# Piper PA-60-601P

- Type: Aircraft model (FAA registry)
- Registry code: 7106016
- Manufacturer (registry): PIPER AIRCRAFT CORPORATION
- Model: PA-60-601P
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Reciprocating
- Seats: 6
- Weight class: Up to 12,499 lb
- Certification: Type certificated
- Data sheet: [TCDS A17WE](https://openairdocs.org/tcds/A17WE) (OpenAirDocs)
- Holder: Aerostar Aircraft Corporation
- Registered aircraft: 9
- Page: https://openairdocs.org/model/piper-pa-60-601p

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 2023-09-09](https://openairdocs.org/ad/2023-09-09): Exhaust Turbine System (Recip) · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 292 more. Effective Jul 17, 2023
- [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 2020-24-10](https://openairdocs.org/ad/2020-24-10): Flight Controls · Aerostar PA-60-601P (Aerostar 601P), PA-60-602P (Aerostar 602P) and PA-60-700P (Aerostar 700P). Effective Jan 22, 2021
- [AD 2005-18-20](https://openairdocs.org/ad/2005-18-20): "FASTprop" propeller de-icers · Hartzell PHC-C3YF-1RF/F8468A(B,K)-8R constant speed propeller (STC SA00718LA or 17 others). Effective Oct 14, 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 2003-22-01](https://openairdocs.org/ad/2003-22-01): Auxiliary fuel transfer pumps · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 2 more. Effective Nov 17, 2003
- [AD 2002-24-07](https://openairdocs.org/ad/2002-24-07): Roto-Master and Rajay scavenge pumps · Aerostar PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P), PA-60-602P (Aerostar 602P) and 1 more. Effective Jan 17, 2003
- [AD 2001-08-10](https://openairdocs.org/ad/2001-08-10): Main Landing Gear Lower Side Brace Assemblies · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 2 more. Effective Jun 12, 2001
- [AD 98-24-29](https://openairdocs.org/ad/98-24-29): Wing Upper Spar Cap · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 2 more. Effective Jan 8, 1999
- [AD 98-04-23](https://openairdocs.org/ad/98-04-23): AFM - Limitations Section - Icing · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 2 more. Effective Mar 13, 1998
- [AD 95-23-11](https://openairdocs.org/ad/95-23-11): Upper And Lower Horizontal Flanges · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 1 more. Effective Nov 30, 1995
- [AD 94-15-13](https://openairdocs.org/ad/94-15-13): Nose Landing Gear Drag Link Assembly · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 2 more. Effective Sep 12, 1994
- [AD 93-13-08](https://openairdocs.org/ad/93-13-08): Torque Links · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 2 more. Effective Aug 20, 1993
- [AD 90-01-02](https://openairdocs.org/ad/90-01-02): Service Bulletin 920 - Fire Prevention · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 2 more. Effective Mar 1, 1990
- [AD 89-03-04](https://openairdocs.org/ad/89-03-04): Cabin Door · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 2 more. Effective Feb 24, 1989
- [AD 88-25-02](https://openairdocs.org/ad/88-25-02): Engine Fluid-Carrying Hoses · Aerostar PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P), PA-60-602P (Aerostar 602P) and 1 more. Effective Dec 26, 1988
- [AD 88-21-05](https://openairdocs.org/ad/88-21-05): Exhaust Systems (STC SA980NM) · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 2 more. Effective Nov 6, 1988
- [AD 87-21-01](https://openairdocs.org/ad/87-21-01): Fuel Filler Openings · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 14 more. Effective Nov 2, 1987
- [AD 87-07-09](https://openairdocs.org/ad/87-07-09): Exhaust System Components · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 2 more. Effective May 15, 1987
- [AD 83-14-07 R3](https://openairdocs.org/ad/83-14-07-R3): Limitations Section -- CG Limit · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 1 more. Effective Nov 25, 1983
- [AD 80-18-03](https://openairdocs.org/ad/80-18-03): Fuel Pressure System · Aerostar PA-60-601 (Aerostar 601) and PA-60-601P (Aerostar 601P). Effective Oct 6, 1980
- [AD 80-19-14](https://openairdocs.org/ad/80-19-14): Horizontal/Vertical Stabilizer · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601) and PA-60-601P (Aerostar 601P). Effective Sep 25, 1980
- [AD 80-17-04](https://openairdocs.org/ad/80-17-04): Fuel Flow Transducers · Aerosonic Fuel Flow Transducers, PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601) and 9 more. Effective Aug 13, 1980
- [AD 80-12-14](https://openairdocs.org/ad/80-12-14): Engine Fire · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601) and PA-60-601P (Aerostar 601P). Effective Jun 19, 1980
- [AD 79-01-05](https://openairdocs.org/ad/79-01-05): Fuel Starvation · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601) and PA-60-601P (Aerostar 601P). Effective Dec 27, 1979
- [AD 79-08-05](https://openairdocs.org/ad/79-08-05): Engine Nacelles · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601) and PA-60-601P (Aerostar 601P). Effective May 24, 1979
- [AD 78-18-05](https://openairdocs.org/ad/78-18-05): Wing Tank Fuel Quantity Indicator · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601) and PA-60-601P (Aerostar 601P). Effective Sep 13, 1978
- [AD 74-25-02](https://openairdocs.org/ad/74-25-02): Electrical Attitude And Directional Gyros · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601) and PA-60-601P (Aerostar 601P) with STC SA2336WE or SA2367WE. Effective Dec 4, 1974

## Information bulletins (advisory) (2)

- [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018
- [SAIB CE-03-55](https://openairdocs.org/saib/CE-03-55): . Issued Sep 18, 2003

## Registered aircraft (9)

- [N1225](https://openairdocs.org/aircraft/N1225): [Fox R Bruce](https://openairdocs.org/faa-owner/FOX%20R%20BRUCE), [Kennesaw, GA](https://openairdocs.org/faa-place/GA/Kennesaw), S/N 61P05727963249
- [N144SJ](https://openairdocs.org/aircraft/N144SJ): [Trigger Down LLC](https://openairdocs.org/faa-owner/TRIGGER%20DOWN%20LLC), [Virginia Beach, VA](https://openairdocs.org/faa-place/VA/Virginia%20Beach), built 1978, S/N 61P-0545-233
- [N3635A](https://openairdocs.org/aircraft/N3635A): [Caljet Inc](https://openairdocs.org/faa-owner/CALJET%20INC), [Van Nuys, CA](https://openairdocs.org/faa-place/CA/Van%20Nuys), built 1980, S/N 61P07748063387
- [N601NG](https://openairdocs.org/aircraft/N601NG): [Bullard Aviation Services Inc](https://openairdocs.org/faa-owner/BULLARD%20AVIATION%20SERVICES%20INC), [Ormond Beach, FL](https://openairdocs.org/faa-place/FL/Ormond%20Beach), built 1980, S/N 61P07908063402
- [N601P](https://openairdocs.org/aircraft/N601P): [Schmidt Richard E](https://openairdocs.org/faa-owner/SCHMIDT%20RICHARD%20E), [Fort Myers, FL](https://openairdocs.org/faa-place/FL/Fort%20Myers), built 1979, S/N 61P06587963306
- [N65966](https://openairdocs.org/aircraft/N65966): built 1990, S/N 0534226
- [N69LP](https://openairdocs.org/aircraft/N69LP): [Southern Aircraft Consultancy Inc Trustee](https://openairdocs.org/faa-owner/SOUTHERN%20AIRCRAFT%20CONSULTANCY%20INC%20TRUSTEE), [Casper, WY](https://openairdocs.org/faa-place/WY/Casper), built 1978, S/N 61P-0541-0230
- [N728RT](https://openairdocs.org/aircraft/N728RT): [Burnside Jack](https://openairdocs.org/faa-owner/BURNSIDE%20JACK), [Rockwall, TX](https://openairdocs.org/faa-place/TX/Rockwall), built 1978, S/N 61P05627963243
- [N86AT](https://openairdocs.org/aircraft/N86AT): [86at LLC](https://openairdocs.org/faa-owner/86AT%20LLC), [Elizabethtown, PA](https://openairdocs.org/faa-place/PA/Elizabethtown), built 1976, S/N 61P-0364-114

## NTSB investigations (3)

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 CEN25LA398](https://openairdocs.org/ntsb/CEN25LA398), Sep 27, 2025: Piper PA-60-601P (N3635A), Del Norte, CO, substantial damage. Probable cause: The loss of directional control during landing roll due to a flat tire.
- [NTSB WPR22LA272](https://openairdocs.org/ntsb/WPR22LA272), Jul 13, 2022: Piper PA-60-601P (N601NG), Scappoose, WA, substantial damage. Probable cause: The pilot’s failure to extend the landing gear before landing. Contributing to the accident was the pilot’s failure to utilize a prelanding checklist.
- [NTSB IAD96LA089](https://openairdocs.org/ntsb/IAD96LA089), Jun 3, 1996: Piper PA60-601P (N86AT), Willard, OH, substantial damage. Probable cause: the pilot's inability to maintain directional control of the airplane during the landing flare/touchdown.

## FAA accident and incident reports (9)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Accident 20250927019709A](https://openairdocs.org/incident/20250927019709A), Sep 27, 2025: Piper Aircraft Corporation PA-60-601P (N3635A), Del Norte, CO, Substantial damage. On September 27, 2025, a Piper PA60 aircraft lost directional control on rollout from landing on runway 24 at krcv due to an undetected tire failure that…
- [Accident 20220712012469A](https://openairdocs.org/incident/20220712012469A), Jul 12, 2022: Piper Aircraft Corporation PA-60-601P (N601NG), Scappoose, OR, Substantial damage. On July 12, 2022, about 1901 pacific daylight time, an Aerostar, [privacy data omitted] sustained substantial damage when it landed gear up at the Scappoose…
- [Incident 20071116827209I](https://openairdocs.org/incident/20071116827209I), Nov 16, 2007: Piper PA60601P (N111RD), Latrobe, PA, No damage. (-23) Right engine oil pressure dropped followed by drop in manifold pressure. Pilot shut down engine, feathered propeller, and initiated emergency landing at…
- [Incident 20051231031029I](https://openairdocs.org/incident/20051231031029I), Dec 31, 2005: Piper PA60601P (N3635A), Portsmouth, NH, Minor damage. (-23) Pilot in command departed his home base beverly, ma (bvy), with a destination of Pease international tradeport (psm), in Portsmouth, NH, purpose of the…
- [Incident 20000122002709I](https://openairdocs.org/incident/20000122002709I), Jan 22, 2000: Piper PA60601P (N312BA), St Augustine, FL, Minor damage. (-5) On January 22, 2000, Mr. Robert allison, pilot and owner of Aerostar N312BA, forgot to extend his landing gear during landing on runway 13 at st.…
- [Incident 19991016029839I](https://openairdocs.org/incident/19991016029839I), Oct 16, 1999: Piper PA60601P (N601NG), Harrisburg, PA. (-23) On oct. 16, 1999, at 1630 hours (local), a Piper PA-60-601P, N601NG, registered to gryphon aviation inc., departed Capital City Airport (cxy). On…
- [Accident 19960603012599A](https://openairdocs.org/incident/19960603012599A), Jun 3, 1996: Piper PA60601P (N86AT), Willard, OH, Substantial damage. On final approach yawed to left, landed, rolled into soft turf, right gear collapsed, wing tip and prop hit ground. (.4) according to the pilot, when the…
- [Incident 19931015045069I](https://openairdocs.org/incident/19931015045069I), Oct 15, 1993: Piper PA60601P (N3635A), Southern Pines, NC, Minor damage. Pilot stated he forgot to lower landing gear. Landed gear u.
- [Incident 19880331019459I](https://openairdocs.org/incident/19880331019459I), Mar 31, 1988: Piper PA60601P (N111RD), Danbury, CT, Minor damage. Aircraft pulled to left with sparks from gear on landing. Left upper main gear torque links had broken.

## Service difficulty reports (64, newest 50)

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

- [SDR 2017FA0000171](https://openairdocs.org/sdr/2017FA0000171), May 3, 2017: EXHAUST PIPE. BROKEN. CLIMBING THROUGH 13,000 MSL THE PILOT REPORTED A LOSS IN MANIFOLD PRESSURE ON THE LT ENGINE. RETURNED TO THE AIRPORT FOR A NORMAL LANDING. DURING INSPECTION, FO
- [SDR HX1R2016041230269](https://openairdocs.org/sdr/HX1R2016041230269), Mar 10, 2016: STUD. BROKEN. DURING INSPECTION, SAW NR 3 CYLINDER WITH ALL OF THE HOLDDOWN STUDS BROKEN OFF. THE CYLINDER MOVED IN AND OUT AND BROKE CONNECTION ROD, PUSH ROD TUBES, FUEL INJ
- [SDR 2015FA0000173](https://openairdocs.org/sdr/2015FA0000173), Apr 27, 2015: ENGINE. FAILED. PILOT REPORTED THAT IN FLIGHT, ENGINE MADE SOME NOISES FOLLOWED BY LOSS OF ENGINE POWER, LT ENGINE. PROP WENT TO UN-COMMANDED FEATHER WITH A SUDDEN INCREASE IN 
- [SDR 2012FA0000303](https://openairdocs.org/sdr/2012FA0000303), Mar 27, 2012: VALVE SPRING. BROKEN. LT ENGINE, AFTER NOTICING MANIFOLD PRESSURE SPLITS, AND A COLD RUNING NR 3 CYLINDER, INSPECTED AND FOUND INNER AND OUTER EXHAUST VALVE SPRINGS BROKEN. REPLACED 
- [SDR 2012FA0000302](https://openairdocs.org/sdr/2012FA0000302), Mar 27, 2012: VALVE SPRING. BROKEN. NOTICED MANIFOLD PRESSURE SPLITS ON LEFT ENGINE, AND A COLD RUNNING NR 3 CYLINDER, INSPECTED AND FOUND INNER AND OUTER EXHAUST VALVE SPRINGS BROKEN. REPLACED BO
- [SDR CA101122016](https://openairdocs.org/sdr/CA101122016), Nov 18, 2010: BELLOWS. DETACHED. (CAN) DURING CRUISE FLIGHT, RT ENGINE LOST POWER. PILOT ELECTED TO RETURN TO AIRPORT OF DEPARTURE (WINDSOR AIRPORT). PILOT CONDUCTED A POST FLIGHT RUN UP AND ON
- [SDR 2010FA0000809](https://openairdocs.org/sdr/2010FA0000809), Jul 29, 2010: FITTING. CORRODED. OWNER STATED HE WAS CRUISING AT ALTITUDE, TAKING ON ICE, ACTIVATED THE DE-ICE BOOT FUNCTION AND THE ICE WAS NOT REMOVED FROM THE ACFT. AFTER MULTIPLE TRIES HE W
- [SDR 2008FA0000044](https://openairdocs.org/sdr/2008FA0000044), Jan 11, 2008: PUSHROD. CORRODED. THE AREA IN WHICH THE CORRODED SECTION OF THE PUSHROD ASSY IS LOCATED IS PRONE TO EXHAUST CONTAMINATION SINCE IT IS DIRECTLY BEHIND THE ENGINE EXHAUST PIPE OUTL
- [SDR IPM2006F00001](https://openairdocs.org/sdr/IPM2006F00001), Jul 6, 2006: MAGNETO. SEPARATED. INSTALLED MAGENTO IAW MM AND GROUND CHECK OK. PILOT REPORTED HIGH CHT AND EGT NR 2 CYLINDER DURING CLIMB ON FIRST TAKEOFF. FOUND BODY OF MAGNETO SEPARATED FROM 
- [SDR 2006FA0000071](https://openairdocs.org/sdr/2006FA0000071), Jan 2, 2006: CYLINDER. CRACKED. COLLAR SEPARATING FROM TUBE DUE TO INSUFFICIENT PENETRATION WHEN PART WAS FURNACE BRAZED OR SILVER SOLDERED TOGETHER WORKING COLLAR CAUSED PART TO WORK AND CRAC
- [SDR 2005FA0001271](https://openairdocs.org/sdr/2005FA0001271), Nov 18, 2004: COLLAR. SEPARATED. COLLAR SEPARATING FROM TUBE DUE TO INSUFFICIENT PENETRATION WHEN PART WAS FURNACE BRAZED OR SILVER SOLDERED TOGETHER, WORKING COLLAR CAUSED PART TO WORK AND CRA
- [SDR AUS20040174](https://openairdocs.org/sdr/AUS20040174), Mar 9, 2004: BELLCRANK. BROKEN. (AUS) RT MAIN LANDING GEAR DOOR BELLCRANK LUG BROKEN.
- [SDR 2003FA0001006](https://openairdocs.org/sdr/2003FA0001006), Aug 29, 2003: CRANKSHAFT. BROKEN. CRANK BROKE ON NR 4 AND NR 6 CHEEK.
- [SDR GH62003F00000](https://openairdocs.org/sdr/GH62003F00000), May 2, 2003: WINDOW. FAILED. WHILE CLIMBING OUT AFTER TAKEOFF, AT APPROX 20,000 FT, CO-PILOT WINDOW EXPERIENCED A CATASTROPHIC FAILURE. WINDOW SHARDS CONTACTED RT PROPELLER. PARTIALLY RIPPI
- [SDR LER2003F00000](https://openairdocs.org/sdr/LER2003F00000), Feb 3, 2003: DUCT. CHAFED. THE ALUMINUM U-SHAPED DUCT CONNECTING THE FUEL SERVO TO THE INTER COOLER WAS FOUND TO BE CHAFING ON THE EXHAUST PIPE ON BOTH ENGINES. UPON FURTHER INSPECTION TH
- [SDR DY12002F00000](https://openairdocs.org/sdr/DY12002F00000), Nov 6, 2002: ROD END. BROKEN. AFTER AIRCRAFT MADE AN UNEVENTFUL LANDING PILOT NOTICED THAT LEFT GEAR DOWN LIGHT WAS BLINKING ON AND OFF WITH SUBSEQUENT ACTIVATION OF GEAR WARNING HORN WHEN L
- [SDR AUS20020457](https://openairdocs.org/sdr/AUS20020457), May 13, 2002: SHAFT. CRACKED. (AUS) NOSE LANDING GEAR STRUT TORQUE TUBE SHAFT CRACKED FROM BOLT HOLE. FOUND DURING MAGNAFLUX INSPECTION.
- [SDR GXPA0202](https://openairdocs.org/sdr/GXPA0202), Apr 16, 2002: EXHAUST PIPE. LOOSE. AIRCRAFT LANDED DUE TO FIRE WARNING ON LEFT ENGINE. FOUND OUTBOARD EXHAUST TUBE CLAMP CAME LOOSE AND EXHAUST TUBE WAS HANGING FROM TURBOCHARGER. REINSTALLED TUB
- [SDR AUS20020326](https://openairdocs.org/sdr/AUS20020326), Apr 5, 2002: SWITCH. INTERMITTENT. (AUS) NOSE LANDING GEAR STEERING SWITCH INTERMITTENT IN OPERATION.BRAKE CALIPERS LEAKING.
- [SDR CA020228016](https://openairdocs.org/sdr/CA020228016), Feb 2, 2002: HOSE. RUPTURED. (CAN) TURBO OIL SUPPLY HOSE FROM OPTIONAL FILTER P/N 300180-501 TO WAISTGATE ACTUATOR ROUTED IN CLOSE PROXIMITY TO EXHAUST PIPES WITH SHARP BENDS DUE TO EXTREMI
- [SDR 2002FA0000204](https://openairdocs.org/sdr/2002FA0000204), Jan 16, 2002: CRANKCASE. CRACKED. CRANKCASE FAILED NEAR NR 2 CYLINDER, CRACKED FROM IN FRONT OF CYLINDER RADIALLY BELOW AND AROUND TO THE REAR OF THE CYLINDER. CRACK EXTENDS MORE THAN 180 DEGREE
- [SDR 2001FA0000107](https://openairdocs.org/sdr/2001FA0000107), Jun 26, 2001: CRANKSHAFT. BROKEN. ENGINE FAILED ON TAKE OFF. FACTORY REP. REPORTED BY PHONE THAT CRANKSHAFT HAD BROKEN.
- [SDR CA010219004](https://openairdocs.org/sdr/CA010219004), Dec 22, 2000: SPARK PLUG. SEPARATED. (CAN) THIS ENGINE HAD APPROXIMATELY 16 MINUTES AFTER ENGINE OVERHAUL. THIS WAS ON NR 2 ENGINE THAT THE SPARK PLUG SEPARATED. WE THEN REMOVED ALL SPARK PLUGS IN 
- [SDR 20010402CW003](https://openairdocs.org/sdr/20010402CW003), Jun 9, 2000: BUCKLE. DEFECTIVE. BACK SIDE, OUTER RADIUS FOR BELT CUT OUT. CRACKS AT CORNERS OF SLOT. BUCKLE MADE OF ALUMINUM.
- [SDR 20000508SH021](https://openairdocs.org/sdr/20000508SH021), Apr 4, 2000: BEARING. CRACKED. CRACK INDICATION ON BOTH SIDES OF BEARING. (X)
- [SDR 20000407SH018](https://openairdocs.org/sdr/20000407SH018), Feb 28, 2000: BEARING. CRACKED. CRACK INDICATION. (X)
- [SDR 99ZZZX3309](https://openairdocs.org/sdr/99ZZZX3309), Aug 2, 1999: CAM FOLLOWER. LOOSE. PILOT REPORTED DEAD MAGNETO ON SECOND LEG OF TRIP. MAGNETO REMOVED AND BREAKER COMPARTMENT INSPECTED REVEALING THE CAM FOLLOWER ON THE CONTACT POINTS WAS NO LON
- [SDR 99ZZZX3003](https://openairdocs.org/sdr/99ZZZX3003), Jul 1, 1999: ENCODER. FAILED. FIRST, FOUND TRANSPONDER HAD BROKEN WIRE. THEN FOUND ENCODER WAS FAULTY, TESTED OK AFTER OVERHAUL, BUT DEFECTIVE AGAIN. REPLACED. CHECKED OK.
- [SDR 99ZZZX3002](https://openairdocs.org/sdr/99ZZZX3002), Jul 1, 1999: TRANSPONDER. FAILED. FIRST, FOUND TRANSPONDER HAD BROKEN WIRE. THEN FOUND ENCODER WAS FAULTY, TESTED OK AFTER OVERHAUL, BUT DEFECTIVE AGAIN. REPLACED. CHECKED OK.
- [SDR 20000714SH027](https://openairdocs.org/sdr/20000714SH027), Jun 24, 1999: FITTING. CORRODED. DURING ANNUAL INSPECTION, FOUND SEVERAL AREAS THROUGHOUT AIRFRAME HAVE SURFACE CORROSION STARTING. RIGHT WING GEAR AFT SIDE BRACE SUPPORT FITTING HAS INTERGRANU
- [SDR AU990707](https://openairdocs.org/sdr/AU990707), Jun 17, 1999: COLLAR. CRACKED. (AUS) NOSE LANDING GEAR STEERING COLLAR FAILED AT THE STEERING ACTUATING MECHANISM ATTACHMENT LUG. INVESTIGATION FOUND THAT THE CRACK HAD EXISTED FOR SOME TIME 
- [SDR 98ZZZX4183](https://openairdocs.org/sdr/98ZZZX4183), Oct 21, 1998: HORN. CRACKED. ELEVATOR HORN CRACKED ON PLATE .1250 INCH FROM COLLAR RADIATING FROM TRIM CABLE HOLE AROUND COLLAR. TOTAL CRACK LENGTH IS ONE INCH.
- [SDR 99ZZZX1119](https://openairdocs.org/sdr/99ZZZX1119), Oct 14, 1998: RELAY. FAILED. BATTERY MASTER RELAY PRIMARY COIL FAILED (SHORTED), HAD NO CIRCUIT PROTECTION. CONTROL WIRE TOOK HEAVY CURRENT AND BURNED THE LENGTH OF FUSELAGE TO MASTER SWITC
- [SDR CA981013013](https://openairdocs.org/sdr/CA981013013), Jul 28, 1998: BRACE. CRACKED. (CAN) ON LANDING ROLL-OUT AT ABOUT 40 KNOTS, THE WARNING HORN SOUNDED AND THE LEFT WING STARTED TO DROP. LEFT ENGINE SHUTDOWN, A/C STAYED ON RUNWAY. LEFT GEAR C
- [SDR AU980916](https://openairdocs.org/sdr/AU980916), Jul 28, 1998: PUSHROD. LOOSE. (AUS) AILERON CONTROL SYSTEM PUSHROD LOWER END FITTING RIVETS LOOSE.
- [SDR 98ZZZX3175](https://openairdocs.org/sdr/98ZZZX3175), Jun 18, 1998: PULLEY. FAILED. PILOT REPORTED THE RT ENGINE ALTERNATOR WAS NOT CHARGING. INSPECTION REVEALED THE ALTERNATOR AND AIR CONDITIONING COMPRESSOR BELTS WERE SHREDDED AND BROKEN. FUR
- [SDR 98ZZZX1114](https://openairdocs.org/sdr/98ZZZX1114), Mar 16, 1998: ALTERNATOR. FAILED. OVERHAULED ALTERNATOR FROM ELECTROSYSTEMS FAILED 3 HOURS INTO FIRST FLIGHT AFTER INSTALLING. (INTERNAL FAILURE).
- [SDR 98ZZZX909](https://openairdocs.org/sdr/98ZZZX909), Jan 24, 1998: CRANKSHAFT. FAILED. PILOT (OWNER) DEPARTING FROM AIRPORT AND CLIMBING THROUGH 4,000 FEET NOTED LOUD BANG AND SEVERE VIBRATION FROM LT ENGINE. ENGINE SHUT DOWN AND SECURED AND SAFE 
- [SDR 98ZZZX773](https://openairdocs.org/sdr/98ZZZX773), Jan 24, 1998: CRANKSHAFT. FAILED. PILOT (OWNER) DEPARTING FROM AIRPORT AND CLIMBING THROUGH 4,000 FEET NOTED LOUD BANG AND SEVERE VIBRATION FROM LT ENGINE. ENGINE SHUT DOWN AND SECURED AND SAFE 
- [SDR GXPA97015](https://openairdocs.org/sdr/GXPA97015), Aug 25, 1997: FUEL SERVO. OUT OF ADJ. SDF - AIRCRAFT DEPARTED ON PART 135 TRIP. TOWER CONTACTED AIRCRAFT STATING BLACK SMOKE COMING FROM RIGHT ENGINE. PILOT RETURNED TO SDF AND LANDED WITHOUT INCIDE
- [SDR 97ZZZX1837](https://openairdocs.org/sdr/97ZZZX1837), Mar 31, 1997: TRANSCEIVER. EXCESS INTERF. UPON IFR CERTIFICATION UPGRADE OF APOLLO 2001GPS, C/W RFI TESTS. FOUND NAV COMM RADIO TO INDUCE EXCESSIVE RFI INTO GPS SYSTEM. CAUSE BEING NAV RADIO; OTHER NAV/
- [SDR 97ZZZX3467](https://openairdocs.org/sdr/97ZZZX3467), Mar 26, 1997: BOLT. CRACKED. DURING A ROUTINE TIRE CHANGE, ONE OF THE WHEEL BOLTS WAS FOUND CRACKED ALL THE WAY AROUND THE BOTTOM OF THE HEAD.
- [SDR 96ZZZX6155](https://openairdocs.org/sdr/96ZZZX6155), Nov 20, 1996: INJECTOR SERVO. FAILED. INJECTOR SERVO 'SHUT DOWN' DURING ACTUAL FUEL FLOW TEST', ALLOWING ONLY A DRIBBLE OF FUEL THROUGH WITH FULL THROTTLE AND FULL MIXTURE AND FUEL PUMP ON. HAD THIS
- [SDR 96ZZZX6020](https://openairdocs.org/sdr/96ZZZX6020), Nov 20, 1996: PISTON. HOLE IN SIDE. DURING TEST FLIGHT, A LARGE STREAM OF OIL, FROM OIL DOOR OF RIGHT ENGINE WAS NOTICED. SUBSEQUENTLY, ENGINE SHUT DOWN WAS PERFORMED AND AN UNEVENTFUL LANDING WAS
- [SDR AU960124](https://openairdocs.org/sdr/AU960124), Feb 5, 1996: RIVET. LOOSE. (AUS) LOWER WING SKIN TO MAIN SPAR CHERRY RIVETS LOOSE AND WORKING - SKIN IN NACELLE AREA SAGGING APPROXIMATELY 4.762MM (0.1875IN)
- [SDR 96ZZZX840](https://openairdocs.org/sdr/96ZZZX840), Jan 22, 1996: LIGHT ASSY. SHORTED. PILOT NOTICED AN ELECTRICAL ARCING WHEN PUSHING ON ANNUNCIATOR PANEL DURING A NIGHT FLIGHT. FOUND A LIGHT ASSY MOUNTED BEHIND ANNUNCIATOR PANEL, HAD INSUFFICIEN
- [SDR AU960014](https://openairdocs.org/sdr/AU960014), Jan 10, 1996: SIDE BRACE. BROKEN. (AUS) LH AND RH MAIN LANDING GEAR LOWER SIDE BRACES BROKEN AT CENTRE PIVOT POINT
- [SDR 95ZZZX6779](https://openairdocs.org/sdr/95ZZZX6779), Oct 26, 1995: ENCODE DISC. MISMFG. ATC ASKED PILOT SEVERAL TIMES TO TURN OFF THE ALTITUDE PORTION OF THE TRANSPONDER BECAUSE OF ERRONEOUS CODE. BENCH CHECKING, CODE ERRATIC AND BLANKING IN SOME Z
- [SDR 95ZZZX6414](https://openairdocs.org/sdr/95ZZZX6414), Oct 18, 1995: HOSE. LEAKING. HOSE FOUND LEAKING INSIDE FIRE SLEEVE. WHEN REMOVED, THE HOSE WAS STIFF OR MORE RIGID THAN IT SHOULD HAVE BEEN. THIS HOSE WAS AN AEROQUIP HOSE DATED 1Q92. HOSE 
- [SDR 95ZZZX6399](https://openairdocs.org/sdr/95ZZZX6399), Oct 18, 1995: HOSE. LEAKING. HOSE FOUND LEAKING INSIDE FIRE SLEEVE. HOSE FOUND STIFF OR MORE RIGID THAN EXPECTED AFTER ONLY 348 HOURS IN SERVICE. THIS HOSE WAS AN AEROQUIP HOSE DATED 1Q92 A

All 64: https://openairdocs.org/model/piper-pa-60-601p/reports.md

## STCs that may be installed (OpenAirDocs) (212, 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 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 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 SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc
- [STC SA04046CH PAGE 1](https://openairdocs.org/stc/SA04046CH%20PAGE%201): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc
- [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd
- [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 SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio. Peregrine
- [STC SA01435LA](https://openairdocs.org/stc/SA01435LA): Installation of engines modified with Firewall Forward Technologies LLC modified camshaft. Centri-Lube 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 SA02010WI](https://openairdocs.org/stc/SA02010WI): Installation of the Mid-Continent Instruments & Avionics MD23 FLEX Custom Function Display (CFD). Mid-Continent Instruments and Avionics
- [STC SA02203AK](https://openairdocs.org/stc/SA02203AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Genesys Aerosystems 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 SA04452NY](https://openairdocs.org/stc/SA04452NY): Installation of MT-Propeller Entwicklung GmbH model MTV-14-B-C-F/CF(L)188-30g 4-blade, constant speed, full feathering propellers and spinners. MT- Propeller Entwicklung GmbH
- [STC SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc
- [STC SA09856AC](https://openairdocs.org/stc/SA09856AC): Installation of BendixKing Aerowave 100 In-flight Data Link System for non-essential, non-required aircraft Cabin Systems & Equipments. Honeywell International Inc (Bendix King)
- [STC SA09902AC](https://openairdocs.org/stc/SA09902AC): Installation of BendixKing KFD 900 Flight Display System. Honeywell International Inc. (Bendix King)
- [STC SA11174SC PAGE 1](https://openairdocs.org/stc/SA11174SC%20PAGE%201): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King)
- [STC SA02265SE](https://openairdocs.org/stc/SA02265SE): Installation of a camera housing. Airborne Sensor LLC
- [STC SA02430SE](https://openairdocs.org/stc/SA02430SE): Fabrication and installation of a camera housing. Airborne Sensor LLC
- [STC SA10822SC](https://openairdocs.org/stc/SA10822SC): Installation of EFD1000 Primary Flight Display. Aspen Avionics Inc
- [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation
- [STC SA04182NY](https://openairdocs.org/stc/SA04182NY): Installation of BendixKing KA 310 Autopilot Adapter. Honeywell International Inc
- [STC SA4472NM](https://openairdocs.org/stc/SA4472NM): Installation of inflatable door seal. The Flight Shop Inc
- [STC SA09764DS](https://openairdocs.org/stc/SA09764DS): Installation of an S-TEC 01326 Digital Flight Control System (DFCS). S-TEC Corporation
- [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc
- [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation
- [STC SA1184CE](https://openairdocs.org/stc/SA1184CE): Installation of King KFC 200 2 axis(3 optional) Flight Control System with King KCS 55 (or -55A) compass and a King KI 255 (or -256) Flight Command Indicator or a KG 258 Attitude Horizon Gyro with a KC 292 Mode Controller. Honeywell International Inc
- [STC SA1530CE-D](https://openairdocs.org/stc/SA1530CE-D): Installation of King KAS 297 altitude selector option. Honeywell International Inc
- [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems. Garmin International Inc
- [STC SA03286CH](https://openairdocs.org/stc/SA03286CH): Install an electronic engine ignition system. Electroair Acquisition Corporation
- [STC SA04032CH](https://openairdocs.org/stc/SA04032CH): Install rocker switch assemblies. Electroair Acquisition Corporation
- [STC SA2207WE](https://openairdocs.org/stc/SA2207WE): Installation of electrically-driven Freon air-conditioning system. Air Comm Corporation
- [STC SA00344BO PAGE 1](https://openairdocs.org/stc/SA00344BO%20PAGE%201): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights. Whelen Aerospace Technologies
- [STC SA00744DE](https://openairdocs.org/stc/SA00744DE): Installation of the Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT31 Transponder and an approved position sensor. Peregrine
- [STC SA00765DE](https://openairdocs.org/stc/SA00765DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine
- [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation
- [STC SA02153LA-D PAGE 1](https://openairdocs.org/stc/SA02153LA-D%20PAGE%201): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc
- [STC SA02503AK](https://openairdocs.org/stc/SA02503AK): Installation of AMSAFE State of the Art Restraint System (SOARS) inflatable restraints. AMSAFE Inc
- [STC SA02013CH](https://openairdocs.org/stc/SA02013CH): Installation of Avidyne Corporation Traffic Advisory System (TAS). Avidyne Corporation
- [STC SA01828SE](https://openairdocs.org/stc/SA01828SE): Installation of J.P. Instruments (JPI) EDM-960 Primary Engine Data Management System. J. P. Instruments
- [STC SA01835WI](https://openairdocs.org/stc/SA01835WI): Installation of Trig Avionics TY-96 or TY-97 VHF Communications Radio. Peregrine

All 212: https://openairdocs.org/model/piper-pa-60-601p/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.

- [RAP164-05006](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID173488801620260722154724.0001): Brake Disc. Rapco Inc. · PMA PQ2101CE · Replaces 164-05006 · Jun 3, 2026
- [MDL TD 031851](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID118069681220250508133537.0001): VA-1A( )AndAccessories. Electronics International Inc · PMA PQ0088NM · Modification part · Apr 10, 2025
- [20002A](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID105416877020250303152537.0001): Air-Oil Cooler. Boyd Niagara LLC · PMA PQ0872NE · Replaces 8526250 · Oct 30, 2024
- [01-7079-24](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID136170424120231108124805.0001): LIGHT-ASSY, StarLight. AeroLEDs LLC · PMA PQ5259NM · Replaces WA7079B-24NLI7079-24CMA-7079B-24A7079B… · Nov 3, 2023
- [APS68-01700](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID131577670320231102131428.0001): Shim, Brake. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 068-01700 · Sep 25, 2023
- [UAV-1004236-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179760513020230707211220.0001): AV-30-C. uAvionix Corporation · PMA PQ05445NM · Modification part · Jun 28, 2023
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195100709020220706160036.0001): Whelen Aerospace Technologies · PMA PQ1372CE · Jun 21, 2022
- [EA-22000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID187055246220220525194331.0001): Controller Wire Harness (14 Pin). Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Apr 25, 2022
- [EA-21000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180869754820220525194157.0001): Six-Cylinder Ignition Controller. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Apr 25, 2022
- [EA-22000T](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID151952144920220525194443.0001): Controller Wire Harness- Twin (14 Pin). Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Apr 25, 2022
- [AA2J4-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID108664051520220725142936.0001): Filter Assembly. Aero Accessories LLC · PMA PQ1206CE · Replaces Airborne1J4-4Aero Accessories AA1J4-4 · Mar 14, 2022
- [89000026-003](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID174241017120240229155312.0001): Final Assembly KCP 100 Control Panel(Landscape). Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Modification part · Nov 15, 2021
- [89000020-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID135386137120240229155256.0001): Final Assembly KSD 100 Primary Flight Display (PFD). Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Modification part · Nov 15, 2021
- [89000023-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID121615886720240229155301.0001): Final Assembly KG 71 Air Data Attitude and Heading Reference System (ADHRS). Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Modification part · Nov 15, 2021
- [89000026-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID104792557320240229155307.0001): Final Assembly KCP 100 Control Panel. Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Modification part · Nov 15, 2021
- [MC153-00900](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID749574486520211021173347.0001): Ring. McFarlane Aviation Inc · PMA PQ3732CE · Replaces 153-00900, 153-9, 755-964 · Sep 9, 2021
- [MC153-01500](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID559779322202110211733540.0001): Ring. McFarlane Aviation Inc · PMA PQ3732CE · Replaces 153-01500, 153-15, 755-930 · Sep 9, 2021
- [MC153-00300](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID311331069320211021173332.0001): Ring. McFarlane Aviation Inc · PMA PQ3732CE · Replaces 153-00300, 755-929, A39070 · Sep 9, 2021
- [MC154-01400](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID275286721320211021173430.0001): Felt. McFarlane Aviation Inc · PMA PQ3732CE · Replaces 154-01400, 154-14, 751-819 · Sep 9, 2021
- [MC155-00100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID246865560202110211734530.0001): Retaining Ring. McFarlane Aviation Inc · PMA PQ3732CE · Replaces 155-00100, 155-1, 3023, 752-830 · Sep 9, 2021
- [MC154-01300](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168798577720211021173428.0001): Felt. McFarlane Aviation Inc · PMA PQ3732CE · Replaces 154-01300, 154-13, 751-810 · Sep 9, 2021
- [EA-23000-A](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID761274132202109231437480.0001): EA-23000 Ignition/Starter Switch Panel. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Jul 28, 2021
- [700-00190-100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID261034086720210921142531.0001): SkyTrax 100B/200 ADS-B Receiver. Avidyne Corporation · PMA PQ4035CE · Replaces ModificationPart · Jul 28, 2021
- [EA-23000-A](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID159699760202109231436460.0001): EA-23000 Ignition/Starter Switch Panel. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Jul 28, 2021
- [ST-984](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID986409859320210810161807.0001): Installation of S-TEC 01326 Digital Flight Control System (DFCS)). S-TEC Corporation · PMA PQ0445SW · Modification part · Apr 8, 2021
- [ST-984-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID981785173520210810161808.0001): Installation of S-TEC 01326 Digital Flight Control System (DFCS). S-TEC Corporation · PMA PQ0445SW · Modification part · Apr 8, 2021
- [ST-984-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID783193906320210810161807.0001): Installation of S-TEC 01326 Digital Flight Control System (DFCS). S-TEC Corporation · PMA PQ0445SW · Modification part · Apr 8, 2021
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID909759096020210702175208.0001): Aspen Avionics · PMA PQ03868SW · Jan 20, 2021
- [1049-4000-03-001C](https://drs.faa.gov/browse/excelExternalWindow/FB6A4D62429A217F86258633006145AB.0001): Roll Steering Converter. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020
- [1049-4201-20](https://drs.faa.gov/browse/excelExternalWindow/ED78E4F8D3C63347862586330061461D.0001): Annunciator Kit GDC31. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020
- [1049-4200-20](https://drs.faa.gov/browse/excelExternalWindow/CBC6239248334CCE86258633006145E5.0001): Connector Kit GDC31. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020
- [1049-4200-50](https://drs.faa.gov/browse/excelExternalWindow/86CBD103649292948625863300614693.0001): Isolation Coupler Installation Kit. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020
- [1049-4000-03-001B](https://drs.faa.gov/browse/excelExternalWindow/6583D9B2B4E75DBE862586330061451A.0001): E50Roll Steering Converter. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020
- [1049-4801-01](https://drs.faa.gov/browse/excelExternalWindow/39A0DF401545910A8625863300614652.0001): Isolation Coupler. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020
- [APS68-01700](https://drs.faa.gov/browse/excelExternalWindow/51CDE584B1A22102862586290049EFF5.0001): Shim, Brake. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 068-01700 · Nov 4, 2020
- [ALE-2008AE-AC](https://drs.faa.gov/browse/excelExternalWindow/E2B30B020A91DE91862585DE00509F79.0001): Stator. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALE-2008AE, as used in alternators ALT… · Sep 1, 2020
- [RA154-03000](https://drs.faa.gov/browse/excelExternalWindow/DD82997F649BC443862585E40035802A.0001): Molded Grease Seal. Rapco Inc · PMA PQ2101CE · Replaces Cleveland Wheels & Brakes 154-03000 · Sep 1, 2020
- [ALE-2008AA-AC](https://drs.faa.gov/browse/excelExternalWindow/C617AAB83C6B799B862585DE0050A01D.0001): Stator. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALE-2008AA, as used in alternators ALY… · Sep 1, 2020
- [XA-943FS-AC](https://drs.faa.gov/browse/excelExternalWindow/B7CC6ECA46AA2F14862585DE00509E71.0001): Pos. Diode. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces XA-943FS, as used in alternators ALE… · Sep 1, 2020
- [ALE-1013AS-AC](https://drs.faa.gov/browse/excelExternalWindow/9F424D3467678943862585DE00509EFC.0001): Alternator Brush. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALE-1013AS, as used in alternators ALE… · Sep 1, 2020
- [ALU-3045BS-AC](https://drs.faa.gov/browse/excelExternalWindow/68353ACEF594EACF862585DE0050A127.0001): Brush Assembly. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALU-3045BS, as used in alternators ALE… · Sep 1, 2020
- [ALE-2008ABS-AC](https://drs.faa.gov/browse/excelExternalWindow/6583E821C11FC24F862585DE0050A086.0001): Stator. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALE-2008ABS, as used in alternators… · Sep 1, 2020
- [XA-944JS-AC](https://drs.faa.gov/browse/excelExternalWindow/0388185039CFC4DD862585DE00509DDD.0001): Neg. Diode. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces XA-944JS, as used in alternators ALE… · Sep 1, 2020
- [APS068-01700](https://drs.faa.gov/browse/excelExternalWindow/068001A41B0BCCA9862585EC004522B5.0001): Shim, Brake. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 068-01700 · Aug 26, 2020
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID887550545520220125131316.0001): DAC International · PMA PQ0986SW · Jul 31, 2020
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID761917634820220125131457.0001): DAC International · PMA PQ0986SW · Jul 31, 2020
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID519877368620220125131335.0001): DAC International · PMA PQ0986SW · Jul 31, 2020
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID253032526202201251314340.0001): DAC International · PMA PQ0986SW · Jul 31, 2020
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID231190298420220125131352.0001): DAC International · PMA PQ0986SW · Jul 31, 2020
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID140413349920220125131409.0001): DAC International · PMA PQ0986SW · Jul 31, 2020

All of them: https://openairdocs.org/model/piper-pa-60-601p/pma.md

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