PA-20 125,135

Number of Active Aircraft: 882 Active- Map

Description:

The addition of the nosewheel christened the PA22 Tri Pacer, with its tricycle landing gear. The “trike” made it easier for new pilots to learn to fly. The “Spud” as it was also known, had many different engine options, the most powerful being the 160 HP. Its production run continued from 1950 to 1964. Over 9000 were built.

The Tri-Pacer featured the “Auto-Control” which relied on the Tri-Pacers bungee linkage of ailerons and rudders that were meant to simplify coordination.

Other varient's sported different engine sizes including the 108 hp 0-235 to the 160 o-320. The 108 hp version was designed as a stripped down version of the Tri-Pacer, only including two seats and one fuel tank. It was named the Colt. It had a lower sticker price which was marketed primarily for training.

823
Fuel Cost ($):
General Stats:
Seat Capacity: 4
Empty Weight: 1020 lbs
Max Weight 1950 lbs
Useful Load: 930 lbs
Engine Name Lycoming O-290-D2
Engine Number 1
Horsepower 135 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 15000 ft
Max Fuel 36 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 108 kts
GPH (75% BHP): 6.1
MPG (75% BHP) 17.7
Range (75% BHP): 548 nm
Fuel Cost Per Seat Mile 0.08 $
Fuel Cost Per Hour 36.6 $
MPG per 1000 lbs of Payload 16.47
F-T (Speed^2/FuelBurn) 19.1 HP
F-T Payload 17.8 kts
MPH To HP: 8 kts
T/O Roll - T/O over 50 FT OBST 0 ft / 1600 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
SA00097SE Installation of a vortex generator kit. Reissued 8/20/2004
SA00207AT Installation of carbon steel brake discs that have melonite surface treatment P/N AA-67. Reissued 11/14/1994
SA00215NY Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system. Amended 8/14/1995
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
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
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
SA01063CH Installation of a Scott Model 3200 Tail Wheel with the AESI #T.S.05P Tail Spring. Reissued 2/16/2006
SA01085LA (PAGE 1) Installation of the VNS 1000 Voice Navigation System. Reissued 4/26/2010 0:00
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
SA01330LA (PAGE 2) Installation of alternate avionics support assembly. Reissued 10/6/2010 0:00
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
SA01669CH Installation of Challenger Reusable Air Filter Amended 6/21/2012
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
SA01704LA Installation of the Grove Disk Brake System Issued 12/21/2004
SA01715SE ONE-ONLY STC: Replacement of existing Control wheels on Piper PA-20 serial number 20-279 with PA-16 Type Conttrol Stick configuration. Issued 11/7/2006
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
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
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
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
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
SA03148NY ( PAGE 1 OF 2) The installation of the Latitude Technologies Corporation S100 Tracking System Issued 9/26/2012
SA09470SC Installation of Starter Indicator light system. Issued 6/18/2001
SA1-157 McCauley fixed pitch MET-L-PROP1A170/GM7450 with Lycoming O-290-D engine. Reissued 8/15/2006
SA1-167 Lycoming O-320 150 hp engine Sensenich M-74DM propeller Piper PA-22-150 engine baffles and and Harrison AP13SJ03-01 oil cooler. Reissued 2/10/2006
SA1-24 McCauley fixed pitch MET-L-PROP Models 1A170/GM7455 and 1A170/ GM7453 with Lycoming O-290-D2 engine. Reissued 8/15/2006
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
SA1-492 Metallizing of wing panel excluding aileron and flap. Amended 
SA1-510 Installation of Sur-Vent fuel tank filler cap manufactured. Reissued 5/11/1994
SA1-89 McCauley fixed pitch MET-L-PROP1A170/GM7452 and 1A170/GM7454 in aircraft with Lycoming O-290-D engines. Reissued 8/15/2006
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
SA10236SC (3 OF 4) Installation of a GDC 31 Roll Steering Converter  Amended 3/22/2011
SA1067GL Surrendered and incorporated into STC SA00478CH. Surrendered 6/14/2002
SA10682SC Installation of alternator and voltage regulator Reissued 11/16/2007
SA10822SC Installation of EFD1000 Primary Flight Display Amended 9/29/2009
SA118GL Installation of Huron Aviation Products alternator P/N 10346 and regulator P/N 10316. Amended 3/23/1978
SA11RM Installation of modified axles wheels and brakes Amended 7/13/1999
SA1255NW Installation of a Lycoming IO-360-B1B engine Hartzell HC-C2YK-1BF/F7666A-2 propeller and associated systems Issued 6/11/1981
SA125AL Installation of squared off wing tips and end plates. Amended 12/1/1965
SA126SO Installation of wing fabric attachment clips. Reissued 6/3/1991
SA12AL Fabrication and installation of Stoddard Aero Service 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
SA12RM Installation of Light Plane Components landing gear vee assembly. Amended 6/5/1997
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
SA1416NM Installation of a right front spar splice Station 85 to 99 Issued 12/28/1981
SA144AL Remote compass bracket. Issued 1/1/1960
SA1455NM Installation of a flame proof auxiliary heater-dryer Model12-1600. Amended 12/11/1985
SA1487WE Installation of Brittain Industries Inc. Model B2C Flight Control System Reissued 1/30/2013
SA1494GL Install shoulder harness and seat belt assembly. Issued 6/28/1990
SA1512WE (2 OF 2) Installation of exhaust gas temperature monitoring systems Model EGT-1. Amended 2/22/2007 0:00
SA1523NM Installation of stamped aluminum wing ribs. Issued 10/25/1982
SA1558NM Installation of Jensen Aircraft fuel valve plug No. 011-1. Reissued 1/29/1999
SA1586NM 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
SA1905NM Installation of Schneider wheel skis 60-inch to 10-inch aluminum wheel adapters and 29x11.0-10 8-ply minimum tires on main landing gear. Issued 1/20/1983
SA2012CE Operation of airplane on unleaded automotive gasoline 87 minimum antiknock index and leaded automatic gasoline 88 minimum antiknock index (RON + MON)/2. Intermixing with aviation gasoline also approved. Amended 6/23/1992
SA2040AK Installation of vented fuel cap assembly (P/N 3267). Issued 9/7/1995
SA211WE Removal of left-hand cabin door for parachute jumping and aerial photography operations. Issued 1/1/1960
SA2127WE Installation of Madras Air Service Model 104 wing tips. Amended 2/4/1982
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
SA224GL Install Gerdes control wheels Model No. A-1561-C and A-1562-C utilizing AN3-12 bolts (2) AN3-65 self-locking nuts (2) and AC-940-316 washers(2). Issued 2/15/1978
SA22RM Manufacture of exact replacement parts front and rear lift strut assembly. Reissued 7/11/1981
SA2350NM Page 1 Installation of Electronics International Inc digital carburetor/outside air temperature gauges Amended 6/6/1990
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
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
SA25EA Conversion of aircraft for parachute jumping and aerial photography. Reissued 9/7/1976
SA2605CE Operation of airplane on leaded and unleaded automotive gasoline 91 minimum antiknock index(RON+MON)/2 per ASTM Specification D-439. Inter-mixing with aviation gasoline also approved. Issued 4/6/1990
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
SA278WE Autopilot. Reissued 10/1/1973
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
SA3-423 Installation of CT-3000 tail ski on airplanes equipped with Scott 3200 or 3400 tail wheels. Amended 4/16/2010
SA3-654 Laminated plastic and fiberglass nose. Issued 1/1/1960
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
SA317NE Installation of Auto-Vac-2 manifold vacuum system. Amended 2/2/1990
SA31CE Removal of rear left door and installation of placard. Issued 1/1/1960
SA3217WE Installation of George M. Adams DGA-2000 or Bodell BMI-2000 wheels and Bodell BMI-252 brakes. Reissued 6/25/2003
SA334SW Installation of InterAv Alternator. Reissued 7/20/1981
SA3423 Installation of CT-3000 tail ski on airplanes equipped with Scott 3200 or 3400 tail wheels. Amended 11/18/2009
SA3518NM Installation of a skylight in accordance with Steve Amended 4/1/2008
SA351NE 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
SA3607NM Installation of landing gear fueling step. Issued 9/18/1986
SA3609NM Installation of Schneider Wheel SKis Inc. SWS-11000 tundra tires wheels and hubs. Issued 10/3/1986
SA3627NM Application of polyurethane finishing system. Issued 7/15/1987
SA384AL Installation of rudder centering device in lieu of ventral fin. Amended 5/18/2004
SA385AL Installation of rudder centering device in lieu of ventral fin. *This approval includes PA20S models with Lycoming O-320 150 hp engine installed per an appropriate STC. Issued 7/21/1970
SA3862NM Page 1 Installation of Electronics International Primary TIT/EGT/CHT instruments remote switches and associated accessories. Amended 4/25/1988
SA387AL Installation of McCauley1A175GM8241 propeller. *Aircraft must be equipped with Edo 88-1650 floats and modified in accordance with STC SA1-167. Issued 7/23/1970
SA388AL Installation of Edo 88-1650 floats(Spec item 209(a)) when modified per STC SA1-167 and SA387AL. Issued 8/3/1970
SA396GL Installation of Aero Ski wheel replacement skis in accordance with the following: 1) Model M1800 and M2000 skis 2) Model M3000H skis. Issued 4/18/1980
SA4-1210 Installation of Eonnex cover on aircraft surfaces. Reissued 8/19/1980
SA4-564 Eonite covering on wings fuselage and control surfaces. Issued 1/1/1960
SA4-778 Ceconite covering. Issued 1/1/1960
SA4-840 Fabric replaced with glass cloth on wings fuselage empennage and/or control surfaces. 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
SA4008NM Installation of removable panels on the battery box slides. Reissued 9/30/2005
SA401AL Conversion of 4-inch wheels and brakes to 6-inch wheels and brakes. Issued 8/19/1970
SA4172NM Installation of Aviation Development oil filter. Amended 5/22/2009
SA41AL Six inch wheels and brakes. Issued 3/7/1963
SA4302NM (PAGE 2) Installation of Electronics Int l digital automatic engine analyzer. Amended 10/13/1989
SA4635NM Modification of wing lift struts. Issued 2/1/1991
SA479AL Installation of fiberglass wing tips. Reissued 5/7/1979
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
SA5-60 Installation of Russ Simpson sea fins. Issued 1/1/1960
SA5-65 25x11x4 tires on Goodrich 4-inch wheels 841696 using rim adapter A-1. Reissued 3/31/2004
SA509AL Addition of crankcase relief valve. Reissued 7/9/1981
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
SA542AL Installation of leading edge cuff. Amended 3/4/1977
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
SA5924NM Installation of RPM instrument. Amended 11/24/1997
SA5925NM Installation of oil pressure/temperature instrument. Amended 12/8/1997
SA5926NM Installation of manifold pressure instrument. Amended 8/15/1993
SA593CH (3 OF 5) Install Champion SlickSTART magneto booster system. Reissued 2/10/2009 0:00
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
SA626AL Install fiberglass wing tip assembly. Issued 3/21/1978
SA635AL Install Avco Lycoming O-320-A2B engine and Sensenich propeller. Issued 6/6/1978
SA666NW Installation of Teflon control yoke bail or control yoke bushings. Amended 5/15/1996
SA671WE BN-1 propeller spinner. Issued 1/1/1960
SA71GL Installation of air filters Reissued 6/20/2000
SA720AL Installation of Schneider model SWS-4000 main wheel skis and Schneider model SWS-1000 tail wheel skis. Issued 3/25/1982
SA73CE Covering with dacron of wings fuselage tail group flaps all control surfaces or any of these individually. Issued 1/1/1960
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
SA8438SW Installation of dual toe brakes including rudder pedals linkages and torque tubes. Reissued 9/8/2006
SA948GL Superseded by STC SA01944CH. Modify airplane to fly on unleaded automotive gasoline 87 minimum antiknock index. Surrendered 3/5/2004
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
SA99AL Installation of six-inch wheels and brakes. Reissued 7/9/1981
ST01085LA (PAGE 1) Installation of the VNS 1000 Voice Navigation System. Reissued 4/26/2010
ST01494LA (PG 1) Installation of the FiberLite Aircraft Lighting System in accordance with Master Document List listed on Aircraft Model List (AML) Number ST01494LA or later FAA approved revisions. No flight manual is required. Reissued 8/30/2011
ST01700NY (2 OF 2) Installation of the following Aerospace Logic aircraft instruments: EGT-100 Exhaust Gas Temperature Indicator CHT-100 Cylnder Head Temperature INdicator FL-100 Dual Fuel Level Indicator FP-100 Fuel Pressure and Ammeter Indicator OL-100 Oil Pressure and Temperature Indicator and VA-100 Voltmeter and Ammeter Indicator.  Issued 7/8/2003
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)