# Rolls-Royce RB211-22B series

- Type: Engine model (FAA registry)
- Registry code: 54036
- Manufacturer (registry): ROLLS-ROYC
- Model: RB211-22B
- Engine type: Turbo-fan
- Power: 42,670 lb thrust
- Data sheet: [TCDS E12EU](https://openairdocs.org/tcds/E12EU) (OpenAirDocs)
- Holder: Rolls-Royce Deutschland Ltd & Co KG
- Installed in: 0 registered aircraft
- Page: https://openairdocs.org/engine/rolls-royce-rb211-22b-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

None registered with this engine model now.

## NTSB investigations

None matched to aircraft with this engine model.

## FAA accident and incident reports

None matched to aircraft with this engine model.

## Service difficulty reports (57, newest 50)

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

- [SDR AMTA200400623](https://openairdocs.org/sdr/AMTA200400623), Jun 1, 2004: ENGINE. MALFUNCTIONED. HIGH SHUDDER AND TGT ON CLIMB. NO FIRE INDICATION. LOW OIL QUANTITY, PRECAUTIONARY ENGINE FAILURE PERFORMED. REMOVED AND REPLACED NR 2 ENGINE IAW MM M11-71-02. 
- [SDR AMTA200400526](https://openairdocs.org/sdr/AMTA200400526), May 5, 2004: ENGINE. VIBRATION. NR 2 ENGINE EXPERIENCED A SUDDEN INCREASE IN VIBRATION FROM .8 TO 2.5 WITH A SELECTED. WARNING LIGHT WAS ON. SELECTED B DID NOT HELP SHUTDOWN ENGINE AT 1350Z EN
- [SDR CA040427009](https://openairdocs.org/sdr/CA040427009), Apr 25, 2004: COUPLING. CRACKED. (CAN) DURING TAXI TO THE GATE, THE HYD SYS STARTED TO DECREASE RAPIDLY. QRH WAS PERFORMED BY THE CREW. HYDRAULIC LEAK WAS FOUND AT NR 3 PYLON REAR SPAR AREA. FO
- [SDR 2002F00812](https://openairdocs.org/sdr/2002F00812), Aug 15, 2002: FUEL FILTER. DIRTY. ON DESCENT NR 3 ENGINE FUEL PRESSURE LIGHT ON, THROTTLES AT IDLE, ENGINE FLAMED-OUT. PERFORMED EMERGENCY RESTART, OK. REMOVED AND REPLACED NR 3 ENGINE LP FUEL F
- [SDR 20010529SG003](https://openairdocs.org/sdr/20010529SG003), Apr 23, 2001: ENGINE. VIBRATION. ENGINE SHUTDOWN FOR HIGH VIBRATION INDICATION AT FL350. IN CRUISE INDICATION 3 AND AMBER LIGHT. BOTH A AND B PICKUPS. LOW SELECTION INDICATES THIS PROBLEM. TEST
- [SDR CA010706002](https://openairdocs.org/sdr/CA010706002), Apr 23, 2001: LINE. BROKEN. (CAN) AIRCRAFT DIVERTED TO YMX DUE HIGH EPR INDICATION INCREASING WITH ALTITUDE WITH ALL OTHER PARAMETERS NORMAL. MAINTENANCE FOUND P1 LINE BROKEN AT CLAMP ATTA
- [SDR WRN2001F00000](https://openairdocs.org/sdr/WRN2001F00000), Apr 22, 2001: TURBINE BLADES. FAILED. INSPECTION REVEALED IP TURBINE BLADE FAILURE. REMOVED AND REPLACED ENGINE IAW TRADEWINDS CARD L2-130-A01 AND FORMS TWM-7103B AND TWM-7103BB. AIRCRAFT RUN AND LE
- [SDR 20010509SG004](https://openairdocs.org/sdr/20010509SG004), Apr 12, 2001: COMPRESSOR. STALLED. ON TAKEOFF ROLL AT 125 KNOTS, NR 1 ENGINE HAD COMPRESSOR STALL. VIBRATION INDICATOR AT 2 UNITS WITH CAUTION LIGHT ON. AIRCRAFT RETURNED TO GATE. PREPARATION FOR
- [SDR WRN2001F00001](https://openairdocs.org/sdr/WRN2001F00001), Apr 12, 2001: COMPRESSOR. STALLED. ON TAKEOFF ROLL AT 125 KNOTS, NR 1 ENGINE HAD COMPRESSOR STALL. VIBRATION INDICATOR AT 2 UNITS WITH CAUTION LIGHT ON. AIRCRAFT RETURNED TO GATE. PREPARATION FOR
- [SDR 20010202SG008](https://openairdocs.org/sdr/20010202SG008), Aug 11, 2000: SHUTOFF VALVE. INOPERATIVE. AFTER INVESTIGATION AND REVIEW OF ALL REPORTS, NO EXTERNAL EXTINGUISHING AGENT WAS APPLIED TO THE HOT ENGINE. TAIL PIPE FIRE PROCEDURES WERE FOLLOWED IAW RR MM 
- [SDR 20001127AP007](https://openairdocs.org/sdr/20001127AP007), Jul 23, 2000: SHUTOFF VALVE. INOPERATIVE. NR 3 ENGINE DID NOT SHUT DOWN WITH FUEL AND IGNITION OFF. SHUT DOWN ENGINE AS PER ABNORMAL CHECKLIST. GROUND PERSONNEL INDICATED ENGINE WAS ON FIRE. ACCOMPLISHE
- [SDR DLL10000796](https://openairdocs.org/sdr/DLL10000796), Apr 24, 2000: ENGINE. SMOKE. SMOKE SMELL IN AFT GALLEY WITH NO SMOKE VISIBLE. SMOKE ALARMS ACTIVATED. REPLACED NR 2 ENGINE DUE PRODUCING OIL SMOKE.
- [SDR 20000619AP010](https://openairdocs.org/sdr/20000619AP010), Mar 1, 2000: COMPRESSOR. STALLED. VCV - DURING TAKEOFF, THE NR 3 ENGINE COMPRESSOR STALLED AND HIGH VIBRATION WAS NOTED. ABORTED TAKEOFF, RETURNED TO BLOCK. MAINTENANCE FERRIED TO IND. ENGINE NR
- [SDR DLL10992380](https://openairdocs.org/sdr/DLL10992380), Oct 27, 1999: ENGINE. FAILED. BIRD STRIKE ON NR 1 ENGINE AT LIFTOFF. ENGINE BEGAN TO VIB, SURGE, STALL AND TGT ROSE TO 900 DEGS FOR GREATER THAN 30 SECS. REPLACED ENGINE.
- [SDR 2000ZZZM250](https://openairdocs.org/sdr/2000ZZZM250), Oct 19, 1999: OIL PUMP. FAILED. NR 2 ENGINE RAPID LOSS OF OIL QTY ENGIEN RAN APPROXIMATELY 2 MINUTES PRIOR TO SHUTDOWN WINDMILLED WITH NO OIL QTY 23 MINUTES OIL PRESSURE NR 2 LIGHT ON. RETURNE
- [SDR DLL10991546](https://openairdocs.org/sdr/DLL10991546), Jul 9, 1999: OIL PUMP. FAILED. NR 3 ENG LOSING OIL IN CRUISE. BROUGHT NR 3 ENG BACK TO IDLE. DIVERTED TO SLC. INSPECTED SCAVENGE AND MAIN OIL FILTERS, NO METAL FOUND. CKD ALL CHIP DETECTORS, 
- [SDR DLL10991443](https://openairdocs.org/sdr/DLL10991443), Jun 27, 1999: SEAL. FAILED. DURING FLT, USUALLY AT REDUCED POWER, CABIN FILLED WITH A BLUE HAZE AND LAV SMOKE DETECTORS IN FWD AND AFT LAVS WENT OFF FOR SEVERAL MINUTES. REPLACED NR 3 ENGI
- [SDR 99ZZZM391](https://openairdocs.org/sdr/99ZZZM391), Jun 15, 1999: ENGINE. VIBRATION. DURING CLIMB ENGINE VIBRATION FILTER PRESSURE LIGHT CAME ON AND CHANNEL 'A' AND 'B' READING 2.5 UNITS. SHUTDOWN ENGINE NR 2 IAW AOM AND CHECKLIST, DUMPED FUEL B
- [SDR CA990330062](https://openairdocs.org/sdr/CA990330062), Mar 5, 1999: LOCK PIN. NOT ENGAGED. (CAN) L3 WARN LIGHT CAME ON, AIRCRAFT LANDED. INVESTIGATION REVEALED LOCK PIN NOT ENGAGED. PIN LUBRICATED AND CHECKED SERVICEABLE.
- [SDR CA990330061](https://openairdocs.org/sdr/CA990330061), Mar 4, 1999: ACTUATOR. MALFUNCTIONED. (CAN) AFTER TAKEOFF, RIGHT MLG DOOR AND INTRANSIT LIGHT ILLUMINATED. INVESTIGATION REVEALED THAT THE DOOR ACTUATOR P/N 2-690021-19 WAS U/S.
- [SDR DLL10990339](https://openairdocs.org/sdr/DLL10990339), Feb 19, 1999: REGULATOR. INOP. ABORTED TAKEOFF AT 60 KNOTS DUE TO FLUCTUATION OF NR 1 ENG INSTRUMENTS. ON STATIC R/U N1 EGT N3 THROTTLE POSTION ALL AT TAKEOFF EPR ONLY REACHED 1.365. REPLACED
- [SDR 99ZZZM285](https://openairdocs.org/sdr/99ZZZM285), Feb 10, 1999: FUEL PUMP. FAILED. DURING TAKEOFF ROLL EPR ON NR 2 ENGINE DECREASED FROM .530 TO .490. REMOVED AND REPLACED NR 2 ENGINE MAIN FUEL PUMP PER MM 73-11-01. LEAK CHECK GOOD ALL PARAMET
- [SDR 99ZZZM284](https://openairdocs.org/sdr/99ZZZM284), Feb 8, 1999: FUEL FLOW REG. INOPERATIVE. DURING TAKEOFF, NR 2 EPR DROPPED TO 460 AFTER V1, N1 88 PERCENT, TGT 650, N2 99 PERCENT, FF 2000 LBS/HR LOW THROTTLE AT FULL FORWARD POSITION, TARGET EPR 535, N
- [SDR CA990311073](https://openairdocs.org/sdr/CA990311073), Jan 24, 1999: CIRCUIT BREAKER. FAILED. (CAN) AT DEPARTURE, BURN SMELL REPORTED BY FLIGHT ATTENDANT. FOUND SB PANEL NR 4 PASS-SERV MDL NR 1 CIRCUIT BREAKER BURNED OUT, PASS-SERV MDL NR 2 AND NR 7 CIRC
- [SDR CA990311070](https://openairdocs.org/sdr/CA990311070), Jan 11, 1999: LINE. CRACKED. (CAN) AIRCRAFT RETURNED DUE TO C-SYSTEM HYDRAULIC QUANTITY DECREASING DURING FLIGHT. FOUND C-HYDRAULIC ELECTRIC PUMP PRESSURE LINE WITH SMALL PIN HOLE CAUSING L
- [SDR CA990311066](https://openairdocs.org/sdr/CA990311066), Jan 7, 1999: BELLCRANK. DAMAGED. (CAN) AFTER ARRIVAL AT GATE, PILOT REPORTED RUDDER JAMMING OCCURRENCE IN THE RUDDER SYSTEM. MAINT FOUND THAT ONE RUDDER BELLCRANK HAD AN ELONGATED HOLE AT THE R
- [SDR CA990311075](https://openairdocs.org/sdr/CA990311075), Dec 24, 1998: TURBINE. FAILED. (CAN) AIR TURBINE MOTOR (RAM AIR TURBINE) INOPERATIVE. LIGHT CAME ON IN-FLIGHT. POST-FLIGHT INSPECTION FOUND OIL MISSING FROM THE RESERVOIR, OIL WAS ADDED AND D
- [SDR CA990311074](https://openairdocs.org/sdr/CA990311074), Dec 2, 1998: ROD. WORN. (CAN) ON INSPECTION OF NR 3 ENGINE PYLON,THE ROD END BEARING BETWEEN THE THROTTLE TORQUE SHAFT AND THE TENSION REGULATOR LEVER WAS FOUND WORN AND THE BEARING DE
- [SDR CA990311068](https://openairdocs.org/sdr/CA990311068), Nov 23, 1998: ENGINE. MALFUNCTIONED. (CAN) ON TAKEOFF ROLL, NR 2 ENGINE VIBRATION WENT TO 3.3 UNITS. TAKEOFF ABORTED. A HIGH POWER RUN WAS CARRIED OUT ON THE WAY BACK TO THE GATE AND THE VIBRATION 
- [SDR 99ZZZX830](https://openairdocs.org/sdr/99ZZZX830), Nov 11, 1998: COMPRESSOR. DAMAGED. DURING A ROUTINE BORESCOPE INSPECTION, FOUND THE NR 3 ENGINE HIGH PRESSURE COMPRESSOR BLADES DAMAGED BEYOND THE MM LIMITS. REMOVED AND REPLACED ENGINE IAW MAINT
- [SDR DLL13982072](https://openairdocs.org/sdr/DLL13982072), Oct 6, 1998: FF REGULATOR. OUT OF ADJUST. NR 2 ENG LOW POWER ON TAKEOFF ROLL .491 EPR WITH LEVER FULL FORWARD TURNED NR 2 PACK OFF WITH NO INCREASE IN POWER. ABORTED AT 80 KTS, ODM BRAKE TIME VERIFIED. 
- [SDR 98ZZZM775](https://openairdocs.org/sdr/98ZZZM775), Aug 29, 1998: PUMP. FAILED. FLT 709 - LAX - ON CLIMB-OUT, NR 3 ENGINE OIL QTY DROPPED TO ZERO (RAPIDLY) FOLLOWED BY NR 3 OIL PRESSURE ALSO READING ZERO. ENGINE WAS SHUT DOWN AND AIR TURN B
- [SDR DLL10981789](https://openairdocs.org/sdr/DLL10981789), Aug 29, 1998: SLAVE RAM. DEFECTIVE. NR 1 THROTTLE FAILED TO DEVELOP T/O THRUST WITH HIGH N2. REPLACED NR 1 ENG MASTER AND SLAVE RAM, RAN PER PFHB TEST NR 4 ALL CKS NORMAL.
- [SDR TWAA9792001](https://openairdocs.org/sdr/TWAA9792001), Aug 11, 1997: GEARBOX. FAILED. STL - FLT 3289 - DURING CRUISE, THE NR 1 ENGINE, SN 4405, INDICATED AN OIL LOSS. REMOVED AND REPLACED THE N4 1 ENGINE GEARBOX, PN M06142, DUE TO DEAIRATOR FAILU
- [SDR TWAA9781001](https://openairdocs.org/sdr/TWAA9781001), Jul 19, 1997: OIL FILTER. DIRTY. LAX - FLT 442 - DURING CLIMB, NR 2 ENGINE, SN 4816, LOST OIL INDICATION. DRAINED GEARBOX, CHANGED MAIN OIL SCREEN AND SCAVENGE SCREEN. SERVICED GEARBOX AND RAN 
- [SDR DLL13970944](https://openairdocs.org/sdr/DLL13970944), May 17, 1997: ENGINE. BIRD STRIKE. ON T/O, NUMBER 3 ENGINE INGESTED AT LEAST ONE LARGE BIRD. PERFORMED FIRST STAGE HPC BORESCOPE INSPECTION AS PER MM. ENGINE FAILED INSPECTION, WILL REQUIRE ENGIN
- [SDR DLL13970595](https://openairdocs.org/sdr/DLL13970595), Apr 1, 1997: COMPRESSOR. DAMAGED. CRUISE AT FL330, EXPERIENCED A YAW TYPE JOLT WITH POPPING SOUNDS FROM CAPTS SIDE OF AIRPLANE. ENG NR 1 VIBS WENT FROM 1.0 TO 1.8 FLIGHT ATTENDANT THEN REPORTED 
- [SDR DLL10970419](https://openairdocs.org/sdr/DLL10970419), Mar 5, 1997: GEARBOX. FAILED. IN CLIMBOUT AT 28,500 FT AND CLIMB 1 POWER NR 3 FLAMED OUT, NO INDICATIONS IN COCKPIT. NO ATTEMPT TO RESTART ENG, RETURNED TO SLC. METAL ON ENG 3 MASTER CHIP DE
- [SDR TWAA9701201](https://openairdocs.org/sdr/TWAA9701201), Jan 26, 1997: FUEL SHUTOFF VLV. LEAKING. STL - DURING APPROACH, SHUT DOWN NR 3 ENGINE, S/N 4472, DUE TO NO THRUST LEVER RESPONSE. FOUND HIGH PRESSURE FUEL SHUTOFF VALVE, MFG P/N MSC102MK2, LEAKING AT S
- [SDR DLL10970140](https://openairdocs.org/sdr/DLL10970140), Jan 24, 1997: FUEL FLOW REG. MALFUNCTIONED. TAILPIPE FIRE NR 3 ENG AT THE START OF T/O ROLL. ACCOMPLISHED EMERGENCY PROCEDURES AND FOLLOW UP ITEM IN POM. SPEED NEVER EXCEED 10 KTS, NO ENGINE PARAMETERS EX
- [SDR DLL13970139](https://openairdocs.org/sdr/DLL13970139), Jan 23, 1997: ENGINE. TAILPIPE FIRE. NR 1 ENG TAILPIPE FIRE. INSPECTED NR 1 ENG, FOUND OK. RAN ENG, CHECKED OK.
- [SDR DLL13970081](https://openairdocs.org/sdr/DLL13970081), Jan 16, 1997: ENGINE. FAILED. ON DESCENT, WHEN IDLING BACK THE CABIN FILLED WITH AN ODOR OF KEROSENE. REPLACED NUMBER THREE ENGINE.
- [SDR DLL10962547](https://openairdocs.org/sdr/DLL10962547), Nov 19, 1996: ENGINE. MALFUNCTIONED. NR 2 ENG EPR GRADUALLY ROLLED BACK ON CLIMBOUT. OTHER ENGINE PARAMETERS FOLLOWED, FUEL AMP NO HELP.
- [SDR DLL10962496](https://openairdocs.org/sdr/DLL10962496), Nov 11, 1996: BREATHER TUBE. BROKEN. NR 2 ENGINE HAD OIL LOST IN CRUISE, FOUND OIL BREATHER TUBE BROKEN ABOVE C1 PUMP.
- [SDR DLL10962431](https://openairdocs.org/sdr/DLL10962431), Nov 1, 1996: FUEL FLOW REG. MALFUNCTIONED. ENG NR 2 FLAMED OUT SHORTLY AFTER TAXIING CLEAR OF RUNWAY AFTER LANDING, WAS VERY HARD TO START. REPLACED FFR ON NR 2 ENG, ENG STARTS NORMALLY. PERFORMED CKS PE
- [SDR DLL10962379](https://openairdocs.org/sdr/DLL10962379), Oct 23, 1996: GEAR BOX. FAILED. ENGINE NR 2 SHUT DOWN IN FLT DUE TO INSTANT LOSS OF OIL QUANTITY. SERVICED ENG WITH OIL, OIL LEAKING FROM STARTER PAD CLAMP. REMOVED ACCESSORY DRIVE CHIP DETECT
- [SDR 96ZZZM1286](https://openairdocs.org/sdr/96ZZZM1286), Aug 10, 1996: ENGINE. FAILED. RIA - FLT 715 - KLAX-PHOG - THREE HOURS INTO FLIGHT NR 1 ENGINE OIL QTY DOWN TO 5 QUARTS AND OIL PRESSURE BELOW 35 PSI. ENGINE WAS SHUTDOWN AND A/C DIVERTED INT
- [SDR TWAA9616002](https://openairdocs.org/sdr/TWAA9616002), Aug 4, 1996: ENGINE. MALFUNCTIONED. LAX - DURING CLIMB, NR 3 ENGINE, S/N 4456 EXPERIENCED HIGH AVM. ENGINE WAS SHUT DOWN. INLET AND EXHAUST WERE CHECKED, CHIP DETECTORS CHECKED, AND GEARBOX WAS DR
- [SDR 96ZZZX3857](https://openairdocs.org/sdr/96ZZZX3857), Jul 17, 1996: ENGINE. FAILED. ON RIA, FLT 711A, MIA/YQX - DURING CLIMB-OUT, NR 2 ENGINE EXPERIENCED HIGH AVM ON BOTH CHANNELS (AVM FOLLOWED THROTTLE). ACFT RETURNED TO MIA. ON GROUND, MAINTE
- [SDR 96ZZZM1175](https://openairdocs.org/sdr/96ZZZM1175), Jun 30, 1996: ENGINE. FAILED. LAX - FLT 150 - DURING CLIMB, SHUT DOWN NR 2 ENGINE, S/N 4813, DUE TO HIGH VIBRATION MONITORING. FOUND METAL PARTICLES IN TAILPIPE. REPLACED ENGINE. ENGINE OPER

All 57: https://openairdocs.org/engine/rolls-royce-rb211-22b-series/reports.md

## 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-rb211-22b-series/pma.md

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