# TCDS TC 628: Spartan Aircraft Company - Type: Type certificate data sheet - Status: Current - Holder: Spartan Aircraft Company - Revision: 0 - Product: Aircraft, Small Airplane - Registered aircraft: 19, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/50/29/50290e5f766ec0d60da75a68ee8e86b305f8e063e878864b28ebc9a8f66e6e0d - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/62E1A412F0CE5C138525673E004CC315.0001 - Page: https://openairdocs.org/tcds/TC%20628 ## Models (1) As the data sheet lists them. - 7W (Army UC-71) ## What the data sheet says This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers. ```text MODELS: Spartan 7W (Army UC-71), 5 PCIM I.C. NUMBER: 628 Engine P & W Wasp Jr. SB with one 4-1/2 N and one 9 N damper (see also item 222) Placard limits Maximum, except take-off Fuel 30.0 in. Hg., 2200 rpm (330 hp) 80 minimum octane (5000 ft.) 28.8 in.Hg.. 2200 rpm (330 hp) (See NOTE 3) 27.5 in. Ag.. 2200 rpm (330 hp) 87 minimum octane (See NOTE 3) 36.5 in. Ng., 2300 rpm (450 hp) Propeller Maximum permissible diameter 103 inches (for clearance) Placard speeds Level flight or climb - 211 mph True Ind. Glide or dive - 257 mph True Ind. Flaps extended - 125 mph True ind. Fuel capacity 112 gallons (5 tanks - 2 fuselage under floor 16-1/2 gallons each (+59.5), 2 in wings 32 gallons each (+42), one in fuselage 15 gallons (-10.5) Cil capacity 7 gallons (-21) No. passengers (1 at +24, 1 at +58, 2 at +70) (crew +24) Baggage Weights Empty - Use actual (approximately 2987 1bs. (+23) with class I items only) Standard - 4400 1bs. C. G. limits (+19.4) and (+29.9) Leveling means Leveling lugs between stations 5 and 6 on right side of fuselage Specification basis Type Certificate No. 628 (Aero. Bulletin 7A) Serial numbers 2. 6 and up eligible per NOTE A and all AAF numbers of Model UC-71. Use manufacturer's number when available. EQUIPMENT: (Datum is wing leading edge at rib number 2) (Second row rivets outboard from fuselage). * Means net increase) (See NOTE 2) 101. Engine ring cowl 37 irs. (-38) Exhaust collector ring (Solar 12-385) 19 ibs. (-38) Generator (Eclipse D-1) 25 lbs. (-33) 43 1bs. (+104) Pressure fire extinguisher (Lux A-1) 18 1bs. (-12) Propeller - Hamilton Standard 2D30 blades 6095A-12 or -13; 6167A-12 or Diameter 8'6-1/8" maximum, For interchangeable blades see Propeller Specification No. at u2 in. rad.' intake valve (Low pitch set, 11'1/2 degrees 157 1bs. (-62) 107. Carburetor air 3 1bs. (-31) Carburetor warm air muff 3 lbs. (-37) Oil radiator (UAP 6" U-3160) 18 1bs. (-26) Fuel pump (hand wobble - Romec D-2) 5 1bs. (+26) Main - 7.50-10 (Goodyear 10 S3M) with brakes and 8.50-10 6-ply HoDs inch streamline tail wheel 70 1bs. (+11) 7 1hs. (+206) Hydraulic brake cylinders (Goodyear) 5 1bs. (-5) Landing gear Retracting mechanism Manual control (Drawing 7W418) Motor (Eclipse Y-150) 18 1bs. (+7) Main (Cleveland XY262S) 78 1bs. (+17) Tail (Cleveland YX162S) 7 1bs. (+204) Control wheel - Throw-over (Drawing 9 Ibs. (+11) 115. Windshield - Plexiglass .20" 9 1bs. (+9) Class II: 200. Miscellaneous items as noted under this number in approved weight and balance report. 201. Starter (Eclipse F-141) 30 1bs. (-27) 202. Battery (Reading 6AR-9) 5 Ibs.* (+104) 203. 4-1/2 minimum flares (International 21 1bs. (+106) 204. Oil radiator (Harrison C-2297) Net decrease 5 1ł:s. (-33) 205. Fuel pump (Romec G-2) 4 1bs. (-34) 206. Engine lubrication - one shot 6 ibs. 1-47 Propeller spinner (Drawing 7W833) 9 lbs. 1-64 208. Vacuum pump, engine-driven (Romec RD 2112) 4 1ts. (-34) shielding (Breeze) 14 1bs. (-41) 210. • 7.50-10 wheels (Hayes 750A) 8 lbs. (+11) Instruments (a) Mixture analyzer (Cambridge) including indicator 2 1bs. (-1) and cells and tubing 5 1ks. (-17) 7 1bs. (-12) (b) • Extra instruments 29 lts. (-1) 213: Cabin warm air muff (Solar 11-162) 2 1bs. (-37) Stabilizer abrasion shoes (Goodrich) 3 lbs. (+204) Windshield - shatter proof glass 12 Its. * (+9) Two at 30 gallons each (replace two at 16-1/2 gallons each) 12 1bs. * (+75) at 15 gallons) 4 lts. * oil tank - one at 9 gallons (replaces one at 7 gallons) 1 1r. * Radio installations Retractable (Waller) 10 1Ds. Reel, fish, leadout 4 Its. Control head and cable 3 1bs. 3 lts. Fixed - Standard receiver 1 1b. Fixed - Compass receiver 2 lts. (RCA AVR-7 series) 29 Ibs. chassis, power supply, support 20 Ibs. wiring, filter 9 1bs. (RCA AVR-8 series) 69 1rs. chassis, power supply, support 34 lts. 15 1bs. Controls and wiring 20 1bs. (Waller AB55-47) 65 lbs. +52 chassis, power supply, support 29 1bs. +73 27 lbs. (+28) cables, control, microphone 9 lbs. (+57) 218. Parachute seats Use actual weights and arms 219. Parachutes 20 1bs. (+24, +58, +70) 220. control wheel (a) Throw-over (Drawing 7W310) Net decrease 1 1t. (+11) (b) Fixed - dual (Drawing 7W340) 4 1bs.* (+11) 221. Constant speed propeller control installation (including control unit 5 1bs. (-34) and Shakespeare C-2164-c flexible control 2 Ibs. (-12) 7 1bs. (-28) 222. P&W Wasp Jr. SB-2 engine with one 4-1/2 N and one 9 N damper 13 1bs.* (-41) 223. Toe brake installation 5 lbs. (-5) Class III: 301. Landing lights (a) (Grimes ST-250) 7 lbs. (+27.5) (b) (Grimes ST-1000) 11 Ibs. (+27.5) 302. Puncture proof tubes 10 lbs. (+11) NOTE A. Each aircraft of model 7w manufactured after 10/20/41, for civil use, must, prior to original certification satisfactorily pass: (a) An inspection for workmanship, materials and conformity before any covering, metal priming or final finish is applied. All woodwork may be varnished. (b) A final inspection of the completed aircraft. (c) A check of flight characteristics. NOTE 1. Eligible for export to all countries except Canada, Australia and New Zealand, subject to inspection for equipment specified in Chapter XII of Inspection Hardbook. NOTE 2. Weight and Balance Report including list of equipment included ir. certificated weight empty, and loading instructions when necessary, must be submitted for each aircraft with original inspector's report and each subsequent report covering change in such equipment. NOTE 3. (a) Mark main fuel tank fillers: "80 octane minimum." (b) Mark auxiliary fuel tank fillers: 1180 octane minimum. " (c) Mark reserve fuel tank filler: "87 octane minimum." (d) Mark fuel selector valve accordingly. ``` ## ADs (1, in force first) - [AD 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI or SA02658SE). Effective Mar 21, 2022 ## Registered aircraft by registry model (OpenAirDocs) - [Spartan 7W](https://openairdocs.org/model/spartan-7w): 19 aircraft (registry code 8430302) ## STCs approved under this data sheet (19) - [STC SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc. - [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC - [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 SA02594SE](https://openairdocs.org/stc/SA02594SE): SkyView HDX Instrumentation and Autopilot System manufactured. Dynon Avionics - [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 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 2](https://openairdocs.org/stc/SA11174SC%20PAGE%202): 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 SA6070NM](https://openairdocs.org/stc/SA6070NM): Installation of a 'quick-disconnect drain plug' on the engine rocker sump for the oil drain retrieval system after engine shutdown.. West Coast Air Creations - [STC SA01282NY](https://openairdocs.org/stc/SA01282NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K015 on aircraft powered by Pratt & Whitney radial reciprocating engine Series R-985, R-1340 and R-1830.. 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 SA5658SW](https://openairdocs.org/stc/SA5658SW): Installation of Brittain Industries B5C Flight Control System. Brittain Industries, Inc - [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 SA122SW](https://openairdocs.org/stc/SA122SW): Installation of fiberglass square wing tip.. Ursell C R --- 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.