Rolls-Royce TAY-651-54
Service difficulty reports · 56
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 = 'TAY65154' 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 = 'TAY65154' 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 DALA2026010500070Engine · fireREJECTED TAKEOFF AT 140 KNOTS DUE TO A LEFT ENGINE FIRE INDICATION. FOUND LEFT ENGINE INNER CORE PANELS DAMAGED AND BLOWN OUT. ALSO NOTED DAMAGED FIRE DETECTOR SENSOR, NO EVIDENCE OF FIRE. DUE TO DAMAGE FOUND, ENGINE CHANGE REQUIRED.(7793260)SDR DALA2022111507349Anti-Ice Valve · faultedSHIP 9547 - ATB - THE CREW RETURNED THE AIRCRAFT TO DTW FOLLOWING A "#1 ENGINE ANTI-ICE" MESSAGE. AN EMERGENCY WAS DECLARED WITH ATC ON APPROACH FOR LANDING. CORRECTIVE ACTION: MAINTENANCE REPLACED THE ENGINE ANTI-ICE PRESSURE VALVE AND THE PRESSURE SWITCH. ALSDR CA131115002Tube · sheared(CAN) THE PHENOLIC TUBE THAT THE DOOR COUNTER BALANCE SPRING IS HOUSED SHREDDED. CAUSING THE COUNTER BALANCING SPRINGS TO BE EJECTED ACROSS THE HANGAR, NO PERSONNEL WERE INJURED. UPON INSPECTION MINOR CRACKING WAS FOUND ON THE PHENOLIC TUBE. NEW TUBE HAS BEENSDR CA131107001Case · corroded(CAN) CORROSION WAS FOUND ON ALL 3 ENGINE INTERMEDIATE CASES ON THE AFT FLANGE. IT WAS DISCOVERED DURING C1 VISIT. ENGINE MFG CONTACTED. REPAIR TEAM WAS SENT TO ACCESS AND REPAIR CORROSION TREATED IAW MM. SUSPECTED CAUSE OF CORROSION IS FROM DISSIMILAR METSDR N93A07072007AProbe · faultedLOW FUEL INDICATION AFTER TAKEOFF. REMOVED AND REPLACED FUEL LEVEL LOW SENSOR PROBE.SDR UPS06248626Indicator · inoperativeN/A ATB - FUEL IMBALANCE BETWEEN TANK NR 1 AND NR 3 STARTED AT NR 1, 11.9, NR 3, 11.2 AFTER TA/O TANK NR 1, 11.5, TANK NR 3, 9.5 DEFERRED NR 3 COCKPIT GAUGE NR M337674 ISSUED. DEFERRED NR 3 COCKPIT GAUGE IAW MEL 28-11-1-1. VERIFIED FUELING STATION GAUGES ARE OSDR UPS06248627Light · malfunctionedINSPECTION TYPE: N/A EMERGENCY EXIT LIGHT ILLUMINATED IN FLIGHT COULD NOT RESET. STAYED ON. ACCOMPLISHED EMERGENCY LIGHTING ADJUSTMENT/TEST IAW MM 33-50-01-5. SYSTEM CHECKS GOOD. UNABLE TO DUPLICATE PROBLEM.SDR UPS06246027Floorbeam · corrodedC-CHECK SI REF. NRC 100662 FLOORBEAM TOP CHORD CORROSION WAS REMOVED BS 344 AND FOUND OUTSIDE LIMITS OF SRM . REPLACE TOP CHORD SECTION RBL 80 - LBL 66 . REF SRM 53-10-8 FIG 7 FLOORBEAM TOP CHORD REMOVED IAW SRM 51-30-02. NEW TOP CHORD FABRICATED IAW SRM SDR UPS06246011Carriage · corrodedINSPECTION C-CHECK AND SI SEVERAL AREAS OF CORROSION ON NR 3 FLAP CARRIAGE. NR3 FLAP CARRIAGE REPLACED IAW MM 27-51-03.SDR UPS06246012Carriage · corrodedC-CHECK AND SI NR 8 FLAP CARRIAGE HAS CORROSION IN SPINDLE BORE. NR 8 FLAP CARRIAGE REPLACED IAW MM 27-51-13.SDR UPS06246031Beam · corrodedINSPECTION TYPE:C AND CORROSION ON UPPER OB SURFACE OF LONGITUDINAL BEAM LWR. CHORD AT BS 7 45 WIRE LOOM ATTACH ANCHOR NUT AT LBL 20. PLS REMOVE ANCHOR NUT, REMOVE CORROSION, RE-INSPECT AND RECTIFY AS NECESSARY. CORROSION IDENTIFIED AND FOUND TO BE OUTSIDE LIMSDR UPS06246085Angle · corrodedINSPECTION TYPE-C RT FUSE ABOVE NR 2 ENG AT THE ANGLE BETWEEN FUSE AND VERT STAB HAS LIGHT SURFACE CORROSION AT BS1428 TO 1464. DAMAGED ANGLE REMOVED AND REPLACEMENT ANGLE FABRICATED IAW DRW. NR QF5314263. REPLACEMENT ANGLE INSTALLED IAW SRM51-30-02 AND DRSDR UPS06246025Stiffener · corrodedC-CHECK AND SI LIGHT SURFACE CORROSION ON AFT 870 LT OB STIFFENER 21 INCHES UP FROM BOTTOM EDGE OF LT. CORROSION REMOVED IAW SRM 51-10-6 AND FOUND TO BE OUTSIDE LIMITS 53-10 -1. REPAIR CARRIED OUT IAW SRM 51-40-4 .SDR UPS06246026Stiffener · corrodedC-CHECK AND SI LIGHT SURFACE CORROSION ON AFT OF 870 B/H RT ON OB STIFFENER 20 INCHES UP FROM BOTTOM EDGE B/H CORROSION REMOVED IAW SRM 51-10-6 AND FOUND TO BE OUTSIDE LIMITS SRM 5 3-10-1. REPAIR CARRIED OUT IAW SRM 51-40-4.SDR UPS06246014Skin · corrodedINSPECTION C-CHECK AND SI EVIDENCE OF SURFACE CORROSION BETWEEN FUSELAGE SKIN AND STRINGER 4R AT BS 990 AT INTERIOR AREA OF FUSELAGE. AREA DERIVATED IAW SRM 51-30-02. CORROSION REMOVED IAW SRM 51-10-01 SE E NRC 100274 FOR REPAIR DETAILS.SDR UPS06246016Skin · corrodedC-CHECK AND SI EVIDENCE OF CORROSION BETWEEN FUSELAGE SKIN AND STRINGER 4 R AT BS 101 0 AT INTERIOR AREA OF FUSELAGE. AREA DERIVETED IAW SRM 51-30-02. CORROSION REMOVED IAW SRM 51-10-01.SDR UPS06246028Skin · corrodedINSPECTION TYPE C AND IS EVIDENCE OF CORROSION BETWEEN FUSELAGE SKIN AND STRINGER 4R AT BS 1040 AT INTERIOR AREA OF FUSELAGE. AREA DIVERTED IAW SRM 51-30-02. CORROSION REMOVED IAW SRM 51-10-01.SDR UPS06246029Lap Joint · corrodedINSPECTION TYPE:C AND IS CORROSION EVIDENT AT LAP JOINT S4 RT BS 1010 TO 990. PLS. CARRY OUT N DI ON LAP JOINT BS 1080 TO 870 RE-INSPECT AND RECTIFY IAW EO APPENDIX IF NECESSARY LFEC INSP. CARRIED OUT IAW NDTM PT 6 51-00-00 FIG 5. - 15 PERCENT MATERIAL LOSS ISDR UPS06246030Lap Joint · corrodedINSPECTION TYPE:C AND CORROSION EVIDENT AT LAP JOINT S4R BS 940 TO 920. PLS. CARRY OUT NDI O N LAP JOINT BS 1080 TO 870. RE-INSPECT AND RECTIFY IAW EO APPENDIX IF NECESSARY LFEC INSP. CARRIED OUT IAW NDTM PT 6 51-00-00 FIG 5 - 15 PERCENT MATERIAL LOSS INDICATISDR UPS06246032Skin · crackedINSPECTION TYPE:C AND IS SUSPECT SKIN CRACK AT FASTENER HOLE SECTION 41 RT AT BS 239 S15R. PL S. CARRY OUT NDI AND RECTIFY IF NECESSARY IAW SRM HFEC INSP. CARRIED OUT IAW NDTM PT 6 51-00-00. CRACK CONFIRMED AND ENDS MARKED. REPAIR CARRIED OUT IAW SRM 53SDR UPS06246086Skin · crackedINSPECTION TYPE-C AND IS SUSPECT SKIN CRACK AT UPPER FWD CORNER OF FWD ENTRY DOOR CUT OUT BETWEEN STR 7 AND 8L PLS. CARRY UT NDI AND RECTIFY AS NECESSARY IAW SRM HFEC INCP CARRIED IAW NDTM 51-00-00 PT 6 CRACK CONFIRMED ENDS MARKED. DAMAGE REMOVED IAW EO 5330-1SDR UPS05245890Floor Support · crackedINSPECTION TYPE: C AFT CARGO FLOOR SUPPORT BEAM CRACK ON S28 BETWEEN FR 1060 AND 1090 AT SP LICE PLATE FROM RIVET HEAD. CUT OUT DAMAGED SECTION OF FLOOR SUPPORT IAW SRM REF 53-10-5. FABRICATED REPAIR PARTS IAW SRM REF 53-10-5 FIG 4. REPAIR CARRIED OUT IAW SRMSDR UPS05245848Light · inoperativeN/A ENTRY DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSY REF AMM 33-50-00-0. OPS CK NORMAL.SDR UPS04243352Control Unit · malfunctionedWHEN F/O TURNED OFF F/D ALTITUDE HOLD, RECEIVED AN INTERMITTENT FIRE WARNING. THE F/O TAPPED THE GLARE SHIELD AND THE FIRE WARNING LIGHT AND BELL CAME ON STEADY. ENGINE NR 3 WAS SHUTDOWN IAW PROCEDURES AND UNEVENTFUL. SIMULATED CREW ACTION BY TAPPING ONSDR UPS04243383Web · crackedINSPECTION TYPE-C BS 740 LOWER WEB RT BL 35 WL160 APPROX SUSPECT CRACK IN THIS LOCATION. HFEC CARRIED OUT ON ABOVE AREA IAW NDTM 51-00-00 PT 6 FIG 4 CRACKS CONTAINED WITHIN FASTENER HOLE. REPAIR PARTS FABRICATED IAW SRM 53-10-09. REPROTECTED REP PARTS AND DASDR UPS04243392Skin · corrodedINSPECTION TYPE-C RT OB AILERON HAS PITTING CORROSION ON CONTROL ROD ATTACH CASTING. AILERON REPLACED IAW MM 27-10-14.SDR UPS04243397Hinge · corrodedINSPECTION TYPE-C RT IB AILERON TAB HINGE CASTINGS ARE CORRODED AND SUSPECT CRACK ON AILERON REAR SPAR. REPLACED REAR SPAR IAW SRM 51-30-02. NEW TAB HINGES INSTALLED IAW SRM 51-30-02SDR UPS04243072Battery · inoperativeINSPECTION TYPE: N/A EMERGENCY EXIT LIGHTS DO NOT COME ON WHEN SWITCH PLACED IN ON POSITION. REMOVED AND REPLACED BATTERY IN EACH EMERGENCY EXIT LIGHT. OPS CK GOOD REF MM 33-50-01.SDR UPS04243067Attach Angle · corrodedINSPECTION TYPE: C, DURING INSPECTION OF SKIN REPAIR, AT 1334 LT SIDE AFT AIRSTAIRS, SKIN ATTACH ANGLE FOUND CORRODED. REPLACED ATTACH ANGLE IAW SRM 51-10-01.SDR UPS04243066Light · defectiveINSPECTION TYPE: C-COCKPIT EMERGENCY LIGHT DOES NOT ILLUMINATE WITH SWITCH ON P5 PANEL TO ON. LIGHT ASSEMBLY FOUND DEFECTIVE IAW WDM 33-51-01. LIGHT ASSY REPLACED IAW MM 33-50-01. FUNCTION CHECKED OK.SDR UPS04243068Strap · corrodedINSPECTION TYPE: C ON INSP FLOOR PANEL SPLICE STRAP FOUND BADLY CORRODED AT BS 520 BETWEEN RBL 24 AND LBL 24. SPLICE STRAP REPLACED IAW SRM 51-20-01SDR UPS04243070Stiffener · corrodedINSPECTION TYPE: C, HORIZONTAL STIFFNER CORRODED AFT OF APU EXHAUST PORT ON LOWER SURFACE OF UPPER PANEL AT 2 LOCATIONS. CORROSION FOUND TO BE OUTSIDE LIMITS. STIFFNER REMOVED IAW SRM 51-30-02. NEW STIFFNER INSTALLED IAW DRG 65-21655.SDR UPS04243077Doubler · crackedINSPECTION TYPE: C, CRACK ON DOUBLER RT SIDE BS 1444 APPROX. CRACK CUT OUT IAW SRM 51-40-02. HFEC CARRIED OUT IAW NDT MANUAL 51- 00-00 PT 6 FIG 4. NO DEFECTS FOUND. REPAIR DOUBLER FABRICATED IAW SRM 51-40-02 AND INSTALLED IAW SRM 51-30-02.SDR UPS04243009Frame · crackedC FRAME LEG CRACKED AT BS 294, STR 9/10L. DAMAGED PORTION OF FRAME REMOVED IAW SRM 53-10-4. HFEC CARRIED OUT AROUND CUTOUT: NO DEFECTS FOUND. REPAIR CARRIED OUT IAW 53-10-4.SDR UPS04243062Skin · debondedINSPECTION TYPE:C LT OB MIDFLAP T-EDGE WEDGE UPPER SKIN DISBOND 45 INCHES IB OF OB EDGE. DAMAGE REPAIRED IAW SRM 51-40-5SDR UPS04243063Lap Joint · corrodedINSPECTION TYPE: C, SUSPECT CORROSION AT LAP JOINT S19L BETWEEN BS 390 AND BS 441, CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 51-30-02. REPAIR CARRIED OUT IAW AAAE 2004-077-006 AND UPS EO B727-5330-21003-A.SDR UPS04242900Switch · inoperativeEMERGENCY EXIT LIGHTS INOPERATIVE, COCKPIT DOOR. TURNED BATTERY SWITCH ON PLACED EMERGENCY LIGHT SWITCH TO ARMED, LIGHT CHECKS GOOD.SDR UPS04243076Skin · corrodedINSPECTION TYPE: C, SUSPECT CORROSION BETWEEN SKIN AND INTERNAL STRUCTURE BS 217 STR 25L. AREA PAINT STRIPPED IAW MM 51-20-15. TRIMMED CORRODED AREA IAW SRM 53-30-03 AND REPAIRED AREA IAW SRM 53-30-3 FIG. 3.SDR UPS04243064Skin · crackedC-CRACKS ON CENTER POST OF COCKPIT WINDOWS, NR 1 LT AND NR 1 RT, LOWER IB CORNERS. HFEC CARRIED OUT AND CRACKS CONFIRMED. CRACKED SKIN REPLACED IAW AAAE EO 2004-077-004 AND UPS FILE NR 727-53-20157.SDR UPS04243000Skin · delaminatedINSPECTION TYPE:C LT IB AFT FLAP LWR SKIN DELAMINATION AT IB END AND BELOW NR 7 CARRIAGE. AFT FLAP REMOVED IAW MM 27-51-02. NEW AFT FLAP INSTALLED IAW MM 27-51-02.SDR UPS04243001Skin · delaminatedINSPECTION TYPE: C, DELAM ON RT IB FORE FLAP UPPER SURFACE AT IB END. RT IB FLAP REPLACED REPLACED IAW MM27-51-01.SDR UPS04243002Skin · crackedINSPECTION TYPE: C, CRACK ON LT MLG WING DOOR INNER SKIN AT TE. HFEC CARRIED OUT AND CRACK CONFIRMED. CRACK STOP DRILLED IAW SRM 51-10-1.HFEC CARRIED OUT AND CRACK CONTAINED WITHIN DRILLED AREA. REPAIR CARRIED OUT IAW SRM 52-80-2 FIG 5.SDR UPS04243008Web · crackedLT MLG WING DOOR LWR END WEB CRACKED. CRACK STOP DRILLED IAW SRM 51-10-1. HFEC INSPECTION CARRIED OUT. CRACK CONTAINED IN STOP DRILLED HOLE. REPAIRED IAW 51-40-02.SDR UPS04242999Hinge · crackedINSPECTION TYPE: C, LT OB AILERON OB HINGE FITTING ON AIRCRAFT HAS A SUSPECT CRACK. NDT CARRIED OUT AND CRACK CONFIRMED. LT OB AILERON REMOVED IAW 27-10 -14. OB HINGE REMOVED IAW SRM 51-30-2. NEW HINGE INSTALLED IAW SRM 51-30-2.OB AILERON INSTALLED MM 27-10SDR UPS04243015Window Frame · crackedINSPECTION TYPE: C, REPLACE LT WINDOW FRAME AT BS 1100 P/N:65-19850-149. FRAME REPLACED WITH NEW FRAME IAW SRM 51-30-2.SDR UPS02238098Engine · failedINSPECTION TYPE:N/A ATB NR 1 ENGINE OIL PRESSURE LOSS (ENGINE SHUT DOWN) NR 1 ENG CHANGE REF BOEING 727 MAINTENANCE FUNCTION TASK CARD 1273. ENGINE CHANGE COMPLETED IAW TC 1273.SDR CA020322003Cage · failed(CAN) THE NR 3 CSD/GEN TRIPPED, FOLLOWED BY LOW ENGINE OIL PRESSURE WHICH RESULTED IN AN IFSD DUE TO LACK OF OIL AND PRESSURE. GROUND MAINTENANCE ADDED 6 LITERS/QTS OF OIL TO THE ENGINE AND TOPPED OFF THE CSD. THERE WERE NO REPORTED NOR ANY SIGNS OF EXTERNAL LSDR UPS02237744Engine · malfunctionedINSPECTION TYPE:N/A NR 3 ENGINE SHUT DOWN IN FLIGHT DUE TO LOW OIL PRESSURE (4 PSI). REPLACED ENGINE NR 3 IAW TC 1273 AND TC 1276. ENGINE RUN SATISFACTORY.SDR UPS01237043Bullet · crackedINSPECTION TYPE:S-10 ENGINE 3 SPINNER CRACK FOUND DURING SEG-10 CHECK. HAS 1 INCH CRACK AT BOLT HOLE. REMOVED AND REPLACED NR 3 ENG SPINNER FAIRING IAW MM 72-30-10. OPS NORMAL AT THIS TIME.SDR CA020509002Gearbox · failed(CAN) EN ROUTE TO BDL, LOW OIL PRESSURE WARNING LIGHT ILLUMINATED AND OIL PRESSURE DROPPED TO 10 PSI. ENGINE SHUTDOWN CARRIED OUT AND AIR TURN BACK TO SDF. MAINTENANCE ADDED 5 QTS OF OIL. NO SIGNS OF EXTERNAL LEAKAGE. ENGINE RUN FOR 15 MIN. AND 2 QTS OF OIL CO
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