- Holder
- The Boeing Company
- Revision
- 0
- Status
- Current
- Product
- Aircraft · Small Airplane
- 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 |
|---|---|---|
| 203-B |
Airworthiness directives · 3
ADs whose products are models on this data sheet, matched by model and maker.
Registered aircraft
Registry models that point at this data sheet, with their registered aircraft.
STCs approved under this data sheet · 3
What the data sheet saysOCR
This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers.
MODELS: Boeing 203-B, 2 POLB
T.C. NUMBER: 2-412
(Remodeled by Boeing School of Aeronautics, Oakland, CA)
Engine R-680B-4C or R-6808-4D
Placard limits For all operations, 2000 rpm (215 hp)
Placard speeds Not required
Fuel capacity 38 gallons (two tanks in upper wing center section
at 19 gallons each)
Oil capacity
No. passengers 1 (Front +37, rear +36)
Faggage
Standard weight 2744 1bs.
C.G. limits (+29.1) and (+33.7)
Spec. basis Aero• Bulletin 7A, Section 3
Serial Nos. 1138. 1139, 1940 and 1986 only eligible
EQUIPMENT: (Datum is leading edge of upper wing) (See NOTE 2)
Class I:
101. 30x5 wheels with brakes
102- 10x3 tail wheel
103- Dual controls and instruments
104- Fin and rudder extension
105. Propeller - Hamilton Standard adj. metal
Class II:
200. Miscellaneous items as noted in approved
weight and balance report
201- Battery 42 1bs. (-8)
202- (a) Radio receiver 22 lbs. (+5)
(b) Radio transmitter 10 lbs. (+73)
(c) Dynamotor 11 Ibs. (+6)
(a) 11 1bs. (+62)
(e) Radio mast 6 1bs. (+101)
203. Hand starter 20 1bs.
204. 25x11-4 wheels, tires and brakes
Class III:
None
Eligibie for export as tollows, subject to inspection for equipment
specified in Chapter XII of Inspection Handbook (10/5/40):
- Landplane
- Skiplane - not eligible.
All other countries except Great Britain and Australia.
NOTE 2. and balance report including list of equipment included in
certificated weight empty, and loading instructions when necessary, must
be submitted for each aircraft with original inspector's report and each
subsequent report covering changes in such equipment.