# New Piper PA-28R-201 - Type: Aircraft model (FAA registry) - Registry code: 7103203 - Manufacturer (registry): NEW PIPER AIRCRAFT INC - Model: PA-28R-201 - 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/new-piper-pa-28r-201 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 2024-10-04](https://openairdocs.org/ad/2024-10-04): Wing, Attach Fittings · Piper PA-28-181, PA-28R-201, PA-44-180 and 1 more. Effective Jun 6, 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 2020-26-16](https://openairdocs.org/ad/2020-26-16): Wing Spar · Piper PA-28-151, PA-28-161, PA-28-181 and 12 more. Effective Feb 16, 2021 - [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 2016-07-21](https://openairdocs.org/ad/2016-07-21): Wing Ribs/Bulkhead · Piper PA-28-161, PA-28-181 and PA-28R-201. Effective Apr 26, 2016 - [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 2009-05-05](https://openairdocs.org/ad/2009-05-05): Primary Flight Displays · Avidyne Primary Flight Display (S-TEC STC SA09543AC-D or 2 others). Effective Apr 3, 2009 - [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 2004-14-12](https://openairdocs.org/ad/2004-14-12): Control wheel attaching hardware · Piper PA-28-161, PA-28-181, PA-28R-201 and 8 more. Effective Aug 10, 2004 - [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 97-01-01 R1](https://openairdocs.org/ad/97-01-01-R1): Main Gear Sidebrace Stud · Piper PA-24, PA-24-250, PA-24-260 and 10 more. Effective Dec 8, 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 94-14-14](https://openairdocs.org/ad/94-14-14): Nose Landing Gear Modification · Piper PA-28R-180, PA-28R-200, PA-28R-201 and 5 more. Effective Aug 19, 1994 - [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 82-06-11 R1](https://openairdocs.org/ad/82-06-11-R1): Nose Landing Gear, Inspect, Rig, Modify · Piper PA-28R-200, PA-28R-201, PA-28R-201T and 2 more. Effective Jun 16, 1982 - [AD 81-11-02 R1](https://openairdocs.org/ad/81-11-02-R1): Oil Drain Valves · Piper PA-28R-200, PA-28R-201 and PA-28RT-201. Effective Oct 2, 1981 - [AD 80-19-01](https://openairdocs.org/ad/80-19-01): Carbon Monoxide In Cabin · Piper PA-28R-180, PA-28R-200, PA-28R-201 and 1 more. Effective Sep 12, 1980 - [AD 80-14-03](https://openairdocs.org/ad/80-14-03): Bendix, King or Narco Transmitters · Piper PA-28-161, PA-28-181, PA-28-201T and 16 more. Effective Jul 1, 1980 - [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 79-22-02](https://openairdocs.org/ad/79-22-02): Fuel Leakage · Piper PA-28-161, PA-28-181, PA-28-201T and 6 more. Effective Oct 26, 1979 - [AD 79-13-03](https://openairdocs.org/ad/79-13-03): Fire Hazard Prevention · Piper PA-28-161, PA-28-181, PA-28-201T and 5 more. Effective Jun 8, 1979 - [AD 79-02-05](https://openairdocs.org/ad/79-02-05): Fuel Flow · Piper PA-28-161, PA-28R-201 and PA-28R-201T. Effective Jan 29, 1979 - [AD 78-25-03](https://openairdocs.org/ad/78-25-03): Hose Assemblies · Piper PA-23-250, PA-28R-180, PA-28R-200 and 11 more. Effective Jan 15, 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 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 2015-20-13](https://openairdocs.org/ad/2015-20-13) (historical): Wing Ribs/Bulkhead · Piper PA-28-161, PA-28-181 and PA-28R-201. Effective Oct 29, 2015 - [AD 2008-06-28](https://openairdocs.org/ad/2008-06-28) (historical): Primary flight display · Avidyne Primary Flight Display (S-TEC STC SA09543AC-D or 2 others). Effective Apr 10, 2008 - [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) (19) - [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 AIR-21-07](https://openairdocs.org/saib/AIR-21-07): WING SPAR, Verification of Correct Washers used with Wing Spar Attach Bolts. Issued Mar 30, 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-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-10-30](https://openairdocs.org/saib/CE-10-30): Landing Gear Nose Gear Drag Link Bolt. Issued May 4, 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-08-13](https://openairdocs.org/saib/CE-08-13): Electrical Power. Issued Feb 27, 2008 - [SAIB CE-07-08](https://openairdocs.org/saib/CE-07-08): Avidyne Primary Flight display (PFD). Issued Oct 31, 2006 - [SAIB CE-01-30](https://openairdocs.org/saib/CE-01-30): . Issued Jul 11, 2001 ## Registered aircraft None registered with this model now. ## 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 GAA16CA506](https://openairdocs.org/ntsb/GAA16CA506), Sep 22, 2016: New Piper PA-28R (N834PC), East St. Louis, IL, substantial damage. Probable cause: The pilot's failure to extend the landing gear, which resulted in a gear-up landing. ## FAA accident and incident reports (2) 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 20160921020509A](https://openairdocs.org/incident/20160921020509A), Sep 21, 2016: New Piper Aircraft Inc PA-28R-201 (N834PC), Cahokia, IL, No damage. Pilot flying for night currency, flying in a rectrable gear airplane. Pilot did not lower the gear and did a gear up landing. - [Incident 20070809019779I](https://openairdocs.org/incident/20070809019779I), Aug 9, 2007: Piper PA28R201 (N833PC), Cahokia/St Lou, IL, Minor damage. (-23) Aircraft was on a training mission that departed parks bi-state and upon landing on runway 30L at parks bi-state student inadvertently failed to lower… ## Service difficulty reports (220, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR ECPR20260731002](https://openairdocs.org/sdr/ECPR20260731002), Jul 30, 2026: SPARK PLUG. CRACKED. FOLLOWING DISCOVERY OF A CRACKED SPARK PLUG ON ANOTHER AIRCRAFT, A PRECAUTIONARY INSPECTION WAS CONDUCTED OF THE SPARK PLUG ON THIS AIRCRAFT AS IT WAS THE SAME - [SDR 2024FA0000489](https://openairdocs.org/sdr/2024FA0000489), May 22, 2023: THROTTLE CABLE. BROKEN. AIRCRAFT THROTTLE CABLE P/N: 455-322 COMPLETELY BROKE OFF AT ENGINE SIDE SWAGE. - [SDR ECPR202304070001](https://openairdocs.org/sdr/ECPR202304070001), Apr 6, 2023: SWITCH. STUCK. DURING THE PRE-TAXI CHECKLIST, STUDENT PILOT MISTAKENLY PLACED THE GEAR SELECTOR IN THE UP POSITION. THE NOSE GEAR RETRACTED, CAUSING THE NOSE OF THE AIRCRAFT T - [SDR 2023FA0000205](https://openairdocs.org/sdr/2023FA0000205), Apr 5, 2023: SWITCH. STUCK. DURING SCHEDULED INSPECTION, LANDING GEAR ANTI-RETRACTION SYSTEM FAILED TO PREVENT GEAR RETRACTION WITH WEIGHT ON WHEELS. INSPECTION FOUND GEAR SAFETY SQUAT SWI - [SDR 2022FA0000579](https://openairdocs.org/sdr/2022FA0000579), Oct 15, 2020: NONE. BROKEN. AN EMERGENCY LANDING WAS DECLARED BY THE INSTRUCTOR ON BOARD N373CB AFTER THE NOSE GEAR SAFE LIGHT FAILED TO ILLUMINATE INDICATING THAT THE NOSE GEAR WAS DOWNED - [SDR 2019FA0000310](https://openairdocs.org/sdr/2019FA0000310), Sep 19, 2019: PUMP. FAILED. PILOT REPORTED FUEL SMELL DURING TAXI / RUN UP. AIRCRAFT RETURNED TO PARKING FOR MAINTENANCE. INSPECTION REVEALED FUEL RESIDUE ON FIREWALL BEHIND ELECTRIC FUEL - [SDR ECPR2019050383335](https://openairdocs.org/sdr/ECPR2019050383335), May 3, 2019: STOP FITTING. BROKEN. DURING A SCHEDULED INSPECTION, THE OVERMOULDED RUBBER BUMPER ON THE NOSE GEAR RETRACTION STOP WAS FOUND BROKEN. THE RUBBER WAS SPLIT AT THE POINT OF CONTACT WIT - [SDR ECPR2019011882002](https://openairdocs.org/sdr/ECPR2019011882002), Jan 17, 2019: BUMPER. SPLIT. DURING A SCHEDULED INSPECTION, THE OVERMOULDED RUBBER BUMPER ON THE NOSE GEAR RETRACTION STOP WAS FOUND BROKEN. THE RUBBER WAS SPLIT AT THE POINT OF CONTACT WIT - [SDR ECPR2018120768568](https://openairdocs.org/sdr/ECPR2018120768568), Dec 6, 2018: STOP. BROKEN. DURING A SCHEDULED INSPECTION, THE OVERMOULDED RUBBER BUMPER ON THE NOSE GEAR RETRACTION STOP WAS FOUND BROKEN. THE RUBBER WAS SPLIT AT THE POINT OF CONTACT WIT - [SDR ECPR2018112981439](https://openairdocs.org/sdr/ECPR2018112981439), Nov 28, 2018: BUMPER. BROKEN. DURING A SCHEDULED INSPECTION, THE OVERMOULDED RUBBER BUMPER ON THE NOSE GEAR RETRACTION STOP WAS FOUND BROKEN. THE RUBBER WAS SPLIT AT THE POINT OF CONTACT WIT - [SDR ECPR2018110768116](https://openairdocs.org/sdr/ECPR2018110768116), Nov 6, 2018: EXHAUST STACK. CRACKED. ON DEPARTURE FOLLOWING A TOUCH AND GO LANDING THE CREW HEARD AN UNUSUAL METALLIC SOUND FROM THE ENGINE. THE CREW REMAINED IN THE PATTERN AND CONDUCTED A FULL ST - [SDR ECPR201811060001](https://openairdocs.org/sdr/ECPR201811060001), Nov 5, 2018: BUMPER BLOCK. BROKEN. DURING A SCHEDULED INSPECTION, THE OVERMOULDED RUBBER BUMPER ON THE NOSE GEAR RETRACTION STOP WAS FOUND BROKEN. THE RUBBER WAS SPLIT AT THE POINT OF CONTACT WIT - [SDR 2018FA0000386](https://openairdocs.org/sdr/2018FA0000386), Sep 25, 2018: DRAG STRUT. CRACKED. WHILE IN FLIGHT OUT OF RDU HEARD A NOISE FROM FORWARD OF AIRCRAFT AND HAD WARNING NOTICE OF NOSE GEAR UNLOCK. MADE EMERGENCY LANDING INTO RDU. TOWED AIRCRAFT OF - [SDR 2018FA0000259](https://openairdocs.org/sdr/2018FA0000259), May 1, 2018: FITTING. DAMAGED. AFTER PERFORMING A VISUAL INSPECTION ON A PA28 RIGHT WING, VISUAL DAMAGE WAS NOTED. AFTER INSPECTION FOUND THAT WHEN THAT AIRCRAFT FUSELAGE IS FIXED, THE RIGHT - [SDR 2017FA0000292](https://openairdocs.org/sdr/2017FA0000292), Jul 19, 2017: LANDING GEAR. INOPERATIVE. NOSE GEAR WOULD NOT EXTEND. - [SDR 2016FA0000318](https://openairdocs.org/sdr/2016FA0000318), Jun 6, 2016: RIB. BUCKLED. RECEIVED A WRITE UP FOR 149DT SAYING IT HAD CUTS IN THE LEFT MAIN TIRE. ON INSPECTION OF TIRE, NOTICED THAT THE WHEEL SEEMED TO BE CANTED. PROCEEDED TO INSPECT - [SDR 2020FA0000112](https://openairdocs.org/sdr/2020FA0000112), May 7, 2016: SHAFT. SHEARED. OWNER REPORTED NO VAC. REMOVED VAC PUMP. PLASTIC SHAFT SHEARED. REPLACED WITH NEW VAC PUMP. OPERATIONS CHECKED GOOD. - [SDR 2015FA0000424](https://openairdocs.org/sdr/2015FA0000424), Sep 2, 2015: SCREEN. DAMAGED. PAPER INDUCTION AIR FILTER, PN 638876 WAS FOUND TO HAVE INNER SCREEN MESH DISTORTED, LOOSE AND PULLING AWAY FROM INSIDE OF FILTER ASSEMBLY. IF ALLOWED TO CONTIN - [SDR 2015FA0000437](https://openairdocs.org/sdr/2015FA0000437), Aug 21, 2015: MAGNETO. INOPERATIVE. THE ACFT WOULD NOT START OR EVEN HIT DESPITE MULTIPLE ATTEMPTS. WHEN THE TIMING WAS CHECKED IT WAS FOUND THAT THE IMPULSE COUPLING WOULD RELEASE AT VARYING TIME - [SDR 2015FA0000324](https://openairdocs.org/sdr/2015FA0000324), Jun 15, 2015: TRUNNION. DETACHED. AFTER A TOUCH AND GO LANDING THE GEAR WAS PUT IN THE UP POSITION WHICH RESULTED IN A FAILURE OF THE GEAR UNSAFE LIGHT TO EXTINGUISH. THE LANDING GEAR WAS PUT IN - [SDR 2015FA0000197](https://openairdocs.org/sdr/2015FA0000197), Apr 15, 2015: ADAPTER. NOT SEATED. AIRCRAFT WAS WRITTEN UP FOR HIGH OIL TEMPERATURE 4/18/15. T 47.2, H-9010.5. OIL FILTER ADAPTER WAS REMOVED AND INSPECTED. THERMO VALVE SEAT AND SEAT IN ADAPTER - [SDR FT8S2015FA0000100](https://openairdocs.org/sdr/FT8S2015FA0000100), Mar 17, 2015: CABLE. BROKEN. THE PILOT REPORTED WHEN HE WENT TO 40 DEGREES OF FLAPS HE HEARD AND FELT A POP. THEY RETURNED TO THE AIRPORT AND MAINTENANCE INSPECTED THE ACFT, FOUND THAT HALF - [SDR N3XR201409110008](https://openairdocs.org/sdr/N3XR201409110008), Sep 10, 2014: WIRE. BROKEN. NO LEFT GEAR DOWN AND LOCKED INDICATION. FOUND THE MIDDLE WIRE ON THE DOWN AND LOCKED SWITCH BROKEN. REPAIRED THE WIRE WITH A NEW RING TERMINAL. PERFORMED AN OP - [SDR N3XR2014100100009](https://openairdocs.org/sdr/N3XR2014100100009), Sep 8, 2014: BUSHING. LOOSE. DURING TAKEOFF, THE PILOT'S CONTROL YOKE SHAFT BUSHING, MOVED AFT OF ITS MOUNTING AND WAS FREE OF THE INSTRUMENT PANEL. THE TAKEOFF WAS ABORTED. THIS OPERATOR H - [SDR N3XR2014091100002](https://openairdocs.org/sdr/N3XR2014091100002), Sep 4, 2014: WIRE. BROKEN. RT MAIN GEAR LIGHT INOPERATIVE. REPLACED THE MIDDLE RING TERMINAL TO DOWNLOCK SWITCH. - [SDR N3XR2014100100011](https://openairdocs.org/sdr/N3XR2014100100011), Aug 22, 2014: BUSHING. LOOSE. THE LT CONTROL YOKE BUSHING, MOVED AFT OF THE INSTRUMENT PANEL, ALLOWING RADIAL MOVEMENT OF THE YOKE SHAFT. - [SDR N3XR2014100100012](https://openairdocs.org/sdr/N3XR2014100100012), Aug 21, 2014: BUSHING. LOOSE. THE LEFT CONTROL YOKE BUSHING, MOVED AFT OF THE INSTRUMENT PANEL, ALLOWING RADIAL MOVEMENT OF THE YOKE SHAFT. - [SDR N3XR2014191100007](https://openairdocs.org/sdr/N3XR2014191100007), Aug 15, 2014: WIRE. BROKEN. IN FLIGHT EMERGENCY WITH THE LT GEAR LIGHT BEING INOPERATIVE. PLACED ACFT ON JACKS AND INSPECTED THE LT GEAR LEG WIRING. FOUND A WIRE BROKEN TO THE DOWNLOCK SWI - [SDR 2014FA0000480](https://openairdocs.org/sdr/2014FA0000480), Aug 14, 2014: SPAR PLATE. DAMAGED. BOLT HOLE ELONGATED ON AFT SPAR PLATE FITTING: DURING ROUTINE MAINTENANCE BOLT FOUND LOOSE IN AFT SPAR PLATE AND HOLE WAS ELONGATED, SAME CONDITION WAS FOUND 5- - [SDR N3XR2014100100014](https://openairdocs.org/sdr/N3XR2014100100014), Aug 12, 2014: BUSHING. LOOSE. THE LEFT CONTROL YOKE BUSHING, MOVED AFT OF THE INSTRUMENT PANEL, ALLOWING RADIAL MOVEMENT OF THE YOKE SHAFT. - [SDR N3XR2014100100013](https://openairdocs.org/sdr/N3XR2014100100013), Aug 4, 2014: BUSHING. LOOSE. THE LEFT CONTROL YOKE BUSHING, MOVED AFT OF THE INSTRUMENT PANEL, ALLOWING RADIAL MOVEMENT OF THE YOKE SHAFT. - [SDR N3XR2014091100005](https://openairdocs.org/sdr/N3XR2014091100005), Jul 31, 2014: WIRE. BROKEN. LEFT LANDING GEAR LIGHT WAS BLINKING ON AND OFF CONSTANTLY. INSPECTED THE LANDING GEAR SYS AND FOUND THE LT DOWNLOCK SWITCH HAD A WIRE BROKEN TO IT. REPAIRED TH - [SDR N3XR201410010010](https://openairdocs.org/sdr/N3XR201410010010), Jul 12, 2014: BUSHING. LOOSE. DURING LANDING AND FLARE, THE LT CONTROL YOKE BUSHING, MOVED AFT OF THE INSTRUMENT PANEL, ALLOWING RADIAL MOVEMENT OF THE YOKE SHAFT. - [SDR N3XR2014091100004](https://openairdocs.org/sdr/N3XR2014091100004), Jul 7, 2014: LIMIT SWITCH. OUT OF ADJUST. ON TAKEOFF, GEAR WARNING LIGHT ILLUMINATED WIH FULL POWER, FLAPS UP, RT MAIN GEAR POSITION LIGHT INOPERATIVE. INSPECTED RT MLG FOR CONDITION, SECURITY AND OPERA - [SDR N3XR2014091100003](https://openairdocs.org/sdr/N3XR2014091100003), Jun 25, 2014: POWERPACK. LOW. RT MLG UNSAFE LIGHT NOT ILLUMINATED. INSPECTED ENTIRE LANDING GEAR HYD AND INDICATING SYSTEMS. FOUND POWERPACK TO BE LOW ON FLUID. SERVICED POWER-PACK WITH FLUI - [SDR FAA20140702000663](https://openairdocs.org/sdr/FAA20140702000663), Jun 24, 2014: DRIVE UNIT. BINDING. PILOT REPORTED PILOT DRIVE FAILED WITH LESS THAN 140 HOURS SINCE O/H. DRIVE UNIT WAS FROZEN AND WOULD NOT RETRACT, NO LUBE WAS VISIBLE ON THE SHAFT AND NO PART, - [SDR N3XR2014100100015](https://openairdocs.org/sdr/N3XR2014100100015), Jun 19, 2014: BUSHING. LOOSE. THE LEFT CONTROL YOKE BUSHING, MOVED AFT OF THE INSTRUMENT PANEL, ALLOWING RADIAL MOVEMENT OF THE YOKE SHAFT. - [SDR N3XR2014100100016](https://openairdocs.org/sdr/N3XR2014100100016), Jun 18, 2014: BUSHING. MIGRATED. THE LT CONTROL YOKE BUSHING MOVED AFT OF THE INSTRUMENT PANEL, ALLOWING RADIAL MOVEMENT OF THE YOKE SHAFT. - [SDR 2013FA0000319](https://openairdocs.org/sdr/2013FA0000319), Jun 5, 2013: DISTRIBUTOR GEAR. FAILED. ACFT RAN ROUGH AND SKIPPED. OPENED MAGNETO FOR INSPECTION. FOUND DISTRIBUTOR GEAR K3008 METAL FINGER BECAME DISLODGED FROM THE CENTER POST. GEAR WAS REPLACED WI - [SDR NX4R000032](https://openairdocs.org/sdr/NX4R000032), Apr 5, 2012: BRACE. BROKEN. WHEN THE PILOT SELECTED "GEAR UP", A NOISE WAS HEARD IN THE NOSE WHEEL AREA. THE NOSE GEAR INDICATION WAS UNSAFE AND WHEN THE LANDING GEAR WAS SELECTED "DOWN", - [SDR 2011FA0000793](https://openairdocs.org/sdr/2011FA0000793), Dec 16, 2011: ATTACH FITTING. CHAFED. UPON INSPECTION OF FLAP CONTROL CABLE TO FLAP HANDLE ATTACHMENT FOUND BUSHING (PN 63900-174) CLEVIS BOLT (PN AN23-11), AND FLAP HANDLE (PN 63781-008) HAD BEEN " - [SDR 2011FA0000677](https://openairdocs.org/sdr/2011FA0000677), Sep 27, 2011: THROTTLE CABLE. BROKEN. DURING GROUND RUN THE PILOT REPORTED AN UNRESPONSIVE THROTTLE. THE ACFT WAS GROUNDED AND BROUGHT INTO THE SHOP FOR INSPECTION. THE THROTTLE CABLE WAS FOUND BROK - [SDR 2011FA0000632](https://openairdocs.org/sdr/2011FA0000632), Aug 15, 2011: TAPPET. DAMAGED. AFTER FINDING MAGNETIC METAL FLAKES IN OIL FILTER AT ANNUAL INSP, ENGINE WAS REMOVED FROM SERVICE AND DISASSEMBLED. INSP REVEALED SEVERE FLAKING AND SPALLING OF - [SDR OG5R20110719001](https://openairdocs.org/sdr/OG5R20110719001), Jul 12, 2011: TIRE. DEFLATED. FLAT TIRE DURING LANDING ROLL OUT; WHILE TAXIING TO PARK THE ACFT. - [SDR OG5R20110714002](https://openairdocs.org/sdr/OG5R20110714002), Jun 9, 2011: TIRE. DEFLATED. LT MAIN TIRE WENT FLAT ON TAXI. - [SDR NX4R000013](https://openairdocs.org/sdr/NX4R000013), Apr 28, 2011: MOUNT. CRACKED. DURING ROUNTINE MX, THE TECH WAS PERFORMING A PRELIMINARY/HIDDEN DAMAGE INSP OF THE AREA SURROUNDING THE AREA WHERE WORK WAS TO BE PERFORMED. NOTICED THE SMALL - [SDR NX4R000011](https://openairdocs.org/sdr/NX4R000011), Apr 20, 2011: ATTACH FITTING. BROKEN. DURING TAKEOFF, THE PILOT RETRACTED THE LANDING GEAR. THE GEAR "UNSAFE LIGHT" REMAINED ILLUMINATED. ALSO THE ATC TOWER CONTROLLER ADVISED THE CREW THAT THEIR NL - [SDR 2010FA0000763](https://openairdocs.org/sdr/2010FA0000763), Jun 29, 2010: BOLT. BROKEN. ON GEAR RETRACTION, GEAR UNSAFE LIGHT REMAINED ON WITH PUMP SHUTOFF. GEAR WAS EXTENDED AND LANDING ACCOMPLISHED WITHOUT INCIDENT. INSP SHOWED THAT THE BOLT ATTA - [SDR 2010FA0000731](https://openairdocs.org/sdr/2010FA0000731), Jun 28, 2010: ROD END. WEAK. (UC2R) THE PILOT REPORTED THA THE PROP GOVEERNOR CONTROL WAS UNRESPONSIVE. THE TECH FOUND THE PROP GOVERNOR ROD END OFF OF THE GOVERNOR ATTACH BALL. THE SPRING - [SDR 2010FA0000706](https://openairdocs.org/sdr/2010FA0000706), Jun 21, 2010: DRAG LINK. BROKEN. DURING A TRAINING FLIGHT, THE LANDING GEAR WAS EXTENDED. UPON GEAR EXTENSION ONLY THE MAIN GEAR DOWN LIGHTS ILLUMINATED. THE NOSE GEAR DOWN LIGHT REMAINED EXTIN All 220: https://openairdocs.org/model/new-piper-pa-28r-201/reports.md ## STCs that may be installed (OpenAirDocs) (306, 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 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 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 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 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 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 SA00060AT](https://openairdocs.org/stc/SA00060AT): Installation of flap gap seals. Whelen Aerospace Technologies. Lists PA-28 Series - [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 SA01319AT](https://openairdocs.org/stc/SA01319AT): Installation of new composite engine cowling with cowl flap and large inspection access doors on both sides of cowling. Whelen Aerospace Technologies - [STC SA3229SO](https://openairdocs.org/stc/SA3229SO): Installation of main landing gear fairings. Whelen Aerospace Technologies - [STC SA02987CH](https://openairdocs.org/stc/SA02987CH): Installation of the Electroair Electronic Ignition System. Electroair Acquisition Corporation - [STC SA04586CH](https://openairdocs.org/stc/SA04586CH): Installation of Electroair Back Up Battery Panel System Control. Electroair Aquisition Corp - [STC SA2156CE](https://openairdocs.org/stc/SA2156CE): Installation of flap and aileron gap seals. 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 - [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc - [STC SA01982AT](https://openairdocs.org/stc/SA01982AT): Installation of new composite wingtip with recognition light. Whelen Aerospace Technologies - [STC SA00028AT](https://openairdocs.org/stc/SA00028AT): Installation of 'speed splitter' flap bracket fairings. Whelen Aerospace Technologies. Lists PA-28 Series - [STC SA04231CH](https://openairdocs.org/stc/SA04231CH): Installation and activation of a TruTrak Vizion autopilot system. Honeywell International Inc - [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 SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc - [STC SA09902AC](https://openairdocs.org/stc/SA09902AC): Installation of BendixKing KFD 900 Flight Display System. Honeywell International Inc. (Bendix King) All 306: https://openairdocs.org/model/new-piper-pa-28r-201/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. - [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 - [MC67184-000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID183977842120260722151904.0001): Axle. Airforms LLC · PMA PQ2644CE · Replaces 67184-000 · May 6, 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 - [MC9812-0023-101](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195858733620250929141436.0001): Fuel Level Sender. McFarlane Aviation Inc. · PMA PQ3732CE · Replaces PS10013-5, 550-503, 7740‑00040 · Sep 5, 2025 - [MC9812-0024-101](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID111314007420250929141436.0001): Fuel Level Sender. McFarlane Aviation Inc. · PMA PQ3732CE · Replaces PS10013-6, 550-504, 7740‑00041 · Sep 5, 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 - [MDL TD 031851](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184021792220250508133546.0001): VA-1A( )AndAccessories. Electronics International Inc · PMA PQ0088NM · Modification part · Apr 10, 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 - [20017A](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID162611629220250303152540.0001): Air-Oil Cooler. Boyd Niagara LLC · PMA PQ0872NE · Replaces 8537820 · Oct 30, 2024 - [LSM-200-106- 2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID129331888620250417195306.0001): Tapered Wing Tip Lens - RH. Whelen Aerospace Technologies · PMA PQ1372CE · Replaces [Modification Article] · Aug 26, 2024 - [8120-GCJ](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID174739227720240625133917.0001): FUEL PUMP. McFarlane Aviation Inc. · PMA PQ3732CE · Replaces 8120-G, 481-780 · Mar 14, 2024 - [CJ33963-02](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID160083325720240625133916.0001): BRACKET ASSEMBLY. McFarlane Aviation Inc. · PMA PQ3732CE · Replaces 33963-02 · Mar 14, 2024 - [8850-5CJ](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137037413620240625133919.0001): MOTOR (14 VDC). McFarlane Aviation Inc. · PMA PQ3732CE · Replaces 8850-5 · 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-601-101](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 - [EA-26000-12](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172302662120230105195522.0001): EA-26000 Series EIS Back-up Battery System Panel. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Jan 3, 2023 - [EA-26000-24](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID121923473020230105195542.0001): EA-26000 Series EIS Back-up Battery System Panel. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Jan 3, 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 - [8000-177](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132353197320240229155223.0001): PMA Link Sensor. Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Replaces 8000-177 · Nov 18, 2022 - [8225-004](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID104685608220240229155225.0001): PA-28 / PA-32Wiring Harness Kit. Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Replaces 8225-004 · Nov 18, 2022 - [8000215](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID157151941320221130202550.0001): Engine Oil Cooler. Aero-Classics Heat Transfer Products Inc · PMA PQ2543NM · Replaces Harrison P/N: 8534108 · Oct 21, 2022 - [8000661](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID141997759220221130202532.0001): Engine Oil Cooler. Aero-Classics Heat Transfer Products Inc · PMA PQ2543NM · Replaces Niagara Development & Mfg. 20017APiper… · Oct 21, 2022 - [APS66-10500](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165749710520221020170258.0001): Brake Lining. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 066-10500 · Aug 10, 2022 - [APS105-00200](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID117355682120221020170415.0001): Rivet. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 105-00200 · Aug 10, 2022 - [AAG5-002](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID106659092420220811111804.0001): G5 Adapter Plate. Affordable Aviation LLC · PMA PQ05456NM · Replaces Garmin 115-02733-00 · Aug 2, 2022 - [OI7201](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132452596220230324134544.0001): Air Vent Assembly. Obvious Innovations LLC · PMA PQ00007CB · Replaces 65735-02, 65735-03, 65735-04… · Jun 24, 2022 - [01-0790906-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID114520480820220706160202.0001): LED Landing Light. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · Jun 21, 2022 - [EA-20000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID174367564720220525194027.0001): Four-Cylinder Ignition Controller. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Apr 25, 2022 - [EA-22000T](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID140464207620220525194136.0001): Controller Wire Harness- Twin (14 Pin). Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Apr 25, 2022 - [EA-22000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID119767468720220525194102.0001): Controller Wire Harness (14 Pin). Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Apr 25, 2022 All of them: https://openairdocs.org/model/new-piper-pa-28r-201/pma.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Piper PA-28R-201](https://openairdocs.org/model/piper-pa-28r-201): 336 registered aircraft, registry code 7102816 - [Piper PA-28R-201](https://openairdocs.org/model/piper-pa-28r-201): 16 registered aircraft, registry code 7102833 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.