# TCDS ATC 595: Piper Aircraft Inc. - Type: Type certificate data sheet - Status: Current - Holder: Piper Aircraft Inc. - Revision: 0 - Product: Aircraft, Small Airplane - Registered aircraft: 69, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/30/4f/304f54e60c152cbb0dedc11347ac971c7d6524fc702a067cbc17be898c66d5a6 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/3D5C1DF860A7069E862572C9006ED968.0001 - Page: https://openairdocs.org/tcds/ATC%20595 ## Models (1) As the data sheet lists them. - J-2 ## What the data sheet says This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers. ```text MODELS: Piper J-2, 2 PO-CL-SM I.C. NUMBER: ATC 595 Engine Continental A-40, A-40-2, A-40-3, A-40-4 or A-40-5 (dual ignition) (See Item 309) Placard limits (7-40) (A-40-2) except take-off (one minute) -- in.Ag., 2550 rpm (37 hp) (A-40-4) Take-off (one minute) 2575 rpm (40 hp) (A-40-5) Maximum, except take-oif -- in.Hg.. 2575 rpm (40 hp) Take-off (one minute) 2575 rpm (40 hp) Propeller Maximum permissible diameter 81 inches Placard speeds Not required Fuel capacity 9 gallons (one in fuselage cil capacity 1 gallon (in engine crankcase) No. passengers 1 (+9) OI (+36) Faggage (1 compartment aft rear seat) Landplane 20 1bs., Seaplane 12 1ks. anchor and rope 12 1lbs. when carried.") Weights Empty - Use actual (Seaplane approximately 88 lbs. net increase over landplane) Standard - 970 1bs. (serials 500 thru 599) Landplane - 1000 1bs. (serials 600 and up) C.G. limits Landplane (+11.8) and (+20.4) Seaplane (*10.2) and (*20.8) Serial Specification basis numbers Approved Type Certificate No. 59y 500 and up manufactured prior to 9/30/39 Seaplane - 658 and up manufactured prior to 9/30/39 eligible. Approval expired as of that date. EQUIPMENT: (Datum is wing leading edge) Class I: (a) 101. landplane: 7.00-4 wheels (Shinn) and tires 102. Tail skid 103. Wood propeller 2 1bs (b) Seaplane: Item 103 PLUS 151. Edo D-1070 floats 145 1bs. 152. Auxiliary fins (on left and right stabilizer) Miscellaneous items as noted in approved weight and balance report. 201. Everel propeller I-38-A or -B (single 2 lbs. 202. Wheel streamlines 1bs. (b) Seaplane: Items 200 and 201 18x8-3 wheels (Goodyear 3INBM, ATC 26) No change in weight Position lights Cockpit enclosure 304. Steerable tail wheel with 6x2.00 tire Aircraft Associates (Drawing E-4) 3 lbs.. Aero Activities (Drawing 1-C) 3 lbs. 305. 8.00-4 wheels (Hayes Model 840) 306. Battery (3-BRL-6) 1cs Carburetor heater 1bs. Model J2-A902 Combination carburetor and cabin 3 1bs. Model J2-190 Air Transport and Equipment A-40-5 engine with dual ignition 13 1ts.* Parachute - 1 or 2 at 311. Miscellaneous extra instruments Grieder pressure cowling (Model A) 2 lbs. Piper S-1000 Transport A or 1220-480 Federal SA-1 Marston MFS-1200 Seaplane: Items 302, 303, 307, 308, 309, 310, 311, and 312 PLUS Edo 54-1140 float installation 152 unnecessary with this installation) No weight change NOTE 1. Eligible for export as follows subject to inspection ior equipment specified in Chapter XII of Inspection Handbook (5/25/38) geaplane provided modified front lift struts in accordance with Taylor Drawing J2-151 are installed. Skiplane - not However, structure complies with Canadian requirements for ski gear when item 313(a) or equivalent is installed. Great Britain provided wing rear spars are reinforced in accordance with Taylor Drawing J2-115. Australia as landplane only provided that: 1) Wing spars are reinforced in accordance with Taylor Drawing J2-115 2) Modified front lift struts in accordance with Taylor Drawin J2-151 are installed. (3) The following placard speeds are displayed: Level flight or climb (d) All other countries. Not ad 32-Ad5 installation may be made in Field uping parce furnisned by and J2-A65. The airplanes eligible are also approved with alternate seats, heel manufacturer. NOTE 3. some aircraft incorporate splices near the tip of the wing spars, made at the factory. ``` ## ADs (3, in force first) - [AD 99-26-19 R1](https://openairdocs.org/ad/99-26-19-R1): Wings · Piper J-2. Effective Jan 21, 2014 - [AD 99-26-19](https://openairdocs.org/ad/99-26-19) (historical): Wing Lift Struts or Forks · Piper J-2. Effective Feb 14, 2000 - [AD 93-10-06](https://openairdocs.org/ad/93-10-06) (historical): Corroded Wing Lift Struts or Cracked Forks · Piper Aircraft, Inc., The New J-2, J-3, J4 and 28 more. Effective Jul 9, 1993 ## Registered aircraft by registry model (OpenAirDocs) - [Piper J-2](https://openairdocs.org/model/piper-j-2): 48 aircraft (registry code 7100402) - [Taylor J-2](https://openairdocs.org/model/taylor-j-2): 21 aircraft (registry code 7100412) - [Taylor/Michmerhuizen Phil J-2](https://openairdocs.org/model/taylor-michmerhuizen-phil-j-2): 0 aircraft (registry code 7100413) ## 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 SA4503NM](https://openairdocs.org/stc/SA4503NM): Remove original cloth covering and install Ceconite covering. Ceconite Division of Poly-Fiber Inc. - [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 SA00780SE](https://openairdocs.org/stc/SA00780SE): Installation of the True Lock Safety Retention Axle Lock Nut System. True Lock LLC - [STC SA00478CH](https://openairdocs.org/stc/SA00478CH): Installation of Cooper Superflite 102 Fabric.. Aviation Products Systems Inc. - [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 1](https://openairdocs.org/stc/SA02825NY%20PAGE%201): Installation of Aerospace Logic Aircraft Instruments. Aerospace Logic Inc. - [STC SA02825NY PAGE 2](https://openairdocs.org/stc/SA02825NY%20PAGE%202): Installation of Aerospace Logic Aircraft Instruments. Aerospace Logic Inc. - [STC SA00680SE](https://openairdocs.org/stc/SA00680SE): Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.. Electronics International - [STC SA01944CH](https://openairdocs.org/stc/SA01944CH): Modify airplane to fly on unleaded automotive gasoline, 87 minimum antiknock index, per ASTM Specification D-439 or D-4818 of any volatility class, A through E, or 82UL AVGAS per ASTM D-6227.. Experimental Aircraft Association Inc. - [STC SA774GL](https://openairdocs.org/stc/SA774GL): Superseded by STC SA01944CH. Modify airplane to fly on unleaded automotive gasoline, 87 minimum antiknock index.. EAA Aviation Foundation - [STC SA8075SW](https://openairdocs.org/stc/SA8075SW): Installation of fiberglass covering. (M-62 SERIES PT-19) (G-73 SCHWEIZER). Razorback Fabrics Inc - [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 SA4-302](https://openairdocs.org/stc/SA4-302): Installation of BN-1 propeller spinner.. ACS Products Co, 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 SA582NW](https://openairdocs.org/stc/SA582NW): Fabrication of replacement wire rope cable assemblies. University Swagging Corp - [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.