- Holder
- Brewster Aeronautical Corporation
- Revision
- 0
- Status
- Current
- Product
- Aircraft · Small Airplane
- Certification basis
- CAR 4
- Models
- 1
The release keeps the latest revision of each data sheet. Model names are as the data sheet lists them.
On this page
Models · 1
| Model | Also known as | Note |
|---|---|---|
| Fleet (Phillips) 7 | Formerly Fleet Aircraft, Ltd. |
Airworthiness directives · 0
ADs whose products are models on this data sheet, matched by model and maker.
No ADs matched this data sheet’s models
STCs approved under this data sheet · 2
What the data sheet saysOCR
This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers.
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."