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 WRLA2008068Doubler · crackedDURING "A4" CHECK INSPECTION IN ZRH FOUND TWO CRACKS IN THE LT AND RT MACHINED DOUBLERS IN THE CENTER LANDING GEAR BAY STA Y=1381. THE CRACKS WERE LOCATED IN THE VERTICAL ROW OF RIVETS THAT ATTACH THE DOUBLER TO THE VERTICAL STIFFENER. THE CRACKS STARTED ANDSDR WRLA2008066ADoubler · crackedDURING "A4" CHECK INSPECTION IN ZRH FOUND TWO CRACKS IN THE LT AND RT MACHINED DOUBLERS IN THE CENTER LANDING GEAR BAY STA Y=1381. THE CRACKS WERE LOCATED IN THE VERTICAL ROW OF RIVETS THAT ATTACH THE DOUBLER TO THE VERTICAL STIFFENER. THE CRACKS STARTED ANDSDR WRLA2008065Longeron · corrodedDURING "C" CHECK INSPECTION IN TPE, FOUND CENTER CARGO LONGERON 49R CORROSION AT STA Y=1707. REPAIRED THE CTR CARGO LONGERON 49R AT STA Y -1707 PER MD-11 SRM 53-10-00 REV. 40. CONDITION CHECK NORMAL AND JOB COMPLETED. (S)SDR WRLA2008064Actuator · odorFLT 1000 (KIAH/FNLU) ITEM: DURING FLIGHT, SMOKE/FUMES IN CABIN IN VICINITY OF ROW 16 & 17. MAINTENANCE FOUND LARGEST ACTUATOR AT SEAT 18G AS SOURCE OF ELECTRICAL ODOR. DEACTIVATED CONTROL BOX FOR SEATS 18 D&G BY STOWING CONNECTORS AND PULLED C/B. REMOVED ASDR WRLA2008061Wedge · debondedDURING 4C CHECK INSPECTION DISBOND WAS FOUND ON THE LT WING OUTBOARD AILERON BETWEEN T/E CORE AND THE UPPER SKIN ASSEMBLY. BOEING HAS AUTHORIZED A TEMPORARY REPAIR WITH A-CHECK REINSPECTIONS AND C-CHECK PERMANENT REPAIR. (A)SDR WRLA2008062Fairing · dentedDURING C CHECK INSPECTION DENT FOUND NR 3 ENGINE NOZZLE FAIRING SKIN DENT AT NAC BETWEEN 3O`CLOCK AND 4O`CLOCK POSITION. (LOOKING FORWARD). REPAIRED NR3 ENG NOZZLE FAIRING SKIN IAW EI W2008 A54B-687 REV.00. JOB COMPLETED AND CONDITION CHECK NORMAL. (A) (S)SDR WRLA2008063Structure · crackedDURING C CHECK INSPECTION CRACK-FOUND RT WING LE INBD SLAT NR 1 AFT SIDE HAD CRACK 11.5 INCHES LONG AT XIS 247. REMOVED THE RT INBD NR 1 SLAT ASSY COMPLETED PER AMM 27-80-20-000-801 REV 62. REPAIRED THE DAMAGED AREA IAW MD-11 SRM VOL ONE 57-10-00 REV. 40. ISDR WRLA2008059Engine · oil consumptionGEC8284 EDDP/K JFK 07/16 ITEM: PRECAUTIONARY SHUT DOWN OF NR 3 ENG DUE TO OIL QUANTITY IN THE RESERVOIR, 2 QUARTS, BOXED IN YELLOW ON SHUT DOWN. OIL TEMP 108C OIL PRESSURE 146PSID AT FL 280 THROTTLE IDLE, N2 69.5. OPEN. (S)SDR WRLA2008069Fuel/Oil Cooler · crackedPRECAUTIONARY SHUT DOWN OF NR 3 ENG DUE TO OIL QUANTITY IN THE RESERVOIR, 2 QUARTS, BOXED IN YELLOW ON SHUT DOWN. OIL TEMP 105C OIL PRESSURE 148 PSID AT FL 280 THROTTLE IDLE, N2 69.3. RAN ENG AND FOUND LEAK AT EXISTING WELD ON FUEL/OIL COOLER. REMOVED AND RSDR WRLA2008049Chiller · malfunctionedKDFW/KATL: FORWARD CHILLER POPS C/B IN FLIGHT WITH ASSOCIATED ODOR OF ELECTRICAL SMOKE. REMOVED AND REPLACED FWD GALLEY CHILLER, OPS CHECK SATISFACTORY PER MD-11 25-37-82. (A)SDR WRLA2008045Attach Fitting · missingKBGR/EDDP - DURING POST-FLIGHT INSPECTION, MAINTENANCE FOUND AFT LT CENTER GEAR DOOR MECHANICAL ACTUATOR ATTACH FITTING AND HARDWARE MISSING. REPLACED BRACKET ASSY AND R&R ROD END IAW MM 32-59-03, RETRACTED & EXTENDED CRT CREA IAW MM 32-35-00 OPS CK OK LEAK CSDR WRLA2008025Skin · debondedDURING C-CHECK INSPECTION FOUND LEFT INBOARD FLAP VANE LOWER SKIN DISBONDED TWO PLACES (20" X 23.5", 18" X 22"). REPAIRED LH FLAP VANE REF JOB CARD 038236 ITEM 1.SDR WRLA2008026Venturi · obstructedDURING C-CHECK INSPECTION L1 SLIDE FAILED TO DEPLOY TEST PER WOA J/C WA1095, SLIDE FAILED TO FULLY INFLATE DUE TO PLASTIC COVERING AIRCRAFT OBSTRUCTED VENTURI. REPLACED SLIDE/RAFT IAW WOA CARD NBR 0048.SDR WRLA2008021Stanchion · corrodedDURING C-CHECK INSPECTION, CORROSION FOUND FWD CARGO COMPARTMENT AND DEFORM ON LT SIDE AFT BULKHEAD PANEL SUPPORT STANCHION AT STA Y=1129.
SDR WRLA2008022Sensor · malfunctionedDURING APPROACH RECEIVED SLAT DISAGREE ALERT, FOLLOWED BY STICK SHAKER. PERFORMED SLAT DISAGREE CHECKLIST, DIVERTED TO KPSM DUE TO RUNWAY CONDITIONS. EMERGENCY DECLARED. REPLACED SLAT POS. SENSORS D1-17 AND D1-18 PER MM 27-84-02. PERFORMED THE SLAT RANGE OFSDR WRLA2008020Flap System · frozenON APPROACH FLAPS WOULD NOT EXTEND, NO FLAPS/SLATS EXTENDED CHECKLIST ACCOMPLISHED, EMERGENCY DECLARED. FOUND AREA ABOVE LT & RT MAIN GEAR BOX FLOODED WITH WATER & FROZEN. DRAINED & VENTILATED DRY. REPLACED INSULATION BLANKETS BS 1381-1521 MM 25-85-01. FLOOR SDR WRLA2008019Flap System · jammedEDDF/CYYZ - FLAPS WOULD NOT EXTEND FOR APPROACH AND LANDING. FLAP HANDLE JAMMED PHYSICALLY. PERFORMED NO FLAP/SLAT EXTENDED LANDING CHECKLIST, DECLARED EMERGENCY. PERFORMED OPERATION OF FLAPS IAW MD-11 MM 27-50-00. ACTUATED FLAPS FROM 0-50 DEGREES THEN STSDR WRLA2008018Flap System · malfunctionedCYYZ/EDDP - ACCOMPLISHED SLATS ONLY APPROACH AND LANDING. FLAPS WOULD NOT EXTEND WHILE ON APPROACH OR AFTER LANDING. PERFORMED FUNCTIONAL TEST OF FLAP SYSTEM, PERFORMED RTS OF FLAP SYSTEM IN FCC 1 & 2, ALL TEST PASSED. NO DEFECTS NOTED. COULD NOT DUPLICATESDR WRLA2008017Skin · crackedDURING A CHECK INSPECTION 9 INCH CRACK FOUND RIGHT WING INBOARD FLAP UPPER SKIN INBOARD AFT SKIN PANEL AT XIFH231.2. REPAIRED PER MD-11 SRM 57-20-00 VOL 1 REF ERA 466462-14.SDR WRLA2008016Skin · debondedDURING C-CHECK MECHANIC FOUND LEFT WING INBOARD FLAP VANE LOWER SKIN DISBONDED 2 PLACES. REPAIRED PER ENGINEERING INSTRUCTION W2008A57B-082 REV.00. REF NRC U01041.SDR WRLA2008015Fairing · crackedDURING C-CHECK INSPECTION, FOUND 2 INCH CRACK IN NR 1 ENGINE LOWER RIGHT AFT SECTION FAIRING. REPAIRED PER ENGINEERING INSTRUCTION NR W2008A57B-059 REV.00. REF EGAT NRC U05004.SDR WRLA2008014Oven · defectiveOKBK/EDDP. OVEN 509 MID GALLEY INOP BURNING SMELL WHEN USED. REMOVED AND REPLACED MID GALLEY OVEN 509 REF MM 25-33-00. DMI CLOSED.SDR WRLA2008009Seat Track · corrodedDURING C-CHECK INSPECTION FOUND SEAT TRACK CORROSION AT STA Y=840 TO 859 X=14. BLENDED CORROSION, WITHIN ALLOWABLE LIMITS PER MD11 SRM VOL.1 53-00-01 FIG.3 REV.40. REF EGAT NRCU 05022.SDR WRLA2008012Angle · corrodedDURING C-CHECK INSPECTION FOUND CORROSION ON LOWER CHORD AT STA Y=1964 L48L. BLENDED CORROSION, AREA MEASURED WITHIN LIMITS PER SRM VOL.1 53-00-01 FIG.3 REV.40.SDR WRLA2008008Floor Support · corrodedDURING C-CHECK INSPECTION FOUND AFT FUSELAGE FLOOR SUPPORT CORROSION AT STA Y=2007, X= 56.65. REPLACED AFT FLOOR SUPPORT PER MD11 SRM VOL.II 51-35-01 FIG.1 REV.40.SDR WRLA2008007Floor Support · corrodedDURING C-CHECK INSPECTION FOUND AFT FUSELAGE FLOOR SUPPORT CORROSION AT STA Y=2000, X= -56.65. REPLACED AFT FUSELAGE FLOOR SUPPORT PER MD-11 SRM VOL.II 51-35-01 FIG.1 REV.40.SDR WRLA2008003Floor Support · corrodedDURING C-CHECK INSPECTION FOUND AFT FUSELAGE FLOOR SUPPORT CORROSION AT STA Y=2007, X= -23.5. REPLACED AFT FUSELAGE FLOOR SUPPORT PER MD-11 SRM VOL.II 51-35-01 FIG.1 REV.40.SDR WRLA2008004Floor Support · corrodedDURING C-CHECK INSPECTION FOUND AFT FUSELAGE FLOOR SUPPORT CORROSION AT STA Y=2007, X= 23.5. REPLACED AFT FLOOR SUPPORT PER MD-11 SRM VOL.II 51-35-01 FIG.1 REV.40.SDR WRLA2008005Floor Support · corrodedDURING C-CHECK INSPECTION FOUND AFT FUSELAGE FLOOR SUPPORT CORROSION AT STA Y=2007, X=27.5. REPLACED AFT FLOOP SUPPORT PER MD-11 SRM VOL.II 51-35-01 FIG.1 REV.40.SDR WRLA2008006Floor Support · corrodedDURING C-CHECK INSPECTION FOUND AFT FUSELAGE FLOOR SUPPORT CORROSION AT STA Y=2007, X= -27.5. REPLACED AFT FUSELAGE FLOOR SUPPORT PER MD-11 VOL.II 51-35-01 FIG.1 REV.40.SDR WRLA2008002Access Panel · crackedDURING C-CHECK INSPECTION FOUND RT WING OUTBOARD SLAT DRIVE MECHANISM ACCESS PANEL SKIN CRACKED. REPAIRED RT WING ACTUATOR ACCESS DOOR OUTER SKIN AT XOS STA 490.85 PER EGAT EI NR W2008A57B-022.SDR WRLA2008001Skin · crackedDURING C-CHECK INSPECTION FOUND CRACK ON RIGHT FWD AIR CONDITION COMPARTMENT DOOR OUTER SKIN UPPER EDGE APPROX 4.5 INCHES. REPAIRED PER MD-11 SRM 52-10-00 VOL.I REV.40.SDR 07FDEA05112Engine · power lossDURING CLIMB FROM FL320 TO FL340 NOTICED A/C DETERIORATION. NR 2 ENG EPR READ .40 LESS THAN NR 1 AND NR 3. N1 READING 20 PERCENT LESS THAN 1 AND 3, N2 20 PERCENT LESS AS WELL. ENG 2 THROTTLE, MOVEMENTS RESULTED IN SLUGGISH RESPONSE W/MAX EPR OUTPUT OF 1.0SDR WRLA2007134Oven · faultyDURING OVEN OPERATIONS, ELECTRICAL BURNING ODOR DETECTED. OVEN SHUT OFF AND BREAKERS PULLED. ODOR WENT AWAY. REMOVED AND REPLACED OVEN IAW MM 25-35-10. OPS CHECK GOOD.SDR WRLA2007127Support Beam · corrodedDURING C-CHECK INSPECTION CORROSION FOUND RT WING TO BODY FAIRING SUPPORT BEAM AT STA Y=1348 Z=-20. REPAIRED THE RT WING TO BODY FAIRING SUPPORT BEAM AT STA Y=1348 Z-20 PER SRM VOL 1 53-00-01 FIG 9 REV 40. REF EGAT NRC U05030.SDR WRLA2007121Skin · corrodedDURING C-CHECK INSPECTION CORROSION FOUND ON RIGHT CENTER WING TANK UPPER SKIN AT XCW=110S1. ACCOMPLISHED ENGINEERING INSTRUCTION NO.W2007A57B-668 REV.00, REPAIR CORROSION ON CENTER WING UPPER SKIN UPPER SURFACE AT XCW=110 S1. REF EGAT NRC U05027.SDR WRLA2007120Seat Track · corrodedDURING C-CHECK INSPECTION FOUND CORROSION AFT CABIN FLOOR CURVED SEAT TRACK AT STA Y=2007 X =107.25. REF EGAT NRC U05001. REPLACED THE DAMAGED AREA PER MD11 SRM 53-70-00 VOL.I FIGURE 8 REV.40. REF EGAT NRC U05028.SDR WRLA2007123Seat Track · corrodedDURING C-CHECK INSPECTION CORROSION FOUND RIGHT HAND SEAT TRACK STA Y=555 X=75.25. REPLACED DAMAGED SEAT TRACK PER MD11 SRM 51-33-01 VOL.II REV.40.SDR WRLA2007125Tee Fitting · corrodedDURING C-CHECK INSPECTION, CORROSION FOUND ON BULKHEAD TEE CHORD STA Y=2007 X=27.5. REPLACED DAMAGE TEE CHORD PER MD11 SRM VOL.II 51-35-01 REV.40 REF EGAT NRC U05014.SDR WRLA2007126Floor Support · corrodedDURING C-CHECK INSPECTION CORROSION FOUND ON AFT FUSELAGE FLOOR SUPPORT AT STA Y=1990 X=27.5. REPLACED DAMAGE SUPPORT PER MD11 SRM VOL.1 51-31-01 REV.40 REF EGAT NRC U05024.SDR WRLA2007128Floor Support · corrodedDURING C-CHECK INSPECTION CORROSION FOUND AFT FUSELAGE FLOOR SUPPORT AT STA Y=2007 X=-23.5. REPLACED DAMAGED SUPPORT PER MD11 SRM VOL II 51-31-01 REV 40. REF EGAT NRC U05025.SDR WRLA2007122Floor Support · corrodedDURING C-CHECK INSPECTION FOUND CORROSION AFT FUSELAGE FLOOR SUPPORT AT STA Y=2007 X=23.5. REPLACED DAMAGED FLOOR SUPPORT PER SRM 51-31-01.SDR WRLA2007119Skin · crackedDURING C CHECK INSPECTION FOUND CRACK IN RIGHT HAND NR 3 AIR CONDITION COMPARTMENT DOOR OUTER UPPER SKIN L=4". REF EGAT NRC U05001. REPAIRED RIGHT NR 3 AIR CONDITION COMPARTMENT DOOR OUTER UPPER SKIN PER MD-11 SRM VOL 1 52-10-00 FIG 1 REV 40.SDR WRLA2007118Cable · brokenRIGHT MAIN GEAR SHOWED UNLOCKED AFTER TAKEOFF. BOTH INDICATOR BY GEAR HANDLE AND CONFIG PAGE WERE RED. CYCLED GEAR, OK NEXT TIME. FOUND RIGHT GEAR FOLLOW UP CABLE BROKEN AND LOWER GEAR DOOR DAMAGED. PER MX FERRY PERMIT ALL 4 GEAR PINS INSTALLED AND SAFETIESDR WRLA2007115Rib · crackedDURING 4C+12A CHECK, FOUND RT OUTBOARD FLAP NR 2 STOP FITTING CRACKED. REF EGAT NRC U05062. PERFORMED BOEING SERVICE BULLETIN MD-11-57-075, REPLACED DAMAGE RIB REV 00.SDR WRLA2007113Seat Track · corrodedDURING 4C+12A CHECK, FOUND RIGHT AFT FLOOR CURVED SEAT TRACK HAS CORROSION AT STA Y=2007 X=107.25. PER MD11 SRM VOL.I 53-70-00 FIG. 1 REV.40.SDR WRLA2007111Seat Track · crackedDURING 4C+12A CHECK, FOUND AFT CABIN LT FLOOR CURVED SEAT TRACK HAS CORROSION AT STA Y=1964, X=107.25. 10-23-07 REPAIRED THE AFT LT FLOOR CURVED SEAT TRACK PER MD-11 SRM VOL.I 53-70-00 FIG.1 REV.40.SDR WRLA2007112Tee Fitting · corrodedDURING 4C+12A CHECK, FOUND STA Y=2007 X=57 BULKHEAD TEE CORRODED. REPLACED DAMAGED TEE PER MD11 SRM VOL.II 51-35-01 REV.40. REF EGAT NRC U05041.SDR WRLA2007110Bracket · corrodedDURING 4C+12A CHECK, FOUND CABIN FLOOR PANEL SUPPORT BRACKET HAS CORROSION AT STA Y=1887 & X=-68. REPLACED WITH NEW PARTS PER MD-11 SRM 51-35-01 VOL.2 REV.40SDR WRLA2007106Skin · corrodedDURING 4C+12A CHECK, SEVERAL CORROSION AREAS WERE FOUND ON CENTER WING TANK UPPER SKIN AT XCW=-110 TO XCW=-106 BETWEEN S-15 TO S-22 AND STA XCW=107 BETWEEN S-18 TO S-15. 10-29-07 REPAIRED PER EGAT ENGINEERING INSTRUCTION W2007A57B-638 REV.00.
Back to Pratt & Whitney PW4462