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"

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.

SDR WRLA2005051Skin · corrodedDURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 23.Feb 11, 2005 · N276 · Doug MD11F · Horizontal Stabilizer, Plate/SkinSDR WRLA2005052Skin · corrodedDURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 19.Feb 11, 2005 · N276 · Doug MD11F · Horizontal Stabilizer, Plate/SkinSDR WRLA2005036Skin · corrodedDURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST RT BARREL NUT HOLE NR 33.Feb 7, 2005 · N276 · Doug MD11F · Horizontal Stabilizer, Plate/SkinSDR WRLA2005039Skin · corrodedDURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST RT BARREL NUT HOLE NR 28.Feb 7, 2005 · N276 · Doug MD11F · Horizontal Stabilizer, Plate/SkinSDR WRLA2005047Skin · corrodedDURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST RT BARREL NUT HOLE NR 05.Feb 7, 2005 · N276 · Doug MD11F · Horizontal Stabilizer, Plate/SkinSDR WRLA2005055Skin · corrodedDURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 09.Feb 7, 2005 · N276 · Doug MD11F · Horizontal Stabilizer, Plate/SkinSDR WRLA2005057Spar Cap · corrodedDURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 01.Feb 7, 2005 · N276 · Doug MD11F · Horizontal Stabilizer, Spar/RibSDR WRLA2005066Skin · corrodedDURING "C04" CHECK INSPECTION, FOUND CORROSION IN CENTER WING SECTION UPPER SURFACE AT S-15 STR X=47.5 TO X=-47.5.Feb 7, 2005 · N276 · Doug MD11F · Wing, Center BoxSDR WRLA2005007Slide · malfunctionedITEM: DURING "C4" CHECK IN TPE R1 SLIDE DEPLOY TEST FAILED, THE SLIDE FELL INSIDE THE GALLEY AREA, AND NOT OUTSIDE THE AIRCRAFT AS IT SUPPOSED TO.Feb 6, 2005 · N276 · Doug MD11F · Escape SlideSDR WRLA2005035Spar Cap · corrodedDURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST RT BARREL NUT HOLE NR 36.Feb 6, 2005 · N276 · Doug MD11F · Horizontal Stabilizer, Tab StructureSDR WRLA2005067Longeron · corrodedDURING "C04" CHECK INSPECTION, FOUND CORROSION IN CENTER CARGO LONGERON AT STA 5-120 L44R.Feb 5, 2005 · N276 · Doug MD11F · Fuselage Main, Longeron/StringerSDR WRLA2005068Longeron · corrodedDURING "C04" CHECK INSPECTION, FOUND CORROSION IN CENTER CARGO LONGERON AT STA 5-120 L45R.Feb 5, 2005 · N276 · Doug MD11F · Fuselage Main, Longeron/StringerSDR WRLA2005069Structure · corrodedDURING "C04" CHECK INSPECTION, FOUND CORROSION IN T CHORD IN AFT CARGO PRESSURE BULKHEAD L27 AND STA 2007, X=-27.5.Feb 5, 2005 · N276 · Doug MD11F · Fuselage Main, BulkheadSDR WRLA2005021Longeron · corrodedDURING "4C" CHECK FOUND CORROSION IN CENTER CARGO LONGERON AT STA 5-120 L44R.Feb 2, 2005 · N276 · Doug MD11F · Fuselage Main, Longeron/StringerSDR WRLA2005022Longeron · corrodedDURING "4C" CHECK FOUND CORROSION IN CENTER CARGO LONGERON AT STA 5-120 L45R.Feb 2, 2005 · N276 · Doug MD11F · Fuselage Main, Longeron/StringerSDR WRLA2005023Support Fitting · corrodedDURING "4C" CHECK, FOUND CORROSION IN CENTER L/G W/W LT TRUNNION SUPPORT FITTING BOOT STRAP AT STA Y=1471.Feb 2, 2005 · N276 · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR WRLA2005070Strap · corrodedDURING "C04" CHECK INSPECTION, FOUND CORROSION IN CENTER LANDING GEAR W/W LT TRUNNION SUPPORT FITTING BOOT STRAP AT STA Y=1470.Feb 2, 2005 · N276 · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR WRLA2005008Skin · damagedITEM: DURING "C2" CHECK IN TPE, FOUND RIGHT WING INBD FLAP VANE SKIN DISBAND. CUT OUT DAMAGED SKIN AREA WITH 0.5" MIN RADIUS PER MD11 SRM 57-90-00 VOL I AND FAA FORM 8100-9 DATED 01/27/05. ACCOMPLISHED CO-CURE REPAIR USING FM300-2 AT 250DEG "F" FOR 90 TO 100Feb 1, 2005 · N273 · Doug MD11 · Trailing Edge FlapsSDR WRLA2005016Skin · corrodedDURING "C2" CHECK INSPECTION, FOUND CORROSION AT BARREL NUT HOLE NR 1 RT. REAMED SUBJECT BARREL NUT HOLE TO 1.594" DIA, PER SECTION 7 OF E/O 02-5510-098 REV 03 AND FABRICATED REPAIR BUSHING PER SECTION 12 OF SAME E/O. CLEANED AND REINSPECTED BOLT AND BARREL Feb 1, 2005 · N273 · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR WRLA2005017Skin · corrodedITEM: DURING "C2" CHECK INSPECTION, FOUND CORROSION AT BARREL NUT HOLE NR 36 RT. CLEANED CORROSION AND OVERSIZED BARREL NUT HOLE TO 2.587" DIA, PER SECTION 7 OF E/O 02-5510-098 REV 03 AND FABRICATED REPAIR BUSHING PER SECTION 12 OF SAME E/O. CLEANED AND REINFeb 1, 2005 · N273 · Doug MD11 · Fuselage Main, Plate/SkinSDR WRLA2005009Skin · canningDURING "C2" CHECK FOUND RIGHT INBD FLAP UPPER SKIN HAVE ONE OIL-CANNING AT XIFH 286 ABOVE T/E 24" L=3" W=3". CUTOUT DAMAGED SKIN AND REPAIRED WITH EXTERNAL DOUBLER (2024-T3 .050 CLAD, L=5.625" W=5") AND RIVET (CR32245-4) REF MD11 SRM 57-20-00 VOL I REV 36 FIGJan 31, 2005 · N273 · Doug MD11 · Trailing Edge FlapsSDR WRLA2005010Skin · dentedDURING "C2" CHECK, FOUND DENT LOCATED AT RT INBD FLAP LOWER SKIN XIFH193 ABOVE T/E 9" L=1.5" W=0.066". CUTOUT AREA 2 INCH BY 1 INCH AND REPAIRED DAMAGE AREA WITH DOUBLER (2024-T3 .050 ALU SHEET) AND RIVET(CR3224-5). CONDITION CHECK SATISFACTORY REF MD11 SRM Jan 31, 2005 · N273 · Doug MD11 · Trailing Edge FlapsSDR WRLA2005011Skin · dentedDURING "C2" CHECK, FOUND RT INBD FLAP LOWER SKIN DENT AT XIFH 139 ABOVE T/E 58" L=0.5" W=0.75" D=0.065". CUTOUT DENT AREA 1.5' BY 1", FABRICATED REPAIR DOUBLER 6" BY 6" (2024-T3 .063" ALU SHEET) AND USED RIVET CR3224-5 TO REPAIR THE DENT. CONDITION CHECK SATJan 31, 2005 · N273 · Doug MD11 · Trailing Edge FlapsSDR WRLA2005012Seat Track · corrodedDURING "C2" CHECK, FOUND SEAT TRACK CORROSION BETWEEN STA 1371 AND STA 1521 X=-75.25. CUTOUT AND REMOVED CORRODED SECTION BETWEEN STA 1371 AND 1531 X=-75.25, FABRICATED AND INSTALLED NEW SEAT TRACK SECTION AND SPLICE HAT. CONDITION CHECK SATISFACTORY REF MD1Jan 31, 2005 · N273 · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR WRLA2005013Seat Track · corrodedDURING "C2" CHECK, FOUND CABIN SEAT TRACK CORROSION BETWEEN STA 865 AND STA 880 X=-8.5. CUT AND REMOVED SECTION BETWEEN STA 832 AND 929 X=-8.5, FABRICATED AND INSTALLED NEW SEAT TRACK SECTION AND SPLICE HAT. CONDITION CHECK SATISFACTORY REF MD11 SRM 53-70-00Jan 31, 2005 · N273 · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR WRLA2005014Seat Track · corrodedDURING "C2" CHECK FOUND CABIN SEAT TRACK CORROSION BETWEEN STA 840 AND STA 860 X=-44.5. CUT AND REMOVED CORRODED SECTION BETWEEN STA 832 AND 909 X=-44.5, FABRICATED AND INSTALLED NEW SEAT TRACK SECTION AND SPLICE HAT. CONDITION CHECK SATISFACTORY REF MD11 SRJan 31, 2005 · N273 · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR WRLA2005015Seat Track · corrodedDURING "C2" CHECK FOUND CABIN SEAT TRACK CORROSION BETWEEN STA 840 AND STA 870 X=-27.5. CUT AND REMOVED CORRODED SECTION BETWEEN STA 832 AND 869 X=-27.5, FABRICATED AND INSTALLED NEW SEAT TRACK SECTION AND SPLICE HAT PER MD11 SRM 53-70-00 FIG 1 REV 36 VOL I. Jan 31, 2005 · N273 · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR WRLA2005018Seat Track · corrodedDURING "C2" CHECK, FOUND CABIN SEAT TRACK CORROSION BETWEEN STA 858 AND STA 873 X=27.5. CUT AND REMOVED CORRODED SECTION BETWEEN STA 816 AND 909 X=75.25, FABRICATED AND INSTALLED NEW SEAT TRACK SECTION AND SPLICE HAT. CONDITION CHECK SATISFACTORY REF MD11 SRJan 31, 2005 · N273 · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR WRLA2005019Seat Track · corrodedDURING "C2" CHECK FOUND CABIN SEAT TRACK CORROSION BETWEEN STA 858 AND STA 873 X=27.5. CUT AND REMOVED CORRODED SECTION BETWEEN STA 832 AND 909 X=27.5, FABRICATED AND INSTALLED NEW SEAT TRACK SECTION AND SPLICE HAT. CONDITION CHECK SATISFACTORY REF MD11 SRM Jan 31, 2005 · N273 · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR WRLA2005020Longeron · corrodedDURING "C2" CHECK, FOUND CORROSION ON LONGERON L46L BETWEEN STA 5-73 AND STA 5-93. CUT AND REMOVED CORRODED SECTION BETWEEN STA 5-63 AND 5-103, CUT FRAME STA 5-73 TO STA 5-93 TO PROVIDE ACCESS FOR REMOVAL/INSTALLATION OF LONGERON L46L. FABRICATED NEW LONGEROJan 31, 2005 · N273 · Doug MD11 · Fuselage Main, Longeron/StringerSDR WRLA2005003A/C Pack · odor"LAV SMOKE" IN COMBINATION WITH A STRONG OILY SMOKE SMELL IN BOTH CABIN AND COCKPIT ON DEPARTURE. TURNING OFF NR 1 PACK ELIMINATED BOTH "LAV SMOKE" INDICATION AND SMELL. "LAV SMOKE" WAS IN FWD LAV. OPEN PACK COMPARTMENT AND RAN PACK, TEMPERATURE AND ALL OPEJan 5, 2005 · N803 · Doug MD11 · Cabin Cooling SystemSDR WRLA2005002A/C Pack · smokeDURING START OF TAXI, SMOKE FROM AIR CONDITIONING DUCT IN COCKPIT. NR 1 AIR CONDITIONING PACK WAS SELECTED OFF. NO FURTHER CREW ACTION TAKEN. AIRCRAFT RETURNED TO BLOCKS. ENTERED IN DMI M21JA0405-13 PER MEL 21-51-1, NR 1 PACK INOP.Jan 4, 2005 · N271 · Doug MD11 · Cabin Cooling SystemSDR WLDA2004121Solenoid · overheatedSMOKE IN COCKPIT WHEN TAXI FOR TAKEOFF, RETURNED TO BLOCKS. FOUND DOOR SOLENOID VERY HOT AND SMOKING. DISCONNECTED AND TAPED WIRES BACK. C/B PULLED AND TRANSFERRED TO DMI M52DE2604-134 PER MEL 52-54-2 CAT "A".Dec 26, 2004 · N271 · Doug MD11 · Passenger/Crew DoorsSDR 04FDEA03481Engine · failedNR 2 ENGINE VIBRATION AT TAKEOFF ROTATION FOLLOWED BY A BANG AT ROTATION. COMPRESSOR STALL REPORTED BY ANOTHER AIRCRAFT. EXCEEDENCE WENT AMBER TO 5.3 ON CLIMB & 4.4 IN CRUISE AT 10K FT, VIBRATION NOTICABLE IN CRUISE WITH ENGINE & WING ANTI-ICE ON & IGNITION Dec 24, 2004 · N580FE · Doug MD11 · Engine (Turbine/Turboprop)SDR WLDA2004108Warning Light · illuminatedAED/ODN COCKPIT DOOR LOCK OVERHEATED INFLIGHT. CABIN CREW SMELLED SMOKE, PULLED DOOR C/B, HEAT AND SMELL DISSIPATED. ENTERED IN DMI M52DE0604-35 CAT-A PER MEL 52-54-2.Dec 6, 2004 · N271 · Doug MD11 · Door Warning SystemSDR WLDA2004107Controller · malfunctionedFRA/KWI REJECTED TAKEOFF AT 40 KTS DUE TO FLAPS TAKEOFF WARNING. RECYCLED FLAPS, OPERATIONS CHECK ALL NORMAL. RESUMED NORMAL PROCEDURES.Nov 27, 2004 · N272 · Doug MD11 · Trailing Edge Flap Control SystemSDR WLDA2004105Sensor · seizedFRA/KWI ABORTED TAKEOFF AT 130 KTS DUE TO LEVEL II TIRE FAILURE AURAL & VISUAL ALERT. FOUND NR 2 TIRE PRESS SENSING UNIT SEIZED. DEACTIVATED SENSING UNIT AND ENTERED IN DMI M32NO2504-138 PER MEL 32-46-3 CAT-C. PERFORMED RTO INSPECTION AS PER WO CARD 0259 NINov 25, 2004 · N271 · Doug MD11 · Brake Anti-Skid SectionSDR WLDA2004103Floor Support · crackedDURING C2 CHECK INSPECTION, FOUND CRACK IN TWO FLOOR PANEL SUPPORT ABOVE 1 INCH AND 1.5 INCH AT STA 1541 RBL 0 TO RBL 30, LBL 0 TO LBL 30. REPAIRED CRACKED AREA USING REPAIR DOUBLERS PER MD11 SRM53-00-01 FIG 5,VOL1 REV 36.Nov 3, 2004 · N279 · Doug MD11 · Fuselage Miscellaneous StructureSDR WLDA2004104Drain · corrodedDURING C2 CHECK INSPECTION FOUND CORROSION IN WASTE TANK DRAIN PAN AT STA 1970 BETWEEN L50L AND L50R. REMOVED WASTE TANK DRAIN PAN AND INSTALLED NEW PART PER MD11 SRM 51-33-01 VOL II REV 36. APPLIED PROTECTION COATING.Nov 3, 2004 · N279 · Doug MD11 · Fuselage Structure (General)SDR 04FDEA02995Warning Light · illuminatedON TAKEOFF, POSSIBLE LIGHTING STRIKE. SHORTLY AFTER RECEIVED (EPGS FAULT) AND (EMERG PWR ON) ALERTS. ALL BUSSES POWERED, ALL GENERATORS OUTPUT NORMAL. REFD QRH AT SAME TIME CAPT'S NO DEFECTS DISPLAYED (MAP FAIL ALERT. SELECTED CAPT ON FMS2 AND CONTINUED OOct 26, 2004 · N620FE · Doug MD11F · AC InverterSDR WLDA2004111Stringer · crackedDURING 2C+12A CHECK, FOUND RT WING FIXED L/E SKIN CRACK ABOUT 10" AND STRINGER DOUBLER CRACK AT STA XOS 906. REPAIRED CRACK ON RT WING FIXED L/E SKIN PANEL AND STRINGER DOUBLER AT STA XOS 906 PER EGAT EI W2004A57B-558 REV 00. (MD-11 SRM VOL.I 57-10-00 FIG 18 Oct 14, 2004 · N271 · Doug MD11 · Wing, Longeron/StringerSDR WLDA2004112Skin Panel · puncturedDURING 2C+12A CHECK, FOUND LT WING NR 1 SLAT L/E AREA HOLE DAMAGE AT STA XIS 186. REPAIRED DAMAGE AREA PER EGAT EI W2004A 57B-560 REV 00 (MD-11 SRM VOL.I 57-10-00 FIG 33 SHEET 6 AND 7). PERFORMED SLAT OPERATION CHECK, FOUND NORMAL.Oct 14, 2004 · N271 · Doug MD11 · Leading Edge DevicesSDR WLDA2004113Skin Panel · dentedDURING 2C+12A CHECK, FOUND 2EA SHARP DENT ON LT WING NR 1 SLAT UPPER SKIN PANEL LOCATED AT STA XIS 240. REPAIRED DAMAGE AREA PER EGAT EI W2004A 57B-564 REV 00(MD-11 SRM VOL.I 57-10-00 FIG 33 SHEET 6 AND 7). SLAT OPERATION AND CONDITION CHECK SATISFACTORY.Oct 14, 2004 · N271 · Doug MD11 · Leading Edge DevicesSDR WLDA2004114Skin · dentedDURING 2C+12A CHECK, FOUND SHARP DENT ON LT WING NR 3 SLAT UPPER SKIN AND INNER RIB AT STA XOS 414. REPAIRED DAMAGE AREA PER EGAT EI W2004A 57B-581 REV 00(MD-11 SRM VOL.I 57-10-00 FIG 33). PERFORMED SLAT OPERATION AND CONDITION CHECK, FOUND SATISFACTORY.Oct 14, 2004 · N271 · Doug MD11 · Leading Edge DevicesSDR WLDA2004115Skin Panel · scratchedITEM: DURING 2C+12A CHECK, FOUND 3 EA SCRATCH ON EXTERNAL SKIN ON LT HST L/E BETWEEN XFS 275.410 AND XFS 263.762. BLENDED REPAIR PER EGAT EI W2004A 55B-575 REV 00 (1-PGVIM WITH FAA 811-3 FORM DATED SEP/23/2004). CONDITION CHECK FOUND SATISFACTORY.Oct 14, 2004 · N271 · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR WLDA2004116Seat Track · corrodedDURING 2C+12A CHECK, FOUND CABIN SEAT TRACK CORRODED AT STA Y=959 X=-8.5. REPAIRED DAMAGED SEAT TRACK PER MD-11 SRM VOL.I 53-70-00, CONDITION CHECK SATISFACTORY.Oct 14, 2004 · N271 · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR WLDA2004117Web · crackedDURING 2C+12A CHECK, FOUND CRACK AT CENTER CARGO COMPARTMENT STA 1841 L-50 RT WEB. REPAIRED CRACK ON FUSELAGE FRAME WEB STA 1841 L-50 RT PER EGAT EI W2004A53B-559 REV.00 (FAA 8110-3 FORM DATED SEP/23/2004). CONDITION CHECK SATISFACTORY.Oct 14, 2004 · N271 · Doug MD11 · Fuselage Miscellaneous StructureSDR WLDA2004118Support Fitting · corrodedDURING 2C+12A CHECK, FOUND CORROSION IN CENTER WING W/W RT/LT SUPPORT FITTING AT STA Y=1481 X=-31.5 AND X=31.5. REPAIRED CORROSION ON LT/RT FWD TRUNNION FITTING BOOT STRAP OF CENTER MLG PER EGAT EI W2004A53B-590 REV.00 (FAA 8110-3 FORM DATED OCT/04/2004). CONOct 14, 2004 · N271 · Doug MD11 · Fuselage Main, Attach FittingsSDR WLDA2004119Skin Panel · nickedDURING C2+12A CHECK, FOUND NICK ON RT WING INBOARD FLAP ON STA XIFH 152WITH D=0.039" AND L=3/8". REPAIRED NICK ON RT WING INBOARD FLAP UPPER SKIN AT XIFH 152 PER EGAT EI W2004A57B-585 REV.00 (MD-11 SRM VOL.I 57-10-00 FIG 34 SHEET 3). CONDITION CHECK SATISFACOct 14, 2004 · N271 · Doug MD11 · Leading Edge DevicesSDR WLDA2004120Skin · crackedDURING 2C+12A CHECK, FOUND LT WING NR 2 SLAT OUTBOARD SIDE ANGLE/UPPER SKIN PANEL CRACK AT XIS 360. REPAIRED LT WING NR 2 SLAT OUTBOARD SIDE ANGLE/UPPER SKIN PANEL CRACK PER EGAT EI W2004A57B-592 REV.00 (MD-11 SRM VOL.I 57-10-00 FIG 33 AND FIG 10). PERFORMEDOct 14, 2004 · N271 · Doug MD11 · Leading Edge Devices
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