Pratt & Whitney PW4158

Service difficulty reports · 689

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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 = 'PW4158'
  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 IPXA2020103161900Deflector · chafedINSPECTION TYPE: A300 NR 2 ENGINE RT T/R-LOWER FWD LATCH ACCESS DOOR HAS CHAFED AREA ON INNER SURFACE. REMOVED & REPLACED DEFLECTOR ASSEMBLY, IAW SRM 51-40-21.Oct 31, 2020 · N138UP · Airbus A300F4622R · Engine Thrust ReverserSDR IPXA2020092460596Web · dentedINSPECTION TYPE: A300 BULK CARGO COMP PANEL WEB LT SIDE ABOVE FLOOR AT FR 69 HAS NUMEROUS DENTS. REMOVED & REPLACED, IAW SRM 51-40-21.Sep 24, 2020 · N130UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2020092560617Strip · damagedINSPECTION TYPE: A300 LT WING INBOARD FLAP UPPER SURFACE INBOARD CHAFE STRIP HAS DEEP GROOVE, AS MARKED. REMOVED & REPLACED RUB STRIP, IAW SRM 51-40-21.Sep 24, 2020 · N130UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2020091196037Support Angle · damagedINSPECTION TYPE: A 300 NR 2 ENG INBOARD TR LOWER FWD ANGLE SUPPORT FOR RUB STRIP HAS CHOTING MARKS. REMOVED & REPLACED REPAIR FILLER, IAW SRM 51-40-21.Sep 9, 2020 · N130UP · Airbus A300F4622R · Engine Thrust ReverserSDR IPXA2020091196038Support Angle · damagedINSPECTION TYPE: A 300 NR 2 OUTBOARD TR LOWER FWD ANGLE SUPPORT FOR RUB STRIP HAS CHOFING MARKS. REMOVED & REPLACED REPAIR FILLER, IAW SRM 51-40-21.Sep 9, 2020 · N130UP · Airbus A300F4622R · Engine Thrust ReverserSDR IPXA2020083199605Web · crackedINSPECTION TYPE:A 300 #1 ENGINE NOSE COLUMN AFT BULKHEAD CRACKED AT AMBIENT PRESSURE SENSOR LINE OUTLET ON RT SIDE 3' OCLOCK POSITION. FABRICATED & INSTALLED WEB IAW SRM 54-10-00.Aug 29, 2020 · N130UP · Airbus A300F4622R · Engine Air Intake SystemSDR IPXA2020083199606Web · crackedINSPECTION TYPE:A 300 #2 ENGINE NOSE INLET AFT SIDE AT 9 O'CLOCK HAS CRACK NET TO ELBOW FITTING. FABRICATED & INSTALLED NEW WEB IAW SRM 54-10-00.Aug 29, 2020 · N130UP · Airbus A300F4622R · Engine Air Intake SystemSDR IPXA2020080548631Angle · damagedNR 1 ENGINE INBD THRUST REVERSER COWL AFT UPPER FWD CUTOUT CORNER METAL SUPPORT DAMAGED. INSTALLED A NEW WEAR ANGLE IAW SRM 51-40-20.Aug 4, 2020 · N125UP · Airbus A300F4622R · Engine Thrust ReverserSDR IPXA2020080548633Plate · damagedNR 1 ENGINE AFT LOWER FAIRING 475AL LT UPPER EDGE FOUR ENLONGATED SCREW HOLES BETWEEN FWD TO AFT EDGES.REMOVE & REPLACE IAW SRM 51-40-21.Aug 4, 2020 · N125UP · Airbus A300F4622R · Nacelle/Pylon, Plate/SkinSDR IPXA2020072978292Valve · inoperativeNR 8 VALVE LIGHT ILLUMINATED IN NR 1 FUEL LEVER AT SHUT DOWN. REPLACED HP FUEL VALVE INHIBIT RELAY (37KC) IAW ESPM 20-46-50 OPS CHECK OF AMNUNCIATOR.Jul 26, 2020 · N133UP · Airbus A300F4622R · Engine Fuel Indicating SystemSDR IPXA2020082659529Mount · corrodedINSPECTION TYPE: SEG, NR 2 PYLON FWD ENGINE MOUNT AFT OTBD HOLE HAS PITTING CORROSION. CLEANED CORROSION IAW SRM 54-51-81- CONFIG 1.Jul 18, 2020 · N139UP · Airbus A300F4622R · Engine Mount SectionSDR IPXA2020082659528Mount · corrodedINSPECTION TYPE:SEG, NR 2 ENGINE FWD MOUNTING FITTING L/H AFT HOLE HAS PITTING CORROSION. REMOVED CORROSION IAW SRM 54-51-81, COFIG 1.Jul 17, 2020 · N139UP · Airbus A300F4622R · Engine Mount SectionSDR IPXA2020062256828Fitting · gougedINSPECTION TYPE:SEG MCD FR 47 SPLICE FITTING AT STR 24-26L SIDE HAS GOUGES. REPAIRED SPLICE FITTING GOUGES IAW EA 300-5710-27-A2458.Jun 21, 2020 · N137UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2020062256793Bulkhead · crackedINSPECTION TYPE:SEG RT WW BULKHEAD PANEL HAS SEAL FLANGE EXFOLIATED AND CRACKED. REMOVED AND REPLACED PART IAW SRM 51-40-21.Jun 20, 2020 · N137UP · Airbus A300F4622R · Fuselage Main, BulkheadSDR IPXA2020062256801Bushing · missingINSPECTION TYPE:SEG RT WW BULKHEAD PANEL (1) BUSHING MISSING AT HINGE. REMOVED & REPLACED HINGE FITTING IAW SRM 51-40-21.Jun 20, 2020 · N137UP · Airbus A300F4622R · Fuselage Main, BulkheadSDR IPXA2020062256803Longeron · wornINSPECTION TYPE:SEG NR 2 PYLON FAIRING RT UPPER CENTER LONGERON HAS WORN HOLES. REMOVED & REPLACED IAW SRM 51-40-21.Jun 20, 2020 · N137UP · Airbus A300F4622R · Nacelle/Pylon, Longeron/StringerSDR IPXA2020062256804Thrust Reverser · damagedINSPECTION TYPE:SEG OB TR AFT UPPER CORNER DAMAGED. REPAIR PER EO A300-7830-50286-C.Jun 20, 2020 · N137UP · Airbus A300F4622R · Engine Thrust ReverserSDR IPXA2020062256805Thrust Reverser · damagedINSPECTION TYPE:SEG OB TR AFT UPPER CORNER DAMAGED. REPAIRED PER EO A300-7830-50286-C.Jun 20, 2020 · N137UP · Airbus A300F4622R · Engine Thrust ReverserSDR IPXA2020061556481Bulkhead · crackedINSPECTION TYPE:A300 NR 2 ENGINE INLET AFT BULKHEAD HAS A CRACK ON LT SIDE NEAR SENSE LINE AT ABOUT 9 O'CLOCK POSITION. REPAIR WEB IAW SRM 54-10-00 REPAIR NR 14.Jun 12, 2020 · N124UP · Airbus A300F4622R · Engine Cowling SystemSDR FDEA2020060541126Unknown · malfunctionedUNCOMMANDED THRUST ON NR 1 ENGINE PDIS 724 73-20 6735 04JUN20 MEM. WHILE AT CRUISE FL340 WITH MANUAL THROTTLES DUE TO ATS SYSTEM MEL'D. WHEN ADJUSTING POWER NOTICED NR 1 ENGINE WAS SLOWLY INCREASING POWER WHILE PULLING NR 1 THROTTLE BACK, EPR POINTER REDUCEJun 4, 2020 · N724FD · Airbus A300B4622R · Fuel Controlling SystemSDR FDEA202006041126Engine · failedWHILE AT CRUISE FL340 WITH MANUAL THROTTLES DUE TO ATS SYSTEM MEL'D WHEN ADJUSTING POWER NOTICED #1 ENGINE WAS SLOWLY INCREASING POWER WHILE PULLING #1 THROTTLE BACK. EPR POINTER REDUCE BUT ALL ENGINE SETTINGS WERE INCREASING.WHILE TROUGLESHOOTING ENGINE Jun 4, 2020 · N724FD · Airbus A300B4622R · Engine (Turbine/Turboprop)SDR IPXA2020052955914Cowling · gougedINSPECTION TYPE, SEG NR 1 ENG IB TR COWL OUTER EDGE JUST FWD OF TR SLEEVE GOUGED IN 3 PLACES. FABRICATED REPAIR FILLER ON TR T20 1495348 AND INSTALLED FILLER IAW SRM 51-40-21.May 29, 2020 · N171UP · Airbus A300F4622R · Engine Thrust ReverserSDR IPXA2020052215604Bracket · wornINSPECTION TYPE:SEG#1 ENG O/B T/R COWL LOWER BRACKET NEXT TO TR PUMP PORT BENT/CORNER WORNREMOVED AND REPLACED BRACKET IAW SRM 51-40-21May 21, 2020 · N171UP · Airbus A300F4622R · Engine Thrust ReverserSDR IPXA2020061986730Web · crackedNR 1 ENGINE NOSE COWL AFT 49306-A BACK AT NINE O'CLOCK POSITION CRACKED AROUND STATIC TUBE. NEW WEB AND SPLICE PLATE LOWER ANGLE IAW SRM 51-40-21 AND PW SRM 54-10-00 FIG 201 REPAIR 14May 12, 2020 · N137UP · Airbus A300F4622R · Engine Mount SectionSDR IPXA2020042454584Rub Strip · wornINSPECTION TYPE:C#2 OUTBRD T/R UPPER CHORD / LOWER WEB ANGLE AMALL RUB STRIP WORN THROUGHACCOMPLISHED SREO A300-7830-16238-G A300 THRUST REVERSER UPPER LONGERON AND PYLON SPRING SEAL CHAFE DAMAGE FASTERER AND PERMANENT REPAIRS SREOMar 17, 2020 · N120UP · Airbus A300F4622R · Engine Thrust ReverserSDR IPXA2020042754609Rub Strip · wornINSPECTION TYPE:A300#2 INBD TR UPPER CHORD LOWER WEB ANGLE SMALL RUB STRIP WORNREPAIRED IAW SREO A300-7830-16238-G OF #2 INBD TRMar 17, 2020 · N120UP · Airbus A300F4622R · Engine Thrust ReverserSDR IPXA2020010650681Bleed Valve · failedAIR TURNBACK DUE TO FAILURE OF THE RIGHT ENGINE BLEED VALVE. SHORLTY AFTER LEVELING FL 300. NR 2 BLEED VALVE FAULT ECAM DISPLAYED, WITH LOSS OF CABIN PRESSURIZATION, ENGINE & WING ANTI ICE HAS BEEN ON SINCE 14,000 FT DURING CLIMB AND REMAINED ON. PRESSUREJan 4, 2020 · N147UP · Airbus A300F4622R · Compressor Bleed ValveSDR IPXA2019111328906Thrust Reverser · inoperativeINSPECTION TYPE:N/AAFTER LANDING #2 THRUST REVERSER WOULD NOT STOWREMOVED AND REPLACED RT ENG I/B REVERSER PER AMM 71-13-03-0401. OPS CK NORMALNov 11, 2019 · N146UP · Airbus A300F4622R · Engine Thrust ReverserSDR IPXA2019103024456Bulkhead · crackedINSPECTION TYPE:SEG#2 ENG NOSE HAS CRACK ON AFT BULKHEAD OTBD SIDEREPAIRED IAW P&W SRM 54-10-00-00- REPAIR 14Oct 1, 2019 · N167UP · Airbus A300F4622R · Nacelle/Pylon, Bulkhead/FirewallSDR IPXA2019090846461Sensor · faultyINSPECTION TYPE:N/A ATB - CLIMBING THROUGH 16,000 ENG ADV ON RIGHT ECAM #2 ENG OIL TEMP WAS INDICATING BETWEEN 162 DEG AND 176 DEG THE INDICATION WAS ERRATIC, PULLED POWER BACK ON #2 ENGINE TO KEEP OIL TEMP WITHIN LIMITS. IT SEEMED TO HELP KEEP THE OIL TEMP LOSep 7, 2019 · N163UP · Airbus A300F4622R · Engine Oil TemperatureSDR IPXA2019062443664Bulkhead Web · crackedNR 2 ENG INLET COWL AFT BULKHEAD WEB CRACKED 9 O'CLOCK POSITION AT SENSE LINE FITTINGREPAIR PER PW SRM 54-10-00 REPAIR #14Jun 12, 2019 · N160UP · Airbus A300F4622R · Turbine Engine Air Inlet SectionSDR IPXA2019062443665Bulkhead Web · crackedNR 2 ENG INLET COWL AFT BULKHEAD WEB CRACKED 3 O'CLOCK POSITION AT SENSE LINE FITTINGREPAIR PER PW SRM 54-10-00 REPAIR #14Jun 12, 2019 · N160UP · Airbus A300F4622R · Turbine Engine Air Inlet SectionSDR FDEA201906111269Oil System · leakingSHORTLY AFTER LEVEL OFF AT FL320, NOTICED ENG #2 OIL QTY SHOWING 7 QTS, WHILE ENG #1 HAD 15 QTS. WITHIN 10 MINUTES, OIL QTY CONTINUED TO DECREASE TO ZERO. DURING THAT TIME OIL PRESSURE WAS NORMAL AT 195 PSI AND OIL TEMP 140 DEGREES. RETARDED THROTTLE #2 TJun 11, 2019 · N722FD · Airbus A300B4622R · Turbine Engine Oil SystemSDR IPXA2019061843447Guide · bentNR 1 ENGINE OUTBOARD TR UPPER LE ATTACH BRACKET FOR ACTUATOR LINE IS BENT. REMOVED AND REPLACED GUIDE ASSEMBLY IAW CMM 78-32-34Jun 10, 2019 · N133UP · Airbus A300F4622R · Engine Thrust ReverserSDR IPXA2019061943505Attach Bracket · crackedINSPECTION TYPE:124C, NR 2 ENGINE OUTBOARD TR LOWER LE ATTACH BRACKET IS CRACKED AT FASTENER HOLE DOT AND STREAMER ATTACHEDREMOVED AND REPLACED CLIP IAW P&W SRM 54-04-01, P&W 54-04-06, AND P&W CMM 78-32-34Jun 10, 2019 · N133UP · Airbus A300F4622R · Engine Thrust ReverserSDR IPXA2019061843446Retainer · brokenNR 1 ENGINE O/B T/R CIRCUMFERENTIAL STRAP UPPER GUIDE AT 1 O`CLOCK POSITION IS BROKEN. REMOVED AND REPLACED RETAINER PER SRM 54-04-01.Jun 9, 2019 · N133UP · Airbus A300F4622R · Engine Thrust ReverserSDR IPXA2019061843453Structure · gougedNR 2 T/R I/B SIDE L/E BOTTOM PREVIOUS REPAIR GOUGED JUST FWD OF FWD BIFURCATION LATCHREPAIRED PER PW SRM 54-05-02Jun 9, 2019 · N133UP · Airbus A300F4622R · Engine Thrust ReverserSDR IPXA2019061943482Rub Strip · wornINSPECTION TYPE:124C, NR 2 T/B I/B SIDE UPPER INNER METAL RUB SEAL WORN ITS IN 2 PIECES, SMALL FWD SECTION AND LONGER SECTIONREMOVED AND REPLACED IAW UPS EO# A300-7830-1638 P&W SRM 54-04-01Jun 9, 2019 · N133UP · Airbus A300F4622R · Engine Thrust ReverserSDR IPXA2019042341403Line · crackedINSPECTION TYPE:12YRLH ENG NOSE COWL SENSE LINE AT OUTBOARD AFT SECTION HAS POSSIBLE CRACK ON FITTING SUPPORT STRUCTUREPERFORMED HFEC CONFIRMING CRACK TERMINATION AND REPAIRED IAW PW SRM 54-10-00Apr 9, 2019 · N163UP · Airbus A300F4622R · Turbine Engine Air Inlet SectionSDR IPXA2019020438663Blocker Door · damaged#2 ENG INBOUND #3 BLOCKER DOOR DAMAGED.REPLACED BLOCKER DOOR REF AMM 78-32-13-0401.OPS CHECK OK.Feb 4, 2019 · N140UP · Airbus A300F4622R · Engine Thrust ReverserSDR IPXA2018121096720Eec · inoperativeDURING DESCENT, AND LEVELING AT 5000 FT, 250 KTS. FIRST ENG ANO LOW OIL PRESSURE WARNING CAME ON ECAM AND RED WARNING LIGHT. RECHECKED, ECAM THEN ENG, 1 FAIL CAME ON. ENGINE ONE WAS AT IDLE AND WOULD NOT RESPOND. STARTED ENGINE FAIL ECAM PROCEEDURE. ACCOMPDec 9, 2018 · N164UP · Airbus A300F4622R · Fuel Controlling SystemSDR IPXA2018072432044Engine · fireNR 1 ENG LOWER SECTION NEAR IDG DAMAGED BY ENG FIRE. REMOVED AND REPLACED NR 1 ENG REF TC 710000-P-1-1-400.Jul 24, 2018 · N134UP · Airbus A300F4622R · Engine (Turbine/Turboprop)SDR IPXA2018072031904Engine · fireENGINE 1 FIRE, FIRE EXTINGUISHERS ACTIVATED, ENGINE WAS SHUT DOWN AND AIR TURN BACK (ATB) ACCOMPLISHED UNEVENTFUL.Jul 19, 2018 · N134UP · Airbus A300F4622R · Engine (Turbine/Turboprop)SDR IPXA2018060630367Spring · brokenNUMBER 2 PYLON AFT BOARD SPRING SEAL WAS BROKEN. REMOVED AND REPLACED THE SPRING SEAL IAW SRM 54-56-10, AND SRM 51-40-21.Jun 6, 2018 · N121UP · Airbus A300F4622R · Engine Thrust ReverserSDR FDEA201804211089Fmu · malfunctionedDURING DESCENT THROUGH FL 250, THE NR 2 ENGINE INDICATIONS ROLLED BACK AND ECAM INDICATED THE NR 2 ENGINE FAILED. NOTHING WAS NOTED AS THE CAUSE FOR THIS, GOOD OIL QUANTITY, AND GOOD FUEL INDICATIONS. AFTER GOING TO CONTINUOUS IGNITION RELIGHT, THE ENGINE Apr 21, 2018 · N728FD · Airbus A300B4622R · Fuel Controlling SystemSDR IPXA2018010825233Engine · smokeEXCESSIVE SMOKE FROM THE NR 1 ENGINE AFTER SHUT DOWN. SERVICED WITH 2 QTS OF OIL IAW MM 71-00-00-0501. TESTED, NO DEFECTS NOTED.Jan 6, 2018 · N172UP · Airbus A300F4622R · Engine (Turbine/Turboprop)SDR FDEA201707051856Eec · failedADVANCED POWER ON BOTH THROTTLES TO BEGIN TAXI AFTER ENGINE START, NR 1 ENGINE WOULD NOT PRODUCE ANY THRUST. CYCLED THE NR 1 THROTTLE FULL FORWARD AND AFT WITH NO THRUST RESPONSE. R & R THE NR 1 ENGINE EEC IAW AMM 73-21-01-04. FADEC ADJUSTMENT TEST ACCOMPLIJul 5, 2017 · N729FD · Airbus A300B4622R · Fuel Controlling SystemSDR IPXA2017040715909Bleed Valve · failedENROUTE, AT FL 31000, THE NR 2 PACK FAULTED. ECAM COMPLETED. UNABLE TO RESTORE THE NR 2 PACK. EMERGENCY DECLARED. LANDED. THE NR 2 PACK FAULTED DUE TO THE NR 2 BLEED VALVE FAILED. THE NR 2 PACK OPS CHECKED GOOD IAW MM 21-11-00.Apr 5, 2017 · N133UP · Airbus A300F4622R · Compressor Bleed ValveSDR IPXA2017010512404Engine · leakingLOST MOST OF THE OIL IN THE NR 1 ENGINE IN FLIGHT. SHUT IT DOWN IAW ECAM CHECKLIST DUE TO LOW OIL PRESSURE. LANDED AT JAX REMOVED AND REPLACED ENGINE.Jan 4, 2017 · N131UP · Airbus A300F4622R · Engine (Turbine/Turboprop)SDR FDEA201607012221Controller · malfunctionedDURING CRUISE AT FL 300, THE NR 1 BLEED FAULTED. THE NR 2 BLEED ALREADY MEL'D. FOLLOW THE QRH PROCEDURES AND DIVERTED. PERFORMED BITE CHECK OF NR 1 PNUEMATIC CONTROLLER. DISPLAYED C CONTROLLER FAULT IAW TSM 41HA CONTROLLER AT FAULT. REPLACED NR 1 PNUEMATIJul 1, 2016 · N728FD · Airbus A300B4622R · Pneumatic Distribution System
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