# Rolls-Royce RB-211-22 series

- Type: Engine model (FAA registry)
- Registry code: 54554
- Manufacturer (registry): ROLLS-ROYC
- Model: RB-211-22
- Engine type: Turbo-fan
- Power: 4,000 hp
- Data sheet: [TCDS E12EU](https://openairdocs.org/tcds/E12EU) (OpenAirDocs)
- Holder: Rolls-Royce Deutschland Ltd & Co KG
- Installed in: 8 registered aircraft
- Page: https://openairdocs.org/engine/rolls-royce-rb-211-22-series

The registry names only the engine series, so ADs for every model in the series are matched.

## 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 2016-08-07](https://openairdocs.org/ad/2016-08-07): LPT support roller bearing · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 22 more. Effective May 16, 2016
- [AD 2010-17-10](https://openairdocs.org/ad/2010-17-10): Rear cooling air holes · Rolls-Royce RB211-22B-02, RB211-524B4-D-02, RB211-524D4-19 and 5 more. Effective Sep 27, 2010
- [AD 2008-20-04](https://openairdocs.org/ad/2008-20-04): HP turbine discs · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 26 more. Effective Nov 3, 2008
- [AD 2006-11-05 R2](https://openairdocs.org/ad/2006-11-05-R2): High pressure compressor (HPC) · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective Feb 21, 2008
- [AD 2006-17-12](https://openairdocs.org/ad/2006-17-12): High pressure (HP) turbine discs · Rolls-Royce RB211-22B-02, RB211-535C-37, RB211-535E4-37 and 3 more. Effective Sep 27, 2006
- [AD 2004-19-04](https://openairdocs.org/ad/2004-19-04): Critical Life-Limited Rotating Engine Parts · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective Nov 1, 2004
- [AD 2004-01-21](https://openairdocs.org/ad/2004-01-21): Frount engine mount housing · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective Feb 27, 2004
- [AD 2003-14-21](https://openairdocs.org/ad/2003-14-21): Engine turbine cooling air overheat monitoring panel · Lockheed Martin L-1011-385-1, L-1011-385-1-14, L-1011-385-1-15 and 7 more. Effective Aug 25, 2003
- [AD 2003-13-12](https://openairdocs.org/ad/2003-13-12): Intermediate pressure (IP) compressor · Rolls-Royce RB211-22B-02 and RB211-22B/MOD 72-8700. Effective Aug 1, 2003
- [AD 2000-11-10](https://openairdocs.org/ad/2000-11-10): Rotor Shafts · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524-02 and 23 more. Effective Aug 7, 2000
- [AD 87-23-04 R1](https://openairdocs.org/ad/87-23-04-R1): Low PressureTurbine Disk · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524-02 and 7 more. Effective May 31, 1989
- [AD 86-15-01 R2](https://openairdocs.org/ad/86-15-01-R2): Stage 1 And 2 HPC Disk Assemblies · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 23 more. Effective Jul 1, 1987
- [AD 86-24-05](https://openairdocs.org/ad/86-24-05): Rotors And Disks Oversped · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 22 more. Effective Dec 20, 1986
- [AD 86-20-09](https://openairdocs.org/ad/86-20-09): Intermediate Pressure Compressor (IPC) Stage 6 to 7 Rotor Assemblies · Rolls-Royce RB211-22B-02 and RB211-22B/MOD 72-8700. Effective Nov 4, 1986
- [AD 85-10-05 R1](https://openairdocs.org/ad/85-10-05-R1): Low Pressure Rotor Location Bearing Area Modifications · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 14 more. Effective Mar 28, 1986
- [AD 80-13-05 R1](https://openairdocs.org/ad/80-13-05-R1): (HPC) Rotor Stage 1 And 2 Disk Assembly · Rolls-Royce RB211-22B-02 and RB211-22B/MOD 72-8700. Effective Nov 28, 1983
- [AD 83-01-03](https://openairdocs.org/ad/83-01-03): Disk Assemblies · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 22 more. Effective Feb 17, 1983
- [AD 82-12-05](https://openairdocs.org/ad/82-12-05): Fan Assembly · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 22 more. Effective Jun 7, 1982
- [AD 78-19-01](https://openairdocs.org/ad/78-19-01): High Pressure Turbine Discs · Rolls-Royce RB211-22B-02 and RB211-22B/MOD 72-8700. Effective Sep 25, 1978
- [AD 76-26-01](https://openairdocs.org/ad/76-26-01): H.P. Turbine Disc · Rolls-Royce RB211-22B-02 and RB211-22B/MOD 72-8700. Effective Jan 3, 1977
- [AD 76-15-09](https://openairdocs.org/ad/76-15-09): Engine Shutdown · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700 and RB211-22C-02. Effective Jul 22, 1976
- [AD 75-16-09](https://openairdocs.org/ad/75-16-09): HS External Gearbox Oil Tank Filler Cap And Housing · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 22 more. Effective Aug 27, 1975
- [AD 75-16-08](https://openairdocs.org/ad/75-16-08): Intermediate and High Pressure Compressors · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 22 more. Effective Aug 22, 1975
- [AD 73-10-01](https://openairdocs.org/ad/73-10-01): VIGV Scheduling · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700 and RB211-22C-02. Effective May 8, 1973

Historical (superseded or no longer in force):

- [AD 2006-11-05 R1](https://openairdocs.org/ad/2006-11-05-R1) (historical): Disc assemblies · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective May 1, 2007
- [AD 2006-11-05](https://openairdocs.org/ad/2006-11-05) (historical): High pressure compressor (HPC) stage 3 disc assemblies · Rolls-Royce RB211-22B-02, RB211-524B-02, RB211-524B-B-02 and 24 more. Effective Jun 27, 2006
- [AD 2004-26-03](https://openairdocs.org/ad/2004-26-03) (historical): High pressure (HP) turbine discs · Rolls-Royce RB211-22B-02, RB211-535C-37, RB211-535E4-37 and 3 more. Effective Jan 13, 2005
- [AD 2004-01-20](https://openairdocs.org/ad/2004-01-20) (historical): High pressure compressor (HPC) · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective Feb 24, 2004
- [AD 2001-23-02](https://openairdocs.org/ad/2001-23-02) (historical): High Pressure Turbine Disks · Rolls-Royce RB211-22B-02, RB211-535C-37, RB211-535E4-37 and 2 more. Effective Dec 24, 2001
- [AD 94-18-03](https://openairdocs.org/ad/94-18-03) (historical): Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524-02 and 23 more. Effective Sep 26, 1994

## Registered aircraft (8)

- [N19130](https://openairdocs.org/aircraft/N19130): [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC), [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago), built 1998, S/N 28970
- [N507YV](https://openairdocs.org/aircraft/N507YV): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), S/N 24607
- [N610G](https://openairdocs.org/aircraft/N610G): [L 3 Capital LLC](https://openairdocs.org/faa-owner/L%203%20CAPITAL%20LLC), [Kalispell, MT](https://openairdocs.org/faa-place/MT/Kalispell), built 1999, S/N 29304
- [N75854](https://openairdocs.org/aircraft/N75854): [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC), [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago), built 2002, S/N 32813
- [N761AJ](https://openairdocs.org/aircraft/N761AJ): [Umb Bank Na Trustee](https://openairdocs.org/faa-owner/UMB%20BANK%20NA%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 2002, S/N 31478
- [N777AZ](https://openairdocs.org/aircraft/N777AZ): [Wilmington Trust Company Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20COMPANY%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 2002, S/N 29743
- [N77865](https://openairdocs.org/aircraft/N77865): [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC), [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago), built 2002, S/N 32589
- [N78866](https://openairdocs.org/aircraft/N78866): [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC), [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago), built 2002, S/N 32591

## NTSB investigations (23)

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 DCA26WA364](https://openairdocs.org/ntsb/DCA26WA364), Sep 14, 2026: Boeing 777-223 (N761AJ), Ezeiza, Argentina, incident, no damage
- [NTSB DCA19CA167](https://openairdocs.org/ntsb/DCA19CA167), Jun 15, 2019: Boeing 757 (N26123), Newark, NJ, substantial damage. Probable cause: an improper landing flare, which resulted in a bounced landing and substantial damage.
- [NTSB DCA18LA285](https://openairdocs.org/ntsb/DCA18LA285), Sep 6, 2018: Boeing 757 (N173AN), New York, NY, no damage. Probable cause: The flight crew’s failure to adequately monitor the airplane’s airspeed, which led to the captain’s aggressive control inputs to increase airspeed; these aggressive inputs resulted in injuries to…
- [NTSB LAX01IA066](https://openairdocs.org/ntsb/LAX01IA066), Dec 30, 2000: Lockheed L-1011-385-1 (N735D), Honolulu, HI, incident, minor damage. Probable cause: the electrical wire arcing and burning as result of insulation degradation, which more than likely resulted from improper clamping.
- [NTSB LAX00LA192](https://openairdocs.org/ntsb/LAX00LA192), May 9, 2000: Lockheed L1011-385-1 (N192AT), Maui, HI, substantial damage. Probable cause: The captain's failure to maintain the proper wind-adjusted Vref airspeed, by a margin which varied from 7 to 20 knots too slow, during the final 10 seconds of the approach prior to touchdown.
- [NTSB NYC97LA129](https://openairdocs.org/ntsb/NYC97LA129), Jun 27, 1997: Lockheed L-1011-385-1 (N723DA), Covington, KY, no damage. Probable cause: the failure of the primary and secondary elevator driveshafts, and the failure of maintenance personnel to detect the failure of the primary shaft during scheduled inspections.
- [NTSB CHI97IA134](https://openairdocs.org/ntsb/CHI97IA134), May 15, 1997: Lockheed L-1011-385-1 (N11003), Saint Louis, MO, incident, minor damage. Probable cause: failure of company maintenance personnel to properly install a mounting eyebolt (and associated cotter pin, washer, spacer and castellated nut) on the lower forward bracket of the left main landing…
- [NTSB NYC97LA064](https://openairdocs.org/ntsb/NYC97LA064), Mar 27, 1997: Lockheed L-1011 (N762DA), Jamaica, NY, no damage, 1 fatal. Probable cause: The failure of the right wing walker, also the push back supervisor, to identify and avoid a hazardous condition, which resulted in his activity near the airplane's nose wheel during tow operations,…
- [NTSB BFO92IA145](https://openairdocs.org/ntsb/BFO92IA145), Sep 20, 1992: Lockheed L1011-385 (N786DL), Boston, MA, incident, minor damage. Probable cause: INADEQUATE LUBRICATION WHICH CAUSED STRESS CORROSION CRACKING AND THE SEPARATION OF THE RIGHT WING NUMBER TWO FLAP VANE.
- [NTSB LAX92IA307](https://openairdocs.org/ntsb/LAX92IA307), Jul 18, 1992: Lockheed L-1011-385-1 (N719DA), Los Angeles, CA, incident, no damage. Probable cause: A FAILURE OF GROUND PERSONNEL TO ENSURE PROPER CLEARANCE BETWEEN A TAXIING AIRPLANE AND AN ADJACENT PARKED AIRPLANE. CONTRIBUTING TO THE ACCIDENT WAS A FAILURE OF GROUND PERSONNEL TO PROPERLY…
- [NTSB ATL92IA113](https://openairdocs.org/ntsb/ATL92IA113), Jun 2, 1992: Lockheed L-1011-1 (N718DA), Atlanta, GA, incident, no damage. Probable cause: THE OVERHEATING OF THE NUMBER 2 AIR CYCLE MACHINE WHICH RESULTED IN AN EMERGENCY EVACUATION VIA SLIDES; THE FAILURE OF THE FLIGHT ATTENDANTS TO SECURE THE SLIDE GIRT BARS.
- [NTSB NYC92IA086](https://openairdocs.org/ntsb/NYC92IA086), Apr 23, 1992: Lockheed L-1011-385 (N721DA), Flushing, NY, incident, minor damage. Probable cause: THE CAPTAIN'S IMPROPER AIRCRAFT CONTROL WHICH RESULTED IN AN EXCESSIVE NOSEWHEEL RATE OF SINK AND SUBSEQUENT OVERLOAD FAILURE OF THE NOSE GEAR TIRES.
- [NTSB LAX90IA101](https://openairdocs.org/ntsb/LAX90IA101), Feb 19, 1990: Lockheed L-1011-385-1 (N31013), Los Angeles, CA, incident, minor damage. Probable cause: THE FAILURE OF THE WELD HOLDING THE SLIP JOINT TO THE PNEUMATIC DUAL COMPENSATOR FROM THE NO. 2 ENGINE.
- [NTSB ATL89FA161](https://openairdocs.org/ntsb/ATL89FA161), Jun 16, 1989: Lockheed L1011-385-1 (N721DA), Jacks Creek, TN, no damage. Probable cause: FAILURE OF THE PASSENGERS TO REMAIN SEATED WITH THEIR SEAT BELTS FASTENED AS THE AIRPLANE ENCOUNTERED UNFORECAST SEVERE CLEAR AIR TURBULENCE.
- [NTSB DCA87MA012](https://openairdocs.org/ntsb/DCA87MA012), Nov 13, 1986: Lockheed L1011 (N714DA), Newark, NJ, substantial damage
- [NTSB FTW86IA020](https://openairdocs.org/ntsb/FTW86IA020), Oct 26, 1985: Lockheed L-1011-385-1 (N714DA), Dallas/Ft.Worth, TX, incident, no damage
- [NTSB MKC85IA131](https://openairdocs.org/ntsb/MKC85IA131), Jun 11, 1985: Lockheed L-1011 (N31013), St. Louis, MO, incident, minor damage
- [NTSB MKC83IA115](https://openairdocs.org/ntsb/MKC83IA115), May 25, 1983: Lockheed L-1011-385-1 (N31013), St. Louis, MO, incident, minor damage
- [NTSB FTW80IA018](https://openairdocs.org/ntsb/FTW80IA018), Nov 25, 1979: Lockheed L-1011 (N714DA), Mineral Wells, TX, incident, no damage, 1 fatal
- [NTSB MKC76AK058](https://openairdocs.org/ntsb/MKC76AK058), Jun 1, 1976: Lockheed L-1011 (N31013), Salina, KS, substantial damage
- [NTSB LAX76IL023](https://openairdocs.org/ntsb/LAX76IL023), Oct 2, 1975: Lockheed 1011 (N31013), Philadelphia, PA, incident, no damage
- [NTSB LAX75AL067](https://openairdocs.org/ntsb/LAX75AL067), Jun 14, 1975: Lockheed 1011 (N41016), Los Angeles, CA, no damage
- [NTSB LAX73IL029](https://openairdocs.org/ntsb/LAX73IL029), Jan 10, 1973: Lockheed 1011 (N11003), Grand Junctn, CO, incident, minor damage

## FAA accident and incident reports (134, 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.

- [Accident 20190615023989A](https://openairdocs.org/incident/20190615023989A), Jun 15, 2019: Boeing 757-224 (N26123), Newark, NJ, Substantial damage. United flight UA627 landed on runway 22L. The aircraft's nose bounced several times several feet in air before several main tires and the left nose tire blew.…
- [Accident 20190615007009A](https://openairdocs.org/incident/20190615007009A), Jun 15, 2019: Boeing 757-224 (N26123), Newark, NJ, Substantial damage. United flight UA627 landed on runway 22L. The aircraft's nose bounced Several times several feet in air before several main tires and the left Nose tire blew.…
- [Incident 20021017028349I](https://openairdocs.org/incident/20021017028349I), Oct 17, 2002: Lkheed 10113851 (N186AT), Memphis, TN. (-23) During cruise approximately 2140 local time a flight attendant notified the flight crew of nauseating odors in the cabin, the flight engineer confirmed…
- [Incident 20020805022109I](https://openairdocs.org/incident/20020805022109I), Aug 5, 2002: Boeing 757224 (N26123), Juneau, AK. (-23) Aircraft was enroute from iah>anc, cala #1507, B-757-224, N26123, etops qualified, & @ cruise altitide, pilots noticed a fuel configuration light…
- [Incident 20010305003899I](https://openairdocs.org/incident/20010305003899I), Mar 5, 2001: Lkheed 10113851 (N188AT), Honolulu, HI, Minor damage. (-23) At approx. 10,000 ft. no. 1 engine experienced an uncontained engine failure. Corrective action will be determined by the chdo.
- [Incident 20001229031759I](https://openairdocs.org/incident/20001229031759I), Dec 29, 2000: Lkheed 10113851 (N735D), Honolulu, HI, Minor damage. (-23) Delta 219, enroute from sfo to hnl, experienced electrical arcing in wiring over first officer's side window. Arcing was followed by smoke, then flame…
- [Incident 20001029031079I](https://openairdocs.org/incident/20001029031079I), Oct 29, 2000: Lkheed 10113851 (N197AT), Indianapolis, IN. (-23) On October 29, 2000, American trans air airlines (amta) operated an L-1011 a/c from shannon, ireland to Indianapolis, Indiana (ind) as ata flight 7146.…
- [Accident 20000509006209A](https://openairdocs.org/incident/20000509006209A), May 9, 2000: Lkheed 10113851 (N192AT), Kahului, HI, No damage. (-23) On may 9, 2000, at 0955 local time (1955Z), American trans air (ata) aircraft N192AT, flight 671, Lockheed L1011-385-1, experienced a tail strike during…
- [Incident 19980625027709I](https://openairdocs.org/incident/19980625027709I), Jun 25, 1998: Lkheed L10113851 (N188AT), Los Angeles, CA, Minor damage. Capt. nevil, PIC of amta 744 used unsafe thrust management procedures while taxiing into gate 26 at lax. His actions caused a baggage container to become…
- [Incident 19980416025219I](https://openairdocs.org/incident/19980416025219I), Apr 16, 1998: Lkheed L10113851 (N189AT), Albuquerque, NM. Due to enroute turbulence, loss of seperation occurred. No injuries. Flight 4401 climbed back to assigned altitude after altitude excursion. They informed…
- [Incident 19971214043549I](https://openairdocs.org/incident/19971214043549I), Dec 14, 1997: Lkheed 10113851 (N197AT), Indianapolis, IN. Narrative: on December 14, 1997, at 1350Z (0850 LCL) a Lockheed L-1011, N197AT registered to American trans air, flight 8449 departed from detroit metro…
- [Incident 19970813029799I](https://openairdocs.org/incident/19970813029799I), Aug 13, 1997: Lkheed 10113853 (N760DH), Denver, CO, Minor damage. Narrative: a delta L-1011 was taxiing to the gate at Denver International Airport, when the right wing of the L-1011 clipped the left horizontal stabilizer of…
- [Accident 19970627046249A](https://openairdocs.org/incident/19970627046249A), Jun 27, 1997: N723DA, Covington/Cinci, KY, No damage. (-23) During acft push back, lt. galley lift fell approx. 5 ft. from upper positin to lower galley. Flight attendant in lift was injured & was removed from…
- [Accident 19970327023269A](https://openairdocs.org/incident/19970327023269A), Mar 27, 1997: Lkheed 10113853 (N762DA), New York, NY, 1 fatal. (.4)The L-1011 was pushed back from the gate by a groundcrew of 3 employees. The tug operator was seated facing the airplane, while wing walkers were placed at…
- [Incident 19970307006819I](https://openairdocs.org/incident/19970307006819I), Mar 7, 1997: Lkheed 10113851 (N188AT), Denver, CO. Narrative: at approximately 100NM east of the Denver VOR, the crew noticed that they were losing fuel. There was approximately 30,000 lb on board at that time.…
- [Incident 19961029040399I](https://openairdocs.org/incident/19961029040399I), Oct 29, 1996: Lkheed 10113853 (N760DH), Atlanta, GA, Minor damage. Narrative: Lockheed L-1011, N7610DH, while on rollout after landing touchdown experienced blown rear left outboard and inboard rear tires. The outboard left…
- [Incident 19960812037399I](https://openairdocs.org/incident/19960812037399I), Aug 12, 1996: Lkheed 10113851 (N310GB), Las Vegas, NV, Minor damage. Narrative: after landing on runway 25L at Las Vegas mccarran international airport at 1:30 pm local time, the aircraft taxied over some temporary runway end…
- [Incident 19960709022459I](https://openairdocs.org/incident/19960709022459I), Jul 9, 1996: Lkheed 10113851 (N718DA), Salt Lake City, UT. Narrative: delta flt 706, a Lockheed L-1011, N718DA, departed seattle int'l, WA at approx. 0830 PDT under VFR conditions. While enroute to atlanta, ga and…
- [Incident 19960623022489I](https://openairdocs.org/incident/19960623022489I), Jun 23, 1996: Lkheed 10113851 (N719DA), Salt Lake City, UT, Minor damage. Narrative: during takeoff the cap from number three (3) forward tire came off. The cap damaged the upper wing panel and wiring in the flap well. Maintenance…
- [Accident 19960221002159A](https://openairdocs.org/incident/19960221002159A), Feb 21, 1996: Lkheed 10113851 (N196AT), Indianapolis, IN, No damage. Parked on ramp, undergoing maintenance, engine fll off aircraft, mechanic trapped inside engine.
- [Incident 19960217006909I](https://openairdocs.org/incident/19960217006909I), Feb 17, 1996: Lkheed 10113851 (N719DA), Salt Lake City, UT, Minor damage. Narrative: on departure number three (3) aft tire blew. A large piece of the tire was ingested into number three engine requiring the crew to shut down the…
- [Incident 19960118002829I](https://openairdocs.org/incident/19960118002829I), Jan 18, 1996: Lkheed 10113851 (N719DA), Salt Lake City, UT. Narrative: delta flight #152, L-1011, departed slc on 01-18-96, reported engine vibration. CFR equipment called out at 1840Z. Delta flight #152 landed slc…
- [Incident 19951217046219I](https://openairdocs.org/incident/19951217046219I), Dec 17, 1995: Lkheed 10113851 (N735D), Salt Lake City, UT. Narrative: a/c aborted t/o due to blown tire. Runway was closed for clean up. The cap was ingested into number one engine and required the engine to be…
- [Incident 19951016042929I](https://openairdocs.org/incident/19951016042929I), Oct 16, 1995: Lkheed 1011385115 (N194AT), Indianapolis, IN. Narrative: on October 16, 1995, at 10:15 local time, a Lockheed L1011, N194AT registered to shawmut bank Connecticut, and operated by American trans air ind.,…
- [Incident 19950604029219I](https://openairdocs.org/incident/19950604029219I), Jun 4, 1995: Lkheed 10113851 (N790DL), Los Angeles, CA. Returned due improper fueling and fuel balance. Fuel burn adjusted to level imbalance. Noncorrect fueling procedure
- [Incident 19950113004609I](https://openairdocs.org/incident/19950113004609I), Jan 13, 1995: Lkheed 10113851 (N719DA), Portland, OR, Minor damage. Narrative: on January 13, 1995, delta airlines flight 558 ingested a bird into number 3 engine shortly after take-off from Portland International Airport.…
- [Incident 19941114043169I](https://openairdocs.org/incident/19941114043169I), Nov 14, 1994: Lkheed 10113851 (N782DL), San Diego, CA, Substantial damage. Turbine overheat light came on during climb. Returned. Turbine casing burnout including inner and outer cowling.
- [Incident 19940531028499I](https://openairdocs.org/incident/19940531028499I), May 31, 1994: Lkheed 10113853 (N753DA), Madrid, SP, Minor damage. Cargo door light came on. Aborted taxied to gate. Main tires flat and small fire. Emergency handled correctly.
- [Incident 19940516028869I](https://openairdocs.org/incident/19940516028869I), May 16, 1994: Lkheed 10113853 (N755DL), Los Angeles, CA. Using engine NR2 to taxi after pushback. Jet blast injured 2 ground crewmen servicing another aircraft.
- [Incident 19940513022819I](https://openairdocs.org/incident/19940513022819I), May 13, 1994: Lkheed 10113851 (N31013), Portland, OR. Leading edge slat problem on approach. Went around landed okay.NR4 and 5 acuators replaced.
- [Incident 19930131010259I](https://openairdocs.org/incident/19930131010259I), Jan 31, 1993: Lkheed 10113851 (N191AT), Honolulu, HI, Minor damage. NR2 engine flamed out on climb. Engine shutdown. Unable to restart. Returned. High speed gear box shaft was sheared
- [Incident 19930112000299I](https://openairdocs.org/incident/19930112000299I), Jan 12, 1993: Lkheed 10113851 (N190AT), San Antonio, TX. Flight engineer became ill en route. Flight engineer was laid on floor and given oxygen. Physician onboard assisted.
- [Incident 19920920044949I](https://openairdocs.org/incident/19920920044949I), Sep 20, 1992: Lkheed 10113851 (N786DL), Boston, MA, Minor damage. Outboard fore flap on right inboard flap assembly broke loose and fell from aircraft on final approach.
- [Incident 19920717036239I](https://openairdocs.org/incident/19920717036239I), Jul 17, 1992: Lkheed 10113851 (N1732D), Dallas-Ft Worth, TX. Left main landing gear departed taxiway while making a turn. Gear sank through thin asphalt shoulder.
- [Incident 19920717032349I](https://openairdocs.org/incident/19920717032349I), Jul 17, 1992: Lkheed 10113851 (N719DA), Los Angeles, CA, Minor damage. Pilot struck a parked aircraft with left wing while taxiing to gate.
- [Incident 19920706028909I](https://openairdocs.org/incident/19920706028909I), Jul 6, 1992: Lkheed 10113851 (N41012), St Louis, MO, Minor damage. Two aft inboard panels from horizontal stabilizer departed on rollout. NR6 and 7 cascade vanes installed wrong.
- [Incident 19920620025369I](https://openairdocs.org/incident/19920620025369I), Jun 20, 1992: Lkheed 10113851 (N721DA), Los Angeles, CA. Captain experienced an illness. Flight engineer occupied left seat and assisted first officer. Landed safely.
- [Incident 19920602021499I](https://openairdocs.org/incident/19920602021499I), Jun 2, 1992: Lkheed 10113851 (N718DA), Atlanta, GA. Smoke in cabin on climb. Returned. Landed safely. Evacuation. Some slides did not deploy. Air cycle machine faulty.
- [Incident 19920423022529I](https://openairdocs.org/incident/19920423022529I), Apr 23, 1992: Lkheed 10113851 (N721DA), New York, NY, Minor damage. Pilot made a hard landing. Fire on nose wheel assembly. Airport closed.
- [Incident 19920201005619I](https://openairdocs.org/incident/19920201005619I), Feb 1, 1992: Lkheed 10113853 (N763DL), Portland, OR. Fire warning on APU generator when switched from ground power. Fired bottles. Smoke from failed generator.
- [Incident 19911130057889I](https://openairdocs.org/incident/19911130057889I), Nov 30, 1991: Lkheed 10113853 (N756DR), Fairbanks, AK. Lost NR2 generator after departure. Diverted due to weather at anchorage. Maintenance corrected problem.
- [Incident 19911105054259I](https://openairdocs.org/incident/19911105054259I), Nov 5, 1991: Lkheed 10113851 (N11005), St Louis, MO. Crew thought aircraft had a blown tire on takeoff. Returned. Left gear retract actuator had blown.
- [Incident 19910701031819I](https://openairdocs.org/incident/19910701031819I), Jul 1, 1991: Lkheed 10113851 (N192AT), San Francisco, CA, Minor damage. NR1 engine vibrating after departure. Shut down and returned. Low pressure turbine failed. Parts in exhaust section
- [Incident 19900905048749I](https://openairdocs.org/incident/19900905048749I), Sep 5, 1990: Lkheed 10113853 (N756DR), Bangor, ME. NR3 engine malfunctioned. Shut down. Dumped fuel. Diverted to Bangor. Faulty generator-alternator.
- [Incident 19900522023789I](https://openairdocs.org/incident/19900522023789I), May 22, 1990: Lkheed 10113853 (N753DA), Covington - Cin, OH. NR2 air data computer unit failed after takeoff. Returned. Replaced unit.
- [Incident 19900517027199I](https://openairdocs.org/incident/19900517027199I), May 17, 1990: Lkheed 10113851 (N191AT), Milwaukee, WI. NR1 engine would not respond to throttle. Diverted. Fuel flow regulator air supply was blocked by gasket.
- [Incident 19900407018889I](https://openairdocs.org/incident/19900407018889I), Apr 7, 1990: Lkheed 1011385115 (N81026), Miami, FL. Fire warning NR2 engine. Shut down in accordance with company procedures. False warning was found after landing.
- [Incident 19900326012289I](https://openairdocs.org/incident/19900326012289I), Mar 26, 1990: Lkheed 10113851 (N11005), Boston, MA, Minor damage. Fire in NR2 and 3 engines. Aborted takeoff. Evacuated passengers. Nr 3 engine had high pressure compressor damage.
- [Incident 19900325012519I](https://openairdocs.org/incident/19900325012519I), Mar 25, 1990: Lkheed 10113853 (N756DR), Covington - Cin, OH. NR2 inertial navigation system failed on climb. Replaced ins computer.
- [Incident 19900309057199I](https://openairdocs.org/incident/19900309057199I), Mar 9, 1990: Lkheed 10113853 (N753DA), Atlanta, GA. NR1 engine power rolled back to idle inflight. Precautionary landing. Fuel flow regulator faulty.

All 134: https://openairdocs.org/engine/rolls-royce-rb-211-22-series/incidents.md

## Service difficulty reports (42)

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

- [SDR CALA2025081107570](https://openairdocs.org/sdr/CALA2025081107570), Aug 9, 2025: SLEEVE. CUT. FOUND CUT ON TEFLON SLEEVE ON NR 1 ENGINE LOCATED BETWEEN 6-7 O'CLOCK. FOUND NO DAMAGED TO KEVLAR WRAP. TEFLON SLEEVE TEAR IS MEASURED TO BE 20"X16". UNABLE TO 
- [SDR CALA2025061005417](https://openairdocs.org/sdr/CALA2025061005417), Jun 7, 2025: SEAL. DAMAGED. FOUND DAMAGE ON THE LH WING LEADING EDGE DUCT VAPOR SEAL, NEED TO BE REPLACE M&E:19-3611-3-0027, PN BOE2049-0001 REPLACED VAPOR SEAL REF AMM TASK 36-11-01-404-1
- [SDR CALA2022060601434](https://openairdocs.org/sdr/CALA2022060601434), Jun 3, 2022: SCREEN. DAMAGED. PDA 1 FOUND #1 ENGINE ACOUSTIC SCREEN DAMAGED AND MISSING PARTS OF THE SCREEN.
- [SDR CALA2018073001710](https://openairdocs.org/sdr/CALA2018073001710), Jul 26, 2018: CONTROL UNIT. FAULTY. ON CLB OUT LT ENG EGT IN AMBER WITH TEMP 150DEG HIGHER THAN LT. ALL OTR INDICATIONS SIMILAR PERFORMED FIM TASK 75-32-00-815-824-R06 BVCU BITE TEST. FAULTS NOTED
- [SDR AALA20170827002](https://openairdocs.org/sdr/AALA20170827002), Aug 26, 2017: TACH GENERATOR. FLUCTUATES. EMERGENCY DECLARED. FLIGHT RETURNED TO DEPARTURE DUE TO A NR 2 ENGINE SPEED CARD FAILED. LANDING UNEVENTFUL. REMOVED AND REPLACED RIGHT ENGINE N3 TACHOMETER GEN
- [SDR AALA20150922008](https://openairdocs.org/sdr/AALA20150922008), Sep 22, 2015: PROBE. DAMAGED. ABOVE 10,000 FT, LT ENG INDICATIONS ABNORMAL, L FF 3.0 N3 79 N2 89 EGT 714 N1 67.2, R FF 8.9 N3 91 N2 71 EGT 489 N1 94.5 & L EFR 1.65 R EFR 1.61. THE FLIGHT DEC
- [SDR AALA20140505002](https://openairdocs.org/sdr/AALA20140505002), May 4, 2014: PRESSURE SWITCH. FAILED. MIA CREW REPORTED LT HAND OIL FILTER EICAS ILLUMINATED ON CLIMB OUT INTERMITTENTLY. EMER DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. R & R THE PRESS O
- [SDR CALA2014020700157](https://openairdocs.org/sdr/CALA2014020700157), Jan 31, 2014: ACCELEROMETER. FAULTY. ON CLIMB OUT, NR 1 ENG N3 INCREASED TO AMBER, RAN QRH, REDUCED THRUST FROM 89% N1 TO 75% N1 TO REMAIN OUT OF THE AMBER RANGE, DIVERTED TO HNL. R & R AVM ACCELER
- [SDR CALA2012050300324](https://openairdocs.org/sdr/CALA2012050300324), May 3, 2012: CONNECTOR. LOOSE. STATUS MSG RT ENGINE SPEED CARD DETECTED ON EICAS DURING FLIGHT. FOUND NR 2 ENG FIREWALL DISCONECT CONNECTOR D1006P LOOSE. RESECURED AND RAN NR 2 ENG AT IDLE AL
- [SDR CALA2010122000624](https://openairdocs.org/sdr/CALA2010122000624), Dec 18, 2010: FLOORBEAM. GOUGED. SUPPORT TASK FLOORBEAM LOWER LEG HAS GOUGES FROM CEILING PANEL SCREWS AT STA 560, BL 0 - RBL 24, 4 EA, REMOVED & AMP; REPAIRED FLOORBEAM LOWER LEG GOUGES IAW SR
- [SDR DL777070032](https://openairdocs.org/sdr/DL777070032), Jan 14, 2007: EEC. MALFUNCTIONED. AFTER T/O LT ENG RELATED MESSAGES, HIGH OIL PRESS EPR/N1/EGT/N3 EXCEEDANCES. AUTOTHROTTLES KICKED OFF. ENGINE RESPONDED NORMALLY. ENG CTLL/EEC C1L/ REPLACED L E
- [SDR 2006FA0001155](https://openairdocs.org/sdr/2006FA0001155), Oct 9, 2006: FRAME. CRACKED. (REF NR: 06DA063) DURING C-CHECK, MAINTENANCE TASK 53-02-1000 INSP FS 983 FRAME. A CRACK, 3 INCHES) FOUND AT LT, BY A CLOSE VISUAL INSP AND CONFIRMED BY NDT. NR
- [SDR DL777060540](https://openairdocs.org/sdr/DL777060540), Jun 30, 2006: BLADES. DAMAGED. DUE TO TGT TREND SHIFTED BOROSCOPED NR 2 ENG HPC FOUND 6TH STG BLADES DAMAGED OUT OF AMM LIMITS. C/W AMM TASKS 600-804 AND 600-805 BOROSCOPE PER TABLE 305 94242
- [SDR AMTA200500168](https://openairdocs.org/sdr/AMTA200500168), Feb 13, 2005: WARNING SYSTEM. MALFUNCTIONED. LT ENG OVHT EICAS CAME ON AT CRUISE ALT (40000) PERFORMED ENG OVHT CHECK LIST AND SHUTDOWN LT ENG. PERFORMED FIM 26-12-00, FIG 103 FOUND NO DEFECTS. RAN ENGINE 
- [SDR DL777050055](https://openairdocs.org/sdr/DL777050055), Jan 23, 2005: CONNECTOR. BURNED. EICAS MESSAGE ENG FUEL FILTER L CAME ON ABOUT 2 HOURS INFLT. FOUND PIN 3 OF CONNECTOR OF DIFF PRESS SWITCH BURNT. REPLACED PIN, SWITCH AND FILTER.
- [SDR AMTA200401158](https://openairdocs.org/sdr/AMTA200401158), Sep 19, 2004: BLEED VALVE. MALFUNCTIONED. ON FINAL, A FIRE DET LIGHT ILLUM WITH FIRE DET LOOP LIGHT. IAW PROCEDURES GOOD (B) LOOP WAS SELECTED AND TESTED GOOD. ON SHORT FINAL (B) LOOP ILLUMINATED WITH F
- [SDR AMTA200301175](https://openairdocs.org/sdr/AMTA200301175), Sep 15, 2003: CHARGER. INOPERATIVE. L3 DOOR EXTERIOR EGRESS LIGHT INOPERATIVE. REMOVED AND REPLACED L3 DOOR EGRESS LIGHTING POWER PA CHECK IAW MM 33-51-03, OPS. CHECK NORMAL.
- [SDR 2003F00003](https://openairdocs.org/sdr/2003F00003), Dec 22, 2002: POWER SUPPLY. DISCHARGED. DURING SCHEDULED INSPECTION RIGHT 1 DOOR EXTERIOR EGRESS LIGHT WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED RIGHT 1 DOOR POWERPACK IAW MM, OPERATIONAL CHECK
- [SDR AMTA200201456](https://openairdocs.org/sdr/AMTA200201456), Dec 1, 2002: SIGN. INOPERATIVE. R-3 DOOR EMERGENCY EXIT SIGN OUT.
- [SDR AMTA200200920](https://openairdocs.org/sdr/AMTA200200920), Jul 2, 2002: SKIN. BENT. LEFT NR 1 DOOR UPPER FORWARD CORNER OUTER SKIN BENT. REPAIRED DOOR PER ER/A.
- [SDR ARWA000303](https://openairdocs.org/sdr/ARWA000303), Mar 31, 2000: ENGINE. MALFUNCTIONED. MIA - FLT 308 - NR 2 ENGINE FILTER PRESSURE LIGHT ON IN STEADY RUNNING CONDITION (OIL) IN CRUISE NR 2 ENGINE SHUTDOWN. REMOVED AND REPLACED NR 2 ENGINE IAW ARRO
- [SDR K4HA99105](https://openairdocs.org/sdr/K4HA99105), Jan 28, 2000: ENGINE. VIBRATION. RME - FLT 15019 - DURING 2 ENGINE FERRY (NR 2 ENGINE WINDMILLING/INOPERATIVE DUE HIGH VIB AT TAKEOFF POWER). NR 2 ENGINE STARTED TO PROVIDE ADDITIONAL AIR FOR L
- [SDR ARWA990110](https://openairdocs.org/sdr/ARWA990110), Jan 15, 1999: ENGINE. VIBRATES. MIA - FLT 501 - DURNG CLIMB, NR 2 EN AVM 2.5, LT ON, VIB FELT IN PEDALS VIB DECREASE WHEN POWER REDUCED, AVM SELECTED TO LOW POSITION (MED AND HIGH POSITIONS BE
- [SDR ARWA990104](https://openairdocs.org/sdr/ARWA990104), Jan 8, 1999: FFR. OUT OF ADJUST. BQN - FLT 508 - ABORTED TAKEOFF. NR 3 ENGINE SLOW TO ACCELERATE. MAX EPR ON TAKEOFF ROLL 1.200 (1500 RQD FOR REDUCED T/O POWER). RETURNED TO RAMP. ADJUSTED FUEL
- [SDR ARWA980797](https://openairdocs.org/sdr/ARWA980797), Jul 10, 1998: AMPLIFIER. FAILED. MIA - FLT 239 - AFTER TAKEOFF, NR 3 ENGINE N1 INDICATOR FAILED. INDICATED 20.7 PERCENT AT ALL THRUST SETTINGS AND N2, HIGH READINGS DUMPED 5 LBS OF FUEL. CORREC
- [SDR DLL19981299](https://openairdocs.org/sdr/DLL19981299), Jun 18, 1998: VIBRATION LIGHT. ILLUMINATED. NR 3 VIBRATION LIGHT CAME ON. INDICATED APPROX 2.9 BOTH A AND B. ACCOMPANIED BY ENGINE VIBRATION. SHUT DOWN ENGINE VIAPOM. CRUISE AT 350. NO THROTTLE MOVEMENT A
- [SDR DLL17981046](https://openairdocs.org/sdr/DLL17981046), May 16, 1998: ENGINE. FAILED. ON T/O, THE NR 1 ENG GAVE LOUD BANG. VIBES PEGGED OUT AT 5 PLUS AND EGT LT CAME ON. SHUT NR 1 ENG DOWN AND LANDED ATL. REPLACE NUMBER ONE ENGINE.
- [SDR ARWA970603](https://openairdocs.org/sdr/ARWA970603), Jun 16, 1997: ENGINE. FLAMED OUT. AGT - FLT 604 - CRUISHING AT FL 390, NR 2 ENIGNE FLAMED OUT. DESCENDED TO FL 310 AND ATTEMPTED TO RESTART. N3 ROTATION WAS INDICATED. ENGINE DID NOT START. FLIG
- [SDR DLL15971133](https://openairdocs.org/sdr/DLL15971133), Jun 15, 1997: FIRE DETECTOR. OIL SOAKED. NR 2 ENG SHUT DOWN DUE TO FIRE WARNING. FOUND B LOOP AT FWD GEAR BOX OIL SOAKED. REPLACED A/B LOOPS CLEANED CONNECTORS AND REPLACED NR 2 ENG FDCU. SYS CK GOOD.
- [SDR DLL10971135](https://openairdocs.org/sdr/DLL10971135), Jun 14, 1997: GEAR BOX. FAILED. IN FLT CRUISE FL350 NR 3 ENG N3 WENT TO ZERO FOLLOWED BY LOSS OF OIL PRESSURE. NR 3 ENG SHUT DOWN WITH NO OTHER ABNORMAL INDICATIONS. REPLACED NR 3 ENG GEARBOX.
- [SDR 96ZZZM974](https://openairdocs.org/sdr/96ZZZM974), May 5, 1996: FUEL FLOW REG. MALFUNCTIONED. LAX - DURING APPROACH WHEN THROTTLES WERE RETARDED FROM HIGH POWER, NR 3 ENGINE REMAINED AT HIGH POWER REGARDLESS OF THROTTLE POSITION. SHUT DOWN ENGINE. REMOVE
- [SDR 96ZZZM271](https://openairdocs.org/sdr/96ZZZM271), Feb 3, 1996: ENGINE. VIBRATION. ON RIA FLT 858, FROM ORD TO JSJ AT 2500 FEET AT CLIMB POWER NR 1 ENGINE VIBRATION INCREASED TO 4.0, ENGINE THRUST WAS REDUCED, AVM ALSO DECREASED. AIRCRAFT DUMP
- [SDR 96ZZZM48](https://openairdocs.org/sdr/96ZZZM48), Dec 22, 1995: GEAR BOX. FAILED. MIA - FLT 149 - DURING CRUISE, LOST OIL RESULTING IN AN ENGINE SHUTDOWN AND DETERMINED HIGH SPEED. MAIN GEAR BOX 29136, S/N 610200 FAILED. REMOVED AND INSTALLED
- [SDR 95ZZZM625](https://openairdocs.org/sdr/95ZZZM625), Oct 16, 1995: FFR. FAILED. NR 2 ENGINE LOST POWER AFTER TAKEOFF POWER RETARDED ITSELF TO 80 PERCENT N1. AIRCRAFT DUMPED FUEL AND RETURNED TO GATE. CHANGED FFR TO CORRECT PROBLEM AND CHANG
- [SDR 95ZZZX6353](https://openairdocs.org/sdr/95ZZZX6353), Oct 16, 1995: CAP. LOOSE. ON TAKEOFF, NR 3 ENGINE FIRE LIGHT ILLUMINATED. ENGINE WAS SHUT DOWN. AIRCRAFT PERFORMED AIR TURN-BACK. INSPECTION REVEALED 6 O'CLOCK BORESCOPE BLANKING PLUG CA
- [SDR DLL13953981](https://openairdocs.org/sdr/DLL13953981), Oct 6, 1995: OIL PUMP. FAILED. ON CLIMB-OUT, HAD STRONG BURNING ODOR IN AFT CABIN, RETURNED ATL. DETERMINED ODOR SOURCE NR 2 ENGINE. REPLACED ENGINE OIL PUMP AND PERFORMED DUCT BURN-OUT AND R
- [SDR DLL10953861](https://openairdocs.org/sdr/DLL10953861), Sep 28, 1995: GEARBOX. FAILED. ENGINE NR 3 FLAMED-OUT AT FLIGHT LEVEL 370, WINDMILL AT N3 26 PERCENT. ATTEMPTED RELIGHT, ENGINE LIGHT OFF. THROTTLE MOVEMENT HAD NO EFFECT ON EPR, TGT, N1, N2,
- [SDR 95ZZZM293](https://openairdocs.org/sdr/95ZZZM293), Jul 21, 1995: OIL FILTER. DIRTY. DURING DESCENT SHUT DOWN NR 2 ENGINE, S/N 4806, DUE TO OIL FILTER DIFFERENTIAL PRESSURE LIGHT ILLUMINATION. FOUND CARBON IN OIL FILTER. REPLACED OIL FILTER, DRA
- [SDR 95ZZZX3182](https://openairdocs.org/sdr/95ZZZX3182), Jun 9, 1995: ENGINE. FAILED. STL - FLT 324 - AFTER TAKEOFF, SHUT DOWN NR 2 ENGINE, SN 4468, DUE TO HIGH AVM ON BOTH A AND B VIBRATION CHANNELS. CHECKED OIL SYSTEM CHIP DETECTORS, LUBRICATED
- [SDR 95ZZZW748](https://openairdocs.org/sdr/95ZZZW748), May 13, 1995: COMP BLADES. FAILED. STL - DURING CLIMB, SHUT DOWN NR 2 ENGINE DUE TO HIGH AVM AND N2 OVERSPEED. REPLACED NR 2 ENGINE. GROUND RUNUP AND OPERATIONS CHECKED NORMAL. S/D INVESTIGATION 
- [SDR 95ZZZW244](https://openairdocs.org/sdr/95ZZZW244), Feb 19, 1995: FILTER. DIRTY. LAS - DURING CLIMB AND CRUSIE, NR 2 ENGINE FILTER PRESSURE LIGHT WAS FLICKERING AND SLIGHT OIL QTY LOSS WAS INDICTED. ENGINE WAS SHUTDOWN AT 1700 AND FLIGHT WAS
- [SDR 95ZZZW243](https://openairdocs.org/sdr/95ZZZW243), Feb 18, 1995: C1 BLADE. LOCKED UP. DURING CRUSIE, HIGH VIBRATION ON NR 1 ENGINE WAS NOTICED. ENGINE WAS SHUTDOWN AT 0133. UPON INSPECTION FOUND C1 BLADES LOCKED UP. PERFORMED MTC MNL PROCEDURE 72

## STCs that may be installed (OpenAirDocs) (2)

Approved for this engine model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [STC SA4005NM](https://openairdocs.org/stc/SA4005NM): Precise Flight Inc. Pulselite Control System. Precise Flight Inc. Lists RB211-22B-02
- [STC SE1516CE](https://openairdocs.org/stc/SE1516CE): Modification of lower fuel control box assembly to incorporate vibration isolators. Trans World Airlines Inc. Lists RB211-22B-02

## PMA parts (OpenAirDocs) (over 1,000, 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.

- [136802](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID197162965820250602133048.0001): Seal. Donaldson Company Inc · PMA PQ2432CE · Replaces QA2064 · May 23, 2025
- [337081](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193115553120250602133049.0001): Filter Element. Donaldson Company Inc · PMA PQ2432CE · Replaces QA03632 · May 23, 2025
- [137080](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137654126120250602133049.0001): Cotter Pin. Donaldson Company Inc · PMA PQ2432CE · Replaces SP90G16 · May 23, 2025
- [R020197](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID110598442420250602133048.0001): Trap Dirt. Donaldson Company Inc · PMA PQ2432CE · Replaces QA10552 · May 23, 2025
- [WF336992](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID102356413920250602133036.0001): Filter Element, Assembly, Oil. Donaldson Company Inc · PMA PQ2432CE · Replaces QA03638, QR1162, QA0757, QA0752 · May 23, 2025
- [AAP-358474-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID199241288120240311212404.0001): Bearing. Approved Air Parts Co Inc · PMA PQ4173NE · Replaces Honeywell P/N 358474-1 · Mar 6, 2024
- [121728-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193505150520230914183353.0001): Flex Drive. Honeywell International Inc. · PMA PQ1222NM · Replaces L922507 · Mar 21, 2023
- [121190-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID192682231220230914183350.0001): Screwjack. Honeywell International Inc. · PMA PQ1222NM · Replaces 121190-3 · Mar 21, 2023
- [121676-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID190066377320230914183345.0001): Ballscrew Gearbox. Honeywell International Inc. · PMA PQ1222NM · Replaces 121676-1 · Mar 21, 2023
- [898330-9](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID189810012720230914183346.0001): PRSOV. Honeywell International Inc. · PMA PQ1222NM · Replaces 898330-9 · Mar 21, 2023
- [121190-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID187448583120230914183349.0001): Screwjack. Honeywell International Inc. · PMA PQ1222NM · Replaces 121190-1 · Mar 21, 2023
- [898330-10](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184991328720230914183347.0001): PRSOV. Honeywell International Inc. · PMA PQ1222NM · Replaces 898330-10 · Mar 21, 2023
- [121186-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID182835823120230914183344.0001): Gearbox. Honeywell International Inc. · PMA PQ1222NM · Replaces 121186-4 · Mar 21, 2023
- [126664-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID182278265820230914183355.0001): Air Motor. Honeywell International Inc. · PMA PQ1222NM · Replaces L922551 · Mar 21, 2023
- [121190-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID173810527020230914183351.0001): Screwjack. Honeywell International Inc. · PMA PQ1222NM · Replaces 121190-4 · Mar 21, 2023
- [121196-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID142021697220230914183352.0001): Flex Drive. Honeywell International Inc. · PMA PQ1222NM · Replaces 121196-3 · Mar 21, 2023
- [898330-11](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132834451320230914183348.0001): PRSOV. Honeywell International Inc. · PMA PQ1222NM · Replaces 898330-11 · Mar 21, 2023
- [121200-7](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID126678642220230914183343.0001): Gearbox. Honeywell International Inc. · PMA PQ1222NM · Replaces 121200-7 · Mar 21, 2023
- [398552-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID116206336720230914183354.0001): Control Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces L922545 · Mar 21, 2023
- [109580-7](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID110979975720230914183357.0001): Lock Ram. Honeywell International Inc. · PMA PQ1222NM · Replaces 109580-7 · Mar 21, 2023
- [121388-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID101573954420230914183352.0001): Flex Drive. Honeywell International Inc. · PMA PQ1222NM · Replaces 121388-2 · Mar 21, 2023
- [126348-8](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID101163195720230914183356.0001): Air Motor. Honeywell International Inc. · PMA PQ1222NM · Replaces 126348-8 · Mar 21, 2023
- [9-217-67](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID196893917720220803181523.0001): Transmitter Assembly, Rate of Fuel Flow. Eldec Corporation · PMA PQ0079NM · Replaces 9-217-67 · Jul 12, 2022
- [9-217-71](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID173672532220220803181524.0001): Fuel Flow Transmitter. Eldec Corporation · PMA PQ0079NM · Modification part · Jul 12, 2022
- [9-217-81](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID140849175320220803181527.0001): Fuel Flow Transmitter. Eldec Corporation · PMA PQ0079NM · Replaces 9-217-81 · Jul 12, 2022
- [DEC31- 161-509](https://drs.faa.gov/browse/excelExternalWindow/CE0068E03231B26A86258629005AC700.0001): Shaft Assembly, Flexible. Turbine Kinetics Inc, A HEICO Aerospace Company · PMA PQ0816NE · Replaces 121734-5 · Nov 16, 2020
- [1391-502ACD](https://drs.faa.gov/browse/excelExternalWindow/E8C3AE789E4B49458625845800605562.0001): Seal. Aircraft Component Design LLC · PMA PQ2138NE · Replaces 1391-502 · Jan 29, 2019
- [3058-064ACD](https://drs.faa.gov/browse/excelExternalWindow/FD3DB5FE4CF169E4862583F60061B986.0001): Seal, Altitude Bias Cover. Aircraft Component Design LLC · PMA PQ2138NE · Replaces 3058-064 · Oct 22, 2018
- [1382-132ACD](https://drs.faa.gov/browse/excelExternalWindow/D143FE9D28A5A8EA862583F60061B972.0001): Seal. Aircraft Component Design LLC · PMA PQ2138NE · Replaces 1382-132 · Oct 22, 2018
- [3058-066ACD](https://drs.faa.gov/browse/excelExternalWindow/6B7858F8EDEDA439862583F60061B99D.0001): Seal. Aircraft Component Design LLC · PMA PQ2138NE · Replaces 3058-066 · Oct 22, 2018
- [1391-626ACD](https://drs.faa.gov/browse/excelExternalWindow/BECA7417A8B98CC386258344006D6C1F.0001): Seal. Aircraft Component Design LLC · PMA PQ2138NE · Replaces 1391-626 · Jul 10, 2018
- [1391-634ACD](https://drs.faa.gov/browse/excelExternalWindow/91A8A459DD82E1C786258344006D6C25.0001): Seal. Aircraft Component Design LLC · PMA PQ2138NE · Replaces 1391-634 · Jul 10, 2018
- [1391-118ACD](https://drs.faa.gov/browse/excelExternalWindow/89135FC3C73AD63C8625833F006BE32D.0001): Ring, Backup. Aircraft Component Design LLC · PMA PQ2138NE · Replaces 1391-118 · Jul 10, 2018
- [1391-134ACD](https://drs.faa.gov/browse/excelExternalWindow/22A17BB2E5D9D64E8625833F006BE344.0001): Ring, Backup. Aircraft Component Design LLC · PMA PQ2138NE · Replaces 1391-134 · Jul 10, 2018
- [1391-622ACD](https://drs.faa.gov/browse/excelExternalWindow/20E45184A8909ED086258344006D6C15.0001): Seal. Aircraft Component Design LLC · PMA PQ2138NE · Replaces 1391-622 · Jul 10, 2018
- [1391-638ACD](https://drs.faa.gov/browse/excelExternalWindow/172AFF9DD825DF0F86258344006D6C2A.0001): Seal. Aircraft Component Design LLC · PMA PQ2138NE · Replaces 1391-638 · Jul 10, 2018
- [75669](https://drs.faa.gov/browse/excelExternalWindow/C959F9950D653E1786258251005EB12E.0001): Fuel Nozzle, Assy. Delavan Inc. · PMA PQ3405CE · Replaces Rolls-Royce L501004 · Feb 6, 2018
- [75668](https://drs.faa.gov/browse/excelExternalWindow/75B577EE141FF7EB86258251005EB12C.0001): Fuel Nozzle, Assy. Delavan Inc. · PMA PQ3405CE · Replaces Rolls-Royce L501003 · Feb 6, 2018
- [QA03963WE](https://drs.faa.gov/browse/excelExternalWindow/FC8D08C38EEB957C86258148007172D3.0001): Element, Oil Filter-Scavenge. Wencor LLC · PMA PQ1370NM · Replaces QA03963 · Feb 1, 2017
- [DECVA3510-1](https://drs.faa.gov/browse/excelExternalWindow/ADBDEFBF9A25763986257F850077427C.0001): Probe, Assy, Magnetic. Turbine Kinetics Inc, A HEICO Aerospace Company · PMA PQ0816NE · Replaces Eaton Aerospace P/N VA3510-1 · Feb 2, 2016
- [VB3505DEC](https://drs.faa.gov/browse/excelExternalWindow/A6D5307AB453E4FD86257F85007743CF.0001): Probe. Turbine Kinetics Inc, A HEICO Aerospace Company · PMA PQ0816NE · Replaces Eaton Aerospace P/N VB3505 · Feb 2, 2016
- [183824](https://drs.faa.gov/browse/excelExternalWindow/4FCB64D9D1B4EF9986257F16004F2E3B.0001): Nozzle Assy-Fuel Spray. Delavan Inc. · PMA PQ3405CE · Replaces 183824 · Dec 3, 2015
- [P39-401](https://drs.faa.gov/browse/excelExternalWindow/CABA6386FDF1E47286257E3C00823A8F.0001): Ejector Valve. CIRCOR Aerospace, Inc. · PMA PQ1168NM · Replaces P39-401 · May 3, 2015
- [P39-401 Rev F](https://drs.faa.gov/browse/excelExternalWindow/85E398D123820B6086257E3C00824314.0001): Valve, Float Fuel. CIRCOR Aerospace, Inc. · PMA PQ1168NM · Replaces P39-401 Rev F · May 3, 2015
- [904429-30](https://drs.faa.gov/browse/excelExternalWindow/FE7F908D6602293786257DF2005DFD33.0001): Thermocouple, T30. Meggitt Safety Systems Inc · PMA PQ0303NM · Replaces 904429-30 · Dec 8, 2014
- [903468-06](https://drs.faa.gov/browse/excelExternalWindow/F805C2D87B628E4086257DF2005DF6AA.0001): Detector Assembly. Meggitt Safety Systems Inc · PMA PQ0303NM · Replaces 903468-06 · Dec 8, 2014
- [903470-04](https://drs.faa.gov/browse/excelExternalWindow/A010BAE820C831CC86257DF2005DF702.0001): Detector Assembly. Meggitt Safety Systems Inc · PMA PQ0303NM · Replaces 903470-04 · Dec 8, 2014
- [903467-04](https://drs.faa.gov/browse/excelExternalWindow/73C9CAD6F3131CA686257DF2005DF64A.0001): Detector Assembly. Meggitt Safety Systems Inc · PMA PQ0303NM · Replaces 903467-04 · Dec 8, 2014
- [904448-20](https://drs.faa.gov/browse/excelExternalWindow/69E934531E47986786257DF2005DFE41.0001): Thermocouple, Rear Overheat. Meggitt Safety Systems Inc · PMA PQ0303NM · Replaces 904448-20 · Dec 8, 2014
- [904430-20](https://drs.faa.gov/browse/excelExternalWindow/5A3FDEF3F6290F2E86257DF2005DFDE7.0001): Thermocouple, Front Overheat. Meggitt Safety Systems Inc · PMA PQ0303NM · Replaces 904430-20 · Dec 8, 2014

All of them: https://openairdocs.org/engine/rolls-royce-rb-211-22-series/pma.md

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