- Holder
- Piper Aircraft Inc.
- Revision
- 0
- Status
- Current
- Product
- Aircraft · Small Airplane
- Models
- 1
- Registered
- 3 aircraft
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 |
|---|---|---|
| J3P |
Airworthiness directives · 9
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 · 20
STC SA04652CHTo allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specificationSTC SA1496GLInstallation of a 12-gallon fuel tank and fuel system in the left wing or left and right wings.STC SA01734SEApplication of Stewart Systems synthetic fabric covering system to aircraft fuselage, wings, tail surfaces, control surfaces and related parts.
See all 20 STCsWhat the data sheet saysOCR
This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers.
MODEIS: Fiper J3P, 2 PCIM
I.C. NUMBER: 695
Engine Lenape Aeromarine AR-3-160 (ATC 74) (See item 309)
Placard limits Maximum, except take-off
-- in.Hg.. 2125 rpm (50 hp)
Take-off (one minute)
-- in.Hg.. 2125 rpm (50 hp)
Propeller Maximum permissible diameter 78 inches
Placard speeds level flight or climb - 90 mph True Ind.
Glide or dive - 122 mph True Ind.
Fuel capacity 12 gallons (-18)
cil capacity gallon (-29)
No. passengers 1 (+9) 01 (+36) (See NOTE 2)
Baggage 20 1bs. (+49)
Standard weight 1100 1bs.
C.G. limits (+10.6) and (+22.7) (See NOTE 3)
Specification basis Type Certificate No. 695
Production Certificate No. 7
Serial numbers 2325, 2327, 2339, 2340, 2342, 2344, 2345, 2347,
2351, 2355 and up manufactured prior to
1/10/42 eligible. Approval expired as of that
date.
EQUIPMENT: (Datum is leading edge of wing) (* Means net increase)
Class I:
101. Propeller - wood (fixed or adj. pitch) 11 lbs. (-51)
102. 8.00-4 wheels (Hayes 840) with tires 20 lbs. (+3)
103. Tail skid (+190)
104- Carburetor air heater (D84B) 3 1bs. (-39)
Class II:
200. Miscellaneous items as noted in
approved weight and balance report.
Class III:
Frieze type ailerons replacing
unbalanced type
20 1bs. (+9)
20 1bs. (+36)
Battery
(a) (Exide 3-AC-7) 10 Ibs. (-19)
(b) (Willard SYR-7-3) 10 1bs. (-19)
(c) (Reading 3-BRL-6) 8 1bs. (+49)
304. 6 x 2.00 steerable tail wheel
(Aircraft Associates) 3 lbs.* (+197)
305. Emergency exit Neglect weight
306. Wheel streamlines Net decrease 3 ibs. (-18) 6 1bs.
307- Alternate fuel tank (9 gallons)
308. Wheels
(a) 18x8-3 (Goodyear 3INBM) with tires Net decrease 2 1bs. (+3)
(b) 7.00-4 (Shinn 2A or 2AV) with
tires Net decrease 1 1b. (+3)
(c) 8.00-4 (Hayes 841) with tires and
Expander Tube brakes 12 lbs.* (+3)
309. Lenape Papoose IM-3 engine with
following limits: Net decrease 12 1bs.
Maximum, except take-off
-- in.Hg.. 2200 rpm (50 hp)
Take-off (one minute)
-- in. Ag., 2200 rpm (50 hp)
310. Skis
(a) Piper S-1000
(b) Fairbanks MF-5
(C) Federal SA-1 or SA-2
(d) Federal SC-1 or SC-2
(e) Aviation Service B
(£) Air Transport 1220-480
(g) Maraton MFS-1600
(h) Heath 655
311. 2-hinge tail surfaces (D-5142-C and
D-4157-C) Neglect weight change
312. Dual brake installation
NOTE 1. Eligible for export as follows subject to inspection for required
equipment (1/10/42):
(a) Canada
- Landplane
- Skiplane - not eligible. However, structure complies with Canadian
requirements for ski installation with item 310(a), or equivalent
skis installed. (Maximum ski height 8-1/2 inches, maximum overhang
3-7/16 inches to outer face of brake plate.)
(b) Australia and Great Britain provided rear spars are reinforced in
accordance with Piper Drawing J3-A140.
(C) All other countries except New Zealand.
NOTE 2. Manufacturer recommends that airplane be flown solo from rear seat
only.
NOTE 3. . 0452, 9457, 4458, 4459, 4460, вави, 4 66, 4467, 4469, 4471, 0473.
4451, 4452,
4474, 4475, 4477, 4478, and 4502 eligible with the following
C.G. limits: (*10.6) and (+21.5)