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 IPXA12174800Floorboard · crackedINSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 222AG LOWER SKIN IS CRACKED ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.SDR IPXA12174801Floorboard · delaminatedINSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 221FG HAS LOWER SKIN TORN AND DELAMINATED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.SDR IPXA12174804Floorboard · damagedINSPECTION TYPE:4C, MAIN CABIN FLOORBOARD 231PH HAS LOWER SKIN TORN. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.SDR IPXA12174805Floorboard · puncturedINSPECTION TYPE:SV, MAIN CABIN FLOORBOARD 231LH HAS LOWER SKIN PUNCTURED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD PER IPXA EO A300-5320-42721-B PARA 6ASDR IPXA12174806Floorboard · delaminatedINSPECTION TYPE:SV, MAIN CABIN FLOORBOARD 231MJ HAS LOWER SKIN DELAMINATED AND INSERTS CORRODED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-B.SDR IPXA12174807Floorboard · puncturedINSPECTION TYPE:SV, MAIN CABIN FLOORBOARD 231KJ HAS UPPER SKIN CRACKED AND LOWER SKIN PUNCTURED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.SDR IPXA12174825Power Supply · inoperativeEMERGENCY EXIT LT WILL NOT ILLUMINATE. R & R EMERGENCY EXIT POWER SUPPLY REF 33-51-14-0101. TESTED OK.SDR IPXA12174829Connector · disconnectedENTRY DOOR SLIDE LIGHT INDICATION INOPERATIVE, BUZZER OPS NORMAL. RESET AND RECONNECTED CONNECTOR 70WN-A ON ASPSU, W/R/T ASA 52-73-00 TESTED SYS W/R/T MM 52-73-11-04 PARA 2.I. NO FAULTS NOTED.SDR FDEA201208072870Floor Support · corrodedMAIN DECK FR11-14 Y1456 FLOOR SUPPORT CORRODED. REPAIRED IAW EA 6-5310-162732.SDR FDEA201208072869Crossbeam · corrodedMAIN DECK FR50 -Y1959 TO -Y2462 CROSSBEAM CORRODED. REMOVED ADAPTOR PER SRM 51-40-21. FABRICATED REPAIR PARTS PER DWG:Y53829705. INSTALLED REPAIR ADAPTOR CROSSBEAM PER SRM 51-40-21 4. RESTORED FINISH PER SRM 51-75-10.SDR IPXA12174790Floorboard · chippedINSPECTION TYPE: 4C, MAIN CABIN FLOORBOARD 221VF IS CHIPPED ON ITS SIDE. FABRICATED MAIN CABIN FLOORBOARD IAW EO APPENDIX B.SDR IPXA12174802Seat Track · corrodedINSPECTION TYPE: 4C, MAIN CABIN SEAT TRACK AT FR 79, STA Y794.3 CORRODED ACCOMPLISHED REPAIR ON MAIN CABIN SEAT TRACK AT FR 79, STA Y794 IAW SRM 53-10-16, PB 201, FIG 201.SDR IPXA12174809Seat Track · corrodedINSPECTION TYPE: 4C, SEAT TRACK CORRODED AT FR79, Y1131.1. REPAIRED SEAT TRACK AT FR79, Y1131.1 IAW SRM 53-10-16, FIG 201, PARA 4, REV 21. REF: RCD, CONTROL NR 554793.SDR IPXA12574775Frame · dentedINSPECTION TYPE:C, FWD CARGO COMPARTMENT BS 760, STR 23R, FRAME DENTED ON INBD FLANGE. CUTOUT DENT FABRICATED AND INSTALLED DOUBLER IAW SRM 53-00-07-2R 5, DETAIL III.SDR IPXA12174791Skin · chafedINSPECTION TYPE: 4C, LT INBD FLAP UPPER SKIN IS CHAFED AT OTBD SIDE. ACCOMPLISHED REPAIR ON LT INBD FLAP UPPER SKIN IAW SRM 57-50-00, FIG 205, PARA 4E.SDR IPXA12174803Seat Track · corrodedINSPECTION TYPE:4C, MAIN CABIN FLOOR SEAT TRACK AT FR 79, STA Y0 IS CORRODED. ACCOMPLISHED REPAIR ON MAIN CABIN SEAT TRACK AT FR 79, STA Y0 IAW SRM 53-10-16, FIG 201.SDR IPXA2174580Wire · disconnectedSUPERNUMERY AREA EMERGENCY LIGHTING FWD WALL MOUNTED EXIT LIGHT INOPERATIVE WHEN DOING EMERGENCY LIGHTS TEST, FIN 91WL. FOUND WIRES DISCONNECTED, RECONNECTED & OPS CHECKED GOOD IAW AMM 33-51-17-0401.SDR IPXA12174708Skin · chafedINSPECTION TYPE:4C, RT INBD FLAP UPPER SKIN MID SECTION IS CHAFED IN THREE PLACES. ACCOMPLISHED REPAIR ON RT INBD FLAP UPPER SKIN BETWEEN RIB 11 AND 14 STR 2.1 -2.4 IAW EO A300-5750-48074-A.SDR IPXA2174415Floorboard · puncturedINSPECTION TYPE: 1C, MAIN CABIN FLOORBOARD 231KG LOWER SKIN IS PUNCTURED AND UPPER SKIN IS PUNCTURED. ACCOMPLISHED REPAIR ON CABIN FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.SDR FDEA201207112536Spar · damagedCENTER WING BOX REAR SPAR & BOTTOM PANEL DAMAGED, BUSHING REPAIRED IAW EA 6-5710-161497.SDR IPXA12174552Skin · chafedINSPECTION TYPE:1C, LT WING OTBD FLAP BULLNOSE L/E LOWER SURFACE HAS CHAFE MARK. ACCOMPLISHED REPAIR ON LT WING OTBD FLAP BULLNOSE SKIN L/E LOWER SURFACE IAW SRM 57-50-00, PB 201, PARA 4H, FIG 208.SDR IPXA12174553Skin · dentedINSPECTION TYPE:1C, RT WING INBD FLAP BULLNOSE SKIN HAS DENTS, GOUGES AND RUB STRIPS HAVE DENTS. ACCOMPLISHED REPAIR ON RT WING INBD FLAP BULLNOSE IAW SRM 57-50-00 PB 201, PARA 4H, FIG 208.SDR FDEA201204241572Sensor · malfunctionedNR 2 ENGINE SHUTDOWN IN FLIGHT, DUE TO HIGH OIL TEMPERATURE AT 180 DEGREES. OIL DELTA T WAS 0 DEGREE CENTIGRADE 31 MIN WINDMILLING. DFDR DATA CONFIRMED THE NR 2 ENGINE OIL TEMPERATURE INDICATION SYS WAS ERRATIC BEFORE ENGINE SHUTDOWN. R & R NR 2 ENGINE TSDR IPXA1170677Sensor · inoperativeON APPROACH, TRIED TO EXTEND FLAPS TO 15. HANDLE WOULD NOT GO PAST SLATS EXTEND DETENT. DID A SLATS ONLY LANDING. NO ABNORMAL INDICATION ON ECAM. EMERGENCY DECLARED. R & R COMMAND SENSOR UNIT REF MM 27-51-17-04. SLATS AND FLAPS OPS CHECKED GOOD.SDR FDEA201109224070Floor Support · corrodedMAIN DECK FLOOR SUPPORT BETWEEN LONGITUTIONAL BEAM 3L AND 2L HAS 1.5 SQ IN CORROSION R & R "T" CAP ON FLOOR SUPPORT FROM FRAME 11 TO FRAME 12A IAW SRM 51-40-21, PARA 5, 6 & 7 AFTER CORROSION WAS FOUND TO BE OUT OF LIMITS WITH MATERIAL LOSS OF .009 WITH BEFORSDR FDEA201109093814Angle · crackedLT WING INBD L/E AREA INSIDE KRUEGER FLAP WELL, OTBD SIDE OF FLAP WELL BETWEEN RIB 1 & RIB 2, 1.50" CRACK ON FIXED L/E STRUCTURE. REMOVED 3 EA PROTECTIVE COVERING IAW SRM 51-40-21. REMOVED CRACKED REINFORCING ANGLE IAW SRM 51-40-21. LOCATED AND DRILLED NEW SDR FDEA201108313592Bulb · failedAFTER LEVEL OFF, GOT ECAM ADVISORY (NO OTHER ALERTS OR WARNINGS) OF NR2 ENG OIL TEMP ABOVE 177 DEG C SHUTDOWN NR 2 ENG ACCORDING TO QRH PROCEDURES DIVERTED. REMOVED AND REPLACED NEW OIL TEMP BULB PER MM 79-32-11-04-0. LEAK CHECKED AND SAFTEY WIRED AFTER CHECSDR FDEA201107212873Floor Panel · corrodedBULK CARGO FLOOR PANEL 161CF FOUND UNDER CORRODED. REMOVED PER AMM 53-10-35 REV 52.0. NEW FLOOR PANEL FABRICATED PER DRAWING SRZ 25-011 REV D. NEW FLOOR PANEL INSTALLED PER AMM 53-10-35 REV 52.0. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.SDR FDEA201106212352Stringer · corrodedFORWARD CARGO AT ABOUT FR 38.2 STRINGER 45L FOUND CORRODED. CARRIED OUT REPAIR AS PER SRM 53-10-14 FIG 201 REV 75. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.SDR IPXA1166693Sleeve · separatedUPON ARRIVAL, MX INSP DISCOVERED RT ENG OTBD THRUST REVERSER SLEEVE PARTIAL SEPARATION FROM ACFT. APPX 1 FT X 7 FT SECTION OF T/R SLEEVE MISSING. DEBRIEF FROM FLT CREW NOTED LANDING SDF RW 35L. TOWER AND CFR WAS NOTIFIED AND RWY INSP RECOVERED SEVERAL SMALLSDR FDEA201104281668Spar Cap · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON THE CENTER WING BOX CENTER SPAR, AT RIGHT HAND CUT-OUT DOUBLER RUNOUT LEFT SIDE LOWER HOLE FIRST LAYER AT 12 O' CLOCK POSITION LOOKING FORWARD. CRACKED AT CENTER WING BOX CENSDR FDEA201104231594Seat Track · corrodedMAIN DECK FWD UTILITY AREA, FLOOR SEAT TRACK ALONG Y 953 BETWEEN FRAME 16 AND FRAME 19 CORROSION FOUND ON CROWN. MAIN DECK FORWARD UTILITY AREA, FLOOR SEAT TRACK ALONG Y 953 BETWEEN FRAME 16 AND FRAME 19 REMOVED AND REPLACED AS PER SRM 51-40-21 REVISION 75.SDR FDEA201104051316Skin · misrepairedREPAIR DOUBLER FOUND AT FUSELAGE BELLY SKIN NEAR JACKPAD FRAME 87, STR 45. EVALUATED AND FOUND NOT INACCORDANCE WITH ANY REPAIR DATA. CARRIED OUT REPAIR AS PER SRM 53-10-12 FIGURE 225 REVISION 75. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112.SDR FDEA201103191083Structure · chafedRT WING KREUGER FLAP FOLDING NOSE OTBD EDGE, SURFACE HAS 1 IN CHAFED MARK. REPAIRED RT WING KREUGER FLAP IAW EA6-5750-145582 INSTRUCTIONS.SDR IPXA1165411Engine · noneEMERGENCY DECLARED. IMMEDIATELY AFTER ROTATION HEARD LOUD BANG & SMELLED SMOKE IN COCKPIT. ALL COCKPIT ENGINE INDICATIONS WERE NORMAL. OCCURRED DURING GEAR RETRACTION. EVIDENCE OF BIRDSTRIKE IN NR 1 ENG. ACCOMPLISHED ENG BIRD STRIKE INSP IAW AMM 05-51-19-00SDR FDEA201102180624Support · damagedAFT FUSELAGE COMPARTMENT - SUPPORT FRAME ON FRAME 86, STRINGER 33 FOUND DAMAGED. DAMAGED SUPPORT FRAME REMOVED AND REPLACED WITH NEW SUPPORT FRAME PER SRM 51-40-21 REV 74. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 111.SDR FDEA201102180626Panel · crackedHORIZONTAL STABILIZER - RT INBD L/E PANEL NR 341AB FOUND WITH 0.75 INCH CRACK ON MOST INBD FRAME (RIB) EDGE. REPAIR ACCOMPLISHED AS PER E.A. 6-5510-142456. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 111.SDR FDEA201102180628Skin · crackedLT WING FIXED T/E PANEL UPPER SURFACE AT APPROX STA 1270, FOUND CRACKED. REPAIRED AS PER SRM 57-51-12 FIGURE 210 REV 74. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 111.SDR IPXA1164807Thrust Reverser · intermittentATB - INTERMITTENT NR1 ENG T/R INDICATION. NO EMERGENCY DECLARED. DEFERRED NR1 T/R IAW MEL. M447243 ASSIGNED. (OPEN)SDR IPXA1164614Warning System · activatedDURING CLIMBOUT PASSING 16,500 FWD CARGO LITE WARNING, SLIGHT PRESSURIZATION DESCENT. LEVEL OFF AT 19,000 WITH WARNING DURING DESCENT TO SDF WARNING LIGHT CLEARED AT 10,000FT. DEFERRED IAW MEL M446301 ASSIGNED.(OPEN)SDR FDEA201102040473Engine · oil consumptionNR 1 ENGINE BURNED 1.5 QTS PER HOUR, THE FIRST 2.5 HRS. AIRCREW RECORDED ENGINE READINGS EACH 30 MINUTES IN FLIGHT. THE NR 2 ENG APPEARED NORMAL. MECHANIC SERVICED NR 1 ENGINE (3 QTS ADDED) TO FULL. PERFORMED GVI OF NR 1 ENGINE COWLING, DRAIN MAST AND TAISDR IPXA11164614Diode · inoperativeDURING CLIMBOUT PASSING 16,500 FWD CARGO LIGHT WARNING, SLIGHT PRESSURIZATION DESCENT. LEVEL OFF AT 19,000 WITH WARNING DURING DESCENT TO SDF WARNING LIGHT CLEARED AT 10,000FT. DEFERRED IAW MEL M446301 ASSIGNED. PERFORMED REPEAT ALERT H-148086 REPLACED 178VD SDR FDEA201102010447Selector Valve · failedGEAR FAILED TO RETRACT ON SYS 1. (SYS 2 UNDER MEL) ADJUSTED LT AND RT MLG 62GB, 63GB, 64GB, 65GB SENSOR GAPS REF AMM 32-00-00-4. R & R LANDING GEAR CONTROL HANDLE MODULE (2GA) IAW AMM 32-31-11-04 THROUGH STEP 2.C, STILL REQUIRES TEST (STEP 2.D). R & R LANSDR IPXA1164283Floorboard · delaminatedINSPECTION TYPE:10YR, MAIN CARGO COMPARTMENT FLOORBOARD 231HG IS DELAMINATED. FABRICATED MAIN CABIN FLOORBOARD NR 231HG IAW EO A300-5320-16407-E, APPENDIX B.SDR FDEA201101120128Computer · faultedPITCH FEEL NR 2 FAULTED TURNED IT OFF FOR APPROX (1) MINUTE RESET AND FAULT WENT AWAY. (2) MINUTES LATER IT FAULTED AGAIN IAW ECAM/QRH TURNED IT OFF AND COMPLIED W/QRH. FOUND FAULT LIGHT ON NR 2 COMPUTER FLC R & R IAW MM 27-23-26-4.SDR IPXA11164158Floor Panel · crackedINSPECTION TYPE:5YR, FLOOR PANEL 241LJ CRACKED AT FWD CORNER LOWER SURFACE. REPAIRED UPPER DECK FLOOR PANEL 241LJ IAW EO A300-5320-38221-B.SDR IPXA11164160Floor Panel · crackedINSPECTION TYPE:5YR, CABIN COMPT FLOOR PANEL 242TK UNDER SURFACE CRACKED. REPAIRED UPPER DECK FLOOR PANEL 242TK REF EO A300-5320-38221-B.SDR IPXA11164137Floor Panel · crackedINSPECTION TYPE:5YR, FLOOR PANEL 261JM IS CRACKED. REPAIRED FLOOR PANEL 261JM IAW EO 5320-38221-B, PARA 6 (1).SDR IPXA1164179Seat Track · corrodedINSPECTION TYPE:5YR, CABIN COMPT SEAT TRACK CORRODED AT Y953 BETWEEN FR61 AND FR62. REPAIRED UPPER DECK SEAT TRACK AT Y953 BETWEEN FR61 AND FR63 REF SRM 53-10-16, FIG 201.SDR IPXA11164166Floor Panel · delaminatedINSPECTION TYPE:5YR, FLOOR PANEL FWD CARGO SECTION 131RG, CORNER DELAMINATED. REPAIRED UPPER DECK FLOOR PANEL 131RG REF EO A300-5320-38221-B.
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