# Service difficulty reports: Rolls-Royce TAY-651-54

A list on [Rolls-Royce TAY-651-54](https://openairdocs.org/engine/rolls-royce-tay-651-54.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 56 reports

- [SDR DALA2026010500070](https://openairdocs.org/sdr/DALA2026010500070.md): Engine · fire · Jan 2, 2026 · N998AT · Boeing 717200 · Engine (Turbine/Turboprop)
  > REJECTED 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 DALA2022111507349](https://openairdocs.org/sdr/DALA2022111507349.md): Anti-Ice Valve · faulted · Nov 13, 2022 · N998AT · Boeing 717200 · Engine Anti-Icing System
  > SHIP 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. AL
- [SDR CA131115002](https://openairdocs.org/sdr/CA131115002.md): Tube · sheared · Nov 14, 2013 · Boeing 72723 · Cargo/Baggage Doors
  > (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 BEEN
- [SDR CA131107001](https://openairdocs.org/sdr/CA131107001.md): Case · corroded · Nov 6, 2013 · Boeing 72723 · Engine (Turbine/Turboprop)
  > (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 MET
- [SDR N93A07072007A](https://openairdocs.org/sdr/N93A07072007A.md): Probe · faulted · Jul 7, 2007 · N440QS · Gulstm GIVXG450 · Fuel Quantity Sensor
  > LOW FUEL INDICATION AFTER TAKEOFF. REMOVED AND REPLACED FUEL LEVEL LOW SENSOR PROBE.
- [SDR UPS06248626](https://openairdocs.org/sdr/UPS06248626.md): Indicator · inoperative · Nov 14, 2006 · N920UP · Boeing 727180C · Fuel Quantity Indicator
  > N/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 O
- [SDR UPS06248627](https://openairdocs.org/sdr/UPS06248627.md): Light · malfunctioned · Nov 14, 2006 · N936UP · Boeing 727108C · Emergency Lighting
  > INSPECTION 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 UPS06246027](https://openairdocs.org/sdr/UPS06246027.md): Floorbeam · corroded · Jan 12, 2006 · N938UP · Boeing 727173C · Fuselage Main, Floor Beam
  > C-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 UPS06246011](https://openairdocs.org/sdr/UPS06246011.md): Carriage · corroded · Jan 10, 2006 · N938UP · Boeing 727173C · Trailing Edge Flaps
  > INSPECTION C-CHECK AND SI SEVERAL AREAS OF CORROSION ON NR 3 FLAP CARRIAGE. NR3 FLAP CARRIAGE REPLACED IAW MM 27-51-03.
- [SDR UPS06246012](https://openairdocs.org/sdr/UPS06246012.md): Carriage · corroded · Jan 10, 2006 · N938UP · Boeing 727173C · Trailing Edge Flaps
  > C-CHECK AND SI NR 8 FLAP CARRIAGE HAS CORROSION IN SPINDLE BORE. NR 8 FLAP CARRIAGE REPLACED IAW MM 27-51-13.
- [SDR UPS06246031](https://openairdocs.org/sdr/UPS06246031.md): Beam · corroded · Jan 10, 2006 · N938UP · Boeing 727173C · Fuselage Main, Structure
  > INSPECTION 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 LIM
- [SDR UPS06246085](https://openairdocs.org/sdr/UPS06246085.md): Angle · corroded · Jan 10, 2006 · N936UP · Boeing 727108C · Fuselage Miscellaneous Structure
  > INSPECTION 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 DR
- [SDR UPS06246025](https://openairdocs.org/sdr/UPS06246025.md): Stiffener · corroded · Jan 8, 2006 · N938UP · Boeing 727173C · Fuselage Miscellaneous Structure
  > C-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 UPS06246026](https://openairdocs.org/sdr/UPS06246026.md): Stiffener · corroded · Jan 8, 2006 · N938UP · Boeing 727173C · Fuselage Miscellaneous Structure
  > C-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 UPS06246014](https://openairdocs.org/sdr/UPS06246014.md): Skin · corroded · Jan 6, 2006 · N938UP · Boeing 727173C · Fuselage Main, Plate/Skin
  > INSPECTION 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 UPS06246016](https://openairdocs.org/sdr/UPS06246016.md): Skin · corroded · Jan 6, 2006 · N938UP · Boeing 727173C · Fuselage Main, Plate/Skin
  > C-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 UPS06246028](https://openairdocs.org/sdr/UPS06246028.md): Skin · corroded · Jan 6, 2006 · N938UP · Boeing 727173C · Fuselage Main, Plate/Skin
  > INSPECTION 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 UPS06246029](https://openairdocs.org/sdr/UPS06246029.md): Lap Joint · corroded · Jan 5, 2006 · N938UP · Boeing 727173C · Fuselage Main, Plate/Skin
  > INSPECTION 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 I
- [SDR UPS06246030](https://openairdocs.org/sdr/UPS06246030.md): Lap Joint · corroded · Jan 5, 2006 · N938UP · Boeing 727173C · Fuselage Main, Plate/Skin
  > INSPECTION 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 INDICATI
- [SDR UPS06246032](https://openairdocs.org/sdr/UPS06246032.md): Skin · cracked · Jan 5, 2006 · N938UP · Boeing 727173C · Fuselage Main, Plate/Skin
  > INSPECTION 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 53
- [SDR UPS06246086](https://openairdocs.org/sdr/UPS06246086.md): Skin · cracked · Jan 4, 2006 · N938UP · Boeing 727173C · Fuselage Main, Plate/Skin
  > INSPECTION 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 5330-1
- [SDR UPS05245890](https://openairdocs.org/sdr/UPS05245890.md): Floor Support · cracked · Dec 13, 2005 · N945UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION 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 SRM
- [SDR UPS05245848](https://openairdocs.org/sdr/UPS05245848.md): Light · inoperative · Nov 30, 2005 · N932UP · Boeing 72725C · Emergency Lighting
  > N/A ENTRY DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSY REF AMM 33-50-00-0. OPS CK NORMAL.
- [SDR UPS04243352](https://openairdocs.org/sdr/UPS04243352.md): Control Unit · malfunctioned · Oct 17, 2004 · N940UP · Boeing 727185C · Fire Detection
  > WHEN 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 ON
- [SDR UPS04243383](https://openairdocs.org/sdr/UPS04243383.md): Web · cracked · Oct 8, 2004 · N954UP · Boeing 727185C · Fuselage Miscellaneous Structure
  > INSPECTION 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 DA
- [SDR UPS04243392](https://openairdocs.org/sdr/UPS04243392.md): Skin · corroded · Oct 6, 2004 · N954UP · Boeing 727185C · Ailerons
  > INSPECTION TYPE-C RT OB AILERON HAS PITTING CORROSION ON CONTROL ROD ATTACH CASTING. AILERON REPLACED IAW MM 27-10-14.
- [SDR UPS04243397](https://openairdocs.org/sdr/UPS04243397.md): Hinge · corroded · Oct 4, 2004 · N954UP · Boeing 727185C · Ailerons
  > INSPECTION 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 51-30-02
- [SDR UPS04243072](https://openairdocs.org/sdr/UPS04243072.md): Battery · inoperative · Sep 6, 2004 · N937UP · Boeing 72725C · Emergency Lighting
  > INSPECTION 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 UPS04243067](https://openairdocs.org/sdr/UPS04243067.md): Attach Angle · corroded · Aug 26, 2004 · N936UP · Boeing 727108C · Fuselage Miscellaneous Structure
  > INSPECTION 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 UPS04243066](https://openairdocs.org/sdr/UPS04243066.md): Light · defective · Aug 23, 2004 · N936UP · Boeing 727108C · Emergency Lighting
  > INSPECTION 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 UPS04243068](https://openairdocs.org/sdr/UPS04243068.md): Strap · corroded · Aug 23, 2004 · N936UP · Boeing 727108C · Fuselage Miscellaneous Structure
  > INSPECTION 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 51-20-01
- [SDR UPS04243070](https://openairdocs.org/sdr/UPS04243070.md): Stiffener · corroded · Aug 23, 2004 · N936UP · Boeing 727108C · Fuselage Miscellaneous Structure
  > INSPECTION 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 UPS04243077](https://openairdocs.org/sdr/UPS04243077.md): Doubler · cracked · Aug 22, 2004 · N936UP · Boeing 727108C · Fuselage Main, Plate/Skin
  > INSPECTION 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 UPS04243009](https://openairdocs.org/sdr/UPS04243009.md): Frame · cracked · Aug 17, 2004 · N945UP · Boeing 72722C · Fuselage Main, Frame
  > C 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 UPS04243062](https://openairdocs.org/sdr/UPS04243062.md): Skin · debonded · Aug 17, 2004 · N936UP · Boeing 727108C · Trailing Edge Flaps
  > INSPECTION TYPE:C LT OB MIDFLAP T-EDGE WEDGE UPPER SKIN DISBOND 45 INCHES IB OF OB EDGE. DAMAGE REPAIRED IAW SRM 51-40-5
- [SDR UPS04243063](https://openairdocs.org/sdr/UPS04243063.md): Lap Joint · corroded · Aug 16, 2004 · N936UP · Boeing 727108C · Fuselage Main, Plate/Skin
  > INSPECTION 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 UPS04242900](https://openairdocs.org/sdr/UPS04242900.md): Switch · inoperative · Aug 13, 2004 · N926UP · Boeing 72731C · Emergency Lighting
  > EMERGENCY EXIT LIGHTS INOPERATIVE, COCKPIT DOOR. TURNED BATTERY SWITCH ON PLACED EMERGENCY LIGHT SWITCH TO ARMED, LIGHT CHECKS GOOD.
- [SDR UPS04243076](https://openairdocs.org/sdr/UPS04243076.md): Skin · corroded · Aug 13, 2004 · N936UP · Boeing 727108C · Fuselage Main, Plate/Skin
  > INSPECTION 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 UPS04243064](https://openairdocs.org/sdr/UPS04243064.md): Skin · cracked · Aug 12, 2004 · N936UP · Boeing 727108C · Fuselage Main, Plate/Skin
  > C-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 UPS04243000](https://openairdocs.org/sdr/UPS04243000.md): Skin · delaminated · Aug 5, 2004 · N945UP · Boeing 72722C · Trailing Edge Flaps
  > INSPECTION 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 UPS04243001](https://openairdocs.org/sdr/UPS04243001.md): Skin · delaminated · Aug 5, 2004 · N945UP · Boeing 72722C · Trailing Edge Flaps
  > INSPECTION TYPE: C, DELAM ON RT IB FORE FLAP UPPER SURFACE AT IB END. RT IB FLAP REPLACED REPLACED IAW MM27-51-01.
- [SDR UPS04243002](https://openairdocs.org/sdr/UPS04243002.md): Skin · cracked · Aug 4, 2004 · N945UP · Boeing 72722C · Landing Gear Doors
  > INSPECTION 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 UPS04243008](https://openairdocs.org/sdr/UPS04243008.md): Web · cracked · Aug 4, 2004 · N945UP · Boeing 72722C · Landing Gear Doors
  > LT 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 UPS04242999](https://openairdocs.org/sdr/UPS04242999.md): Hinge · cracked · Aug 2, 2004 · N945UP · Boeing 72722C · Ailerons
  > INSPECTION 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 27-10
- [SDR UPS04243015](https://openairdocs.org/sdr/UPS04243015.md): Window Frame · cracked · Jul 7, 2004 · N945UP · Boeing 72722C · Fuselage Main, Structure
  > INSPECTION 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 UPS02238098](https://openairdocs.org/sdr/UPS02238098.md): Engine · failed · Apr 30, 2002 · N916UP · Boeing 727172C · Engine (Turbine/Turboprop)
  > INSPECTION 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 CA020322003](https://openairdocs.org/sdr/CA020322003.md): Cage · failed · Mar 4, 2002 · Boeing 727100 · Turbine Engine Accessory Drive
  > (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 L
- [SDR UPS02237744](https://openairdocs.org/sdr/UPS02237744.md): Engine · malfunctioned · Mar 1, 2002 · N922UP · Boeing 72731C · Engine (Turbine/Turboprop)
  > INSPECTION 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 UPS01237043](https://openairdocs.org/sdr/UPS01237043.md): Bullet · cracked · Oct 14, 2001 · N902UP · Boeing 72751C · Turbine Engine Air Inlet Section
  > INSPECTION 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 CA020509002](https://openairdocs.org/sdr/CA020509002.md): Gearbox · failed · Apr 30, 2000 · Boeing 727* · Turbine Engine Accessory Drive
  > (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

Next page: https://openairdocs.org/engine/rolls-royce-tay-651-54/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/engine/rolls-royce-tay-651-54/reports

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