# New Piper PA-44-180

- Type: Aircraft model (FAA registry)
- Registry code: 7104403
- Manufacturer (registry): NEW PIPER AIRCRAFT INC
- Model: PA-44-180
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Reciprocating
- Seats: 4
- Weight class: Up to 12,499 lb
- Certification: Type certificated
- Data sheet: [TCDS A19SO](https://openairdocs.org/tcds/A19SO) (OpenAirDocs)
- Holder: Piper Aircraft Inc.
- Registered aircraft: 4
- Page: https://openairdocs.org/model/new-piper-pa-44-180

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

## ADs that may apply (OpenAirDocs)

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

- [AD 2024-10-04](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 2015-26-08](https://openairdocs.org/ad/2015-26-08): Rudder Control System · Piper PA-44-180 and PA-44-180T. Effective Jan 20, 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 2006-12-07](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 2005-15-10](https://openairdocs.org/ad/2005-15-10): Combustion heater fuel pumps · Piper PA-34-200T, PA-34-220T, PA-44-180 and 1 more. Effective Aug 26, 2005
- [AD 2004-25-16 R1](https://openairdocs.org/ad/2004-25-16-R1): Fuel regulator shutoff valve · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant), CL-215-6B11 (CL-415 Variant) and 64 more. Effective Jun 20, 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 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 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 85-02-05 R1](https://openairdocs.org/ad/85-02-05-R1): Piper P/N s 81090-02, 683-107 Placard Installation · Lavia Argentina PA-25, PA-25-235, PA-25-260 and 32 more. Effective Nov 21, 1997
- [AD 96-10-03](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 94-13-11](https://openairdocs.org/ad/94-13-11): Main Landing Gear Trunnion · Piper PA-34-200, PA-34-200T, PA-34-220T and 2 more. Effective Aug 12, 1994
- [AD 81-16-10](https://openairdocs.org/ad/81-16-10): Outboard Leading Edge Skin · Piper PA-44-180 and PA-44-180T. Effective Sep 17, 1981
- [AD 81-10-04](https://openairdocs.org/ad/81-10-04): Aileron Modification · Piper PA-44-180. Effective Apr 30, 1981
- [AD 81-10-01](https://openairdocs.org/ad/81-10-01): Nose Cone Spars · Piper PA-44-180. Effective Apr 30, 1981
- [AD 80-21-11](https://openairdocs.org/ad/80-21-11): Left and Right Ailerons · Piper PA-44-180. Effective Oct 17, 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 80-12-03](https://openairdocs.org/ad/80-12-03): Nose Landing Gear · Piper PA-44-180. Effective Jun 3, 1980
- [AD 79-12-11](https://openairdocs.org/ad/79-12-11): Fuel Primer Modification Kits · Piper PA-44-180. Effective Jun 21, 1979
- [AD 79-05-11](https://openairdocs.org/ad/79-05-11): Engine Power Control Loss · Piper PA-44-180. Effective Mar 15, 1979
- [AD 79-02-02](https://openairdocs.org/ad/79-02-02): Fuel Supply Lines · Piper PA-44-180. Effective Jan 24, 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

Historical (superseded or no longer in force):

- [AD 2008-06-28 R1](https://openairdocs.org/ad/2008-06-28-R1) (historical): Primary Flight Displays (PFDs) · Avidyne Primary Flight Displays, 441, LC41-550FG and 22 more. Effective Apr 10, 2008
- [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 2003-11-14](https://openairdocs.org/ad/2003-11-14) (historical): Combustion heater fuel pump · Piper PA-34-200T, PA-34-220T, PA-44-180 and 1 more. Effective Jun 20, 2003

## Information bulletins (advisory) (13)

- [SAIB AIR-21-10](https://openairdocs.org/saib/AIR-21-10): Wing, Attach Fittings (JASC 5740). Issued Jun 29, 2021
- [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018
- [SAIB CE-11-12R1](https://openairdocs.org/saib/CE-11-12R1): Wings - PA-28, PA-32, PA-34, and PA-44 Rear Spar Corrosion at Fuselage Attach Fitting. Issued Dec 2, 2015
- [SAIB CE-14-23](https://openairdocs.org/saib/CE-14-23): Powerplant; Air Intake. Issued Aug 6, 2014
- [SAIB CE-11-42](https://openairdocs.org/saib/CE-11-42): Flight Controls: Control Cable/Pulley Inspections. Issued Jun 29, 2011
- [SAIB CE-11-37](https://openairdocs.org/saib/CE-11-37): Engine Oil: Oil Filter Interference. Issued May 31, 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-11-10](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-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 (4)

- [N231WU](https://openairdocs.org/aircraft/N231WU): built 2006, S/N 4496231
- [N356HA](https://openairdocs.org/aircraft/N356HA): [Hillsboro Aero Academy LLC](https://openairdocs.org/faa-owner/HILLSBORO%20AERO%20ACADEMY%20LLC), [Hillsboro, OR](https://openairdocs.org/faa-place/OR/Hillsboro), built 1978, S/N 44-7995004
- [N705BS](https://openairdocs.org/aircraft/N705BS): [Aims Community College](https://openairdocs.org/faa-owner/AIMS%20COMMUNITY%20COLLEGE), [Greeley, CO](https://openairdocs.org/faa-place/CO/Greeley), S/N 4496500
- [N885FT](https://openairdocs.org/aircraft/N885FT): [Florida Institute Of Technology](https://openairdocs.org/faa-owner/FLORIDA%20INSTITUTE%20OF%20TECHNOLOGY), [Melbourne, FL](https://openairdocs.org/faa-place/FL/Melbourne), built 2006, S/N 4496225

## NTSB investigations

None matched to aircraft with this model.

## 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.

- [Incident 20241209017709I](https://openairdocs.org/incident/20241209017709I), Dec 9, 2024: New Piper Aircraft Inc PA-44-180 (N885FT), Melbourne, FL, Minor damage. On December 9, 2024 at approximately 1130 EST, a 2006 Piper PA-44-180 departed lakeland-linder international airport (lal) for Melbourne-Orlando international…
- [Incident 20180227003169I](https://openairdocs.org/incident/20180227003169I), Feb 27, 2018: New Piper Aircraft Inc PA-44-180 (N885FT), St Cloud, FL, Minor damage. The 141 flight school reported a "significant bird strike" on the upper nose cone during a dual cross country flight, and provided the following details: "IAS…

## Service difficulty reports (882, newest 50)

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

- [SDR 2026FA0000909](https://openairdocs.org/sdr/2026FA0000909), Oct 16, 2026: DOWNLOCK SWITCH. DEFECTIVE. WHILE THE LANDING GEAR WAS DOWN AND LOCKED THE INDICATION ON DISPLAYS SHOWED AN UNSAFE NOSE GEAR. WHILE TROUBLESHOOTING IT WAS FOUND THAT THE NOSE GEAR DOWNLOCK
- [SDR 2026FA0000833](https://openairdocs.org/sdr/2026FA0000833), Oct 13, 2026: SQUAT SWITCH. DEFECTIVE. THE LEFT LANDING GEAR SQUAT SWITCH WAS FOUND TO BE DEFECTIVE/INOPERATIVE RESULTING IN A SAFETY CONCERN. IF SOMEONE WERE TO ACCIDENTALLY SELECT GEAR UP WHILE ON 
- [SDR 2026FA0000834](https://openairdocs.org/sdr/2026FA0000834), Oct 12, 2026: DOWNLOCK SWITCH. DEFECTIVE. LEFT LANDING GEAR DOWN LOCK SWITCH INTERMITTENT FAILURE. THE LEFT GEAR DOWNLOCK SWITCH WAS FOUND TO BE INTERMITTENT WHEN SLIGHT PRESSURE WAS APPLIED TO THE WIRE
- [SDR 2026FA0000829](https://openairdocs.org/sdr/2026FA0000829), Oct 12, 2026: SAFETY VALVE. LEAKING. LANDING GEAR EMERGENCY FREE-FALL VALVE FOUND TO BE LEAKING INTERNALLY, GEAR WILL NOT HOLD PRESSURE AND CONTINUES TO DROP FROM RETRACTED POSITION.
- [SDR 2026FA0000791](https://openairdocs.org/sdr/2026FA0000791), Sep 29, 2026: MOTOR. OVERHEATED. VENT MOTOR FOUND INOPERATIVE, WITH EVIDENCE OF OVERHEATING.
- [SDR 2026FA0000660](https://openairdocs.org/sdr/2026FA0000660), Aug 20, 2026: NUT. SHEARED. DURING THE AIRCRAFT'S FIRST 100 HOUR INSPECTION, THERE IS TASK TO RETORQUE THE ENGINE MOUNT-TO-FIREWALL BOLTS AS SPECIFIED IN MAINTENANCE MANUAL 71-00-00, FIGUR
- [SDR 2026FA0000574](https://openairdocs.org/sdr/2026FA0000574), Jun 19, 2026: STRUT. BROKEN. DURING TAXI, FAILURE OF THE LEFT MAIN LANDING GEAR OCCURRED AROUND THE OLEO STRUT PISTON TUBE BOLT HOLE. PIPER AIRCRAFT SERVICE LETTER 1263 RECOMMENDS ROUTINE I
- [SDR 2026FA0000522](https://openairdocs.org/sdr/2026FA0000522), Jun 10, 2026: HYDRAULIC SYSTEM. MALFUNCTIONED. HYDRAULIC PUMP WOULD NOT DEACTIVATE. RAN CHECKLIST AND NO CHANGE. HAD TO USE THE EMERGENCY GEAR HANDLE TO DROP THE GEAR, ALL 3 LDG CAME DOWN AFTER L/H MAIN SHOW
- [SDR 2026FA0000527](https://openairdocs.org/sdr/2026FA0000527), Jun 3, 2026: HYDRAULIC SYSTEM. LEAKING. LANDING GEAR POWER PACK LEAKING INTERNALLY
- [SDR 2026FA0000491](https://openairdocs.org/sdr/2026FA0000491), Jun 1, 2026: SAFETY VALVE. DEFECTIVE. LANDING GEAR EMERGENCY FREE-FALL VALVE FOUND TO BE LEAKING.
- [SDR 2026FA0000490](https://openairdocs.org/sdr/2026FA0000490), Jun 1, 2026: SAFETY VALVE. DEFECTIVE. LANDING GEAR EMERGENCY FREE-FALL VALVE FOUND TO BE LEAKING.
- [SDR 2026FA0000523](https://openairdocs.org/sdr/2026FA0000523), May 11, 2026: HYDRAULIC SYSTEM. MALFUNCTIONED. RECEIEVED A GEAR UNSAFE INDICATION ON SHORT FINAL ON THE NOSE GEAR. CYCLED THE GEAR ON UPWIND AND WE GOT 3 GREEN. LANDED WITHOUT ISSUE
- [SDR 2026FA0000488](https://openairdocs.org/sdr/2026FA0000488), Apr 16, 2026: SAFETY VALVE. DEFECTIVE. LANDING GEAR EMERGENCY FREE-FALL VALVE FOUND TO BE LEAKING.
- [SDR 2026FA0000266](https://openairdocs.org/sdr/2026FA0000266), Apr 13, 2026: BEARING. BROKEN. FOUND THE LEFT AND RIGHT HAND OUTBOARD NOSE GEAR TRUNNION ASSY BEARINGS BROKEN AT THEIR FLANGES RESULTING IN MUCH SIDE-TO-SIDE PLAY IN THE NOSE LANDING GEAR. IN
- [SDR 8HBR20260419080](https://openairdocs.org/sdr/8HBR20260419080), Apr 3, 2026: WIRE. BROKEN. PILOTS REPORTED NO GEAR DOWN AND LOCKED INDICATION FOR LH MAIN LANDING GEAR. INSPECTION REVEALED BROKEN WIRES ON THE LH MAIN LANDING GEAR DOWN LOCK SWITCH.
- [SDR 2026FA0000186](https://openairdocs.org/sdr/2026FA0000186), Mar 11, 2026: QUICK DISCONNECT. DEFECTIVE. WHILE IN FLIGHT THE LEFT ENGINE RPM READING BECAME ERRATIC, GOING FROM NORMAL TO PAST RED LINE QUICKLY BACK AND FORTH. PIC PRECAUTIONARY SHUT DOWN ENGINE AND RE
- [SDR 2026FA0000134](https://openairdocs.org/sdr/2026FA0000134), Feb 18, 2026: ACTUATOR. BLEW OUT. IT WAS AN OLD ACTUATOR THAT GAVE OUT ON A HARDER LANDING THAN NORMAL.
- [SDR 2026FA0000135](https://openairdocs.org/sdr/2026FA0000135), Jan 26, 2026: CONTROL CABLE. SHEARED. UPON TAKEOFF ROLL ON RUNWAY 33 AT X04, PILOTS WENT TO APPLY BACK PRESSURE ON THE YOKE TO BEGIN ROTATION AT 80KIAS AND REPORTED LACK OF AUTHORITY / CONTROL OF TH
- [SDR 2026FA0000023](https://openairdocs.org/sdr/2026FA0000023), Jan 12, 2026: BATTERY CABLE. BROKEN. NEGATIVE BATTERY CABLE TERMINAL END BROKEN
- [SDR 2025FA0000778](https://openairdocs.org/sdr/2025FA0000778), Nov 21, 2025: CABLE. CHAFED. DURING AIRCRAFT INSPECTION FOUND THAT THE LEFT ENGINE ALTERNATE AIR CABLE HAD CHAFED INTO THE ENGINE MOUNT REQUIRING IT TO BE SENT FOR REPAIR. THE WAY THE CABLE
- [SDR 2025FA0000777](https://openairdocs.org/sdr/2025FA0000777), Nov 20, 2025: CABLE. CHAFED. DURING AIRCRAFT INSPECTION FOUND THAT THE LEFT ENGINE ALTERNATE AIR CABLE HAD CHAFED INTO THE ENGINE MOUNT REQUIRING IT TO BE SENT FOR REPAIR. THE WAY THE CABLE
- [SDR 2025FA0000774](https://openairdocs.org/sdr/2025FA0000774), Oct 28, 2025: CABLE. CHAFED. DURING AIRCRAFT INSPECTION FOUND THAT THE LEFT ENGINE ALTERNATE AIR CABLE HAD CHAFED INTO THE ENGINE MOUNT REQUIRING IT TO BE SENT FOR REPAIR. THE WAY THE CABLE
- [SDR 2025FA0000776](https://openairdocs.org/sdr/2025FA0000776), Oct 2, 2025: PUMP. DEFECTIVE. DURING AIRCRAFT INSPECTION, THE LANDING GEAR HYDRAULIC PUMP WOULD INTERMITTENTLY FAIL DURING THE FUNCTIONAL TEST.
- [SDR 2025FA0000495](https://openairdocs.org/sdr/2025FA0000495), Jul 14, 2025: FUEL CELL. COLLAPSED. AIRCRAFT INSPECTED AFTER EMERGENCY LANDING AT OFFUTT AFB, NE. DETERMINED LH FUEL TANK TO BE EMPTY AND LH FUEL GAUGE READING 20 GALLONS. FUELED AIRCRAFT AND RAN,
- [SDR 2025FA0000262](https://openairdocs.org/sdr/2025FA0000262), Apr 11, 2025: IMPULSE COUPLING. FAILED. IN FLIGHT, RH ENGINE SUFFERED PARTIAL OIL PRESSURE LOSS. PRECAUTIONARY LANDING MADE AT KOXB. TROUBLESHOT LOSS OF OIL PRESSURE, DETERMINED TO BE AN INTERNAL ENGI
- [SDR 2025FA0000103](https://openairdocs.org/sdr/2025FA0000103), Feb 12, 2025: MAGNETO. CONTAMINATED. THE MAGNETO WAS FOUND TO HAVE A LARGE AMOUNT OF GREASE ON THE CAM, ENOUGH TO EASILY SLING INTO THE POINT ASSEMBLY WHICH WOULD CAUSE THE MAGNETO TO COMPLETELY FA
- [SDR 2025FA0000105](https://openairdocs.org/sdr/2025FA0000105), Feb 11, 2025: MAGNETO. CONTAMINATED. THE MAGNETO ROTOR SHEARED, THE MAGNETO DROPS DURING A CHECK WERE FOUND TO BE VERY HIGH. WHEN THE MAGNETO WAS REMOVED FROM THE ENGINE IT WAS FOUND THAT THE ROTOR
- [SDR 2025FA0000104](https://openairdocs.org/sdr/2025FA0000104), Feb 11, 2025: MAGNETO. CONTAMINATED. THE MAGNETO WAS FOUND TO HAVE A LARGE AMOUNT OF GREASE ON THE CAM, ENOUGH TO EASILY SLING INTO THE POINT ASSEMBLY WHICH WOULD CAUSE THE MAGNETO TO COMPLETELY FA
- [SDR 2025FA0000009](https://openairdocs.org/sdr/2025FA0000009), Jan 7, 2025: ACTUATOR. FAILED. CLEVELAND/PARKER HYDRAULIC ACTUATOR P/N11-17 CODE # 445-987. THE ACTUATOR FAILED SHORTLY AFTER TAKEOFF RESULTING IN A NOSE GEAR UP LANDING. AFT SECTION OF THE P
- [SDR 2024FA0000976](https://openairdocs.org/sdr/2024FA0000976), Dec 19, 2024: TUBE. SEPARATED. DURING THE LANDING ROLL-OUT THE LEFT MAIN GEAR COLLAPSED. THE INSPECTION OF THE LANDING GEAR REVEALED THAT THE MAIN GEAR TUBE SEPARATED FROM THE FORK AT THE MOU
- [SDR 2024FA0000773](https://openairdocs.org/sdr/2024FA0000773), Oct 3, 2024: MUFFLER. CRACKED. L/H ENGINE RUNNING ROUGH AT HIGHER POWER SETTINGS. EGT WAS 300-400 DEGREES HIGHER THAN NORMAL. L/H ENGINE RUNNING ROUGH AT HIGHER POWER SETTINGS. EGT WAS 300-40
- [SDR FQAR202409251214](https://openairdocs.org/sdr/FQAR202409251214), Sep 25, 2024: SHAFT. SHEARED. MAGNETO REMOVED AFTER 67 HRS IN SERVICE SINCE LAST 500HR INSPECTION, UPON DISSASSEMBLY FOUND THE DRIVE END OF THE ROTATING MAGNET SHAFT SHEARED INSIDE THE MAGNE
- [SDR 2024FA0000589](https://openairdocs.org/sdr/2024FA0000589), Aug 8, 2024: WIRE. LOOSE. UPON AIRCRAFT INSPECTION NOTED THE PLASTIC TAB ON TOP OF UNIT HOUSING CRACKED, WIRE LOOSE.
- [SDR 2024FA0000510](https://openairdocs.org/sdr/2024FA0000510), Jul 22, 2024: FLANGE. CRACKED. WHILE COMPLYING WITH PIPER SB1161D, CRACKING WAS DISCOVERED ON THE FLANGES IDENTIFIED BY THE SERVICE BULLETIN, ON BOTH WINGS. THE FLANGES WERE PART OF A PREVIOU
- [SDR 2024FA0000509](https://openairdocs.org/sdr/2024FA0000509), Jul 9, 2024: FLANGE. CRACKED. WHILE COMPLYING WITH PIPER SB1161D, CRACKING WAS DISCOVERED ON THE FLANGE IDENTIFIED BY THE SERVICE BULLETIN, ON THE LEFT WING. THE FLANGE WAS PART OF A PREVIOU
- [SDR 2024FA0000482](https://openairdocs.org/sdr/2024FA0000482), Jul 1, 2024: HYDRAULIC SYSTEM. DEFECTIVE. ON TAKE0OFF FROM TTN LANDING GEAR FAILED TO RETRACT. AIRCRAFT MADE AN UNSCHEDULED LANDING BACK AT TTN, TROUBLESHOOT TO A BAD LANDING GEAR HYDRAULIC POWER PACK.
- [SDR 2024FA0000455](https://openairdocs.org/sdr/2024FA0000455), Jun 18, 2024: RESERVOIR. LEAKING. HYDRAULIC POWER PACK SEVERE LEAK FROM RESERVOIR, PIPER PART NUMBER 601-940, GARKENYON PART NUMBER BELOW.
- [SDR 2024FA0000454](https://openairdocs.org/sdr/2024FA0000454), Jun 18, 2024: RESERVOIR. LEAKING. HYDRAULIC POWER PACK SEVERE LEAK FROM RESERVOIR, PIPER PART NUMBER 601-940,
- [SDR 2024FA0000453](https://openairdocs.org/sdr/2024FA0000453), Jun 18, 2024: POWERPACK. FAILED. HYDRAULIC POWER PACK FAILURE RESULTING IN EMERGENCY LANDING GEAR EXTENSION, PIPER PART NUMBER 601-940, GARKENYON PART NUMBER LISTED BELOW.
- [SDR 2024FA0000452](https://openairdocs.org/sdr/2024FA0000452), Jun 18, 2024: POWERPACK. DEFECTIVE. LANDING GEAR HYDRAULIC POWER PACK FAILURE RESULTING IN EMERGENCY GEAR EXTENSION ON LANDING. PIPER PART NUMBER 601-940,
- [SDR 2024FA0000411](https://openairdocs.org/sdr/2024FA0000411), May 30, 2024: HYDRAULIC SYSTEM. FAULTY. HYDRAULIC LANDING GEAR POWER PACK P/N 601-940 MANUFACTURER GARKENYON PART NUMBER 98827-1 FAILED AND LANDING GEAR EMERGENCY EXTENSION WAS REQUIRED TO LOWER LANDI
- [SDR 2024FA0000774](https://openairdocs.org/sdr/2024FA0000774), Mar 13, 2024: MUFFLER. CRACKED. R/H ENGINE DOES NOT DEVELOP FULL POWER. REMOVED DISASSEMBLED AND INSPECTED R/H AND L/H MAGNETOS PN: 4330, SN: 19121021 AND PN: 4330, SN: 19110026. FOUND POINTS 
- [SDR FQAR202311271214](https://openairdocs.org/sdr/FQAR202311271214), Nov 2, 2023: LANDING GEAR. BROKEN. LEFT MAIN GEAR DOWN LIGHT WOULD NOT COME ON, PILOT SWAPPED BULBS WITH NO CHANGE, PERFORMED EMERGENCEY GEAR EXTENSION WITH NO LIGHT, AIRCRAFT LANDED WITH NO PROB
- [SDR 2023FA0000681](https://openairdocs.org/sdr/2023FA0000681), Oct 25, 2023: PUMP. FAILED. HYDRAULIC PUMP ON INDICATION CAME ON. TRIED TO DEPLOY LANDING GEAR AND IT WOULDN'T EXTEND. HAD TO PULL EMERGENCY GEAR EXTEND. JACKED AIRCRAFT, APPLIED POWER TO 
- [SDR 2023FA0000574](https://openairdocs.org/sdr/2023FA0000574), Sep 28, 2023: SPRING. BROKEN. PA44 AIRCRAFT HAVE AN OUTER AND INNER SPRING THAT ASSISTS THE NOSE LANDING GEAR EXTENSION. IT IS BELIEVED THAT THE INNER SPRING (PN 67168-000) BROKE DURING FLIG
- [SDR 2023FA0000707](https://openairdocs.org/sdr/2023FA0000707), Jun 16, 2023: NUT. MISSING. LANDING ROLL OUT NOSE GEAR STEERING LINKAGE HARDWARE SEPARATED CAUSING LOSS OF DIRECTIONAL CONTROL.
- [SDR FQAR20231212](https://openairdocs.org/sdr/FQAR20231212), May 17, 2023: POWERPACK. MALFUNCTIONED. DURING THE REPAIR OF A LANDING GEAR ISSUE, THE POWERPACK WAS REPLACED WITH UNITS FROM INVENTORY, BOTH HYDRAULIC POWERPACKS WERE FOUND TO BE BYPASSING INTERNALLY
- [SDR FQAR20231211](https://openairdocs.org/sdr/FQAR20231211), May 17, 2023: POWERPACK. UNKNOWN. DURING THE REPAIR OF A LANDING GEAR ISSUE, THE POWERPACK WAS REPLACED WITH UNITS FROM INVENTORY, BOTH HYDRAULIC POWERPACKS WERE FOUND TO BE BYPASSING INTERNALLY
- [SDR NI1R552PC030623](https://openairdocs.org/sdr/NI1R552PC030623), Mar 6, 2023: OIL COOLER. CRACKED. DURING A DUAL TRAINING FLIGHT THE PILOT NOTICE THE OIL PRESSURE DROPPING AND THE OIL TEMP CLIMBING. A PRECAUTIONARY ENGINE SHUTDOWN WAS PERFORMED, AND THE AIRCR
- [SDR 2022FA0000691](https://openairdocs.org/sdr/2022FA0000691), Nov 15, 2022: TRANSDUCER. FLUCTUATES. PILOT ABORTED TAKEOFF DUE TO A HIGH OIL PRESSURE INDICATION. AIRCRAFT EXITED AND TAXIED TO PARKING WITHOUT INCIDENT, MAINTENANCE REPLACE A FAULTY OIL PRESSURE T

All 882: https://openairdocs.org/model/new-piper-pa-44-180/reports.md

## STCs that may be installed (OpenAirDocs) (199, 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 SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc
- [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 SA01120SE](https://openairdocs.org/stc/SA01120SE): Installation of Door Steward. Mountain View Aviation LLC
- [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 SA02760SE](https://openairdocs.org/stc/SA02760SE): Installation of Absolute Solutions LLC Gear Warning System Upgrade. Absolute Solutions 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 SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio. Peregrine
- [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 SA02725SE](https://openairdocs.org/stc/SA02725SE): Installation of Absolute Solutions LLC Gear Warning System Upgrade. Absolute Solutions LLC
- [STC SA00262AT](https://openairdocs.org/stc/SA00262AT): Installation of flap gap seals. Whelen Aerospace Technologies
- [STC SA00263AT](https://openairdocs.org/stc/SA00263AT): Installation of 'speed splitter' flap bracket fairings. Whelen Aerospace Technologies
- [STC SA00264AT](https://openairdocs.org/stc/SA00264AT): 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 SA00076IB](https://openairdocs.org/stc/SA00076IB): Installation of Photo luminescent Safety Systems. STG AEROSPACE GERMANY GmbH
- [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications 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 SA04195NY](https://openairdocs.org/stc/SA04195NY): Installation of the KFC 230 Aerocruze Automatic Flight Control System (FCS) upgraded from KFC 200 FCS. 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 2](https://openairdocs.org/stc/SA11174SC%20PAGE%202): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King)
- [STC SA02265SE](https://openairdocs.org/stc/SA02265SE): 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 SA4235WE](https://openairdocs.org/stc/SA4235WE): Installation of inflatable door seal. TALCO Aviation Corp
- [STC SA02426AK](https://openairdocs.org/stc/SA02426AK): Approval of the FreeFlight FDL-978-TX ADS-B system installed. FreeFlight Systems
- [STC SA01831WI](https://openairdocs.org/stc/SA01831WI): To allow the use of UL91 (minimum) grade aviation fuel. Petersen Aviation Inc
- [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 SA1504CE](https://openairdocs.org/stc/SA1504CE): Installation of King KFC 200 automatic flight control system, (2 axis), with or without flight director. Honeywell International Inc
- [STC SA2321CE-D](https://openairdocs.org/stc/SA2321CE-D): Installation of the Bendix/King KFC 150 two axis Automatic Flight Control System. Honeywell International Inc
- [STC SA01560WI-D](https://openairdocs.org/stc/SA01560WI-D): Installation of the Honeywell KFD 840 Primary Flight Display System. 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

All 199: https://openairdocs.org/model/new-piper-pa-44-180/stcs.md

## PMA parts (OpenAirDocs) (over 1,000, first 50)

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

- [73-CFG-R](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139218545420260806152425.0001): Fuel Quantity Indication Placard. Swift Fuels, LLC · PMA PQ04423CE · Modification part · Jul 20, 2026
- [S1069](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID113256326820260806152332.0001): 100R Fuel Placard. Swift Fuels, LLC · PMA PQ04423CE · Modification part · Jul 20, 2026
- [066-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID120510874920260723131534.0001): Rivet. Game Aerospace, LLC · PMA PQ00052CB · Replaces Cleveland Wheels and Brakes P/N… · Jun 9, 2026
- [RAP164-21600](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132311683620260722154733.0001): Brake Disc. Rapco Inc. · PMA PQ2101CE · Replaces 164-21600 · Jun 3, 2026
- [RAP164-02300](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID131469465520260722154717.0001): Brake Disc. Rapco Inc. · PMA PQ2101CE · Replaces 164-02300 · Jun 3, 2026
- [MC67184-000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID183977842120260722151904.0001): Axle. Airforms LLC · PMA PQ2644CE · Replaces 67184-000 · May 6, 2026
- [AS-GHBA-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID121296658520260508190540.0001): Gear Horn and Bracket Assembly. Absolute Solutions LLC · PMA PQ05464NM · Modification part · May 4, 2026
- [KATS-13-002](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID197186573820260320170103.0001): Electric Air Conditioning System. Kelly Aerospace Thermal Systems, LLC · PMA PQ2727CE · Modification part · Mar 16, 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
- [MC9812-0025-101](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132413113220250929141437.0001): Fuel Level Sender. McFarlane Aviation Inc. · PMA PQ3732CE · Replaces PAC86688-002, 548-218, 7740‑00164 · Sep 5, 2025
- [AL24-P70-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID120990538120250925194441.0001): Alternator Assembly, 24V. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces 602-484 · May 14, 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
- [A80543](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID126120293520250611143006.0001): Pump. Aero Accessories LLC · PMA PQ1206CE · Replaces Piper 481-842 · 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
- [A89364-012](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID108105319320241030141800.0001): Clamp. Aerospace Welding Minneapolis, Inc. · PMA PQ2712CE · Replaces 89364-012 · Aug 16, 2024
- [A89364-019](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID101333476420241030141759.0001): Shroud Assembly, Carburetor Heat. Aerospace Welding Minneapolis, Inc. · PMA PQ2712CE · Replaces 89364-003, 89364-019 · Aug 16, 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
- [90D39-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165136830320250729170755.0001): Heater Blower. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces 90D39-1,452-955 · Jan 8, 2024
- [90D39-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID122765715020250729170755.0001): Heater Blower. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces 90D39-2,689-941 · Jan 8, 2024
- [SG8995](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193035766520231121213647.0001): Flexible Overcarpet for SSUL with Tape. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8995 · Nov 20, 2023
- [10-50011-XFCCC](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID191347028920231121213639.0001): SSUL-X11 Track Assembly. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 10-50011-XFCCC · Nov 20, 2023
- [12-50013](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178425299820231121213802.0001): Assembly: saf-Tglo® Whiter Background Door Operation Signage. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50013 · Nov 20, 2023
- [10-50008-XFCCC](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID173001492420231121213614.0001): SSUL-X Track Assembly. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 10-50008-XFCCC · Nov 20, 2023
- [12-50003](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID170771092320231121213727.0001): Assembly: saf-Tglo® Exit (USES). STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50003 · Nov 20, 2023
- [12-50009](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165218956220231121213748.0001): Assembly: saf-Tglo® Whiter Background EXIT Sign (Text). STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50009 · Nov 20, 2023
- [30-50001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID159388179720231121213713.0001): Scapa 5169 Filler. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 30-50001 · Nov 20, 2023
- [12-50011](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID146035034520231121213755.0001): Assembly: saf-Tglo® Whiter Background EXIT Sign (USES). STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50011 · Nov 20, 2023
- [10-50010-XFCCC](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132009636520231121213631.0001): SSUL-X11 Lateral Extension Track Assembly. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 10-50010-XFCCC · Nov 20, 2023
- [12-50007](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID124681546620231121213741.0001): Assembly: saf-Tglo® Supplemental Signage/Placard. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50007 · Nov 20, 2023
- [12-50001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID122834804820231121213720.0001): Assembly: saf-Tglo® Exit (Text). STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50001 · Nov 20, 2023
- [10-50009-XFCCC](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID122183612920231121213622.0001): SSUL-X Lateral Extension Track Assembly. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 10-50009-XFCCC · Nov 20, 2023
- [12-50005](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID121113655120231121213733.0001): Assembly: saf-Tglo® Door Operation Sign. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50005 · Nov 20, 2023
- [SG8996](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID119996075220231121213656.0001): Flexible Overcarpet End Cap for SSUL with Tape. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8996 · Nov 20, 2023
- [SG8916](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID115804351820231121213705.0001): Filler. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8916 · Nov 20, 2023
- [ASGWS-MDL-000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID170074401120231108181644.0001): PA-44-180 Gear Warning upgrade. Absolute Solutions LLC · PMA PQ05464NM · Modification part · Oct 31, 2023
- [ASGH-MDL-000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID117622013020231108181644.0001): PA-44-180 Gear Horn Upgrade. Absolute Solutions LLC · PMA PQ05464NM · Modification part · Oct 31, 2023
- [AA617053](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID135238710720240813144831.0001): Induction Air Filter. Aero Accessories LLC · PMA PQ1206CE · Replaces Donaldson P617053Piper Aircraft… · Oct 17, 2023
- [APS68-01100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID102488499820231102131426.0001): Shim, Brake. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 068-01100 · Sep 25, 2023
- [UAV-1004236-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179059944320230707211347.0001): AV-30-C. uAvionix Corporation · PMA PQ05445NM · Modification part · Jun 28, 2023
- [A80543](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID174000232920231018194108.0001): Pump. Aero Accessories, LLC · PMA PQ1206QE · Replaces Piper P/N:481-842 · Apr 6, 2023
- [APS66-10500](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165749710520221020170258.0001): Brake Lining. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 066-10500 · Aug 10, 2022
- [APS177-00300](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID156099139020221020170337.0001): Pin. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 177-00300 · Aug 10, 2022
- [APS66-06200](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID138096606220221020170231.0001): Brake Lining. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 066-06200 · 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
- [01-0790906-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID128707842020220706160210.0001): LED Landing Light. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · Jun 21, 2022
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID157614225820220809130916.0001): Aviation Devices & Electronic Components LLC (Av-DEC) · PMA PQ3846SW · May 10, 2022
- [EA-9000A](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193786240420220525194006.0001): Crank Shaft Trigger Wheel Kit (Lycoming STD and Aerobatic). Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Apr 25, 2022

All of them: https://openairdocs.org/model/new-piper-pa-44-180/pma.md

## The same model under other registry codes

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

- [Piper PA-44-180](https://openairdocs.org/model/piper-pa-44-180): 402 registered aircraft, registry code 7104402
- [Piper PA-44-180](https://openairdocs.org/model/piper-pa-44-180): 158 registered aircraft, registry code 7104406

---
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.