# Piper / Beaumont PA-28-140

- Type: Aircraft model (FAA registry)
- Registry code: 7102822
- Manufacturer (registry): PIPER / BEAUMONT
- Model: PA-28-140
- 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-beaumont-pa-28-140

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 2005-01-19](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 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 75-08-03](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 74-13-04](https://openairdocs.org/ad/74-13-04): Throttle Control Cable · Piper PA-28-140. Effective Jun 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 74-06-02](https://openairdocs.org/ad/74-06-02): AVCON Mufflers · Lycoming 150 and160 hp Model O-320-( ) engine (Williams Robert or Barbara STC SA750CE or 3 others). Effective Mar 18, 1974
- [AD 72-24-02](https://openairdocs.org/ad/72-24-02): Throttle Movement Placard · Lavia Argentina PA-25, PA-28-140, PA-28-150 and 2 more. Effective Nov 17, 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 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 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

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) (23)

- [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-18-25](https://openairdocs.org/saib/CE-18-25): Powerplant; Air Intake. Issued Aug 30, 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-05-67](https://openairdocs.org/saib/CE-05-67): . Issued Jul 7, 2005
- [SAIB CE-05-29R1](https://openairdocs.org/saib/CE-05-29R1): . Issued Feb 3, 2005
- [SAIB CE-05-29](https://openairdocs.org/saib/CE-05-29) (historical): . Issued Feb 1, 2005
- [SAIB CE-04-63](https://openairdocs.org/saib/CE-04-63): . Issued Apr 16, 2004
- [SAIB ACE-97-02](https://openairdocs.org/saib/ACE-97-02): . Issued Apr 22, 1997

## 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 (364, newest 50)

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

- [SDR 2026FA0000795](https://openairdocs.org/sdr/2026FA0000795), Sep 7, 2026: MAGNETO. FAULTED. DURING FLIGHT, THE ENGINE EXPERIENCED A SMOOTH PARTIAL LOSS OF POWER WITH AN RPM DECREASE OF APPROX 200–400 RPM. DISCONTINUED THE FLIGHT & MADE AN EMERGENCY LAN
- [SDR 2026FA0000419](https://openairdocs.org/sdr/2026FA0000419), May 20, 2026: MAGNETO. OUT OF ADJUST. ENGINE WAS INSTALLED JULY 2025. TIME SINCE OVERHAUL IS 100 HOURS. FOUND ENGINE DAMAGE DUE TO LEFT MAG BEING ADVANCED 15 DEGREES. PULLED ENGINE AND SHIPPED BACK 
- [SDR 2024FA0000746](https://openairdocs.org/sdr/2024FA0000746), Oct 3, 2024: SPAR CAP. CORRODED. DEFECT WAS DISCOVERED WHILE CONDUCTING A 100HR/ANNUAL INSP. R/H WING INBOARD LOWER AFT SPAR CAP HAS INTERGRANULAR/ EXFOLIATION CORROSION. DEFECT IS APPROXIMATEL
- [SDR 2024FA0000484](https://openairdocs.org/sdr/2024FA0000484), Jun 6, 2024: EXHAUST VALVE. BROKEN. DURING CLIMB OUT FROM RIGBY, ID, AIRCRAFT EXPERIENCED PARTIAL ENGINE POWER LOSS. POST INCIDENT INSPECTION REVEALED #3 CYLINDER EXHAUST VALVE WAS DAMAGED/MISSING
- [SDR 2024FA0000182](https://openairdocs.org/sdr/2024FA0000182), Feb 20, 2024: STARTER. BROKEN. STARTER DRIVE MOTOR WAS FOUND LOOSE FROM BENDIX ASSEMBLY DURING 100 HOUR INSPECTION. MOTOR IS ATTACHED TO BENDIX WITH 2 BOLTS THREADED INTO BENDIX HOUSING. BOTH
- [SDR 2023FA0000611](https://openairdocs.org/sdr/2023FA0000611), Oct 19, 2023: SPAR. CORRODED. WE REMOVED THE RH FUEL TANK TO REPLACE A FLEXIBLE FUEL LINE. UPON REMOVING THE FUEL TANK WE SAW EXTENSIVE EXFOLIATION CORROSION ON THE UPPER WING SPAR BEHIND TH
- [SDR 2023FA0000335](https://openairdocs.org/sdr/2023FA0000335), Jun 22, 2023: CYLINDER. SEPARATED. #2 CYLINDER SEPARATED FROM CASE. APPEARS CONNECTING ROD OR WRIST PIN SEPARATED FROM PISTON WHICH CAUSED CYLINDER TO SEPARATE. ENGINE HAD APPROXIMATELY 6 QUARTS 
- [SDR 2022FA0000639](https://openairdocs.org/sdr/2022FA0000639), Oct 21, 2022: TIRE. DEFECTIVE. MAIN TIRE WAS FOUND FLAT PARKED IN THE HANGAR. REMOVED TIRE AND TUBE INSPECTED TUBE AND FOUND HOLE IN SIDEWALL LOCATION ON THE TUBE CAUSED BY THE COARSENESS OF 
- [SDR 2022FA0000236](https://openairdocs.org/sdr/2022FA0000236), Apr 26, 2022: ALTIMETER. INACCURATE. ALTIMETER BARO SCALE ADJUSTMENT DISCONNECTED FROM ALTIMETER MECHANISM. ROTATING THE BARO ADJUST KNOB RESULTS IN THE ALTIMETER BARO SCALE MOVING BUT DOES NOT CHA
- [SDR 2022FA0000010](https://openairdocs.org/sdr/2022FA0000010), Dec 26, 2021: ELT. FALSE ACTIVATION. ACK E-04 STARTED TRANSMITTING WHEN A/C WAS STATIONARY WITH BATTERY SWITCH OFF. COCKPIT INDICATIONS: RED LIGHT ON REMOTE PANEL AND AUDIO ALERT SOUNDED. RESET ELT
- [SDR 2021FA0000316](https://openairdocs.org/sdr/2021FA0000316), Nov 8, 2021: NONE. FAILED. FOUND BAFFLE LIBERATED FROM ENGINE MUFFLER BLOCKING EXHAUST GAS PATH CAUSING ENGINE POWER LOSS. RECORDS INDICATE INSTALLED MUFFLER ASSEMBLY WAS PN 99482-00 WHIC
- [SDR 2021FA0000199](https://openairdocs.org/sdr/2021FA0000199), Apr 30, 2021: EXHAUST PIPE. CRACKED. EXHAUST COLLECTOR TUBES WERE CRACKED AND NEARLY UNDETECTABLE WITHOUT REMOVAL OF EXHAUST AND INSPECTION WITH A BRIGHT LIGHT SOURCE. IT APPEARS THE CRACKS WENT UN
- [SDR 2020FA0000395](https://openairdocs.org/sdr/2020FA0000395), Sep 4, 2020: NUT PLATE. CORRODED. DEFECT DISCOVERED UPON REMOVAL OF RT FUEL TANK. ALL 4 INDEPENDENT FLOATING NUT PLATES MS2106L08 FOUND SEVERELY CORRODED WITH RUST. THE NUT PLATE HOUSING AND THR
- [SDR 2018FA0000516](https://openairdocs.org/sdr/2018FA0000516), Dec 11, 2018: SKIN. DAMAGED. ON ANNUAL INSPECTION IT WAS FOUND THAT THE TRAILING EDGE CAP ON THE BOTTOM RIGHT INBOARD LONGITUDINAL EXTERIOR RUNNER HAD TWO POPPED RIVET HEADS AND SURFACE COR
- [SDR 2018FA0000515](https://openairdocs.org/sdr/2018FA0000515), Dec 11, 2018: SKIN. CRACKED. ON ANNUAL INSPECTION TWO SMALL CRACKS WERE FOUND ON THE TOP OF THE RIGHT WING AND ONE SMALL CRACK ON THE TOP OF THE LEFT WING. THE FIRST CRACK WAS FOUND AT THE 
- [SDR 2020FA0000051](https://openairdocs.org/sdr/2020FA0000051), Aug 25, 2018: CARBURETOR. SEPARATED. REPORTED PROBLEM WAS PARTIAL ENGINE POWER LOSS DURING CLIMB OUT. UPON INSPECTION OF ENGINE AND ACCESSORIES THE CARBURETOR WAS FOUND TO HAVE THE PARTING FLANGE S
- [SDR 2018FA0000521](https://openairdocs.org/sdr/2018FA0000521), Jul 3, 2018: HOSE. COLLAPSED. INVESTIGATING HIGH OIL TEMPERATURE IT WAS DISCOVERED THAT APPROXIMATELY 4 INCHES OF THE INSIDE LAYER OF THE OIL SUPPLY HOSE TO THE OIL COOLER AT THE ENG END BEG
- [SDR 2018FA0000462](https://openairdocs.org/sdr/2018FA0000462), Apr 6, 2018: CYLINDER. CRACKED. CYLINDER HEAD IS CRACKED. THIS IS THE THIRD CYLINDER ON THIS ENGINE THAT THE HEAD HAS DEVELOPED HOLES IN THEM. THE FIRST WENT AT ABOUT 800 HOURS. WE OPERATE THI
- [SDR 2018FA0000110](https://openairdocs.org/sdr/2018FA0000110), Feb 28, 2018: CYLINDER. BROKEN. FAILURE OF THE UPPER PART OF THE RIGHT MAIN GEAR, THE CYLINDER. THIS FAILURE APPEAR TO BE A MECHANICAL FAILURE OF BOTH THE UPPER ATTACHMENT EARS FOR THE TORQUE 
- [SDR 2018FA0000350](https://openairdocs.org/sdr/2018FA0000350), Feb 18, 2018: MUFFLER. ERODED. DURING AN ANNUAL INSPECTION OF AN AIRCRAFT THAT HAD ACCUMULATED 300 HOURS SINCE THE INSTALLATION OF SUPPLEMENTAL TYPE CERTIFICATE (STC) SA02168AT THE FOLLOWING 
- [SDR 2017FA0000578](https://openairdocs.org/sdr/2017FA0000578), Nov 11, 2017: SPAR. CORRODED. RIGHT WING SPAR INSPECTED IAW SB 1006. FOUND TO BE CORRODED WITH INTERGRANULAR CORROSION ON FORWARD FACE OF SPAR WEB, UPPER SPAR CAP IN FRONT OF LANDING GEAR ST
- [SDR 2017FA0000164](https://openairdocs.org/sdr/2017FA0000164), Apr 22, 2017: CRANKCASE. CRACKED. PILOT MADE AN EMERGENCY OFF AIRPORT LANDING AFTER EXPERIENCING A LOUD BANG FOLLOWED BY A LOSS OF ENGINE POWER AND SMOKE. INSPECTION OF THE ENGINE REVEALED A CRA
- [SDR 2017FA0000095](https://openairdocs.org/sdr/2017FA0000095), Feb 10, 2017: THROTTLE CABLE. BROKEN. DURING FLIGHT THE PILOT ATTEMPTED TO REDUCE ENGINE POWER AND THE THROTTLE CABLE BROKE WITH THE ENGINE STUCK AT CRUISE POWER. MIXTURE CONTROL WAS USED OVERHEAD T
- [SDR 2017FA0000415](https://openairdocs.org/sdr/2017FA0000415), Oct 25, 2016: SEAT TRACK. CORRODED. SEAT TRACK WAS CORRODED UNDER THE CARPET TO THE POINT THAT THE RIVETS HOLDING IT TO THE ACFT WERE FALLING OUT. THE ACFT HAS BEEN STORED OUTSIDE FOR SOME TIME AN
- [SDR C2XA2016FA0000390](https://openairdocs.org/sdr/C2XA2016FA0000390), Aug 26, 2016: CARBURETOR. LOOSE. COMPLAINT RECEIVED OF ENGINE, DEISELING, ON SHUTDOWN. FOUND CARBURETOR UPPER HALF AND LOWER SEPARATING AT MATING SURFACE. REMOVED CARBURETOR RETIGHTENED SCREWS 
- [SDR 2016FA0000253](https://openairdocs.org/sdr/2016FA0000253), May 23, 2016: ELT. INOPERATIVE. WHEN PURCHASED NEW IN 2013 CASE EXTERIOR APPEARED TO BE USED OR RE-MANUFACTURED. ELT UNIT FUNCTIONAL CHECKED OK & INSTALLED IN ACFT. WITH APPROX 2 YEARS LEFT ON
- [SDR 2016FA0000229](https://openairdocs.org/sdr/2016FA0000229), May 10, 2016: EXHAUST DUCT. LEAKING. WATER ON TOP ENGINE COWLING LEAKING THROUGH COWLING HINGE. DOWN NR 1 EXHAUST RISER OF POWERFLOW EXHAUST AND COLLECTING IN SCAT DUCTING FOR CARB HEAT. QUANITY RE
- [SDR CA160307002](https://openairdocs.org/sdr/CA160307002), Mar 2, 2016: BAR. CRACKED. (CAN) THE CONTROL COLUMN TEE BAR ASSEMBLY WAS REMOVED FROM AIRCRAFT C-GQPV MODEL PA-28-140 SERIAL NUMBER 28-7725161 AT 18602.5 HOURS TTAF TO SERVICE C-GQPN MODE
- [SDR 2016FA0000117](https://openairdocs.org/sdr/2016FA0000117), Feb 28, 2016: WIRE HARNESS. CHAFED. AS THE AIRCRAFT WAS CLIMBING THROUGH 400 FEET AGL, THE PILOT DETECTED SMOKE COMING FROM UNDERNEATH THE LT HALF OF THE INSTRUMENT PANEL. THE PILOT DECLARED AN EM
- [SDR CA160213001](https://openairdocs.org/sdr/CA160213001), Feb 13, 2016: BAR. FAILED. (CAN) TRAINING FLIGHT, STUDENT IN LH SEAT, INSTRUCTOR IN RH SEAT. THE INSTRUCTOR WAS VERBALLY COACHING THE STUDENT ON APPROACH TO RUNWAY 13 WIND 140/12KTS, 10 D
- [SDR 9LIS2016FA0000006](https://openairdocs.org/sdr/9LIS2016FA0000006), Dec 22, 2015: CYLINDER HEAD. CRACKED. THE CYLINDER HEAD CRACKED AT THE NINETH COOLING FIN. CRACK RUNS ALONG THE FIN. THE CRACK IS ABOUT .5" LONG. THE CYLINDER HAD LOW COMPRESSION. THE CRACK OCCURRED
- [SDR CA151215007](https://openairdocs.org/sdr/CA151215007), Nov 30, 2015: UNKNOWN. ODOR. (CAN) THE OPERATOR INVESTIGATED FOR AN OIL ODOR IN CABIN ISSUE SINCE OCTOBER 26TH. EXTENSIVE TROUBLESHOOTING WAS PERFORMED TO IDENTIFY THE PROBLEM. THE FSR RECO
- [SDR 9LIS2015082100394](https://openairdocs.org/sdr/9LIS2015082100394), Aug 11, 2015: SUPPORT. CRACKED. HIGH TIME PA23: STRESS CRACKS AT FORWARD RADIUS X2 NEAR FORWARD HOLD DOWN BOLTS DELTA SHAPE RUDDER PEDAL INSTALLATION SUPPORT ASSY.
- [SDR 2015FA0000360](https://openairdocs.org/sdr/2015FA0000360), Aug 2, 2015: SEAT FRAME. BROKEN. PILOTS SEAT FRAME BROKE COMPLETELY THROUGH APPROXIMATELY 2" FORWARD OF SEAT BACK ATTACHMENT CAUSING PILOT TO FALL BACKWARDS TOWARD THE REAR SEATS. EVENT HAPPENE
- [SDR CA150608011](https://openairdocs.org/sdr/CA150608011), Jun 7, 2015: GEAR. FAILED. (CAN) PILOTS REPORTED ROUGH RUNNING ENGINE. THE RT MAGNETO HAD AN INTERNAL FAULT ON THE ROTOR GEAR WHICH WAS NEW FROM THE FACTORY 385 HRS AGO. THE METAL TAB ON 
- [SDR 2015FA0000239](https://openairdocs.org/sdr/2015FA0000239), May 28, 2015: GASKET. LEAKING. DURING LANDING ROLLOUT ENGINE STOPPED AND WOULD NOT RESTART. MAINTENANCE INSPECTED ACFT AND FOUND THAT CARBURETOR FUEL BOWL GASKET WAS LEAKING FUEL.
- [SDR CA140908026](https://openairdocs.org/sdr/CA140908026), Sep 5, 2014: OUTLET. ERODED. (CAN) DURING ROUTINE INSPECTION IT WAS DISCOVERED THAT THE MUFFLER OUTLET PIPE HAD AN EXTENSION PIECE THAT APPEARS TO BE OF UNAPPROVED, SUBSTANDARD MATERIAL WEL
- [SDR 2014FA0000631](https://openairdocs.org/sdr/2014FA0000631), Jul 2, 2014: EXHAUST VALVE. FAILED. DURING CLIMBOUT, AT APPROXIMATELY 500FT AGL, THE ACFT BEGAN TO LOOSE ENGINE POWER, STUDENT ON CONTROLS TRANSFERED TO INSTRUCTOR. INSTRUCTOR ATTEMPTED TO RETURN 
- [SDR CA140429007](https://openairdocs.org/sdr/CA140429007), Apr 28, 2014: BAFFLE. COLLAPSED. (CAN) DURING A TRAINING FLIGHT, THE PILOT NOTICED SIGNIFICANT ENGINE POWER LOSS AND RETURNED TO BASE. UPON INSPECTION IT WAS FOUND THAT THE INTERNAL BAFFLE INSI
- [SDR CA131118026](https://openairdocs.org/sdr/CA131118026), Nov 15, 2013: HOSE. DETERIORATED. (CAN) DURING A 100 HR INSPECTION OF THE ACFT, IT WAS NOTED THAT THE RT FUEL TANK FLEX HOSE LINKING THE TANK TO THE ACFT FUEL SYS WAS IN POOR CONDITION. REMOVAL 
- [SDR 2013FA0000611](https://openairdocs.org/sdr/2013FA0000611), Sep 6, 2013: TURNBUCKLE. CRACKED. ONE CABLE HAS FRAYED STRANDS, THE OTHER CABLE HAS STRESS CRACKS IN TURNBUCKLE END. CABLES WERE FOUND ON ANNUAL INSPECTION AND AD COMPLIANCE. REPLACED CABLES.
- [SDR 2013FA0000610](https://openairdocs.org/sdr/2013FA0000610), Sep 6, 2013: CABLE. FRAYED. ONE CABLE HAS FRAYED STRANDS, THE OTHER CABLE HAS STRESS CRACKS IN TURNBUCKLE END. CABLES WERE FOUND ON ANNUAL INSPECTION AND AD COMPLIANCE. REPLACED CABLES.
- [SDR GQRR201306289952](https://openairdocs.org/sdr/GQRR201306289952), Apr 24, 2013: MANIFOLD. MALFUNCTIONED. ON LANDING ROLL OUT, THE ACFT SUSTAINED AN UN-COMMANDED STEERING INPUT AND SUBSEQUENTLY EXITED THE RUNWAY, DAMAGE WAS MINOR. TESTING CONCLUDED THE FAILURE TO BE
- [SDR 2013FA0000055](https://openairdocs.org/sdr/2013FA0000055), Jan 25, 2013: RIB. CORRODED. DURING AN ANNUAL INSPECTION, VISUAL INSPECTION UNVEILED THE OTBD RIB ON THE RT FLAP HAD EXCESSIVE CORROSION. AFTER UNRIVETING THE L/E SKIN, IT WAS DISCOVERED TH
- [SDR CA130819018](https://openairdocs.org/sdr/CA130819018), Oct 11, 2012: CLAMP. SEPARATED. (CAN) THE EXHAUST CLAMP ON THE LT OF THE EXHAUST HAS A PIN WHICH LOCATES THE CLAMP ON BOTH THE MUFFLER AND THE PIPE IT ATTACHES TO. THE PIN HAD ERODED TO THE PO
- [SDR 2012FA0000549](https://openairdocs.org/sdr/2012FA0000549), Aug 6, 2012: HOSE. FAILED. PILOT REPORTED AFTER LANDING, DURING FUEL TOP OFF FOR NEXT FLIGHT, A POOL OF OIL UNDER THE ENGINE COWL, INVESTIGATION SHOWED ONE OF THE OIL COOLER HOSES HAD SPL
- [SDR 2012FA0000508](https://openairdocs.org/sdr/2012FA0000508), May 26, 2012: EXHAUST VALVE. FAILED. NR 1 EXHAUST VALVE FAILED IN CRUISE.
- [SDR 2012FA0000312](https://openairdocs.org/sdr/2012FA0000312), May 11, 2012: CASTING. CRACKED. TWO INCH CRACK WAS DISCOVERED DURING A ANNUAL INSPECTION ON THE RT MLG CASTING, LOCATED AT THE UPPER OUTER ATTACHMENT EAR FOR THE LANDING GEAR TORQUE LINK.
- [SDR 2012FA0000202](https://openairdocs.org/sdr/2012FA0000202), Apr 22, 2012: AIR FILTER. FAILED. AIR FILTER ELEMENT CAME APART AT THE SEAM. SECOND ONE FOUND.
- [SDR CA120202006](https://openairdocs.org/sdr/CA120202006), Feb 2, 2012: SPAR. CRACKED. (CAN) VISUAL INSPECTION WITH LIGHT AND MIRROR THRU END, RIB BS 24 INDICATED LINES. CLOSER INSPECTION WITH VIDEO CAMARA FOUND THE CRACKS.

All 364: https://openairdocs.org/model/piper-beaumont-pa-28-140/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 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 SA04586CH](https://openairdocs.org/stc/SA04586CH): Installation of Electroair Back Up Battery Panel System Control. Electroair Aquisition Corp
- [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-beaumont-pa-28-140/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
- [066-106](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID126294031320260728184416.0001): Brake Lining. Game Aerospace, LLC · PMA PQ00052CB · Replaces Cleveland Wheels and Brakes P/N… · Jun 9, 2026
- [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
- [Petersen Dwg 
List Piper 
Cherokee 140/150](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID119557434120260423211203.0001): 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
- [P002-1247130-A021](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID146457202320250813154902.0001): Spinner Assembly. Aero Tech Aviation Design, LLC · PMA PQ04281CE · Replaces 35323,36850,14422-A,D3339 · Jul 31, 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
- [A78360](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169972944920250611143005.0001): Pump. Aero Accessories LLC · PMA PQ1206CE · Replaces Piper 481-666 · Jan 13, 2025
- [A76088](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID144449520020250611143006.0001): Pump. Aero Accessories LLC · PMA PQ1206CE · Replaces Piper 461-740 · Jan 13, 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
- [UAV-1004236-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179059944320230707211347.0001): AV-30-C. uAvionix Corporation · PMA PQ05445NM · Modification part · Jun 28, 2023
- [A76088](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID159963518520231018194104.0001): Pump. Aero Accessories, LLC · PMA PQ1206QE · Replaces Piper P/N:461-740 · Apr 6, 2023
- [A78360](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID144446956420231018194103.0001): Pump. Aero Accessories, LLC · PMA PQ1206QE · Replaces Piper P/N:481-666 · Apr 6, 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

All of them: https://openairdocs.org/model/piper-beaumont-pa-28-140/pma.md

## The same model under other registry codes

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

- [Piper PA-28-140](https://openairdocs.org/model/piper-pa-28-140): 4,258 registered aircraft, registry code 7102802
- [Piper/Miller PA-28-140](https://openairdocs.org/model/piper-miller-pa-28-140): 0 registered aircraft, registry code 7102800

---
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