# Piper/Anderson PA 28-180

- Type: Aircraft model (FAA registry)
- Registry code: 7102821
- Manufacturer (registry): PIPER/ANDERSON
- Model: PA 28-180
- 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 2A13](https://openairdocs.org/tcds/2A13) (OpenAirDocs)
- Holder: Piper Aircraft Inc.
- Registered aircraft: 0
- Page: https://openairdocs.org/model/piper-anderson-pa-28-180

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 2024-14-03](https://openairdocs.org/ad/2024-14-03): Autopilot System · Garmin GFC 500 Autopilot (STC SA01866WI). Effective Aug 20, 2024
- [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 2020-24-05](https://openairdocs.org/ad/2020-24-05): Wing Spar · Piper PA-28-140, PA-28-150, PA-28-160 and 4 more. Effective Dec 28, 2020
- [AD 2018-07-03](https://openairdocs.org/ad/2018-07-03): Placard and Markings · Piper PA-28-140, PA-28-150, PA-28-151 and 12 more. Effective Apr 20, 2018
- [AD 2017-14-04](https://openairdocs.org/ad/2017-14-04): Engine Oil · Piper PA-28-140, PA-28-150, PA-28-151 and 22 more. Effective Aug 15, 2017
- [AD 2013-02-13](https://openairdocs.org/ad/2013-02-13): Stabilizer Control System · Piper PA-28-140, PA-28-150, PA-28-151 and 33 more. Effective Mar 11, 2013
- [AD 2010-15-10](https://openairdocs.org/ad/2010-15-10): Control wheel shafts · Piper PA-28-140, PA-28-150, PA-28-151 and 33 more. Effective Aug 31, 2010
- [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 2005-25-08](https://openairdocs.org/ad/2005-25-08): Electronic Flight Information System (EFIS) · B-N Group BN-2A, 172, 180 and 22 more. Effective Jan 23, 2006
- [AD 2005-19-20](https://openairdocs.org/ad/2005-19-20): Bushing screw thread expanders · Piper PA-28-160, PA-28-161, PA-28-180 and 1 more. Effective Nov 4, 2005
- [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 98-21-21 R1](https://openairdocs.org/ad/98-21-21-R1): Electric Inflatable Door Seals · Cessna 17-30, 17-30A, 17-31 and 267 more. Effective May 1, 2000
- [AD 99-05-09](https://openairdocs.org/ad/99-05-09): Induction Air Filter · Piper PA-23-235, PA-23-250, PA-23-250 (Navy UO-1) and 20 more. Effective Mar 19, 1999
- [AD 96-10-01 R1](https://openairdocs.org/ad/96-10-01-R1): Landing Light Support and Seal Assembly · Piper PA-28-140, PA-28-150, PA-28-160 and 1 more. Effective Dec 14, 1998
- [AD 96-10-03](https://openairdocs.org/ad/96-10-03): Flap Handle Attach Bolt · Piper PA-28-140, PA-28-150, PA-28-151 and 28 more. Effective Jun 14, 1996
- [AD 87-08-08 R3](https://openairdocs.org/ad/87-08-08-R3): Lower spar cap · Piper PA-28-140, PA-28-150, PA-28-151 and 28 more. Effective May 22, 1989
- [AD 86-17-01](https://openairdocs.org/ad/86-17-01): Ammeter Replacement · Piper PA-28-150, PA-28-160, PA-28-180 and 20 more. Effective Aug 21, 1986
- [AD 79-26-05](https://openairdocs.org/ad/79-26-05): Oil and Fuel System Hoses · Piper PA-28-140, PA-28-150, PA-28-151 and 28 more. Effective Jan 3, 1980
- [AD 69-22-02](https://openairdocs.org/ad/69-22-02): Failure of Control Wheel · Piper PA-28-140, PA-28-150, PA-28-160 and 4 more. Effective Jul 30, 1979
- [AD 79-07-02](https://openairdocs.org/ad/79-07-02): Batteries · Aircraft Parts & Development A, A-2, A-3 and 149 more. Effective Apr 3, 1979
- [AD 77-23-03](https://openairdocs.org/ad/77-23-03): Rod End Bearings · Piper PA-28-140, PA-28-151, PA-28-161 and 12 more. Effective Nov 14, 1977
- [AD 77-01-01](https://openairdocs.org/ad/77-01-01): Fuel Quantity Gauge · Piper PA-28-140, PA-28-150, PA-28-151 and 7 more. Effective Jan 7, 1977
- [AD 75-24-02](https://openairdocs.org/ad/75-24-02): Loose Seats · Piper PA-28-180, PA-28-235, PA-28R-180 and 5 more. Effective Nov 21, 1975
- [AD 75-08-03](https://openairdocs.org/ad/75-08-03): Fuel Drain Valves · Piper PA-28-140, PA-28-150, PA-28-151 and 6 more. Effective Apr 4, 1975
- [AD 75-02-03](https://openairdocs.org/ad/75-02-03): Nose Wheel Fork Assembly · Large nose gear fork and 8.00-6 nose gear tire (Airglas STC SA281AL)
- [AD 74-26-07](https://openairdocs.org/ad/74-26-07): Incorrect Placard Detection · Piper PA-28-180. Effective Dec 21, 1974
- [AD 74-09-04](https://openairdocs.org/ad/74-09-04): Rear Seat Belt Installation · Piper PA-28-140, PA-28-180, PA-28-235 and 1 more. Effective Apr 24, 1974
- [AD 72-17-05](https://openairdocs.org/ad/72-17-05): Electric Trim Switch · Piper PA-28-180, PA-28-235, PA-28R-180 and 3 more. Effective Aug 15, 1972
- [AD 72-14-07](https://openairdocs.org/ad/72-14-07): Bolts in Stabilator Hinge Fittings · Piper PA-28-140, PA-28-150, PA-28-160 and 7 more. Effective Jul 7, 1972
- [AD 70-16-05](https://openairdocs.org/ad/70-16-05): Engine Exhaust Muffler · Piper PA-28-140, PA-28-150, PA-28-160 and 3 more. Effective May 19, 1972
- [AD 72-08-06](https://openairdocs.org/ad/72-08-06): Main Landing Gear Torque Links · Piper PA-28-140, PA-28-150, PA-28-160 and 4 more. Effective Apr 14, 1972
- [AD 71-21-08](https://openairdocs.org/ad/71-21-08): Binding of Fuel Selector Handle · Piper PA-28-140, PA-28-180, PA-28R-180 and 1 more. Effective Oct 13, 1971
- [AD 71-14-06](https://openairdocs.org/ad/71-14-06): Magnetos Grounding · Piper PA-28-140, PA-28-150, PA-28-160 and 2 more. Effective Jul 9, 1971
- [AD 70-26-04](https://openairdocs.org/ad/70-26-04): Stabilizer Balance Weight Tube · Piper PA-28-140, PA-28-150, PA-28-160 and 8 more. Effective Jun 24, 1971
- [AD 70-18-05](https://openairdocs.org/ad/70-18-05): Landing Gear Torque Link Bolts · Piper PA-28-140, PA-28-150, PA-28-160 and 4 more. Effective Sep 7, 1970
- [AD 69-15-01](https://openairdocs.org/ad/69-15-01): Control Wheel Retaining Pin · Piper PA-28-180, PA-28-235, PA-28R-180 and 3 more. Effective Jul 21, 1969
- [AD 67-26-02](https://openairdocs.org/ad/67-26-02): Fuel Selector Valve · Piper PA-28-140, PA-28-150, PA-28-160 and 8 more. Effective May 22, 1968
- [AD 67-26-03](https://openairdocs.org/ad/67-26-03): Fuel System Screens and Filters · Piper PA-28-140, PA-28-150, PA-28-160 and 7 more. Effective Apr 12, 1968
- [AD 67-20-04](https://openairdocs.org/ad/67-20-04): Main Landing Gear Torque Link · Piper PA-28-140, PA-28-150, PA-28-160 and 8 more. Effective Sep 27, 1967
- [AD 67-12-06](https://openairdocs.org/ad/67-12-06): Open End Steel Tube Assemblies · Piper PA-28-140, PA-28-150, PA-28-160 and 3 more. Effective May 4, 1967
- [AD 66-20-05](https://openairdocs.org/ad/66-20-05): Propeller Spinner · Piper PA-28-150, PA-28-160 and PA-28-180. Effective Aug 27, 1966
- [AD 65-06-06](https://openairdocs.org/ad/65-06-06): Fuel Quantity Gauge Sender Units · Piper PA-28-140, PA-28-150, PA-28-160 and 2 more. Effective Mar 12, 1965
- [AD 64-06-06](https://openairdocs.org/ad/64-06-06): Control Wheels · Piper PA-28-150, PA-28-160, PA-28-180 and 3 more. Effective Apr 6, 1964
- [AD 62-19-03](https://openairdocs.org/ad/62-19-03): Propeller Attach Bolts · Piper PA-28-150, PA-28-160 and PA-28-180. Effective Aug 28, 1962

Historical (superseded or no longer in force):

- [AD 2018-02-05](https://openairdocs.org/ad/2018-02-05) (historical): Placard and Markings · Piper PA-28-140, PA-28-150, PA-28-151 and 12 more. Effective Feb 7, 2018
- [AD 96-10-01](https://openairdocs.org/ad/96-10-01) (historical): Landing Light Support and Seal Assembly · Piper PA-28-140, PA-28-150, PA-28-160 and 1 more. Effective Jun 10, 1996
- [AD 95-26-13](https://openairdocs.org/ad/95-26-13) (historical): Inspect Oil Cooler Hoses · Piper PA-28-140, PA-28-150, PA-28-151 and 22 more. Effective Feb 5, 1996

## Information bulletins (advisory) (20)

- [SAIB 2022-20](https://openairdocs.org/saib/2022-20): Wing Spar. Issued Oct 19, 2022
- [SAIB AIR-21-10](https://openairdocs.org/saib/AIR-21-10): Wing, Attach Fittings (JASC 5740). Issued Jun 29, 2021
- [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018
- [SAIB CE-11-12R1](https://openairdocs.org/saib/CE-11-12R1): Wings - PA-28, PA-32, PA-34, and PA-44 Rear Spar Corrosion at Fuselage Attach Fitting. Issued Dec 2, 2015
- [SAIB CE-14-23](https://openairdocs.org/saib/CE-14-23): Powerplant; Air Intake. Issued Aug 6, 2014
- [SAIB CE-14-22](https://openairdocs.org/saib/CE-14-22): Fuel Selector/Shut-Off Valve. Issued Jul 10, 2014
- [SAIB CE-13-26](https://openairdocs.org/saib/CE-13-26): Engine Air Intake System; Air Box Vanes. Issued Mar 27, 2013
- [SAIB CE-11-42](https://openairdocs.org/saib/CE-11-42): Flight Controls: Control Cable/Pulley Inspections. Issued Jun 29, 2011
- [SAIB CE-11-14](https://openairdocs.org/saib/CE-11-14): Stabilizers- Vertical Stabilizer on Piper PA-28, PA-32, PA-34 Forward Attach Point Corrosion. Issued Jan 5, 2011
- [SAIB CE-11-13](https://openairdocs.org/saib/CE-11-13): Wings - Piper PA-28, PA-32, PA-34 Forward Spar Corrosion. Issued Jan 5, 2011
- [SAIB CE-11-12](https://openairdocs.org/saib/CE-11-12) (historical): PA-28, PA-32, PA-34, and PA-44 Rear Spar Corrosion at Fuselage Attach Fitting. Issued Jan 5, 2011
- [SAIB CE-11-11](https://openairdocs.org/saib/CE-11-11): Wings - Piper PA-28, PA-32, and PA-34 Aileron Hinge Fitting Corrosion. Issued Jan 5, 2011
- [SAIB CE-11-10](https://openairdocs.org/saib/CE-11-10): Piper PA-28, PA-32, PA-34, and PA-44 Corrosion on Flap Hinges, Brackets, and Ribs. Issued Jan 5, 2011
- [SAIB CE-11-01](https://openairdocs.org/saib/CE-11-01): Stabilizers -Horizontal Stabilator   Turnbuckle. Issued Oct 4, 2010
- [SAIB CE-10-17](https://openairdocs.org/saib/CE-10-17): Landing Gear - Piper PA-28 and PA-32 Main Landing Gear Torque Link Inspection Interval. Issued Feb 23, 2010
- [SAIB CE-09-23](https://openairdocs.org/saib/CE-09-23): Fuel: Piper PA-28, PA-32, PA-34. Issued Apr 7, 2009
- [SAIB CE-09-17](https://openairdocs.org/saib/CE-09-17): Fuel: Piper PA-28 Series Aircraft Fuel Vent and Supply Hose Condition. Issued Mar 10, 2009
- [SAIB CE-05-29R1](https://openairdocs.org/saib/CE-05-29R1): . Issued Feb 3, 2005
- [SAIB CE-04-63](https://openairdocs.org/saib/CE-04-63): . Issued Apr 16, 2004
- [SAIB CE-02-43](https://openairdocs.org/saib/CE-02-43): . Issued Sep 10, 2002

## Registered aircraft

None registered with this model now.

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (194, newest 50)

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

- [SDR 2024FA0000435](https://openairdocs.org/sdr/2024FA0000435), Jun 7, 2024: CASE. CRACKED. ON CLIMB TO CRUISING ALTITUDE PIC FELT AN ENGINE VIBRATION AND DECIDED TO TURN BACK TO KARG. ON TURN BACK TO DEPARTURE AIRPORT OIL PRESSURE DROPPED TO "0" AND E
- [SDR 2024FA0000421](https://openairdocs.org/sdr/2024FA0000421), Jun 3, 2024: SCREW. LOOSE. OWNER COMPLAINED OF A ROUGH RUNNING ENGINE. DIAGNOSIS FOUND THE BEARING CAP ASSEMBLY MOUNTING SCREWS HAS COME LOOSE ON THE RH MAGNETO.ONE SCREW AND RETAINER HAS
- [SDR 2024FA0000065](https://openairdocs.org/sdr/2024FA0000065), Jan 11, 2024: PISTON. FAILED. FOLLOWING A FLT TEST, IN PATTERN WITH ACFT & NEW ENG, DEPARTED KLUD FOR THE 2ND BREAK-IN FLT IAW SERVICE INSTRUCTIONS. MADE A FULL-STATIC POWER RUNUP & INITIATE
- [SDR 2023FA0000841](https://openairdocs.org/sdr/2023FA0000841), Dec 4, 2023: COWLING. FAILED. UPPER COWLING BROKE AWAY FROM AIRCRAFT DURING FLIGHT. AFTER INSPECTING THE AIRCRAFT, IT SEEMS THE FRONT PIN BROKE OFF THE COWLING POSSIBLY THE ADESSIVE FAILED A
- [SDR 2023FA0000235](https://openairdocs.org/sdr/2023FA0000235), Apr 20, 2023: TUBE. UNKNOWN. PILOT NOTED SMALL WISPS OF SMOKE IN THE COCKPIT AND CO PILOT NOTICED OIL ON THE LEADING EDGE OF THE RH WING. PILOT RETUNED TO AIRPORT AND BROUGHT THE AIRPLANE T
- [SDR 2023FA0000234](https://openairdocs.org/sdr/2023FA0000234), Apr 20, 2023: LINE. UNKNOWN. THE B NUT ON THE OIL RETURN LINE FROM THE #1 CYLINDER WAS FOUND TO BE LOOSE. OIL WAS LEAKING FORM THIS LOCATION AND SOME WAS NOTED ON THE LEADING EDGE OF THE RH
- [SDR 2023FA0000023](https://openairdocs.org/sdr/2023FA0000023), Jan 10, 2023: NONE. NONE. UNDERSTANDING OF THE 1ST GENERATION FUEL SELECTOR FOR PIPER AIRCRAFT. SEE SB 840A, SAIB CE-14-22, SB 1309A, PIPER SB 355, SA-075. PILOTS ARE INADVERTENTLY SELEC
- [SDR 2022FA0000422](https://openairdocs.org/sdr/2022FA0000422), Jul 18, 2022: CARBURETOR. INACCURATE. FACTORY OVERHAULED ENGINE INSTALLED IN AIRFRAME. PERFORMANCE WAS NORMAL, BUT NOTED THAT CARBURETOR WAS DIFFICULT TO SET AND MAINTAIN LEAN CUTOFF RISE IN RPM DUR
- [SDR 2021FA0000144](https://openairdocs.org/sdr/2021FA0000144), Jan 13, 2021: GYRO. FAULTED. AIRCRAFT WAS OPERATING UNDER 14 CFR 141 RULES IN IMC CONDITIONS WHEN THE AIRCRAFT EXPERIENCED AN INSTRUMENTATION FAILURE OF THE HORIZONTAL SITUATION INDICATOR. 
- [SDR 2020FA0000286](https://openairdocs.org/sdr/2020FA0000286), Jun 8, 2020: SPINNER. SEPARATED. IN VFR CRUSE FLIGHT WITH ATC, THE PILOT REPORTED HEARING A LOUD BANG AND A SLIGHT ENGINE VIBRATION. A PRECAUTIONARY LANDING WAS MADE, INSPECTION OF THE AIRCRAFT
- [SDR 2019FA0000316](https://openairdocs.org/sdr/2019FA0000316), Sep 24, 2019: SELECTOR VALVE. STIFF. FUEL SELECTOR VALVE WAS STIFF AND WOULD JUMP PASS DETENT CAUSING LOSS OF FUEL FLOW FROM RIGHT TANK.
- [SDR 2019FA0000308](https://openairdocs.org/sdr/2019FA0000308), Aug 30, 2019: VOLT REGULATOR. INTERMITTENT. CUSTOMER COMPLAINED THAT ALTERNATOR WOULD QUIT CHARGING AFTER APPROXIMATELY 20 MINUTE FLIGHT. CONDUCTED TEST FLIGHT OF AIRCRAFT, MONITORED CHARGING VOLTAGE WITH
- [SDR 2019FA0000227](https://openairdocs.org/sdr/2019FA0000227), Jul 19, 2019: CABLE GUARD. CHAFED. CABLE PULLEY GUARD CHAFFED IN 3 PIECES BY RUDDER CABLES AT BASE OF CONTROL YOKE. GUARD PLACED IN WRONG HOLE IN CONSOLE. CORRECT HOLE COVERED BY HEAT DUCT MOUNT 
- [SDR 2019FA0000210](https://openairdocs.org/sdr/2019FA0000210), Jun 21, 2019: TURNBUCKLE. CRACKED. WHILE RETENSIONING THE LOWER STABILATOR TURN BUCKLE AFTER STABILATOR REPLACEMENT THE AFT CABLE END APPEARED BENT. CLOSE INSPECTION SHOWED A CRACK AND PARTIAL PA
- [SDR 2017FA0000516](https://openairdocs.org/sdr/2017FA0000516), Oct 17, 2017: WING ROOT. CRACKED. AT INSPECTION, FOUND BOTH R/H WING ROOT SKIN DOUBLER CRACKED. CONTACTED THE MANUFACTURER, FOUND THAT THIS IS A COMMON PROBLEM.
- [SDR 2017FA0000398](https://openairdocs.org/sdr/2017FA0000398), Aug 9, 2017: SKIN. CRACKED. DURING AN ANNUAL INSPECTION, A 4.5 INCH CRACK WAS FOUND IN THE SKIN AT THE AFT EDGE OF THE BOTTOM CHANNEL STIFFENER, REAR SPAR LOCATION. STOP DRILLED THE CRACK 
- [SDR 2015FA0000216](https://openairdocs.org/sdr/2015FA0000216), May 14, 2015: PIN. SHEARED. FLAP HANDLE WILL NOT CLICK INTO DE-TENT ON LANDING. INSPECTION SHOWED DETENT PIN SHEARED IN HALF THROUGH RETENTION ROLL PIN HOLE. CAUSING FLAP TO RETRACT ON LAN
- [SDR 2015FA0000163](https://openairdocs.org/sdr/2015FA0000163), Apr 28, 2015: STRUCTURE. CORRODED. EXTENSIVE CORROSION IN FUSELAGE AND WINGS, ESPECIALLY THE LEFT WING. THE PLANE WAS SO BADLY CORRODED IT LOOKED AS IF THE PLANE HAD BEEN IMMERSED IN SALT WATER A
- [SDR CA141224003](https://openairdocs.org/sdr/CA141224003), Dec 23, 2014: G SWITCH. FAILED. (CAN) WHILE TESTING THE ELT ON ITS ANNUAL CERTIFICATION AS PER CAR 571 APPENDIX G FOUND G SWITCH IN UNIT WOULD NOT ACTIVATE & OUTPUT POWER LOW. UNIT REMOVED FRO
- [SDR KC2R1010201449428](https://openairdocs.org/sdr/KC2R1010201449428), Oct 15, 2014: IMPULSE COUPLING. CRACKED. DURING ROUTINE 500 HOUR INSPECTION, DISCOVERED IMPULSE COUPLING CRACKED AT FULL ADVANCE STOP ON FLYWEIGHT BASE PLATE. CRACKS DETECTED USING MAGNETIC PARTICLE ND
- [SDR 2014FA0000559](https://openairdocs.org/sdr/2014FA0000559), Sep 25, 2014: CONTROL CABLE. FRAYED. TRIM CABLE FRAY AND BROKEN, STRANS AT TRIM BARREL AT STABILIZER.
- [SDR 2014FA0000452](https://openairdocs.org/sdr/2014FA0000452), Jul 28, 2014: MUFFLER. BLOCKED. THE FORWARD MUFFLER WAS REMOVED FROM THE NR 1 AND NR 2 CYLINDERS. THE INTERIOR SURFACES OF THE LT AND RT RISERS REVEALED WHITE AND GRAY DEPOSITS CONSISTENT WITH
- [SDR 2014FA0000048](https://openairdocs.org/sdr/2014FA0000048), Jan 29, 2014: SPAR. CORRODED. CORROSION FOUND DURING A ANNUAL INSPECTION, ON INBOARD LOWER RT WING SPAR WS 44.2.
- [SDR 2014FA0000028](https://openairdocs.org/sdr/2014FA0000028), Dec 13, 2013: SKIN. CRACKED. CRACK NEAR AFT WING SPAR SPLICE, LOWER WING SKIN, FWD INBD END, LT AND RT.
- [SDR 2013FA0000301](https://openairdocs.org/sdr/2013FA0000301), May 30, 2013: SHAFT. MISMANUFACTURED. NEW SHAFT FROM MFG IS .010 UNDER DIAMETER. PART IS USED TO COMPLY AD10-15-10.
- [SDR 2014FA0000123](https://openairdocs.org/sdr/2014FA0000123), Apr 29, 2013: CYLINDER HEAD. FRACTURED. ALUMINUM CYLINDER HEAD FRACTURED CIRCUMFERENTIALLY ADJACENT TO UPPER EDGE OF STEEL CYLINDER BARREL ON 4/28/13 DESPITE A SATISFACTORY COMPRESSION CHECK (79/80) 4
- [SDR 2013FA0000113](https://openairdocs.org/sdr/2013FA0000113), Feb 10, 2013: DISTRIBUTOR BLK. INOPERATIVE. PILOT COMPLAINED OF ROUGH ENGINE & LOSS OF POWER. GROUND RUN DETERMINED THAT THE RT MAGNETO WAS CAUSING PROBLEM. ENSURED RT WAS CORRECT POSITION ON SWITCH. PULL
- [SDR CA120625002](https://openairdocs.org/sdr/CA120625002), Jun 7, 2012: LEG ASSY. CRACKED. (CAN) DURING INSPECTION IAW SB 1131, RT MLG LEG WAS FOUND CRACKED AT THE UPPER INBD TORQUE LINK ATTACH LUG. THIS LG STRUT CYLINDER WAS CAST TYPE.
- [SDR 2012FA0000338](https://openairdocs.org/sdr/2012FA0000338), May 10, 2012: LINE. LEAKING. OIL LEAK ON BACK SIDE OF FIREWALL, UNDER THE PANEL ON THE ENGINE OIL PRESSURE HARD LINE AFTER COMPLETING ENGINE CHANGE DURING FIRST ENGINE RUN-UP, FOUND EXCESSI
- [SDR REXA201200065](https://openairdocs.org/sdr/REXA201200065), Apr 27, 2012: LIGHT. UNKNOWN. FLOOR TRACK LIGHTING ASSEMBLIES IN FRONT OF LT FORWARD GALLEY NEEDS REPLACEMENT. REMOVED AND REPLACED FLOOR TRACK LIGHTING IN FRONT OF LT FORWARD GALLEY IAW CRJ
- [SDR 2012FA0000224](https://openairdocs.org/sdr/2012FA0000224), Apr 20, 2012: TRANSMITTER. ERRATIC. DURING ALL OPERATIONS, NOTICED VERY ERRATIC FUEL QUANTITY INDICATIONS FROM BOTH TANKS. DURING ANNUAL INSPECTION, MECHANIC DISCOVERED THAT THE BOTH FUEL QUANTITY
- [SDR 2012FA0000135](https://openairdocs.org/sdr/2012FA0000135), Feb 25, 2012: CYLINDER. CRACKED. DURING ANNUAL COMPRESSION TEST, CYLINDER WAS FOUND TO HAVE NO COMPRESSION. UPON FURTHER INVESTIGATION AIR WAS FOUND LEAKING FROM THE BACK OF CYLINDER ASSY AT TH
- [SDR 2012FA0000115](https://openairdocs.org/sdr/2012FA0000115), Feb 16, 2012: SELECTOR VALVE. WORN. THE FUEL TANK SELECTOR VALVE, WHEN THE VALVE WAS ROTATED, IT WAS STIFF TO MOVE AND COULD NOT FEEL THE DETENT AT EACH POSITION. A TEARDOWN OF THE VALVE SHOWED TH
- [SDR 2011FA0000524](https://openairdocs.org/sdr/2011FA0000524), Aug 16, 2011: SKIN. BUCKLED. RT WING HAS BUCKLING ON BOTTOM INBD PANELS. INSP OF INSIDE OF WING ROOT REVEALED MISSING AND INCOMPLETE BUCKED RIVETS.
- [SDR 2011FA0000190](https://openairdocs.org/sdr/2011FA0000190), Mar 11, 2011: CYLINDER. BROKEN. RT MLG LOWER STRUT FELL OFF WHEN ACFT LIFTED OFF THE RUNWAY AT 2H2. STUDENT PILOT FLEW AND LANDED RESULTING IN DAMAGE TO THE UPPER LANDING GEAR STRUT HSG. WHEN 
- [SDR CA100813008](https://openairdocs.org/sdr/CA100813008), Aug 13, 2010: HUB. CORRODED. (CAN) PROPELLER RECEIVED FOR COMPLIANCE WITH CARS, PART 6, STANDARD 625, APPENDIX C. 6. FIRST THING NOTICED WAS WHITE CORROSION POWDER IN THE 6 BOLT HOLE COUNTE
- [SDR 2010FA0000529](https://openairdocs.org/sdr/2010FA0000529), Jun 8, 2010: TORQUE LINK. BROKEN. LT MLG TORQUE LINK BROKE ABOUT 1" BELOW UPPER MOUNT AFTER LANDING. TORQUE LINK WAS SENT TO NTSB FOR TESTING WITH THE FOLLOWING REPORT. THE FATIGUE ORIGIN AREAS 
- [SDR C2XA10IA142](https://openairdocs.org/sdr/C2XA10IA142), May 9, 2010: RELAY. INOPERATIVE. IAH, FLIGHT 2170, THE CREW REPORTED EICAS MESSAGES ON ROTATION FOR ELECTRIC ABNORMAL, AND EMERGENCY LIGHTS NOT ARMED, AND ELECTRICAL SURGING ON THE FLIGHT DECK 
- [SDR CA081106005](https://openairdocs.org/sdr/CA081106005), Oct 31, 2008: BAFFLE. FAILED. (CAN) POWER LOSS ON TAKEOFF DUE TO BAFFLE FAILURE INSIDE MUFFLER WHICH RESTRICTED EXHAUST OF ENGINE CAUSING PARTIAL POWER LOSS.
- [SDR 2008FA0000725](https://openairdocs.org/sdr/2008FA0000725), Oct 29, 2008: RIB. CORRODED. DURING ANNUAL INSPECTION FOUND ALL FLAPS, LEADING EDGE RIBS WERE SEVERELY CORRODED. DETECTION METHOD WAS TO TAKE THE FOREFINGER AND THUMB AND SQUEEZE LEADING ED
- [SDR CA080919001](https://openairdocs.org/sdr/CA080919001), Sep 17, 2008: MOUNT BRACKET. CRACKED. (CAN) THE EXISTING ELT MOUNTING BRACKET WAS INSPECTED PRIOR TO REPLACEMENT OF THE VHF ELT WITH A 406 MHZ ELT. UPON REMOVING THE NARCO ELT10 MOUNTING TRAY, IT WA
- [SDR 2007FA0000820](https://openairdocs.org/sdr/2007FA0000820), Sep 24, 2007: BEARING. DESTROYED. BEARING LW14227 CAGE DESTROYED AND APPROXIMATELY 50 PERCENT MISSING. THIS IS THE ENGINE SIDE BEARING OF THE LW15416 MAGNETO DRIVE ADAPTER (MAGNETO ISOLATION DRI
- [SDR 2007FA0000819](https://openairdocs.org/sdr/2007FA0000819), Sep 24, 2007: BEARING. DESTROYED. BEARING LW14227 CAGE DESTROYED AND APPROXIMATELY 50 PERCENT MISSING. THIS IS THE ENGINE SIDE BEARING OF THE LW15416 MAGNETO DRIVE ADAPTER (MAGNETO ISOLATION DRI
- [SDR 2007FA0000526](https://openairdocs.org/sdr/2007FA0000526), Jun 15, 2007: TERMINAL. LOOSE. 217 HOURS AFTER OVERHAUL, THE OUTPUT TERMINAL BECAME LOOSE IN THE BUSS STRAP INSIDE THE ALTERNATOR, CAUSING COMPLETE FAILURE. LIKELY THIS FIT (NORMALLY A PRESS 
- [SDR 2007FA0000075](https://openairdocs.org/sdr/2007FA0000075), Jan 23, 2007: BULKHEAD. CORRODED. THE BULKHEAD, BRACKETS, AND DOUBLERS AT STA. 228.3 WERE SEVERELY CORRODED. THIS BULKHEAD IS THE FRONT SUPPORT FOR THE VERTICAL STABILIZER/RUDDER ASSEMBLY. THE C
- [SDR 2007FA0000074](https://openairdocs.org/sdr/2007FA0000074), Jan 23, 2007: BULKHEAD. CORRODED. THE BULKHEAD, BRACKETS, AND DOUBLERS AT STA. 228.3 WERE SEVERELY CORRODED. THIS BULKHEAD IS THE FRONT SUPPORT FOR THE VERTICAL STABILIZER/RUDDER ASSEMBLY. THE C
- [SDR 2006FA0000904](https://openairdocs.org/sdr/2006FA0000904), Sep 14, 2006: PUMP. LEAKING. UPON RETURNING FROM A TRAINING FLIGHT, A FAINT SMELL OF GAS WAS NOTED. SINCE THE ELECTRIC PUMP WAS ON, IT WAS TURNED OFF. NO ENGINE PERFORMANCE PROBLEMS WERE NO
- [SDR 2006FA0000905](https://openairdocs.org/sdr/2006FA0000905), Sep 14, 2006: DIAPHRAGM. RUPTURED. UPON RETURNING FROM A TRAINING FLIGHT, A FAINT SMELL OF GAS WAS NOTED. SINCE THE ELECTRIC PUMP WAS ON, IT WAS TURNED OFF. NO ENGINE PERFORMANCE PROBLEMS WERE NO
- [SDR CA061011002](https://openairdocs.org/sdr/CA061011002), Aug 30, 2006: CONNECTOR. BROKEN. (CAN) WHEN MANUAL RUDDER TRIM WAS APPLIED IN CLIMB THERE WAS NO RESPONSE. SUBSEQUENT INSPECTION FOUND THAT THE ARM THAT CONNECTS THE TRIM ACTUATOR TO THE RUDDER
- [SDR CA060925003](https://openairdocs.org/sdr/CA060925003), Aug 30, 2006: CONNECTOR. BROKEN. (CAN) WHEN MANUAL RUDDER TRIM WAS APPLIED THE RUDDER FAILED TO RESPOND. SUBSEQUENT INSPECTION FOUND THAT THE ARM THAT CONNECTS THE TRIM ACTUATOR TO THE RUDDER C

All 194: https://openairdocs.org/model/piper-anderson-pa-28-180/reports.md

## STCs that may be installed (OpenAirDocs) (399, 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 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 SA02279AT](https://openairdocs.org/stc/SA02279AT): Installation of a Boom Beam bulb, starter, and ballast. Whelen Aerospace Technologies
- [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 SA02661LA](https://openairdocs.org/stc/SA02661LA): Installation to enlarge the existing main landing gear over-wing access hole in the upper wing skin. M2 Aviation Soultions LLC
- [STC SA01147WI](https://openairdocs.org/stc/SA01147WI): Installation of Concorde FLA or VRSLA series batteries in Piper Light Airplanes. Concorde Battery Corporation
- [STC SA800EA](https://openairdocs.org/stc/SA800EA): Installation of Whelen Anti-Collision, Position, or Anti-Collision/Position Light System, and applicable associated power supplies. Whelen Aerospace Technologies
- [STC SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc
- [STC SA01866WI](https://openairdocs.org/stc/SA01866WI): Installation of Garmin GFC 500 Autopilot with Electronic Stability and Protection. Garmin International Inc
- [STC SA04075CH](https://openairdocs.org/stc/SA04075CH): Installation of Dynon EFIS-D10A EAA sales kit part number 102778-000. Dynon Avionics 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 SA5581SW](https://openairdocs.org/stc/SA5581SW): Installation of ALCOR true-flow/ totalizer system. Alcor LLC. Lists PA-28 Series
- [STC SA02168AT](https://openairdocs.org/stc/SA02168AT): Modification of engine exhaust system for improved engine performance by installation of a Laminar Flow System Extractor Exhaust System. Power Flow Systems Inc
- [STC SA316SO](https://openairdocs.org/stc/SA316SO): Carburetor ice detector. LegacySTC.com. Lists PA-28 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 SA00037WI](https://openairdocs.org/stc/SA00037WI): Installation of B & C Specialty Products BC100-1 battery. B & C Specialty Products Inc
- [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd
- [STC SA01120SE](https://openairdocs.org/stc/SA01120SE): Installation of Door Steward. Mountain View Aviation LLC
- [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 SA01757WI](https://openairdocs.org/stc/SA01757WI): To allow the use of UL91 or UL94 (minimum) grade aviation fuel. Swift Fuels LLC
- [STC SA04568CH](https://openairdocs.org/stc/SA04568CH): Installation of the uAvionix tailBeaconX, a tail mounted position light with integrated Automatic Dependent Surveillance - Broadcast (ADS-B) Out and 1090MHz Mode-S transponder functionality. uAvionix Corporation
- [STC SA01941LA](https://openairdocs.org/stc/SA01941LA): Installation of stabilizer trim handle and cabin door handle. McFarlane Aviation LLC
- [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 SA02575AK](https://openairdocs.org/stc/SA02575AK): Installation of the nose tire scraper P/N TSL-100. Aero Twin Inc
- [STC SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio. Peregrine
- [STC SA04400NY](https://openairdocs.org/stc/SA04400NY): Installation of the Integrated Back-up Battery System (IBBS). TCW Technologies LLC
- [STC SA04192NY](https://openairdocs.org/stc/SA04192NY): KFD 900 Primary Flight Display System Additional Functions. Honeywell International 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 SA11137SC](https://openairdocs.org/stc/SA11137SC): Installation of Plane-Power ALT-FLX alternator. Hartzell Engine Technologies, LLC
- [STC SA224CE](https://openairdocs.org/stc/SA224CE): Installation of Model A3000 main skis and NB-1200 nose skis. F.Atlee Dodge Aircraft Services
- [STC SA00060AT](https://openairdocs.org/stc/SA00060AT): Installation of flap gap seals. Whelen Aerospace Technologies. Lists PA-28 Series
- [STC SA00063AT](https://openairdocs.org/stc/SA00063AT): Installation of aileron gap seals. Whelen Aerospace Technologies
- [STC SA01038AT](https://openairdocs.org/stc/SA01038AT): Installation of composite construction wingtips with Hoernr chordwise section with a clear plexiglass nose enclosure for aircraft lighting. (PA-28, -28R, -32, -32R, -34 series MODELS WITH CONSTANT-CHORD WINGS). Whelen Aerospace Technologies. Lists PA-28 Series
- [STC SA02987CH](https://openairdocs.org/stc/SA02987CH): Installation of the Electroair Electronic Ignition System. Electroair Acquisition Corporation
- [STC SA1072CE](https://openairdocs.org/stc/SA1072CE): Installation of wing leading edge cuffs and droop tips, dorsal fin and vertical stabilizer vortex generator. Curry Aviation LLC
- [STC SA2156CE](https://openairdocs.org/stc/SA2156CE): Installation of flap and aileron gap seals. Curry Aviation LLC
- [STC SA2194CE](https://openairdocs.org/stc/SA2194CE): Installation of Hoerner style wing tips. Curry Aviation LLC
- [STC SA2230CE](https://openairdocs.org/stc/SA2230CE): Installation of replacement stabilator tips. Curry Aviation LLC
- [STC SA00954WI](https://openairdocs.org/stc/SA00954WI): Installation of Concorde RG Series Batteries in Piper Single Engine Airplanes. Aero-Mach Wilco LLC

All 399: https://openairdocs.org/model/piper-anderson-pa-28-180/stcs.md

## PMA parts (OpenAirDocs) (over 1,000, 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.

- [A63300-016W](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID182894196620260909135052.0001): Horn Assembly, Nose Wheel Steering, White. Aerospace Welding Minneapolis, Inc. · PMA PQ2712CE · Replaces 63300-000, 63300-008, 63300-014… · Aug 6, 2026
- [A63300-016B](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID152416243620260909135052.0001): Horn Assembly, Nose Wheel Steering, Black. Aerospace Welding Minneapolis, Inc. · PMA PQ2712CE · Replaces 63300-000, 63300-008, 63300-014… · Aug 6, 2026
- [MC65887-000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID160671399220260722173231.0001): BLOCK ASSEMBLY. Airforms LLC · PMA PQ2644CE · Replaces 65887-000 · Jul 21, 2026
- [MC79220-900](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID141429774720260722173232.0001): NOSE FORK ASSY. Airforms LLC · PMA PQ2644CE · Replaces 79220-900, 79220-800 · Jul 21, 2026
- [MC79110-003](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID129580956620260722173231.0001): NOSE FORK ASSEMBLY. Airforms LLC · PMA PQ2644CE · Replaces 79110-003 · Jul 21, 2026
- [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
- [066-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID120510874920260723131534.0001): Rivet. Game Aerospace, LLC · PMA PQ00052CB · Replaces Cleveland Wheels and Brakes P/N… · Jun 9, 2026
- [210608](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID126781545220260701191843.0001): G35 Foam Insert. EarthX, Inc. · PMA PQ05466NM · Modification part · Jun 4, 2026
- [RAP164-01900](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180304311520260722154717.0001): Brake Disc. Rapco Inc. · PMA PQ2101CE · Replaces 164-01900 · Jun 3, 2026
- [RAP164-00500](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139460967420260722154712.0001): Brake Disc. Rapco Inc. · PMA PQ2101CE · Replaces 164-00500 · Jun 3, 2026
- [SSV35-231553-4M](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184970016620260713144517.0001): ROD END BEARING. McFarlane Aviation Inc. · PMA PQ3732CE · Replaces 131553-4M, 452-383, 452-860, HM4… · May 4, 2026
- [SSV35-231765-1M](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID142043761020260713144519.0001): ROD END BEARING. McFarlane Aviation Inc. · PMA PQ3732CE · Replaces 452-334, 452-357, M34-14, M34-14M · May 4, 2026
- [SSV35-231765-1F](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132699716920260713144519.0001): ROD END BEARING. McFarlane Aviation Inc. · PMA PQ3732CE · Replaces 131765-1F, 452-335, F34-14, F34-14… · May 4, 2026
- [SSV35-231765-L1F](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID104549240720260713144520.0001): ROD END BEARING. McFarlane Aviation Inc. · PMA PQ3732CE · Replaces 452-336, FL34-14 · May 4, 2026
- [AFC301002-0103](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172761002820260612142644.0001): Motor, Actuator. Airforms LLC · PMA PQ2644CE · Replaces 761-519761 519 · May 1, 2026
- [AFC301002-0103](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID159550390120260612142643.0001): Motor, Actuator. Airforms LLC · PMA PQ2644CE · Replaces C145-200 · May 1, 2026
- [60-79445-80A](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178118516920251125152237.0001): Rear Bulkhead Door. Texas Aeroplastics · PMA PQ03888SW · Replaces 79445-00,79445-000 · Nov 20, 2025
- [28-TL-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID120616516320260423211201.0001): Leaded and 
Unleaded 
automotive 
gasoline. Air Plains Services Corp · PMA PQ3524CE · Modification part · Aug 29, 2025
- [28-TL-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID105007958120260423211201.0001): Leaded and 
Unleaded 
automotive 
gasoline. Air Plains Services Corp · PMA PQ3524CE · Modification part · Aug 29, 2025
- [AE945](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137768050120250908153028.0001): Rotor Shaft. Aerospace Turbine Rotables · PMA PQ3736CE · Replaces Prestolite Part Number ALE-277 · Aug 27, 2025
- [RAP164-02000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID117298395720250829181749.0001): Brake Disc. Rapco Inc · PMA PQ2101CE · Replaces 164-02000 Cleveland · Aug 27, 2025
- [A63300-016](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID105253473120250724121526.0001): Horn Assembly, Nose Wheel Steering. Aerospace Welding Minneapolis, Inc. · PMA PQ2712CE · Replaces 63300-000, 63300-008, 63300-014… · Jun 23, 2025
- [P002-1247130-A011](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID192575457920250610210918.0001): Spinner Assembly. Aero Tech Aviation Design, LLC · PMA PQ04281CE · Replaces 63760-04, 65805-00,D-3328 · May 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
- [SC-W/T-1041](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID189780454920250328114128.0001): Piper Storm Vent Window - Metal Frame Type (Solar Control Green). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 21027-04 · Feb 27, 2025
- [SC-W/G-1041](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID173696917020250328114128.0001): Piper Storm Vent Window - Metal Frame Type (Solar Control Gray). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 21027-04 · Feb 27, 2025
- [SC-W/T-1041-250](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169687815120250328114129.0001): Piper Storm Vent Window - Metal Frame Type (.250” Solar Control Green). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 21027-04 · Feb 27, 2025
- [SC-W/G-1041-250](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID123968167420250328114130.0001): Piper Storm Vent Window - Metal Frame Type (.250” Solar Control Gray). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 21027-04 · Feb 27, 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
- [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
- [CJ33963-02](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID160083325720240625133916.0001): BRACKET ASSEMBLY. McFarlane Aviation Inc. · PMA PQ3732CE · Replaces 33963-02 · Mar 14, 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
- [MDL103216-000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133870189020240221143427.0001): SkyView HDX Instrumentation. Dynon Avionics, Inc. · PMA PQ05359NM · Modification part · Jan 26, 2024
- [TAU03323](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID194359759020240221143039.0001): AV/Cabin Heat Kit. Hartzell Propeller LLC · PMA PQ2040CE · Modification part · Dec 14, 2023
- [01-7079-24](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168735715720231108124804.0001): LIGHT-ASSY, StarLight. AeroLEDs LLC · PMA PQ5259NM · Replaces WA7079B-24NLI7079-24CMA-7079B-24A7079B… · Nov 3, 2023
- [TSL-100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID123406381820230906211240.0001): Nose Tire Scraper. Aero Twin Inc · PMA PQ2503CE · Modification part · Aug 29, 2023
- [PCW-601-103](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145853679620230823125036.0001): Control Wheel. Custom Aircraft Services · PMA PQ5436NM · Replaces 62818-0062824-00 · Aug 16, 2023
- [PCW-601-101](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID105071834020230823125032.0001): Control Wheel. Custom Aircraft Services · PMA PQ5436NM · Replaces 85292-0785292-0985292-01085292-02210057… · Aug 16, 2023
- [UAV-1004236-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179059944320230707211347.0001): AV-30-C. uAvionix Corporation · PMA PQ05445NM · Modification part · Jun 28, 2023
- [AF67769-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID160617906520230511175842.0001): WINTERIZATION CLOSURE ASSEMBLY. Airforms LLC · PMA PQ2644CE · Replaces 67769-00 · May 2, 2023
- [AF99578-01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID143174717520230511175840.0001): LH FWD INBOARD BAFFLE ASSEMBLY. Airforms LLC · PMA PQ2644CE · Modification part · May 2, 2023
- [AF99771-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID102107349620230511175841.0001): RH FWD INBOARD BAFFLE ASSEMBLY. Airforms LLC · PMA PQ2644CE · Replaces 99771-00 · May 2, 2023
- [8100-065](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID189478147320240229155225.0001): 60 in-lb. PMA Servo 24V. Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Replaces 8100-065 · Nov 18, 2022
- [8200-141](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID185883423620240229155220.0001): Piper PA28 Kit Parts. Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Replaces 8200-141 · Nov 18, 2022
- [8100-064](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178963419020240229155224.0001): 60 in-lb. PMA Servo 12V. Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Replaces 8100-064 · Nov 18, 2022
- [8000-174](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171620492620240229155221.0001): Vizion PMA 2 Inch. Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Replaces 8000-174 · Nov 18, 2022
- [8000-176](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID160691672620240229155222.0001): Vizion PMA 3 Inch. Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Replaces 8000-176 · Nov 18, 2022
- [8000-175](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID151385150220240229155221.0001): VizionPMA Flat. Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Replaces 8000-175 · Nov 18, 2022

All of them: https://openairdocs.org/model/piper-anderson-pa-28-180/pma.md

## The same model under other registry codes

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

- [Piper PA-28-180](https://openairdocs.org/model/piper-pa-28-180): 3,504 registered aircraft, registry code 7102808

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