Pratt & Whitney PW4462

Service difficulty reports · 778

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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"

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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.Oct 8, 2007 · N273WA · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 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.40Oct 8, 2007 · N273WA · Doug MD11 · Fuselage Main, Longeron/StringerSDR 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.Oct 8, 2007 · N273WA · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 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 DISAOct 6, 2007 · N278WA · Doug MD11 · Air Distribution SystemSDR 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.Oct 4, 2007 · N273WA · Doug MD11 · Nacelle/Pylon Miscellaneous StructureSDR 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.Sep 20, 2007 · N278WA · Doug MD11 · Electrical Power System WiringSDR 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.Aug 23, 2007 · N275WA · Doug MD11F · Wing, Plate/SkinSDR 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.Aug 23, 2007 · N275WA · Doug MD11F · Wing, Longeron/StringerSDR 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.40Aug 23, 2007 · N275WA · Doug MD11F · Trailing Edge FlapsSDR 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.59Aug 16, 2007 · N275WA · Doug MD11F · Turbine Engine Air Inlet SectionSDR 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 Aug 16, 2007 · N275WA · Doug MD11F · Wing Main, Frame StructureSDR 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.40Aug 14, 2007 · N275WA · Doug MD11F · Landing Gear DoorsSDR 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.40Aug 14, 2007 · N275WA · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 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.Aug 14, 2007 · N275WA · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 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 M25JU0107May 31, 2007 · N278WA · Doug MD11 · Passenger Compartment EquipmentSDR 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 461879-14May 15, 2007 · N273WA · Doug MD11 · Wing, Plate/SkinSDR 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.May 8, 2007 · N274WA · Doug MD11F · Passenger/Crew DoorsSDR 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 May 6, 2007 · N271WA · Doug MD11 · Stabilizer Position IndicatingSDR 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.Apr 17, 2007 · N274WA · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 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.Apr 17, 2007 · N274WA · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 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] REPAIRApr 13, 2007 · N274WA · Doug MD11F · Nacelle/Pylon, Plate/SkinSDR 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.Apr 12, 2007 · N274WA · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 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.Apr 12, 2007 · N274WA · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 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 1Apr 12, 2007 · N274WA · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 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.Apr 7, 2007 · N274WA · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 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.38Mar 25, 2007 · N271WA · Doug MD11 · Leading Edge DevicesSDR 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.10Mar 18, 2007 · N271WA · Doug MD11 · Fuselage Miscellaneous StructureSDR 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.Mar 18, 2007 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 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.Mar 18, 2007 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 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.38Mar 14, 2007 · N271WA · Doug MD11 · Fuselage Main, BulkheadSDR 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.38Mar 12, 2007 · N271WA · Doug MD11 · Fuselage Main, Floor BeamSDR 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.Mar 12, 2007 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 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.Mar 12, 2007 · N271WA · Doug MD11 · Fuselage Main, Longeron/StringerSDR 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.Mar 12, 2007 · N271WA · Doug MD11 · Fuselage Main, Longeron/StringerSDR WRLA2007045Longeron · corrodedDURING C-04 CHECK, FOUND LONGERON L52 CORRODED STA Y=1541. REPAIRED PER MD-11 SRM VOL II 51-33-01 REV.38.Mar 12, 2007 · N271WA · Doug MD11 · Fuselage Main, Longeron/StringerSDR 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.38Mar 11, 2007 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 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 57-8Mar 9, 2007 · N271WA · Doug MD11 · Wing, Plate/SkinSDR 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.Mar 9, 2007 · N271WA · Doug MD11 · Wing, Rib/BulkheadSDR 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.Mar 9, 2007 · N274WA · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 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.1Mar 9, 2007 · N274WA · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 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.Mar 9, 2007 · N274WA · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 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 DMIFeb 22, 2007 · N275 · Doug MD11F · Escape SlideSDR 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 SFeb 4, 2007 · N276WA · Doug MD11F · Fuselage Main, Floor BeamSDR 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 MDJan 28, 2007 · N276WA · Doug MD11F · Fuselage Miscellaneous StructureSDR 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.Jan 20, 2007 · N276WA · Doug MD11F · Fuselage Main, Longeron/StringerSDR 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.Jan 12, 2007 · N276WA · Doug MD11F · Fuselage Main, Longeron/StringerSDR 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.Jan 12, 2007 · N276WA · Doug MD11F · Fuselage Main, Longeron/StringerSDR 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 SJan 12, 2007 · N276WA · Doug MD11F · Fuselage Main, Floor BeamSDR 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.CONDITIONJan 11, 2007 · N276WA · Doug MD11F · Wing, Plate/SkinSDR 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 DOOJan 11, 2007 · N276WA · Doug MD11F · Landing Gear Doors
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