# TCDS TC 745: Bellanca Aircraft Corporation - Type: Type certificate data sheet - Status: Current - Holder: Bellanca Aircraft Corporation - Revision: 0 - Revised: October 30, 1941 - Product: Aircraft, Small Airplane - Certification basis: CAR 4a - Registered aircraft: 3, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/b5/dd/b5dd462decd56a60f6e647cc31fe96e8d993b92c2df0eea1b3acd93068c91ba1 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D43C205AF029C4868525672F00693BA5.0001 - Page: https://openairdocs.org/tcds/TC%20745 ## Models (1) As the data sheet lists them. - 14-12F-3 ## What the data sheet says This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers. ```text 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). ``` ## ADs (2, in force first) - [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 76-20-07](https://openairdocs.org/ad/76-20-07): Wood Decayed Wing Spars · Bellanca 14-12F-3, 14-13, 14-13-2 and 11 more. Effective Oct 8, 1976 ## Registered aircraft by registry model (OpenAirDocs) - [Bellanca 14-12F-3](https://openairdocs.org/model/bellanca-14-12f-3): 3 aircraft (registry code 1200902) ## STCs approved under this data sheet (6) - [STC SA4503NM](https://openairdocs.org/stc/SA4503NM): Remove original cloth covering and install Ceconite covering. Ceconite Division of Poly-Fiber Inc. - [STC SA02825NY PAGE 1](https://openairdocs.org/stc/SA02825NY%20PAGE%201): Installation of Aerospace Logic Aircraft Instruments. Aerospace Logic Inc. - [STC SA1315WE](https://openairdocs.org/stc/SA1315WE): Installation of Mixture Monitor (exhaust gas temperature probe, gage and selector) in accordance with Delta Products Part Lists A-192 and A-193, or in accordance with Tri-Star Corporation Mixture Monitor Installation Instructions dated December 9, 1981, or later FAA approved revision and/or Drawing List MM-127 dated November 15, 1981, or later FAA approved revision in aircraft models listed in Master Eligibility List P-80-A-6 revised March 29, 1968, copy attached, or later FAA approved revision.. Universal Corporation - [STC SA2683NM](https://openairdocs.org/stc/SA2683NM): Installation of Precise Flight, Inc. stand-by vacuum system (SVS). Precise Flight Inc - [STC SA8075SW](https://openairdocs.org/stc/SA8075SW): Installation of fiberglass covering. (M-62 SERIES PT-19) (G-73 SCHWEIZER). Razorback Fabrics Inc - [STC ST01700NY](https://openairdocs.org/stc/ST01700NY): Installation of the following Aerospace Logic aircraft instruments: EGT-100 Exhaust Gas Temperature Indicator, CHT-100 Cylnder Head Temperature INdicator, FL-100 Dual Fuel Level Indicator, FP-100 Fuel Pressure and Ammeter Indicator, OL-100 Oil Pressure and Temperature Indicator, and VA-100 Voltmeter and Ammeter Indicator.. Aerospace Logic Inc. --- 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.