# Service difficulty reports: Piper PA-44-180 A list on [Piper PA-44-180](https://openairdocs.org/model/piper-pa-44-180.md). Newest first. General aviation reporting is voluntary. Page 1 of 18 · 881 reports - [SDR 2026FA0000833](https://openairdocs.org/sdr/2026FA0000833.md): Squat Switch · defective · Oct 13, 2026 · N869AT · Piper PA44180 · Landing Gear Position and Warning > 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 THE GROUND, THE GEAR WOULD RETRACT. THE FUNCTION OF THE SWITCH IS TO PREVENT THIS FROM HAPPENING. TH - [SDR 2026FA0000834](https://openairdocs.org/sdr/2026FA0000834.md): Downlock Switch · defective · Oct 12, 2026 · N897AT · Piper PA44180 · Landing Gear Position and Warning > 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 HARNESS AT BASE OF SWITCH. A LANDING GEAR UNSAFE INDICATION WAS REPORTED ON THE LEFT GEAR 09/23/202 - [SDR 2026FA0000829](https://openairdocs.org/sdr/2026FA0000829.md): Safety Valve · leaking · Oct 12, 2026 · N864AT · Piper PA44180 · Landing Gear Retraction/Extension System > 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.md): Motor · overheated · Sep 29, 2026 · N443BG · Piper PA44180 · Air Distribution Fan > VENT MOTOR FOUND INOPERATIVE, WITH EVIDENCE OF OVERHEATING. - [SDR 2026FA0000660](https://openairdocs.org/sdr/2026FA0000660.md): Nut · sheared · Aug 20, 2026 · N60WU · Piper PA44180 · Engine Mount Section > 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, FIGURE 1. DURING TORQUE CHECK, FOUND MULTIPLE NUTS UNDER-TORQUED AND ONE NUT THAT FAILED, SHEARING INTO M - [SDR 2026FA0000574](https://openairdocs.org/sdr/2026FA0000574.md): Strut · broken · Jun 19, 2026 · N145WW · Piper PA44180 · Main Landing Gear Strut/Axle/Truck > 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 INSPECTION OF THIS FAILURE POINT EVERY 700 HOURS TIS ON AIRCRAFT WITH OVER 6,500 TOTAL HOURS IN SERV - [SDR 2026FA0000522](https://openairdocs.org/sdr/2026FA0000522.md): Hydraulic System · malfunctioned · Jun 10, 2026 · N890ND · Piper PA44180 · Hydraulic System, Main > 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 SHOWED RED. LANDED WITH NO ISSUE - [SDR 2026FA0000527](https://openairdocs.org/sdr/2026FA0000527.md): Hydraulic System · leaking · Jun 3, 2026 · N897ND · Piper PA44180 · Hydraulic System, Main > LANDING GEAR POWER PACK LEAKING INTERNALLY - [SDR 2026FA0000491](https://openairdocs.org/sdr/2026FA0000491.md): Safety Valve · defective · Jun 1, 2026 · N898AT · Piper PA44180 · Landing Gear Retraction/Extension System > LANDING GEAR EMERGENCY FREE-FALL VALVE FOUND TO BE LEAKING. - [SDR 2026FA0000490](https://openairdocs.org/sdr/2026FA0000490.md): Safety Valve · defective · Jun 1, 2026 · N867AT · Piper PA44180 · Landing Gear System > LANDING GEAR EMERGENCY FREE-FALL VALVE FOUND TO BE LEAKING. - [SDR 2026FA0000523](https://openairdocs.org/sdr/2026FA0000523.md): Hydraulic System · malfunctioned · May 11, 2026 · N896ND · Piper PA44180 · Landing Gear System > 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.md): Safety Valve · defective · Apr 16, 2026 · N867AT · Piper PA44180 · Landing Gear Retraction/Extension System > LANDING GEAR EMERGENCY FREE-FALL VALVE FOUND TO BE LEAKING. - [SDR 2026FA0000266](https://openairdocs.org/sdr/2026FA0000266.md): Bearing · broken · Apr 13, 2026 · N445BG · Piper PA44180 · Fuselage, Landing Gear Attach Fittings > 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. INSPECTION OF THE O.D. OF THE TRUNNION ASSY IN WHICH THE BEARINGS ARE INSTALLED WAS IN TOLERANCE. NO O - [SDR 8HBR20260419080](https://openairdocs.org/sdr/8HBR20260419080.md): Wire · broken · Apr 3, 2026 · N125MG · Piper PA44180 · Landing Gear System Wiring > 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.md): Quick Disconnect · defective · Mar 11, 2026 · N8024Q · Piper PA44180 · Engine RPM Indicating System > 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 RETURNED TO HOME FIELD. AFTER TROUBLESHOOTING IT WAS FOUND THE LEFT HAND TACH GENERATOR SENSOR PLASTIC - [SDR 2026FA0000134](https://openairdocs.org/sdr/2026FA0000134.md): Actuator · blew out · Feb 18, 2026 · N4405Q · Piper PA44180 · Landing Gear Actuator > IT WAS AN OLD ACTUATOR THAT GAVE OUT ON A HARDER LANDING THAN NORMAL. - [SDR 2026FA0000135](https://openairdocs.org/sdr/2026FA0000135.md): Control Cable · sheared · Jan 26, 2026 · N292ND · Piper PA44180 · Stabilizer Control System > 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 THE HORIZONTAL STABILATOR AND ABORTED TAKEOFF. PILOTS TAXI'D BACK TO TAXIWAY A4 AND SQUAWKED / GROUNDE - [SDR 2026FA0000023](https://openairdocs.org/sdr/2026FA0000023.md): Battery Cable · broken · Jan 12, 2026 · N318PA · Piper PA44180 · Electrical Power System Wiring > NEGATIVE BATTERY CABLE TERMINAL END BROKEN - [SDR 2025FA0000778](https://openairdocs.org/sdr/2025FA0000778.md): Cable · chafed · Nov 21, 2025 · N221FL · Piper PA44180 · Engine Mount Section > 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 IS ROUTED AND SECURED FROM THE FACTORY IS WITH ADEL CLAMPS AND SILICONE UNDER THE CABLE. OVER TIME - [SDR 2025FA0000777](https://openairdocs.org/sdr/2025FA0000777.md): Cable · chafed · Nov 20, 2025 · N260FL · Piper PA44180 · Engine Mount Section > 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 IS ROUTED AND SECURED FROM THE FACTORY IS WITH ADEL CLAMPS AND SILICONE UNDER THE CABLE. OVER TIME - [SDR 2025FA0000774](https://openairdocs.org/sdr/2025FA0000774.md): Cable · chafed · Oct 28, 2025 · N280FG · Piper PA44180 · Engine Mount Section > 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 IS ROUTED AND SECURED FROM THE FACTORY IS WITH ADEL CLAMPS AND SILICONE UNDER THE CABLE. OVER TIME - [SDR 2025FA0000776](https://openairdocs.org/sdr/2025FA0000776.md): Pump · defective · Oct 2, 2025 · N8024Q · Piper PA44180 · Hydraulic Pump (Electric/Engine), Main > DURING AIRCRAFT INSPECTION, THE LANDING GEAR HYDRAULIC PUMP WOULD INTERMITTENTLY FAIL DURING THE FUNCTIONAL TEST. - [SDR 2025FA0000495](https://openairdocs.org/sdr/2025FA0000495.md): Fuel Cell · collapsed · Jul 14, 2025 · N450VV · Piper PA44180 · Fuel Storage > 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, NO DISCREPANCIES NOTED. AIRCRAFT FLOWN BACK TO CBF AIRPORT. DRAINED FUEL FROM AIRCRAFT. REMOVE - [SDR 2025FA0000262](https://openairdocs.org/sdr/2025FA0000262.md): Impulse Coupling · failed · Apr 11, 2025 · N8024Q · Piper PA44180 · Magneto/Distributor > IN FLIGHT, RH ENGINE SUFFERED PARTIAL OIL PRESSURE LOSS. PRECAUTIONARY LANDING MADE AT KOXB. TROUBLESHOT LOSS OF OIL PRESSURE, DETERMINED TO BE AN INTERNAL ENGINE ISSUE. REMOVED ENGINE FROM SERVICE AND SENT TO COLUMBIA AIRCRAFT SERVICES INC. FOR INSPECTION/REP - [SDR 2025FA0000103](https://openairdocs.org/sdr/2025FA0000103.md): Magneto · contaminated · Feb 12, 2025 · N5823A · Piper PA44180 · Magneto/Distributor > 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 FAIL. THIS WAS AN OUT OF BOX ISSUE, NEW MAGNETO. - [SDR 2025FA0000105](https://openairdocs.org/sdr/2025FA0000105.md): Magneto · contaminated · Feb 11, 2025 · N834AT · Piper PA44180 · Magneto/Distributor > 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 SHAFT HAD COMPLETELY SHEARED. - [SDR 2025FA0000104](https://openairdocs.org/sdr/2025FA0000104.md): Magneto · contaminated · Feb 11, 2025 · N834AT · Piper PA44180 · Magneto/Distributor > 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 FAIL. THIS WAS AN OUT OF BOX ISSUE, NEW MAGNETO. - [SDR 2025FA0000009](https://openairdocs.org/sdr/2025FA0000009.md): Actuator · failed · Jan 7, 2025 · N885FT · Piper PA44180 · Landing Gear Actuator > 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 PART SEPARATED UNDER PRESSURE BY BLOWING OUT THE RETAINMENT C-CLIP AND PART OF THE RETAINMENT HOUSING - [SDR 2024FA0000976](https://openairdocs.org/sdr/2024FA0000976.md): Tube · separated · Dec 19, 2024 · N827AT · Piper PA44180 · Main Landing Gear > 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 MOUNT. FURTHER INSPECTION INDICATED THAT THE TUBE HAD CRACKED AT THE MOUNT AND EVENTUALLY SHEARED OFF C - [SDR 2024FA0000773](https://openairdocs.org/sdr/2024FA0000773.md): Muffler · cracked · Oct 3, 2024 · N280AG · Piper PA44180 · Engine Noise Suppressor > 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 300-400 DEGREES HIGHER THAN NORMAL."- FOUND FORWARD AND AFT EXHAUST MUFFLER BAFFLES CRACKED AND CREATING - [SDR FQAR202409251214](https://openairdocs.org/sdr/FQAR202409251214.md): Shaft · sheared · Sep 25, 2024 · N302PA · Piper PA44180 · Magneto/Distributor > 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 MAGNET BODY - [SDR 2024FA0000589](https://openairdocs.org/sdr/2024FA0000589.md): Wire · loose · Aug 8, 2024 · N221FL · Piper PA44180 · Hydraulic Power System Wiring > UPON AIRCRAFT INSPECTION NOTED THE PLASTIC TAB ON TOP OF UNIT HOUSING CRACKED, WIRE LOOSE. - [SDR 2024FA0000510](https://openairdocs.org/sdr/2024FA0000510.md): Flange · cracked · Jul 22, 2024 · N3128T · Piper PA44180 · Wing, Rib/Bulkhead > 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 PREVIOUSLY INSTALLED REPAIR KIT AND WERE NOT THE WING RIB'S ORIGINAL FLANGE. THE REPAIR KIT IS NOT AN ADEQU - [SDR 2024FA0000509](https://openairdocs.org/sdr/2024FA0000509.md): Flange · cracked · Jul 9, 2024 · N336PA · Piper PA44180 · Landing Gear System > 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 PREVIOUSLY INSTALLED REPAIR KIT AND WAS NOT THE WING RIB'S ORIGINAL FLANGE. THE REPAIR KIT IS NOT AN ADEQUA - [SDR 2024FA0000482](https://openairdocs.org/sdr/2024FA0000482.md): Hydraulic System · defective · Jul 1, 2024 · N260FL · Piper PA44180 · Hydraulic System, Main > 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.md): Reservoir · leaking · Jun 18, 2024 · N221FL · Piper PA44180 · Hydraulic Power Accumulator, Main > HYDRAULIC POWER PACK SEVERE LEAK FROM RESERVOIR, PIPER PART NUMBER 601-940, GARKENYON PART NUMBER BELOW. - [SDR 2024FA0000454](https://openairdocs.org/sdr/2024FA0000454.md): Reservoir · leaking · Jun 18, 2024 · N221FL · Piper PA44180 · Hydraulic Power Accumulator, Main > HYDRAULIC POWER PACK SEVERE LEAK FROM RESERVOIR, PIPER PART NUMBER 601-940, - [SDR 2024FA0000453](https://openairdocs.org/sdr/2024FA0000453.md): Powerpack · failed · Jun 18, 2024 · N221FL · Piper PA44180 · Hydraulic System, Main > 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.md): Powerpack · defective · Jun 18, 2024 · N8024Q · Piper PA44180 · Hydraulic System, Main > 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.md): Hydraulic System · faulty · May 30, 2024 · N275FL · Piper PA44180 · Hydraulic System, Main > 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 LANDING GEAR AND LAND SAFELY, EMERGENCY WAS DECLARED. UPON FURTHER INSPECTION HYDRAULIC POWER PACK WAS FO - [SDR 2024FA0000774](https://openairdocs.org/sdr/2024FA0000774.md): Muffler · cracked · Mar 13, 2024 · N278AG · Piper PA44180 · Engine Noise Suppressor > 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 AND ROTORS IN BOTH L/H AND R/H MAGNETOS TO HAVE EXCESSIVE WEAR AND SIGNS OF ARCING. INSTALLED NEW L - [SDR FQAR202311271214](https://openairdocs.org/sdr/FQAR202311271214.md): Landing Gear · broken · Nov 2, 2023 · N302PA · Piper PA44180 · Landing Gear System > 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 PROBLEM, AIRCRAFT WAS MOVED INTO THE MAINT HANGAR AND PLACED ON JACKS. DURING TROUBLE SHOOTING A BROKEN - [SDR 2023FA0000681](https://openairdocs.org/sdr/2023FA0000681.md): Pump · failed · Oct 25, 2023 · N221FL · Piper PA44180 · Hydraulic Pump (Electric/Engine), Main > 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 HYDRAULIC PUMP SELECTED GEAR UP, FAILURE CONFIRMED. RELAYS ACTUATED BUT PUMP DID NOT TURN ON. GRASP - [SDR 2023FA0000574](https://openairdocs.org/sdr/2023FA0000574.md): Spring · broken · Sep 28, 2023 · N4405Q · Piper PA44180 · Landing Gear Retraction/Extension System > 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 FLIGHT. WHEN THE NOSE GEAR IS RETRACTED THIS SPRING IS EXTENDED. WHEN THE SPRING TANG BROKE THE SPRING C - [SDR 2023FA0000707](https://openairdocs.org/sdr/2023FA0000707.md): Nut · missing · Jun 16, 2023 · N870CA · Piper PA44180 · Landing Gear Steering System > LANDING ROLL OUT NOSE GEAR STEERING LINKAGE HARDWARE SEPARATED CAUSING LOSS OF DIRECTIONAL CONTROL. - [SDR FQAR20231212](https://openairdocs.org/sdr/FQAR20231212.md): Powerpack · malfunctioned · May 17, 2023 · Piper PA44180 · Hydraulic Power System > 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 AND WOULD NOT DEVOLOPE SUFFICIANT PRESSURE TO OPERATE THE SHUT OFF SWITCH. - [SDR FQAR20231211](https://openairdocs.org/sdr/FQAR20231211.md): Powerpack · unknown · May 17, 2023 · Piper PA44180 · Hydraulic Power System > 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 AND WOULD NOT DEVOLOPE SUFFICIANT PRESSURE TO OPERATE THE SHUT OFF SWITCH. - [SDR NI1R552PC030623](https://openairdocs.org/sdr/NI1R552PC030623.md): Oil Cooler · cracked · Mar 6, 2023 · N552PC · Piper PA44180 · Engine Fuel/Oil Cooler > 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 AIRCRAFT RETURNED TO THE AIRPORT. THE INVESTIGATION REVEALED THE L/H OIL COOLER HAD CRACKED ALONG THE BOT - [SDR 2022FA0000691](https://openairdocs.org/sdr/2022FA0000691.md): Transducer · fluctuates · Nov 15, 2022 · N886FT · Piper PA44180 · Engine Oil Indicating System > PILOT ABORTED TAKEOFF DUE TO A HIGH OIL PRESSURE INDICATION. AIRCRAFT EXITED AND TAXIED TO PARKING WITHOUT INCIDENT, MAINTENANCE REPLACE A FAULTY OIL PRESSURE TRANSDUCER, THE AIRCRAFT HAS MADE SEVERAL FLIGHT WITHOUT FURTHER INCIDENT. - [SDR ECPR2022160000001](https://openairdocs.org/sdr/ECPR2022160000001.md): Points · failed · Sep 9, 2022 · N5911L · Piper PA44180 · Magneto/Distributor > DURING RUNUP, CREW FOUND THAT THE LEFT ENGINE QUIT WHEN THE LEFT MAGNETO WAS SELECTED. THE MAGNETO WAS REPLACED. THE REMOVED MAGNETO WAS DISASSEMBLED AND INSPECTED. THE PORTION OF THE PRIMARY CONTACT POINTS THAT IS ACTED UPON BY THE CAM WAS FOUND BROKEN FRE Next page: https://openairdocs.org/model/piper-pa-44-180/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = 'PA44180' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/model/piper-pa-44-180/reports --- 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.