Pratt & Whitney PW4158
Service difficulty reports · 689
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 = '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.
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
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 IPXA10162611Floorboard · delaminatedINSPECTION TYPE:5YRF, MAIN CABIN FLOOR PANEL 241VK IS DELAMINATED AT CORNER. FABRICATED MAIN CABIN FLOORBOARD 241VK IAW EO APPENDIX B.SDR IPXA10162627Floorboard · brokenINSPECTION TYPE:5YRF, MAIN CABIN FLOORBOARD NR261DM IS BROKEN AT AFT SECTION OF PANEL FABRICATED MAIN CABIN FLOORBOARD NR261DM IAW EO APPENDIX B.SDR IPXA10162741Floorboard · puncturedINSP TYPE:5YR, MAIN CABIN FLOORBOARD NR 241CM IS PUNCTURED. FABRICATED MAIN CABIN FLOORBOARD NR 241CM IAW EO A300-5320-16407-E, APPENDIX B.SDR IPXA10162609Floorboard · misrepairedINSPECTION TYPE:5YR, REPAIR VALIDATION SURVEY,REPAIR OF BULK CARGO FLOOR PANEL NR161GF. FABRICATED BULK CARGO FLOORBOARD NR161GF IAW EO A300-5320-16407-E, APPENDIX D.SDR IPXA10162610Floorboard · misrepairedINSPECTION TYPE:5YRF, REPAIR VALIDATION SURVEY, REPAIR OF BULK CARGO FLOORBOARD NR161HF. FABRICATED BULK CARGO FLOORBOARD NR161HF IAW EO APPENDIX D.SDR IPXA10162612Floorboard · damagedINSPECTION TYPE:5YRF, REPAIR VALIDATION SURVEY, REPAIR OF BULK PIT FLOORBOARD NR161JF HAS DAMAGE. FABRICATED BULK CARGO FLOORBOARD NR161JF IAW EO, APPENDIX D.SDR FDEA201009043273Skin · gougedLT WING OTBD FLAP INBD L/E GOUGED APPROX 0.500 IN LENGTH X 0.250IN WIDTH BLENDED AREA ON LT OTBD FLAP INBD L/E REF SRM 51-73-00 NDT FOUND NO CRACK REF NTM 51-10-08 BEFORE BLEND 0.053 MAT LOSS 0.017 IN MAT REMAINING 0.036 IN OUT OF LIMITS REF SRM 57-50-00 REMSDR IPXA10162396Floorboard · delaminatedINSPECTION TYPE:10YR, MAIN CARGO COMPARTMENT FLOORBOARD NR 241TK IS DELAMINATED AT FWD LOWER AREA. ACCOMPLISHED REPAIR IAW EO A300-5320-38221-B, PARA 6A.SDR IPXA10162400Floorboard · puncturedINSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR252XG HAS A PUNCTURE ACOMPLISHED REPAIR ON MAIN CARGO FLOORBOARD NR252XG IAW EO A300-5320-38221-B PARA 6A.SDR IPXA10162417Floorboard · crackedINSPECTION TYPE:10YR, MAIN CARGO FLOORBOARD NR 242ZF HAS A CRACK ACCOMPLISHED REPAIR ON MAIN CARGO FLOORBOARD NR 242ZF IAW EO A300-5320-38221-B PARA 6A.SDR IPXA10162436Floor Panel · puncturedINSPECTION TYPE:10YR, MAIN CARGO COMPT FLOOR PANEL 252VF IS PUNCTURED. REPAIRED MAIN CARGO COMPT FLOOR PANEL 252VF IAW EO A300-5320-38221-B.SDR IPXA10162700Skin · gougedINSPECTION TYPE:10YR LEFT WING CENTER FLAP UPPER SURFACE PREVIOUS REPAIR IS GOUGED. ACCOMPLISHED REPAIR IAW EO A300-5750-39715-A, PARA 6A.SDR IPXA10162315Wire · brokenNORMAL APPROACH, LANDING AND TOUCHDOWN DURING ROLLOUT BETWEEN 60 TO 45 KTS NOSE WHEEL STEERING BECAME INCREASINGLY DIFFICULT TO CONTROL. FOUND BROKEN WIRE AT PIN A OF CONNECTOR 3GC A, REF AWM 32-51-01. REPINNED 3 GCA CONNECTOR IAW ESPM 20-48-53, PROCEDURESSDR IPXA10162287Skin · dentedRT INBD FLAP DENTED WITH GOUGE. REPAIRED IAW EO A300-5750-35971-C.SDR FDEA201008203058Skin · corrodedLT WING BOTTOM SKIN LOWER SURFACE HAS CORROSION BETWEEN THE CTR SPAR AND THE REAR SPAR IN NUMEROUS SPOPTS JUST INBD OF THE NR1 PYLON. RIB 7-8. REMOVED SEAL, AFT LOWER FAIRING SECTION, AFT PYLON SECTION AND 3 EA. ATTACH BRACKETS PER SRM 51-40-21, PARA'S 5SDR IPXA10162068Floor Panel · crackedINSPECTION TYPE:4C REPAIR VALIDATION SURVEY, FWD CARGO PIT FLOOR PANEL 252XJ REQUIRES RE REPLACEMENT. FABRICATED NEW FWD CARGO PIT FLOOR PANEL 252XJ IAW EO A300-5320-16407-D, APPENDIX C.SDR IPXA10162069Floor Panel · crackedINSPECTION TYPE:4C, REPAIR VALIDATION SURVEY, FWD CARGO PIT FLOOR PANEL 242HN REQUIRES REPLACEMENT. FABRICATED NEW FWD CARGO PIT FLOOR PANEL 242HN IAW EO A300-5320-16407-D APPENDIX C.SDR IPXA10162198Floor Panel · puncturedINSPECTION TYPE:4C, REPAIR VALIDATION, MAIN CARGO DECK FLOOR PANEL, 242DF REQUIRES REPLACEMENT. FABRICATED NEW MAIN CARGO FLOOR PANEL 242DF IAW EO A300-5320-16407-D, APPENDIX B.SDR FDEA201008102910Skin · crackedRT WING LOWER SKIN PANEL FASTENER HOLE CRACKED. COMPLIED WITH EA 6-5710-136685.SDR FDEA201008102905Rib · crackedINBD FLAP LT WING - RIB 25A FOUND CRACKED. REPLACED AS PER EA 6-5750-141552 AND SB A300-57-6098.SDR FDEA201008102903Rib · crackedFLAP INBD RT WING - RIB 25A FOUND CRACKED. REPLACED IAW EA 6-5750-141552.SDR FDEA201008062856Sill · crackedAFT COMPARTMENT - SILL BEAM AT AFT COMPARTMENT DOOR WITH CRACK BTW FR60/61. SILL-BEAM WAS REPAIRED AS PER EA 6-5310-141556.SDR IPXA10162065Adapter · brokenINSPECTION TYPE:5 YR, MAIN CABIN SEAT TRACKS AFTER CLEANING FOUND ADAPTER CLS ONE SIDE BROKEN AT FR20 AND RBL 75.5 REMOVED, FABRICATED, AND INSTALLED CLS ADAPTER IAW STA-SA EA 300-5310-01-A2612 I/R AND EO A300-5310-39266-A.SDR FDEA201008032788Fitting · crackedRT WING JACK PAD FITTING IS CRACKED. REMOVED FITTING SRM 51-40-21, PARA 5, PG 7. MACHINED NEW JACK PAD IAW DWG A57240935, ISSUE "C". DIMENSION CHECK ON JACK PAD WITHIN LIMITS. FINAL HOLE SIZES WILL BE REAMED TO SIZE PRIOR TO INSTALLATION ON ACFT IAW DWG A5SDR FDEA201008022784Support · crackedNR1 PYLON LT FWD L/E NACELLE FAIRING STRUCTURE IS CRACKED AT A FASTENER. R & R CRACKED A5461221600040 SUPPORT WITH A NEW A5461221600040 SUPPORT, PO 688444.2 IAW SRM 51-40-21, PG 7.SDR FDEA201008022785Support · crackedNR 2 PYLON RT FWD L/E NACELLE FAIRING STRUCTURE IS CRACKED AT A FASTENER. R & R CRACKED A5461221600040 SUPPORT WITH A NEW A5461221600040 SUPPORT, PO 688444.2 IAW SRM 51-40-21, PG 7.SDR IPXA10161535Skin · gougedINSPECTION TYPE:4C, REPAIR SURVEY SEQUENCE NR 136-W4-01 EXISTING REPAIR DOUBLER GOUGED ON RT WING CTR FLAP UPPER SURFACE. ACCOMPLISHED REPAIR IAW SRM 57-50-00 PARA 4E, FIG 205.SDR IPXA10161499Floorboard · crackedINSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 241LT CRACKED. REPAIRED MAIN CABIN FLOORBOARD 241LT IAW EO A300-5320-38221-B.SDR IPXA0161381Actuator · leakingENROUTE AT FL320, BLUE SYS PRESSURE AND QTY WENT TO ZERO. RAN ECAM AND LANDED. ON FINAL, NEEDED CONSIDERABLE LT/AILERON TO MAINTAIN WINGS LEVEL. NR7 SPOILER APPEARED TO BE STUCK UP. FOUND NBR7 SPOILER ACTUATOR LEAKING EXTERNALLY. R & R ACTUATOR AND BLUE SYSDR FDEA201007283145Skin · dentedFUSELAGE - DEFORMITY (DENT) BETWEEN FR14A AND 15 BTW STGR 27-30LT. DENT WAS REPAIRED AND FOUND ACCEPTABLE IAW EA 6-5330-141557.SDR IPXA10161276Skin · damagedSKIN DAMAGED AT FR10 STR25L. REPAIRED IAW EO A300-5330-38818-A.SDR FDEA201007242656Stiffener · corrodedAVIONICS COMPARTMENT FUSELAGE STRUCTURE BELOW WASTE WATER CONNECTION BOX AT FRAME 12 STR 44L HAS CORROSION ON INTERNAL DOUBLE REMOVED LEVEL 1 CORROSION. REPLACED INTERNAL DOUBLE/STIFFENER AT WASTE WATER CONNECTION BOX IAW EA NR 6-5310-135232, DATED 7/23/10SDR FDEA201007232802Skin · damagedRT WING - AILERON T/E LOWER SURFACE BTW RIB13-RIB16 WITH EXISTING REPAIR FILLER. EXISTING REPAIR FILLER WAS REMOVED AND NEW REPAIR HAS BEEN PERFORMED IAW SRM 57-61-11, PB 201 & 51-77-12, FIG 222.SDR IPXA10161855Seat Track · corrodedINSPECTION TYPE:10YR, MAIN CABIN SEAT TRACK AT Y0, FR 80 IS CORRODED. ACCOMPLISHED REPAIR IAW SRM 53-10-16, FIG 201, PARA 4.SDR IPXA0162018Skin · gougedINSP TYPE:10YR RT INBD FLAP UPPER SKIN REPAIR DOUBLER IS GOUGED ACCOMPLISHED REPAIR IAW EO A300-5750-39205-A, PARA 6A.SDR IPXA10161857Skin · chafedINSPECTION TYPE:10YR, LT WING CTR FLAP UPPER SKIN CHAFED, APPROX 12" FWD OF RUB STRIP AND OTBD OF NR3 FLAP TRACK. ACCCOMPLISHED REPAIR IAW EO A300-5750-39128-A.SDR FDEA201007152535Attach Bracket · crackedMAIN CABIN UNDER FLOOR WEB ATTACH BRACKET CRACKED. FR.48,RBL70. REMOVED CRACKED WEB ATTACH BRACKET IAW SRM 51-40-21. DRILLED TO FIT, NEW WEB BRACKET IAW SRM 51-72-10, PG 2. INSTALLED NEW WEB ATACH BRACKET IAW SRM 51-72-10 PG 2 AND SRM51-40-21.SDR FDEA201007092451Floorboard · brokenMAIN CABIN CARGO COMPARTMENT FLOORBOARD NR 242 ZH IS BROKEN.SDR FDEA201007082418Stiffener · crackedLT WING T/E CAVITY UNDER PANEL 575 BB; UPPER PANEL SUPPORT IS CRACKED. RIB 6A-RIB 7. REMOVED CRACKED SUPPORT (STIFFENER) AND ADJACENT BRACKET IAW SRM 51-40-21, PARA 7. FABRICATED NEW STIFFENER IAW DWG A57241059 (-200). ALODINED AND PRIMED STIFFENER IAW SRSDR FDEA201007082405Landing Gear · malfunctionedGEAR WOULD NOT RETRACT ON T/O. SWITCHED TO SYS 1, NO JOY. COMPLIED WITH QRH. RETURNED FIELD. ALSO PITCH TRIM NR 2, ATS, NR 1 PRESSURE REGULATOR FAULTED AT SAME TIME. PILOT ATTEMPTED TO THROW THE HANDLE, WOULD NOT GO PAST HALFWAY. THEN GOT ECAM INDICATIONSDR IPXA10160998Floor Panel · crackedINSPECTION TYPE:5YR, MAIN DECK FLOOR PANEL 251PG IS CRACKED. REPAIRED MAIN DECK FLOOR PANEL 251PG IAW EO A300-5320-38221-B.SDR IPXA10161071Skin · chafedINSP TYPE:5YR, RT WING CTR FLAP OTBD L/E CHAFED. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-50-00 PARA, 4H FIG 208.SDR IPXA10160959Floorboard · crackedINSPECTION TYPE:10YR, CRACKED AND PUNCTURED FLOORBOARD NR 241LJ IN MAIN CABIN. FABRICATED MAIN CABIN FLOORBOARD NR 241LJ IAW EO A300-5320-16407-D, APPENDIX B.SDR IPXA0160670Warning Light · illuminatedEMERGENCY DECLARED - REVERSER LIGHT CAME ON AT FL240 ON NR 2 ENG. DEFERRED NR 2 ENG T/R IAW MEL 79-30-01 C/W DMP 78-30-01. M427865 ISSUED PLACARD INSTALLED. OPENSDR IPXA10160670Flex Drive · failedEMERGENCY DECLARED - REVERSER LIGHT CAME ON AT FL240 ON NR 2 ENG. DEFERRED NR 2 ENG T/R IAW MEL 79-30-01 C/W DMP 78-30-01. M427865 ISSUED PLACARD INSTALLED. REF MM 78-31-12-04, REPLACED 2 EA FLEX SHAFTS ON RT TR HALF FOR BINDING AND DAMAGE. OPS AND ADJ TEST GSDR FDEA201006162030Bearing · wornLT ELEVATOR NR 7 UPPER HINGE ARM BEARING WORN. REMOVED LT NR 7 ELEVATOR HINGE ARM PER AMM 55-16-45. REPLACED 3 EA BEARINGS & REWORKED HINGE ARM PER AMM 55-16-11-8 & E A 6-5520-136665 . MECHANICAL CONTROL & PITCH UNCOUPLING FUNCTIONAL TEST COMPLETED ON WORK SDR FDEA201006141997Support Angle · corrodedAFT CARGO COMPARTMENT UPPER ATTACH SUPPORT ANGLE FOR FWD BULKHEAD PANEL 151 BW HAS EXFOLIATED CORROSION. REMOVED BRACKET IAW SRM 51-40-21, PARA 6. LOCATED AND DRILLED NEW BRACKET PN A5341076720000 IAW SRM 51-40-10. INSTALLED BRACKET IAW SRM 51-40-21, PARA 7SDR FDEA201006142004Arm · wornVERT STABILIZER TO RUDDER ATTACH FITTING NR 3 HINGE; BEARINGS HAVE PLAY. (3EA.)DOTS: Q098, Q099, Q097 R & R BEARINGS IAW AMM 55-36-11-8; A300-600 SB A300-55- 6022 AND EA 6-5540-136664 "STABILIZERS - VERT.STAB. - RUDDER HINGE ARM BEARINGS".SDR FDEA201006142006Arm · wornRUDDER HINGE ARM; NR 7 BEARINGS 3 EA ARE WORN. DOTS: Q105; Q106; Q107 REMOVED 3 EA WORN BRG ASSEMBLIES AND INSTALLED 3 EA SERVICABLE BEARING ASSEMBLIES IAW EA 6-5540-136664 "STABILZERS - VERT. STAB.- RUDDER HINGE ARM BEARINGS".SDR IPXA10160397Module · inoperativeNR 2 ENG, NO FIRE DETECTION (A LOOP FAILURE, ACFT DEPARATED WITH MEL 26-12-01-1, NR 2 ENGINE FIRE DETECTION SYS B LOOP INOP. DEF NR 427111, CLEANED AND SECURE C/P'S DH3 AND DH4 AT R SIDE ENG CORE FIRE SENSING LOOPS. CLEANED AND SECURED C/P'S D4989P (1) D4953P
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