum Leveling Means Certification Basis Wing leading edge Drop plumb line from wing leading edge such that plumb line is 2.8 in. (Model ), 0.8 in. (Model ) forward of front face of fuselage-strut attach fitting. Part 23 of the Federal Aviation Regulations dated February, 965, as amended by 23- and 23-6 (Normal and Acrobatic Category); and FAR 36, amended thru 36-9, for Models and (S/N and up). Part 2.25 of the Federal Aviation Regulations dated February, 965 (Restricted Category), for Model aircraft (S/N 29-75, and up). S/N 29-75, and up are eligible for Multiple Airworthiness Certification in the Restricted Category when agricultural spray equipment is installed per Bellanca Drawing Application for Type Certificate dated November 6, 967. Type Certificate No. A2CE issued October 6, 970. Production Basis American Champion Aircraft Production Limitation Record 333CE, dated July 2, 997. Production authorized Oct. 5, 992 () and June 7, 993 (). Equipment The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) must be installed in the aircraft for certification. In addition, the following items are required:. FAA Approved Airplane Flight Manual for Model and Model. 2. Accelerometer (Acrobatic Category Only) per Champion Drawing (Model ). 3. Stall warning indicator Champion Drawing NOTE. NOTE 2. Current weight and balance report, together with list of equipment included in certificated empty weight must be provided for each aircraft at time of original certification. The certificated empty weight and corresponding center of gravity location must include for Model, unusable fuel of 4.5 lb. at (-3) in. and 3.5 lb. at (+26) in. and undrainable oil of 5 lb. at (-34) in., and for Model unusable fuel of 8.4 lb. at (+5.00) in. for 36 gal. system or 3 lb. at (+5.00) in. for 72 gal. system and undrainable oil 4 lb. at (-36) Constant Speed Propeller Only. All placards specified in the FAA Approved Airplane Flight Manual must be displayed in the airplane. Flight Manual Applicability Model Manual Issue Date Revision No. Revision Date Serial No. Applicability 50 h.p. (C.S & F.P.) April 5, 97 April 4, h.p. May 9, 977 April 7, A B A B April 30, (Seaplane) (Agricultural) September 24, 974 May 2, 975, thru thru except , thru thru thru thru thru except thru thru thru thru thru thru thru thru , thru , thru All subsequent airplanes contain an Airplane Flight Manual bearing a serial number effectivity. NOTE 3. Mandatory inspection times for strut attach fittings 3-69 () and () on metal spar winged aircraft must be inspected in accordance with American Champion Aircraft Airworthiness Limitations, dated May 9, 996 or later FAA approved revision.

5 A2CE -5- Rev. NOTE 4. NOTE 5. The -5.0g limit load factor (Acrobatic Category) is required due to expected flight loads while accomplishing certain approved maneuvers. (Model ) Optional engine and applicable limitations (Model ) Lycoming AEIO-360-HA or AEIO-360-HB 9/96 minimum grade aviation gasoline 00/30 may be used 00% of the time. Propeller Limits For all other operations, 2700 r.p.m. (80 hp.) Hartzell HC-C2YR-4CF/FC7666A-2 Diameter: not over 74 in., not under 72 in. Pitch setting at 30 in. sta.: low.0 ± 0.2 o, high 2.5 ± 0.5 o Hartzell spinner ass'y Woodward propeller governor D20688 (AEIO-360-HA Only) Woodward propeller governor B20988 (AEIO-360-HB Only) Placard required: "AVOID CONT. RPM ACRO ONLY." Airspeed Limits (CAS) Never exceed 200 mph (74 knots) 60 mph (39 knots) Normal Category 2 mph (05 knots) Acrobatic Category 30 mph (3 knots) C. G. Range (+3.5) to (+8.5) at 800 lbs. (Normal or Acrobatic) (+.5) to (+8.5) at 550 lbs. or less NOTE 6. In order to comply with the requirements of Part 36 of the Federal Aviation Regulations, revised have been established for the Model (S/N and up). The revised limits are: Maximum normal operating power, 2550 r.p.m. (50 hp.) For all other operations, 2700 r.p.m. (80 hp.) These limits do not apply to aircraft utilized for dispensing agricultural chemicals and fire fighting materials. NOTE 7. In order to comply with European noise requirements (including Switzerland), revised Limits have been established for the model (80 h.p.) European Exports. The revised limits are: Maximum normal operating power, 2400 r.p.m. For all other operations, 2700 r.p.m. -- END --