# TCDS ATC 600: Fairchild Industries Inc. - Type: Type certificate data sheet - Status: Current - Holder: Fairchild Industries Inc. - Revision: 0 - Product: Aircraft, Small Airplane - Registered aircraft: 6, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/10/79/107900cb850092515a3aa4d5088ac8af0377bb7bfa94aa8ef106796ceb4f76a2 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D3B57233D80FD57485256735005AF709.0001 - Page: https://openairdocs.org/tcds/ATC%20600 ## Models (2) As the data sheet lists them. - 24 C8ES - 24 C8E ## What the data sheet says This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers. ```text MODELS: Fairchild 24 CAE and C8ES, 3 PCL-SM I.C. NUMBER: ATC 600 I - Specifications Pertinent to Both Models: Engine Warner Super Scarab Series 40, 50, or 504 Placard limits laximum, except takeoff - in. 2050 Ipm (145 họ) Takeoff (one minute) Placard speed Flaps extended 94 Fuel 40 gallons (one 20 gallon tank in each wing) (+26) (See item 307) Oil 3 gallons No. passengers (front +26, rear +53) (See item 307) Spec. basis Approved Type Certificate No. 600 Serial Nos. 2800 and up manufactured prior to 9/30/39 eligible. Approval expired as of that date. EQUIPMENT: (Datum is wing leading edge) (* Means net increase) Class I: Landplane Engine ring cowl 24 1bs. 102. Battery - in engine compartment (Exide 6-TS-7-1 or Reading 6-ARL-9) 23 1bs. 103. Starter (Eclipse Y-150) 18 1bs. 1040 0.207 10 weeds 105. & in. streamline tail wheel 106. Propeller - wood (fixed pitch) 27 1bs. (-48) 107. B. Seaplane: 151. 152. Seaplane type fin underneath fuselage Class I! Miscellaneous items as noted in approved 200. weight and balance 'lares - three 1-1/2 minute 20 1bs. (+48) dadio equipment (a) 22 lbs. installed at approximate location of instrument board (+6) (b) Additional (or other) equipment with C.G. approximately same as baggage (+42) Approved installations by manufacturer are as follows: RCA AVR-7 Series 22 1bS (+6) 0I (+42) Western Electric 17A 22 Ibs (11 1b. receiver at +6) (11 1b. dynamotor at +42) RCA AVR-8 compass 58 1bs. (30 1b. receiver unit at +42 with rear seat moved to right) Fairchild-Kreusi Type RC-3 compass 70 1bs. (+42) 203. Engine metalizing and corrosion proofing 33 1bs. Class III: 301- Landing lights (a) Two (Adams Westlake Type A-6 or Grimes ST-250) 9 1bs. (+4) (b) One in fuselage 5 1bs. (0) 302. Generator and control boz Shielding (a) (b} Bosch LE70/12 B-5) Leece Herille 3CG-3 Wind driven 10 1bs. 20 1bs. 12 1bs. 4 1bs. (-18) (-10) (-18) (-35) Wheel streamlines (on standard type cantilever gear) 16 1bs. (+3) Sport type landing gear with wheel streamlines and Vee strut Drawing cantilever type landing gear) NO. 43117 (replacing standard Met decrease 8 1bs. 306- Propeller - adj. metal (Hamilton Standard hub 7056, blades or -17) (Landplane only) 33 lbs.* 307- Propeller (Curtiss 55511) - fixed pitch metal Use actual weight 307. Auxiliary 20 gallon fuel tank replacing rear passenger seat baggage may be increased this installation) 11 Ibs. * 308. Cabin heater and rentilator 7 1bs. (-5) 309. below 2820) oil radiator (for serial numbers 11 1bs. Parachutes replacing cushions - front seats only 18 1bs. each (+26) 311. Pressure fire extinguisher Bonding 18 lbs. 5 1bs. (-11) (+22) for equipment NOTE 1. specified in Chapter - Skiplane - not eligible. Howeven when special landing gear per structure complies with Canadian requirements for ski installation raving 43143 is installed. (b) All other countries except Australia. II - Model C8E, Designation 3 PCIM: 100 1bs. (carried on both sides of rear passenger (See Item 307) Standard weight 2400 1bs. c.G. limits (+19-0) and (+24.4) III - Model C8ES, Designation 3 PCSM: 135 1DS - (+42) (carried on both sides of rear passenger ssee Item 307) (includes anchor and rope 15 lbs.) Standard weight C.G. limits (+19.5) and (+25.5) ``` ## ADs (3, in force first) - [AD 46-40-01](https://openairdocs.org/ad/46-40-01): Fuel Tank Selector Valve Placard · Fairchild Industries 24 C8, 24 C8A, 24 C8B and 29 more. Effective Dec 31, 1946 - [AD 46-21-01](https://openairdocs.org/ad/46-21-01): Landing Gear Universal Joints · Fairchild Industries 24 C8, 24 C8A, 24 C8B and 14 more - [AD 46-40-02](https://openairdocs.org/ad/46-40-02): Oleo Tube Reinforcement · Fairchild Industries 22 C7, 22 C7A, 22 C7AM and 23 more ## Registered aircraft by registry model (OpenAirDocs) - [Fairchild 24 C8E](https://openairdocs.org/model/fairchild-24-c8e): 6 aircraft (registry codes 3370216, 3370215) - [Fairchild 24 C8ES](https://openairdocs.org/model/fairchild-24-c8es): 0 aircraft (registry code 3370218) ## 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 SA4503NM](https://openairdocs.org/stc/SA4503NM): Remove original cloth covering and install Ceconite covering. Ceconite Division of Poly-Fiber Inc. - [STC SA01406NY](https://openairdocs.org/stc/SA01406NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K017 on single and multi-engine fixed light aircraft and rotary wing. Airwolf Filter Corporation - [STC SA4-1210](https://openairdocs.org/stc/SA4-1210): Installation of Eonnex cover on aircraft surfaces.. Ceconite, Inc --- 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.