# TCDS A-709: Consolidated Vultee Aircraft Corporation Stinson Division - Type: Type certificate data sheet - Status: Current - Holder: Consolidated Vultee Aircraft Corporation Stinson Division - Revision: 5 - Revised: November 9, 1956 - Product: Aircraft, Small Airplane - Certification basis: CAR 4a - Registered aircraft: 62, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/16/2c/162cc249462f460268191ddafd21d2be8b86a51d27de238d210628573009cfea - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/024EA3CF82D8C6858525673E00595693.0001 - Page: https://openairdocs.org/tcds/A-709 ## Models (2) As the data sheet lists them. - HW-75 - 10 ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text Page No. 1 2 3 4 Rev. No. 5 5 5 5 DEPARTMENT OF COMMERCE CIVIL AERONAUTICS ADMINISTRATION A-709 Revision 5 STINSON HW-75 10 November 9, 1956 AIRCRAFT SPECIFICATION NO. A-709 Manufacturer Stinson Division Consolidated Vultee Aircraft Corp. I - Model HW-75, 3 PCLM, Approved May 20, 1939 and Model 10, 3 PCLM, Approved April 22, 1940 (Model 10 is same as HW-75 except for wider cabin and minor structural changes.) Engine Continental A-75-3 (See item 314 for optional engines). Fuel 73 min. grade aviation gasoline Engine limits For all operations, 2650 rpm (75 hp) Propeller limits (75 hp): Max. permissible diameter 81 in. (with item 101) (80 hp): Static rpm at max. permissible throttle setting: Not over 2635, not under 2325. No additional tolerance permitted. Diameter: Not over 81 in., not under 67.5 in. Airspeed limits Level flight or climb 120 mph (104 knots) True Ind. Glide or dive 144 mph (125 knots) True Ind. Flaps extended 85 mph ( 74 knots) True Ind. C.G. range (+14.7) to (+19) Empty weight C.G. range (+14.6) to (+15.5) When empty weight C.G. falls within this range, computation of critical fore and aft C.G. positions is unnecessary. Range is not valid for non-standard arrangements. Datum Wing leading edge Leveling means Top of door frame Maximum weight 1580 lbs. No. seats 3 (2 front at +16 and one rear at +39). Maximum baggage 24 lbs. (+39). Baggage may be increased to 194 lbs. when rear seat passenger is not carried - 100 lbs. on rear seat and 94 lbs. on floor. Fuel capacity HW-75: 18 gals. (+22) See item 305 for extra tanks 10: 20 gals. (+22) Oil capacity 4 1/2 qts. (-40) See item 305 for extra capacity. Control surface movements Not available. A-709 2 Serial Nos. eligible HW-75: 7000 and up manufactured prior to Feb. 28, 1941. Approval expired as of that date. 10: 7501 and up manufactured prior to Feb. 28, 1941. Approval expired as of that date. Required equipment Items 101, 102, 103, 104 and 105 SPECIFICATIONS PERTINENT TO ALL MODELS Certification basis Type Certificate No. 709 (CAR 4a) Production basis Not pertinent - see "Serial Nos. Eligible." Export eligibility Eligible for export to all countries except as follows subject to the provisions of MOP 2-4 . Canada - Landplane - eligible Seaplane - not eligible. However, structure complies with Canadian requirements for ski installation with a maximum ski height of 8-11/16 in. and a tread of 6 ft. 11-5/8 in. (centerline of ski 3-1/16 in. out from edge of torque plate). Equipment: A plus (+) or minus (-) sign preceding the weight of an item indicates net weight change when that item is installed. Propellers and Propeller Accessories 101. Propeller - wood (fixed or adj. pitch) 13 lbs. (-60) 317. Propeller - controllable wood Static rpm at max. permissible throttle setting: Not over 2500, not under 2325. No additional tolerance permitted. Low pitch setting 14° at 22 in. sta. (a) Beech R-1 hub C-100, blades R100-70 +12 lbs. (-60) Diameter: Not over 70 in., not under 68 in. (b) Flottorp R002, hub R002-208, blades R002-205-72 +18 lbs. (-60) (See Prop. Spec. P-804, NOTE 6, for interchangeable blades) Diameter: Not over 72 in., not under 68 in. (c) Propeller control (Beech Dwg. R000-000) to be used with 2 lbs. (-30) either of above propellers 318. Propeller - McCauley 1A90 26 lbs. (-60) Static rpm at max. permissible throttle setting: Not over 2440, not under 2340. No additional tolerance permitted. Diameter: Not over 70 in., not under 68.5 in. 319. Propeller - Beech controllable, hub R002-101 or R003-100, 29 lbs. (-60) blades R003-201-72T includes Beech mechanical pitch control. (See Prop. Spec. P-804, NOTE 6 for interchangeable blades) Static rpm at max. permissible throttle setting: (low pitch): Not over 2500, not under 2325 No additional tolerance permitted. Diameter: Not over 72 in., not under 72 in. Placard required: "Do not exceed 2575 engine rpm in level flight or climb." 320. Propeller - Sensenich M74CK-2 fixed pitch metal (A75 engine only) 21 lbs. (-60) Static rpm at max. permissible throttle setting: Not over 2440, not under 2340. No additional tolerance permitted. Diameter: Not over 72 in., not under 70 in. 3 A-709 Engines and Engine Accessories - Fuel and Oil System 105. Carburetor air heater (Dwg. T-3225) 3 lbs. (-35) 301. Starters (a) (Eclipse E-80) (Item 304(b) required) 18 lbs. (-33) (b) (Eclipse No. 635) (Item 304(b), (c) or (d) required) 16 lbs. (-33) (c) Wiring and switch 2 lbs. (-6) 305. Extra tanks (a) 18 gal. fuel tank (Model HW-75 only) 15 lbs. (+22) (b) 20 gal. fuel tank (Model 10 only) 15 lbs. (+22) (c) 2 gal. oil tank 1 lb. (-40) 313. Revised engine mount (Dwg. T-3830) for engines with No wt. change integral rubber bushings 314. Engines (Continental - see Engine Specs. Nos. 213 and 217) (a) A-75-6 (Limits same as for A-75-3) +3 lbs. (b) A-75-8 No wt. change Engine limits: For all operations, 2600 rpm (75 hp) (c) A-75-9 (Limits same as for A-75-8) +3 lbs. (d) A-80-6, A-80-6J, A-80-9, A-80-9J +3 lbs. Engine limits: For all operations, 2700 rpm (80 hp) Fuel: 80 min. octane (See NOTE 1 for further restrictions.) (e) A-80-8 or A-80-8J No wt. change Limits same as for (d). (See NOTE 1 for further restrictions.) Landing Gear 102. 6.00-6 wheels with brakes (Goodrich 600M) and 4-ply tires 28 lbs. (+1) (Wheels must be placarded for these tires) 103. 6x2.00 solid tail wheel (Firestone No. 206-7B) 2 lbs. (+168) 107. Parking brake 3 lbs. (+13) 302. Wheel streamlines 6 lbs. (+1) 311. Puncture seal tubes 2 lbs. (+1) 315. Skis Use actual wt. change (a) Federal SC-2 316. Wheels (a) 8.00-4 (Goodrich 841) with brakes and 4-ply tires No wt. change (Wheels must be placarded for these tires) (b) Steerable tail wheel control +1 lbs. (+155) Electrical Equipment 104. Battery - 6 volt (Reading No. 324) with box 14 lbs. (-25) 303. Landing lights (Grimes ST-250) one or two 5 lbs. ea. (+14) 304. Battery and box (a) (Reading R-24, 12 vo.) 27 lbs. (-25) (b) (Exide 6TS-7-1, 12 vo.) 28 lbs. (+15) (c) (Exide 6TS-7-1, 12 vo.) 28 lbs. (-25) (d) (Exide 6TS-13-1, 12 vo.) (For serial nos. 7601 and up of model 10 only) 40 lbs. (+15) (e) (Exide 6TS-13-1, 12 vo.) 40 lbs. (+29) A-709 4 310. Generator - wind driven (Air Associates 6 or 12 volt) 8 lbs. (+10) Interior Equipment 201. Flares - three 1 minute International 8 lbs. (+34) 306. Cabin heater 2 lbs. (-35) Miscellaneous (not listed above) 106. Two cabin doors 16 lbs. (+16) NOTE 1. The approval of Continental A-80 Series engines expired May 11, 1949. The only A-80 series engines eligible for installation in certificated aircraft are those manufactured or converted to this series prior to May 11, 1949. Such engines installed in Stinson Model HW-75 and Model 10 aircraft are acceptable provided the following conditions are observed: (a) Propeller Item 101, 317, 318 or 319 must be installed. (b) Fuel tank filler neck or cap must be placarded for 80 octane minimum. (c) Revised engine baffles in accordance with Stinson Dwg. 2-4306 for up-exhaust engine and 2-4305 for down-exhaust engine must be installed. (d) Tachometer must be marked for maximum of 2700 rpm. .....END..... ``` ## ADs (1, in force first) - [AD 46-39-01](https://openairdocs.org/ad/46-39-01): Oleo Truss Wear · Consolidated Vultee Aircraft Corporation, Stinson Division 10 and HW-75 ## Registered aircraft by registry model (OpenAirDocs) - [Stinson 10](https://openairdocs.org/model/stinson-10): 28 aircraft (registry code 8632004) - [Stinson HW75](https://openairdocs.org/model/stinson-hw75): 23 aircraft (registry code 8632002) - [Waco 10](https://openairdocs.org/model/waco-10): 11 aircraft (registry code 9602202) - [Fleet 10](https://openairdocs.org/model/fleet-10): 0 aircraft (registry code 1462002) - [Volaircraft 10](https://openairdocs.org/model/volaircraft-10): 0 aircraft (registry code 9550102) ## STCs approved under this data sheet (29) - [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC - [STC SA00081NY](https://openairdocs.org/stc/SA00081NY): Installation of Iceman Aviation Supplies, Inc. Carburetor Ice Detector.. Alcor LLC - [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 SA01831WI](https://openairdocs.org/stc/SA01831WI): To allow the use of UL91 (minimum) grade aviation fuel. Petersen Aviation Inc - [STC SA00478CH](https://openairdocs.org/stc/SA00478CH): Installation of Cooper Superflite 102 Fabric.. Aviation Products Systems Inc. - [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 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 SA593CH](https://openairdocs.org/stc/SA593CH): Install Champion SlickSTART magneto booster system.. Champion Aerospace LLC - [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 SA01944CH](https://openairdocs.org/stc/SA01944CH): Modify airplane to fly on unleaded automotive gasoline, 87 minimum antiknock index, per ASTM Specification D-439 or D-4818 of any volatility class, A through E, or 82UL AVGAS per ASTM D-6227.. Experimental Aircraft Association Inc. - [STC SA944GL](https://openairdocs.org/stc/SA944GL): Superseded by STC SA01944CH. Modify airplane to fly on unleaded automotive gasoline, 87 minimum antiknock index.. EAA Aviation Foundation - [STC SA8075SW](https://openairdocs.org/stc/SA8075SW): Installation of fiberglass covering. (M-62 SERIES PT-19) (G-73 SCHWEIZER). Razorback Fabrics Inc - [STC SA1008WE](https://openairdocs.org/stc/SA1008WE): Installation of Poly-Fiber covering material.. Poly-Fiber Inc. - [STC SA02520AT](https://openairdocs.org/stc/SA02520AT): Installation of M-20 Oil Separator, model 600-WP.. M-20 Oil Separators LLC - [STC SA5159NM](https://openairdocs.org/stc/SA5159NM): Installation of chip detector system.. Northwest Aircraft Inc - [STC SA5755NM](https://openairdocs.org/stc/SA5755NM): Installation of a propeller anti theft device.. Davis Ray G - [STC SA4-302](https://openairdocs.org/stc/SA4-302): Installation of BN-1 propeller spinner.. ACS Products Co, Inc - [STC SA1351WE](https://openairdocs.org/stc/SA1351WE): Replace existing fabric on wings, fuselage, empennage, and/or control surfaces, with Ceconite101 material. (262A Series -12). Ceconite Inc - [STC SA342SW](https://openairdocs.org/stc/SA342SW): Installation of Lycoming O-235-C1 engine with Sensenich M76AM-2 propeller, associated powerplant changes and electrical changes.. James A Schultze - [STC SA4-1210](https://openairdocs.org/stc/SA4-1210): Installation of Eonnex cover on aircraft surfaces.. Ceconite, Inc - [STC SA798EA](https://openairdocs.org/stc/SA798EA): Installation of Monitair exhaust gas combustion monitor kit.. Rosemount Engineering Co - [STC SA1350WE](https://openairdocs.org/stc/SA1350WE): Replace existing fabric on wings, fuselage, empennage and/or control surfaces with fiberglass cloth.. Ceconite, Inc - [STC SA4-1575](https://openairdocs.org/stc/SA4-1575): Ceconite 101 covering of complete airplane.. Cooper Engineering Corporation - [STC SA4-840](https://openairdocs.org/stc/SA4-840): Fabric replaced with glass cloth on wings, fuselage, empennage and/or control surfaces.. Air Fibre Inc - [STC SA4-184](https://openairdocs.org/stc/SA4-184): Replaced ASO-9 engine with C85-12F engine in accordance with drawing (Form ACA-337 dated 1/26/57).. 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