# TCDS TC 716: Bellanca Aircraft Corporation - Type: Type certificate data sheet - Status: Current - Holder: Bellanca Aircraft Corporation - Revision: 0 - Revised: August 24, 1939 - Product: Aircraft, Small Airplane - Certification basis: CAR 4a - Registered aircraft: 11, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/ab/ac/abaca188adf31658e00bcd5ed93c19822bab9d789fa714df2c98a68bb96e430f - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A1D1CD5395E9CD268525672F00692906.0001 - Page: https://openairdocs.org/tcds/TC%20716 ## Models (2) As the data sheet lists them. - 14-9L - 14-9 ## What the data sheet says This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers. ```text MODELS: Bellanca 14-9, 14-91 T.C. NUMBER: 716 I - Model 14-9, 3 PCIM (Approved 8/24/39) Engine Rearwin LeBlond 90 5 F or Ken Royce 90 5G Fuel 65 minimum octane aviation gasoline Engine limits For all operations, 2250 rpm (90 hp) Airspeed limits Level flight or climb - 135 mph True Ind. Glide or dive - 170 mph True Ind. Flaps extended - 86 mph True Ind. (See NOTE 4) Propeller limits Static rpm at maximum permissible throttle setting - not more than 2130, not less than 2030 No additional tolerance permitted Diameter - not more than 74 in., not less than C.G. range (+18_0) (See NOTES 2+21.2) Maximum weight NO - seats 3 (two at +18 and one at +54) Maximum baggage 60 1bs- (+29) (See Items 206 and 305) Fuel capacity 22 gallons (+29) (See Item 303) Oil capacity 2 gallons (-21) Control surface Elevators - up 15 degrees (with landing gear movements retracted) - up 23 degrees (with landing gear extended) down 22 degrees Blevator tab - up 0 degrees, down 22 degrees Rudder - 18 degrees right and left from centerline Ailerons - up 22 degrees, down 22 degrees Plaps - 48 degrees down Serial Nos. eligible 1003 and up Required equipment Items 101, 102, 103, 104, 105, and 106 II - Model 14-9L, 3 PCLM (Approved 12/13/40) Engine Lenape Brave IM-5 Fuel 73 minimum octane aviation gasoline Engine limits For all operations, 2200 rpm (95 hp) Airspeed limits Level flight or climb - 135 mph True Ind. Glide or dive - 170 mph True Ind. Flaps extended - 86 mph True Ind. (See NOTE 4) Propeller limits Static rpm with maximum permissible throttle setting - not more than 2090, not less than 1990 No additional tolerance permitted Diameter - not more than 74 in., not less than 72 in. €. G. range (+18.0) to (+24.2) (See NOTES 2 and 3) Maximum weight 1750 1bs. NO. seats 2 (two at +18 and one at 54) Maximum baggage 60 1bs. maximum (+29) (See Items 206 and 305) Fuel capacity 22 gallons (+29) (See also Item 303) Oil capacity 2 gallons (-21) 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 1011 and up Required equipment Items 101, 102, 103, 104, 105 and 106 Specifications Pertinent to All Models: Datum Leading edge of wing at rib No. 1 (rib No. 1 is from fuselage centerline) Leveling means Lugs on right side of cockpit below door Certification basis Type Certificate No. 716 (CAR 4(a)) Production basis Production Certificate No. Export eligibility Eligible for export as follows subject to provisions - Landplane - eligible - Skiplane - not (b) All other countries except Australia and Eguipment: A plus *) or minus (-) sign preceding the weight of an optional indicates the net weight change when that item is installed. Propellers and Propeller Accessories Propeller - wood (fixed or adjustable pitch) (less hub) 14 1bs. (-44) Engines and Engine Accessories - Fuel and Oil System Engine ring cowl (-30) Carburetor air heater (-32) 20 gallon (replacing standard) No weight change 20 gallon auxiliary (replacing standard baggage compartment) (+28) Loading Gear and Floats 8.00-4 wheels with brakes Goodrich or 841) and 4-ply tires (wheels must be placarded for these tires) (+11) solid rubber tail wheel (Drawing or 6x2.00 sponge rubber Drawing (+198) Electrical Equipment 106. 2 dry cell batteries (Burgess 4P2H) cequired for warning devices 6 1bs. (-11) 202. Battery (a) (Exide 3-AC-7-1) 8 1bs. (-16) (b) (Exide 6-TS-7-1) 28 1bs. (+35) (c) (Willard SYR-7-6) 15 1bs. (-16) 203. Generator (Champion 128-#) 204. Landing light (Grimes ST-250) (Drawing 7825) 10 1bs. 4 1bs- (+14) (+18) Interior Equipment 205. Flares (5 one minute, International) (Drawing 7817) 17 1bs. (+86) 206. 35 1b. capacity baggage compartment (on rear floor - Drawing Neglect weight change 301- Parachutes (one, two or three) 20 1bs. each 302- Cabin heater (Drawing 7790-A) 3 1bs. (-22) 305. 63 1bs- (replacing rear seat) +1 1b. (+57) he 1 that here oct in the case of si cat ice operations Current weight and balance report including list of equipment having an approved weight control system). Elevator tab travel must be adjusted to 0 degrees up and 22 degrees 1006, 1007 and 1008 must have forward C.G. limited until tab range is so increased in accordance with Drawings 7630-D and 7749-C. NOTE 3. This range applies to airplanes equipped vith flaps. For airplanes which do not have flaps (Serial Nos. below 1038) the following C.G. range applies: (+16-1) to (+2402). NOTE 4. Serial numbers 1003 through 1037 eligible for flaps if reworked in accordance with Bellanca Drawings 7815, 7822, 7919, and 7577 Change L. ``` ## 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 14-9](https://openairdocs.org/model/bellanca-14-9): 10 aircraft (registry code 1200802) - [Bellanca 14-9L](https://openairdocs.org/model/bellanca-14-9l): 1 aircraft (registry code 1200804) ## STCs approved under this data sheet (8) - [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC - [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 SA1-551](https://openairdocs.org/stc/SA1-551): Replacement of fuselage and fin fabric covering with metal skin in.. Skycraft Corporation Inc. - [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 SA3989WE](https://openairdocs.org/stc/SA3989WE): Installation of Lycoming O-360-A1D engine, Hartzell HC-C2YK-1BF/F7666A propeller, and associated installation components. Basil Mikhalkin --- 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.