# TCDS ATC 632: Fairchild Industries Inc. - Type: Type certificate data sheet - Status: Current - Holder: Fairchild Industries Inc. - Revision: 0 - Product: Aircraft, Small Airplane - Registered aircraft: 9, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/8d/79/8d79b8bdd3b5e02ad2027de1d41eb3c3fc52cac016ffbca9cfc7cda158a5a876 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/7086C257A715816A8525673500633A21.0001 - Page: https://openairdocs.org/tcds/ATC%20632 ## Models (2) As the data sheet lists them. - 24H - 24HS ## What the data sheet says This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers. ```text MODELS: Fairchild 24H and 24HS, 3 PCI-SM I.C. NUMBER: ATC 632 Specifications Pertinent to Both Models: Engine Ranger 6-390D3 Placard limits all operations: Placard speeds Level flight or climb - 138 mph True Ind. Glide or dive - 165 mph frue Ind. Flaps extended - 94 mph Irue Ind. Fuel 40 gallons (two tanks, 20 gallons in each wing) oil 3 gallons (-19) NO. passengers (front +26, rear +45) Baggage 76 1bs. (Baggage carried on both sides of rear passenger seat) (+42) Spec. basis Approved Type Certificate No. 632 Serial Nos. 3200 and up manufactured prior to 9/30/39 eligible. Approval expired as of that date. EQUIPMENT: (Datum is wing leading edge) (* Means net increase) Landplane Generator (Elec. Spec. NA1) and cutout 17 1bs. (-12) 102. Battery (Reading 6-ARI-1) in engine compartment 29 1bs. (-19) 103. Starter (Eclipse Y-150) 18 1bs. (-13) 104. 6.50-10 wheels (Warner 3270) and tires 55 1bs. (+2) 105. 8 inch streamline tail wheel with 6-ply heavy duty tire (+209) 106. Oil cooler (Harrison) 11 1bs. (-27) 107. Wheel streamlines 16 1bs. (+3) 108. Wood propeller (fixed pitch) 31 1bs. (-60) 109- Flaps and controls 39 lbs. (+51) B. Seaplane: Items 101, 102, 103, 106, 108 and 109 PLUS 151. Edo Model 44-2425 floats with water rudders 151. Seaplane fin 4 1bs. (+196) Class II: Landplane 200. Miscellaneous items as noted in approved weight and balance report. 201. Parachute front seats: (a) Irvin Hike or eaten proting 35 lbs. (+34) (b) Switlik 30 1bs. (+34) 202. Flares (three 1-1/2 minute) 20 1bs. (+56) 203. Metalizing and corrosion proofing 12 1bs. (+42) 204. Corrosion proofing 8 1bs. (+42) 205. Radio equipment (a) Receiver (RCA AVR-7 Series) 25 1bs. (+46) (Chassis at side of or under rear seat) (b) Receiver (W.E. 17A) 25 1bs. (+30) (Chassis at instrument panel power supply at side of or under rear seat) Receiver (RCA AVR-10 Series) 11 1bs. (+11) (Chassis at instrument panel - power supply at +14) (₫) Transmitter (RCA AVT-7 Series) 33 1bs. (+67) (Chassis at side of or supply aft of seat) (e) Compass (Fairchild RC-3) 65 1bs. (+41) (Chassis forward of rear seat - power supply at side of or under (E) Compass (RCA AVR-8) 58 1bs. (+43) (Chassis at side of or under rear Pressure fire extinguisher 18 1bs. (+42) B. Seaplane: Items 200, 201 to 206, inclusive, PLUS 304, 305, 306 and 311 Class III: Landplane Extra 20 gallon fuel tank (replacing rear seat) (Allowable baggage may be increased 40 1bs.) 11 Ibs. (+45) 302. Hub streamlines Yet decrease 12 lts. 303. Seaplane fittings Neglect weight change 304- Generators (a) Wind-driven (Air Associates SK-880) 10 1rs. (-10) (b) Wind-driven (Air Associates 41475) 8 1bs. (+9) 305. Propeller - fixed pitch metal (Curtiss) 15 1bs. (-60) 306. Engine shielding 307. Landing lights (a) One or two (Grimes SI-250) 4-1/2 1bs. each (+16) (b) Two (Adams-Westlake A-6) 9 lbs. (+2) 309. Cabin heater 4 lbs. (-21) 309. Cabin ventilator 310. Dual brake controls 5 1bs. (-7) 311. Fxtra instruments 23 1bs. 312. Quick release door hinges 1 1b. (+10) 313. Engine (a) Ranger 6-410-BIA No weight change Limits: For all operations, 2450 Ipm (165 h₽) B. Seaplane: Items 301, 303, 307, 308, 309, 312 and 313 NOTE 1. up elseator travelt have destees brer setting of -2 degrees, and an Seaplanes must nave NOTF 2. eligible for export as follows subject to inspection for equipmen pecified in Chapter XII of Inspection Handbook (9/30/39) Canada Landplane and Seaplane - Skiplane - not eligible. (b) Australia - Landplane only. (c) All other countries. II - Model 24H, Designation 3 PCIM: eropeller Maximum permissible dianeter 107 in. Standard weiqht 2400 1bs. C.G. limits (+17.1) and (+22.6) III - Model 24HS, Desiqnation 3 PCSM (See NOTE 1) : Propeller Maximum permissible dianeter !12 in. Standard weight 2550 1bs. C.G. limits (+19.2) and (+23.9) ``` ## 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 H](https://openairdocs.org/model/fairchild-24-h): 9 aircraft (registry code 3370302) - [Fairchild 24 HS](https://openairdocs.org/model/fairchild-24-hs): 0 aircraft (registry code 3370304) ## STCs approved under this data sheet (5) - [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 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 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.