- Holder
- Grumman American Aviation Corporation
- Revision
- 0
- Status
- Current
- Product
- Aircraft · Small Airplane
- Certification basis
- CAR 4
- Models
- 2
- Registered
- 1 aircraft
The release keeps the latest revision of each data sheet. Model names are as the data sheet lists them.
On this page
Models · 2
| Model | Also known as | Note |
|---|---|---|
| G-32 | ||
| G-32A (Army UC-103) |
Airworthiness directives · 0
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STCs approved under this data sheet · 1
What the data sheet saysOCR
This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers.
MODELS: Grumman G-32 and G-32A (Army UC-103), 2 PCLB
I.C. NUMBER: 2-544
I - Specifications Pertinent to Both Models
Airspeed limits Level flight or climb - 240 mph
(T.I.A.S) Glide or dive - 331 mph
Flaps extended - 135 mph
oil capacity (9 gallons carried when
No. passengers
Baggage
C. G. limits (-7-6) and (-0.5)
Cert. basis CAR 04.031
EQUIPMENT:
(Datum is lover wing leading edge.)
Class I:
101- Propeller - Hamilton Standard hub 3D40,
blades 6101A-12 to 6101A-14, inclusive.
Diameter 9'0" maximum, 8'10" minimum. 246 1bs. (-63)
102. Battery (Reading 36 amp. hr.) and box 32 1bs. (+12)
103. Genertor (Eclipse D-1) 26 1bs. (-32)
104- Autofan tail wheel with 10.5 in.
streamline 6-ply tire
105. Radio equipment 57 1bs. (+48)
106. Oil radiator (U.A.P. 0-3190) 24 1bs. (-30)
107. Pressure fire extinguisher (lux
5 1bg. C0-2)
(See Sections II and III)
Class II:
201. Landing light (Adams Westlake A6A) § lbs. (-2)
II - Hodel G-32
Engine Wright Cyclone R-1820G-2
Fuel 97 minimum octane aviation gasoline
Engine limits Maximum continuous
Straine it are Variation 2100 pm (820 hp)
with altitude to 5800 ft.) 34.5 in. Hg..
2100 pm (850 bp)
Takeoff (one minute)
40.0 in. Hg.. 2200 rpm (1000 bp)
Fuel capacity 150 gallons maximum, main 83 gallons (-6),
auriliary 47 gallons (+15), reserve 20
gallons (+38)
Standard weight 4663 1bs.
Serial Nos. 446 only eligible
Class I equipment (continued)
Starter (Federal Cartridge Type L) 41 1bs. (-28)
8.50-10 wheels (Hayes 851A)
8.50-10 6-ply tires (wheels must be
placarded for these tires) 90 1bs.
III - Model G-32A (UC-103)
Engine Wright Cyclone SR-1820F-52 or military R-1820-22
Fuel 87 minimum octane aviation gasoline
Engine limits SR- 1820F-52
Maximum continuous
(S. L.) 34.5 in. 2100 rpm (745 hp)
(Straight line manifold pressure variation with
altitude to 5800 ft.) 34.5 in. Hg.. 2100 rpm
39-0 in. Hg., 2200 rpm (890 hp)
Maximum continuous
35.7 in. Hg.. 2100 rpm (850 hp)
(Straight line manifold pressure variation with
altitude to 6000 ft.) 34.0 in. Hg.. 2100 Ipm
(850 hp)
Takeoff (one minute)
41.0 in. Hg., 2200 rpm (1000 hp)
Fuel capacity 130 gallons maximum: main 83 gallons (-6),
auxiliary 47 gallons (*15)
Standard weight 4372 1bs. (with SR-1820F-52 engine)
4663 1bs. (with R-1820-22 engine)
Serial Nos. 447 only eligible
Class I equipment (continued)
Starter (Eclipse E-160) 39 1bs.
26x6 wheels (Bendix) with 26x6 6-ply
tires (wheels must be placarded
these tires) 86 1bs.
NOTE 1. Eligible for certification with the R-1820-22 engine provided the
two-speed blower controls are removed and the blower speed control lever
on the engine is locked in the "low blower" position.