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 WRLA2007107Seat Track · corrodedDURING 4C+12A CHECK, SEAT TRACK CORROSION FOUND AT STA X=-67 Y=517. 10-25-07 REPLACED DAMAGED SEAT TRACK PER MD-11 SRM VOL.I 53-70-00 FIG.8 REV.40.SDR WRLA2007108Longeron · corrodedDURING 4C+12A CHECK, LONGERON CORROSION FOUND AT STA 1953 L44R. 10-26-07 REPAIRED THE DAMAGED AREA PER MD11 SRM 53-10-00 VOL.I REV.40SDR WRLA2007109Seat Track · corrodedDURING 4C+12A CHECK, SEAT TRACK CORROSION FOUND AT STA X=-75.25 Y=1870. REPAIRED PER MD-11 SRM 53-70-00 VOL.1 FIG.1 REV.40.SDR WRLA2007104Unknown · odorFLT 1001 FNLU/KIAH. DURING CRUISE FLT 9+20HRS AFTER DEPART ELEC ODOR EMANATING NEAR INSTRUMENT PANEL. NO SMOKE WAS OBSERVED. SOURCE OF ODOR UNKNOWN. ELEC ODOR DISSIPATED OVER TIME. SEL ANNUNCIATOR LIGHT TEST IND MASTER WARNING, MASTER CAUTION AND ABS DISASDR WRLA2007105Retainer · damagedDURING C-CHECK, FOUND NR 3 PYLON AFT LOWER FAIRING RETAINER DAMAGE. 10-29-07 ACCOMPLISHED ERA NUMBER 07-54-107. REPLACED NR 3 PYLON AFT LOWER FAIRING RETAINER.SDR WRLA2007090Connector · failedFLT 100 KIAH/FNLU ELECTRICAL ODOR/SMELL EMANATING FROM SEATS 25A-C DURING CRUISE. POWER PLUG SUPPLY PULLED C/B TO AFFECTED ZONES. 10-18-07 R & R 26A-C SEAT CONTROL BOX, REPAIRED DAL NR 68 & NR 14 REF WOA WO D10106.SDR WRLA2007088Skin · crackedDURING 3C+12A CHECK, EGAT MECHANIC FOUND CRACK ON RIGHT HAND WING FIXED LEADING EDGE NOSE SKIN AT STA XOS=906. 09-26-07 PERFORM NDT/ET FOR REWORK AREA REF JC 0032337. REPAIR CRACK AREA PER MD-11 SRM 57-10-00 FIG.41 VOL.1 REV.40.SDR WRLA2007089Doubler · crackedDURING 3C+12A CHECK, EGAT MECHANIC FOUND CRACK ON RIGHT HAND WING FIXED LOWER LEADING EDGE STRINGER DOUBLER AT STA XOS 906. 09-26-07 REPAIRED PER MD-11 SRM 57-10-00 FIG.18 VOL.1 REV.40.SDR WRLA2007087Skin · damagedDURING 3C+12A, EGAT MECHANIC FOUND CRACK ON INBOARD FLAP SKIN AT STA XIFH 198, YIFH 40 ON LEFT HAND WING. 09-26-07 PERFORM NDT/ET FOR CUTOUT AREA REF JC31896, NO CRACK FOUND. REPAIR CRACK AREA PER MD11 SRM VOL.157-10-00 REV.40SDR WRLA2007085Bellmouth · crackedTHREE EA CRACKS AT NUMBER 2 ENGINE BELLMOUTH BETWEEN 6-7 O'CLOCK POSITION. REPLACED NR 2 ENGINE BELLMOUTH ASSYWITH NEW PARTS AS PER AMM 71-11-04-000-868/71-11-04-400-868 REV.59SDR WRLA2007086Door Frame · crackedRIGHT WING FIXED LEADING EDGE ANTI-ICING TELESCOPING DUCT DOOR CUT OUT CORNER FOUND CRACK AT STA XOS464 AND XOS470. 09-26-07 PERFORM NDT/ET FOR REWORK AREA REF JC0032000. REPAIR DAMAGE PER MD-11 SRM 57-10-00 VOL.1 REV.40 AND EI NR 2006P20A-124 REV.00. REF SDR WRLA2007082Frame · crackedDURING 3C+12A CHECK, EGAT MECHANIC FOUND RT CENTERLINE LANDING GEAR DOOR FORWARD FRAME EXISTING DOUBLER CRACK AT STA Y=1378.225. 09-26-07 REPLACED THE CRACKED FRAME WITH NEW PART PER MD-11 SRM VOL.II 51-35-01 & 51-33-01 REV.40SDR WRLA2007084Seat Track · crackedDURING 3C+12A CHECK, EGAT MECHANIC FOUND MAIN DECK SEAT TRACK CROWN WORN AT STA Y=625, X=75.25. REPAIRED IAW MD-11 SRM VOL.1 53-70-00 FIGURE 1 REV.40SDR WRLA2007083Seat Track · crackedDURING 3C+12A CHECK, EGAT MECHANIC FOUND MAIN DECK CARGO COMPARTMENT SEAT TRACK CROWN WORN AT STA Y=585, X=27.50. REPAIR IAW MD-11 SRM VOL.1 53-70-00 FIGURE 1 REV.40.SDR WRLA2007076Control Unit · smokeFNLU/KIAH FLT 101 05/31/07. SEAT 14G CONTROL INOPERATIVE. SMOKE AND ODOR COMING FROM SEAT WHEN SEAT ACTIVATED. ISOLATED TO POWER CONTROL UNIT. REMOVED POWER CONTROL UNIT, DEACTIVATED SEAT ELECTRICALLY AS PRECAUTIONARY MEASURE. PLACED SEAT ON DMI M25JU0107SDR WRLA2007068Panel · damagedFLT 8129/LEJ/ATL 05/15/2007. ON POST FLIGHT INSPECTION WORLD AIRWAYS MAINTENANCE FOUND LEFT WING REFUEL PANEL DAMAGED AND PINCHED BY NR 4 LEADING EDGE SLAT. REMOVED LEFT WING FUELING PANEL DOOR, TRIMMED OUT DAMAGE, INSPECTED PER DELTA AIR LINES ERA 461879-14SDR WRLA2007067Skin · deformedDURING PERFORMING 4C CHECK OF DATUM A/C, EGAT FOUND A DEFORMATION ON RIGHT FORWARD PASSENGER DOOR SKIN AFT UPPER CORNER. TRIM OUT DAMAGED AREA AND INSTALL FILLER AND EXTERNAL DOUBLER PER SRM 52-10-00 FIGURE 10.SDR WRLA2007066Drive Assy · shearedAIR RETURN. AFTER TAKEOFF CAPTAIN AND FIRST OFFICER FOUND LONGITUDINAL TRIM HANDLE WOULD NOT TRIM THE HORIZONTAL STAB. STAB REMAINED AT 7.6 UNITS OF TRIM. AUTOPILOT LEFT AND RIGHT DID NOT AFFECT TRIM POSITION. DURING PRESENT AND MODERATE PITCH CHANGE FELT SDR WRLA2007064Seat Track · crackedDURING 4C+30/60M CHECK, EGAT MECHANIC FOUND MAIN DECK CARGO SEAT TRACK CRACK AT Y:755, X:48, Z:-18. [SUP 05-02-07] REPLACED MAIN DECK CARGO SEAT TRACK PER MD-11 SRM 53-70-00 VOL.1 REV 38 FIG.1.SDR WRLA2007065Seat Track · crackedDURING 4C+30/60M CHECK, EGAT MECHANIC FOUND MAIN DECK CARGO SEAT TRACK CRACK AT Y:755, X:78, Z:-18. [SUP 05-02-07] REPLACED MAIN DECK CARGO SEAT TRACK PER MD-11 SRM 53-70-00 VOL.1 REV 38 FIG.1.SDR WRLA2007059Skin · crackedDURING 4C+12A CHECK, EGAT MECHANIC FOUND CRACK ON NR 2 ENGINE INLET COWL INNER SKIN AT 6 O'CLOCK POSITION 1EA, 7 O'CLOCK POSITION 4EA, 8 O'CLOCK POSITION 3EA, 10 O'CLOCK POSITION 1EA, 11 O'CLOCK POSITION 2EA AND 12 O'CLOCK POSITION 1EA. [SUP 05-02-07] REPAIRSDR WRLA2007060Seat Track · corrodedDURING 4C+30/60M CHECK, MAIN DECK CARGO SEAT TRACK CORROSION AT Y:627, X:-28, Z:-18. [SUP 05-02-07] REPLACED MAIN DECK CARGO SEAT TRACK PER MD-11 SRM 53-70-00 VOL.1 REV 38 FIG 1.SDR WRLA2007061Seat Track · wornDURING 4C+30/60M CHECK, MAIN DECK CARGO SEAT TRACK WORN AT Y:630, X:-8, Z:-18. [SUP 05-02-07] REPLACED MAIN DECK CARGO SEAT TRACK PER MD-11 SRM 53-70-00 VOL.1 REV 38 FIG.1.SDR WRLA2007062Seat Track · corrodedDURING 4C+30/60M CHECK, MAIN DECK CARGO SEAT TRACK CORROSION AT Y:735, X:-8, Z:-18. [SUP 05-02-07] REPLACED MAIN DECK CARGO SEAT TRACK PER MD-11 SRM 53-70-00 VOL.1 REV 38 FIG 1SDR WRLA2007063Seat Track · crackedDURING 4C+30/60M CHECK, EGAT MECHANIC FOUND MAIN DECK CARGO SEAT TRACK CRACK AT Y:755, X:28, Z:-18. [SUP 05-02-07] REPLACED MAIN DECK CARGO SEAT TRACK PER MD-11 SRM 53-70-00 VOL.1 REV 38 FIG.1.SDR WRLA2007048Skin · gougedDURING C-04 CHECK, RIGHT WING NR 8 SLAT INTERNAL SURFACE SKIN GOUGE STATION XOS 1009. REPAIRED PER MD-11 SRM 57-10-00 FIG.=10 VOL.1 REV.38SDR WRLA2007053Channel · crackedDURING C-04 CHECK IN TPE, CRACK .55 INCH FOUND ON UPPER HORIZONTAL DECK OF FORWARD AFT FUSELAGE COMPARTMENT AT EMPENNAGE STA Y=2015, X=-14, Z=+61. INSTALLED REPAIR PER MD-11 SRM VOL.I 53-00-01 REV.38 FIG.10SDR WRLA2007051Seat Track · corrodedDURING C-04 CHECK IN TPE, CORROSION FOUND CABIN SEAT TRACK STA Y=460-470, X=-27, Z=-18. INSTALLED SEAT TRACK AND SPLICE PER MD-11 SRM VOL.II 51-33-01 REV.38.SDR WRLA2007052Seat Track · corrodedDURING C-04 CHECK IN TPE, CORROSION FOUND CABIN SEAT TRACK STA Y=855-860, X=10, Z=-18. INSTALLED SEAT TRACK AND SPLICE PER MD-11 SRM VOL.II 51-33-01 REV.38.SDR WRLA2007047Frame · corrodedDURING C-04 CHECK, CORROSION FOUND AT BULKHEAD TEE CHORD STA Y=2007, Z=20, X=-20. REPAIR PER MD-11 SRM 51-33-01 & 51-35-01 REV.38SDR WRLA2007046Floorbeam · brokenDURING C-04 CHECK, FOUND FLOORBEAM BULKHEAD BROKEN AT STA Y=1841 X=42. REPAIRED PER SRM VOL.III 53-16-01 REV.38 AND SRM 53-00-01 VOL.I FIG.10 REV.38SDR WRLA2007042Seat Track · corrodedDURING C-04 CHECK, FOUND SEAT TRACK AREA Y=840-855 X=44 CORRODED. INSTALLED SEAT TRACK AND SPLICE PER MD-11 SRM VOL.II 51-33-01 REV.38.SDR WRLA2007043Longeron · corrodedDURING C-04 CHECK, FOUND LONGERON L40R CORRODED STA Y=1953. PERFORM LONGERON REPAIR PER MD-11 SRM VOL.I 53-10-00 FIG.2 TABLE I R=5. 2.INSTALLED REPAIR FITTING AND REPAIR LONGERON PER MD-11 SRM VOL.II 51-33-01 & 51-35-01 REV.38.SDR WRLA2007044Longeron · corrodedDURING C-04 CHECK, FOUND LONGERON L42R CORRODED STA Y=1953. PERFORM LONGERON REPAIR PER MD-11 SRM VOL.I 53-10-00 FIG.2 TABLE 1 R=5. 2. INSTALLED REPAIR FITTING AND LONGERON PER SRM VOL.II 51-33-01,51-35-01 REV.38.SDR WRLA2007045Longeron · corrodedDURING C-04 CHECK, FOUND LONGERON L52 CORRODED STA Y=1541. REPAIRED PER MD-11 SRM VOL II 51-33-01 REV.38.SDR WRLA2007050Seat Track · corrodedDURING C-04 CHECK IN TPE, CENTER GALLEY AREA SEAT TRACK CORRODED AREA Y=840-850, X=27.5. INSTALLED SEAT TRACK & SPLICE PER MD-11 SRM VOL.II 51-33-01 REV.38SDR WRLA2007041Skin · crackedDURING C-04 CHECK FOUND CRACK LT WING FIXED LEADING EDGE ACCESS DOOR CUTOUT BOTH UPPER SIDE XOS:464 TO XOS:470, NR 3 SLAT. PERFORM REPAIR PER MD-11 SRM 57-10-00 FIG 42 VOL 1 REV 38 TR 57-8SDR WRLA2007049Rib · crackedDURING C-04 CHECK IN TPE, FOUND RT WING FIXED LEADING EDGE SLAT TRACK RIB R16 CRACK .5 INCH XORS:885. REPLACED RIB AND FASTENERS PER MD-11 SRM 51-33-01 VOL.II REV.38.SDR WRLA2007057Seat Track · crackedDURING 4C+30/60M CHECK, MAIN DECK CARGO SEAT TRACK CRACKED AT Y:635, X:27, Z:-18. [SUP 05-02-07] REPLACED MAIN DECK CARGO SEAT TRACK PER MD-11 SRM 53-70-00 VOL.1 REV 38 FIG 1.SDR WRLA2007058Seat Track · crackedDURING 4C+30/60M CHECK, MAIN DECK CARGO SEAT TRACK CRACKED AT Y:635, X:47, Z:-18. [SUP 05-02-07] REPLACED MAIN DECK CARGO SEAT TRACK PER MD-11 SRM 53-70-00 VOL.1 REV 38 FIG.1SDR WRLA2007056Seat Track · crackedDURING 4C+30/60M CHECK, MAIN DECK CARGO SEAT TRACK CRACKED AT Y:635, X:8.5, Z:-18. [SUP 05-02-07] REPLACE MAIN DECK CGO SEAT TRACK PER MD-11 SRM 53-70-00 VOL.1 REV 38.SDR WRLA2007040Slide · unwanted deployR1 SLIDE WAS INADVERTANTLY DEPLOYED, THE DEPLOYMENT WAS UNSUCCESSFUL. REMOVED DEPLOYED SLIDE, REARMED DOOR, REARMED EMERGENCY BOTTLE, REFILLED EMERGENCY DOOR BOTTLE TO NORMAL WORKING PRESSURE OPS CHECK ALL NORMAL. DEFERRED R1 DOOR SLIDE PER MEL 52-10-03 TO DMISDR WRLA2007Floorbeam · corrodedDURING 2C+12A+150M CHECK, EGAT MECHANIC FOUND M/D CARGO FLOORBEAM CORRODED AT STA Y=1321,X= -8 TO -25 AREA. FABRICATED THE NEW PARTS IAW E1 NR W2007P53B-056 REV. 00 AND APPROVED DOCUMENT MFG CONTROL NR PO209366. INSTALLED THE NEW FABRICATED PARTS IAW MD-11F SSDR WRLA2007018Floor Support · brokenDURING 2C+12A+150M CHECK, EGAT MECHANIC FOUND FWD CARGO COMPARTMENT FLOOR PANEL SUPPORT BRACKET AT STA Y=879, RT. FABRICATE THE NEW PARTS IAW E1 NR W2007P53B-057 REV.00 AND APPROVED DOCUMENT MFG CONTROL NR PO209353. INSTALLED THE NEW FABRICATED PARTS IAW MDSDR WRLA2007016Rib · crackedDURING 2C+12A+150M CHECK, MECHANIC FOUND 2 EA RIBS CRACK IN LEFT W/W OUTBOARD END AFT SIDE. REPLACED THE DAMAGED RIBS 2 EA PER MD 11F SRM VOL II 51-35-01 FIG REV 38. CONDITION CHECK NORMAL AND JOB COMPLETED.SDR WRLA2007023Longeron · corrodedDURING 2C+12A+150M CHECK, MECHANIC FOUND CENTER CARGO INTERNAL RT SIDE LONGERON CORRODED BETWEEN STA Y=1621 TO Y=1681 L38R. EGAT NRC U05086. PN ARB1567-1 AND ARB1617-1.SDR WRLA2007024Longeron · corrodedDURING 2C+12A+150M CHECK, MECHANIC FOUND CENTER CARGO INTERNAL RT SIDE LONGERON CORRODED BETWEEN STA Y=1621 TO Y=1681 L39R. EGAT NRC U05086. PN ARB1567-1 AND ARB1617-1.SDR WRLA2007019Floorbeam · corrodedDURING 2C+12A+150M CHECK, EGAT MECHANIC FOUND M/D CARGO FLOORBEAM CORRODED AT STA Y=1321,X= -8 TO -25 AREA. FABRICATED THE NEW PARTS IAW E1 NR W2007P53B-056 REV. 00 AND APPROVED DOCUMENT MFG CONTROL NR PO209366. INSTALLED THE NEW FABRICATED PARTS IAW MD-11F SSDR WRLA2007005Skin · corrodedDURING 2C+12A+150M CHECK, EGAT MECHANIC FOUND CORROSION UNDER LEFT WING T/E FIXED PANEL UPPER SURFACE NEAR NR 5 SPOILER OUTBOARD SIDE. REPAIR THE DAMGED AREA PER EGAT E1 NR W2007A57B-066 REV.OO & APPROVED DOCUMENT BOEING MESSAGE NR 1-277655111-2. 2.CONDITIONSDR WRLA2007006Structure · wornDURING 2C+12A+150M CHECK, EGAT MECHANIC FOUND LEFT MAIN LANDING GEAR DOOR AFT SIDE CORNER HAS WEAR AT STA Y=1461 AREA. REMOVE THE WORN CORNER PER MD-11F SRM VOL.II 51-35-01 REV.38. REPLACED DOOR CORNER PER MD-11F SRM VOL.II 51-35-01 REV.38. 3. CONDITION DOO
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