# TCDS ATC 484: Consolidated Vultee Aircraft Corporation Stinson Division - Type: Type certificate data sheet - Status: Current - Holder: Consolidated Vultee Aircraft Corporation Stinson Division - Revision: 0 - Product: Aircraft, Small Airplane - Data sheet PDF: https://openairdocs.org/files/sha256/dc/82/dc826d45875cfe564c943f28ec4d09afe73fabbc65ac447b73e50603f098bc5f - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/BACFA1897DB588148525673E00578EFA.0001 - Page: https://openairdocs.org/tcds/ATC%20484 ## Models (1) As the data sheet lists them. - U ## What the data sheet says This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers. ```text MODEIS: Stinson U, 10-12 PCLB I.C. NUMBER: 484 Engines 3 Lycomings R-680-BA at 240 hp Propellers Adjustable metal. Blades on outboard engines must be Hamilton Standard 5B1-12 (8 ft. diameter) Fuel 140 gallons or 160 gallons (See NOTES 1 and 5) Oil 12 gallons or 15 gallons No. passengers 530 106: (Sc not 4 ad 5) Baggage Standard weight Specification basis Approved Type Certificate No. 484 Serial numbers 9001 and up manufactured prior to 5/15/34 eligible. Approval expired as of that date. Inspector should specify equipment included in empty weight. The following is a list of equipment approved for this model: 3 small engine ring cowls 72 lbs.; 3 larger engine ring cowls 93 lbs.: wheel streamlines 52 lbs.; radio complete 181 lbs.; 2 landing lights 25 lbs.; battery 72 1bs.; 2 flares generators: 25 amp. 21 1bs.; 3 heaters 20 lbs.; toilet equipment 21 lbs.; water container and 3 gallons water 30 lbs.; Pyrene pressure fire extinguisher 12 lbs.; 35x15-5 wheels 160 1bs.; 12.50-14 tires 201 lbs.; co-pilot's chair 19 lts.; duals 11 lbs.; tail wheel. NOTE 1. Serial numbers 9007 and up have additional one gallon balance tank on fuselage firewall and are also approved with 21 gallon additional fuel tank. Maximum for serial numbers 9007 and up 182 gallons. NOTE 2. Serial numbers 9001 to 9006, maximum allowable baggage 335 lbs. in lower wing stub compartments plus 170 1bs. (total 505 1bs.) when folding auxiliary baggage compartment in right hand forward corner of passenger cabin, which replaces the passenger seat when in use, is installed. go tang auxi dr compat ement replacing Tight front passenger 170 1bs. 2 at 200 1bs. (total 400 folding auxiliary compartment replacing right front passenger 170 capacity of fuselage compartment may be increased to 330 lbs. wher radio (receiver, transmitter and dynamo) is not installed. Serial numbers 9007 and up also eligible with two forward passenger seats removed and large fuselage mail or baggage compartment installed subject to the approval of the air carrier inspector for the specific Maximum allowable capacity win ment 500 1bs. serial numbers y007 and up have iirst bay forward of iront win ttachment fitting lengthened 20 inches for addition of fuselace mai compartment and are eligible with forward sloping or rearward sloping windshield and with or without dual controls. NOTE 4j0 ibs. when remodeled at the factory in accordance with approved data Serial numbers 9015 and up also eligible with a standard weight of (new control system installed). Maximum baggage is 600 1bs. (200 1bs. in each wing stub compartment and 200 lbs. in the fuselage compartment). The allowable baggage in the fuselage compartment may be increased to 330 lbs. when radio not installed. Serial numbers 9015 and up also eligible as the "Executive" model with 6 passengers, crew of 2, with or without dual controls, maximum fuel capacity of 201 gallons (standard 70 gallon tanks increased to 80 gallons, two 20 gallon tanks installed and one gallon balance tank on fuselage firewall), maximum baggage of 410 lbs. (180 1bs. in each wing stub and 0 ibs. in rear of pilot), and maximum standard weight of 9400 lbs. wher remodeled at the factory in accordance with approved data. Note: secretary seat in front is not a passenger seat. No. 2-990) . NOT baded home not the tors uld tied passengere. loaded from the rear. and cargo from the front to rear. Each airworthiness certificate wi!! ``` ## ADs None name its models. ## Registered aircraft by registry model (OpenAirDocs) - [Stinson U](https://openairdocs.org/model/stinson-u): 0 aircraft (registry code 8631702) ## 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 SA01757WI](https://openairdocs.org/stc/SA01757WI): To allow the use of UL91 or UL94 (minimum) grade aviation fuel. Swift Fuels LLC - [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 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 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.