# Rolls-Royce TAY-650-15

- Type: Engine model (FAA registry)
- Registry code: 54557
- Manufacturer (registry): ROLLS-ROYC
- Model: TAY 650-15
- Engine type: Turbo-fan
- Power: 15,100 lb thrust
- Data sheet: [TCDS E25NE](https://openairdocs.org/tcds/E25NE) (OpenAirDocs)
- Holder: Rolls-Royce Deutschland Ltd & Co KG
- Installed in: 0 registered aircraft
- Page: https://openairdocs.org/engine/rolls-royce-tay-650-15

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 2022-26-05](https://openairdocs.org/ad/2022-26-05): Turbine Engine Combustion Section · Rolls-Royce Deutschland TAY 620-15 and TAY 650-15. Effective Jan 12, 2023
- [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 2013-06-01](https://openairdocs.org/ad/2013-06-01): Low-pressure compressor (LPC) rotor disc assemblies · Rolls-Royce Deutschland TAY 620-15 and TAY 650-15. Effective Apr 24, 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 2003-08-01](https://openairdocs.org/ad/2003-08-01): Rotor discs · Rolls-Royce Deutschland TAY 650-15. Effective May 20, 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 2009-22-01](https://openairdocs.org/ad/2009-22-01) (historical): Low-pressure turbine disk stage 2 or stage 3 · Rolls-Royce Deutschland TAY 650-15. Effective Nov 12, 2009
- [AD 2008-10-14](https://openairdocs.org/ad/2008-10-14) (historical): Excessively corroded low pressure turbine disks stage 2 and stage 3 · Rolls-Royce Deutschland TAY 650-15. Effective Jun 25, 2008
- [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 2002-24-06](https://openairdocs.org/ad/2002-24-06) (historical): Low pressure (LP) fuel tubes · Rolls-Royce Deutschland TAY 620-15 and TAY 650-15. Effective Dec 18, 2002
- [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
- [AD 2000-08-01](https://openairdocs.org/ad/2000-08-01) (historical): Turbine Disks · Rolls-Royce Deutschland TAY 650-15. Effective Jun 19, 2000

## Registered aircraft

None registered with this engine model now.

## NTSB investigations (14)

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 NYC03FA190](https://openairdocs.org/ntsb/NYC03FA190), Sep 4, 2003: Fokker F.28 Mk 0100 (N1450A), Flushing, NY, substantial damage. Probable cause: An in-flight collision with birds.
- [NTSB CHI02IA270](https://openairdocs.org/ntsb/CHI02IA270), Sep 5, 2002: Fokker 100 (N1473K), Minneapolis, MN, incident, minor damage. Probable cause: The improper installation of the #2 main landing gear wheel, including the axle nut not being properly torqued and safetied, which resulted in the wheel separation during takeoff.
- [NTSB FTW02LA088](https://openairdocs.org/ntsb/FTW02LA088), Mar 6, 2002: Fokker F-28 MK-100 (N1425A), Dallas, TX, substantial damage. Probable cause: The ground crew inadvertent application of deicing fluid in the auxiliary power unit resulting in an overspeed and turbine wheel burst. A contributing factor was the gusty wind.
- [NTSB FTW01FA127](https://openairdocs.org/ntsb/FTW01FA127), May 23, 2001: Fokker F28 Mk 0100 (N1419D), DFW Airport, TX, substantial damage. Probable cause: A forging fold that was introduced during the manufacture of the right main landing, which resulted in a fatigue crack in the right main landing gear cylinder, and its subsequent failure during…
- [NTSB CHI01IA102](https://openairdocs.org/ntsb/CHI01IA102), Mar 6, 2001: Fokker F28 MK 0100 (N1426A), Montreal, Canada, incident, minor damage. Probable cause: the inaccurate aircraft deicing service the ground personnel performed alowing fluid injestion and the auxiliary power unit's turbine failure while standing. A factor was the auxiliary power unit's…
- [NTSB NYC00IA231](https://openairdocs.org/ntsb/NYC00IA231), Aug 17, 2000: Fokker F-100 (N860US), Norfolk, VA, incident, no damage. Probable cause: The failure of the airplane's ground/flight switch and a malfunction of the thrust reverser deploy switch, which resulted in an in-flight thrust reverser deployment.
- [NTSB CHI00LA076](https://openairdocs.org/ntsb/CHI00LA076), Feb 21, 2000: Fokker F28 MK100 (N1403M), Chicago, IL, substantial damage. Probable cause: the driver of the refueling truck fell asleep which resulted in him not maintaining clearance with the parked aircraft. Factors associated with the accident were severe obstructive sleep apnea and…
- [NTSB CHI98LA154](https://openairdocs.org/ntsb/CHI98LA154), May 13, 1998: Fokker F-28 MK100 (N1400H), Ft. Wayne, IN, no damage. Probable cause: In-flight encounter with turbulence.
- [NTSB NYC98LA075](https://openairdocs.org/ntsb/NYC98LA075), Mar 12, 1998: Fokker F-100 (N863US), Philadelphia, PA, substantial damage. Probable cause: The driver's failure to maintain clearance from the parked airplane. Related factors were night conditions and the driver's diverted attention.
- [NTSB MIA98FA089](https://openairdocs.org/ntsb/MIA98FA089), Feb 26, 1998: Fokker F28 MK 0100 (N867US), Birmingham, AL, substantial damage. Probable cause: Were the 1) the inoperative alternate anti-skid control valve due to the disconnected electrical connector on the parking brake shut-off valve, the area was inspected 2 days earlier 2) the total loss…
- [NTSB MIA98FA025](https://openairdocs.org/ntsb/MIA98FA025), Nov 7, 1997: Fokker F100 (N865US), Charlotte, NC, substantial damage. Probable cause: Improper written instructions (job/task card) by company maintenance personnel. The procedures did not reflect the correct manufactures maintenance manual servicing procedure, and did not ensure that…
- [NTSB ATL94IA088](https://openairdocs.org/ntsb/ATL94IA088), May 1, 1994: Fokker F28 MK 0100 (N890US), Charlotte, NC, incident, minor damage. Probable cause: THE IMPROPER RIGGING OF THE NOSE WHEEL STEERING SYSTEM BY COMPANY MAINTENANCE PERSONNEL.
- [NTSB BFO93IA070](https://openairdocs.org/ntsb/BFO93IA070), May 7, 1993: Fokker F28-MK-0100 (N867US), Pittsburgh, PA, incident, minor damage. Probable cause: THE IMPROPER INSTALLATION OF THE SPACERS BY THE MECHANIC AND THE UNCLEAR INFORMATION SUPPLIED FROM THE MANUFACTURER AND OPERATOR REGARDING THE INSTALLATION OF THE SPACERS.
- [NTSB CHI93IA110](https://openairdocs.org/ntsb/CHI93IA110), Mar 13, 1993: Fokker 100 (N895US), Chicago, IL, incident, minor damage. Probable cause: FAILURE OF THE COMPANY STATION MANAGER TO FOLLOW PROPER DISPATCH PROCEDURES, AND ICE ACCUMULATION ON THE NOSE GEAR LOCKING MECHANISM. FACTORS RELATED TO THE INCIDENT WERE: WET SNOW (SLUSH) ON THE…

## FAA accident and incident reports (94, newest 50)

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 20030924030729I](https://openairdocs.org/incident/20030924030729I), Sep 24, 2003: Fokker F28MK0100 (N1466A), Buffalo, NY. (-23) On September 24, 2003, at 2040 EST, American airline, flt. 1485 Fokker 100, landed at the Buffalo airport, Buffalo, NY after reporting a vibration in the…
- [Accident 20030904021109A](https://openairdocs.org/incident/20030904021109A), Sep 4, 2003: Fokker F28MK0100 (N1450A), New York, NY, Substantial damage. (-23) On September 04, 2003, at 0624E, American airlines flight 549, a Fokker-28-MK100, registration number N1450A (2CG), serial number 11459, departed on…
- [Incident 20030708019089I](https://openairdocs.org/incident/20030708019089I), Jul 8, 2003: Fokker F28MK0100 (N1414D), Chicago, IL, Substantial damage. (-23) On July 8, 2003, at 12:30 central standard time, an American airlines F-100 aircraft, N1414D, was parked at gate H-12 at o'Hare international airport in…
- [Incident 20020912027199I](https://openairdocs.org/incident/20020912027199I), Sep 12, 2002: Fokker F28MK0100 (N1455K), Omaha, NE. (-23) American airline flight 1718, F-28-MK0100, was being pushed back from the gate at Omaha, NE, when the number one engine starter failed during atempt to…
- [Incident 20020905029409I](https://openairdocs.org/incident/20020905029409I), Sep 5, 2002: Fokker F28MK0100 (N1473K), Chicago, IL, Minor damage. (-23) On Thursday September 05, 2002 an inspector from the o'Hare flight standards district office (FSDO) received a telephone call from the amrcmo pmi terry…
- [Incident 20020620036109I](https://openairdocs.org/incident/20020620036109I), Jun 20, 2002: Fokker F28MK0100 (N1460A), Memphis, TN. (-23) American airlines, flight #2069, registration N1460, F-28 Fokker, flight plan cvg-dfw, diverted into mem, declaring an emergency. The number one engine…
- [Incident 20020610011909I](https://openairdocs.org/incident/20020610011909I), Jun 10, 2002: Fokker F28MK0100 (N1461C), Chicago, IL, Minor damage. (-23) On June 10, 2002 the o'hare (FSDO) flights standards district office received a notice by fax from the great lakes operation center. The notice was that…
- [Incident 20020409035729I](https://openairdocs.org/incident/20020409035729I), Apr 9, 2002: Fokker F28MK0100 (N1411G), Chicago, IL, Minor damage. (.23) Notified by o'Hare city operations of the following incident: an American airlines Fokker-100, N1411G, flight 1949, blew four main landing gear tires…
- [Accident 20020306003829A](https://openairdocs.org/incident/20020306003829A), Mar 6, 2002: Fokker F28MK0100 (N1425A), Dallas-Ft Worth, TX, No damage. (-23) During deicing at dfw type I deicing fluid and possibly ice runoff was ingested into the APU inlet. The substance ingested caused the APU to overspeed…
- [Incident 20011011027249I](https://openairdocs.org/incident/20011011027249I), Oct 11, 2001: Fokker F28MK0100 (N851US), Louisville, KY, Minor damage. (-23) No narrative.
- [Accident 20010523009809A](https://openairdocs.org/incident/20010523009809A), May 23, 2001: Fokker F28MK0100 (N1419D), Dallas-Ft Worth, TX, No damage. (-23)On may 23, 2001, at approximately 304 pm CDT, during the landing roll-out phase of flight on runway 17 center at the Dallas/fort Worth, Texas airport…
- [Incident 20001229037789I](https://openairdocs.org/incident/20001229037789I), Dec 29, 2000: Fokker F28MK0100 (N861US), Middletown, PA. (-23) Pilot reported that "going through 1000 ft AGL, aircraft pitched up to approx. 25 degrees nose up. Airspeed started bleeding off. Disconnected autopilot.…
- [Incident 20000817026129I](https://openairdocs.org/incident/20000817026129I), Aug 17, 2000: Fokker F28MK0100 (N860US), Norfolk, VA. (-23) On 8/17/2000 at 1522 EDT, a U.S. Airways flight 471 was enroute from lga to ric, when flight 471 diverted to orf and landed on runway 05 after the left…
- [Incident 20000726036039I](https://openairdocs.org/incident/20000726036039I), Jul 26, 2000: Fokker F28MK0100 (N855US), Syracuse, NY. (-23)On Wednesday, July 26, 2000, U.S. Airways flight 1802, an F-100, N855US, was enroute from pittsburg, pa (pit) to new york, NY (lga) when the crew noted a…
- [Accident 20000221017949A](https://openairdocs.org/incident/20000221017949A), Feb 21, 2000: Fokker F28MK0100 (N1403M), Chicago, IL, Substantial damage. (.4)They reported seeing the refueling truck parked at a 45 degree angle to the lead in line on the right side of the airplane. The truck then moved forward…
- [Incident 19990924029159I](https://openairdocs.org/incident/19990924029159I), Sep 24, 1999: Fokker F28MK0100 (N1417D), Little Rock, AR. (-23) On September 24, 1999, at 0915 CDT, N1417D, a Fokker F-28-MK0100, registered to and operated by American airline as flight 526, enroute from dfw to sdf,…
- [Incident 19990807029949I](https://openairdocs.org/incident/19990807029949I), Aug 7, 1999: Fokker F28MK0100 (N1468A), Minneapolis, MN. (-23) After takeoff and gear retraction, nose gear light failed to go out. Gear cycled, light remained on. Reseated and relamped, operation check normal.
- [Incident 19990803024279I](https://openairdocs.org/incident/19990803024279I), Aug 3, 1999: Fokker F28MK0100 (N889US), Nashville, TN. At cruise flight about 40 miles east of Nashville, TN, the captain, first officer and jumpseat rider all smelled noxious smoke smell. After crew troubleshot…
- [Incident 19990722032619I](https://openairdocs.org/incident/19990722032619I), Jul 22, 1999: Fokker F28MK0100 (N1427A), Middletown, PA. (-23) The #1 hydraulic system low quantity light came on in cruise at FL29. A non-eventful landing was made at the destination airport, Middletown (MDT).…
- [Incident 19990713023619I](https://openairdocs.org/incident/19990713023619I), Jul 13, 1999: Fokker F28MK0100 (N855US), Buffalo, NY. (-23) On Tuesday, July 13, 1999, at 1842 local, a usairways F100, N855US, reported a flap asymmetry problem inbound to Buffalo niagara airport. The aircraft…
- [Incident 19990627022709I](https://openairdocs.org/incident/19990627022709I), Jun 27, 1999: Fokker F28MK0100 (N859US), Raleigh-Durham, NC, Minor damage. During pushback from jetway at rdu, the horizontal stabilizer of usaa 460 (N859) contacted the horizontal stabilizer of usa 1282 (N897) parked at an adjacent…
- [Incident 19990626023629I](https://openairdocs.org/incident/19990626023629I), Jun 26, 1999: Fokker F28MK0100 (N862US), Buffalo, NY. (-23) On Saturday, June 26, 1999, a usairways Fokker F100, N862US, diverted to Buffalo niagra international airport after reporting smoke puffs above the…
- [Incident 19990626022859I](https://openairdocs.org/incident/19990626022859I), Jun 26, 1999: Fokker F28MK0100 (N867US), Wilmington, NC, Minor damage. (-23) On June 26, 1999 at 18:10 EST a usairways F-28-MK0100 experienced a left main brake fire on landing at ilm. Once aircraft came to a stop airport fire…
- [Incident 19990625022119I](https://openairdocs.org/incident/19990625022119I), Jun 25, 1999: Fokker F28MK0100 (N1468A), Wichita, KS. Aircraft N1468A diverted to ict due to low oil quantity #1 hydraulic system. Reservoir was serviced and the system was inspected. It was determined that the…
- [Incident 19990609029939I](https://openairdocs.org/incident/19990609029939I), Jun 9, 1999: Fokker F28MK0100 (N1460A), Sioux Falls, SD. (-23) While N1460A was enroute from msp to dfw, flight attendant advised cockpit crew that something was burning in the galley, smoke and source could not be…
- [Incident 19990521021819I](https://openairdocs.org/incident/19990521021819I), May 21, 1999: Fokker F28MK0100 (N882US), South Bend, IN, Minor damage. (From .19 this incident was investigated by NTSB) on may 21, 1999, at 1207 eastern standard time, a Fokker F-100, N882US, operated by us airways, incorporated,…
- [Incident 19990328021369I](https://openairdocs.org/incident/19990328021369I), Mar 28, 1999: Fokker F28MK0100 (N885US), Indianapolis, IN. On taxi out, the pilot felt a vibration like a nose tire out of balance. When they were turning to return to the gate, the right inboard tire departed aircraft.
- [Incident 19990315021399I](https://openairdocs.org/incident/19990315021399I), Mar 15, 1999: Fokker F28MK0100 (N896US), Indianapolis, IN. On 3/15/99 at 0135 local time a us airways F-28, N896US flight 569 enroute to ind from lga experienced nose gear indication problem on approach to ind. The…
- [Incident 19990124009959I](https://openairdocs.org/incident/19990124009959I), Jan 24, 1999: Fokker F28MK0100 (N1461C), Charlotte, NC, Minor damage. The half couplings that connect the hydraulic supply/return lines to the brake shuttle valve were found to have worn teeth on brake #3 preventing a positive…
- [Incident 19980910035789I](https://openairdocs.org/incident/19980910035789I), Sep 10, 1998: Fokker F28MK0100 (N888AU), Norfolk, VA. Usair flt 1041 departed Norfolk (orf) 09:46 1C1 en route to pittsburg (pit). After rotation a no. 2 engine fire light illuminated. The crew shut down the no. 2…
- [Incident 19980530023209I](https://openairdocs.org/incident/19980530023209I), May 30, 1998: Fokker F28MK0100 (N1458H), Rochester, NY. Aircraft struck a deer on takeoff. Circled field and landed uneventfully.
- [Accident 19980513046339A](https://openairdocs.org/incident/19980513046339A), May 13, 1998: Fokker F28MK0100 (N1400H), Ft. Wayne, IN. (.4)The #1 flight attendant suffered a fractured ankle when she got up from a passenger seat to answer the interphone during moderate turbulence. The captain…
- [Accident 19980311024789A](https://openairdocs.org/incident/19980311024789A), Mar 11, 1998: Fokker F28MK0100 (N863US), Philadelphia, PA, Substantial damage. (.4)After the airplane was pushed back from the gate at night, a fuel truck travelling eastbound on the outer service road struck the left wing tip of the…
- [Accident 19980226007449A](https://openairdocs.org/incident/19980226007449A), Feb 26, 1998: Fokker F28MK0100 (N867US), Birmingham, AL, Substantial damage. Lightning strike on final. Blew holes in hydro system lines. Alternate used blew tires ldg. Nose gear sheared off. (.4)while flying in precipitation deviating…
- [Accident 19971107032609A](https://openairdocs.org/incident/19971107032609A), Nov 7, 1997: Fokker F28MK0100 (N865US), Charlotte, NC, Substantial damage. Right main laning gear attach fittings failed on landing roll. (.4)the Fokker F100 was on landing rollout when the right main landing gear collapsed. Review of…
- [Incident 19971104035589I](https://openairdocs.org/incident/19971104035589I), Nov 4, 1997: Fokker F28MK0100 (N1410E), Albany, NY, Minor damage. Narrative: #2 engine tailpipe fire indication during engine start crew attempted to blow out fire by re-energizing starter motor. Via radio, adjacent aircraft…
- [Incident 19970423011509I](https://openairdocs.org/incident/19970423011509I), Apr 23, 1997: Fokker F28MK0100 (N864US), Buffalo, NY. Narrative: on April 23, 1997, at 1530 EST, a Fokker 28, N864US, flight 821, operated by us airways, during the takeoff phase from Buffalo international airport…
- [Incident 19970305007289I](https://openairdocs.org/incident/19970305007289I), Mar 5, 1997: Fokker F28MK0100 (N859US), Middletown, PA, Minor damage. Narrative: on March 5, 1997, at 1855 hours a Fokker 28, model MK0100, registration number 859US, registered to us air inc, and made an emergency landing at the…
- [Incident 19961018038599I](https://openairdocs.org/incident/19961018038599I), Oct 18, 1996: Fokker F28MK0100 (N852US), Elmira, NY. After departure from 1th, at 12,000 ft., during a left turn, the fuel totalizer was fluctuating. A precautionary, diverted landing was made in Elmira. Found no…
- [Incident 19960921037869I](https://openairdocs.org/incident/19960921037869I), Sep 21, 1996: Fokker F28MK0100 (N887US), Pittsburgh, PA. Narrative: when descending into pit at approximately 50 NM southeast of the airport, the crew got an emergency DC bus failure message on the multi-function…
- [Incident 19960821028169I](https://openairdocs.org/incident/19960821028169I), Aug 21, 1996: Fokker F28MK0100 (N852US), Atlanta, GA. Narrative: us air 1184 was enroute from new orleans to bwi. When just north of mgm, a female passenger seated in 13A showed a message written on the inside of…
- [Incident 19960727025329I](https://openairdocs.org/incident/19960727025329I), Jul 27, 1996: Fokker F28MK0100 (N889US), Syracuse, NY. Narrative: usaa flight 1052 enroute from pwm to pit diverted to syr with a cracked windshield. The aircraft landed without incident. Usaa maintenance in syr…
- [Incident 19960625024359I](https://openairdocs.org/incident/19960625024359I), Jun 25, 1996: Fokker F28MK0100 (N858US), Wilmington, NC, Minor damage. Narrative: on June 25, 1996, usair flight 909, a Fokker F-28-100, N858US, with richard w. kozel as PIC and george e. pence as SIC, landed at Wilmington, NC…
- [Incident 19960621021899I](https://openairdocs.org/incident/19960621021899I), Jun 21, 1996: Fokker F28MK0100 (N851US), Pittsburgh, PA, Minor damage. Narrative: on June 21, 1996, usair aircraft N851US, a F28MK0100, departed Pittsburgh international airport as flight 1050. At lift off, flight crew felt slight…
- [Incident 19960619019639I](https://openairdocs.org/incident/19960619019639I), Jun 19, 1996: Fokker F28MK0100 (N896US), Kansas City, MO. Narrative: on 06/19/96, usair flight 1193 departed phl for mci. En route the captains EFIS lighting failed. The first officer EFIS lighting remained…
- [Incident 19960314007779I](https://openairdocs.org/incident/19960314007779I), Mar 14, 1996: Fokker F28MK0100 (N852US), Kansas City, MO. Narrative: on 3/14/96, USA734 aborted takeoff from mci. The aircrew experienced a thrust reverser unlock light on the #2 engine. The aircraft was returned to…
- [Incident 19960222007029I](https://openairdocs.org/incident/19960222007029I), Feb 22, 1996: Fokker F28MK0100 (N869US), Charlotte, NC, Minor damage. Narrative: after takeoff from raleigh-durham international airport (rdu), the crew was unable to retract landing gear. Rdu ATCT reported that there was debris…
- [Incident 19960212030369I](https://openairdocs.org/incident/19960212030369I), Feb 12, 1996: Fokker F28MK0100 (N1410E), Atlanta, GA, Minor damage. Narrative: when aa flight 752 arrived at gate T-13 at atl, there was a marshaller and two wing walkers directing the plane to its parking spot. The left wing…
- [Incident 19960120001839I](https://openairdocs.org/incident/19960120001839I), Jan 20, 1996: Fokker F28MK0100 (N1417D), Rochester, NY. Narrative: on January 20, 1996, at 0955 EST, a folker, FK28, N1417D, operated by American airlines, during descent phase of flight to Rochester international…
- [Incident 19960103001239I](https://openairdocs.org/incident/19960103001239I), Jan 3, 1996: Fokker F28MK0100 (N890US), Pittsburgh, PA, Minor damage. Narrative: on January 3, 1996, at 1520 EST a usair F28MK0100, N890US, lost the left outboard wheel and brake assembly while departing Pittsburgh international…

All 94: https://openairdocs.org/engine/rolls-royce-tay-650-15/incidents.md

## Service difficulty reports (164, newest 50)

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

- [SDR 2010FA0000216](https://openairdocs.org/sdr/2010FA0000216), Sep 9, 2009: TURBINE BLADES. FRACTURED. THE REPORT SUGGEST THAT THE LPT3 BLADE HAD FRACTURED IN HIGH CYCLE FATIGUE THAT HAD PROPAGATED FROM AN INTERGRANULAR CRACK ON THE AIRFOIL T/E.
- [SDR CA070109005](https://openairdocs.org/sdr/CA070109005), Nov 8, 2006: VALVE. MALFUNCTIONED. (CAN) DATE OF DELAY NOV 8, 2006 CADORS NR: 2006C2915. THE FLIGHT CREW WAS NOTIFIED THAT DURING TAXI FOR DEPARTURE FUEL WAS LEAKING FROM LT WING. AIRCRAFT TAXIED
- [SDR CA070110005](https://openairdocs.org/sdr/CA070110005), Oct 9, 2006: WARNING SYSTEM. MALFUNCTIONED. (CAN) THE REFERENCED AIRCRAFT AN EVENT INVOLVING THE AUTOMATIC SILENCING OF CABIN CHIMES. NORMALLY THE FLIGHT CREW WILL ADVISE THE FLIGHT ATTENDANTS TO TAKE THE
- [SDR CA060919005](https://openairdocs.org/sdr/CA060919005), Sep 10, 2006: ACTUATOR. MALFUNCTIONED. (CAN) FLIGHT CREW REPORTED THAT THE SPEED BRAKE WOULD NOT RETRACT UPON SELECTION TO DO SO. FOLLOWING LANDING. BOTH PADDLES CONFIRMED OPEN. AIRCRAFT WAS FERRIED 
- [SDR AU510001439](https://openairdocs.org/sdr/AU510001439), Dec 12, 2005: MICROPHONE. FAULTY. (AUS) HAND MICROPHONE SWITCH STICKING.(OTHER CAUSE: STICKY SWITCH - MATERIAL ) (CASA# 510001439)
- [SDR AU510001481](https://openairdocs.org/sdr/AU510001481), Dec 12, 2005: NIPPLE. MISSING. (AUS) FLAP BALL NUT GREASE NIPPLE MISSING.(OTHER CAUSE: UNKNOWN ) (CASA# 510001481)
- [SDR AU510001497](https://openairdocs.org/sdr/AU510001497), Dec 12, 2005: STRUT. FAULTY. LT MAIN LANDING GEAR STRUT INTERNAL SLEEVE MIGRATED OUT OF POSITION AND BLOCKED BLEED PLUG HOLE, FOUND DURING INSPECTION IAW AD/F100/64.
- [SDR AU510001498](https://openairdocs.org/sdr/AU510001498), Dec 12, 2005: STRUT. CRACKED. RT MAIN LANDING GEAR STRUT BLEED PORT CRACKED, FOUND DURING INSPECTION IAW AD/F100/64.
- [SDR AU510001521](https://openairdocs.org/sdr/AU510001521), Dec 12, 2005: IGNITER. FAILED. APU IGNITER PLUG FAILED. WORKSHOP INVESTIGATION FOUND THAT ONLY APPARENT FAULT WAS SLIGHT SOILING ON THE CERAMIC INSIDE OF THE CONNECTOR END OF THE IGNITER. THE
- [SDR AU510001534](https://openairdocs.org/sdr/AU510001534), Dec 12, 2005: CONNECTOR. LOOSE. ENGINE INDICATION SYSTEM PRESSURE BULKHEAD CONNECTOR P2874 LOOSE.
- [SDR AU510001540](https://openairdocs.org/sdr/AU510001540), Dec 12, 2005: PRESSURE SWITCH. FAULTY. RT ENGINE LP FUEL PRESSURE SWITCH FAULTY.
- [SDR AU510001648](https://openairdocs.org/sdr/AU510001648), Dec 12, 2005: PITOT HEAD. FAULTY. NR 3 PITOT HEAD HEATING SYSTEM FAILED.
- [SDR AU510001654](https://openairdocs.org/sdr/AU510001654), Dec 12, 2005: BEARING. WORN. LT ENGINE INLET GUIDE VANE BEARINGS PNO UP60336 (1OFF) AND PNO EU61711 (2OFF) WORN. FOUND DURING INSPECTION IAW SB TAY-75-1655.
- [SDR AU510001655](https://openairdocs.org/sdr/AU510001655), Dec 12, 2005: CONNECTOR. LEAKING. CREW OXYGEN MASK BOX ASSEMBLY CONNECTOR LEAKING. LOSS OF OXYGEN.
- [SDR AU510001667](https://openairdocs.org/sdr/AU510001667), Dec 12, 2005: SMOKE DETECTOR. FAULTY. REPORT OF CIGARETTE SMOKE SMELL IN CABIN. TOILET SMOKE DETECTOR DID NOT ACTIVATE ALARM. INVESTIGATION CONTINUING.
- [SDR AU510001721](https://openairdocs.org/sdr/AU510001721), Dec 12, 2005: HOSE. FAILED. LT TOILET SMOKE DETECTOR TO AIR EJECTOR HOSE SPLIT AT EJECTOR END. RT SMOKE DETECTOR TO AIR EJECTOR TUBE SIDEWALL COLLAPSED. HOSES ALLOW FOR AIRFLOW THROUGH SMO
- [SDR AU510001726](https://openairdocs.org/sdr/AU510001726), Dec 12, 2005: PIPE. FRACTURED. HYDRAULIC PIPE LOCATED ON THE FORWARD WALL OF THE REAR CARGO HOLD LEAKING. INVESTIGATION FOUND A FRACTURED FLARE. PIPE WAS A -4 STAINLESS STEEL TYPE.
- [SDR AU510001740](https://openairdocs.org/sdr/AU510001740), Dec 12, 2005: EXCITER. FAULTY. APU IGNITION EXCITER UNIT FAULTY.
- [SDR AU510001751](https://openairdocs.org/sdr/AU510001751), Dec 12, 2005: FUEL CONTROL. FAILED. (AUS) APU AUTO-SHUTDOWN IN FLIGHT. INVESTIGATION FOUND A FAULTY FUEL CONTROL UNIT. (CASA NR 510001751)
- [SDR AU510001802](https://openairdocs.org/sdr/AU510001802), Dec 12, 2005: MOTOR. SHEARED. APU STARTER MOTOR DRIVE SHAFT SHEARED.
- [SDR AU510001804](https://openairdocs.org/sdr/AU510001804), Dec 12, 2005: BOLT. BROKEN. NR 2 MAIN WHEEL TIE BOLT BROKEN. BOLT HEAD MISSING. INVESTIGATION CONTINUING.
- [SDR AU510001805](https://openairdocs.org/sdr/AU510001805), Dec 12, 2005: IRU. FAILED. NR 2 INERTIAL REFERENCE UNIT (IRU) INTERMITTENTLY FAILS CODE 2. INVESTIGATION CONTINUING.
- [SDR AU510001887](https://openairdocs.org/sdr/AU510001887), Dec 12, 2005: SWITCH. FAULTY. NR 1 ENGINE ANTI-ICE SWITCH FAULTY.
- [SDR AU510001903](https://openairdocs.org/sdr/AU510001903), Dec 12, 2005: DRIVE SHAFT. SHEARED. (AUS) APU STARTER MOTOR DRIVESHAFT SHEARED. INVESTIGATION FOUND THAT THE BROKEN END WAS JAMMED IN THE CLUTCH ASSEMBLY. (CASA NR 510001903)
- [SDR AU510001914](https://openairdocs.org/sdr/AU510001914), Dec 12, 2005: BOLT. LOOSE. (AUS) LT AILERON TAB OB HINGE BRACKET ATTACHMENT BOLTS LOOSE. BOLTS WERE THREADBOUND IN ANCHOR NUTS. INVESTIGATION FOUND INCORRECT BOLTS WERE FITTED BY A PREVIO
- [SDR AU510001915](https://openairdocs.org/sdr/AU510001915), Dec 12, 2005: CONTROL CABLE. MISRIGGED. (AUS) CONTROL CABLES FOR FLAPS ( F1 AND F2) WERE FOUND TO BE 43LB LOW IN TENSION. THE LT AILERON WING CABLE WAS 30LB LOW. THE LT AND RT AILERON UPFLOAT CABLES W
- [SDR AU510001923](https://openairdocs.org/sdr/AU510001923), Dec 12, 2005: COOLING FAN. FAULTY. (AUS) AVIONICS COOLING FAN NOISY IN OPERATION.
- [SDR AU510001935](https://openairdocs.org/sdr/AU510001935), Dec 12, 2005: STRINGER. CORRODED. NR 3 LT STRINGER LOCATED AT STN 13851 IN THE FORWARD CARGO COMPARTMENT CORRODED.
- [SDR AU510001947](https://openairdocs.org/sdr/AU510001947), Dec 12, 2005: SHUTOFF VALVE. FAILED. LT ENGINE ANTI-ICE PRESSURE REGULATING AND SHUTOFF VALVE (PRSOV) FAILED.
- [SDR AU510001948](https://openairdocs.org/sdr/AU510001948), Dec 12, 2005: MOTOR. FAULTY. FUEL SYSTEM RT CROSS FLOW VALVE MOTOR FAULTY. VALVE STUCK IN CLOSED POSITION.
- [SDR AU510002018](https://openairdocs.org/sdr/AU510002018), Dec 12, 2005: IGNITER. WORN. NR 2 ENGINE IGNITER WORN.
- [SDR AU510002019](https://openairdocs.org/sdr/AU510002019), Dec 12, 2005: SOLENOID. FAULTY. NR 2 ENGINE THRUST REVERSER INTERMITTENT WARNING. INVESTIGATION FOUND THE SECONDARY LOCK SOLENOID HAD A FAULTY INTERNAL SWITCH.
- [SDR AU510002024](https://openairdocs.org/sdr/AU510002024), Dec 12, 2005: FAIRING. CRACKED. ENGINE EXHAUST SPOKE FAIRING CRACKED IN TWO PLACES AT THE 7:30 O`CLOCK AND 9 O`CLOCK POSITIONS.
- [SDR AU510002107](https://openairdocs.org/sdr/AU510002107), Dec 12, 2005: SHUTOFF VALVE. FAULTY. RT BLEED AIR PRESSURE REGULATING AND SHUTOFF VALVE (PRSOV) FAULTY.
- [SDR AU510002112](https://openairdocs.org/sdr/AU510002112), Dec 12, 2005: TRANSPONDER. FAILED. NR 2 ATC TRANSPONDER FAILED. INVESTIGATION CONTINUING.
- [SDR AU510002116](https://openairdocs.org/sdr/AU510002116), Dec 12, 2005: CONTROL PANEL. FAULTY. NR 2 ATC TRANSPONDER SYSTEM CONTROL PANEL DISPLAY DIGITS NOT VISIBLE.
- [SDR AU510002130](https://openairdocs.org/sdr/AU510002130), Dec 12, 2005: OXYGEN BOTTLE. LEAKING. COCKPIT OXYGEN BOTTLE LEAKING FROM VALVE.
- [SDR AU510001987](https://openairdocs.org/sdr/AU510001987), Dec 10, 2005: IGNITER. FAILED. NR 1 ENGINE IGNITER PLUG FAILED.
- [SDR AU510001988](https://openairdocs.org/sdr/AU510001988), Dec 10, 2005: APU. FAILED. APU AUTO SHUTDOWN. INVESTIGATION COULD FIND NO FAULTS. DURING TEST FLIGHT THE APU AGAIN SHUT DOWN. INVESTIGATION CONTINUING.
- [SDR AU510001708](https://openairdocs.org/sdr/AU510001708), Dec 8, 2005: APU. INOPERATIVE. APU FAILED TO START. INVESTIGATION CONTINUING.
- [SDR AU510001579](https://openairdocs.org/sdr/AU510001579), Dec 7, 2005: SHUTOFF VALVE. FAULTY. (AUS) PNEUMATIC SYSTEM PRESSURE REGULATING SHUTOFF VALVE (PRSOV) FAULTY. (CASA NR 510001579)
- [SDR AU510001587](https://openairdocs.org/sdr/AU510001587), Dec 7, 2005: COMPUTER. FAULTY. (AUS) AUTOPILOT COMPUTER SUSPECT FAULTY. (CASA NR 510001587)
- [SDR AU510001588](https://openairdocs.org/sdr/AU510001588), Dec 7, 2005: SLIDE. FAULTY. (AUS) RT ESCAPE SLIDE FAILED TO DEPLOY CORRECTLY. FOLLOWING MANUAL OPERATION THE SLIDE INFLATED BUT WAS NOT CORRECTLY ORIENTATED TO THE DOOR OPENING. SUSPECT CA
- [SDR AU510002078](https://openairdocs.org/sdr/AU510002078), Nov 11, 2005: LINE. CRACKED. (AUS) HYDRAULIC PIPE CRACKED AND LEAKING. LOSS OF HYDRAULIC FLUID. (CASA NR 510002078)
- [SDR AU510001989](https://openairdocs.org/sdr/AU510001989), Nov 10, 2005: PUMP. FAILED. NR 2 SYSTEM HYDRAULIC PUMP FAILED. INVESTIGATION CONTINUING.
- [SDR AU510001518](https://openairdocs.org/sdr/AU510001518), Nov 6, 2005: COMPUTER. FAULTY. AUTOPILOT COMPUTER INTERMITTENT FAULT.
- [SDR AU510002087](https://openairdocs.org/sdr/AU510002087), Oct 11, 2005: PRESSURE SWITCH. FAULTY. FUEL TRANSFER PUMP PRESSURE SWITCH FAULTY.
- [SDR AU510002126](https://openairdocs.org/sdr/AU510002126), Oct 11, 2005: PRESSURE SWITCH. FAILED. LT AND RT HYDRAULIC PRESSURE SWITCHES FOR THE NR 2 STABILIZER SYSTEM FAULTY.
- [SDR AU510002127](https://openairdocs.org/sdr/AU510002127), Oct 11, 2005: TOTALIZER. FAULTY. FUEL INDICATING SYSTEM COMBINED PROCESSOR TOTALIZER UNIT (CPT) FAULTY.
- [SDR AU510002086](https://openairdocs.org/sdr/AU510002086), Sep 11, 2005: IDG. FAULTY. LT ENGINE INTEGRATED DRIVE GENERATOR (IDG) FAULTY. LT GENERATOR LINE CONTACTOR P/N S6002206 ALSO CHANGED.

All 164: https://openairdocs.org/engine/rolls-royce-tay-650-15/reports.md

## PMA parts (OpenAirDocs) (94, 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
- [JE00072](https://drs.faa.gov/browse/excelExternalWindow/FDBD18F11127968586257284005FBBFF.0001): Bushing. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces EU76491 · Nov 20, 2006
- [JK00096](https://drs.faa.gov/browse/excelExternalWindow/E6237E4E4A14417286257284005FC3FC.0001): Trunnion. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces JR19920 · Nov 20, 2006

All of them: https://openairdocs.org/engine/rolls-royce-tay-650-15/pma.md

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