# Rolls-Royce RB211-22B-02

- Type: Engine model (FAA registry)
- Registry code: 54035
- Manufacturer (registry): ROLLS-ROYC
- Model: RB211-22B-02
- Engine type: Turbo-fan
- Power: 41,030 lb thrust
- Data sheet: [TCDS E12EU](https://openairdocs.org/tcds/E12EU) (OpenAirDocs)
- Holder: Rolls-Royce Deutschland Ltd & Co KG
- Installed in: 1 registered aircraft
- Page: https://openairdocs.org/engine/rolls-royce-rb211-22b-02

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 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 (1)

- [N31019](https://openairdocs.org/aircraft/N31019): [Save A Connie Inc DBA](https://openairdocs.org/faa-owner/SAVE%20A%20CONNIE%20INC%20DBA), [Kansas City, MO](https://openairdocs.org/faa-place/MO/Kansas%20City), built 1974, S/N 193B-1066

## 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 (211, newest 50)

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

- [SDR CA030526002](https://openairdocs.org/sdr/CA030526002), May 25, 2003: BLADE. DAMAGED. (CAN) AIRCRAFT RETURNED TO STATION AFTER TAKE OFF DUE TO NR 3 ENGINE HIGH VIBRATION ( 2.5 UNITS ) DURING CLIMB. ENGINE WAS SHUT DOWN AND THE AIRCRAFT RETURNED T
- [SDR WRNA200300010](https://openairdocs.org/sdr/WRNA200300010), May 21, 2003: FIRE LOOP. FALSE ACTIVATION. AFTER TAKE OFF AND DURING CLIMB OUT A FULL FIRE INDICATION ON NR 3 ENGINE. LOOP A & B ON, FIRE HANDLE ON, FIREBELL ON. ENGINE WAS SHUTDOWN, FIRE INDICATION OFF 
- [SDR WRNA200300011](https://openairdocs.org/sdr/WRNA200300011), May 21, 2003: PRESSURE SWITCH. LEAKING. DURING CLIMB/CRUISE FULL FIRE INDICATION ON ENG NR 3, LOOP A&B ON, FIRE HANDLE ON, FIRE BELL ON. ENGINE WAS SHUTDOWN, FIRE INDICATIONS OFF IMMEDIATELY AFTER ENG
- [SDR CA030428001](https://openairdocs.org/sdr/CA030428001), Apr 21, 2003: HOSE. LEAKING. (CAN) CREW REPORTED OXYGEN CYLINDER PRESSURE LOW ON ARRIVAL. DURING INVESTIGATION MAINTENANCE FOUND THE LP OXYGEN LINE LEAKING AT THE BOTTLE. LINE WAS REPLACED 
- [SDR CA030317002](https://openairdocs.org/sdr/CA030317002), Mar 16, 2003: VALVE. OPEN. (CAN) LOSS OF CABIN PRESSURE AT FL 310. CABIN RATE OF CLIMB 1500 FPM. RAPID DEPRESSURIZATION DRILL WAS CARRY OUT. WITH CROSS BLEED CLOSED CABIN CAME BACK TO NOR
- [SDR CA021223007](https://openairdocs.org/sdr/CA021223007), Dec 22, 2002: ADC. MALFUNCTIONED. (CAN) SHORTLY AFTER T/O (A/C RETURNED), THE FOLLOWING INDICATIONS CAME UP ON F/O'S SIDE: MACH FLAG IN A/S INDICATOR, SSC FLAG IN ALTIMETER, F/D FLAG IN ADI, OFF
- [SDR CA030113015](https://openairdocs.org/sdr/CA030113015), Nov 23, 2002: ACCESS DOOR. SEPARATED. (CAN) ON ARRIVAL IN YYZ FROM FLIGHT 651 (PVR-YYZ), NR 1 ENGINE START CONTROL VALVE ACCESS PANEL WAS MISSING. NO DAMAGE TO COWLING. MTCE REPLACED THE DOOR IAW AM
- [SDR WRNA200200007](https://openairdocs.org/sdr/WRNA200200007), Oct 22, 2002: FIRE LOOP. SHORTED. Enroute to BDL @ approx. 270fl, A&B fire loop on #1 engine came on. Engine fire lights came on and fire bell. Bell silenced, #1 engine shutdown per procedures. 
- [SDR CA021108018](https://openairdocs.org/sdr/CA021108018), Oct 16, 2002: ACTUATOR. CRACKED. (CAN) WHILE PERFORMING A MLG RETRACTION TEST, AFTER REPLACEMENT OF ALL GEARS ON A/C, WE NOTICED AFTER A COUPLE RETRACTIONS, THAT THE MLG ACTUATOR PIN (P/N 15230
- [SDR CA021110003](https://openairdocs.org/sdr/CA021110003), Oct 10, 2002: CONTROL BOX. FAILED. (CAN) CENTER CARGO LT SIDE CIRCUIT BREAKER ON CONTROL RELAY BOX ASSEMBLY POPPED WHEN RESELECTED (PUSHED IN), SPARKS OCCURRED INSIDE OF THE CONTROL RELAY BOX NEA
- [SDR CA020705006](https://openairdocs.org/sdr/CA020705006), Jun 22, 2002: ACTUATOR. CRACKED. (CAN) FOUND LT MLG DOOR ACTUATOR CRACKED .250 INCHES AND LEAKING (CONFIRMED BY NDT), IN DOOR CLOSED POSITION. MAINTENANCE REPLACED THE ACTUATOR IAW AMM 32-33-01
- [SDR CA020527007](https://openairdocs.org/sdr/CA020527007), May 19, 2002: SHAFT. SHEARED. (CAN) 'D1' HYD SYSTEM PRESSURE AT 0 PSI WITH SWITCH LATCHED IN LOW PRESSURE LIGHT ON . NO HYD QUANTITY LOSS, NO HIGH TEMP 'CD' PTU SELECTOR TO BRING SYSTEM PRES
- [SDR CA020527003](https://openairdocs.org/sdr/CA020527003), May 17, 2002: ENGINE. VIBRATION. (CAN) ENGINE NR 3, AT 22 000 FT, THE VIB. CHANNEL A + B , 2.6 TO 2.8 UNITS. ENGINE SHUT DOWN WAS CARRIED OUT PER QRH. AT TAKE OFF , THE VIB. WAS AT 2.0 TO 2.2 U
- [SDR CA020426005](https://openairdocs.org/sdr/CA020426005), Apr 20, 2002: PIN. CORRODED. (CAN) DURING WALK AROUND , FOUND NR 3 ENGINE GLOVE FAIRING ADRIFT. GLOVE FAIRING FOUND RETAINED BY TWO LANYARD AND PIP PIN NOT IN PLACE FOR SECURITY. THE PIN WA
- [SDR CA020308004](https://openairdocs.org/sdr/CA020308004), Mar 8, 2002: SLEEVE. BROKEN. (CAN) DURING WALKAROUND FOUND NLG UPPER TORQUE LINK RT DETENT SLEEVE BROKEN IN TWO. REPLACED UPPER TORQUE LINK'S RT SPRING, INDEX AND DETENT SLEEVES AND A/C WAS
- [SDR CA020221018](https://openairdocs.org/sdr/CA020221018), Feb 2, 2002: FAN BLADE. DAMAGED. (CAN) SHORTLY AFTER TAKEOFF NR 2 ENGINE N1 INDICATION SHOWED 10 PERCENT HIGHER THAN NR 1 AND 3 ENGINES. ALL PARAMETERS WERE THE SAME. WHEN THRUST WAS REDUCED TO
- [SDR CA020117007](https://openairdocs.org/sdr/CA020117007), Jan 11, 2002: BULKHEAD. CRACKED. (CAN) CRACK FOUND ON PRESSURE BULKHEAD 1363 AT RBL 44.5 & WL 130. STIFFENERS SURROUNDING CRACK REMOVED FOR ACCESS IN ACCORDANCE WITH S.R.M. 51-40-01. CRACK STOP
- [SDR ARWA20020110](https://openairdocs.org/sdr/ARWA20020110), Jan 10, 2002: ENGINE. MALFUNCTIONED. NR 2 ENGINE STARTS AFTER 2 MINUTES ENGINE ROLL BACK TO ZERO AND SHUT DOWN.
- [SDR CA020111002](https://openairdocs.org/sdr/CA020111002), Dec 9, 2001: BLOCKER DOOR. BROKEN. (CAN) FOUND NR 2 ENGINE NOZZLE COLLECTOR DAMAGED, ONE BLOCKER DOOR MISSING. BLOCKER DOOR BROKEN IN TWO PIECES AT HINGE AND ONE PIECE DAMAGE NOZZLE COLLECTOR, RT
- [SDR CA011210024](https://openairdocs.org/sdr/CA011210024), Nov 13, 2001: LENS. LOOSE. (CAN) -THE REFLECTOR HAS BEEN FOUND LOOSE IN LENS OF LIGHT ASSEMBLY CAUSING C/B PANEL NR 2 , K3 POSITION, POPPED DUE TO BULB CONTACT SHORTED TO LIGHT ASSEMBLY B
- [SDR CA011211025](https://openairdocs.org/sdr/CA011211025), Sep 7, 2001: WIRE. BURNED. (CAN) LOWER GALLEY ZONE 130 , OVEN FEEDER 1-5 (CB11) PHASE "A" WIRE AT TB 2531-1 TERMINAL NR 5 FOUND BURNED OUT.
- [SDR CA010823002](https://openairdocs.org/sdr/CA010823002), Aug 19, 2001: ACM. CONTAMINATED. (CAN) DURING TAXI NR 2 AIR CONDITIONING SYSTEM BECAME NOISY. LOUD GRINDING NOISE WAS NOTICED IN THE FLIGHT DECK. SMOKE AND ODOUR WERE NOTICED IN THE CABIN. NR 2
- [SDR CA010823007](https://openairdocs.org/sdr/CA010823007), Aug 19, 2001: SWITCH. SHORTED. (CAN) DURING TAXI, NR 2 AIR CONDITIONING SYSTEM BECAME NOISY AND PRODUCING SMOKE AND ODOUR IN THE CABIN. NR 2 PACK WAS SHUT DOWN. EMERGENCY EVACUATION WAS EXECU
- [SDR CA010808060](https://openairdocs.org/sdr/CA010808060), Aug 1, 2001: ROD. STIFF. (CAN) AFTER TAKE OFF, LEFT HAND NOSE GEAR DOOR WOULD NOT RETRACT. AIRCRAFT RETURNED TO THE STATION. FOUND THE LEFT HAND GEAR DOOR ROD ACTUATOR VERY STIFF. UNIT 
- [SDR CA010704021](https://openairdocs.org/sdr/CA010704021), Jun 29, 2001: FUEL BOWL. CRACKED. (CAN) AFTER ARRIVAL IN PUJ NOT ABLE TO START APU, ON WALK AROUND FOUND FUEL LEAK COMING FROM APU, INVESTIGATED FOUND FUEL BOWL COVER LEAKING. MAINTENANCE REPLAC
- [SDR CA010704019](https://openairdocs.org/sdr/CA010704019), Jun 19, 2001: FUEL BOWL. CRACKED. (CAN) ON PREPARING AIRCRAFT FOR DEPARTURE MAINTENANCE EXPERIENCED AN APU HUNG START ABORTED, ON INVESTIGATION FOUND APU FILTER BOWL CRACKED. 3RD OCCURANCE OF DE
- [SDR CA010704020](https://openairdocs.org/sdr/CA010704020), Jun 13, 2001: HEAT EXCHANGER. CRACKED. (CAN) FUEL LEAK AT HEAT EXCHANGER CORE.
- [SDR CA010531007](https://openairdocs.org/sdr/CA010531007), May 8, 2001: FUEL BOWL. CRACKED. (CAN) DURING THE TAXI IN THE AIRCRAFT LOST APPROXIMATELY 600 LBS OF FUEL. MAINTENANCE FOUND FUELLEAK FROM APU. UPON INSPECTION FOUND THAT THE FUEL WAS COMING FR
- [SDR CA010706004](https://openairdocs.org/sdr/CA010706004), Apr 29, 2001: SWITCH. FAILED. (CAN) AFTER DEPARTURE FROM YMX, THE TRUCK LIGHT CAME ON, NORMAL PROCEDURES WHERE NOT TO RETRACT THE GEAR, CREW DUMPED FUEL AND RETURNED TO BASE. FOUND TRUCK SWI
- [SDR 2001F00004](https://openairdocs.org/sdr/2001F00004), Apr 14, 2001: O-RING. PINCHED. NR 3 ENGINE OIL QUANTITY DROPPED TO 1 QUART, OIL PRESSURE FLUCTUATED BUT DID NOT DROP BELOW 35 PSI. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND DAMAGED (PINCHED) O-
- [SDR CA010430015](https://openairdocs.org/sdr/CA010430015), Apr 7, 2001: RETAINER. BROKEN. (CAN) AFTER TAKEOFF AT 20,000 FEET, AIRCRAFT EXPERIENCED PRESSURIZATION PROBLEMS AND CREW COULD HEAR A KNOCKING SOUND AGAINST THE FUSELAGE ON THE RT SIDE. CREW 
- [SDR CA010430016](https://openairdocs.org/sdr/CA010430016), Apr 7, 2001: ENGINE. FAILED. (CAN) DRUING FLIGHT ENGINE NR 1 EXPERIENCED A SUDDEN VIBS INCREASE TO 3.5 UNITS ON BOTH CHANNELS A & B, WARNING LIGHTS CAME ON, ENGINE SHUT DOWN WAS ACCOMPLISHE
- [SDR CA010402012](https://openairdocs.org/sdr/CA010402012), Mar 3, 2001: PROXIMITY SENSOR. FAULTY. (CAN) DURING APPROACH AT YMX, NO GREEN LIGHT ILLUMINATE ON LT MLG DOWN & LOCK, PROXIMITY SENSOR AT FAULT, R&R C/OUT, GEAR WING C/OUT, CHECK SERVICEABLE.
- [SDR CA010402010](https://openairdocs.org/sdr/CA010402010), Mar 1, 2001: LIGHT. SHORTED. (CAN) AFT LOWR GALLEY CEILING LIGHT SHORT OUT (FIRST LIGHT ASSY IN FRONT OF GALLEY LIFT) CAUSING SMELL OR SMOKE IN CABIN.
- [SDR CA010402011](https://openairdocs.org/sdr/CA010402011), Feb 28, 2001: FUEL LINE. LEAKING. (CAN) STEEL BRAIDED FLEX FUEL SUPPLY LINE, NR 2 ENGINE & APU, IN HYDRAULIC SERVICE CENTER COMPARTMENT LEAKING APPROXIMATELY 3 FEET FROM FORWARD END DUE TO INTER
- [SDR CA010307015](https://openairdocs.org/sdr/CA010307015), Feb 25, 2001: ENGINE. FAILED. (CAN) AFTER TAKEOFF ENGINE NR 3 VIBS INCREASED TO 2.5 UNITS, THROTTLE RETARDED TO KEEP BELOW LIMITS. AIRCRAFT RETURNED TO MAINTENANCE BASE YMX. TROUBLESHOOTING 
- [SDR CA010307017](https://openairdocs.org/sdr/CA010307017), Feb 18, 2001: ENGINE. VIBRATION. (CAN) AFTER TAKEOFF (DURING FIRST STAGES OF CLIMB) THE NR 2 ENGINE VIBRATION INCREASED, FLIGHT CREW SHUTDOWN ENGINE IN ACCORDANCE WITH OPERATING PROCEDURE AND R
- [SDR CA010307016](https://openairdocs.org/sdr/CA010307016), Feb 16, 2001: PUMP. CRACKED. (CAN) IN CRUISE AT FL300, HYDRAULIC SYSTEM C, LOST OF PRESSURE, EDP SHUT-OFF ACTIVATED BY FLIGHT CREW AND GEARS EXTENDED USING MANUAL SYSTEM. MAINTENANCE FOUND 
- [SDR DLL10002204](https://openairdocs.org/sdr/DLL10002204), Nov 10, 2000: COVER. LEAKING. OIL QTY ON NR 1 ENGINE WENT TO ZERO AND OIL PRESS DROPPED INTO RED. SHUT DOWN ENG AT 1925Z. (ENG SHUT DOWN 18 MIN PRIOR TO LANDING). OIL TEMP REMAINED THE SAME 
- [SDR CA001212004](https://openairdocs.org/sdr/CA001212004), Nov 7, 2000: CONNECTOR. SHORTED. (CAN) NR2 INBOARD FUEL BOOST PUMP C/B POPPED DURING FLIGHT.INVESTIGATION FOUND CANNON PLUG TO PUMP HOUSING PLUG IN TO BE SEVERELY BURNT AND ARCED.SYSTEM DE-ACTI
- [SDR CA010103019](https://openairdocs.org/sdr/CA010103019), Nov 2, 2000: SEPARATOR. BLOCKED. (CAN) DURING CLIMB OUT ALL LAVATORYS SMOKE DETECTORS ALARM CAME ON. OIL ODOR IN COCKPIT.ISOLATION VALVE NR 1 AND NR 2 CLOSED AND OIL ODOR WAS ELIMINATED. OIL RE
- [SDR DLL10002139](https://openairdocs.org/sdr/DLL10002139), Oct 31, 2000: ACM. SMOKE. OILY SMOKE IN AFT CABIN ON CLIMBOUT. ISOLATED NR 1 ENG AND PACK, SMOKE DISSIPATED. FOLLOWED AIR CONDITIONING SMOKE PROCEDURE IN POM. ENDED UP WITH 1 PACK OFF AN
- [SDR CA001107004](https://openairdocs.org/sdr/CA001107004), Oct 28, 2000: WIRE. BROKEN. (CAN) DURING CRUISE LOST BOTH FORWARD AND AFT OUTFLOW VALVE AUTO CONTROL, COMPLETED FLIGHT ON MANUAL MODE.6 WIRES WERE FOUND BROKEN IN THE CONNECTOR PLUG BACK S
- [SDR DLL10002127](https://openairdocs.org/sdr/DLL10002127), Oct 27, 2000: HOUSING. LEAKING. NR 1 ENG OIL QTY DROPPED FROM 16 TO 4 QTS IN 1.5 HRS OIL QTY DECREASED TO ZERO, ENGINE SHUTDOWN PER POM 23-107. RAPID DECREASE IN OIL QTY OIL PRESS REMAINED ABO
- [SDR CA001102003](https://openairdocs.org/sdr/CA001102003), Oct 13, 2000: CONNECTOR. WRONG PART. (CAN) DURING DEFECT TROUBLE SHOOTING OF THE YAW SAS 2 FAIL & RUDDER HYDRAULIC LIMITER FOUND WRONG PART INSTALLED, (UNION WITH OUT A RESTRICTOR), INSTALLED ON TH
- [SDR CA001102002](https://openairdocs.org/sdr/CA001102002), Oct 8, 2000: CIRCUIT BREAKER. FAILED. (CAN) SPARKS WHERE SEEN COMING FROM LT MID GALLEY SERVICE OUTLET DURING TAKEOFF, CIRCUIT BREAKERS J19 & C13 PULLED AND COLLARED. SYSTEM DE-ACTIVATED AND AIRCRAF
- [SDR CA001005016](https://openairdocs.org/sdr/CA001005016), Sep 7, 2000: ACTUATOR. CRACKED. (CAN) DURING TAKEOFF ROLL (80 KNTS), HYDRAULIC ''C'' SYSTEM LOST ALL FLUID. A/C RETURN TO GATE. INVESTIGATION FOUND LOWER FLANGE OF LT MLG ACTUATOR CRACKED AT E
- [SDR CA000830002](https://openairdocs.org/sdr/CA000830002), Aug 12, 2000: CABLE. SHEARED. (CAN) AUGUST 17,2000 AFTER LANDING IN BORDEAUX THE CREW COULD NOT DEPLOY THE NR2 ENGINE TR EVEN WHEN THE TR UNLOCK LIGHT WAS ON.AFTER ENGINE SHUTDOWN FOUND THAT
- [SDR CA001004008](https://openairdocs.org/sdr/CA001004008), Aug 12, 2000: CABLE. BROKEN. (CAN) AUGUST 17, 2000 AFTER LANDING IN BORDEAUX THE CREW COULD NOT DEPLOY THE NR 2 ENGINE TR EVEN WHEN THE TR UNLOCK LIGHT WAS ON.AFTER ENGINE SHUT DOWN FOUND T
- [SDR CA000830013](https://openairdocs.org/sdr/CA000830013), Aug 11, 2000: INDICATOR. MALFUNCTIONED. (CAN) DURING CRUISE F/E STARTED TO SMELL SMOKE AND SAW SPARKS COMING FROM THE NR 2 ENGINE OIL QTY GAUGE, MANUALLY PULLED C.B. INDICATOR STOPPED SPARKING.AIRCRAF

All 211: https://openairdocs.org/engine/rolls-royce-rb211-22b-02/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
- [STC SE1516CE](https://openairdocs.org/stc/SE1516CE): Modification of lower fuel control box assembly to incorporate vibration isolators. Trans World Airlines Inc

## 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-02/pma.md

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