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 WRLA20091101285Angle · crackedCRACK - ANGLE, C/T WING TO BODY FAIRING SUPPORT STRUCTURE STA Y=1361, RT FUSELAGE L=1". REPLACED WITH NEW ANGLE IAW MD-11 SRM 51-33-01 AND SRM 51-35-01 REV 41. COND CHECK NORMAL AND JOB COMPLETED.SDR WRLA20091101286Support Bracket · crackedCRACK - THE SUPPORT BRACKET OF FUEL PIPE AT Y=1441, L32L, LEFT UPPER FUSELAGE, CRACKED ABOUT .25 INCH. FABRICATED NEW PART IAW EGAT EI W2009P53B-1353 REV 00. INSTALLED NEW PART IAW MD11 SRM 51-33-01 REV 41.SDR WRLA20091101289Intercostal · crackedCRACK - INTERCOSTAL 2 AIR CONDITION DOOR L=5", QTY = 1 AREA. REPLACED WITH NEW INTERCOSTAL ON 2 AIR CONDITION DOOR IAW MD11 SRM 51-35-01 REV 41.SDR WRLA20091101290Intercostal · crackedCRACK - INTERCOSTAL 3 AIR CONDITION DOOR L=0.5" QTY =1 AREA. REPLACED INTERCOSTAL IAW MD11 SRM 51-35-01 REV 41.SDR WRLA20091101291Seat Track · crackedCRACK - SEAT TRACK STA 755 X=47.5 M/D CARGO FLOOR. REPAIRED THE SEAT TRACK IAW MD11 SRM 53-00-52 REV 41. APPLY PROTECTION COATING IAW MD11 SRM 51-21-01 REV 41.SDR WRLA20091101293Retainer · crackedCRACK - RETAINER STA 1521 LBL 11 PRESSURE BULKHEAD CENTER CARGO COMPARTMENT DIMENSION: 1 INCH. REPLACED WITH NEW RETAINER IAW MD11 SRM 53-00-01 REV 41.SDR WRLA20091101294Retainer · crackedCRACK - RETAINER STA 1521 LBL 49 PRESSURE BULKHEAD OF CENTER CARGO COMPARTMENT QTY =1EA. REPLACED WITH NEW RETAINER IAW EGAT EI W2009P53B-1374 REV 00.SDR WRLA20091101296Bracket · crackedCRACK - BRACKET OF TAIL CONE WORK PLATFORM LIGHT BOTH OF AFT FUSELAGE BULKHEAD ABOUT 1 INCH QTY = 2EA. REPLACED NEW BRACKET IAW MD11 SRM 51-35-01 REV 41.SDR WRLA20091101297Skin · deformedDEFORMED - EDGE OF SKIN FWD LOWER CORNER OF CENTER CARGO DOOR. MEASURE DEFORMED AREA DIMENSION (LXWXD = 1.5"X1.5"X0.03") AND NDT CHECK NORMAL AND IAW MD11 SRM 53-00-01 REV 41 WITHIN LIMITATION.SDR WRLA20091101299Intercostal · crackedCRACK - INTERCOSTAL, STA Y=6-50, L-42R, FWD CARGO COMPARTMENT L=0.1 INCH. REPAIRED INTERCOSTAL CRACK AREA IAW MD11 SRM 53-00-00 FIG 204 REV 41.SDR WRLA20091101300Fitting · crackedCRACK- ONE CLIP CRACKED ABOUT .5 INCH, Y=1401, L31L, LEFT UPPER FUSELAGE TO WING FAIRING SUPPORT QTY =1. REPLACED WITH NEW CLIP IAW MD11 SRM 51-35-01 FIG 2 AND SRM 51-33-01 FIG 2 REV 41.SDR WRLA20091101301Fitting · crackedCRACK - ONE CLIP CRACKED ABOUT 1 INCH Y=1341, L31L, LEFT UPPER FUSELAGE TO WING FAIRING SUPPORT QTY=1. FABRICATED PART IAW EGAT EI W2009P53B-1375 REV 00. INSTALLED WITH NEW PARTS IAW MD11 SRM 51-33-01.SDR WRLA20091101287Fitting · crackedCRACK - FITTING RT WING LOWER WINGLET STRUCTURE, DIMENSION =2.6 INCH QTY 1 EA. IAW AMM 57-31-00-000-801 REV 65 REMOVED THE RT LOWER WINGLET. REFERENCE THE EI W2009A57B-1483 REV 01 TO REPAIR THE WINGLET. IAW AMM 57-31--00-400-801 REV 65 INSTALL THE RT WING LSDR WRLA20091027324Fitting · corrodedFOUND RT WING OUTBOARD FLAP INBOARD INTERNAL SUPPORTING FITTING MOUNT HOLE CORROSION TOTAL 8 EA. REPAIRED THE 8 HOLES CORROSION AREA IAW DRAWING SR11570051 SHEET 1 AND REF JOB CARD ATTACHING SHEET 087988.070667. COND CHECK SATISFY AND JOB COMPLETED.SDR WRLA20091024265Doubler · crackedCRACK - FIXED PANEL STRINGER DOUBLER AT XORS 446, RT WING L/E, L=1". REPLACED STRINGER DOUBLER IAW MD11 SRM 51-33-01 REV 41.SDR WRLA20091023256Skin Panel · corrodedCORROSION WAS FOUND ON FIXED L/E OF LT WING NEAR PNL 518CB. PERFORM EI W2009A57B-1425 REV 00 REPAIR CORROSION ON LT WING FIXED LEADING EDGE SKIN PANEL AT XOS 464.00. COND CHECK NORMAL AND JOB COMPLETED.SDR WRLA20091023257Bushing · wornFOUND LT WING OUTBOARD FLAP INBOARD FWD HINGE ACTUATOR CONNECTION BUSHING WORN. REMOVED RT OUTBOARD FLAP OUTBOARD AFT HINGE IAW AMM 20-50-02-900-801 REV 65. REPAIRED OUTBOARD FLAP OUTBOARD AFT HINGE REF EGAT NRC U01038 JOB CARD ATTACHING SHEET 074960 & 07496SDR WRLA20091023258Bushing · wornFOUND LT WING OUTBOARD FLAP INBOARD AFT HINGE LWR BUSHING WORN. REMOVED LT OUTBOARD FLAP INBOARD AFT HINGE IAW AMM 20-50-02-900-801 REV 65. REPAIRED LT OUTBOARD FLAP OUTBOARD AFT HINGE REF EGAT NRC U01042 JOB CARD ATTACHING SHEET 074962 & 070606. INSTALLED SDR WRLA20091023259Bearing · damagedFOUND RT WING OUTBOARD FLAP OUTBOARD FWD HINGE LWR BEARING DAMAGE AND THE HOLE CORROSION AND ACTUATOR CONNECTION BUSHING. REMOVED RT OUTBOARD FLAP OUTBOARD FWD HINGE IAW AMM 57-01-000-801 REV 65. REPAIRED OUTBOARD FLAP OUTBOARD FWD HINGE REF EGAT NRC U01038 SDR WRLA20091023260Bushing · wornFOUND RT WING OUTBOARD FLAP INBOARD AFT HINGE UPPER AND LWR BUSHING WORN (2 POINT). REMOVED RT OUTBOARD FLAP INBOARD AFT HINGE IAW AMM 20-50-02-900-801 REV 65. REPAIRED RT OUTBOARD FLAP INBOARD AFT HINGE REF EGAT NRC U01041 JOB CARD ATTACHING SHEET 074961 & SDR WRLA20091023261AFitting · crackedCRACK - FITTING NLG TRUNNION FITTING, LT SIDE STA Y= 595 L= 2. IAW AMM 32-21-01-000-801 REV 65 RMV NOSE LANDING GEAR. REPAIRED CRACK AREA IAW MD11 SRM 53-10-14 REV 41 FIG 202 REPAIR 2. RE-INSTALLED NOSE LANDING GEAR ASSY REF EGAT NRC U05011.SDR WRLA20091023261Bushing · wornFND LT WING OUTBD FLAP INBD FWD HINGE ACTUATOR CONNECTION BUSHING WORN. CORRECTIVE ACTION: 1. REMOVED L/H OUTBD FLAP FWD HINGE IAW AMM 57-53-01-000-801 REV. 65. 2. REPAIRED OUTBD FLAP OUBD FWD HINGE REF EGAT NRC U01038 JOB CARD ATTACHING SHEET NR 07497907060SDR WRLA20091023262Bushing · wornFOUND LT WING OUTBOARD FLAP INBOARD FWD HINGE ACTUATOR CONNECTION BUSHING WORN. REMOVED LT OUTBOARD FLAP FWD HINGE IAW AMM 57-53-01-000-801 REV 65. REPAIRED OUTBOARD FLAP OUTBOARD FWD HINGE REF EGAT NRC U01038 JOB CARD ATTACHING SHEET 074979070604. INSTALLESDR WRLA20091023263Bushing · wornFOUND LT WING OUTBOARD FLAP OUTBOARD AFT HINGE LWR BUSHING WORN. REMOVED LT OUTBOARD FLAP OUTBOARD AFT HINGE IAW AMM 20-50-02-900-801 REV 65. REPAIRED LT OUTBOARD FLAP OUTBOARD AFT HINGE REF EGAT NRC U01042 JOB CARD ATTACHING SHEET 074963 & 070602. INSTALLESDR WRLA20091023264Door · crackedCRACK - DOOR MAIN LANDING GEAR FLIPPER DOOR RT FWD EDGE L= I" QTY=1. REPAIRED MAIN LANDING GEAR FLIPPER DOOR RT CRACK IAW MD11 SRM 58-82-01 REV 41.SDR WRLA20091003251Support Fitting · crackedDURING 2C CHECK FOUND CRACK ON CABIN FLOOR FRAME SUPPORT CLIP AT STA Y=1119, X=-65. FABRICATE PART IAW EI W2009P53B-1110 REV 00. REPLACE GUSSET PER MD-11 61-35-02 REV 41.SDR WRLA20090926210Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 1880, X=-27.50. REPAIR THE SEAT TRACK PER MD-11 SRM 53-00-52 REV 41, APPLY PROTECTION COATING PER MD-11 SRM 51-21-01 REV 41.SDR WRLA20090926212Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D CABIN SEAT TRACK, STA 1881 Y=-8.50. REPAIR THE SEAT TRACK PER MD-11 SRM 53-00-52 REV 41. APPLY PROTECTION COATING PER MD-11 SRM 51-21-01 REV 41.SDR WRLA20090926213Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 1878, X=27.50. REPAIR THE SEAT TRACK PER MD-11 SRM 53-00-52 REV 41. APPLY PROTECTION COATING PER MD-11 SRM 51-21-01 REV 41.SDR WRLA20090926215Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 1881, X=-47.50. REPAIR THE SEAT TRACK PER MD-11 SRM 53-00-52 REV 41. APPLY PROTECTION COATING PER MD-11 SRM 51-21-01 REV 41.SDR WRLA20090926228Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION M/D CABIN SEAT TRACK, STA1875 Y=8.5. REPAIR THE SEAT TRACK PER MD-11 SRM 53-00-52 REV 41. APPLY PROTECTION COATING PER MD-11 SRM 51-21-01 REV 41.SDR WRLA20090926209Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 453-455, X=-27.5. CLEAN-UP CORROSION AREA MEASURE THE TRACK AREA THICKNESS: 0.100" (REF JOB CARD ATTACHING SHEET 074290) WITHIN LIMITS PER SRM 53-00-52 REV 41. APPLY PROTECTION COATING PSDR WRLA20090926219Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 457, X=-33.5. CLEAN-UP CORROSION AREA MEASURE THE ORIGINAL AND REWORK THICKNESS RESULT: 0.090-0.082" (REF JOB CARD ATTACHING SHEET 074291) WITHIN LIMITS PER MD-11 SRM 53-00-00 PAGE 206 RESDR WRLA20090926254Longeron Splice · crackedDURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON LONGERON SPLICE FITTING, CENTER CARGO, STA 5-123, L4R. PART REPLACED PER WOA EI W2009P53B-1134 REV 00.SDR WRLA20090926211Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D CABIN FLOOR SUPPORT, STA 1878 X=-36. REPLACEMENT FLOOR SUPPORT IAW MD-11 SRM 51-31-01 REV 41. APPLY PROTECTION COATING IAW MD-11 SRM 51-21-01 REV 41.SDR WRLA20090926214Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D FLOOR SUPPORT AT STA 1880, X=36. REPLACEMENT FLOOR SUPPORT IAW MD-11 SRM 51-31-01 REV41. APPLY PROTECTION COATING IAW MD-11 SRM 51-21-01 REV 41.SDR WRLA20090926217Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 820-864, X=-8.50. REPAIR THE SEAT TRACK IAW MD-11 SRM 53-00-52 REPAIR 1 REV 41. APPLY PROTECTION COATING IAW MD-11 SRM 51-21-01 REV 41.SDR WRLA20090926220Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 840-870, X=-27.5. REPAIRED THE SEAT TRACK IAW MD-11 SRM 53-00-52 REPAIR 1 REV 41. APPLY PROTECTION COATING IAW MD-11 SRM 51-21-01 REV 41.SDR WRLA20090926221Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 925-968, X=-75.25. REPAIRED THE SEAT TRACK IAW MD-11 SRM 53-00-52 REPAIR 1 REV 41. APPLY PROTECTION COATING IAW MD-11 SRM 51-21-01 REV 41.SDR WRLA20090926225Beam · crackedDURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON THE LEFT MAIN LANDING GEAR TRUCK BEAM PIVOT PIN. REMOVED THE LEFT MAIN LANDING GEAR TRUCK BEAM PIVOT PIN IAW AMM 32-12-20-000-908 REV 65. INSTALLED THE LEFT MAIN LANDING GEAR TRUCK BEAM PIVOT PIN IAW AMM 32-12-20SDR WRLA20090926231Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 830-882, X=8.5. REPAIRED THE SEAT TRACK IAW MD-11 SRM 53-00-52 REPAIR 1 REV 41. APPLY PROTECTION COATING IAW MD-11 SRM 51-21-01 REV 41.SDR WRLA20090926232Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 1240-1247, 5142 X=107.25. REPAIRED THE SEAT TRACK IAW MD-11 SRM 53-00-52 REPAIR 1 REV 41. APPLY PROTECTION COATING IAW MD-11 SRM 51.21.01 REV 41.SDR WRLA20090926233Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 1398, X=107.25. REPAIRED THE SEAT TRACK IAW MD-11 SRM 53-00-52 RPR 1 REV41. APPLY PROTECTION COATING IAW MD-11 SRM 51-21-01 REV41.SDR WRLA20090926235Longeron Splice · crackedDURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON THE LONGERON SPLICE FTG , CTR CGO , L=1 , STA 5-123 , L45L. REMOVED DAMAGE LONGERON SPLICE IAW MD-11 SRM 51-33-01 REV 41. FABRICATE NEW LONGERON SPLICE IAW EI NO W2009P53B-1123 REV 00. INSTALL NEW LONGERON SPLICSDR WRLA20090926236Longeron Splice · crackedDURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON THE LONGERON SPLICE FTG , CTR CARGO , L=4 , STA 123, L49L. REMOVED DAMAGE LONGERON SPLICE IAW MD-11 SRM 51-33-01 REV 41. FABRICATE NEW LONGERON SPLICE IAW EI NO W2009P53B-1124 REV 00. INSTALL NEW LONGERON SPLICESDR WRLA20090926237Longeron Splice · crackedDURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON THE LONGERON SPLICE FTG , CTR CARGO , L=1 , STA 5-123 , L44L. REMOVED DAMAGE LONGERON SPLICE IAW MD-11 SRM 51-33-01 REV 41. FABRICATE NEW LONGERON SPLICE IAW EI NR W2009P53B-1125 REV 00. INSTALL NEW LONGERON SPLSDR WRLA20090926238Longeron Splice · crackedDURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON THE LONGERON SPLICE FTG , CENTER CARGO , L=5, STA 123 , L49R. REMOVED DAMAGE LONGERON SPLICE IAW MD-11 SRM 51-33-01 REV 41. FABRICATE NEW LONGERON SPLICE IAW EI NR W2009P53B-1126 REV 00. INSTALL NEW LONGERON SPLSDR WRLA20090926239Longeron Splice · crackedDURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON THE LONGERON SPLICE FTG , CENTER CARGO , L=4, STA 123 , L37L. REMOVED DAMAGE LONGERON SPLICE IAW SRM 51-33-01 REV 41. ABRICATE NEW LONGERON SPLICE IAW EI NO W2009P53B-1127 REV00. INSTALL NEW LONGERON SPLICE IAW SDR WRLA20090926240Longeron Splice · crackedDURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON THE LONGERON SPLICE FTG , CENTER CARGO , L=1, STA 123 , L35R. REMOVED DAMAGE LONGERON SPLICE IAW MD-11 SRM 51-33-01 REV 41. FABRICATE NEW LONGERON SPLICE IAW EI NR W2009P53B-1128 REV 00. INSTALL NEW LONGERON SPLSDR WRLA20090926241Longeron Splice · crackedDURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON THE LONGERON SPLICE FTG , CENTER CARGO , L=1, STA 5-126 , L38R. REMOVED DAMAGE LONGERON SPLICE IAW MD-11 SRM 51-33-01 REV 41. FABRICATE NEW LONGERON SPLICE IAW EI NR W2009P53B-1129 REV00. INSTALL NEW LONGERON SP
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