# TCDS TC 2-562: Brewster Aeronautical Corporation - Type: Type certificate data sheet - Status: Current - Holder: Brewster Aeronautical Corporation - Revision: 0 - Product: Aircraft, Small Airplane - Certification basis: CAR 4 - Data sheet PDF: https://openairdocs.org/files/sha256/89/3d/893d0386177988b3b8f91513951a8da6793c39e5d05c0c82a4a8177918d4a695 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F854B738A6416F34852567300049548C.0001 - Page: https://openairdocs.org/tcds/TC%202-562 ## Models (1) As the data sheet lists them. - Fleet (Phillips) 7 ## What the data sheet says This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers. ```text MODELS: Brewster Pleet (Phillips) 7, 2 POLB I.C. NUMBER: 2-562 (Remodeled by Phillips Aviation Company, South Pasadena, CA.) Engine Engine limits Por all operations, 2100 Ipm (120 hp) Propeller Static rpm at maximum permissible throttle setting - not more than 1720, not less than 1720 Diameter - not more than 84 in., not less than Airspeed limits Let tight a ma he n true in. Fuel capacity 24 gallons (one tank in fuselage) (-6.5) Oil capacity gallons (-27.5) No. passengers (+9.5) (pilot at +39.5) (See NOTE 3) Baggage Maximum weight 1678 1bs. C.G. range (*1.8) (32.7 percent MAC) to (+3.1) (35.8 percent MACY MAC 44.1 in. L.E. MAC (+12.6) Certification basis CAR 04.031 effective prior to 11/9/45 Serial Nos. 212 and 403 eligible (See NOTE A EQUIPMENT: (Datum is lower ving leading edge) Propeller - Hamilton Standard adjustable metal, hub 5008, blades 13B0-12 48 1bs. (-70) 102. 22x10-4 (Goodyear) wheels, tires 71 1bs. (-13) Tail wheel - Firestone 3.00x6 4.5 lbs. (+169.5) Phillips D637 oil radiator 5 lbs. (-25.5) Carburetor heater (Phillips 5692) 1 1b. (-5705) 14.5 1bs. (-48-5) Parachute in rear seat (See NOTE 2) 20 1bs. (+39.5) Class II: Miscellaneous items as noted in approved weight and balance report Class III: None Additional airplanes of Fleet 7 may be made eligible when changed Each aircraft certificated must satisfactorily pass. An inspection of the revised structure fining shal finish is and conformity before covering, metal priming or final All woodwork may be varnished. final inspection of the completed aircraft. A complete check of flight and engine cooling characteristics. The serial number (s) of all aircraft certificated under this note must be forwarded to the West Coast Engineering Branch at the time of certification in order that this specification may be revised to include the additional airplane(s) under NOTE 1- Eligible for export as follows subject to inspection for equipment specified in Chapter III of Inspection Handbook: Canada - Landplane - Skiplane - not eligible. All other countries except Great Britain, Australia and New Zealand. NOTE 2. Parachute must be carried at all times in rear seat unless weight and balance is substantiated with parachute removed. Rear cockpit must be placarded: "Parachute must be carried at all times in rear seat." NOTE 3. Front cockpit must be placarded as follows: "When airplane is flown solo, pilot must occupy rear seat." ``` ## ADs None name its models. ## STCs approved under this data sheet (2) - [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. --- 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.