# TCDS TC 695: Piper Aircraft Inc. - Type: Type certificate data sheet - Status: Current - Holder: Piper Aircraft Inc. - Revision: 0 - Product: Aircraft, Small Airplane - Registered aircraft: 3, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/67/8c/678c9e025ac19925f72cc1a59f12e7f77acd0471149e3c8d3e55f24e69708c17 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/AE0AECBCA42009EB862572C9006EDB1B.0001 - Page: https://openairdocs.org/tcds/TC%20695 ## Models (1) As the data sheet lists them. - J3P ## What the data sheet says This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers. ```text 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) ``` ## ADs (9, in force first) - [AD 2015-08-04](https://openairdocs.org/ad/2015-08-04): Wings · FS 2000 L-14, AE-1, HE-1 and 77 more. Effective Jun 3, 2015 - [AD 85-06-04](https://openairdocs.org/ad/85-06-04): Fuel Tank · FS 2001 AE-1, HE-1, J5A-80 and 60 more. Effective May 4, 1985 - [AD 78-10-03](https://openairdocs.org/ad/78-10-03): Fuel Venting · FS 2001 AE-1, HE-1, J5A-80 and 66 more. Effective May 23, 1978 - [AD 68-05-01](https://openairdocs.org/ad/68-05-01): Exhaust Mufflers · FS 2001 J5A-80, J5A (Army L-4F), J5B (Army L-4G) and 67 more. Effective Mar 31, 1968 - [AD 58-12-02](https://openairdocs.org/ad/58-12-02): Aileron Hinge Brackets · Piper J-3, J3C-40, J3C-50 and 20 more - [AD 58-01-07](https://openairdocs.org/ad/58-01-07): Control System Turnbuckles · FS 2001 J5A-80, J5A (Army L-4F), J5B (Army L-4G) and 18 more - [AD 52-07-03](https://openairdocs.org/ad/52-07-03): Lift Strut Rework · Piper J-3, J3C-40, J3C-50 and 15 more - [AD 47-50-03](https://openairdocs.org/ad/47-50-03): Canvas Seat Inspection · Piper J-3, J3C-40, J3C-50 and 14 more - [AD 49-14-01](https://openairdocs.org/ad/49-14-01): Elevator Connector Tube Fitting · FS 2003 J-3, J3C-40, J3C-50 and 17 more ## Registered aircraft by registry model (OpenAirDocs) - [Piper J3P](https://openairdocs.org/model/piper-j3p): 3 aircraft (registry code 7100552) ## STCs approved under this data sheet (20) - [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC - [STC SA1496GL](https://openairdocs.org/stc/SA1496GL): Installation of a 12-gallon fuel tank and fuel system in the left wing or left and right wings.. Crown MN Aviation, LLC - [STC SA01734SE](https://openairdocs.org/stc/SA01734SE): Application of Stewart Systems synthetic fabric covering system to aircraft fuselage, wings, tail surfaces, control surfaces and related parts.. Andrew D. Humphrey - [STC SA02428AK](https://openairdocs.org/stc/SA02428AK): Installation of a hydraulically actuated ski drag assembly. Northern Airframes LLC - [STC SA02295SE](https://openairdocs.org/stc/SA02295SE): Installation of an alternate method of fastening aluminum wing ribs to wood spars. Rainbow Flying Service LLC - [STC SA02825NY PAGE 2](https://openairdocs.org/stc/SA02825NY%20PAGE%202): Installation of Aerospace Logic Aircraft Instruments. Aerospace Logic Inc. - [STC SA00270BO](https://openairdocs.org/stc/SA00270BO): Installation of a Teledyne Continental A-65-8, A-65-8F, A-65-9, A-75-8, A-75-8F, A-75-9, C-75-8, C-75-12, C-85-8, C-85-12, C-90-8F or C-90-12F engine and corresponding propeller identified under Limitations and Conditions, and components for a landplane maximum gross weight of 1220 lbs.. Clyde R Smith Jr - [STC SA3AL](https://openairdocs.org/stc/SA3AL): Installation of Fred A. Shaw tundra-bird Model 2500 skis.. Aircraft Innovations, LLC - [STC SA8075SW](https://openairdocs.org/stc/SA8075SW): Installation of fiberglass covering. (M-62 SERIES PT-19) (G-73 SCHWEIZER). Razorback Fabrics Inc - [STC SA00932SE](https://openairdocs.org/stc/SA00932SE): Installation of the Stewart wing tip assembly. Steve Pierce - [STC SA00002DE](https://openairdocs.org/stc/SA00002DE): Installation of replacement Aft Fuselage Section.. Univair Aircraft Corporation - [STC SA00116DE](https://openairdocs.org/stc/SA00116DE): Installation of Replacement Vertical Stabilizer.. Univair Aircraft Corporation - [STC SA1626NM PAGE 2](https://openairdocs.org/stc/SA1626NM%20PAGE%202): Installation of Electronics Int'l Digital EGT/CHT Instruments and accessories. (201 Series). Electronics International - [STC SA2350NM PAGE 1](https://openairdocs.org/stc/SA2350NM%20PAGE%201): Installation of Electronics International Inc digital carburetor/outside air temperature gauges. Electronics International - [STC SA4302NM](https://openairdocs.org/stc/SA4302NM): Installation of Electronics Int'l digital automatic engine analyzer.. Electronics International - [STC SA3862NM PAGE 1](https://openairdocs.org/stc/SA3862NM%20PAGE%201): Installation of Electronics International Primary TIT/EGT/CHT instruments, remote switches and associated accessories.. Electronics International - [STC SA1455NM](https://openairdocs.org/stc/SA1455NM): Installation of a flame proof auxiliary heater-dryer, Model12-1600.. Thermal, Inc - [STC SA2190NM PAGE 1](https://openairdocs.org/stc/SA2190NM%20PAGE%201): Installation of electronics International Digital Volt/Amp Gauges and Accessories.. Electronics International - [STC SA2666WE](https://openairdocs.org/stc/SA2666WE): Ceconite 102 material covering complete aircraft. (262A SERIES -12). Ceconite Inc - [STC SA2350NM](https://openairdocs.org/stc/SA2350NM) (historical): Installation of Electronics International Inc digital carburetor/outside air temperature gauges listed on the attached continuation sheet and the associated accessories.. Electronics International --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.