Pratt & Whitney PW4168
Service difficulty reports · 32
Newest first. General aviation reporting is voluntary.
Query with SQL
duckdb -csv -c "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 engine_model_key = 'PW4168' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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 engine_model_key = 'PW4168' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DALA2025090806595Plug · missingATB DUE TO NR 2 ENG ANTI-ICE FAILURE. INSTALLED MISSING PLUG ON ANTI-ICE VALVE. OK FOR SERVICE. (7073340)SDR DALA2024112011091Elec Connector · unsecureSHIP 3355 - ATB - DUE TO DUAL ENGINE BLEED FAULTS. CORRECTIVE ACTION: SECURED CANNON PLUG 9HA1, R/R NUMBER 1 AND NUMBER 2 PRVS, AND REPLACED SENSE LINE FOR NUMBER 2 PRV. OPS CHECK GOOD. (6699742)SDR DALA2024052805569Engine · odorSHIP 3304 MUSTY ODOR NOTED IN FLIGHT DECK DURING CLIMBOUT AND DESCENT. CORRECTIVE ACTION: R/R #1 ENGINE PER A330 AMM 71-01. OK FOR SERVICE. (5323930)SDR AALA201810029009Compressor · stalledDURING INITIAL TAKE OFF, EXPERIENCED TWO VIOLENT COMPRESSOR STALLS ON THE RIGHT ENGINE. REJECTED TAKE OFF AND RETURNED BACK TO GATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED ENGINE IAW 33L40071001.SDR AN0R2017705009Beam · wornFAN REVERSER ASSEMBLY WITH A WEAR AREA MEASURING UP TO .038 DEEP ALONG THE ENTIRE LENGTH OF THE LOWER LATCH BEAM AUXILIARY GUIDE RAIL.SDR AN0R20170210003Beam · wornFAN REVERSER LOWER LATCH BEAM EXHIBITS WEAR COMMON TO THE AUXILIARY GUIDE RAIL MEASURING .065 INCHES DEEP THE ENTIRE LENGTH OF GUIDE RAIL.SDR AN0R20170210004Beam · wornFAN REVERSER LOWER LATCH BEAM EXHIBITS WEAR MEASURING .045" DEEP COMMON TO AUXILIARY GUIDE RAIL ALONG ENTIRE LENGTH OF GUIDE RAIL.SDR AN0R20170208002Beam · wornFAN REVERSER ASSEMBLY WITH A WEAR AREA MEASURING UP TO .030 DEEP ALONG THE ENTIRE LENGTH OF THE LOWER LATCH BEAM AUXILIARY GUIDE RAIL.SDR AN0R20170208001Frame · crackedFAN REVERSER FORWARD TORQUE BOX FRAME (LH) P/N: 73M100-003 EXHIBITED ONE CRACK APPROXIMATELY .650” LONG AT THE UPPER EOP.SDR DALA1022133355Seat Track · corrodedDURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y1959, FR19 & FR24. REPAIRED IAW SRM 51-42-11.SDR DALA1022153355Seat Track · corrodedDURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y450 FR62 TO FR65. REPAIRED IAW SRM 51-42-11.SDR DALA1022183355Seat Track · corrodedDURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y450 FR53.8-FR53.9 & FR54. REPAIRED IAW SRM 51-42-11.SDR DALA1021563355Seat Track · corrodedDURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y1959, FR64, FR65 & FR 68. REPAIRED IAW SRM 53-42-11.SDR DALA108453352Seat Track · corrodedDURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y1959 FR58. REPAIRED IAW ERA 481350-14 REV O AND COMPLETED ASSOCIATED ERA 13-481350.SDR DALA105543307Seat Track · corrodedDURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y450 FR69. REPLACED SEAT TRACK IAW SRM 51-42-11.SDR BA08017Wire Harness · faultyPHL - FLT 754 EN-ROUTE PHL TO CDG. THE AIRCRAFT FAILED THE VERIFICATION FLIGHT FOR AN ENGINE 1 EGT INDICATION INOPERATIVE. THE FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED ENGINE 1 EGT WIRE HARNESS. OPERATIONALLY CHECKSSDR BA08016Relay · unserviceablePHL FLT 754 - EN ROUTE PHL - CDG. DURING FLIGHT, RECEIVED ECAM MESSAGE "AUTO FLT A/THR OFF", AND " ENG 1 EPR MODE FAULT". THE FLIGHT RETURNED TO FIELD PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NUMBER ONE ENGINE RELAY UNIT. OPERATIONSDR USAA050179Floor Support · corrodedBFM - S1 - AUX BEAM SUPPORT, (1.0 INCH L X 1.0 INCH W X .050 INCH D) CORROSION; LEVEL 2; TASK NR J7-900-09000-015, FR 71.8, Y2080- Z240. REMOVED AND REPLACED WITH NEW PORT IAW SRM. (K)SDR CA040617006Relay · failedCOFFEEMAKER WAS REMOVED DUE TO TRIPPING CIRCUIT BREAKER. STRIP REPORT REVEALED THAT THE UNAPPROVED RELAY WAS FITTED TO THE COFFEEMAKER. CORRECT P/N KR-90693-1 P/N FOUND KR 14DGE24.SDR CA030723006Web · torn(CAN) ON ARRIVAL, MAINTENANCE NOTICED APPROXIMATELY 18 INCHES OF METAL PROTRUDING INTO THE AIR STREAM OF NR 1 ENGINE INBOARD THRUST REVERSER, JUST FORWARD OF THE CASCA DE VANES. FURTHER INVESTIGATION REVEALEDTHE DAMAGE TO BE THAT THE TORQUE-BOX FLOW WEB PANELSDR USAABA03017Eec · malfunctionedPHL - FLT 196 - EN ROUTE, CREW RECEIVED THE ECAM WARNING 'ENG 1 FADEC A FAULT.' FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE EEC. (M)SDR CA030328006Slide · malfunctioned(CAN) DURING DEPLOYMENT OF SLIDE RAFT L1 AND L4, AUTOMATIC INFLATION DID NOT OCCUR. DOOR AND SLIDE BOTTLE PRESSURES WERE IN THE GREEN RANGE. DEPLOYMENT NORMAL UP TO POINT OF SPEED LACING NOT RELEASING. MANUAL INFLATION HANDLE PULLED AND REMAINING DEPLOYMENT WASDR CA030304004Mount · burned(CAN) A/C ARRIVED YVR WITH APU INOP. INSPECTION OF THE 5000VE PANEL REVEALED THAT THE FUSE F/N 6KA1 WAS INFACT BLOWN. CLOSER INSPECTION ALSO FOUND THAT ONE STUD BOLT OF THE MOUNT P/N NSA931190-1 THAT THE FUSE SITS ON WAS HEAVILY DAMAGED BY EXTREME HEAT. NUT OSDR CA021223004Controller · malfunctioned(CAN) REJECTED TAKE-OFF AT APPROX. 50 KTS FOR ECAM WARNING: ENG-THRUST LOSS (AMBER) ABNORMAL WING A. ICE (AMBER)THRUST LEVERS, IDLE (BLUE) AIRCRAFT RETURNED TO GATE WHERE MAINTENANCE FOLLOWED TROUBLE SHOOTING TASK 71-00-00-810-934, REPLACED THE ZONE CONTROLLSDR CA011018006O-Ring · fretted(CAN) A/C EXPERIENCED LOSS OF YELLOW HYDRAULIC SYS, ECAM WARNING - HYD RSVR LO/HYD SYS LO PR, APPROX 1(ONE) HR INTO FLT. FLT CREW SECURED SYS AS PER THE AFM&DIVERTED FLT TO MAN. UPON ARRIVAL IN MAN, MAINT FOUND FLUID DRIPPING FROM NR 2 ENGINE THRUST REVERSDR CA010726026Probe · blocked(CAN) A/C ARRIVED WITH CAPTS. AIRSPEED READING INCORRECTLY. MTCE SWAPPED ADIRU #1 INTO #3 POSITION TO DEFER WITH LEAST AMOUNT OF IMPACT. A/C DEPARTED AND REJECTED T/O. ADM WAS OBTAINED FROM AIR CANADA AND INSTALLED IN A/C SSV. AVIONICS WAS CALLED IN TO C/O PITSDR CA991116012Blade · cracked(CAN) DURING ROUTINE INSPECTION OF RAM AIR TURBINE, SCRATCH FOUND ON BLADE ROOT. FURTHER INVESTIGATION REVEALED A CRACK. THE SUBMITTER INDICATED THAT THERE IS NO SPECIFIC INSPECTION TASK CALLING UP THE INSPECTION OF THE RAM BLADES.SDR CA991103045O-Ring · cracked(CAN) THRUST REVERSER HYDRAULIC FILTER ASSY O-RING WAS FOUND CUT AND EXTRUDED.SDR CA990907059Ecam · false signal(CAN) ECAM MESSAGE ON TAKEOFF INDICATED LOSS OF THRUST AND ENGINE ANTI-ICE FAULT WITH NO APPARENT FAULT. AIRBUS OIT 999.0106/96/SB AND TFU 73.25.000016.SDR CA990728081Blocker Door · detached(CAN) DURING DAILY INSPECTION, NR 2 ENGINE BLOCKER DOOR WAS FOUND TO BE HANGING DOWN IN THE FAN BYPASS DUCT. INVESTIGATION REVEALED A STRUCTURAL FAILURE OF UNKNOWN ORIGIN. BLOCKER DOOR SENT TO MANUFACTURER FOR ANALYSIS.SDR CA981019010Valve · failed(CAN) THE AIRCRAFT WAS ON A TRANSIT STOP AND THE ENGINES WERE SERVICED WITH OIL. ON CLIMB OUT, THE NR 2 ENGINE OIL PRESSURE INDICATION FLUCTUATED AND THEN WENT TO AMBER XX INDICATION, INDICATING LOSS OF DATA. THE OIL PRESSURE INDICATION RETURNED INTERMITTENTSDR 98ZZZX3615Blade · damagedUPON ATTAINING CRUISE ALTITUDE FL 290, ENGINE STALLED AND FIRE WARNING ACTIVATED. DISASSEMBLY INSPECTION REVEALED TWELVE 2ND STAGE TURBINE BLADES BROKEN AT PLATFORM AND AN ADDITIONAL 10 BLADES BROKEN APPROXIMATELY ONE INCH ABOVE PLATFORM. HPT MODULE 851 HOUR
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