TCDS TC 745

Type certificate data sheet · Bellanca Aircraft Corporation · Aircraft · Small Airplane

Holder
Bellanca Aircraft Corporation
Revision
0
Revised
October 30, 1941
Status
Current
Product
Aircraft · Small Airplane
Certification basis
CAR 4a
Models
1
Registered
3 aircraft

The release keeps the latest revision of each data sheet. Model names are as the data sheet lists them.

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Models · 1

ModelAlso known asNote
14-12F-3Formerly Aeronca, American Champion

Airworthiness directives · 2

ADs whose products are models on this data sheet, matched by model and maker.

Registered aircraft

Registry models that point at this data sheet, with their registered aircraft.

STCs approved under this data sheet · 6

What the data sheet saysOCR

This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers.

MODELS: Bellanca 14-12F-3, 3 PCLM I. C. NOMBER: 745 (Approved 10/30/41) Engine Franklin 6AC-264-F3 Fuel 80 minimum octane aviation gasoline Engine limits For all operations, 2600 rpm (120 hp) Airspeed limits Level flight or climb - 143 mph True Ind. Glide or dive - 171 mph True Ind. Flaps extended - 86 mph True Ind. Propeller limits Static rpm at maximum permissible throttle setting - not more than 2210, not less than 1915 No additional tolerance permitted Diameter - not more than 74 in., not less than C.G. range Datum Leading edge of wing at Rib No. 1 (Rib No. 1 is 24 inches outboard from fuselage centerline) Leveling means Lugs on right side of cabin at seat level Maximum weight NO. seats 3 (two at +20 and one at +53.5) Maximum baggage 60 Ibs. (+29) (See Items 209 and 301) Fuel capacity 20 gallons (*29) (See Item 201) oil capacity 2 gallons (-36) Control surface Elevators - up 15 degrees (with landing gear movements retracted). up 23 degrees (with landing gear extended) down 22 degrees Elevator tab - up 0 degrees, down 22 degrees Rudder - 18 degrees right and left from centerline Ailerons - up 22 degrees, down 22 degrees Flaps - 48 degrees down Serial Nos. eligible 1042 and up Required equipment Items 101, 102, 103, 104, 105, 106, 107 and 108 Specifications Pertinent to All Models: Certification basis Type Certificate No. 745 (Car 4a) Production basis Production Certificate No. Export eligibility Eligible for export as follows subject to provisions of - Landplane - eligible - Seaplane - not eligible (b) All other countries except Australia and New Zealand Equipment: A plus (+) or minus (-) sign preceding the weight of an optional item indicates the net weight change when that item is installed. Propellers and Propeller Accessories 101. Propeller - wood (fixed or adjustable pitch) 11 1bs. (-48) 107. Propeller spinner 1 1b. (-48) Engines and Engine Accessories - Fuel and Oil System Starter (Autolite type MBG 15 1bs. (-26) 201- (Harrison Model HE-212) 3 1bs. (-47) Fuel tank (20 gallons) right wing 8 lbs. (+29) Landing Gear and Floats 102. Wheels and brakes (Firestone or Shinn 6C2YFB) and 6.00-6 4-ply tires 30 1bs. (+9) 103. 6x2.00 sponge rubber tail wheel (Drawing 7791) 2 1bs. (+192) Flectrical Equipment Battery (Reading R-24L) and box 26 1bs. (+39) 106- Generator (Autolite type GBY 12V) 12 1bs. (-24) 202. Landing lights (Grimes 3T-250) 4 1bs. (*18) 207. Radio shielding 4 Ibs. (-31) 208- Position lights (Grimes) 3 1bs. (+46) Interior Equipment 209. 35 lb. capacity baggage compartment (on rear floor - Drawing 7905) Neglect weight change 301- 63 1b. capacity baggage compartment replacing rear seat + 1 1b. (+57) NOTE 1. Current weight and balance report including list of equipment included in certificated weight empty, and loading instructions wher necessary, must be in each aircraft at the time of original certificatior and at all times thereafter (except in the case of air carrier operators having an approved weight control system).