| Rearwin
Junior |
| Specifications |
3000 |
3001 |
3100 |
4000
|
Aircraft Type Certificate
|
|
|
#481
(05-06-32) |
|
Length |
21
ft 11 in |
|
|
22
ft 3 in |
Height |
7
ft 6 in |
|
|
7
ft 6 in |
Wing
Span |
36
ft |
|
|
36
ft |
Wing
Area |
179.5
sq ft |
|
|
179.5
sq ft |
| Construction |
| The
fuselage
framework was built of welded chrome-moly and 1025 steel tubing,
lightly faired to shape and fabric covered. One elongated cockpit
seated
two in tandem; there was a large windshield in front and a smaller
windshield for the rear seat. A detachable full enclosure was optional.
A large rectangular door offered easy entry into either seat. The
wing framework in two halves was built up of laminated spruce spar
beams with spruce and birch plywood truss-type wing ribs. The
leading edges were covered with plywood sheet and the completed
framework was covered in fabric. The center section was mounted
high above the cockpit on steel tube struts and the wings were
braced to the lower fuselage by streamlined steel tube struts.
The split-axle landing gear of 72 inch tread used a spool of rubber
shock-cord or Rusco rubber compression rings to absorb the shock.
16x7-4 Goodyear airwheels w/o brakes were standard equipment. Tail
skid was of steel spring-leaf type. The fabric-covered tail group
was built up of welded steel tubing and channel sections. Horizontal
stabilizer was adjustable in flight. A wooden Aeromarine propeller,
dual joystick controls were standard equipment. A 12 lb. or 28
lb detachable winter enclosure was optional. |
| |
| Power
Plant |
Engine MFG
|
Szekely |
Poyer |
Szekely |
Aeromarine |
Model |
SR-3-0 |
|
SR-3-55 |
AR-3 |
H.P. |
45 |
40 |
50 |
40-50 |
| Fuel
Data |
Gasoline
capacity (upper wing)
|
|
|
|
12
gal |
Gasoline
capacity (fuselage) |
|
|
|
|
Oil
capacity |
|
|
|
6
qts |
| Equipment |
| |
| Load |
Weight
empty
|
569
lbs |
|
|
506
lbs /617 lbs* |
Useful
load |
430
lbs |
|
|
433
lbs/423 lbs* |
Payload |
177 lbs |
|
|
180
lbs/170 lbs* |
Gross
weight loaded |
999 lbs |
|
|
1038
lbs / 1040 lbs* |
| Performance |
High
speed (full load)
|
|
|
|
91
mph |
High
speed (pilot alone) |
|
|
|
|
Cruising
speed (full load) |
|
|
|
76 mph |
Landing
speed (full load) |
|
|
|
30
mph |
Cruising
range (full load) |
|
|
|
240
miles |
Climb
at sea level (full load) |
|
|
|
700
ft |
Climb
to 10,000 feet (full load) |
|
|
|
|
Take
off time (pilot alone) |
|
|
|
|
Take
off time (full load) |
|
|
|
|
Absolute
ceiling (full load) |
|
|
|
16,000
ft |
| Cost |
Retail
price from factory |
$1,800 |
|
|
$1,880 |
| Comments |
| |
|
|
|
* specifications
shown with/without the removable cockpit enclosure |
