# Piper/Pierce Tony PA-22-150

- Type: Aircraft model (FAA registry)
- Registry code: 7102201
- Manufacturer (registry): PIPER/PIERCE TONY
- Model: PA-22-150
- Aircraft type: Fixed wing single engine
- Category: Airplane
- Engines: 1 · Reciprocating
- Seats: 4
- Weight class: Up to 12,499 lb
- Certification: Type certificated
- Data sheet: [TCDS 1A6](https://openairdocs.org/tcds/1A6) (OpenAirDocs)
- Holder: Piper Aircraft Inc.
- Registered aircraft: 1
- Page: https://openairdocs.org/model/piper-pierce-tony-pa-22-150

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2025-02-11](https://openairdocs.org/ad/2025-02-11): Rudder Structure · FS 2001 J5A (Army L-4F), J5A-80, J5B (Army L-4G) and 67 more. Effective Mar 20, 2025
- [AD 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI or SA02658SE). Effective Mar 21, 2022
- [AD 2015-08-04](https://openairdocs.org/ad/2015-08-04): Wings · FS 2000 L-14, AE-1, HE-1 and 77 more. Effective Jun 3, 2015
- [AD 2006-12-07](https://openairdocs.org/ad/2006-12-07): ECi cylinder assemblies · Aerostar AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 386 more. Effective Jul 11, 2006
- [AD 2006-03-08](https://openairdocs.org/ad/2006-03-08): Vacuum pumps · Aero Advantage 14-19, 14-19-2, 14-19-3 and 299 more. Effective Mar 10, 2006
- [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005
- [AD 2001-23-17](https://openairdocs.org/ad/2001-23-17): GNS 430 units · Cessna 172, 182, 206 and 209 more. Effective Dec 28, 2001
- [AD 85-02-05 R1](https://openairdocs.org/ad/85-02-05-R1): Piper P/N s 81090-02, 683-107 Placard Installation · Lavia Argentina PA-25, PA-25-235, PA-25-260 and 32 more. Effective Nov 21, 1997
- [AD 96-09-06](https://openairdocs.org/ad/96-09-06): Air Filter Assemblies · Maule Aerospace Technology 7ACA, 7ECA, 7FC and 180 more. Effective Jun 7, 1996
- [AD 85-06-04](https://openairdocs.org/ad/85-06-04): Fuel Tank · FS 2001 AE-1, HE-1, J5A-80 and 60 more. Effective May 4, 1985
- [AD 78-10-03](https://openairdocs.org/ad/78-10-03): Fuel Venting · FS 2001 AE-1, HE-1, J5A-80 and 66 more. Effective May 23, 1978
- [AD 74-17-04](https://openairdocs.org/ad/74-17-04): Fabric Reinforcement · FS 2002 PA-14, PA-12, PA-12S and 18 more. Effective Apr 11, 1977
- [AD 73-09-06](https://openairdocs.org/ad/73-09-06): Operating Limitation Placard - Throttle Hangup · Piper PA-22, PA-22-108, PA-22-135 and 5 more. Effective May 7, 1973
- [AD 72-21-03](https://openairdocs.org/ad/72-21-03): Fuel Line Failure · Piper PA-20, PA-20-115, PA-20-135 and 11 more. Effective Oct 13, 1972
- [AD 68-05-01](https://openairdocs.org/ad/68-05-01): Exhaust Mufflers · FS 2001 J5A-80, J5A (Army L-4F), J5B (Army L-4G) and 67 more. Effective Mar 31, 1968
- [AD 67-24-02](https://openairdocs.org/ad/67-24-02): Engine Fuel Starvation · Piper PA-22, PA-22-108, PA-22-135 and 5 more
- [AD 64-05-04](https://openairdocs.org/ad/64-05-04): Upper Main Oleo Bearings · Piper PA-22, PA-22-108, PA-22-135 and 2 more. Effective Mar 30, 1964
- [AD 60-01-07](https://openairdocs.org/ad/60-01-07): Tail Brace Wires · FS 2002 PA-14, PA-12, PA-12S and 5 more
- [AD 61-16-05](https://openairdocs.org/ad/61-16-05): Control Cable Replacement · Piper PA-18-150, PA-18A-135, PA-18A-150 and 6 more. Effective Jul 26, 1961
- [AD 60-05-03](https://openairdocs.org/ad/60-05-03): Safety Belt · Piper PA-22-150 and PA-22-160
- [AD 60-10-08](https://openairdocs.org/ad/60-10-08): Fuel Selector Valve · Piper PA-18, PA-18-105 (Special), PA-18-125 (Army L-21A) and 30 more. Effective Jul 15, 1960
- [AD 57-22-01](https://openairdocs.org/ad/57-22-01): Fire Prevention Rework · Piper PA-16, PA-16S, PA-20 and 12 more

Historical (superseded or no longer in force):

- [AD 99-01-05 R1](https://openairdocs.org/ad/99-01-05-R1) (historical): Wings · FS 2000 L-14, AE-1, HE-1 and 73 more. Effective Jan 14, 2014
- [AD 99-01-05](https://openairdocs.org/ad/99-01-05) (historical): Wing Lift Struts or Forks · FS 2000 L-14, AE-1, HE-1 and 73 more. Effective Feb 8, 1999

## Information bulletins (advisory) (1)

- [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018

## Registered aircraft (1)

- [N6956B](https://openairdocs.org/aircraft/N6956B): [Bushplane Lab LLC](https://openairdocs.org/faa-owner/BUSHPLANE%20LAB%20LLC), [Wilderville, OR](https://openairdocs.org/faa-place/OR/Wilderville), built 1956, S/N 22-4237P

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB SEA67F0116](https://openairdocs.org/ntsb/SEA67F0116), Sep 1, 1966: Piper PA-22 (N6956B), Redmond, OR, substantial damage

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (30)

As reported by operators and repair stations, by the model named in the report.

- [SDR 2020FA0000135](https://openairdocs.org/sdr/2020FA0000135), Feb 2, 2020: TERMINAL. MISINSTALLED. WHILE PERFORMING PREFLIGHT MAGNETO CHECK, IT WAS DETERMINED THAT THE LEFT MAGNETO WAS NOT PERFORMING CORRECTLY. THE AIRCRAFT RETURNED TO THE TIE DOWN AREA. ON D
- [SDR 2017FA0000548](https://openairdocs.org/sdr/2017FA0000548), Nov 8, 2017: LANDING GEAR. CORRODED. RIGHT LANDING GEAR RUSTED FROM INSIDE OUT WHERE FORWARD SUPPORT TUBE JOINS THE AXLE. FOUND WHEN SPOTTED A RUST LINE. USING PUNCH AND SMALL HAMMER FOUND THE COMP
- [SDR BQVR20120204](https://openairdocs.org/sdr/BQVR20120204), Feb 4, 2012: BRAKE. LOCKED. AT THE BEGINNING OF THE TAKEOFF ROLL, THE NOSE OF THE ACFT SUDDENLY LOWERED AND THE PROPELLER MADE CONTACT WITH THE GROUND. MX ARRIVED AT THE ACFT AND DISCOVERE
- [SDR CA101209012](https://openairdocs.org/sdr/CA101209012), Dec 1, 2010: COMPASS. INOPERATIVE. (CAN) WHEN SWINGING THE COMPASS THE EAST WEST ADJUSTMENT WAS NON RESPONSIVE COMPASS REPLACED WITH A NEW UNIT (TC# 20101209012)
- [SDR 2008FA0000376](https://openairdocs.org/sdr/2008FA0000376), Dec 26, 2007: CLAMP. LOOSE. ENGINE DID NOT RESPOND WHEN POWER WAS APPLIED ON A LOW FLY BY OF THE RUNWAY AND CAUSED THE PLANE TO LAND NEXT TO THE RUNWAY IN THE SNOW DAMAGING THE AIRCRAFT. T
- [SDR 2008FA0000375](https://openairdocs.org/sdr/2008FA0000375), Dec 26, 2007: CLAMP. WORN. ENGINE DID NOT RESPOND WHEN POWER WAS APPLIED ON A LOW FLY BY OF THE RUNWAY AND CAUSED THE PLANE TO LAND NEXT TO THE RUNWAY IN THE SNOW DAMAGING THE AIRCRAFT. T
- [SDR 2008FA0000098](https://openairdocs.org/sdr/2008FA0000098), Dec 26, 2007: MOUNT. CRACKED. FOUND NOSE GEAR MOUNT CORRODED THIN IN SPOTS ON THE LOWER TUBES FROM THE INSIDE. ORIGINAL THICKNESS .049 INCH AND IN THE THIN SPOTS THE THICKNESS WAS LESS THAN 
- [SDR 2008FA0000028](https://openairdocs.org/sdr/2008FA0000028), Dec 26, 2007: CLAMP. LOOSE. ENGINE DID NOT RESPOND WHEN POWER APPLIED ON A LOW FLY BY AND CAUSED THE PLANE TO LAND NEXT TO RUNWAY IN SNOW, DAMAGING ACFT. FOLLOWING PROBLEMS WERE FOUND ON P
- [SDR 2005FA0001473](https://openairdocs.org/sdr/2005FA0001473), Oct 28, 2005: P-LEAD. DETERIORATED. DURING RUNUP AFTER ANNUAL INSPECTION, LEFT MAG WAS NOT WORKING. FOUND INSULATION ON P-LEAD WIRE WAS DETERIORATING AND SHORTING TO SHIELDING CAUSING MAG TO BE CO
- [SDR 2005FA0001472](https://openairdocs.org/sdr/2005FA0001472), Oct 28, 2005: P-LEAD. DETERIORATED. DURING RUNUP AFTER ANNUAL INSPECTION, LEFT MAG WAS NOT WORKING. FOUND INSULATION ON P-LEAD WIRE WAS DETERIORATING AND SHORTING TO SHIELDING CAUSING MAG TO BE CO
- [SDR 2005FA0001471](https://openairdocs.org/sdr/2005FA0001471), Oct 28, 2005: P-LEAD. DETERIORATED. DURING RUNUP AFTER ANNUAL INSPECTION, LT MAG WAS NOT WORKING. FOUND INSULATION ON P-LEAD WIRE WAS DETERIORATING AND SHORTING TO SHIELDING CAUSING MAG TO BE CONT
- [SDR 2005FA0001470](https://openairdocs.org/sdr/2005FA0001470), Oct 28, 2005: P-LEAD. DETERIORATED. DURING RUNUP AFTER ANNUAL INSPECTION, LT MAG WAS NOT WORKING. FOUND INSULATION ON P-LEAD WIRE WAS DETERIORATING AND SHORTING TO SHIELDING CAUSING MAG TO BE CONT
- [SDR 2005FA0001632](https://openairdocs.org/sdr/2005FA0001632), Aug 31, 2005: TAIL WHEEL. WORN. PILOT REPORTED SEVERE TAILWHEEL SHIMMY DURING LANDING ROLLOUT LEADING TO LOSS OF CONTROL AND GROUND LOOP WITH SIGNIFICANT DAMAGE TO AIRCRAFT. POST ACCIDENT INSP
- [SDR 2003FA0001081](https://openairdocs.org/sdr/2003FA0001081), Oct 9, 2003: FUEL CAP. INADEQUATE. FUEL CAP DID NOT VENT. THE FUEL CAP WAS RETURNED TO MFG AND THEY REPORTED THE CAP TO BE VENTING PROPERLY. MFG REPLACED THE CAP AND THE REPLACEMENT REFUSED TO VE
- [SDR 2003FA0001046](https://openairdocs.org/sdr/2003FA0001046), Oct 1, 2003: FUEL CAP. MALFUNCTIONED. NEW FUEL CAP DID NOT VENT. FUEL TANK WAS PARTIALLY COLLAPSED AND SPEWING SOUND WAS COMING FROM THE CAP. CAP WAS TURNED FOR REMOVAL AND WHEN THE INDENTS RELEASED
- [SDR 2002FA0001105](https://openairdocs.org/sdr/2002FA0001105), Sep 6, 2002: FUEL CAP. BLOCKED. AIRCRAFT WAS AT A CRUISE ALTITUDE OF 1800 FT WHEN ENGINE QUIT RUNNING. MADE AN EMERGENCY LANDING IN A HAY FIELD. FUEL SELECTOR WAS SELECTED ON RT TANK. POST INS
- [SDR 20000913SH017](https://openairdocs.org/sdr/20000913SH017), Jul 13, 2000: DRUM. WARPED. INNER WHEEL HALF ASSEMBLY CAUSING BRAKE DRUMS TO WARP. FOUND EXCESSIVE BRAKE DRAGGING WHEN PERFORMING ANNUAL INSPECTION. SINCE NO SPECIFIC KEY POSITION, ASSEMBL
- [SDR 20000724SH017](https://openairdocs.org/sdr/20000724SH017), Jul 13, 2000: FUEL LINE. DETERIORATED. A MECHANIC PERFORMING ANNUAL INSP, REPORTED THE FUEL SYSTEM WOULD NOT FLOW FOR THE FUEL STRAINER TEST AND CLEANING. T/S FUEL SYS, FOUND BOTH RUBBER FUEL LINES I
- [SDR CA000516031](https://openairdocs.org/sdr/CA000516031), Apr 26, 2000: PROPELLER. CORRODED. (CAN) NO TEXT
- [SDR 99ZZZX2286](https://openairdocs.org/sdr/99ZZZX2286), May 1, 1999: VALVE. FAILED. EXHAUST VALVE NR 3 CYLINDER BROKE AT STEM CLOSE TO FACE OF VALVE. COMPLETE HEAD OF VALVE GONE, NOT FOUND. CAUSE UNKNOWN. NOTE: LOG SHOWS PART AS NR 74541. PART 
- [SDR 98ZZZX3557](https://openairdocs.org/sdr/98ZZZX3557), Jul 18, 1998: PUSHROD SPRING. BROKEN. PILOT NOTED THE ENGINE WOULD MISS THEN RUN. PILOT MADE PRECAUTIONARY LANDING. THE VALVE COVER ON CYLINDER NR 2 HAD A HOLE IN IT. INVESTIGATION SHOWED THE PUSHRO
- [SDR AU981019](https://openairdocs.org/sdr/AU981019), Jul 7, 1998: STUD. BROKEN. (AUS) NR 1 CYLINDER HOLDDOWN STUDS BROKEN OR LOOSE.
- [SDR AU980522](https://openairdocs.org/sdr/AU980522), May 13, 1998: MOUNT. CRACKED. (AUS) TOP RT ENGINE MOUNT TUBE CRACKED IN AREA ADJACENT TO THE WELD.
- [SDR 98ZZZX760](https://openairdocs.org/sdr/98ZZZX760), Jan 22, 1998: STRUT. RUSTED. WING STRUTS WERE INSPECTED IAW AD 93-10-06 AND SB 528D IN DEC '96 AND FOUND OK. DURING '97 ANNUAL, OWNER HAD ALL FOUR STRUTS INSPECTED AND MODIFIED. STC SA 4635
- [SDR CA970429006](https://openairdocs.org/sdr/CA970429006), Apr 22, 1997: BLADE. CORRODED. (CAN) PROPELLER RECEIVED FOR REPITCH. INSPECTION FOUND THE PROPELLER BLADES BENT WITH GOUGES AND CORROSION WHICH REQUIRED GRINDING AND FILLING.
- [SDR AU961197](https://openairdocs.org/sdr/AU961197), Aug 26, 1996: TUBE. CORRODED. (AUS) FUSELAGE STRUCTURE LH REAR LONGITUDINAL TUBE LOCATED TO THE REAR OF THE LH PASSENGER DOOR CORRODED THROUGH IN THREE PLACES IN A 152.4MM (6IN) LENGTH
- [SDR 96ZZZX3541](https://openairdocs.org/sdr/96ZZZX3541), Jun 10, 1996: GASKET. DEFECTIVE. GASKET SOFT AND CAME APART WHEN TOUCHED. AIRCRAFT USES AUTOGAS AND WHEN MANUFACTURER CALLED, THEY SAID THEY NEVER CHECK THE GASKETS WITH AUTO FUEL AND DID NOT K
- [SDR 96ZZZX3329](https://openairdocs.org/sdr/96ZZZX3329), Jun 1, 1996: TUBE. CRACKED. CONVERTED FROM TRI-PACER TO PACER CONFIG BY STC 5A45RM, TIME AS PACER, APPROXIMATELY 1,220 HRS. TAIL POST TUBE CRACKED AT .25 INCH HOLE THAT FORMERLY HELD TAIL 
- [SDR CA960222018](https://openairdocs.org/sdr/CA960222018), Feb 12, 1996: TUBING. CRACKED. (CAN) AIRCRAFT WAS INSPECTED AND FOUND TO HAVE SEVERAL CRACKS AND CORROSION IN STRUCTURAL TUBING, AS PER SKETCH, THAT APPEARS TO BE THE RESULT OF WATER FREEZING
- [SDR 95ZZZX1271](https://openairdocs.org/sdr/95ZZZX1271), Feb 28, 1995: SWITCH. DEFECTIVE. DEFECTIVE BENDIX SWITCH FAILED ON TAKEOFF RESULTING IN ENGINE STOPPAGE AND SUBSTANTIAL DAMAGE TO AIRCRAFT. AD 76-7-12 WAS COMPLIED WITH 80 HOURS (THIS IS TO COR

## STCs that may be installed (OpenAirDocs) (315, first 50)

Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [STC SA00343BO](https://openairdocs.org/stc/SA00343BO): Installation of a single configuration or a dual configuration Avidyne Corporation Integrated Flight Display, Model IFD540 loaded with Release 10.0 software (or later FAA approved release). Avidyne Corporation
- [STC SA00352BO PAGE 2](https://openairdocs.org/stc/SA00352BO%20PAGE%202): Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version),. Avidyne Corporation
- [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display). Garmin International Inc
- [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. TCW Technologies, LLC
- [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC
- [STC SA12428CH](https://openairdocs.org/stc/SA12428CH): Installation of the Lycoming Engines Electronic Ignition System (EIS). Lycoming Engines, An Operating Division of AVCO Corporation
- [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC
- [STC SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc
- [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC
- [STC SA02636SE](https://openairdocs.org/stc/SA02636SE): Installation of Garmin GPS 175 Navigation System and GNX 375 Navigation System with ADS-B In/Out Transponder. Garmin International Inc
- [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc
- [STC SA01147WI](https://openairdocs.org/stc/SA01147WI): Installation of Concorde FLA or VRSLA series batteries in Piper Light Airplanes. Concorde Battery Corporation
- [STC SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc
- [STC SA01005DE](https://openairdocs.org/stc/SA01005DE): Installation of a EarthX ETX900-TSO Lithium battery. EarthX Inc
- [STC SA00081NY](https://openairdocs.org/stc/SA00081NY): Installation of Iceman Aviation Supplies, Inc. Carburetor Ice Detector. Alcor LLC
- [STC SA12025AT](https://openairdocs.org/stc/SA12025AT): This STC allows the exchange of the valid Standard Airworthiness Certificate issued to aircraft serial number 22-2838, a Piper PA-22-150 aircraft registered as N2463P, which meets the requirements of 14 CFR Part 21.24(a)(1) for a Special Airworthiness - Primary Category Airworthiness Certificate, under the existing provisions of 14 CFR Part 21.184(c). Christopher Allen Cox
- [STC SA316SO](https://openairdocs.org/stc/SA316SO): Carburetor ice detector. LegacySTC.com. Lists PA-22 Series
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc
- [STC SA04046CH PAGE 2](https://openairdocs.org/stc/SA04046CH%20PAGE%202): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc
- [STC SA26EA](https://openairdocs.org/stc/SA26EA): Conversion of aircraft for parachute jumping and aerial photography. Steve Pierce
- [STC SA11854CH](https://openairdocs.org/stc/SA11854CH): Installation of modified exhaust system in lieu of original components. Dakota Cub Aircraft Inc
- [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd
- [STC SA02594SE](https://openairdocs.org/stc/SA02594SE): SkyView HDX Instrumentation and Autopilot System manufactured. Dynon Avionics
- [STC SA02386AK](https://openairdocs.org/stc/SA02386AK): Replacement of existing landing and/or taxi light reflector and bulbs with Light Emitting Diode (LED) lighting systems. AeroLED's Holding LLC
- [STC SA03898NY](https://openairdocs.org/stc/SA03898NY): Installation and maintenance of ORATEX covering and coating material. Aircraft Design & Certification Ltd
- [STC SA01343WI](https://openairdocs.org/stc/SA01343WI): Installation of B&C Specialty Products BC400 alternator. B & C Specialty Products Inc
- [STC SA09150SC](https://openairdocs.org/stc/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. Peter C. Morrison
- [STC SA8334SW](https://openairdocs.org/stc/SA8334SW): Installation of dual toe brakes including rudder pedals, linkages and torque tubes. Peter C. Morrison
- [STC SA8438SW](https://openairdocs.org/stc/SA8438SW): Installation of dual toe brakes including rudder pedals, linkages and torque tubes. Peter C. Morrison
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA02532AT](https://openairdocs.org/stc/SA02532AT): Installation of subject Michelin tires on appropriate aircraft. For Michelin 5, 6, 8, and 10-inch rim diameter tires on General Aviation Aircraft. Michelin North America Inc
- [STC SA01899WI](https://openairdocs.org/stc/SA01899WI): Installation of Garmin G3X Touch Electronic Flight Instrument System. Garmin International Inc
- [STC SA02576AK](https://openairdocs.org/stc/SA02576AK): Installation of Cleveland and ABI, LLC Wheel and Brake Kits. ABI LLC
- [STC SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio. Peregrine
- [STC SA02233AK](https://openairdocs.org/stc/SA02233AK): Installation of high visibility fuel sight gauge. Dakota Cub Aircraft Inc
- [STC SA00756DE](https://openairdocs.org/stc/SA00756DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT22 Transponder and an approved Global Positioning System (GPS) Position Sensor. Peregrine
- [STC SA3-494](https://openairdocs.org/stc/SA3-494): Installation of Model C2200 main ski and AWN-1200A nose wheel ski. F.Atlee Dodge Aircraft Services. Lists PA-22 Series
- [STC SA02987CH](https://openairdocs.org/stc/SA02987CH): Installation of the Electroair Electronic Ignition System. Electroair Acquisition Corporation
- [STC SA00954WI](https://openairdocs.org/stc/SA00954WI): Installation of Concorde RG Series Batteries in Piper Single Engine Airplanes. Aero-Mach Wilco LLC
- [STC SA02534AK](https://openairdocs.org/stc/SA02534AK): Installation of Airframes Alaska Aluminum Lift Struts. Airframes Alaska LLC
- [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc
- [STC SA04776NY](https://openairdocs.org/stc/SA04776NY): The HIPEC Covering and Finishing System must be performed and maintained. HIPEC Aircraft Coatings Inc
- [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC
- [STC SA02153AK](https://openairdocs.org/stc/SA02153AK): Installation of Burl's Aircraft Rebuild Magnum I tail wheel Penetration ski. Burl's Aircraft Rebuild LLC
- [STC SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc
- [STC SA02553AK](https://openairdocs.org/stc/SA02553AK): Fabrication and installation of a Tail Wheel Anti-Shimmy Dampener. Keller Engineering Group LLC
- [STC SA11174SC PAGE 2](https://openairdocs.org/stc/SA11174SC%20PAGE%202): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King)
- [STC SA10822SC](https://openairdocs.org/stc/SA10822SC): Installation of EFD1000 Primary Flight Display. Aspen Avionics Inc
- [STC SA220SO](https://openairdocs.org/stc/SA220SO): Tow bar, release mechanism, and safety tow link. Fliegen Works Inc. d/b/a Pacific Aerial Tow Hooks
- [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation

All 315: https://openairdocs.org/model/piper-pierce-tony-pa-22-150/stcs.md

## PMA parts (OpenAirDocs) (570, first 50)

Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this model on its data sheet, so check the FAA record before relying on it. Newest first.

- [73-CFG-R](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139218545420260806152425.0001): Fuel Quantity Indication Placard. Swift Fuels, LLC · PMA PQ04423CE · Modification part · Jul 20, 2026
- [S1069](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID113256326820260806152332.0001): 100R Fuel Placard. Swift Fuels, LLC · PMA PQ04423CE · Modification part · Jul 20, 2026
- [066-106](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID126294031320260728184416.0001): Brake Lining. Game Aerospace, LLC · PMA PQ00052CB · Replaces Cleveland Wheels and Brakes P/N… · Jun 9, 2026
- [AF40622](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID191324127820260518151656.0001): Rudder Assembly. Dakota Cub Aircraft · PMA PQ2498CE · Replaces 40622-07 · Apr 22, 2026
- [AF40622](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID188328415320260313134658.0001): Rudder Assembly. Dakota Cub Aircraft · PMA PQ2498CE · Replaces 40622-00 · Mar 11, 2026
- [AF40622](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165776775320260313134659.0001): Rudder Assembly. Dakota Cub Aircraft · PMA PQ2498CE · Replaces 15726-02 · Mar 11, 2026
- [AF40622](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID117894135320260313134657.0001): Rudder Assembly. Dakota Cub Aircraft · PMA PQ2498CE · Replaces 40622-08 · Mar 11, 2026
- [PP-260-MDL](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID107087814920260310191150.0001): Piper PA22 Oil Cooler System. KNR - Inc · PMA PQ2575NM · Replaces ModificationArticle · Feb 23, 2026
- [PP-260-MDL](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID136385101920250918163918.0001): Piper PA22 Oil Cooler System. KNR - Inc · PMA PQ2575NM · Replaces ModificationArticle · Sep 20, 2025
- [V674903](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID173604854020260423211205.0001): Leaded and Unleaded Automotive Gasoline. Air Plains Services Corp · PMA PQ3524CE · Modification part · Aug 29, 2025
- [P002-1247130-A021](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID121120551020250813154902.0001): Spinner Assembly. Aero Tech Aviation Design, LLC · PMA PQ04281CE · Replaces 14422-A · Jul 31, 2025
- [SC-W/T-1036-6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID175141724820250430172143.0001): Piper PA-20 & 22 Pilot Window (with 6 hole ventilator, Solar Control Green). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 14248-00 · Apr 22, 2025
- [SC-W/G-1036-5](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172030709820250430172144.0001): Piper PA-20 & 22 Pilot Window (with 5 hole ventilator, Solar Control Gray). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 13888-00 · Apr 22, 2025
- [SC-W/G-1036-0](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161567849020250430172145.0001): Piper PA-20 & 22 Pilot Window (Without ventilator hole, Solar Control Gray). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 13888-00, 14248-00 · Apr 22, 2025
- [SC-W/T-1036-0](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145224315320250430172145.0001): Piper PA-20 & 22 Pilot Window (Without ventilator hole, Solar Control Green). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 13888-00, 14248-00 · Apr 22, 2025
- [SC-W/G-1036-6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID120959114920250430172144.0001): Piper PA-20 & 22 Pilot Window (with 6 hole ventilator, Solar Control Gray). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 14248-00 · Apr 22, 2025
- [SC-W/T-1036-5](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID103113312920250430172144.0001): Piper PA-20 & 22 Pilot Window (with 5 hole ventilator, Solar Control Green). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 13888-00 · Apr 22, 2025
- [MDL TD 031851](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184021792220250508133546.0001): VA-1A( )AndAccessories. Electronics International Inc · PMA PQ0088NM · Modification part · Apr 10, 2025
- [AF40622](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID156514375820250224215855.0001): Rudder Assembly. Airframes Alaska LLC · PMA PQ3848CE · Replaces 40622 · Feb 20, 2025
- [MDL RR1-2-01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID188380771120250311133057.0001): Alternate Avionic SupportStrut Assemblies. Radiorax Aviation Systems LLC · PMA PQ00040WB · Modification part · Jan 17, 2025
- [SC-W/T-1035](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID185429404520241230194536.0001): Piper PA-20 & 22 Hinged Window (Solar Control Green). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 13849-00 · Dec 18, 2024
- [SC-W/G-1035](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID162009872820241230194537.0001): Piper PA-20 & 22 Hinged Window (Solar Control Gray). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 13849-00 · Dec 18, 2024
- [LSM-200-700-11](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID187312814920250417183925.0001): Hub Cap Assy. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · Dec 10, 2024
- [110HS](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193059656020240221142908.0001): Drain Valve Assembly. Saf-Air Products Inc · PMA PQ2036CE · Replaces CAV-110H-4 · Jan 30, 2024
- [110SS](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184612663120240221142904.0001): Drain Valve Assembly. Saf-Air Products Inc · PMA PQ2036CE · Replaces CAV-110 · Jan 30, 2024
- [ABI-199-71](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID185216082420230911142530.0001): Wheel & Brake Kit 1.25” Axle, 6 Bolt. ABI LLC · PMA PQ4204CE · Modification part · Aug 30, 2023
- [ABI-199-62A](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID131457142520230911142552.0001): Wheel & Brake Kit 1.5” Axle, 6 Bolt. ABI LLC · PMA PQ4204CE · Modification part · Aug 30, 2023
- [ABI-199-62](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID117544472620230911142538.0001): Wheel & Brake Kit 1.5” Axle, 3 Bolt. ABI LLC · PMA PQ4204CE · Modification part · Aug 30, 2023
- [AF51708](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID198644398920230906211302.0001): PARKING BRAKE SEAT. Airframes Alaska LLC · PMA PQ3848CE · Replaces 4206 · Aug 29, 2023
- [AF51705](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID162907821920230906211255.0001): PARKING BRAKE ASSEMBLY. Airframes Alaska LLC · PMA PQ3848CE · Replaces 492-023 · Aug 29, 2023
- [AF51706](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID144876925220230906211256.0001): PARKING BRAKE BODY. Airframes Alaska LLC · PMA PQ3848CE · Replaces 4201 · Aug 29, 2023
- [AF51707](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID142727659420230906211301.0001): PARKING BRAKE SHAFT. Airframes Alaska LLC · PMA PQ3848CE · Replaces 4203 · Aug 29, 2023
- [AF51711](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID106262958220230906211303.0001): PARKING BRAKE LEVER ARM ASSEMBLY. Airframes Alaska LLC · PMA PQ3848CE · Replaces 4208 · Aug 29, 2023
- [UAV-1004236-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179059944320230707211347.0001): AV-30-C. uAvionix Corporation · PMA PQ05445NM · Modification part · Jun 28, 2023
- [CS-2000-13](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID177394590420221103165921.0001): Fitting Assembly, Rear Gear. Airframes Alaska LLC · PMA PQ3848CE · Replaces CS-2000-13 · Oct 26, 2022
- [CS-2000-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID129651210120221103165919.0001): Cabane V Assembly. Airframes Alaska LLC · PMA PQ3848CE · Replaces CS-2000-4 · Oct 26, 2022
- [CS-2000-12](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID127144160520221103165920.0001): Fitting Assembly, Front Gear. Airframes Alaska LLC · PMA PQ3848CE · Replaces CS-2000-12 · Oct 26, 2022
- [CS-2000-15](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID120650729520221103165922.0001): End Adapter / Maule Oleo Strut. Airframes Alaska LLC · PMA PQ3848CE · Replaces CS-2000-15 · Oct 26, 2022
- [SA-820](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID199575972920221103171154.0001): Control, Propeller. Svenn's Aviation LLC · PMA PQ4124CE · Modification part · Oct 21, 2022
- [SA-810](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID198441677920221103171145.0001): Governor Arm. Svenn's Aviation LLC · PMA PQ4124CE · Modification part · Oct 21, 2022
- [SA-815 Assembly](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID182846679220221103171151.0001): Governor Bracket Assembly. Svenn's Aviation LLC · PMA PQ4124CE · Modification part · Oct 21, 2022
- [SA-814](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID181274383420221103171149.0001): Propeller Control Bracket. Svenn's Aviation LLC · PMA PQ4124CE · Modification part · Oct 21, 2022
- [SA-811](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180410512620221103171146.0001): Propeller Cable Clip. Svenn's Aviation LLC · PMA PQ4124CE · Modification part · Oct 21, 2022
- [SA-813](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169790196220221103171148.0001): Governor Bracket. Svenn's Aviation LLC · PMA PQ4124CE · Modification part · Oct 21, 2022
- [SA-815](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID162089244720221103171150.0001): Governor Bracket. Svenn's Aviation LLC · PMA PQ4124CE · Modification part · Oct 21, 2022
- [SA-817](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID151439137720221103171152.0001): Governor Arm. Svenn's Aviation LLC · PMA PQ4124CE · Modification part · Oct 21, 2022
- [SA-812](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149111349120221103171147.0001): Propeller Cable Clamp. Svenn's Aviation LLC · PMA PQ4124CE · Modification part · Oct 21, 2022
- [8000328](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID143578811220221130202557.0001): Engine Oil Cooler. Aero-Classics Heat Transfer Products Inc · PMA PQ2543NM · Replaces Harrison 8521940 · Oct 21, 2022
- [SA-813 Assembly](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID115817967120221103171149.0001): Governor Bracket Assembly. Svenn's Aviation LLC · PMA PQ4124CE · Modification part · Oct 21, 2022
- [SA-819](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID102126253320221103171153.0001): Firewall Recess. Svenn's Aviation LLC · PMA PQ4124CE · Modification part · Oct 21, 2022

All of them: https://openairdocs.org/model/piper-pierce-tony-pa-22-150/pma.md

## The same model under other registry codes

Amateur-built copies and renamed makers get their own codes.

- [Piper PA-22-150](https://openairdocs.org/model/piper-pa-22-150): 1,200 registered aircraft, registry code 7102210

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