# TCDS A-774: Consolidated Vultee Aircraft Corporation Stinson Division - Type: Type certificate data sheet - Status: Current - Holder: Consolidated Vultee Aircraft Corporation Stinson Division - Revision: 2 - Revised: September 24, 2001 - Product: Aircraft, Small Airplane - Certification basis: CAR 4a - Registered aircraft: 85, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/41/00/4100ca94b82647110f1505bceaf0301471c67a9513c9f01871969001017df361 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/0EE231EB3B8B355586256AD800570462.0001 - Page: https://openairdocs.org/tcds/A-774 ## Models (1) As the data sheet lists them. - V-77 (Army AT-19) ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text P a g e N o .1234 Rev No. 2 2 2 - DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A-774 Revision 2 STINSON V-77 (Army AT-19) September 24, 2001 AIRCRAFT SPECIFICATION NO. A-774 Type Certificate Holder Consolidated Vultee Aircraft Corporation Stinson Division Wayne, Michigan I - Models V-77 (Army AT-19), 3 PCLM, Approved November 26, 1946 Engine Lycoming R-680E3B (R-680-13) Fuel 87 minimum octane aviation gasoline Engine Limits Maximum continuous, at any altitude, 28.0 in. Hg., 2200 rpm (285 hp Full throttle) Take-off (one minute), 28.0 in. Hg., 2300 rpm (300 hp Full throttle) Airspeed Limits Level flight or climb 155 mph True Ind. Glide or dive 198 mph True Ind. Flaps extended 108 mph True Ind. C.G. Range (90.6) to (92.1) at 4000 lbs. (84.4) to (92.1) at 3178 lbs. or less. Straight line variation between points given Datum 70 in. fwd. of most fwd. point of wing leading edge or 42 3/8 inches fwd. of the firewall. Leveling means Lugs on left side of cabin interior just below door. Maximum Weight 4000 lbs. No. Seats 3 (two at 84 and one at 120). See Note 3 for 4 or 5 pl ace installations. Maximum Baggage None. Fuel Capacity 76 gals. (Two 38 gal. wing tanks at 103.5) Oil Capacity 4.25 gals. (37) Control Surface Movements Wing flaps 35 o down Elevator 34 o up 19 o down Elevator trim tab 15 o up 22 o down Aileron 20 o up 16 o down Rudder 16 o right 16 o left Stabilizer Fixed Serial Nos. Eligible All AF numbers. Use manufacturer’s number when available. Required Equipment Items 1 or 2, 3, 101, 102, 103, 104, 105, 201, 202, 301, 302, 304, 401. A-774 Page 2 of 4 SPECIFICATION PERTINENT TO ALL MODELS Certification Basis Type Certificate No. 774 (CAR 4a) Export eligibility Eligible for export to all countries except as follows subject to the provisions of ASR 312 (MOP 2-4 contains the same information); Canada - Landplane only eligible. NOTE - Export license from State Department may be necessary prior to export of this type aircraft. EQUIPMENT: A plus (+) or minus (-) sign preceding the weight of an optional item indicates net weight change between that item and the equivalent required item. Propellers and Propeller Accessories 1. Ham. Std. hub 2B20, blades 6135A-6 to 6135A-10 106 lbs. (+1) Diameter limits: 8’6-1/8” max., 8’1-7/8” min. Pitch settings: With 6135A-6, -7 & -8 blades 19 o High, 6.5o Low With 6135A-9 & -10 blades 19 o High, 8o Low 2. Ham. Std. hub 2B20, with Erco blades 3086A (AAF 42K18993) 116 lbs. (+1) Diameter limits: 8’6” max., 8’1-7/8” min. Pitch settings: 22o High, 6.5o Low 3. Ham. Std. governor (1012-G) 5 lbs. (+9) 4. Montgomery (Ajax Die Casing Co.) propeller Type D-72 spinner 8 lbs. (+1) for Hamilton Standard propeller Engines and Engine Accessories - Fuel and Oil System 101. Carburetor heater 102. Carburetor air filter 103. Starter (Eclipse type 397 model 15) 20 lbs. (+36) 104. Omitted (March 5, 1947) 105. Vacuum pumps (Eclipse type 692 model 2) Landing Gear 201. 7.50-10 wheels (Goodrich); 8.5-10 6-ply tires and tubes; Expander tube hydraulic brakes (Goodrich, Army G-2-210) 202. 10 in. tail wheel (Goodrich, Army B-3-28A); 5 lbs. (+298) 10 in. S.C. 4-ply tire and tube Electrical Equipment 301. Generator (Eclipse type 307 model 11) 22 lbs. (+35) 302. Battery (Exide R129DN) 39 lbs. (+166) 303. Landing light (Grimes) 4 lbs. (+88.5) 304. Generator control box (type 1035 model 2) 4 lbs. (+67) 305. Position lights (a) 2 Grimes type C (Wing) 2 lbs. (+91) (b) 1 Grimes type A (Tail) 1 lb. (+299) Page 3 of 4 A-774 Interior Equipment 401. Pilot’s seat with Army type B-11 safety belt 12 lbs. (+84) 403. Heating system 6 lbs. (+38) 404. Ventilating system 2 lbs. (+85) 405. Escape hatch in roof of cabin 18” x 24” NOTE 1. Current weight and balance report including list of equipment included in certificated weight empty, and loading instructions when necessary, must be in each aircraft at the time of original certification and at all times thereafter (except in the case of air carrier operators having an approved weight control system). NOTE 2. Prior to certification as a civil aircraft, the following must be accomplished: A. Fuel and Oil Systems and Tanks: (1) Each fuel and oil tank filler opening, or the structure adjacent thereto, shall be placarded as to contents, capacity and octane rating. (2) A satisfactory means of measuring the oil shall be provided. (3) A suitable guard shall be placed over the fuel tank drain valve located on cabin floor between seats to prevent inadvertent opening during flight. (4) Fuel gages must be checked for accuracy. B. Aircraft and Engine Nameplates: (1) The following information must be listed on the manufacturer’s nameplates: (a) Manufacturer’s name, model designation, serial number, date of manufacture and date of conversion, on aircraft nameplate. (b) Type certificate number, and if military engine, equivalent commercial designation on the engine nameplate. C. Instruments: (1) All instruments must be marked for approved operating limitations. D. Control System Lock: (1) The rudder pedal control lock on the co-pilot’s side must be removed. E. The following placard must be placed on the instrument panel in full view of the pilot: “Intentional spinning prohibited.” F. A placard reading as follows must be installed in such a location that it will be unmistakably visible to anyone removing the co-pilot’s controls: “When co-pilot’s controls are removed, the universal joint must also be removed.” G. Electrical System: (1) The “master” and “generator” switches should be ganged to provide simultaneous operation to the “off” position. (2) For day operation, circuit protectors in the circuits to electrical equipment used in the operation should be made accessible to the pilot in flight. The airplane should be restricted to day operation. (3) To make the airplane eligible for night operation, the following must be accomplished: (a) Relocate all electrical circuit protective devices so they are accessible to the pilot in flight. (b) Remove the resistors in the wing position light circuit and gang all position lights to operate simultaneously. A-774 Page 4 of 4 NOTE 3. Prior to certificate as a 4 or 5-place airplane, the following must be complied with: Passenger seat, or seats, flooring and safety belt installations other than originally provided by the manufacturer must be Shown to meet the requirements of CAR 4a. The following manufacturers have fabricated rear seat kits which, when properly installed, meet the requirements set forth above: Aircraft Utilities Summit and Lafayette Streets, Toledo 4 Ohio (Seat kits to be installed in accordance with the manufacturer’s installation instructions dated July 27, 1946) Carl E. Guldberg 610 Wolverine Bldg., Ann Arbor, Michigan (Seat kits to be installed in accordance with the manufacturer’s installation instructions dated August 8, 1946) Allied Aircraft Co. Clarendon Hills, Illinois (Seat kits to be installed in accordance with the manufacturer’s installation instructions dated August 9, 1946) All American Aviation, Inc. Wilmington, Delaware (Seat kits to be installed in accordance with the manufacturer’s installation instructions dated September 13, 1946) .....END..... ``` ## ADs None name its models. ## Registered aircraft by registry model (OpenAirDocs) - [Stinson VULTEE V-77](https://openairdocs.org/model/stinson-vultee-v-77): 85 aircraft (registry code 8631802) - [Stinson V77](https://openairdocs.org/model/stinson-v77): 0 aircraft (registry code 8631851) ## STCs approved under this data sheet (36) - [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC - [STC SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc. - [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc. - [STC SA04046CH PAGE 2](https://openairdocs.org/stc/SA04046CH%20PAGE%202): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc. - [STC SA01757WI](https://openairdocs.org/stc/SA01757WI): To allow the use of UL91 or UL94 (minimum) grade aviation fuel. 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 SA04776NY](https://openairdocs.org/stc/SA04776NY): The HIPEC Covering and Finishing System must be performed and maintained. HIPEC Aircraft Coatings Inc. - [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC - [STC SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc. - [STC SA11174SC PAGE 1](https://openairdocs.org/stc/SA11174SC%20PAGE%201): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King) - [STC SA10822SC](https://openairdocs.org/stc/SA10822SC): Installation of EFD1000 Primary Flight Display. Aspen Avionics Inc. - [STC SA01831WI](https://openairdocs.org/stc/SA01831WI): To allow the use of UL91 (minimum) grade aviation fuel. Petersen Aviation Inc - [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation - [STC SA2691SO](https://openairdocs.org/stc/SA2691SO): Installation of Cleveland hydraulic brake conversion kit no. 199-167. Rare Aircraft Ltd - [STC SA00024NY](https://openairdocs.org/stc/SA00024NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K007 on single or multi-engine fixed wing light aircraft incorporating Lycoming reciprocating engines of 450 horsepower or less.. Airwolf Filter Corporation - [STC SA01734SE](https://openairdocs.org/stc/SA01734SE): Application of Stewart Systems synthetic fabric covering system to aircraft fuselage, wings, tail surfaces, control surfaces and related parts.. Andrew D. Humphrey - [STC SA00478CH](https://openairdocs.org/stc/SA00478CH): Installation of Cooper Superflite 102 Fabric.. Aviation Products Systems Inc. - [STC SA02442AK PAGE 2](https://openairdocs.org/stc/SA02442AK%20PAGE%202): Approval of the L-3 Communications NGT 2000/2500 ADS-B system. ADS-B Technologies, LLC - [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 2](https://openairdocs.org/stc/SA02402SE%20PAGE%202): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) CGR-30C. Electronics International Inc. - [STC SA03283CH](https://openairdocs.org/stc/SA03283CH): Installation of a 450 H.P. Pratt & Whitney Model R985-AN-14B Engine with Hamilton Standard Propeller Model 6167A-12 propeller and Model 2D30-237 Hub. Rare Aircraft Ltd - [STC SA00068SE](https://openairdocs.org/stc/SA00068SE): Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1). Electronics International Inc. - [STC SA01988SE](https://openairdocs.org/stc/SA01988SE): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.. Electronics International Inc. - [STC SA02033AT](https://openairdocs.org/stc/SA02033AT): Modification to install an air-oil separator to prevent oil from being aspirated from the engine breather line.. M-20 Oil Separators LLC - [STC SA01157LA](https://openairdocs.org/stc/SA01157LA): Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument.. Electronics International Inc. - [STC SA8075SW](https://openairdocs.org/stc/SA8075SW): Installation of fiberglass covering. (M-62 SERIES PT-19) (G-73 SCHWEIZER). Razorback Fabrics Inc - [STC SA1236GL](https://openairdocs.org/stc/SA1236GL): Surrendered and incorporated into STC SA00478CH.. Cooper Aviation Supply Company, Inc. - [STC SA02520AT](https://openairdocs.org/stc/SA02520AT): Installation of M-20 Oil Separator, model 600-WP.. M-20 Oil Separators LLC - [STC SA00068LA](https://openairdocs.org/stc/SA00068LA): Installation of tail wheel adapter ring.. R-R-R-Russ Aircraft - [STC SA4-1210](https://openairdocs.org/stc/SA4-1210): Installation of Eonnex cover on aircraft surfaces.. Ceconite, Inc - [STC SA2622WE](https://openairdocs.org/stc/SA2622WE): Installation of Pratt & Whitney R-985-39, -39A, -AN-1, -AN-3, or -AN14BM1 engine and Hamilton Standard 2D30/6101A-15 or -21 propeller. (V-77 (ARMY AT-19) Landplane only, normal category). Serv-Aero Engineering Inc - [STC SA368CE](https://openairdocs.org/stc/SA368CE): Replace wing rib stitches with P-K screws.. Roberts William - [STC SA4-1620](https://openairdocs.org/stc/SA4-1620): Removal of cabin door for parachute jumping and aerial photography operations.. Lawrence Parks - [STC SA4-428](https://openairdocs.org/stc/SA4-428): Glass cloth with resin applied to all fabric surfaces except movable controls.. Glasco-Air Products - [STC SA4-478](https://openairdocs.org/stc/SA4-478): Ceconite 101 covering of fuselage and vertical stabilizer.. Cooper Engineering Corporation - [STC SA1-34](https://openairdocs.org/stc/SA1-34): Modification for camera installation.. L S Taylor Engineering --- 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.