# TCDS TC 674: Dart Aircraft Corporation - Type: Type certificate data sheet - Status: Current - Holder: Dart Aircraft Corporation - Revision: 0 - Product: Aircraft, Small Airplane - Registered aircraft: 43, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/6e/0d/6e0d10a246a51b12ef4c16030cb4b57df5ee4522de4a755c22a274bffe052c93 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/9B6883BFAB0920B98525673200619BEC.0001 - Page: https://openairdocs.org/tcds/TC%20674 ## Models (4) As the data sheet lists them. - G - GW - GK - GC ## What the data sheet says This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers. ```text DART AIRCRAFI COBPORATION HODELS: Dart G, GS, GR, GH I.C. NUMBER: 674 I - Model G. 2 PCLM (Approred 4/19/38) Engine Lambert R-266 Engine limits Por all operations, 2375 rpm (90 hp) Airspeed limits Level flight or clinb - 122 mph frue Ind. Glide or dive - 160 nph Irue Ind. Propeller limits Maxinun permissible dianeter 80 in. C.G. range (+16-2) Maximum weight 1550 1bs. No. seats 2(+24) Maximum baggage Fuel capacity 25 gallons (two tanks in wing at 12-1/2 gallons each) (+29) oil capacity Serial NOS. eligible up per NOTE A (Also see NOTE 2) Required equipment Items 101(9), 102(3), 123, 104, 105, 106 and 107 (a) II - Model GK, 2 PCIM (Approved 12/14/38) Engine LeBlond 90 5F Engine limits For all operations, 2250 rpm (90 hp) Airspeed limits Level flight or clinb - 122 mph True Ind. Glide or dive - 16) Propeller limits Maximum permissible dianeter 80 in. C.G. range to (+20.4) Maximum weight NO. seats Maximum baggage 40 1bs. (+37) Fuel capacity 25 gallons (two tanks in wing at 12-1/2 gallons each) (+29) Oil capacity 2-1/2 gallons (-13) Serial Nos. eligible GK-8 and up per NOIE A Required equipment Items 101(a), 102(a), 103, 104, 105, 106, 107(3) III - Model GW, 2 PCLM (Approved 5/16/39) (See NOTE 3) Engine Warner Scarab Jr. Engine limits Por all operations 2025 rpm (90 hp) Airspeed limits Level flight or climb - 122 mph frue Ind. Glide or dive - 16) mph True Ind. Propeller limits Maximum permissible dianeter 78 in. C.G. range (+15.6) to (+1706) Maximum weight 1650 1bs. NO. seats 2(+24) Maximum baggage None Fuel capacity 25 gallons (two tanks in wing at 12-1/2 gallons each (+29) Oil capacity 2-1/2 gallons (-13) Serial Nos. eligible GW-20 and up per NOTE A Required equipment Itens 101(a), 102(3), 103, 104, 105, 106, 197 (b) and 108 IV - Model GC, 2 PCLY (Approved 7/30/46) Engine Continental 4-100-1 Fuel 73 mininum octane aviation Jasoline Engine limits For all operations, 2350 cpn (100 hp) Airspeed limits Level flight or clinb - 122 nph True Ind. Glide or dive - 16) nph True Ind. Propeller limits Static rpn at maxinun permissible throttle setting - not over 2030, not inder 1930. No additional tolerance permitted. Diameter - not over 76 in., not under 74.5 in. C.G. range (+16.2) to (+20.4) Maxinum weight 1550 1bs. No. seats 2 (+24) Maximum baggage None Fuel capacity 25 gallons (two tanks in wing at 12-1/2 gallons each) (+29) oil capacity 6 quarts (-31) Serial NOS. eligible Required equipment Itens 101 (b), 102 (b), 103, 124, 105, 105 and 107(3) Specifications Pertinent to All Models: Datum Leading edge of wing at fuselage Leveling means Left window sill is horizontal when airplane level. Certification basis Type Certificate No. 674 (Aero. Bulletin 74) production basis None (See NOTE A) Export eligibility Eliqible for export to all countries except Australia, Great britain anl New Zealand EQUIPMENT: A plus (*) or ninus (-) sign preceding the weight of an optional iten indicates the net weight change when that iten is installed. Propeller and Propeller Accessories: 107. Propeller (a) Wood (fixed pitch) 22 1bs. (-41) (b) hub 7005, 7019 or 7029, blades netal (Hamilton Standard 25V2-6) (Model GW only) 35 1bs. (-41) Engine and Engine Accessories - fuel and Oil System Ring cowl NACA smooth type (Models G, GK and SW) 17 1bs. - 28 Engine cowl (Model 16 1bs. -24 Collector ring with carburetor air heater (Models G. carburetor heater and cabin 10 Ibs. (-30) Engine driven fuel pump Hand pump AC No. 1523197 4 1bs. (-12.5) 109. Strainer - Tillotson Imperial No. 41775 (Model GC only) 2 lbs. (-12.5) Eclipse Y-150 (Models G and G4) 17 1bs. 1-17 Eclipse Y-150 (Model GW) 18 1bs. 1-141 (c) Delco-Reny CEX 40194 (Model GS) 15 1bs. 306- Generator (a) Air driven (Air Associates) 7 1bs. (+12) (b) Engine driven (Denco-Reny KX-33371) 303. Cabin heater (Models S, GK and GH) 309. Dual throttle + 1 1b. (-3) 311. Engine ring cowl (with proJections) (Model G only) - 4 1bs. (-28) 18x8-3 wheels (Goodyear 33 1bs. (+5) 3 1bs. (+163) Landing gear strut fairing 8 1hs. (+5) Wheel streamlines (Hill) 12 1bs. (-17) Dual brake pedals +2 1bs. (-41) wheel and tire 7 1bs. (+161) Scott tail wheel 3-245, General 5 1bs. (+164) Electrical Equipment 305. Battery and container Exide 6A2-7-1 (Models G, GK, and GW) 19 1bs. Or (-13) (b) Rending Type R33L (Model GC) 30 1bs. (+37) Interior Equipment: 302. Miscellaneous extra instruments 10 1bs. (+4) 303. Two parachutes at 20 1bs. each 40 1bs. (+24} Pior to original certification, each aircraft must satisfactorily An inspection for workmanship, naterials and conformity before any covering, metal priming or final finish is applied. A final inspection of the completed aircraft. A check of the flight chatacteristics. Current weight and balance report including list of equipment and at si time thereafter locept in the same of of carrier spearsion having an approved weight control system). NOTE 2. Serial Nos. G-2, G-3 and G-4 were manufactured by Monocoupe Corp. under Approval No. Serial No. G-1 manufactured by Monocoupe, also eligible with the following changes: (maximum permissible diameter 78 in.) Wheel streamlines 6.50-10 wheels and brakes (Ebbert Hatch) Exhaust collector ring NOTE 3. Model GW airplanes nust have elevator up travel restricted to 19 degrees and aileron bell crank (part 13-9) installed restricting down aileron travel. ``` ## ADs (4, 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 - [AD 94-18-04 R1](https://openairdocs.org/ad/94-18-04-R1) (historical): Outer Wing Panels · Univair 415-C, 415-CD, 415-D and 7 more. Effective Mar 24, 1995 - [AD 86-22-09](https://openairdocs.org/ad/86-22-09) (historical): Fuel Line Nipple · Univair 415-C, 415-CD, 415-D and 4 more. Effective Nov 13, 1986 - [AD 52-02-02](https://openairdocs.org/ad/52-02-02) (historical): Aileron Balance Assembly · Univair 415-C, 415-CD, 415-D and 2 more ## Registered aircraft by registry model (OpenAirDocs) - [Ercoupe G](https://openairdocs.org/model/ercoupe-g): 21 aircraft (registry code 0420722) - [Dart GC](https://openairdocs.org/model/dart-gc): 6 aircraft (registry code 2700104) - [Dart G](https://openairdocs.org/model/dart-g): 5 aircraft (registry code 2700102) - [Dart GK](https://openairdocs.org/model/dart-gk): 5 aircraft (registry code 2700106) - [Dart GW](https://openairdocs.org/model/dart-gw): 4 aircraft (registry code 2700108) - [Forney G](https://openairdocs.org/model/forney-g): 1 aircraft (registry code 0420702) - [Monocoupe G](https://openairdocs.org/model/monocoupe-g): 1 aircraft (registry code 5810120) ## STCs approved under this data sheet (4) - [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels 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 SA01959SE](https://openairdocs.org/stc/SA01959SE): Installation of a Lycoming O-320-A2B engine and Sensenich M74DM-58 propeller; installed in accordance with FW-TAL385-04, Revision IR, dated July 3, 2008, and maintained in accordance with Instructions for Continued Airworthiness Document Number FW-TAL385-13, Revision IR, dated 9/25/08.. Timothy A. Lunceford --- 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.