# Rolls-Royce TAY-651-54

- Type: Engine model (FAA registry)
- Registry code: 54564
- Manufacturer (registry): ROLLS-ROYC
- Model: TAY 651-54
- Engine type: Turbo-fan
- Power: 15,400 lb thrust
- Data sheet: [TCDS E25NE](https://openairdocs.org/tcds/E25NE) (OpenAirDocs)
- Holder: Rolls-Royce Deutschland Ltd & Co KG
- Installed in: 2 registered aircraft
- Page: https://openairdocs.org/engine/rolls-royce-tay-651-54

Model codes come from the FAA registry's reference file.

## ADs that may apply (OpenAirDocs)

Matched to this engine model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2019-14-01](https://openairdocs.org/ad/2019-14-01): Turbine Engine Compressor Section · Rolls-Royce Deutschland TAY 650-15 and TAY 651-54. Effective Aug 26, 2019
- [AD 2016-17-01](https://openairdocs.org/ad/2016-17-01): Stage 1 HPT disks · Rolls-Royce Deutschland TAY 650-15 and TAY 651-54. Effective Sep 27, 2016
- [AD 2014-06-05](https://openairdocs.org/ad/2014-06-05): Low-pressure (LP) compressor module · Rolls-Royce Deutschland TAY 620-15, TAY 650-15 and TAY 651-54. Effective May 8, 2014
- [AD 2014-03-16](https://openairdocs.org/ad/2014-03-16): Low-pressure compressor (LPC) fan blades · Rolls-Royce Deutschland TAY 620-15, TAY 650-15 and TAY 651-54. Effective Mar 18, 2014
- [AD 2013-23-01](https://openairdocs.org/ad/2013-23-01): High-pressure (HP) air bleed valve · Rolls-Royce Deutschland TAY 620-15, TAY 650-15 and TAY 651-54. Effective Dec 30, 2013
- [AD 2010-17-12 R1](https://openairdocs.org/ad/2010-17-12-R1): Engine · Rolls-Royce Deutschland TAY 650-15 and TAY 651-54. Effective Nov 18, 2010
- [AD 2010-20-22](https://openairdocs.org/ad/2010-20-22): Disc · Rolls-Royce Deutschland TAY 620-15, TAY 650-15 and TAY 651-54. Effective Nov 9, 2010
- [AD 2007-26-19](https://openairdocs.org/ad/2007-26-19): Low pressure (LP) compressor case · Rolls-Royce Deutschland TAY 611-8, TAY 611-8C, TAY 620-15 and 2 more. Effective Feb 11, 2008
- [AD 2005-26-18](https://openairdocs.org/ad/2005-26-18): High pressure compressor (HPC) stage 12 disc assembly · Rolls-Royce Deutschland TAY 650-15 and TAY 651-54. Effective Feb 3, 2006
- [AD 2005-03-06](https://openairdocs.org/ad/2005-03-06): LP fuel tubes · Rolls-Royce Deutschland TAY 611-8, TAY 620-15, TAY 650-15 and 1 more. Effective Mar 17, 2005
- [AD 2003-22-14](https://openairdocs.org/ad/2003-22-14): Fan blades · Rolls-Royce Deutschland TAY 650-15 and TAY 651-54. Effective Dec 18, 2003
- [AD 2002-09-02](https://openairdocs.org/ad/2002-09-02): Airworthiness Limitations Section (ALS) - Critical Life-Limited Rotating Engine Part · Rolls-Royce Deutschland TAY 650-15 and TAY 651-54. Effective Jun 6, 2002
- [AD 99-24-01](https://openairdocs.org/ad/99-24-01): Rolls-Royce Deutschland TAY 620-15, TAY 650-15 and TAY 651-54. Effective Jan 18, 2000

Historical (superseded or no longer in force):

- [AD 2010-17-12](https://openairdocs.org/ad/2010-17-12) (historical): Low- pressure turbine disks · Rolls-Royce Deutschland TAY 650-15 and TAY 651-54. Effective Sep 27, 2010
- [AD 2007-03-02](https://openairdocs.org/ad/2007-03-02) (historical): LP compressor fan blades · Rolls-Royce Deutschland TAY 611-8, TAY 620-15, TAY 650-15 and 1 more. Effective Mar 5, 2007
- [AD 2006-18-14](https://openairdocs.org/ad/2006-18-14) (historical): Cyclic life of stage 1 HPT discs, and stage 1 LPT discs · Rolls-Royce Deutschland TAY 650-15 and TAY 651-54. Effective Oct 13, 2006
- [AD 2004-26-10](https://openairdocs.org/ad/2004-26-10) (historical): Ice-impact Panels Installed in the Low Pressure (LP) Compressor Case · Rolls-Royce Deutschland TAY 611-8, TAY 620-15, TAY 650-15 and 1 more. Effective Jan 21, 2005
- [AD 2004-05-22](https://openairdocs.org/ad/2004-05-22) (historical): Low pressure (LP) compressor case · Rolls-Royce Deutschland TAY 611-8, TAY 611-8C, TAY 620-15 and 2 more. Effective Mar 25, 2004
- [AD 2003-05-04](https://openairdocs.org/ad/2003-05-04) (historical): Low pressure (LP) fuel tubes · Rolls-Royce Deutschland TAY 611-8, TAY 620-15, TAY 650-15 and 1 more. Effective Mar 26, 2003
- [AD 2002-01-29](https://openairdocs.org/ad/2002-01-29) (historical): High Pressure Compressor (HPC) Stage 11/12 Disc Spacer · Rolls-Royce Deutschland TAY 650-15 and TAY 651-54. Effective Feb 15, 2002
- [AD 2001-22-18](https://openairdocs.org/ad/2001-22-18) (historical): Fan Blades · Rolls-Royce Deutschland TAY 650-15 and TAY 651-54. Effective Dec 18, 2001

## Registered aircraft (2)

- [N394AJ](https://openairdocs.org/aircraft/N394AJ): [Glf4 1470 LLC](https://openairdocs.org/faa-owner/GLF4%201470%20LLC), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 2001, S/N 1470
- [N998AT](https://openairdocs.org/aircraft/N998AT): [Delta Air Lines Inc](https://openairdocs.org/faa-owner/DELTA%20AIR%20LINES%20INC), [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta), built 2002, S/N 55142

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB CHI96IA200](https://openairdocs.org/ntsb/CHI96IA200), Jun 14, 1996: Boeing 727-30C (N906UP), Chicago, IL, incident, no damage. Probable cause: low pressure in the fuel lines caused when the crossfeed valve was closed and the boost pumps to the effected fuel tank were turned off, a fuel pressure surge (spike) accompanied by a rapid drop in…

## FAA accident and incident reports (8)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20040829020869I](https://openairdocs.org/incident/20040829020869I), Aug 29, 2004: Boeing 717200 (N998AT), Flint, MI, Minor damage. (-23) Around 07:am on August 29, 2004 an air tran aircraft N998AT was taking off from Flint Bishop international airport (fnt). About 20 miles east of fnt the…
- [Incident 20000712034919I](https://openairdocs.org/incident/20000712034919I), Jul 12, 2000: Boeing 72730C (N906UP), Middletown, PA. (-23) The aircraft declared an emergency due to fumes in the cockpit. The aircraft landed on runway 31 at 2303E. The ARFF responded and the aircraft taxied to…
- [Incident 19910930050799I](https://openairdocs.org/incident/19910930050799I), Sep 30, 1991: Boeing 72731C (N923UP), Toluca, Mexico, Minor damage. Aircraft not aligned with center of runway. Elected to go around. Banked and wing tip hit ground. Landed safely.
- [Incident 19900409014359I](https://openairdocs.org/incident/19900409014359I), Apr 9, 1990: Boeing 727180C (N921UP), Des Moines, IA. Gear indication light inoperative. Landed safely. Found 2 downlock target wires broken.
- [Incident 19900409012739I](https://openairdocs.org/incident/19900409012739I), Apr 9, 1990: Boeing 72731C (N926UP), Des Moines, IA, Minor damage. NR2 engine fire warning. Secured and returned. Found bleed air leak at manifold flange. Bolts not safety wired.
- [Incident 19890825047699I](https://openairdocs.org/incident/19890825047699I), Aug 25, 1989: Boeing 72731C (N925UP), Fort Myers, FL. Lost system a hydraulic fluid. Emergency landing. Found flap drive leak on left inboard side.
- [Incident 19860409023529I](https://openairdocs.org/incident/19860409023529I), Apr 9, 1986: Boeing 72727C (N908UP), Omaha, NE. Lost hydraulic pressure on climb. Returned and found crack in casting of sequence valve in left wheel well.
- [Incident 19841211070699I](https://openairdocs.org/incident/19841211070699I), Dec 11, 1984: Boeing 727180C (N921UP), Chicago, IL. Aileron control difficulty after descent from cruise temperature. Suspect moisture in aileron control network.

## Service difficulty reports (56, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR DALA2026010500070](https://openairdocs.org/sdr/DALA2026010500070), Jan 2, 2026: ENGINE. FIRE. 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 
- [SDR DALA2022111507349](https://openairdocs.org/sdr/DALA2022111507349), Nov 13, 2022: ANTI-ICE VALVE. FAULTED. 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. CO
- [SDR CA131115002](https://openairdocs.org/sdr/CA131115002), Nov 14, 2013: TUBE. 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 PERSO
- [SDR CA131107001](https://openairdocs.org/sdr/CA131107001), Nov 6, 2013: CASE. 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
- [SDR N93A07072007A](https://openairdocs.org/sdr/N93A07072007A), Jul 7, 2007: PROBE. FAULTED. LOW FUEL INDICATION AFTER TAKEOFF. REMOVED AND REPLACED FUEL LEVEL LOW SENSOR PROBE.
- [SDR UPS06248626](https://openairdocs.org/sdr/UPS06248626), Nov 14, 2006: INDICATOR. INOPERATIVE. 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 
- [SDR UPS06248627](https://openairdocs.org/sdr/UPS06248627), Nov 14, 2006: LIGHT. MALFUNCTIONED. 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. S
- [SDR UPS06246027](https://openairdocs.org/sdr/UPS06246027), Jan 12, 2006: FLOORBEAM. CORRODED. 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 SR
- [SDR UPS06246011](https://openairdocs.org/sdr/UPS06246011), Jan 10, 2006: CARRIAGE. CORRODED. 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), Jan 10, 2006: CARRIAGE. CORRODED. 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), Jan 10, 2006: BEAM. CORRODED. 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, REM
- [SDR UPS06246085](https://openairdocs.org/sdr/UPS06246085), Jan 10, 2006: ANGLE. CORRODED. 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 REPLAC
- [SDR UPS06246025](https://openairdocs.org/sdr/UPS06246025), Jan 8, 2006: STIFFENER. CORRODED. 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
- [SDR UPS06246026](https://openairdocs.org/sdr/UPS06246026), Jan 8, 2006: STIFFENER. CORRODED. 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 
- [SDR UPS06246014](https://openairdocs.org/sdr/UPS06246014), Jan 6, 2006: SKIN. CORRODED. 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-
- [SDR UPS06246016](https://openairdocs.org/sdr/UPS06246016), Jan 6, 2006: SKIN. CORRODED. 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
- [SDR UPS06246028](https://openairdocs.org/sdr/UPS06246028), Jan 6, 2006: SKIN. CORRODED. 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. CO
- [SDR UPS06246029](https://openairdocs.org/sdr/UPS06246029), Jan 5, 2006: LAP JOINT. CORRODED. 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 APPE
- [SDR UPS06246030](https://openairdocs.org/sdr/UPS06246030), Jan 5, 2006: LAP JOINT. CORRODED. 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 
- [SDR UPS06246032](https://openairdocs.org/sdr/UPS06246032), Jan 5, 2006: SKIN. CRACKED. 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. CARRI
- [SDR UPS06246086](https://openairdocs.org/sdr/UPS06246086), Jan 4, 2006: SKIN. CRACKED. 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 SR
- [SDR UPS05245890](https://openairdocs.org/sdr/UPS05245890), Dec 13, 2005: FLOOR SUPPORT. CRACKED. 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
- [SDR UPS05245848](https://openairdocs.org/sdr/UPS05245848), Nov 30, 2005: LIGHT. INOPERATIVE. 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), Oct 17, 2004: CONTROL UNIT. MALFUNCTIONED. 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
- [SDR UPS04243383](https://openairdocs.org/sdr/UPS04243383), Oct 8, 2004: WEB. CRACKED. 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 CONT
- [SDR UPS04243392](https://openairdocs.org/sdr/UPS04243392), Oct 6, 2004: SKIN. CORRODED. 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), Oct 4, 2004: HINGE. CORRODED. 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 INST
- [SDR UPS04243072](https://openairdocs.org/sdr/UPS04243072), Sep 6, 2004: BATTERY. INOPERATIVE. 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 G
- [SDR UPS04243067](https://openairdocs.org/sdr/UPS04243067), Aug 26, 2004: ATTACH ANGLE. CORRODED. 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), Aug 23, 2004: LIGHT. DEFECTIVE. 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 REPLAC
- [SDR UPS04243068](https://openairdocs.org/sdr/UPS04243068), Aug 23, 2004: STRAP. CORRODED. 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), Aug 23, 2004: STIFFENER. CORRODED. 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. S
- [SDR UPS04243077](https://openairdocs.org/sdr/UPS04243077), Aug 22, 2004: DOUBLER. CRACKED. 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 FO
- [SDR UPS04243009](https://openairdocs.org/sdr/UPS04243009), Aug 17, 2004: FRAME. CRACKED. 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
- [SDR UPS04243062](https://openairdocs.org/sdr/UPS04243062), Aug 17, 2004: SKIN. DEBONDED. 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), Aug 16, 2004: LAP JOINT. CORRODED. 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 
- [SDR UPS04242900](https://openairdocs.org/sdr/UPS04242900), Aug 13, 2004: SWITCH. INOPERATIVE. 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), Aug 13, 2004: SKIN. CORRODED. 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-
- [SDR UPS04243064](https://openairdocs.org/sdr/UPS04243064), Aug 12, 2004: SKIN. CRACKED. 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
- [SDR UPS04243000](https://openairdocs.org/sdr/UPS04243000), Aug 5, 2004: SKIN. DELAMINATED. 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-
- [SDR UPS04243001](https://openairdocs.org/sdr/UPS04243001), Aug 5, 2004: SKIN. DELAMINATED. 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), Aug 4, 2004: SKIN. CRACKED. 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 CR
- [SDR UPS04243008](https://openairdocs.org/sdr/UPS04243008), Aug 4, 2004: WEB. CRACKED. 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-
- [SDR UPS04242999](https://openairdocs.org/sdr/UPS04242999), Aug 2, 2004: HINGE. CRACKED. 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
- [SDR UPS04243015](https://openairdocs.org/sdr/UPS04243015), Jul 7, 2004: WINDOW FRAME. CRACKED. 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), Apr 30, 2002: ENGINE. FAILED. 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 COMPL
- [SDR CA020322003](https://openairdocs.org/sdr/CA020322003), Mar 4, 2002: CAGE. 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
- [SDR UPS02237744](https://openairdocs.org/sdr/UPS02237744), Mar 1, 2002: ENGINE. MALFUNCTIONED. 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), Oct 14, 2001: BULLET. CRACKED. 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
- [SDR CA020509002](https://openairdocs.org/sdr/CA020509002), Apr 30, 2000: GEARBOX. 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. MAIN

All 56: https://openairdocs.org/engine/rolls-royce-tay-651-54/reports.md

## PMA parts (OpenAirDocs) (71, first 50)

Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this engine model on its data sheet, so check the FAA record before relying on it. Newest first.

- [663700-124WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID181194553420250226225454.0001): Packing. Wencor, LLC · PMA PQ1370NM · Replaces 663700-124 · Jan 30, 2025
- [3214684-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID192281819320230914182347.0001): Starter Control Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces L922745 · Mar 22, 2023
- [3505648-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID189961871720230914182346.0001): Starter. Honeywell International Inc. · PMA PQ1222NM · Replaces L922718 · Mar 22, 2023
- [3507226-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID155716632320230914182303.0001): Output Shaft. Honeywell International Inc. · PMA PQ1222NM · Replaces 3507226-1 · Mar 22, 2023
- [3214684-5](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137063836520230914182305.0001): Air Starter Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 3214684-5 · Mar 22, 2023
- [3505648-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID114607307120230914182306.0001): Air Turbine. Honeywell International Inc. · PMA PQ1222NM · Replaces 3505648-2 · Mar 22, 2023
- [3503227-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID110620003420230914182304.0001): Vee Clamp. Honeywell International Inc. · PMA PQ1222NM · Replaces 3503227-1 · Mar 22, 2023
- [NSL870 B1/2](https://drs.faa.gov/browse/excelExternalWindow/D02AEBC7008B811686257D19004F9761.0001): Sealant. Dedicated Packaging, LLC · PMA PQ4210CE · Replaces PRC-DeSoto Sealant Pro Seal 870 B1/2 · Jul 15, 2014
- [NSL870 B2](https://drs.faa.gov/browse/excelExternalWindow/79754D781B68555386257D19004F9769.0001): Sealant. Dedicated Packaging, LLC · PMA PQ4210CE · Replaces PRC-DeSoto Sealant Pro Seal 870 B2 · Jul 15, 2014
- [NSL1428-B1/2](https://drs.faa.gov/browse/excelExternalWindow/F7183CB2BC43F62F86257D1000653FD7.0001): Sealant. Dedicated Packaging, LLC · PMA PQ4210CE · Replaces PRC-DeSoto Sealant PR-1428-B1/2 · Jun 30, 2014
- [NSL1428-B2](https://drs.faa.gov/browse/excelExternalWindow/36A26347DBF38ABB86257D1000653FD8.0001): Sealant. Dedicated Packaging, LLC · PMA PQ4210CE · Replaces PRC-DeSoto Sealant PR-1428-B2 · Jun 30, 2014
- [AS3145P](https://drs.faa.gov/browse/excelExternalWindow/DE1C00CB5E094F1F86257AD7006CF07C.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 162, RTV 162, DOW 3145, RTV 3145 · Dec 9, 2012
- [AS112](https://drs.faa.gov/browse/excelExternalWindow/C9558B7A8E61E26D86257AD7006CF06B.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 112 · Dec 9, 2012
- [AS3145](https://drs.faa.gov/browse/excelExternalWindow/BE764A2C6FEE1C9886257AD7006CF065.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 162, Dow 3145 · Dec 9, 2012
- [AS157](https://drs.faa.gov/browse/excelExternalWindow/B4A82CB1CBF23CF386257AD7006CF063.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 157, Dow 732 · Dec 9, 2012
- [AS106](https://drs.faa.gov/browse/excelExternalWindow/9BF65FF149C49D0D86257AD7006CF09E.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 106, RTV 106 · Dec 9, 2012
- [AS159](https://drs.faa.gov/browse/excelExternalWindow/9BA1992E44EE2E3986257AD7006CF05D.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 159, GE 106, Dow 736 · Dec 9, 2012
- [AS118](https://drs.faa.gov/browse/excelExternalWindow/8DADE792DAB865F186257AD7006CF070.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 118 · Dec 9, 2012
- [AS159](https://drs.faa.gov/browse/excelExternalWindow/6F91E6B11B31244C86257AD7006CF074.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 159, RTV 159, GE 106, RTV 106, Dow… · Dec 9, 2012
- [AS118](https://drs.faa.gov/browse/excelExternalWindow/617664DAA8C4485F86257AD7006CF084.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 118, RTV 118 · Dec 9, 2012
- [AS157](https://drs.faa.gov/browse/excelExternalWindow/4FF3AA8AF56BFB5586257AD7006CF077.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 157, RTV 157, Dow 732, RTV 732 · Dec 9, 2012
- [AS3145](https://drs.faa.gov/browse/excelExternalWindow/4CC01A26D1DC5BD486257AD7006CF079.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 162, RTV 162, DOW 3145, RTV 3145 · Dec 9, 2012
- [AS116](https://drs.faa.gov/browse/excelExternalWindow/4AB87B0DC36E248F86257AD7006CF081.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 116, RTV 116 · Dec 9, 2012
- [AS3145P](https://drs.faa.gov/browse/excelExternalWindow/4365D6FE16FC91EC86257AD7006CF068.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 162, Dow 3145 · Dec 9, 2012
- [AS116](https://drs.faa.gov/browse/excelExternalWindow/2B43C6B50D22E12F86257AD7006CF06C.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 116 · Dec 9, 2012
- [AS112](https://drs.faa.gov/browse/excelExternalWindow/17A2F94467E39E9F86257AD7006CF07F.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 112, RTV112 · Dec 9, 2012
- [AS3145 & AS3145P](https://drs.faa.gov/browse/excelExternalWindow/FD2C033E3F15F47D86257AAD006A780A.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 162, RTV 162, Dow 3145, RTV 3145 · Oct 23, 2012
- [AS159](https://drs.faa.gov/browse/excelExternalWindow/D052D5208644168B86257AAD006A7802.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 159, RTV 159, GE 106, RTV 106, Dow… · Oct 23, 2012
- [AS159](https://drs.faa.gov/browse/excelExternalWindow/BB05AE50D2C4355D86257AAD006A77C2.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 159, GE 106, Dow 736 · Oct 23, 2012
- [AS106](https://drs.faa.gov/browse/excelExternalWindow/AACF134D7566072186257AAD006A784A.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 106, RTV 106 · Oct 23, 2012
- [AS3145](https://drs.faa.gov/browse/excelExternalWindow/90C6AC462D32F1B386257AAD006A77C6.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 162, Dow 3145 · Oct 23, 2012
- [AS118](https://drs.faa.gov/browse/excelExternalWindow/8F5FF0B2D52B579E86257AAD006A7831.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 118, RTV 118 · Oct 23, 2012
- [AS112](https://drs.faa.gov/browse/excelExternalWindow/8E518499870C01D686257AAD006A77CD.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 112 · Oct 23, 2012
- [AS3145P](https://drs.faa.gov/browse/excelExternalWindow/7F996162E046213786257AAD006A77CA.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 162, Dow 3145 · Oct 23, 2012
- [AS116](https://drs.faa.gov/browse/excelExternalWindow/699A146AEFCCFD7786257AAD006A77D0.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 116 · Oct 23, 2012
- [AS112](https://drs.faa.gov/browse/excelExternalWindow/5FFDD126D3F3D3E886257AAD006A780B.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 112, RTV 112 · Oct 23, 2012
- [AS118](https://drs.faa.gov/browse/excelExternalWindow/5EBDAB2435C52CB486257AAD006A77E9.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 118 · Oct 23, 2012
- [AS157](https://drs.faa.gov/browse/excelExternalWindow/2B691205ECAAB3D786257AAD006A7806.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 157, RTV 157, Dow 732, RTV 732 · Oct 23, 2012
- [AS157](https://drs.faa.gov/browse/excelExternalWindow/15839E79F9773F7986257AAD006A77C5.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 157, Dow 732 · Oct 23, 2012
- [AS116](https://drs.faa.gov/browse/excelExternalWindow/06F9202F2290B40986257AAD006A7819.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 116, RTV 116 · Oct 23, 2012
- [AS106](https://drs.faa.gov/browse/excelExternalWindow/BF98A7DB29BD440B862579F400625E1A.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 106, RTV 106 · Apr 30, 2012
- [NSL1428-B2](https://drs.faa.gov/browse/excelExternalWindow/9CDF429324A7A32F862579F400626DC2.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces PRC-DeSoto Sealant PR-1428-B2 · Apr 30, 2012
- [NSL1428-B1/2](https://drs.faa.gov/browse/excelExternalWindow/2A6C84F363F393DB862579F400626D80.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces PRC-DeSoto Sealant PR-1428-B1/2 · Apr 30, 2012
- [S9413-012WE](https://drs.faa.gov/browse/excelExternalWindow/14AB47A2D26843BA862579E300659824.0001): Packing, Preformed - Fluorocarbon. Wencor LLC · PMA PQ1370NM · Replaces S9413-012 · Apr 4, 2012
- [NSL870 B1/2](https://drs.faa.gov/browse/excelExternalWindow/E88CFB0EA4E4036F862578650062C6E3.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces PRC-DeSoto Sealant Pro Seal 870 B1/2 · Mar 22, 2011
- [NSL870 B1/2](https://drs.faa.gov/browse/excelExternalWindow/9F7C8DF7AD73CC2A862576C5004F437C.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces PRC-DeSoto Sealant Pro Seal 870 B1/2 · Jan 31, 2010
- [NSL870 B2](https://drs.faa.gov/browse/excelExternalWindow/41DFFFCCF77FC2D2862576C5004F43B5.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces PRC-DeSoto Sealant Pro Seal 870 B2 · Jan 31, 2010
- [7596674-101](https://drs.faa.gov/browse/excelExternalWindow/E3AAC1F0564432798625767E0057E69A.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces MFFA370/2 APPH · Nov 3, 2009
- [358388-1WD](https://drs.faa.gov/browse/excelExternalWindow/2A8E509367F8B810862570F30068161F.0001): Bearing, Ball, Annular. Wencor LLC (formerly Dixie Aerospace LLC) · PMA PQ1630CE · Replaces Honeywell 358388-1 · Dec 19, 2005
- [358452-1WD](https://drs.faa.gov/browse/excelExternalWindow/C6872863E5DA76A0862570F30067DF05.0001): Bearing, Ball, Annular. Wencor LLC (formerly Dixie Aerospace LLC) · PMA PQ1630CE · Replaces Honeywell 358452-1 · Dec 9, 2005

All of them: https://openairdocs.org/engine/rolls-royce-tay-651-54/pma.md

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