# TCDS ATC 165: Ford Motor Company - Type: Type certificate data sheet - Status: Current - Holder: Ford Motor Company - Revision: 0 - Product: Aircraft, Large Airplane - Registered aircraft: 1, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/f3/ab/f3ab59b89e1f5815431c8900c8fa823ae9aa823ff19a488a46c2aeabb00e6eb1 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/9BA92A71EC918B9F85256737004EA0C3.0001 - Page: https://openairdocs.org/tcds/ATC%20165 ## Models (1) As the data sheet lists them. - 5-AT-C ## What the data sheet says This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers. ```text MODELS: Ford 5-AI-C, 17 PCIM I.C. NUMBER: ATC 165 Engines 3 P&W Wasps C1 420 hp (See NOTE 2) 210pe-.e1e Adj. metal Fuel 555 gallons (with no wing tip main compartments) Oil 33 gallons No. passengers 15 Baggage No. and maxinum capacity of compartnents: Double wing tip with extended aileron hinges and special aileron 14003-B each With standard ailerons each Single wing tip Center section (wing root) (400 1bs. each side) Convertible fuselage notes aprone deate -- 800 1bs. compartments installed in rear of fuselage 440 1bs. (On basis of 5-AI-B and fact that so many of this model have compartments in rear now Maximum weight 13500 1bs. (See NOTE 3) Spec. Approved Type Certificate No. 165 Serial Nos. 46 to 96 eligible Eligible with or without convertible mail compartnents in fuselage, iteration outine untain conformit With proved data, 15.00-16 tires on Warner landing gear, 44x10 wheels and brakes, flares, generator, food compartments, batteries, landing and positio lights, radio installation, cabin heater, Pederal SA-14 or Wien Alaska WAA-10 skis, emergency exit in top deck of fuselage between rear wing edge of wing when installed in accordance with approved manufacturer's drawings, tail wheel or skid, and other special equipment approved by inspector. Also eligible with P&W Wasp SC1 engines with the following: Engine limits Maximum continuous 30 in. Hg., 2100 Ipm (450 hp) Takeoff (one minute) 31 in. Hg.. 2100 In (450 hp) 32 in. Hg.. 2000 rpm (450 hp) Airspeed limits Level flight or climb - 144 mph Irue Ind. Glide or dive - 173 mph Irue Ind. Eligible with a maxinum weight of 1400 1bs. with a maximum seating capacity including crew of 14 provided the modified stabilizer with the 6 in. or 12 in. leading edge extension and either wing tip baggage conpart- ments or wing tip fuel tanks are installed. compartments are installed, at least 150 1bs. nust be carried in each double type or 190 lbs. in each single type at all times when flying at a maximum weight of 1400 1bs. If the wing tip fuel tanks are installed, t least 42 gallons must be carried in each at all times when flyin a maximum weight of 1400 1bs. ``` ## ADs None name its models. ## Registered aircraft by registry model (OpenAirDocs) - [Ford 5-AT-C](https://openairdocs.org/model/ford-5-at-c): 1 aircraft (registry code 3590204) ## STCs approved under this data sheet (3) - [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC - [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 SA4302NM](https://openairdocs.org/stc/SA4302NM): Installation of Electronics Int'l digital automatic engine analyzer.. Electronics International --- 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.