TCDS ATC 595

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.