# TCDS TC 713: Textron Aviation Inc. - Type: Type certificate data sheet - Status: Current - Holder: Textron Aviation Inc. - Revision: 3 - Revised: October 12, 2016 - Product: Aircraft, Small Airplane - Certification basis: CAR 4a - Registered aircraft: 1, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/28/bb/28bbfe81ac2655688a15f0bdff7bbe6214da279291ab71cebd25e745497ba675 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/819378B920640A3286258113006616D2.0001 - Page: https://openairdocs.org/tcds/TC%20713 ## Models (1) As the data sheet lists them. - D17A (Army UC-43F) ## What the data sheet says Some pages are OCR from the scanned FAA data sheet. OCR can misread letters and numbers. ```text Page No. 1 2 3 4 Rev. No. 3 1 1 1 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 713 Revision 3 Textron Aviation D17A October 12, 2016 TYPE CERTIFICATION DATA SHEET NO. 713 Type Certificate Holder Textron Aviation Inc. One Cessna Boulevard Wichita, Kansas 67215 Type Certificate Holder Record: Beech Aircraft Corporation transferred to Raytheon Aircraft Company on April 15, 1996 Raytheon Aircraft Company transferred to Hawker Beechcraft Corporation on March 26, 2007 Hawker Beechcraft Corporation transferred to Beechcraft Corporation on April 12, 2013 Beechcraft Corporation transferred to Textron Aviation Inc. on October 12, 2016 713 2 Rev. 3 MODELS: Beechcraft D17A (Army UC-43F), 5 PCLB T.C. NUMBER: 713 (Approved 11/7/39) (Same as Model D17R, T.C. 638, except engine installation) Engine Wright R-760E-2 Fuel 80 min. octane aviation gasoline Engine limits Maximum, except take-off, 2200 rpm (320 hp) (one minute), 2400 rpm (350 hp) Airspeed limits Level flight or climb 186 mph; glide (T.I.A.S.) or dive 223 mph; flaps extended Propellers limits Maximum permissible diameter 106 in. (For clearance) C.G. range (+16.4) (6.7 percent MAC) to (+25.5) (22.6 percent MAC) Datum Leading edge of lower wing MAC 57.2 inches (LE. of MAC at (+12.6) Leveling means Airplane is level when stagger (horizontal distance between wing trailing edges near fuselage) Maximum weight No. seats Maximum baggage Fuel capacity 98 gallons (one fuselage tank, 29 gallons (+32), the upper right wing ta, an ga0nh : (See Item 205) Oil capacity 6.5 gallons (-14) Control surface 26 degrees down movements Elevator tabs 14.5 degrees up 14.5 degrees down 33 degrees up 25 degrees down 28 degrees right 28 degrees left 20 degrees right 20 degrees left 45 degrees down Serial Nos. eligible D17A-305 and up and all AAP Nos. Required equipment e5, 010, 1011, 112, 113, 858 106 105, 106, 107, 108, Specifications Pertinent to All Models: Type Certificate No. 713 (CAR 4a) Export eligibility Eligible for export as follows, subject to provisions of MOP 2-4: - Landplane - eligible - Skiplane - not eligible However, structure complies with Canadian requirements for ski gear when item 310 is installed. Maximum pedestal height 17 in. Tread is same as landplane. (b) All other countries except New Zealand 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. Propellers and Propeller Accessories Propeller - Hamilton Standard hub 2B20, blades 6135A-12 or 6135A-13. 8' 1/8" maximum, 7" 9-7/8" minimum. Low pitch setting 11.7 degrees. 108 1bs. (-66) Constant speed governor (Hamilton Standard type 1A1-A5) 5 1bs. (-61) Engine and Engine Accessories - Fuel and Oil Systems Engine ring cowling (NACA type) 39 1bs. (-48) Carburetor air heater (muff type) 4 1bs. (-41) 103. Starter (Eclipse E80) 20 1bs. (-33) Rev. 3 3 713 109. Oil radiator (Draving D1758950) 8 1bs. -39 Wobble pump (Type D-2) 4 1bs. (+12 11. Engine driven fuel pump (Pesco 40 Series or Romec RD-3080 5 1bs. - 3- 204. Oil tanks 8 or 9.5 gallons 5 lbs. ‹- 14 205- Auxiliary fuel tanks (a) One 23 gallon tank, upper left wing 20 1bs. (*S2) (b) One 49 gallon tank, fuselage 25 lbs. (May replace lower ving tanks.) 207. Ignition shielding (Breeze) 15 1bs- (-47) 219- Special oil drain 1 1b. (-27) 220- Fuel analyzer (Breeze or Cambridge) 5 1bs. (-83 Landing Gear and Floats 106- 7.50-10 wheels (Goodyear 10 HBM or Hayes 750 Series) with 7.50-10 6-ply tires (wheels must be placarded for these tires) 75 1bs. (+5) 107- 10x3 tail wheel 5 lbs. (+205) 305- Dual brakes (copilot) +2 1bs. (-8) 306- Hand operated parking brake 2 1bs. (-4) 307. Emergency wood landing skids (Drawing E170140) 16 1bs. (+22) 308- Puncture proof tubes +8 1bs. (+5; 310- Skiplane landing gear (Drawing D17820 and D17840) +3 1bs. (+20) 312. 10 in. smooth contour tail wheel assembly with 6-ply tire No weight change Electrical Equipment 104. Generator - 15 amp 15 1bs. (-33) 105. Battery (Exide 6TS-13-1) 36 lbs. (+-21) 112- Landing gear motor (Dumore D5, fuse required) 9 1bs. (+7) 113. Flap motor (Dumore X special 4253, 30 amp fuse required) 5 1bs. (+45) 201. Generator (a) 25 amp (Eclipse D) 20 1bs. (-33 (b) 50 amp (Eclipse E) 25 lbs. (-33 217. Landing lights (a) One or two (Hall A-6) 3.5 1bs. each (+35) (b) One or two (Grimes ST-250) 5 1bs each (+21) (c) One or two (Grimes ST-1220) (+21) 311. Cannon plug (tor electric starter) 3 1bs. (-2) OI (-8) Interior Equipment 108- Swing-over control column (See Item 301) 11 1bs. ‚+0 202- Cabin heater (Muff type) 3 1bs. 1-41 203. Fire extinguisher (a) (Lux -2 1bs.) 12 1bs. (-3) (b) (Lux -5 lbs.) 17 1bs. (-13) (Pyrene No. 5C) 12 lbs. (-10) 10 1bs. (-10) (lux -5 1bs.) (Drawing I-170555) 21 1bs. (+50) 206. Parachute flares Three or four 1-1/2 minute (International MX-1) 6 1bs. each (+80) or (+108) (b) One or two 3 minute (Wiley A-8) 18 1bs. each (+105) 208. Golf bag compartment (Drawing I-17006) (Maximum capacity 70 1bs., included in baggage allowance) 9 1bs. (+100) 209- Parachutes or parachute type chairs 211. Vacuum equipment (a) 5 1bs. (-34) (b) Venturi tubes 1 1b. (+17) 222. Package drop (under baggage compartment) +8 1bs. (+84) 301. Control column - "T" type (See Item 108) No weight change 309. Folding back seat (may replace standard front seats) 16 lbs. (+21) 313- Utility case 4 1bs. (+771 Miscellaneous (Not listed above) Extra cabin door on right side +5 lbs. (+42) Fuselage alterations for special- Photographic version (Item 214) Includes front and rear floor camera and viewfinder wells, and change in location of cables (Drawings D17015 and 713 4 Rev. 3 D170160) +13 1bs. (+33) Ambulance version (Item 215) Includes rear seat center support and litter floor attachments (Drawings I-17073 and I-17077) +2 lbs. (+53) Mailplane version (Item 216) Includes rear seat center support and metal lined baggage compartment and right rear of cabin (Drawings I-170812 and I-170813) + 15 1bs. (+73) Photographic version (See Item 213(a)) Camera and viewfinder 110 1bs. max. (+51) Photographer's stool 4 1bs. (+65) (These items (a and b) may be installed after fuselage alterations (Item 213(a)) have been made, and standard rear seat, 31 1bs. (+67), camera and viewfinder cover plates, 3 1bs. (+51), have been removed Oxygen tank installation 150 1bs. max. (+73) Ambulance version Special right or left half rear seat (Drawing I-17073) (May replace standard rear seat (+6/), if fuselage alterations 213(b)) have been made.) 17 1bs. each (+67) First aid box installation 7 1bs. (+48) Ambulance litter (May be installed after fuselage alteration and removal of right half rear seat (a) and copilot's seat, 16 1bs. (+21) 14 lbs. (+42) Mailplane version (See Item 213(c)) Same as Item 215(a) except Drawing I-170812 Removable front and inner sides of forward mail compartment (see c) 10 1bs. (+52) Mail compartments and capacities: 200 1bs. max. (+54) 150 1bs. max. (+ 88) Ballast at tail post (Drawing I-17007) 25 1bs. max. (+224) 302. Metal cover for wing fuel tanks 3 1bs. each (+24) or (+47) 304. Quick door release 1 1b. (+25) Prior to original certification, each aircraft manufactured prior to august /, 1945, must satisfactorily pass: An inspection for workmanship, materials and conformity before covering, metal priming or final firish is applied. (b) A final inspection of the completed aircraft A check of the flight characteristics Current weight and balance report including list of equipment included in certificated weight empty, and loading instructions when ecessary, must be in each aircraft at the time of original certificatior nd at all times thereafter (except in the case of air carrier operator having an approved weight control system). Fuel restriction placard must state: "Use fuselage tank (s) for take-off and landing. Fill fuselage tank (s) before filling wing Use wing tanks before using fuselage tank (s).' When upper wing fuel tang are store ding er wing tanks. tanks before tanks are installed, filling upper --- END --- ``` ## ADs (3, in force first) - [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023 - [AD 99-05-13 R1 WD](https://openairdocs.org/ad/99-05-13-R1-WD): Withdrawal of AD 99-05-13 · Beech B17B, B17L, B17R (Army UC-43H) and 107 more. Effective Jul 5, 2000 - [AD 99-05-13](https://openairdocs.org/ad/99-05-13) (historical): Fuel Tank Selector · Beech B17B, B17L, B17R (Army UC-43H) and 107 more. Effective Apr 19, 1999 ## Registered aircraft by registry model (OpenAirDocs) - [Beech D17A](https://openairdocs.org/model/beech-d17a): 1 aircraft (registry code 1150530) ## STCs approved under this data sheet (13) - [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.. TCW Technologies, LLC - [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC - [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 SA02930NY](https://openairdocs.org/stc/SA02930NY): Installation of Insight Instrument Corporation Graphic Engine Monitor (GEM 610C) models G3, G2, and G1 and 1200C model G4 as primary Cylinder Head Temperature (CHT), Exhaust Gas Temperature (EGT), and Turbine Inlet Temperature (TIT) Instruments. Insight Instrument Corporation - [STC SA02283SE PAGE 2](https://openairdocs.org/stc/SA02283SE%20PAGE%202): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P. Electronics International Inc. - [STC SA02402SE PAGE 1](https://openairdocs.org/stc/SA02402SE%20PAGE%201): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) CGR-30C. Electronics International Inc. - [STC SA02825NY PAGE 1](https://openairdocs.org/stc/SA02825NY%20PAGE%201): Installation of Aerospace Logic Aircraft Instruments. Aerospace Logic Inc. - [STC SA8075SW](https://openairdocs.org/stc/SA8075SW): Installation of fiberglass covering. (M-62 SERIES PT-19) (G-73 SCHWEIZER). Razorback Fabrics Inc - [STC SA00068LA](https://openairdocs.org/stc/SA00068LA): Installation of tail wheel adapter ring.. R-R-R-Russ Aircraft - [STC SA1455NM](https://openairdocs.org/stc/SA1455NM): Installation of a flame proof auxiliary heater-dryer, Model12-1600.. Thermal, Inc - [STC SA1461NM](https://openairdocs.org/stc/SA1461NM): Installation of fuselage structure assembly. Anything Antiques - [STC SA555NW](https://openairdocs.org/stc/SA555NW): Installation of front and rear landing gear truss assemblies.. Anything Antiques --- 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.