PA-22 160

Number of Active Aircraft: 597 Active- Map

Description:

Like the other aircraft in the PA 22 line the 160 Horsepower model included a tricycle landing gear. The most powerful of the PA 22 line, the two seat version was certified for utility category.

203
Fuel Cost ($):
General Stats:
Seat Capacity: 4
Empty Weight: 1110 lbs
Max Weight 2000 lbs
Useful Load: 890 lbs
Engine Name Lycoming O-320-B2A
Engine Number 1
Horsepower 160 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 16500 ft
Max Fuel 36 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 113 kts
GPH (75% BHP): 8.3
MPG (75% BHP) 13.6
Range (75% BHP): 406 nm
Fuel Cost Per Seat Mile 0.11 $
Fuel Cost Per Hour 49.8 $
MPG per 1000 lbs of Payload 12.12
F-T (Speed^2/FuelBurn) 15.4 HP
F-T Payload 13.7 kts
MPH To HP: 7.1 kts
T/O Roll - T/O over 50 FT OBST 0 ft / 1480 ft

SA00024NY Installation of Airwolf remote mounted engine oil filter kit AFC-K007 on single or multi-engine fixed wing light aircraft incorporating Lycoming reciprocating engines of 450 horsepower or less. Amended 10/3/2012
SA00061LA Installation of JPI digital tachometer. Amended 1/12/1996
SA00068SE (PAGE 2) Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1) Amended 10/20/2010 0:00
SA00081NY Installation of Iceman Aviation Supplies Inc. Carburetor Ice Detector. Amended 5/15/2002
SA00092SE 30.5 gallon fuel tanks manufactured and installed. Reissued 1/31/1995
SA00097SE Installation of a vortex generator kit. Reissued 8/20/2004
SA00191AT Installation of carbon steel brake discs that have melonite surface treatment. Reissued 11/14/1994
SA00215NY Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system. Amended 8/14/1995
SA00315SE Installation of a Harrison oil cooler Part No 8526250 mounted to the baffling behind cylinder #4 Issued 3/8/1996
SA00393SE Installation of the G/S 2500 and G/S2500R Aircraft Security Alarm System. Issued 12/6/1996
SA00402SE Installation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed) Amended 1/23/2007
SA00428SE Installation of a modified instrument panel Amended 1/2/2008
SA00432SE (PG 4) Installation of EGT 701 series fuel flow instrument. Amended 4/12/2013
SA00478CH (PAGE 2) Installation of Cooper Superflite 102 Fabric. Amended 5/10/2012
SA00633DE Installation of Leading Edge Exhaust System Issued 6/14/2007
SA00678SE Installation of J. P. Instruments 8Jimline EGT-100 series primary instruments Issued 3/5/1999
SA00680SE (5 OF 6 Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.  Reissued 7/8/2005
SA00711DE Installation of an Aero Vision International Inc. Metal Halide High Intensity Discharge (HID) lamp for use in the landing and taxi lighting system. Issued 3/13/2010
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
SA00851SE Installation of Rudder Trim System. Issued 11/10/2000
SA00854SE Removal of upper cross bar from control yoke(s). Issued 11/27/2000
SA00861SE Page 4 Installation of J.P. Instruments (JPI) fuel flow indicating system Amended 4/12/2013
SA00866SE Installation of 8.50x6 8.00x6 or 7.00x6 tires and tubes in matched sets on the main landing gear. The tires used in this modification must be manufactured under a TSO authorization. This modification is valid only as long as the aircraft is modified to a tailwheel landing gear configuration. The operating pressure for the main landing gear tires remains unchanged. Issued 1/9/2001
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
SA00954SE (1 OF 2) Installation of J.P. Instruments (JPI) Primary Temperature Indicating System in accordance with JPI Installation Manual for the EDM 711 Report 106P Revision B dated August 2 2001 or later FAA approved revision. Amended 8/11/2003
SA00954WI Installation of Concorde RG Series Battiers in Piper Single Engine Airplanes. Issued 4/2/2001
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
SA01031SE Data pertaining to this modification are considered inadequate for duplication in other aircraft. This approval for change in type design is limited to Piper Model PA-22-150 serial number 22-7497 only Issued 12/18/2001
SA01085LA (PAGE 1) Installation of the VNS 1000 Voice Navigation System. Reissued 4/26/2010 0:00
SA01100AT Installation of Composite Spinner. Amended 3/31/2004
SA01147WI Installation of Concorde FLA or VRSLA series batteries in Piper Light Airplanes. Reissued 7/30/2012
SA01229SE Page 1 Installation of CNX80 GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Amended 6/27/2007
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
SA01280CH Installation of Challenger Spin-On Oil Filters.(For Cessna 182 model s/n 67042 and up) (For Cessna 421C model s/n 1017 thru 1404) Issued 8/29/2000
SA01330LA (PAGE 2) Installation of alternate avionics support assembly. Reissued 10/6/2010 0:00
SA01365CH Installation of Aero Ski Manufacturing Co. Model T3000 tail ski. Issued 12/20/2000
SA01435SE Installation of J.P. Instruments (JPI) Primary Engine Data Management System Amended 9/17/2013
SA01473SE (4 OF 5) Installation of a GTX 32 (mode C) GTX 33 (mode S) or GTX 33D (mode S with diversity) Remote Transponde Amended 5/21/2008
SA01487SE-D (Page 2) Installation of a GDL 69 or GDL 69A XM Satellite Receiver Amended 5/4/2012
SA01516SE Replacement of the Scott Master Brake Cylinder (Non-Vented Diamphram type) with a Steve Amended 7/16/2007
SA01577SE Data pertaining to this modification are considered inadequate for duplication in other aircraft. This approval for change in type design is limited to Piper Model PA-22-150 serial number 22-5243 only. Issued 7/14/2005
SA01669CH Installation of Challenger Reusable Air Filter Amended 6/21/2012
SA01678SE Installation of a Lycoming O-360-A1P engine with a Hartzell HC-C2YK-1BF/F7666A propeller.  Issued 6/8/2006
SA01692SE (Page 1 OF 2) Installation of a Garmin GMX 200 Multi-Function Display Reissued 10/3/2012
SA01695SE (4 OF 5) Installation of an antenna Amended 2/15/2007
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
SA01770NY Installation of CAM 556-643. Reissued 10/23/2003
SA01800SE (PG 3) Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.  Reissued 12/1/2011
SA01861SE (PAGE 3)  Fabrication and installation of Landing Light Controller Reissued 12/1/2011
SA01863SE Installation of Niagara Oil Cooler in the above model aircraft Amended 1/27/2009
SA01923LA Installation of the P-1000 Digital Electronic Tachometer. Issued 1/23/2007
SA01933LA-D Page 2 Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation );INSERT INTO stc_table VALUES ( System Amended 4/1/2013
SA01933LA (4 OF 5)  Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System Amended 11/6/2006 0:00
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
SA01988SE (PAGE 5) Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.  Issued 4/17/2009 0:00
SA02019SE-D Page 2 Installation of Garmin GTN 6XX/7XX Navigation System Amended 12/19/2012
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
SA02093AK Installation of hourmeter airspeed switch. Issued 10/17/1997
SA02110CH (PAGE 2) Installation of a Time Trac Data Recorder  Reissued 1/11/2010
SA02115AK Fabrication and installation of 30.5 gallon wing fuel tank sight gages. Amended 1/20/2004
SA02119SE Page 2 Installation of Garmin GDL 88 ADS-B UAT Transceiver System Issued 12/28/2012
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
SA02154AK (PAGE 2) Installation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display P/N 430-0270-500. Amended 1/12/2005 0:00
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
SA02217AK (4 OF 5) Installation of Garmin AT Model GDL90 UAT Data Link System in accordance with Garmin AT Inc. GDL 90 UAT Master Data List P/N 560-0278-01 Revision A dated November 12 2004 or later FAA approved revision.  Amended 12/1/2004 0:00
SA02241AK Installation of a Maule Fuel Selector Valve and Associated Fuel System Upgrade in accordance with the Descriptive Data listed in Trimmer Aviation LLC Master Data List MDL-001 dated March 22 2005 or later FAA approved revision. Issued 5/6/2005
SA02246LA Installation of a flap handle extension. Amended 11/16/2010
SA02263AK Fabrication and Installation of a Left Hand Seaplane Door. Issued 3/17/2006
SA02264AK Fabrication and Installation of a Right Hand Seaplane Door. Issued 3/24/2006
SA02268CH (PAGE 4) Installation of Airwolf Filter Corp. Air Oil Separator Amended 8/28/2011
SA02268CH (PAGE 5) Installation of Airwolf Filter Corp. Air Oil Separator Amended 8/28/2011
SA02280AK Installation of a Maule Fuel Selector Valve.  Amended 11/29/2006
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
SA02306AK Installation of a Lycoming O-360-A1A A1D A2A A2D A2E A2F A3A A3D A4A A4M A4N or A4P engine on Piper PA-22 PA-20 and PA-16 airplanes. Issued 3/11/2008
SA02309AK Installation of a stabilizer trim system Issued 4/17/2008
SA02321AK Installation of EDO 89-2000 floats modified Issued 8/29/2008
SA02345AK Installation of Piper PA-18 three-inch extended gear & Maule Oleo Strut Issued 6/30/2009
SA02383AK Installation of offset single handle control yoke (left side left offset and right side right offset) with push-to-talk switch in accordance with Trimmer Aviation LLC Drawing No. 2015101 Rev. A dated May 29 2011 or later FAA approved revision. Issued 6/23/2011
SA02434NY Installation of a Digital Engine Monitoring system. Amended 2/7/2012
SA02532AT Installation of subject Michelin tires on appropriate aircraft. For Michelin 5 6 8 and 10-inch rim diameter tires on General Aviation Aircraft. Issued 6/5/2002
SA02547AT (PG 2) Installation of a Voice Alert System. Amended 8/28/2007 0:00
SA02567CH Installation of Piper Part Number 12769 Stabilizer and Piper Part Number 12770 Elevators in lieu of original components Amended 5/19/2010
SA02670CH Installation of McCauley Propeller model 1A175GM824X Reissued 2/25/2009
SA02672CH Installation of 8:50 tires and tubes in lieu of original components in accordance with installation instructions listed on AML No. SA02672CH. Issued 1/30/2009
SA02717NY Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module Amended 1/9/2012
SA02734CH Installation of Lightweight Battery and Circuit Breaker Master Switch in lieu of original components Issued 6/22/2009
SA02738CH (PAGE 2) Installation of L-3 Communications Avionics Systems Amended 5/7/2010
SA02751CH Installation of McCauley Propeller model 1A200FA824X Amended 6/25/2012
SA02790CH Installation of modified wingtips  Issued 12/16/2009
SA02846CH Installation of MT Propeller model MTV-15-B/210-58 on Piper Aircraft models PA-20 and PA-22  Issued 6/22/2010
SA02858CH Installation of Piper Part Number 21242 and F. Atlee Dodge P/N 3143-12 float fittings in lieu of original components Issued 7/2/2010
SA02865AT Installation of ACS Products Company cockpit control wheels. Limited to installation on PA-22-150 serial number 22-2895 ONLY. Reissued 3/15/2005
SA02898CH Installation of new engine baffling and rear mounted engine oil cooler Issued 11/19/2010
SA02899CH Installation of new lower cowling and carburetor air box  Issued 11/19/2010
SA02929CH Installation of Lycoming O-360 engine in accordance with Installation Instructions Report SA300 dated 7/5/2009. Issued 3/25/2011
SA02934CH Installation of the Custom Fiberglass Molding Inc. (CFMI) Model Alaskan 2500 Main Landing Gear Skis in accordance with Custom Fiberglass Molding Inc. installation design data listed on AML No. SA02934CH or later FAA Approved revision. Issued 3/2/2011
SA02987CH Installation of the Electroair Electronic Ignition System Amended 7/23/2013
SA03113AT Installation of Gomolzig Quietflight low noise silencer P/N PA-22-606500. Issued 5/26/2005
SA03148NY ( PAGE 1 OF 2) The installation of the Latitude Technologies Corporation S100 Tracking System Issued 9/26/2012
SA09150SC Replacement of Piper wheel assembly p/n 451-750 and brake assembly p/n 451-708 with Cleveland wheel assembly pn 40-86 and brake assembly pn 30-55. Reissued 9/8/2006
SA09470SC Installation of Starter Indicator light system. Issued 6/18/2001
SA09745SC Modification of the airframe. Issued 7/17/2000
SA1-108 69A110 gyro stabilizer. Issued 1/1/1961
SA1-128 Dry vacuum pump 113A1 for counter- clockwise engine accessory drive and 113A2 for clockwise drive or 10-113-1 and 10-113-2. Issued 
SA1-22 McCauley fixed pitch propellers1A170/GM7459 and 1A170/GM7457 with Lycoming O-320 engine. Issued 
SA1-22 McCauley fixed pitch propellers1A170/GM7459 and 1A170/GM7457 with Lycoming O-320 engine. Reissued 8/15/2006
SA1-23 McCauley fixed pitch propellers1A170/GM7455 and 1A170/GM7453 with Lycoming O-290-D2 engine. Reissued 8/15/2006
SA1-255 Dart I-M turn control unit. Issued 
SA1-274 Installation of Lycoming O-320(150 hp) series engine and Sensenich M74DM propeller. Reissued 9/7/1976
SA1-275 Lycoming O-320 150 hp engine and Sensenich M74DM propeller Piper PA-22-150 engine baffles Harrison AP13SJ03-01 oil cooler. Reissued 2/10/2006
SA1-282 Replacement of fabric covering with metal skins. Reissued 11/15/2007
SA1-325 Replacement of fabric covering with metal skins ailerons and flaps. Reissued 8/15/2007
SA1-327 Replacement of fabric covering with metal skins. Reissued 8/15/2007
SA1-337 Oil-free vacuum pump PA-201. Issued 
SA1-383 Lube oil filter PB 55-1. Issued 
SA1-386 Installation of heated pitot tube. Installation of heated pitot tube. Public domain. Contact FAA s New York Aircraft Certification Office 10 Fifth Street Third Floor Valley Stream NY 11581-1200 phone 516.256.7500 Amended 10/17/2001
SA1-492 Metallizing of wing panel excluding aileron and flap. Amended 
SA1-510 Installation of Sur-Vent fuel tank filler cap manufactured. Reissued 5/11/1994
SA1-604 Installation of Aerostat external power receptacle. Reissued 10/15/1974
SA1-90 McCauley fixed pitch MET-L-PROP1A170/GM7452 and 1A170/GM7454 in aircraft with Lycoming O-290-D engine. Reissued 8/15/2006
SA1002NW Installation of a pilot s door Issued 8/6/1980
SA1008WE Installation of Poly-Fiber covering material. Reissued 5/27/2003
SA10126SC (2 OF 2) Installation of Aero Advantage ADV200 series vacuum pump per Aero Advantage Drawing Number ADVMSI 500 latest FAA approved revision.  Amended 10/23/2003
SA1015NW Installation of a Lycoming O-360-A3A engine a McCauley 1A200/DFA-8243 (Seaplane) propeller cowling air inlet filter assembly baffling and Edo 248-2440 floats (with aileron/rudder interconnect) Issued 8/15/1980
SA10236SC (3 OF 4) Installation of a GDC 31 Roll Steering Converter  Amended 3/22/2011
SA1027NW Auxiliary fuel tanks. Reissued 2/6/2006
SA1033EA Replace steel oil cooler lines with Aeroquip type 303-8 hose using AN-823-8D elbows AN-816-8D nipples and AN-321-8 hose fittings. Issued 1/29/1976
SA10682SC Installation of alternator and voltage regulator Reissued 11/16/2007
SA1068GL Surrendered and incorporated into STC SA00478CH. Surrendered 6/14/2002
SA10822SC Installation of EFD1000 Primary Flight Display Amended 9/29/2009
SA1177WE WECO carburetor temperature monitor. Issued 1/1/1960
SA1202WE Installation of control position indicator (CPI) system. Reissued 2/18/1972
SA1238NW Installation of a Lycoming engine and Sensenich propeller Issued 5/12/1981
SA124EA Shur-Vent fuel tank filler cap. Issued 1/1/1960
SA1259GL Install Aero Ski Model R2800 retractable skis. Issued 1/11/1988
SA126SO Installation of wing fabric attachment clips. Reissued 6/3/1991
SA1315WE Installation of Mixture Monitor (exhaust gas temperature probe gage and selector) in accordance with Delta Products Part Lists A-192 and A-193 or in accordance with Tri-Star Corporation Mixture Monitor Installation Instructions dated December 9 1981 or later FAA approved revision and/or Drawing List MM-127 dated November 15 1981 or later FAA approved revision in aircraft models listed in Master Eligibility List P-80-A-6 revised March 29 1968 copy attached or later FAA approved revision. Reissued 4/15/2011
SA1351WE (PG 2) Replace existing fabric on wings fuselage empennage and/or control surfaces with Ceconite101 material. (262A Series -12) Amended 8/19/1983 0:00
SA1360CE Chrome-plated brake disc installation. Issued 8/18/1977
SA1418SO Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) Reissued 6/12/1984
SA1426GL Surrendered and incorporated into STC SA241CH. Surrendered 6/14/2002
SA143EA Univair Aeromatic F-200H/0074E propeller on aircraft utilizing Lycoming O-320 or O-320-A1A engine. Issued 1/1/1960
SA144AL Remote compass bracket. Issued 1/1/1960
SA1455NM Installation of a flame proof auxiliary heater-dryer Model12-1600. Amended 12/11/1985
SA145CE APU receptacle under the right front seat to the right of battery box. Issued 1/1/1960
SA1487WE Installation of Brittain Industries Inc. Model B2C Flight Control System Reissued 1/30/2013
SA1493GL Install shoulder harness and seat belt assembly. Amended 7/13/1998
SA1512WE (1 OF 2) Installation of exhaust gas temperature monitoring systems Model EGT-1. Amended 2/22/2007
SA1524NM Installation of stamped aluminum wing ribs. Issued 10/25/1982
SA1557NM Installation of Jensen Aircraft fuel valve plug No. 011-1. Reissued 1/29/1999
SA157CE Jump seat baggage compartments. Issued 1/1/1960
SA1587NM Installation of replacement long-life lift strut. Reissued 1/29/1999
SA1626NM Page 2 Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) Amended 3/9/1993
SA1678NM Installation of replacement wing ribs. Issued 11/18/1982
SA181RM Installation of Lycoming Model O-360-A4A engine and Sensenich Model 76EM8-60 propeller. Reissued 7/11/1981
SA1906NM Installation of Schneider wheel skis 6-inch to 10-inch aluminum wheel adapters and 29x11.0-10 8-ply minimum tires on main landing gear. Issued 1/22/1983
SA191NE Replace original brake discs with discs modified in accordance with Roland Longarzo procedure. Reissued 10/4/1984
SA1949CE 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
SA2-945 Installation of Fiberglass Covering. Reissued 9/10/1963
SA2040AK Installation of vented fuel cap assembly (P/N 3267). Issued 9/7/1995
SA2105WE Installation of Model EGT-3 exhaust gas temperature monitor(with rising temperature alarm). (DC-6B (NAVY R6D-1Z) 680) Issued 2/9/1970
SA2127WE Installation of Madras Air Service Model 104 wing tips. Amended 2/4/1982
SA2137NM Installation of an AVCO Lycoming 0-360-A4A engine and a Sensenich Model 76EMM-60 Issued 8/12/1983
SA2142WE Installation of DASCO Heated Pitot Tube Kit 2022-12. Issued 3/31/1970
SA2167NM Installation of the Precise Flight stand-by vacuum system (SVS). Amended 11/7/2003
SA2190NM Page 1 Installation of electronics International Digital Volt/Amp Gauges and Accessories. Issued 2/16/1984
SA21NW Installation of a 70 pound baggage compartment in either or both EDO 89-2000 89A-2000 or 689-2130 floats Amended 9/25/2009
SA220SO Tow bar release mechanism and safety tow link. Reissued 10/3/2011
SA22RM Manufacture of exact replacement parts front and rear lift strut assembly. Reissued 7/11/1981
SA232GL Installation of Huron Aviation Products alternator P/N 10346 and regulator P/N 10316. Issued 3/23/1978
SA2335SO Installation of Appalachian Accessories P/N 73-5 brake discs. Reissued 9/29/1995
SA2350NM Page 1 Installation of Electronics International Inc digital carburetor/outside air temperature gauges Amended 6/6/1990
SA2355NM Installation of two 30 gallon tanks. Total useable fuel is 58 gallons. (PA-22-160 modified per STC SA 819SW) (PA-22S-160 modified per STC SA 819SW) (PA-22-150 modified per STC SA819SW) Reissued 12/29/2005
SA236NW Installation of a Hartzell HC-C2YL-1B/F7663-4 propeller a Woodward 210452 Governor with a Lycoming drive adapter a Piper PA18-150 muffler and heat muff and a modified firewall Issued 11/7/1975
SA241CH Install Ceconite 101 fabric. Amended 7/11/2006
SA247SO Removal of door during operation of aircraft. Issued 1/1/1960
SA2557NM (1 OF 2) Installation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring system. Amended 2/22/2007
SA2586NM (PAGE 4) Installation of J.P. Instruments temperature monitoring systems. Amended 7/20/2008 0:00
SA2599CE Operation of airplane on unleaded and leaded automotive gasoline 91 minimum antiknock index (RON+MON)/2 per ASTM Specification D-439. Inter-mixing with aviation gasoline also approved. Amended 8/24/2007
SA2687NM (PAGE 1) Installation of Truboplus/ Electronics Int l gauges and switches. Amended 10/25/2000
SA2693NM (PAGE 2) Installation of Electronics International digital volt/amp gauges and accessories. Amended 12/10/2009 0:00
SA26EA Conversion of aircraft for parachute jumping and aerial photography. Reissued 9/7/1976
SA281NW Installation of squared off rectangular wing tips Issued 4/6/1976
SA2844CE (1 OF 2) Installation of a plastic cap enclosure over the anti-collision strobe light system. Issued 7/29/1992
SA2939SO Installation of a PA-22 tricycle gear as modified to a conventional gear PA-20 pacer configuration. The rudder control was modified to accept toe- brake pedals and hydraulic cylinders and a hydraulic parking brake was installed. Amended 4/15/1991
SA297AL Installation of McCauley 1A175 GM8241 propeller. Issued 1/1/1960
SA3-143 Grimes D7080-12 rotating beacon on fuselage access panel. Issued 1/1/1960
SA3-363 Installation of Doyn Fiberglass Wheel Fairings in accordance with Doyn Drawingg No. 1300 and Doyn Process Specification for Fiberglass Parts No. PS-100. Reissued 8/16/2011
SA3-382 Manually operated oil cooler shutter assembly. Issued 1/1/1960
SA3-477 Installation of Model C-2200 main main and AWN1200A nose wheel skis. Reissued 2/16/1993
SA3-494 Installation of Model C2200 main ski and AWN-1200A nose wheel ski. Reissued 2/16/1993
SA3-631 Dacron cover. Issued 1/1/1960
SA3-639 Removal of rear door operation with door removed and reinstal- lation of door. Issued 1/1/1960
SA3-654 Laminated plastic and fiberglass nose. Issued 1/1/1960
SA3-709 Install Piper control modification kit P/N 754-174. Issued 1/1/1960
SA3-77 Vertical fin plates attached to tip ribs of horizontal stabilizer seaplane operation only. Issued 1/1/1960
SA304NW Installation of a PA20 landing gear and removal of rudder/aileron interconnect Issued 6/15/1976
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
SA314SO Installation of Lycoming 0-290-D engine. Reissued 11/8/1984
SA316SO Carburetor ice detector. Amended 10/5/1966
SA317NE Installation of Auto-Vac-2 manifold vacuum system. Amended 2/2/1990
SA3259NM Increase maximum weight to 1736 pounds. Amended 5/16/2003
SA3276NM Replace stabilizer adjustment control pulleys. Issued 8/20/1986
SA334SW Installation of InterAv Alternator. Reissued 7/20/1981
SA3518NM Installation of a skylight in accordance with Steve Amended 4/1/2008
SA3519NM Installation of a skylight Amended 11/21/2000
SA3527NM Increases length of each fuel tank by 9 inches to provide an increase in fuel volume of approximately 6 gallons per wing.  Issued 7/9/1986
SA352NE Airframe modification for installation of modern instrument panel. Reissued 5/27/2003
SA3531NM Installing copper electrical cables. (182 S/N 33000 THRU 33842) (8E 833 and UP) Reissued 9/8/2010
SA356CH Installation of seaplane safety covers. Issued 5/22/1995
SA3608NM Installation of landing gear fueling step. Issued 9/18/1986
SA3610NM Installation of Schneider Wheel Skis Inc. SWS-11000 tundra tires wheels and hubs. Issued 10/6/1986
SA3614NM Installation of PA-14 wings modified lift struts lengthening fuselage install PA-18 empennage and associated control system. Issued 11/19/1986
SA3628NM Application of polyurethane finishing system. Issued 7/15/1987
SA3862NM Page 1 Installation of Electronics International Primary TIT/EGT/CHT instruments remote switches and associated accessories. Amended 4/25/1988
SA388SO Metalize wings wing landing/taxi light installation. Amended 7/2/1970
SA395GL Installation of Aero Ski wheel in accordance with the following: 1) Model M180 and M2000 skis2) Model M3000H skis. Reissued 2/11/2004
SA4-114 Arcon. Issued 1/1/1960
SA4-1210 Installation of Eonnex cover on aircraft surfaces. Reissued 8/19/1980
SA4-1263 Installation of conventional landing gear. (PA-22-160 landplane normal category only) Reissued and Amended 12/4/1979
SA4-1346 Fiberglas covering of airplane surfaces. Issued 1/1/1960
SA4-1502 AB-6564 brake blocks. Issued 1/1/1960
SA4-1587 Retractable wheel fairing on main landing gear. Issued 1/1/1960
SA4-1621 Removal of left-hand door for parachute jumping and aerial photography. Issued 1/1/1960
SA4-222 Fiberglass covering. Issued 1/1/1960
SA4-298 Fuselage structural alterations and additions to provide for the installation of Fairchild Aviation aerial camera A5A or similar. Issued 1/1/1960
SA4-302 Installation of BN-1 propeller spinner. Reissued 10/30/1985
SA4-343 B Arcon. Issued 1/1/1960
SA4-391 Fiberglass wheel fenders. Issued 1/1/1961
SA4-423 Autopilot. Reissued 10/1/1973
SA4-815 Installation of a Lycoming O-320 engine and Sensenich M74DM propeller Reissued 11/19/2012
SA4-840 Fabric replaced with glass cloth on wings fuselage empennage and/or control surfaces. Issued 1/1/1960
SA4-871 Aerofilter 30409A with element 1A0235. Issued 1/1/1960
SA4-903 Ceconite 101 covering of fuselage wings horizontal and vertical stabilizer ailerons flaps rudder and elevator. Issued 1/1/1960
SA4-925 Magnetic flight director 2000. Issued 1/1/1960
SA4-938 Eonite covering on entire aircraft. Issued 1/1/1970
SA4-977 Installation of Fiberglass rudder post mount for either Grimes or Whelen WRM rotating beacons. Amended 10/6/2005
SA4-998 Installation of wheel fairings. Reissued 2/9/1971
SA4005NM (PG 4) Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) Amended 12/18/2007
SA4008NM Installation of removable panels on the battery box slides. Reissued 9/30/2005
SA402NW Installation of a Prestolit Alternator and electrical system Issued 1/31/1977
SA40EA Wet-to-dry vacuum pump conversion kit 300-1. Reissued 4/22/2003
SA4172NM Installation of Aviation Development oil filter. Amended 5/22/2009
SA447WE Torso tank 61900 or 64200. Amended 10/18/1965
SA448CE Prestolite ALK-5000 alternator. Issued 1/1/1960
SA453AL Installation of fiberglass wing tips. Reissued 5/7/1979
SA45RM Conversion from tri-cycle landing gear (nose wheel) to conventional landing gear (tail wheel). (PA-22-160 PA-22-135 PA-22 PA-22-108 PA-22-150 normal category only) Amended 1/24/1994
SA461WE Removal of right-hand door for parachute jumping and aerial photography operations. Issued 1/1/1960
SA4635NM Modification of wing lift struts. Issued 2/1/1991
SA4653NM Fabrication of Model 8400 brake booster assembly and modification of Scott Aviation Model B-711 brake master cylinder by installation of said assembly. (PA-22-108 SN 22-8000 thru 22-9848) Reissued 1/26/2006
SA466NW Conversion of the landing gear Issued 6/15/1977
SA481WE Lycoming O-320-A1A engine and Sensenich M74DM propeller. Issued 1/1/1960
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
SA48AL L1650A or L2000A skis. Issued 1/1/1960
SA4900NM Installation of Cleveland wheels and brakes Issued 2/14/1990
SA4947NM Installation of a Lycoming O-360-A4A engine and Sensenich76EM8-60 propeller. Issued 6/18/1990
SA5-13 Installation of 8.50x6 tires and tubes with Hayes 6-inch wheels. Reissued 9/11/2009
SA5-2 Installation of conventional tail wheel type landing gear from Piper PA-20 in place of tricycle type. Reissued 9/11/2009
SA5-30 Rear door removed. Issued 1/1/1960
SA5-60 Installation of Russ Simpson sea fins. Issued 1/1/1960
SA5096NM Removal of original engine oil cooler and installation of a Piper engine oil cooler. Limited to installation on serial number 2170 ONLY. Issued 6/28/1991
SA5156NM Fabrication and installation of Pulsar-MOSFET Landing Light Flasher System Amended 5/22/2012
SA5156NM (PG 2) Fabrication and installation of Pulsar-MOSFET Landing Light Flasher System Amended 7/29/2010 0:00
SA5159NM (1 OF 2) Installation of chip detector system. Amended 11/6/1992
SA536AL Fabrication and installation of Stoddard Aero Service wing auxiliary fuel tanks per Stoddard Aero Service Drawing List No. 12 dated February 7 1975 or later Federal Aviation Administration approved revision. Stoddard Aero Service Airplane Flight Manual Supplement dated January 29 1969 is required with this installation. Reissued 1/26/2012
SA545AL Installation of leading edge cuff. Reissued 2/20/1976
SA557AL Installation of left hand front door. Reissued 9/11/2009
SA563CH Authorizes installation of engines equipped w/Unison Limited Authority Spark Advance Regulator (LASAR) ignition system w/Cylinder Head Temp. (CHT) monitoring capability on airframes. engines. Reissued 2/10/2009
SA5656NM Installation of burglar alarm system. Reissued 7/21/1993
SA5656NM (PAGE 1) Installation of burglar alarm system. Reissued 7/21/1993
SA573SW Installation of Plane Booster wing tip kit 101-250. Reissued 1/28/1996
SA589WE Full flow oil filter F-94056 and F-94056-12 with element E-3560 MEL 800. Reissued 10/5/1976
SA5924NM Installation of RPM instrument. Amended 11/24/1997
SA5925NM Installation of oil pressure/temperature instrument. Amended 12/8/1997
SA593CH (3 OF 5) Install Champion SlickSTART magneto booster system. Reissued 2/10/2009 0:00
SA60CE Installation of Pee-Kay Model 1800 floats. Reissued 12/23/1980
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
SA625AL Install fiberglass wing tip assembly. Issued 3/27/1978
SA666NW Installation of Teflon control yoke bail or control yoke bushings. Amended 5/15/1996
SA666WE Edo 88-1650 floats with Harrison oil cooler AP13SJ03-01 or AP12CU03-01 bottom engine cowl assembly 13159-8 side engine cowl 14237 reinforced fuselage12480 and Sensenich M74DM or M76AM-2 propellers. Issued 1/1/1960
SA703CE Install aileron and wing fences and booster tips per STC SA573SW. Issued 5/19/1970
SA7086NM Installation of instrument panel. Issued 5/11/1994
SA715NW Installation of wing fabric attachment clips Issued 2/16/1979
SA71GL Installation of air filters Reissued 6/20/2000
SA721AL Installation of Schneider Model SWS-4000 main wheel skis and Schneider Model SWS-1000 tail wheel skis. Issued 3/25/1981
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
SA819SW Installation of extended wings and fuselage drooped wing tips (optional) and modified landing gear or Edo 89-2000 seaplane floats in accordance with Simpson Aviation Company Top Drawing SAC-1000. Amended 11/16/2004
SA8334SW Installation of dual toe brakes including rudder pedals linkages and torque tubes. Reissued 9/8/2006
SA8438SW Installation of dual toe brakes including rudder pedals linkages and torque tubes. Reissued 9/8/2006
SA847EA Installation of Lycoming O-320-A(150 hp) or O-320-B (160 hp) engine. Amended 4/7/1978
SA849GL Superseded by STC SA01944CH. Modify airplane to fly on unleaded automotive gasoline 87 minimum antiknock index. Surrendered 3/5/2004
SA889GL Installation of Ceconite 102 fabric. Limited to installation on Piper PA-22 serial number 22-5692 ONLY. Reissued 7/11/2002
AirFrame
Fusulage Construction
Airframe Material
Number of Doors
Wing
Wing Location
Wing Construction
Wing Rib Material
Wing Skin Material
--Aileron
Aileron Type
Aileron Trim
Aileron Control System
--Flap
Flap Type
Wing Flap Actuation
Empennage
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
Retractable
Retraction System
Emergency Extension
Ground Steering
Shock Absorbtion Main Gear
Shock Absorbtion Other Gear
Brake Type
Brake Controls
Cabin
Instrument Panel
Flight Control
Number of Seats
Heating
Window Defrost
Cooling
Profiles
Normal Climb Profile Speed (KIAS)
Maximum Climb Profile Speed (KIAS)
Engine
Number of Engines
Engine Manufacturer
Engine Model
Engine Type
Geared
Cooled
Fuel/Air Mechanism
Number of Cylinders
Max HP
Starter System
Propeller
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
Limitations
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)