Pratt & Whitney PW4462
Service difficulty reports · 778
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 = 'PW4462' 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 = 'PW4462' 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 WRLA20090926245Longeron Splice · crackedDURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON THE LONGERON SPLICE FTG , CENTER CARGO , L=2, STA 5-123 , L50R. REMOVED DAMAGE LONGERON SPLICE IAW MD-11 SRM 51-33-01 REV 41. FABRICATE NEW LONGERON SPLICE IAW EI NR W2009P53B-1133 REV 00. INSTALLED NEW LONGERONSDR WRLA20090926248Longeron Splice · crackedDURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON THE LONGERON SPLICE FTG , CENTER CARGO , L=1, STA 5-123 , L34L. REMOVED DAMAGE LONGERON SPLICE IAW SRM 51-33-01 REV 41. FABRICATE NEW LONGERON SPLICE IAW EI NR W2009P53B-1130 REV 00. INSTALL NEW LONGERON SPLICE SDR WRLA20090926249Longeron Splice · crackedDURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON THE LONGERON SPLICE FTG , CENTER CARGO , L=2, STA 5-123 , L38L. REMOVED DAMAGE LONGERON SPLICE IAW MD-11 SRM 51-33-01 REV 41. FABRICATE NEW LONGERON SPLICE IAW EI NR W2009P53B-1131 REV 00. INSTALL NEW LONGERON SSDR WRLA20090926250Longeron Splice · crackedDURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON THE LONGERON SPLICE FTG , CENTER CARGO , L=3, STA 5-123 , L51L. REMOVED DAMAGE LONGERON SPLICE IAW MD-11 SRM 51-33-01 REV 41. FABRICATE NEW LONGERON SPLICE IAW EI NR W2009P53B-1132 REV00. INSTALL NEW LONGERON SPSDR WRLA20090926216Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 1870, X=-75.25. REPAIR THE SEAT TRACK IAW SRM 53-00-52 REPAIR REV 41. APPLY PROTECTION COATING IAW SRM 51-21-01 REV41.SDR WRLA20090926218Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 6-30, X=8.5. REPAIRED THE SEAT TRACK IAW MD-11 SRM 53-00-52 RPR REV41. APPLY PROTECTION COATING IAW MD-11 SRM 51-21-01 REV41.SDR WRLA20090926223Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 1239-1250, X=-107.25. REPAIRED THE SEAT TRACK IAW SRM 53-00-52 RPR 1 REV41. APPLY PROTECTION COATING IAW SRM 51-21-01 REV41.SDR WRLA20090926229Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 909-929, X=107.25. REPAIRED THE SEAT TRACK IAW MD-11 SRM 53-00-52 RPR REV41. APPLY PROTECTION COATING IAW MD-11 SRM 52-21-01 REV41.SDR WRLA20090926230Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 532-559, X=73. REPAIRED THE SEAT TRACK IAW MD-11 SRM 53-00-52 RPR1 REV41. APPLY PROTECTION COATING MD-11 SRM 51-21-01 REV41.SDR WRLA20090926234Beam · crackedDURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON THE LT WING FIXED INNER T/E LOWER BEAM, STA XW200,L=14 . JOB COMPLETED IAW EI NR W2009A57B-1122 REV00 AND REV01.SDR WRLA20090926222Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 1121-1127, X=-75.25. REPAIR THE SEAT TRACK IAW SRM 53-00-52 RPR REV 41. APPLY PROTECTION COATING IAW SRM 51-21-01 REV 41.SDR WRLA20090926224Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 1249, X=107.25. REPAIR THE SEAT TRACK IAW MD-11 SRM 53-00-52 RPR REV 41. APPLY PROTECTION COATING IAW MD-11 SRM 51-21-01 REV 41.SDR WRLA20090926246Skin · delaminatedDURING 2C CHECK, EGAT MECHANIC FOUND DISBOND ON THE RIGHT WING INBOARD FLAP VANE LOWER SKIN DISBOND 12 *19 AT XIFH210. REMOVED RIGHT WING INBOARD FLAP VANE (J/C ATTACHING SHEET NR 088958 ITEM 01). REPAIRED THE DISBOND DAMAGE AREA IAW EGAT EI NR W2009A57B-113SDR WRLA20090926247Skin · delaminatedDURING 2C CHECK, EGAT MECHANIC FOUND DISBOND ON THE LEFT WING INBOARD FLAP VANE LOWER SKIN DISBOND (7 *17 ) AT XIFH 192. CUT OUT DENT SKIN SANDED AROUND THE AREA AND CLEAN BONDED FIBERGLASS FABRIC USE WET LAY-UP AT 200 OF CURE FOR 220 MINS WITH VACUUM PRESSURSDR WRLA20090919208Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK BETWEEN STA 1351 AND STA 1361, X=107.25. REPAIR THE SEAT TRACK IAW SRM 53-00-52 RPR 1 REV 41. APPLY PROTECTION COATING IAW SRM 51-21-01 REV41.SDR WRLA20090918205Skin · crackedDURING 2C CHECK, EGAT MECHANIC FOUND CRACK WITH FASTENER HOLE WORN OUT ON INBD/OUTBD SKIN (P/N: AUB7562-5 AND AUB7652-6) OF NR 3 PYLON FWD FAIRING. PERFORM EI W2009A54B-1109, REV 00 TO REPAIR THE DAMAGED AREA.SDR FDEA200909173312Shear Tie · corrodedAFT CARGO COMPARTMENT - STA 1953 FROM LONGERON 50 LT TO LONGERON 49 RT FRAME SHEAR CLIP FOUND CORROSION. REPAIRED IAW SRM 51-31-01 REV 41.SDR WRLA20090917204Fitting · crackedDURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON NLG TRUNNION SUPPORT FITTING, Y=582, X=24. CRACK LENGTH MEASURED 1 INCH. REPAIR THE NLG TRUNNION SUPPORT FITTING IAW MD-11 SRM 53-10-14 FIGURE 202, REPAIR 2, REV 41.SDR WRLA20090917201Doubler · crackedCRACK - DURING 2C CHECK, EGAT MECHANIC FOUND THE STIFFENER DOUBLER AT THE CENTER GEAR W/W WEB Y:1382, X:+31.50 HAS CRACKED FROM THE FASTENER AREA (LEFT STIFFENER). ACCORDING TO EI W2009A53B-1114 REV 00 TO FABRICATE REPAIR PARTS. REINSTALL FASTENERS PER MD-11SDR WRLA20090917202Doubler · crackedCRACK - DURING 2C CHECK, EGAT MECHANIC FOUND THE STIFFENER DOUBLER AT THE CENTER GEAR W/W WEB Y:1381, X:-31.50 HAS CRACKED FROM THE FASTENER AREA (RIGHT STIFFENER). ACCORDING TO EI W2009A53B-1115 REV 00 TO FABRICATE REPAIR PARTS. RE-INSTALLED FASTENERS PER MSDR WRLA20090917203Skin Panel · crackedDURING 2C CHECK, EGAT MECHANIC FOUND SKIN BULGE ON RT NOSE FUSELAGE UPPER, STA 275, X=-10. INSTALLED SKIN REPAIR IAW EI W2009A53B-1120 REV 00.SDR WRLA20090916199Rib · crackedDURING 2C CHECK, EGAT MECHANIC FOUND THE STOP RIB AT THE L/E (XOVH 537) OF RIGHT OUTBOARD T/E FLAP CRACK. ACCOMPLISH E.I NO:W2009A57B-1092, REV 00 AND E.I NR :W2009A57B-1207 REV 00.SDR WRLA20090916200Rib · crackedDURING 2C CHECK, EGAT MECHANIC FOUND THE STOP RIB AT THE L/E (XOVH 537) OF LEFT OUTBOARD T/E FLAP CRACK. ACCOMPLISH EI NR:W2009A57B-1093, REV 00 AND EI NR:W2009A57B-1205.SDR FDEA200909063263Skin · corrodedLT WING UPPER SKIN AT STA, XORS 130 TO XORS 197 FOUND CORROSIONS. REPAIR IAW EA 1-5710-132213 TITLE: "WINGS-LT WING UPPER SKIN SURFACE CORROSION - REPAIR"SDR FDEA200909043258Skin · corrodedLEFT STA 1229 XCW= 97 TO XCW= 107 CTR WING UPPER PANEL FOUND CORROSION. REPAIRED IAW EA 1-5710-133850. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 107.SDR FDEA200908253085Hinge Bracket · corrodedRT WING - WING SIDE OTBD FLAP OTBD HINGE LWR MOUNT OTBD HOLE FOUND CORRODED. REPAIRED IAW EA 1-5750-132208 (MAJOR REPAIR).SDR FDEA200908243080Cargo Track · crackedCRACKED LOWER FLANGE OF FLOOR TRACK AT LT STA 755, X=27.5 IN MAIN DECK CARGO. REPAIRED AS PER SRM53-00-52 FIG201 REPAIR1 REV41 (MAJOR REPAIR).SDR FDEA200908233072Longeron Splice · crackedAFT CABIN RT SIDE AT APPROX STA 5-123, LONGERON 12 RT FOUND LONGERON SPLICE CRACKED. REMOVED AND REPLACED IAW SRM 51-31-01, REVISION 41. NEW LONGERON SPLICE MACHINE IAW DWG A5A7112, REVISION D. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 107.SDR WRLA20090819198Pump · leakingDURING CLIMBOUT, NR 3 ENGINE LT EDP INDICATED OVERTEMP. ONE HOUR AFTER DEPARTURE, NR 3 ENGINE RT EDP INDICATED OVERTEMP. ONE HOUR FIFTEEN MINUTES AFTER DEPARTURE NR 3 HYDRAULIC SYSTEM INDICATED 0 HYDRAULIC FLUID QUANTITY. DIVERTED TO LEJ (EDDP) FOR MAINTENASDR WRLA20090814255Skin · damagedTHE RT DETACHABLE ELEVATOR WAS DAMAGED DUE TO CONTACT WITH GROUND EQUIPMENT. THE UPPER AND LOWER SKINS WERE DAMAGED ON THE TRAILING EDGE. THE INBD CORNER WAS CRACKED AND WAS REMOVED THROUGH ALL PLIES. IN ADDITION, THE INNERMOST PLY OF THE OUTER SKIN IS DAMASDR WRLA20090810196Skin · damagedDAMAGE TO THE FUSELAGE SKIN AT THE FORWARD LOWER CORNER OF THE UPPER CARGO DOOR CUTOUT. REPAIRED IN ACCORDANCE WITH WOA ERA 09-53-103.SDR WRLA2009189Engine · vibrationNR 1 ENGINE HI VIBRATION/LOW RPM IN INITIAL CLIMB OUT. HIGH EGT 917C. DURING SHUTDOWN ENGINE FIRE AGENT DISCHARGED.SDR WRLA2009119Seat Track · corrodedDURING "C" CHECK INSPECTION FOUND MAIN DECK CARGO CABIN SEAT TRACK CORROSION AND WEAR ON STA 1847-1884 AND X=47.5. CUT OUT SEAT TRACK FROM Y= 1831 TO 1887 AT X= 47.5 AND REPAIRED SEAT TRACK IAW MD-11 SRM 53-70-00 VOL 1 REV 40 FIG 1. JOB COMPLETED AND CONDITISDR WRLA2009120Seat Track · corrodedDURING "C" CHECK INSPECTION IN TPE, FOUND CORROSION ON MAIN DECK SEAT TRACK FLOOR PANEL SUPPORT AREA AT STA 976 AND X=8.5. CUT OUT SEAT TRACK FROM Y= 919 TO 985 AT X= 8.5 AND REPAIRED SEAT TRACK IAW SRM 53-70-00 VOL 1 REV 40 FIG 1. JOB COMPLETED AND CONDITIOSDR WRLA2009121Seat Track · corrodedDURING "C" CHECK INSPECTION IN TPE FOUND MAIN DECK SEAT TRACK CRACK ON STA 1832 AND X=8.5. CUT OUT SEAT TRACK FROM Y= 1731 TO 1832 AT X= 8.5 AND REPAIRED SEAT TRACK IAW SRM 53-70-00 VOL 1 REV 40 FIG 1. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR WRLA2009122Seat Track · corrodedDURING "C" CHECK INSPECTION IN TPE, FOUND MAIN DECK CABIN SEAT TRACK CORROSION AND WEAR ON STA 1776-1811 AND X=-8.5. CUT OUT SEAT TRACK FROM Y= 1731 TO 1811 AT X= -8.5 AND REPAIRED SEAT TRACK IAW SRM 53-70-00 VOL 1 REV 40 FIG 1. JOB COMPLETED AND CONDITION SDR WRLA2009123Seat Track · corrodedDURING "C" CHECK INSPECTION FOUND MAIN DECK CABIN SEAT TRACK CORROSION AND WEAR ON STA 1787 - 1682 AND X=8.5. CUT OUT SEAT TRACK FROM Y= 1682 TO 1707 AT X= 8.5 AND REPAIRED SEAT TRACK IAW SRM 53-70-00 VOL 1 REV 40 FIG 1. JOB COMPLETED AND CONDITION CHECK NORSDR FDEA200903291096Engine · power lossENG NR 3 FLAMED OUT IN FLIGHT. FL 320. LOUD BANG & SHUDDER WITH HIGH EGT INDICATION. DUMPED 59K LBS OF FUEL. LOUD COMPRESSOR STALL SOUND AND LOOKS LIKE EGT WENT TO 680 DEG C. ENGINE APPEARED TO ROLL BACK. HE CONSIDERED A RESTART BUT HIGH EGT PROMPTED SHUTDOWSDR FDEA200903251036Pump · failedNR 3 ENG FLAME OUT DURING DESCENT, 280KTS/13000. PERFORMED LEVEL 3 ENG RPM LOW CHECKLIST, FOLLOWED BY ENG RESTART IN FLIGHT CHECKLIST, GOOD RESTART 10000/270 KTS. CKD ALL DEU AND FADEC NO FAULT SHOWN, INSP INLET & EXHUAST, CORE AREA NO DEFECT NOTED, R & R SDR WRLA2009011Rib · crackedDURING A04 CHK, LT WING INBOARD SLAT FILLET CHAFING AT WING FUSELAGE FAIRING. SLAT I/B RIB CRACKED & FAIRING RIB CRACKED. REMOVED AND REPLACED NR 1 SLAT.SDR FDEA200901150208Unknown · vibrationAFTER TAKEOFF PASSING 13000 FT IN CLIMB PWR NR 1 ENG STARTED VIBRATING. AT LEVEL OFF PULLED NR 1 THROTTLE TO IDLE AND WHEN PASSING BELOW 80 PERCENT N1 VIBRATION WENT DOWN SIGNIFICANTLY AND AT IDLE NO VIBRATION NOTED. KEPT THROTTLE BELOW 80 PERCENT TO REMAINDSDR WRLA2009007Mount · corrodedNR 3 ENG MOUNT ISOLATOR, INSIDE FAN CASE, HAS RED POWDERY SUBSTANCE DRIPPING OUT ONTO COMPRESSOR, A-07 CHECK. REMOVED NR 3 ENG FWD MOUNT ISOLATOR IAW MM 71-00-39 PW ENG MANUAL. INSP, OK TO INSTALL. 01-09-09 REPLACED MOUNT WITH SERVICEABLE MOUNT IAW ENG MANUASDR WRLA2009001Engine · defectiveIN CRUISE RECEIVED A LVL 2 ENG 2 OIL FILTER ALERT. NOTICED INCREASING EVM COMP INDICATION AND RECIEVED A LVL 1 ENG 2 VIB HI ALERT. LATER MODERATE A/C VIB NOTICED, EVM COMP OF 5.0, A LVL 2 SEL FADEC ALT ALERT AND A DROP IN N1 OF NR 2 ENG COMPLETED IFSD PROCEDURSDR WRLA2008073Skin · corrodedDURING INSPECTION FOUND FUSELAGE SKIN AND REINFORCING DOUBLER CORRODED AT AFT LAV EXHAUST PORT STA 1959 BETWEEN LONGERONS LS9R AND L40R. CORRECTIVE ACTION: REF. DELTA ERA 47026114 REMOVED DAMAGED AREA, PERFORMED HF EDDY CURRENT INSPECTION AS REQUIRED, FABRICASDR WRLA2008071Doubler · crackedCENTER MLG WW RT BULKHEAD CUTOUT DOUBLER CRACKED AT RT FWD CORNER.SDR WRLA2008070Doubler · crackedDURING INSPECTION FOUND CRACK ON CENTER LANDING GEAR WHEEL WELL FORWARD BULKHEAD LT & RT AROUND LATERAL CONTROL MIXER. CORRECTIVE ACTION: INSTALLED ANGLE REF ROD SKETCH 91-09-09-002.SDR WRLA2008068ADoubler · crackedDURING A CHECK INSPECTION SR TECHNICS, CRACKS FOUND ON CENTER LANDING GEAR WHEEL WELL FORWARD BULKHEAD LT SIDE AROUND LATERAL CONTROL MIXER DOUBLERS. REPAIRED PER WORLD AIRWAYS ENGINEERING REPAIR AUTHORIZTION DOCUMENT 08-53-73. (S)SDR WRLA2008069ADoubler · crackedDURING INSPECTION FOUND CRACK ON CLG WHEEL WELL LT AND RT DOUBLER AT Y=1381, X=31.5 AND -31.5. REPAIRED CRACK AREA IAW EI W2008A53B-761 REV.00. JOB COMPLETED AND CONDITION CHECK NORMAL. (S)SDR WRLA2008066Seat Track · crackedDURING "C" CHECK INSPECTION IN TPE FOUND CRACK IN THE MAIN DECK SEAT TRACK AT Y=760, X=47.5. (S)SDR WRLA2008067Seat Track · crackedDURING INSPECTION FOUND MAIN DECK CARGO SEAT TRACK CRACK AT Y=760, X=47.6. REPAIRED CRACK SET TRACK IAW MD-11SRM VOL 1 53-70-00 REV 40. JOB COMPLETED AND CONDITION CHECK NORMAL. (S)
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