Number of Active Aircraft: 470 Active- Map


A later variant of the J-3. Modifications include a fully closed cowl, fuel tanks in the wing instead of by the firewall, seats moved slightly aft tapering the window back, and lowering the engine. They were built between 1947 and 1949. As evident from its specs, it included a higher power engine.

Fuel Cost ($):
General Stats:
Seat Capacity: 2
Empty Weight: 750 lbs
Max Weight 1220 lbs
Useful Load: 470 lbs
Engine Name Continental C90-8
Engine Number 1
Horsepower 90 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 16000 ft
Max Fuel 18 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 87 kts
GPH (75% BHP): 4
MPG (75% BHP) 21.8
Range (75% BHP): 305 nm
Fuel Cost Per Seat Mile 0.14 $
Fuel Cost Per Hour 24 $
MPG per 1000 lbs of Payload 10.22
F-T (Speed^2/FuelBurn) 18.9 HP
F-T Payload 8.9 kts
MPH To HP: 9.7 kts
T/O Roll - T/O over 50 FT OBST 0 ft / 700 ft

SA00002DE Installation of replacement Aft Fuselage Section. Reissued 6/21/1999
SA00029DE Installation of Replacement Fuselage. Reissued 6/21/1999
SA00054DE Installation of replacement wing panel assembly. Issued 10/7/1993
SA00055DE Installation of replacement cabin door. Reissued 6/21/1999
SA00068SE (PAGE 2) Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1) Amended 10/20/2010 0:00
SA00073SE Installation of vortex generators to the wing upper surface at the leading edge. Issued 4/7/1994
SA00079NY Installation of Airwolf remote mounted engine oil filter kit AFC-K008 on single and multi engine fixed wing light aircraft incorporating Teledyne Continental reciprocating engines of 450 horsepower or less. Amended 10/31/2012
SA00081NY Installation of Iceman Aviation Supplies Inc. Carburetor Ice Detector. Amended 5/15/2002
SA00116DE Installation of Replacement Vertical Stabilizer. Reissued 6/21/1999
SA00138BO Wing rib spacing modification. Approval limited to Piper model J3C-65 serial number 15327 ONLY. Issued 10/3/2001
SA00148BO Wing rib spacing modification per Scootair Modification to Clipped Wing Piper J3C-65 for Fuel Tank Installation Instructions of 11/10/01. Issued 5/29/2002
SA00207AT Installation of carbon steel brake discs that have melonite surface treatment P/N AA-67. Reissued 11/14/1994
SA00243BO (4 OF 5) Installation of Centurion Consulting Inc. GPS Steering Assist Module (SAM) with roll steering (p/n 0025-5100) or without roll steering (p/n 0025-5200). Amended 7/21/2011
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. Issued 10/29/2009
SA00276LA Modify the auxiliary fuel system by rerouting the fuel transfer line. (S/N 17422) Issued 11/7/1996
SA00343DE Installation of Replacement Fuselage. Reissued 6/21/1999
SA00402SE Installation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed) Amended 1/23/2007
SA00478CH (PAGE 2) Installation of Cooper Superflite 102 Fabric. Amended 5/10/2012
SA00680SE (5 OF 6 Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.  Reissued 7/8/2005
SA00715CH Installation of Air Energy Service P/N J-3-212 ball type sight fuel tank quantity gauge on the side of an AESI P/N AESI-125 12-gallon wing tank. Amended 6/9/2010
SA00780SE (PAGE 1) Installation of the True Lock Safety Retention Axle Lock Nut System in accordance with AML No. SA00780SE dated February 1 2001 or later FAA approved revision. Amended 5/11/2010
SA00932SE Installation of the Stewart wing tip assembly in accordance with Stewart Wing Tip Assembly Master Drawing List SWT 3001 dated April 8 2001 or later FAA approved revision. Amended 1/25/2002
SA01015SE Installation of eligible Alaska Tire and Rubber Company TSO-C62d Tires as listed in Approved Model List SA01015SE dated November 7 2001 or later FAA approved revision. Amended 10/4/2012
SA01026SE (PAGE 1) Improved fuel gascolator assembly. Amended 12/19/2012
SA01233SE Manufacture of Alaskan Bushwheel Inc. (ABI) tail wheel and fork assembly per ABI Document ABI-3200B Revision A dated April 28 2005 or later FAA approved revision.  Amended 5/22/2012
SA01240SE (4 OF 5) Installation of secondary voltage indication system Reissued 4/3/2006 0:00
SA01251SE The manufacture of a Sunvisor System. Amended 2/28/2012
SA01516SE Replacement of the Scott Master Brake Cylinder (Non-Vented Diamphram type) with a Steve Amended 7/16/2007
SA01669CH Installation of Challenger Reusable Air Filter Amended 6/21/2012
SA01704LA Installation of the Grove Disk Brake System Issued 12/21/2004
SA01734SE (PG 1) Application of Stewart Systems synthetic fabric covering system to aircraft fuselage wings tail surfaces control surfaces and related parts. Amended 3/23/2011
SA01734SE (PG 3) Application of Stewart Systems synthetic fabric covering system to aircraft fuselage wings tail surfaces control surfaces and related parts. Amended 3/23/2011
SA01765SE Installation of Alaskan Bushwheel Inc (ABI) TSO-C26d wheels Part Number (P/N) ABI-1010. Amended 10/11/2012
SA01944CH (2 OF 2) 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. Issued 3/5/2004 0:00
SA02002SE Installation of vortex generators on the above model aircraft Issued 5/22/2009
SA02007AK Installation of main landing gear long step no. 3195. Amended 5/23/2006
SA02033AT (PAGE 3) Modification to install an air-oil separator to prevent oil from being aspirated from the engine breather line (47J series w stc s SH4-235SW SH4-826SW or SH479SW) Amended 7/25/2008
SA02043AK Fabrication and installation of pilot s seat belt attachment brackets. Issued 12/13/1995
SA02093AK Installation of hourmeter airspeed switch. Issued 10/17/1997
SA02128LA Installation of aileron and flap hinge repair bushings Amended 6/10/2009
SA02153AK Installation of Burl s Aircraft Rebuild Magnum I tail wheel penetration tail ski per Burl s Aircraft Rebuild LLC Master Data List No. MDL-3234-1 latest FAA approved revision. Issued 12/22/1999
SA02171AK Installation of a 24-gallon right wing fuel tank P/N DC18049-24G-25R and 24-gallon left wing fuel tank P/N DC10849-24G-32L. Amended 1/8/2008
SA02212AK (PG 3) Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems. Amended 5/4/2011
SA02233AK Installation of high visibility fuel sight gauge. Reissued 10/28/2010
SA02234AK Installation of a high Pressure Brake Master Cylinder assembly DCA1248-1260. Issued 1/13/2005
SA02236AK Fabrication and installation of F. Atlee Dodge Heavy Duty Standard Length Main Landing Gear P/N 3225A in accordance with F. Atlee Dodge Master Data List No. 3225-1.5 Revision: None dated March 14 2005 or later FAA approved revisions. );INSERT INTO stc_table VALUES (  Issued 3/29/2005
SA02268CH (PAGE 5) Installation of Airwolf Filter Corp. Air Oil Separator Amended 8/28/2011
SA02283SE Page 1 Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P Reissued 8/27/2013
SA02295AK Installation of a high capacity fule gascolator assembly. Issued 8/21/2007
SA02299AK Installation of a replacement fuel selector valve. Issued 9/13/2007
SA02309AK Installation of a stabilizer trim system Issued 4/17/2008
SA02316AK Installation of 8.50-6 and 8.50-10 tires Issued 9/5/2008
SA02387CH Installation of Piper Part Number 12649-00 Stabilizer and Piper Part Number 12647-00 Elevators in lieu of original components. Issued 4/5/2007
SA02520AT Installation of M-20 Oil Separator model 600-WP. Issued 5/30/2002
SA02566CH Installation of the Custom Fiberglass Molding Inc. (CFMI) Model 1500 Aircraft Main Landing Gear Skis. Amended 3/6/2009
SA02604CH Installation of a battery powered engine starting system. Issued 7/24/2008
SA02987CH Installation of the Electroair Electronic Ignition System Amended 7/23/2013
SA03112AT Installation of Gomolzig Quietflight low noise silencer P/N PA-18-606500. Issued 5/26/2005
SA09470SC Installation of Starter Indicator light system. Issued 6/18/2001
SA1-423 Sensenich M74CK-2 fixed pitch metal propeller. Issued 
SA1-497 Franklin 4AC-176-F3 engine. Amended 
SA1-510 Installation of Sur-Vent fuel tank filler cap manufactured. Reissued 5/11/1994
SA10077SC Installation of push-button starter system. Amended 4/26/2005
SA1008WE Installation of Poly-Fiber covering material. Reissued 5/27/2003
SA1011NW Installation of a 18 gallon right hand wing auxiliary fuel tank Issued 9/16/1980
SA1038SO Installation of Aqua Model 1500 floats. Amended 3/21/1994
SA1066GL Modified fuel and exhaust system. Reissued 10/1/1986
SA107RM Install Continental O-200-A engine and McCauley 1A101/DCM or Univair aeromatic F200/00-73E propeller with 18-gallon wing fuel tank. (J3C-65 with Reed Wing Conversion) Issued 7/26/1977
SA10921SC Installation of an alternator and regulator as a replacement to existing OEM generators and mechanical voltage regulators Issued 11/10/2008
SA111AL Conversion of 4-inch wheels and brakes to 6-inch wheels and brakes. Amended 8/19/1970
SA1175NW Installation of a 13 gallon left hand auxilliary fuel tank Issued 9/13/1978
SA11RM Installation of modified axles wheels and brakes Amended 7/13/1999
SA1237NW Installation of two PA-18 17 gallon wing fuel tanks one header tank Issued 5/21/1981
SA1249GL Installation of Ceconite 102 fabric. Approved for installation on Piper J3C-65 serial number 16217. Reissued 7/11/2002
SA1251NW Installation of Cleveland wheels and brakes Goodyear tires/tubes Univair front lift struts top fuselage plexiglass window L.H. fuselage tube frame window and L.H. wing auxiliary (transfer) fuel tank Issued 6/3/1981
SA1251WE Belt-driven 35A or 55A alternator on Continental A-65-8 engines. Issued 1/1/1960
SA126SO Installation of wing fabric attachment clips. Reissued 6/3/1991
SA1350WE Replace existing fabric on wings fuselage empennage and/or control surfaces with fiberglass cloth. Reissued 3/6/1969
SA1351WE (PG 1) Replace existing fabric on wings fuselage empennage and/or control surfaces with Ceconite101 material. (262A Series -12) Amended 8/19/1983
SA144AL Remote compass bracket. Issued 1/1/1960
SA1455NM Installation of a flame proof auxiliary heater-dryer Model12-1600. Amended 12/11/1985
SA1486GL Fabricate and install engine mount to accept Continental Aircraft engine C-85-12 rated at 85 H.P. at 2575 RPM. Reissued 10/23/2004
SA1487GL Fabricate and install engine mount to accept Continental Aircraft engine O-200 rated at 100 H.P. at 2750 RPM. Reissued 10/23/2004
SA1496GL Installation of a 12-gallon fuel tank and fuel system in the left wing or left and right wings. Amended 6/9/2010
SA1516NM Installation of stamped aluminum wing ribs. Issued 10/25/1982
SA1541NM Installation of cabane vee. Reissued 1/29/1999
SA1545NM Installation of hydra strut. Reissued 1/29/1999
SA1581GL Install shoulder harness and seat belt assembly. Issued 4/3/1991
SA158GL Installation of engine fiberglass cowling. Issued 3/10/1977
SA1626NM Page 2 Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) Amended 3/9/1993
SA1678GL Surrendered and incorporated into STC SA241CH. Surrendered 6/14/2002
SA1763SO Installation of Lycoming O-235-L2C engine derated and McCauley 1A103/ TCM6958 propeller. Reissued 2/14/1997
SA1765GL Fabricate and install engine mount to accept Continental Aircraft C90 and O-200 engines. Reissued 10/23/2004
SA1777NM Installation of nitrate and butyrate dope over the stits polyfiber cover Issued 2/10/1983
SA187AL Install Continental C-90 and PA-18-95 cowl and baffles. Issued 1/1/1960
SA196GL Replacement of main wheels and brakes with Gerdes Products wheel A-1780 and A-1870-4 brake. Issued 10/27/1977
SA2040AK Installation of vented fuel cap assembly (P/N 3267). Issued 9/7/1995
SA2057SO Installation of shoulder harness. Issued 2/3/1987
SA2080CE Operation of airplane on unleaded automotive gasoline 87 minimum antiknock index and leaded automotive gasoline 88 minimum antiknock index (RON+MON)/2. Intermixing with aviation gasoline also approved. Amended 6/23/1992
SA2127WE Installation of Madras Air Service Model 104 wing tips. Amended 2/4/1982
SA214AL Install L1650A and L-2000A wheel replacement skis. Issued 1/1/1960
SA2190NM Page 1 Installation of electronics International Digital Volt/Amp Gauges and Accessories. Issued 2/16/1984
SA220SO Tow bar release mechanism and safety tow link. Reissued 10/3/2011
SA2306NM Installation of hydraulic ski- brake assembly. Issued 5/22/1984
SA2346NM Installation of landing gear fueling step. Issued 9/16/1986
SA2350NM Page 1 Installation of Electronics International Inc digital carburetor/outside air temperature gauges Amended 6/6/1990
SA241CH Install Ceconite 101 fabric. Amended 7/11/2006
SA2508SO Replacement of Cleveland brake discs No. 164-67 or 164-167 with Appalachian Accessories stainless steel brake discs Part No. 73-67. Reissued 9/29/1995
SA252CH Installation of replacement wing ribs. Issued 9/1/1994
SA254CE Model A fiberglass floats. Issued 1/1/1960
SA262AL Install 6x6x44 fish pole tube. Issued 1/1/1960
SA2666WE Ceconite 102 material covering complete aircraft. (262A SERIES -12) Amended 8/19/1983
SA2844CE (1 OF 2) Installation of a plastic cap enclosure over the anti-collision strobe light system. Issued 7/29/1992
SA293AL Installation of Stoddard improved brake system. Reissued 7/9/1981
SA2NE Installation of Cleveland wheels and brakes 7.00-6 or 6.00-6 C38500-HA 40-6 in accordance with S.V. Scherbon modifications 3/6/73 on several models of Piper aircraft. Issued 4/5/1973
SA3-111 Wing modification. Issued 1/1/1960
SA3-202 Fabrication and installation of wing splate. Issued 1/1/1960
SA3-35 Beech controllable propeller R003-100 hub with R003-232-72T blades in airplanes with Conti- nental C85 engines. Issued 1/1/1960
SA3-356 Installation of Wipaire Skis Model C-2200 main ski and Model AWT-2500 or AWT-2500A tail wheel skis. Reissued 2/16/1993
SA3-357 Installation of Wipaire Skis Model C-2200 main skis and Model AWT-2500 or AWT-2500A tail wheel ski. Reissued 2/16/1993
SA3-424 Installation of Wiparie Skis Model CTF-2200 (Acft Skis) (FluiDyne) (Federal) tail ski on airplanes equipped with Scott Model 3000 tail wheel. Reissued 2/16/1993
SA3-47 Extra 17-gallon right wing fuel tank. Issued 1/1/1960
SA3-514 Modification to exhaust and carburetor air preheater muff systems and installation of exhaust stack shields on cowling. Issued 1/1/1960
SA302AL Installation of AD 2500x10.5 wheel replacement skis and rigging. Amended 1/30/1970
SA308EA (2 OF 2) Installation of carburetor ice detection system 105AP in single and twin engine aircraft and single engine helicopters powered by Continental Franklin and Lycoming type engines equipped with Marvel-Schebler MA-2 MA-3 MA-4 MA-4-5 MA-6 and HA-6 series carburetors. (Normal Utility and Acrobatic Category airplanes and helicopters equipped with engines and carburetors as described.) Amended 11/20/1978 0:00
SA3220SO Installation of basic type BPE-14 Model No. 1008 air driven alternator. Issued 6/25/1992
SA322CE Manufacture hitch and bracket. Install tow hitch. Amended 5/6/1971
SA323CE Manufacture hitch and bracket. Install tow hitch. Amended 5/6/1971
SA3284WE Installation of Geroge M. Adams DGA-2000 or Bodell BMI-2000 wheels and Bodell BMI-252 brakes. Amended 12/27/1978
SA3310NM Installation of Teledyne-Continental Model O-200 engine Issued 12/31/1985
SA333CE Omni view window. Issued 1/1/1960
SA338CE Continental C-90-12-F engine. Issued 1/1/1960
SA357CE Model B fiberglass floats. Issued 1/1/1960
SA35AL Installation of PA-18 flaps. Reissued 7/9/1981
SA3623NM Application of polyurethane finishing system. Issued 7/15/1987
SA36CH Installation of Baumann Model 1420 floats. Reissued 4/29/2005
SA3862NM Page 1 Installation of Electronics International Primary TIT/EGT/CHT instruments remote switches and associated accessories. Amended 4/25/1988
SA3AL Installation of Fred A. Shaw tundra-bird Model 2500 skis. Reissued 9/11/2009
SA4-1210 Installation of Eonnex cover on aircraft surfaces. Reissued 8/19/1980
SA4-469 Application of glass cloth with resin. Issued 1/1/1960
SA4-479 Application of glass cloth with resin. Issued 1/1/1960
SA4-813 Removal of original 12 gallon fuel tank and related parts from fuselage. Limited to installation on serial number 19952 ONLY. Issued 4/30/1959
SA4-840 Fabric replaced with glass cloth on wings fuselage empennage and/or control surfaces. Issued 1/1/1960
SA4-907 Ceconite 101 covering of wings fuselage ailerons elevator rudder and horizontal and vertical stabilizer. Issued 1/1/1960
SA4-977 Installation of Fiberglass rudder post mount for either Grimes or Whelen WRM rotating beacons. Amended 10/6/2005
SA4005NM (PG 4) Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) Amended 12/18/2007
SA4302NM (PAGE 2) Installation of Electronics Int l digital automatic engine analyzer. Amended 10/13/1989
SA455AL Installation of PA-18 fuel system. Issued 11/19/1971
SA456AL Installation of PA-18 wing lift struts. Issued 11/22/1971
SA457AL Forward fuselage structural changes to PA-11 configuration. Approval is limited to those Piper J3C-65 and J3C-65S aircraft which have FAA approved PA-18 fuel system installed. Issued 11/22/1971
SA458AL Installation of PA-18 horizontal stabilizer trim system. Issued 11/23/1971
SA459AL Installation of PA-18 baggage compartment. Approval is limited to those Piper J3C-65 and -65S aircraft which have FAA approved PA-18 elevator control system installed. Issued 11/23/1971
SA4609NM Installation of main landing gear safety cable kit. Issued 5/2/1989
SA460AL Installation of PA-18 pilot-static system. Issued 11/24/1971
SA460SW Install wing tips in accordance with Cub Crafters Inc. Master Drawing List. MDL102400 Revision C dated May 30 2001 or later FAA approved revision. Reissued 1/26/2012
SA4615NM Fabrication and installation of welded steel universal aft fuselage float strut attachment fittings. Reissued 8/21/2007
SA461AL Installation of PA-18 landing gear cabane. Issued 11/24/1971
SA4629NM Fabrication of Model 8400 brake booster assemblies and modification of Scott Aviation Model B-711 brake master cylinders by installation of said assemblies. Reissued 1/26/2006
SA462AL Installation of PA-18 front seat. Issued 11/24/1971
SA463AL Installation of PA-18 elevator control system. Issued 11/24/1971
SA464AL Installation of PA-18 rear seat. Approval limited to those Piper J3C-65 and J3C-65S aircraft which have FAA approved PA-18. Issued 12/1/1971
SA465AL Installation of PA-18 boot cowl and windshield. Issued 12/15/1971
SA482NW Installation of a Piper PA-18 Top Deck Assembly Issued 7/14/1977
SA489EA Installation of ARP Inc. carburetor ice detection system Models 107AP (-12 -R-12 -24 and -R-24 series) in single and twin engine aircraft and single engine helicopters powered by Continental Franklin and Lycoming type engines equipped with Precision A ir-Motive (Facet or Marvel-Schebler) MA-2 MA-3 MA-3SPA MA-4 MA-4-5 MA-4SPA MA-5 MA-6 MA-6AA and HA-6 series carburetors. Amended 12/5/2002
SA5-13 Installation of 8.50x6 tires and tubes with Hayes 6-inch wheels. Reissued 9/11/2009
SA5-33 Removed unbalanced tail surfaces and installed balanced tail surfaces. Install elevators Piper 12789-00 and 12789-01 and stabilizers Piper 12790-00 and12790-01. Reissued 6/12/1997
SA5-39 Large horizontal stabilizers and elevators. Issued 1/1/1960
SA5-65 25x11x4 tires on Goodrich 4-inch wheels 841696 using rim adapter A-1. Reissued 3/31/2004
SA5-9 25x11x4 tires and tubes with Airglass Engineering Company adapters LWA 950. Issued 1/1/1960
SA501AL Installation of fiberglass wing tips. Reissued 9/11/2009
SA507AL Installation of alternate crankcase breather. Reissued 7/9/1981
SA5159NM (1 OF 2) Installation of chip detector system. Amended 11/6/1992
SA525CE Concurrently incorporate the following items of Aircraft Specifications No. A-691 625-clipped wing installation except operating limitations are not changed 617-wing tip spill plates (optional) 311(c)(9) - Continental C85-8 or -12 engine C85-8 or -12 engine. Reissued 6/2/2000
SA560GL Installation of Aero Fabricators 8-gallon or 12-gallon wing auxiliary fuel tanks. Issued 9/24/1981
SA573NW Installation of a Continental O-200-A engine Sensenich M69CK/6952 propeller PA-11 engine mount and cowling PA-11 windshield PA-18 flaps PA-18 balanced horizontal tail surfaces wing leading edge cuff modification kit and PA-18 fuel system Issued 3/10/1978
SA573SW Installation of Plane Booster wing tip kit 101-250. Reissued 1/28/1996
SA5755NM Installation of a propeller anti theft device. Issued 8/5/1992
SA588NW Installation of a Continental O-200A engine Issued 5/17/1978
SA593CH (3 OF 5) Install Champion SlickSTART magneto booster system. Reissued 2/10/2009 0:00
SA5949NM Installation of vorex generators on wing upper leading edge and on lower trailing edge of fixed surface of horizontal tail. Issued 4/29/1993
SA615EA (PAGE 2) Installation of Whelen Anti-Collision Strobe Light Systems Part Number 01-0770006-( ) 01-0770028-( ) 01-0770029-( ) 01-0770062-( ) 01-0770900-( ) and 01-0771055-( ) as replacement for originally installed anti-collision lights. Reissued 7/6/2010
SA683SW Convert from monoplane to biplane configuration by adding all metal lower wings. Reissued 10/20/1994
SA68AL Fabrication and installation of Stoddard Model 3 wing tank per Stoddard Aero Service Drawing List No. 68 dated February 7 1975 or later Federal Aviation Administration approved revision. Reissued 1/26/2012
SA69NW Installation of Matney s engine charge air-air filter assembly. (AA-1B AA-1 AA-1A 1969 AND ON) (AA-5 1972 1973 AND 1974 ONLY) Amended 10/8/1974
SA710NW Installation of a Lycoming O-235-C1 engine Sensenich M76AM-2 propeller PA-18 fuel system and modified exhause and heater muff system Issued 1/17/1979
SA71GL Installation of air filters Reissued 6/20/2000
SA736GL Superseded by STC SA01944CH. Modify airplane to fly on unleaded automotive gasoline 87 minimum antiknock index. Surrendered 3/5/2004
SA737NW Installation of Continental engine Sensenich propeller and Edo floats Issued 4/9/1979
SA7435SW Install Teledyne O-200A engine and McCauley 1A101-DCM propeller. Amended 6/19/2003
SA744NW Installation of a Piper PA-11 cowl and a fuel level sight gauge Issued 4/27/1979
SA7965SW Application of fabric and polyurethane finishing system. Amended 7/15/1994
SA800EA (PAGE 2) Installation of Aviation White Anti-Collision Strobe Lights. Whelen Models A429 A430 A434 A450 A408 (white) A408R/W or A47OR/W (red/white) A500 A625 or A650 and associated power supplies or Model SA strobe light system. Amended 7/6/2010
SA8075SW (PAGE 3) Installation of fiberglass covering. (M-62 SERIES PT-19) (G-73 SCHWEIZER) Reissued 11/10/2003 0:00
SA811SW Clip wings and install Continental A-75-8 engine. Issued 1/1/1960
SA820CE Install Aero Model M1500 M1800 or M2000 main skis. Reissued 12/12/2003
SA835CE Installation of wing tip splates. Issued 8/1/1972
SA842GL Incorporated into STC SA00478CH. Surrendered 6/14/2002
SA916NW Installation of a Continental O-200-A engine a McCauley 1S90/CF 7144 propeller two 13 gallon wing tanks and associated systems Issued 4/14/1980
SA923GL Installation of Ceconite 102 fabric. Limited for installation in Piper model J3C-65 serial number 20728. Reissued 7/11/2002
SA95AL Maule SFS-1-4-P8 tail wheel Hayes D-15-26 brake assembly using Kennedy Air Service adapter 64-1 Hayes wheel assembly D3-105MD and800x6 850x6 or 900x6 4-ply tires and tubes. Issued 1/1/1960
SA98CH Installation of replacement wing ribs. Amended 1/13/1997
SA99AL Installation of six-inch wheels and brakes. Reissued 7/9/1981
Fusulage Construction
Airframe Material
Number of Doors
Wing Location
Wing Construction
Wing Rib Material
Wing Skin Material
Aileron Type
Aileron Trim
Aileron Control System
Flap Type
Wing Flap Actuation
Empennage Type
Empennage Rib Material
Empennage Skin Material
Rudder Trim
Yaw Trim Actuator
Yaw Control System
Pitch Trim
Pitch Control System
Pitch Trim Actuator
Landing Gear
Landing Gear Type
Retraction System
Emergency Extension
Ground Steering
Shock Absorbtion Main Gear
Shock Absorbtion Other Gear
Brake Type
Brake Controls
Instrument Panel
Flight Control
Number of Seats
Window Defrost
Normal Climb Profile Speed (KIAS)
Maximum Climb Profile Speed (KIAS)
Number of Engines
Engine Manufacturer
Engine Model
Engine Type
Fuel/Air Mechanism
Number of Cylinders
Max HP
Starter System
Propeller Manufacturer
Propeller Model
Number of Blades
Minimum Diameter
Maximum Diameter
Propeller Type
Propeller Governor
Fuel System
Fuel System Type
Approved Fuel Type 1
Approved Fuel Type 2
Approved Fuel Type 3
Fuel Capacity (G)
Tank Type 1 Location
Tank Type 1 Capacity (G)
Tank Type 2 Location
Tank Type 2 Capacity (G)
Usable Fuel (G)
Oil Capacity (Quarts)
Electrical System
Power Source
Power Storage
System Voltage
Alternator Amp
Battery Voltage
Battery Amp/Hour
Maximum T/O Weight (lbs)
Maximum LDG Weight (lbs)
Standard Empty Weight (lbs)
Useful Load (lbs) 0
Station 1 Baggage Location
Max Weight Station 1 (lbs)
Station 2 Baggage Location
Max Weight Station 2(lbs)
Station 3 Baggage Location
Max Weight Station 3(lbs)
Wing Loading (lbs/sq.ft)
Vne (KCAS)
Vno (KCAS)
Va(Max Gross) (KCAS)


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