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 WRLA20100204337Fitting · crackedDURING PERFORM TASK CARD WA3007, FOUND RT WING TIP FITTING ARB7602-R CRACKED. PER AMM 20-50-02-900-801 REV 66 REPLACED THE FITTING, CONDITION SATISFACTORY.SDR IPXA10M58545Skin · crackedINSP TYPE:1C LT WING TELESCOPIC DUCT SPRING DOOR CUT-OUT CRACKED AT BOTH UPPER CORNERS. GAINED ACCESS TO AREA, CUT-OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER AND FILLERS REF SRM 57-40-01, REPAIR 10, FIG 201, RESTORED AREA.SDR WRLA20100120332Slide · damagedR4 EVAC SLIDE FELL FROM CONTAINER AND IS DAMAGED. REMOVED AND REPLACED R4 SLIDE.SDR WRLA20100120333Stringer · crackedCRACK - STRAP XORS 987.2 & XOS 993.3 LT WING FIXED L/E. REPAIRED CRACK IAW EI W201057B-143 REV 00 2. COND CHECK NORMAL AND JOB COMPLETED.SDR WRLA20100105329Membrane · crackedDURING 01C CHECK FOUND Y=360 X=-2 Z=-10 MEMBRANE ABA 7202-117 DEFORM AND 2EA CRACK, L=0.9" AND L=1.2" ON LIGHTENING HOLE. NRCU05014 ISSUED. ACCOMPLISHED THE REPAIR PER EI: W2010A53B-050 REV 00, 01,02: CUT THE DAMAGED AREA AS SHOWN IN W2010A53B-050 FIG 1, FASDR WRLA20100105331Fitting · crackedDURING 01C CHECK FOUND NOSE GEAR TRUNNION LT FITTING P/N ACA7017-502 CRACKED.SDR WRLA20100105330Stop Fitting · crackedDURING 01C CHECK FOUND RIGHT WING OUTBOARD FLAP STOP RIB (P/N:ARC4125-502) CRACKED AT XOF 563.244. NRC U05078 ISSUED. PER EI:W2010A57B-072 REV00 AND AMM REV66, RMV THE FLAP, RPL THE LEADING EDGE RIB, RE-INST THE FLAP. PFM AMM SUBTASK 27-50-30-830-003 TO ADJSDR WRLA20091119326Fitting · corrodedFOUND LT WING OUTBOARD FLAP INBOARD INTERNAL SUPPORT FITTING MOUNT HOLE CORROSION TOTAL 5 EA. REPAIRED THE 5EA HOLES CORROSION AREA IAW DRAWING SR11570051 SHEET 1 AND REF JOB CARD ATTACHING SHEET 087985, 070668.SDR WRLA20091116309Seat Track · wornWORN - SEAT TRACK CROWN BETWEEN STA 630 AND 635 X= 8.5 INCHES IN MID 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 WRLA20091116311Seat Track · wornWORN - SEAT TRACK CROWN, STA 1163, X=-8.5, IN 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 WRLA20091116312Seat Track · wornWORN - SEAT TRACK CROWN, STA 645 X=24, IN 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 WRLA20091116313Seat Track · wornWORN - SEAT TRACK CROWN, STA 638 TO STA 650, X=42, IN 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 WRLA20091116314Seat Track · wornWORN - SEAT TRACK CROWN, STA 1887 X=27.5, IN 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 WRLA20091116315Skin · corrodedCORROSION - SKIN Y=1226~1228 X=57~61 EXFOLIATION AROUND FASTENERS HEAD CTR WING TANK UPPER SURFACE TOTAL: 3 AREAS. REPAIRED THE CORROSION AREA IAW EGAT EI W2009A57B-1378 REV 00.SDR WRLA20091116316Mount · corrodedFOUND RT WING OUTBOARD FLAP INBOARD AFT HINGE MOUNT HOLE CORROSION TOTAL 7 EA. IAW AMM 20-50-02-900-801 REV 65 REMOVED THE RT WING OUTBOARD FLAP INBOARD AFT HINGE. SEND TO SHOP FOR REPAIR REF J/C ATTACHING SHEET 070608. IAW AMM 20-20-01-400-801 REV 65 RE-INSDR WRLA20091116317Support Fitting · corrodedFOUND RT WING OUTBOARD FLAP OUTBOARD INTERNAL SUPPORT FITTING MOUNT HOLE CORROSION TOTAL 3 EA. REPAIRED THE 3EA HOLES CORROSION AREA IAW DRAWING SR11570051 SHEET 1 AND REF JOB CARD ATTACHING SHEET 087986. COND CHECK SATISFACTORY AND JOB COMPLETED.SDR WRLA20091116318Hinge Fitting · corrodedFOUND RT WING OUTBOARD FLAP OUTBOARD FWD HINGE LWR MOUNT FITTING AND SIDE BOLT FITTING SURFACE HAS CORROSION. IAW AMM 57-53-01-000-801 REV 65 RMV THE RT WING OUTBOARD FLAP OUTBOARD FWD HINGE. SEND TO SHOP FOR RPR REF J/C ATTACHING SHEET 070610, 070611. IAW SDR WRLA20091116319Seat Track · wornWORN - SEAT TRACK CROWN, STA 716 X=-46, IN 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 WRLA20091116320Seat Track · wornWORN - SEAT TRACK CROWN, STA 735 X=107.5, IN 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 WRLA20091116321Seat Track · wornWORN - SEAT TRACK CROWN, STA 1887 X=47.5, IN 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 WRLA20091116322Skin · corrodedEXFOLIATION CORROSION - SKIN CTR WING Y=1226~1239 X=-42~-97 WING TANK UPPER SURFACE TOTAL:39 AREA. REPAIRED THE CORROSION AREA IAW EGAT EI W2009A57B-1378 REV 00.SDR WRLA20091116323Doubler · brokenBROKEN - LWR DOUBLER OF LT WING FIXED L/E NOSE SECTION XOS 487. FABRICATED PART IAW EGAT EI W2009P57B-1344 REV 00. INSTALLED PART IAW MD11 SRM 51-33-01 REV 41.SDR WRLA20091114307Mount Fitting · corrodedFOUND LT WING OUTBOARD FLAP INBOARD FWD HINGE LWR MOUNT FITTING AND SIDE BOLT FITTING SURFACE HAS CORROSION. IAW AMM 57-53-04-000-801 REV 65, REMOVED THE LT WING OUTBOARD FLAP INBOARD FWD HINGE. SEND TO SHOP FOR REPAIR REF EGAT NRC U05183 J/C ATTACHING SHEETSDR WRLA20091114308Mount · corrodedFOUND LT WING OUTBOARD FLAP INBOARD AFT HINGE MOUNT HOLE CORROSION TOTAL: 3 EA. IAW AMM 20-50-02-900-801 REV 65 REMOVED THE LT WING OUTBOARD FLAP INBOARD AFT HINGE. SEND TO SHOP FOR REPAIR REF EGAT NRC U05182 J/C ATTACHING SHEET 070607. IAW AMM 20-50-02-90SDR IPXA99M57904Wire Harness · damagedINSPECTION TYPE:N/A ATB - NR 2 ENGINE HIGH VIBRATION DURING CLIMB. RETURNED TO ANC. LANDED SAFELY. REMOVED AND REPLACED NR 2 ENG VIBRATION HARNESS IAW MM 71-50-01-4/2 AND REMOVED AND REPLACED NR 2 ENG FAN CASE ACCELEROMETER PER MM 77-32-03-4/2. HIGH POWER SDR WRLA20091105327Seat Track · wornWORN - SEAT TRACK CROWN, BETWEEN STA 1661. REPAIR THE SEAT TRACK IAW MD-11 SRM 53-00-52 REV 41. APPLY PROTECTION COATING IAW MD-11 SRM 51-21-01 REV 41. JOB COMPLETED AND COND CHECK NORMAL.SDR WRLA20091105302Doubler · crackedCRACK - BEADED DOUBLER FINED L/E UPPER STRUCTURE RIGHT WING STA XORS 540 LENGTH THE FRONT SPAR 11 INCH. REPAIR BEADED DOUBLER IAW MD-11 SRM 57-40-02 REV 41. COND CHECK NORMAL AND JOB COMPLETED.SDR WRLA20091105303Doubler · crackedCRACK - BEADED DOUBLER FIXED L/E UPPER STRUCTURE RIGHT WING STA XORS 540 LENGTH THE FRONT SPAR 9 INCHES. REPAIR BEADED DOUBLE IAW MD-11 SRM 57-40-02 REV 41. COND CHECK NORMAL AND JOB COMPLETED.SDR WRLA20091105304Doubler · crackedCRACK - BEADED DOUBLER FIXED L/E UPPER STRUCTURE RIGHT WING STA XORS 560 LENGTH THE FRONT SPAR 9 INCHES. REPAIR BEADED DOUBLER IAW MD-11 SRM 57-40-02 REV 41. COND CHECK NORMAL AND JOB COMPLETED.SDR WRLA20091105305Doubler · crackedCRACK - BEADED DOUBLER FIXED L/E UPPER STRUCTURE RIGHT WING STA XORS 546. REPAIR BEADED DOUBLER IAW MD-11 SRM 57-40-02 REV 41. COND CHECK NORMAL AND JOB COMPLETED.SDR WRLA20091101288Intercostal · crackedCRACK - INTERCOSTAL, CAC COMPARTMENT FLOOR SUPPORT BEAM STA 6-90 RBL=-65 L=.5. CLEANED AND INSPECTED CRACK AREA, FOUND ONLY PAINT CRACK AND NDI INSPECTED, ALSO NO CRACK WAS FOUND DETAIL DATA REFER TO JOB CARD ATTACHING SHEET NO. 070649 2. RE-APPLY PAINT AND SDR WRLA20091101266Doubler · crackedCRACK - BEADED DOUBLER-FIXED L/E UPPER STRUCTURE RIGHT WING STA X0RS 560 LENGTH THE FRONT SPAR 11 INCHES. REPAIR BEADED DOUBLER IAW MD11 SRM 57-40-02 REV 41.SDR WRLA20091101267Doubler · crackedCRACK - BEADED DOUBLER - FIXED L/E UPPER STRUCTURE RIGHT WING STA XORS 560 LENGTH THE FRONT SPAR 13 INCHES. REPAIR BEADED DOUBLER PER MD11 SRM 57-40-02 REV 41.SDR WRLA20091101268Doubler · crackedCRACK - DOUBLER FIXED L/E UPPER STRUCTURE RIGHT WING STA XORS 562 L=3. REPLACE DOUBLER IAW MD11 SRM 51-33-01 REV 41.SDR WRLA20091101269Stiffener · crackedCRACK - STIFFENER OF PNL 616ET AT RT WING UPPER SURFACE 1 PLACE AT XW 327. REPAIRED CRACK AREA IAW MD11 SRM 57-40-02 FIG 201 REV 41.SDR WRLA20091101270Stiffener · crackedCRACK - ZEE STIFFENER OF LT WING FIXED L/E UPPER PNL 516ET 1 EA AT XW 297. REPAIRED CRACK AREA IAW MD11 SRM 57-40-02 FIG 201 REV 41.SDR WRLA20091101271Stiffener · crackedCRACK - ZEE STIFFENER OF LT WING FIXED L/E UPPER PNL 516ET 1 EA AT XW291. REPAIRED CRACK AREA IAW MD11 SRM 57-40-02 FIG 201 REV 41.SDR WRLA20091101272Stiffener · crackedCRACK - STIFFENER OF PNL 616ET AT RT WING UPPER SURFACE 1 PLACE AT XW 291. REPAIRED CRACK AREA IAW MD11 SRM 57-40-02 FIG 201 REV 41.SDR WRLA20091101273Skin · crackedCRACK - SKIN STA 1250.750 AT CENTER FUSELAGE DOOR JAMB RT NR 3 MED, L=0.275 INCH. REPAIR CRACK AREA IAW MD11 SRM 53-40-15 REV 41.SDR WRLA20091101274Skin · crackedCRACK - SKIN STA 1250.750 AT CENTER FUSELAGE DOOR JAMB LT NR 3 MED L=0.265 INCH. REPAIRED CRACK AREA IAW MD11 SRM 53-40-15 REV 41.SDR WRLA20091101275Plate · crackedCRACK - PLATE CTR CARGO AWD DOOR JAMB STA 1671 L=2 QTY = 1EA. REPLACED PLATE IAW MD11 SRM 51-31-01 REV 41.SDR WRLA20091101276Stiffener · crackedCRACK - ZEE STIFFENER OF LEFT WING FIXED L/E UPPER PNL 516ET QTY = 1EA AT XW 303. REPAIRED CRACK AREA IAW MD11 SRM 57-40-02 REV 41.SDR WRLA20091101277Rib · crackedCRACK - RIB, STA XOS 1003 NR 16 SLAT TRACK IN LT WING FIXED L/E COMPARTMENT L=0.375 INCH, QTY=1EA. REPLACED THE RIB IAW MD11 SRM 51-33-01 REV 41.SDR WRLA20091101278Fairing · crackedCRACK - T CHORD, LOWER SIDE OF INBOARD FAIRING, LT WING OUTBOARD FLAP, L=2. REPLACED WITH NEW T CHORD 2 EA. IAW MD11 SRM 51-35-01 REV 41.SDR WRLA20091101279Skin · crackedCRACK - CLIP, AFT UPPER OF HORIZONTAL STAB COMPARTMENT UPPER SIDE, Y=2106. X=7 LENGTH =.25 INCH SINCE HI-LOK FROM LT OUTBOARD SIDE. REPAIRED AFT UPPER OF HORIZONTAL STAB COMPARTMENT UPPER SIDE AREA IAW MD11 SRM 53-70-07 REV 41.SDR WRLA20091101280Former · crackedCRACK - FORMER (P/N:ARB1164-5) CRACKED ABOUT .75 INCH LEFT WING FRONT SPAR LWR CHORD XOS 993 QTY = 1. REPAIRED THE CRACK FORMER IAW MD11 SRM 57-00-00 REV 41.SDR WRLA20091101281Stiffener · crackedCRACK - STIFFENER, STA 1841, RBL 38 LWR SIDE WEB OF FLOORBEAM, AFT CARGO COMPARTMENT L=0.5 INCH. REPLACED WITH NEW STIFFENER IAW MD11 SRM 51-33-01 FIG 2 REV 41.SDR WRLA20091101282Stiffener · crackedCRACK - STIFFENER OF PANEL 616ET RT WING L/E UPPER SURFACE, 1 PLACE AT XW 297. REPAIRED CRACK AREA IAW MD11 SRM 57-40-02 FIG 201 REV 41.SDR WRLA20091101283Web · crackedCRACK - WEB, LT OF FWD UPPER HORIZONTAL STAB COMPARTMENT ACCESS CUTOUT Y = 2042,, X=14, LENGTH = .375 INCH. REPAIRED THE CRACK AREA IAW MD11 SRM 53-00-00 FIG 211 REV 41.SDR WRLA20091101284Web · crackedCRACK - WEB, LT WING TO BODY FAIRING SUPPORT STRUCTURE, L=1.5", Y=1341. REPAIRED WEB CRACK AREA IAW MD11 SRM 53-00-00 FIG 204 REV 41.
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