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 FDEA201209063236Cargo Track · corrodedMAIN DECK CARGO SEAT TRACK AT BS 1581, X=-8.5, FOUND WITH CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA.1571 TO STA..1691 , X= -8.5 AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 50 REPAIR CLASSIFIED MAJOR AS PER GMM 6- 2-100 REVISISDR FDEA201209063237Cargo Track · damagedMAIN DECK CARGO TRACK AT BS 997, X= 75 , FOUND CROWN CHIPPED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM BS 989 TO 1049 , X=75 AS PER SRM 53-00- 52 FIGURE 201 REPAIR 1 REVISION 50 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201209063238Rib · crackedRIGHT WING RIB NR 16 AT FIXED L/E AREA (INBD SIDE) FOUND CRACKED. RIB REMOVED AS PER SRM 51-31-01 REV. 50 AND REPLACED WITH NEW RIB 16 AS PER DWG ARB7565 REV. C REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201209063239Cargo Track · corrodedMAIN DECK CARGO TRACK AT BS 1689, X=-8.5 , FOUND WITH CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM BS 1571 TO 1691 , X= -8.5 AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 50 REFER TO SNRM N00262 FOR WORK DETAILS. REPAIR CLASSIFIED MAJORSDR IPXA12M75379Trunnion · crackedINSPECTION TYPE:3C, NLG TRUNNION FITTING CRACKED, LT SIDE NEAR TRUNNION PIN. REPAIRED NLG LT TRUNION FITTING IAW SRM 53-10-14, REPAIR 2, FIG 202. (MAJOR)SDR FDEA201209033211Switch · unsecureRT DOOR PRESSURE SENSING LIGHT INOPERATIVE. SECURED SWITCH BACK TO TEST LIGHT OPS CHECKS GOOD IAW AMM 25-61-04-4 .SDR FDEA201208253167Latch · inoperativeEMERGENCY O2 MASK DOOR WILL NOT STAY LATCHED IN LAVATORY. RESET LOCK AND RESECURED PANEL IAW SMP.SDR IPXA12M74830Warning Light · false activationEMERGENCY LIGHT SYS TEST DISPLAYS "BATTERY 1 LOW" PERFORMED FUNCTIONAL TEST OF EMERGENCY LIGHT SYSTEM, ALL TESTS PASSED IAW AMM 33-51-01. THIS CLEARS DMI M485777.SDR FDEA201207182602Actuator · inoperativeSHORTLY AFTER SETTING TAKEOFF PWR, NR 3 THRUST REVERSER CAME ON. ABORTED TAKEOFF & RETURNED TO RAMP. REMOVED AND REPLACED #3 ENGINE O/B UPPER FEEDBACK ACTUATOR AIW ATA/WRI 78-30/2865 AND ATA/WRI 78-30/2869. A/C OK FOR SERVICE. REMOVED AND REPLACED #3 ESDR IPXA2M74624Doubler · crackedINSPECTION TYPE: 4C, RT WING FIXED L/E COMPT BEADED DOUBLER CRACKED BETWEEN XORS 518-523. REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS625-629 IAW STA SA EA 011-5730-01-A4074 REV IR & EO MD11-5730-47975-A, FAA 8100-9.SDR IPXA2M74398Doubler · crackedINSPECTION TYPE: 4C, LEFT WING FIXED L/E BEADED DOUBLER CRACKED BETWEEN XOS 698-703. REPAIRED LT WING FIXED L/E BEADED DOUBLER AT XOS698-703, REF EA 011-5730-01-A4030 REV I/R AND EO MD11-5730-47834-A.SDR WRLA20120602546Skin · gougedGOUGE / DENT FOUND DURING PRIMARY INSPECTION AT FUSELAGE STA 755 L-24 & L25 MEASURED 3.00 X .133. ACCOMPLISHED HFEC INSPECTION ON DENT, NO CRACKS FOUND FOLLOWING BLEND-OUT OF THE EFFECTED AREA ACCOMPLISHED UT INSPECTION OF EFFECTED AREA AND FOUND SKIN THICKNESDR WRLA20120524545Structure · corrodedCORROSION ON TOP OF CENTER WING BOX AT STA 1249 BETWEEN X=75.25 AND X=709.25 RT.SDR WRLA20120521544Fitting · crackedCRACK - FOUND NOSE LANDING GEAR TRUNNION FITTING ON LEFT SIDE HAD CRACK STA Y=595 L=0.5". IAW AMM 32-21-01-000-801 REV B REMOVED NOSE LANDING GEAR ASSY. REPAIR THE CRACK AREA IAW SRM 53-10-14 FIGURE 202 RE. 49 REPAIR 2 IAW AMM 32-21-01-400 REINSTALLED NOSE LSDR FDEA201201260347Pressure Switch · failedMAX POWER TAKE OFF, NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. OIL PRESSURE INDICATED NORMAL ON GAUGES. ABORT WAS ACCOMPLISHED AT 20 KIAS. LIGHT WENT OUT WHEN POWER MOVED TO IDLE. ALL OIL INDICATIONS REMAINED NORMAL. R & R LOW OIL PRESSURE SWITCH IAWSDR WRLA20120116534Longeron · corrodedDURING DAMAGE REMOVAL, A SECTION OF LONGERON 39R (1D0542T) WAS REMOVED FROM STATION 1879 TO THE FACTORY SPLICE AT STA 1894.015 (52641454) NORMAL THICKNESS OF THE LONGERON BASE IS .206. HOWEVER, THE REMOVED SECTION INCORPORATE A TAPER IN THE BASE THICKNESS FROSDR WRLA20111226529Ballast · defectiveELECTRICAL SMOKE SMELL IN A ZONE. PULLED CEILING LIGHTS OUTBOARD CIRCUIT BREAKER AND THE SMELL WENT AWAY. FWD CABIN LIGHT INOP. ITEM PUT IN DMI LOG DMI M33DE2011-214 MEL 33-10-01-01 CAT "C", DUE ON -01-12 C ON BALLAST DISC AND C/B PULLED ON CEILING LIGHT POSDR WRLA20111212527Oven · malfunctionedGALLEY BUS 3 OFF ALERT CAME ON WHEN F/A STARTED OVENS IN AFT GALLEY. SUSPECT OVENS 1 AND 2. F/A HEARD A POP SOUND AND SAW SPARKS FROM OVEN. SHUT OVENS 1 AND 2 OFF AND RESET GALLEY BUS 3.SDR WRLA20111118525Light · inoperativeEMERGENCY FLOOR LIGHTING INOP AT 4-6 HJK. ITEM PLACED ON MEL - DMI REF NO NM31101811-103 DUE DATE 28 NOV 2011, PLACARD INSTALLED CAT-C MX CONT NOTIFIED.SDR WRLA20111020524Light · no testEMERGENCY LIGHT TEST FAILED.SDR WRLA20111009522Skin · crackedRT WING SKIN SURFACE L/E CRACKED. REPAIRED CRACK IAW EI W2011A57B-2156, REV 00 AND REV 01.SDR WRLA20111009523Strap · crackedSTRAP ON RT WING L/E CRACKED FROM BOLT HOLE ABOUT 1" XOS 608. REMOVED DAMAGED STRAP IAW SRM 51-35-01 REV.47. FABRICATED STRAP IAW EI W2011P57B-2164 REV 00 AND REV 01. REPLACED DAMAGED STRAP IAW SRM 51-35-01 REV 47.SDR WRLA20111007521Skin · crackedDURING 3C+A12 CHECK, A 0.5 INCH CRACK WAS FOUND ON RT WING L/E SKIN AT LWS 889. REPAIRED CRACK IAW EI W2011A57B-2129 REV.00, REV.01 AND REV.02.SDR WRLA20111005520Door · damagedREMOVE EXISTING DOUBLER FOR INSPECTION DUE NO REPAIR DOCUMENTATION. AIR CONDITIONING EQUIP SYS 3 ACCESS DOOR UPPER FWD DOOR CORNER SKIN REF: EGAT N/R U05004. RMV THE DOUBLER IAW SRM 51-35-01 REV. 47. REPAIR DAMAGED AREA IAW SRM 52-40-01. REPAIR 1 FIGURE 201SDR WRLA20111005519Intercostal · crackedINTERCOSTAL CRACKED STA 2141, L9R. PERFORMED EI NO: W2011A53B-2141 REV.00 AND REV.01.SDR WRLA20111004516Structure · damagedAFT CARGO DOOR LWR AFT CORNER DAMAGED. REPAIRED DAMAGE AREA IAW EI: W2011A52B-2148 REV. 00, REV.01 REV.02.SDR WRLA20111003514Seat Track · corrodedCORROSION FOUND ON RT MAIN DECK SEAT TRACK STA Y = 535 X = 75.25. REPLACED DAMAGED TRACK WITH NEW PART IAW SRM 53-33-01 AND 51-35-01 REV 47.SDR WRLA20111003515Seat Track · corrodedCORROSION FOUND LT MAIN DECK SEAT TRACK CORROSION STA Y535 X = 75.25. REPAIRED SEAT TRACK IAW SRM 53-00-52 REPAIR 1 REV.47 AND EI W2011A53B-2224, REV.00.SDR WRLA20111003518Trunnion · crackedFOUND NOSE LANDING GEAR TRUNNION FITTING ON LT SIDE HAS CRACK STA Y=595 L=0.6. REPAIRED IAW SRM 53-10-14, REPAIR 2, FIG 202, REV. 47 AND EI W2011A53B-2159. REV. 00SDR WRLA20110920510Skin · dentedAIRCRAFT DAMAGE FOUND AT SCHEDULE A-6 CHECK INITIAL WALKAROUND, DENT ON FUSELAGE FORWARD OF L-2 DOOR BETWEEN Y715 AND Y736, AT Z27. DENT WAS 4 INCH LONG, 0.750 WIDE, 0.145 DEEP. BEING REPAIRED PER SRM 53-00-01.SDR WRLA20110826509Battery · dischargedEMER LT 1L TEST FAIL. REMOVED AND REPLACED EMER LIGHT BATT SYSTEM, OPS CHECK GOOD MM 33-50.SDR WRLA20110823508Skin · corrodedCORROSION ON TOP OF CENTER TANK UPPER SKIN. REFERENCE EGAT NON-ROUTINE U05062; U05065; U05067; U05069; U05072; U05083. RE-WORKED CORROSION AREAS IAW EI W2011A57B-1770 REV. 01 AND REV. 02 FAA FORM 8100-9 SUBMITTED. SEE BOEING ACTIVITY NUMBER 1-WNM371 ALL WORKSDR FDEA201108223399Engine · failedNR 3 ENGINE OIL QUANTITY INDICATED BOXED AMBER SHOWING 1 GAL OIL. TEMP INCREASED TO 135 DEGREE C. OIL PRESSURE INDICATED 80 PSI. SHUTDOWN ENGINE & LANDED. ENGINE OPERATED AT WINDMILLING RPM FOR APPROX 30 MINUTES, OIL QUANTITY APPROX 1 GAL. ALL OTHER INSDR WRLA20110819507Skin · gougedGOUGE- LEFT LOWER FUSELAGE OUTER SKIN STATION Y = 1150 TO Y = 1156 L44L. BLENDED AND OUT OF LIMIT. BLEND OUT GOUGE AND MEASURE RE-WORKED AREA AND THICKNESS, DETAIL DATA OUT OF LIMIT. REPAIRED DAMAGED AREA IAW SRM 53-40-01-2R-2. REPAIR NR 2 REV 46.SDR WRLA20110818501Seat Track · crackedCRACK - AFT CARGO LT SIDE STATION 1944, SEAT TRACK. THE DAMAGED AREA AND RESULT ARE WITHIN ALLOWABLE LIMITS REF SRM 53-00-52 NDT VERIFIED NO CRACK. APPLIED PROTECTIVE COATING.SDR WRLA20110818502Seat Track · crackedCRACK - MAIN DECK SEAT TRACK, STA 755, X76 FWD CARGO COMPARTMENT. REPAIRED THE EXISTING DAMAGED SEAT TRACK SECTION IAW SRM 53-00-52-2R-1 REV 46 AND SRM 51-33-01 REV 46.SDR WRLA20110818504Seat Track · crackedCRACK - MAIN DECK SEAT TRACK, STA 755, X28, FWD CARGO COMPARTMENT. REPAIRED THE EXISTING DAMAGED SEAT TRACK SECTION IAW SRM 53-00-52-2R-1 REV 46 AND SRM 51-33-01 REV 46.SDR WRLA20110818505Seat Track · crackedCRACK - MAIN DECK SEAT TRACK, STA 635, X48 FWD CARGO COMPARTMENT. REPAIRED THE EXISTING DAMAGED SEAT TRACK SECTION IAW SRM 53-00-52-2R-1 REV 46 AND SRM 51-33-01 REV 46.SDR WRLA20110818503Seat Track · crackedCRACK - MAIN DECK SEAT TRACK, STA 755, X48 FWD CARGO COMPARTMENT REF: EGAT N/R U05201. REPAIRED THE EXISTING DAMAGED SEAT TRACK SECTION IAW SRM 53-00-52-2R-1.SDR WRLA20110818506Seat Track · crackedCRACK - MAIN DECK SEAT TRACK, STA 635, X10, FWD CARGO COMPARTMENT REF: EGAT N/R U05202. REPAIRED THE EXISTING DAMAGED SEAT TRACK SECTION IAW SRM 53-00-52-2R-1 AND SRM 51-33-01 REV 46.SDR WRLA20110812500Pan · crackedDURING 2 C CHECK DATUM AIRCRAFT, CRACK WAS FOUND ON RETAINING PAN OF CABIN WINDOW PLUG ASSY. REFERENCE EGAT NON-ROUTINE U05111. REPAIRED DAMAGED AREA IAW EGAT EI NR W2011A56B-1756 PER REV 00, REV 01 REV 02 BOEING MSG EGA-WLD-11-00007-02B.SDR WRLA20110806499Vent · corrodedAFT RT FUSELAGE FWD LAV EXH VENT CORRODED AND POPPED RIVET AT 6 O'CLOCK POSITION. FWD VENT STA 1895 BETWEEN LONGERON 39 AND 40 RT.SDR WRLA20110730497Pin · defectiveFLOOR EMERGENCY LIGHTS, ZONE B, LIT, SEAT 19D AND FWD INOP. CLEANED ALL CONNECTIONS ON FLOOR AND REPLACED AP5660023 PINS ON WIRES FRH-20WH. LIGHTS CHECK NORMAL PER MM 33-52, TROBLESHOOTING PER WDM 33-52-06.SDR WRLA20110720494Battery Pack · failedNR 1 EMERGENCY BATTERY FAILED TEST. REMOVED AND REPLACED NR 1 EMERGENCY LT BATTERY PACK ALL TEST PASSED.SDR WRLA20110615492Fire Loop · failedLEVEL 3 FIRE WARNING, NR 3 ENG INTERMITTENT ON CLIMBOUT. ON/OFF SEVERAL TIMES, FOLLOWED BY LEVEL 1 ENG 3 FIRE DET FAIL. SECOND ALERT WAS INTERMITTENT FOR 20 MINS. BOTH WERE OFF IN CRUISE. ISSUED DMI PER MEL 26-11-01-01 CAT C LOOP "B" FAIL DM: M26JU1111-76SDR WRLA20110608491Structure · crackedAPU DOOR INNER STRUCTURE CRACKED NEAR SNUBBER FITTING.SDR WRLA20110603489Support Fitting · crackedRT NLG SUPPORT FITTINGS 15MM CRACKED.SDR WRLA20110601487Longeron · corrodedRT SIDE LONGERON 28 BELOW OVERWING DOOR ON TWICE POSITIONS CORRODED.SDR WRLA20110601488Longeron · corrodedLT SIDE LONGERON 28 BELOW OVERWING DOOR CORRODED.SDR WRLA20110601490Nose Cowl · crackedENGINE NR 2 FRONT SPAR OF NOSE COWL INSIDE CRACKED 0400 POS. LIP SKIN ON POSITION 12/3/6/9 CLOCK POS. FOUND SEVERAL NEW CRACKS NEXT TO EXISTING DOUBLER.
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