# Rolls-Royce RB211-524B402

- Type: Engine model (FAA registry)
- Registry code: 54040
- Manufacturer (registry): ROLLS-ROYC
- Model: RB211-524B402
- Engine type: Turbo-fan
- Power: 49,120 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-rb211-524b402

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 2015-16-03](https://openairdocs.org/ad/2015-16-03): High-pressure turbine (HPT) blades · Rolls-Royce RB211-524B-02, RB211-524B2-19, RB211-524B3-02 and 6 more. Effective Sep 15, 2015
- [AD 2013-16-23](https://openairdocs.org/ad/2013-16-23): Cracked and distorted FCL metering panel · Rolls-Royce RB211-524B-02, RB211-524B2-19, RB211-524B3-02 and 13 more. Effective Oct 8, 2013
- [AD 2011-18-21](https://openairdocs.org/ad/2011-18-21): Combustion liners · Rolls-Royce RB211-524B-02, RB211-524B2-19, RB211-524B2-B-19 and 19 more. Effective Feb 13, 2012
- [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 2008-16-18](https://openairdocs.org/ad/2008-16-18): High Pressure (HP) turbine disc · Rolls-Royce RB211-524B-02, RB211-524B-B-02, RB211-524B2-19 and 20 more. Effective Sep 15, 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 2007-14-07](https://openairdocs.org/ad/2007-14-07): Fluorescent penetrant inspections (FPI) · Rolls-Royce RB211-524B-02, RB211-524B-B-02, RB211-524B2-19 and 21 more. Effective Aug 16, 2007
- [AD 2007-06-10](https://openairdocs.org/ad/2007-06-10): Intermediate pressure compressor (IPC) stage 5 disks · Rolls-Royce RB211-524B-02, RB211-524B-B-02, RB211-524B2-19 and 20 more. Effective Apr 19, 2007
- [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 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 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 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 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 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

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 2004-26-05](https://openairdocs.org/ad/2004-26-05) (historical): Head section and meterpanel assembly of the combustion liner · Rolls-Royce RB211-524B-02, RB211-524B-B-02, RB211-524B2-19 and 20 more. Effective Feb 9, 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 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 (102, newest 50)

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

- [SDR 1LSM2010LVS01](https://openairdocs.org/sdr/1LSM2010LVS01), Nov 22, 2010: ACTUATOR. STICKING. SHORTLY AFTER ROTATION ON TAKEOFF, NR 1 ENGINE COMPRESSOR STALLED & SURGED, TOWER REPORTED SEEING FLAMES FROM TAIL PIPE. ENGINE SHUTDOWN, SECURED & FIRE BOTTLE 
- [SDR ARWA20040103](https://openairdocs.org/sdr/ARWA20040103), Jan 19, 2004: LINER. DAMAGED. ENGINE NR 3 EXPERIENCED A SLOW INCREASE IN VIBRATION FROM 105 TO 218 UNITS IN 3 MINUTES WITH A OR B SELECTED. ALL OTHER PARAMETERS NORMAL. INSPECT MASTER AND IN
- [SDR ARWA20030706](https://openairdocs.org/sdr/ARWA20030706), Jul 11, 2003: COMPRESSOR. DAMAGED. LOG PAGE 23902 NR 3 ENGINE VIBRATION 4 UNITS BOTH A & B CHANNELS IN NORMAL POSITION NR 3 ENGINE SHUTDOWN AT 1340 Z. INSPECTED NR 3 ENGINE; FOUND METAL ON EXHAUS
- [SDR CA030704001](https://openairdocs.org/sdr/CA030704001), Jul 3, 2003: LINE. RUPTURED. (CAN) DURING CLIMB-OUT, A COMPLETE (RAPID) LOSS OFB HYD SYS OCCUR. THE AIRCRAFT RETURNED TO THE STATION WITH NO FURTHER PROBLEM. DURING INVESTIGATION THE (B PRE
- [SDR ARWA20030601](https://openairdocs.org/sdr/ARWA20030601), Jun 10, 2003: ENGINE. VIBRATION. ABORTED TAKE OFF AT 130 KTS 470,000 LBS DUE TO NR 3 ENGINE VIBRATION WARNING AT 2.8 UNITS. BRAKES OK, TIRES OK. RETURNED TO RAMP. LUBED FAN BLADES, PERFORMED IN
- [SDR CA030428003](https://openairdocs.org/sdr/CA030428003), Apr 27, 2003: OIL CAP. LEAKING. (CAN) DURING ENGINE START NR 3 ENGINE OIL CAP WAS LEAKING FROM THE CENTER. OIL CAP WAS REPLACED AND SYSTEM CHECKED SERVICEABLE.
- [SDR CA030317003](https://openairdocs.org/sdr/CA030317003), Mar 16, 2003: ELECTRICAL BOX. BURNED. (CAN) FLIGHT CREW REPORTED BURNING ODOR IN CABIN BETWEEN ROW 22 AND 28.MAINTENANCE FOUND THE SEAT ELECTRONIC BOX (SEB) AT FAULT. UNIT WAS REPLACED AND SYSTEM TE
- [SDR CA030304001](https://openairdocs.org/sdr/CA030304001), Mar 3, 2003: LANDING GEAR. MALFUNCTIONED. (CAN) AFTER GEAR SELECTED DOWN , THE INTRANSIT LIGHT WAS ON, ALL OTHER GEARS AND DOORS LIGHT WERE OFF. GEARS DID NOT EXTEND. ALTERNATE GEAR EXTENSION PROCEDURE 
- [SDR CA030228005](https://openairdocs.org/sdr/CA030228005), Feb 22, 2003: FAN. SEIZED. (CAN) TROUBLE SHOOTING WAS CARRIED OUT BY MAINTENANCE ON ALL CABIN INTERIOR ELECTRICAL SYSTEMS. UNABLE TO DUPLICATE. ALL CABIN SYSTEMS CHECKED SERVICEABLE AS IA
- [SDR ARWA20030104](https://openairdocs.org/sdr/ARWA20030104), Jan 22, 2003: ENGINE. VIBRATION. NR 3 ENGINE VIBRATION DURING CRUISE AT 350 FT LOW POSITION A-B 2.8 CAUTION LIGHT ON. SHUTDOWN ENGINE AT 06:35 Z. REMOVE AND REPLACE ALL NR 3 ENGINE C-1 BLADES I
- [SDR ARWA20030103](https://openairdocs.org/sdr/ARWA20030103), Jan 19, 2003: BLADE. DAMAGED. NR 3 ENGINE AT 370 FEET, BOTH CHANNEL A AND B 2.7 CAUTION LIGHT ON. SHUTDOWN ENGINE 1200Z. FEELING THE VIBRATION ON THE FLOOR. REMOVED AND INSPECTED MASTER AND 
- [SDR CA030130005](https://openairdocs.org/sdr/CA030130005), Jan 12, 2003: ENGINE. VIBRATION. (CAN) DURING TAKE OFF, CREW REPORTED NR 1 ENG HIGH VIBRATION, VIBRATION REACHED 5 UNITS ON BOTH CHANNELS. THE ENGINE WAS SHUTDOWN AS PER QRH. ESN 14858 HAD SHOW
- [SDR CA030113004](https://openairdocs.org/sdr/CA030113004), Jan 9, 2003: TUBE. CRACKED. (CAN) HYDRAULIC LEAK RT SIDE FLAP WELL NEAR NR 1 SPOILER ACTUATOR. SPOILER NR 1 PRESSURE HYDRAULIC TUBE, SYSTEM B REPAIRED PER AMM 20-29-02, P801.
- [SDR CA030113013](https://openairdocs.org/sdr/CA030113013), Dec 29, 2002: ENGINE. VIBRATION. (CAN) UPON DEPARTURE OF FLIGHT 703 FROM VRA-YMX, TAKE OFF WAS REJECTED DUE TO NR 3 ENGINE VIBRATION LIGHT CAME ON. DURING TAKE OFF, VIBRATION WAS CONFIRMED ON B
- [SDR CA021227003](https://openairdocs.org/sdr/CA021227003), Dec 16, 2002: ROD END. SHEARED. (CAN) DURING FLIGHT FROM, FLIGHT CREW REPORTED THAT, RUDDER HYD LIMITER ANNUNCIATOR AND RUDDER LIMITER HYDRAULIC PUSH LIGHTS ON, FLAPS 4 DEGREES, AIRSPEED 190 K
- [SDR CA030113012](https://openairdocs.org/sdr/CA030113012), Dec 14, 2002: FUEL TANK. CONTAMINATED. TANK 2R INBD, QTY HIGHER THAN NORMAL WITH QTY SWITCH LIGHT LATCHED IN. FUEL QTY GAUGES OK. INBD QTY READS 4000 LBS, WITH TOTAL BELOW 7000LBS. PER FAULT ISOLATIO
- [SDR CA021223006](https://openairdocs.org/sdr/CA021223006), Dec 5, 2002: PROXIMITY SENSOR. FAILED. (CAN) A/C ABORTED TAKE OFF AND RETURNED TO THE GATE DUE TO UNSAFE TAKE OFF WARNING RT SLAT NR 3 GREEN LIGHT 'OFF', ON THE FLIGHT ENGINEER PANEL AND LEADING EDGE
- [SDR CA030112010](https://openairdocs.org/sdr/CA030112010), Dec 5, 2002: SENSOR. FAILED. (CAN) AT 5:45 HRS LOCAL , FLIGHT 044, REJECTED T/O AT 90 KNOTS, DUE TO UNSAFE T/O WARNING HORN RELATED TO SLAT MALFUNCTION. THE PROXIMITY CARD A12 (P/N 805006, 
- [SDR CA030112003](https://openairdocs.org/sdr/CA030112003), Nov 30, 2002: SKIN. DAMAGED. (CAN) DURING WALK AROUND IN YYZ, MTCE FOUND THE LT STABILIZER TRAILING EDGE TIP SKIN DAMAGED. A REPAIR WAS CARRIED OUT IAW SRM 55-22-00. LOOSE RIVITS REPLACED I
- [SDR CA030112007](https://openairdocs.org/sdr/CA030112007), Nov 24, 2002: DUCT. SEPARATED. (CAN) A DEPRESSURIZATION OCCURRED AT 21000 , ABNORMAL PROCEDURE CARRIED PER QRH. LOUD NOISE HEARD IN FLIGHT DECK DURING APPROACH. FOUND NR 2 WATER SEPARATOR DUC
- [SDR CA021117001](https://openairdocs.org/sdr/CA021117001), Nov 16, 2002: DUCT. CHAFED. (CAN) IN HANGAR, AT ENGINE INSTALLATION DURING RE CONNECTION OF THE INTERMEDIATE PRESSURE, (IP) DUCT INSIDE THE PYLON NR 3 AREA IT WAS NOTICED THAT THE FLEXIBLE
- [SDR CA021001013](https://openairdocs.org/sdr/CA021001013), Sep 26, 2002: HOSE. CRACKED. (CAN) THE 'MEDIUM PRESSURE OXYGEN HOSE ASSY AT THE OXYGEN CYLINDER HOOKUP PANEL, WAS FOUND TO DAMAGED. THIS FLEXIBLE BRAID LINE WAS FRAYED AT THE PANEL CONNECTI
- [SDR CA020912004](https://openairdocs.org/sdr/CA020912004), Sep 7, 2002: BLOCKER DOOR. BENT. (CAN) ENGINE NR 3, BLOCKER DOOR AT 5 O`CLOCK POSITION BENT ACROSS ITS WIDTH. MAINTENANCE REPLACED THE BLOCKER DOOR PER AMM 78-31-16
- [SDR CA020912001](https://openairdocs.org/sdr/CA020912001), Sep 3, 2002: WIRE HARNESS. CHAFED. (CAN) NR 2 PACK RAM AIR LOUVER WILL NOT POSITION PROPERLY ON GROUND, IN FLIGHT IT STAYS AT ONE O`CLOCK POSITION. C/B TRIPPED WHEN PACK NR 2 IS OPERATED IN MANUA
- [SDR CA020829015](https://openairdocs.org/sdr/CA020829015), Aug 27, 2002: ENGINE. VIBRATION. (CAN) AFTER TAKE OFF, THE NR 3 THROTTLE WAS RETARDED, THE ENGINE WAS SHUT DOWN DUE TO HIGH VIBRATIONS (2.5 2.7 UNITS) , CHANNEL A&B FROM LOW CHANNEL. THE AIRCRA
- [SDR CA020829016](https://openairdocs.org/sdr/CA020829016), Aug 26, 2002: BLOCKER DOOR. BENT. (CAN) FOUND NR 1 ENGINE THRUST REVERSER BLOCKER DOOR AT THE 8 O`CLOCK POSITION, DAMAGED AND THE TRANSLATING SLEEVE NOT CLOSED PROPERLY (GAP TO LARGE). MAINTENAN
- [SDR CA020912002](https://openairdocs.org/sdr/CA020912002), Aug 24, 2002: WIRE HARNESS. DAMAGED. (CAN) APU FAILS TO START, NO ROTATION. AIRCRAFT RELEASED PER MEL 49-00-01. BLEED AIR VALVE CONFIRMED CLOSED. CHECKED CURRENT LIMITER AND FOUND SERVICEABLE. RERA
- [SDR CA020820009](https://openairdocs.org/sdr/CA020820009), Aug 18, 2002: TUBE. CRACKED. (CAN) CREW REPORTED AFT CABIN BURNING ODOR WITH WHITE SMOKE NEAR AFT GALLEY LT CABIN DOOR AREA. THE AFT GALLEY POWER WAS TURNED OFF IN FLIGHT BY CREW AND THE SI
- [SDR CA020820010](https://openairdocs.org/sdr/CA020820010), Aug 18, 2002: MANIFOLD. CRACKED. (CAN) DURING NORMAL MAINTENANCE OPERATION, THE MAIN LANDING GEAR CONTROL MODULE IN THE HYDRAULIC SERVICE CENTER, WAS FOUND LEAKING BECAUSE THE MAIN LANDING GEAR
- [SDR CA020829017](https://openairdocs.org/sdr/CA020829017), Aug 18, 2002: CONTROLLER. FAILED. (CAN) THE AIRCRAFT WAS FLYING AND DIVERTED DUE TO NR 2 PACK UNABLE TO CONTROL IN MANUAL MODE WHILE THE AUTO MODE WAS UNDER MEL 21-21-01 CATC. MAINTENANCE REPLAC
- [SDR CA020816003](https://openairdocs.org/sdr/CA020816003), Aug 12, 2002: FAIRING. MISSING. (CAN) UPON ARRIVAL, THE CREW NOTICED THAT THE C2 CARGO DOOR FAIRING ASSY. WAS MISSING. FURTHER INVESTIGATION REVEALED THAT C2 CARGO PANEL ASSY DOOR FAIRING , TO
- [SDR CA020816001](https://openairdocs.org/sdr/CA020816001), Aug 10, 2002: SENSOR. MISSING. (CAN) LEFT ALPHA AIR DATA SENSOR HEAT OFF LEGEND CAME ON IN FLIGHT. ON ARRIVAL IT WAS FOUND THAT THE AOA VANE WAS MISSING. AN INSPECTION OF THE WING AND STABILI
- [SDR CA020708003](https://openairdocs.org/sdr/CA020708003), Jun 25, 2002: MODULE. CRACKED. (CAN) AIRCRAFT(IN MANCHESTER) RETURNED TO RAMP DUE TO B HYD SYSTEM LEAK FROM LT BRAKE MODULE. MAINTENANCE DISCOVERED THAT THE UNIT WAS CRACKED 2.5 INCHES JUST O
- [SDR CA020705005](https://openairdocs.org/sdr/CA020705005), Jun 23, 2002: SIGNAL COND UNIT. MALFUNCTIONED. (CAN) IN CLIMB, EPR 1.515, ENG NR 2 , VIBRATION CONFIRMED ON BOTH CHANNELS, 4.2 INDICATED, CAUSED IN-FLT SHUTDOWN. -ALL MCD INSP & NO CONTAMINATION FOUND PER AM
- [SDR CA020705004](https://openairdocs.org/sdr/CA020705004), Jun 18, 2002: DECODER. FAILED. (CAN) WHILE PERFORMING READING LIGHT TEST, BURNING ODOR COMING FROM AREA AROUND SEAT ROWS 26 ABC TO 30 ABC NOTICED. ALL READING LIGHTS WERE WORKING AT TIME & SM
- [SDR CA020527004](https://openairdocs.org/sdr/CA020527004), May 16, 2002: ACCESS PANEL. DEPARTED. (CAN) ON ARRIVAL AT DESTINATION, FOUND INBOARD OF NR 1 ENGINE, INSPECTION PANEL (BLOW OUT), MISSING ( BROKEN AT HINGE LEVEL, REFERENCE IPC 57-33-10,ITEM 272). M
- [SDR CA020429004](https://openairdocs.org/sdr/CA020429004), Apr 19, 2002: ACTUATOR. FAILED. (CAN) WHEN LOWERING THE LANDING GEAR CONTROL LEVER A LOUD BAG WAS HEARD, LT GEAR CONFIRMED DOWN AND LOCK WITH THE OVERWING GEAR POP-UP INDICATOR AND AIRCRAFT LA
- [SDR CA020501009](https://openairdocs.org/sdr/CA020501009), Apr 13, 2002: WINDSHIELD. FAILED. (CAN) CAPTAIN WINDSHIELD HAD MAJOR DELAMINATION IN FLIGHT . THE CREW PROCEDURES WERE CARRIED OUT BY PULLING THE CIRCUIT BREAKER TO DEACTIVATE THE WINDSHIELD HEA
- [SDR CA020408013](https://openairdocs.org/sdr/CA020408013), Apr 2, 2002: CONTROL BOX. FAILED. (CAN) SEAT ELECTRONIC BOX POSITIONED AT ROW 25 DE , STARTED SMOKING. THE SEB WAS DICONNECTED BY THE CREW. MAINTENANCE REPLACED THE UNIT.
- [SDR CA020405027](https://openairdocs.org/sdr/CA020405027), Mar 31, 2002: TUBE. BROKEN. (CAN) WHILE CLIMBING THROUGH FLT LEVEL 290 , NR 2 ENGINE POWER WENT DOWN TO IDLE POWER ONLY. ABNORMAL CHECK LIST CARRIED OUT WITH NO SUCCESS. A/C RETURNED TO YM
- [SDR CA020221017](https://openairdocs.org/sdr/CA020221017), Feb 10, 2002: ENGINE. OVERHEATED. (CAN) 2 MINUTES AFTER LANDING , AFTER THRUST REVERSER STOWING , THE FIRST OFFICER CALLED OUT HIGH TGT RAISING RAPIDALY AND ENGINE RUN DOWN , TEMPERATURE ROSE TO
- [SDR CA020201011](https://openairdocs.org/sdr/CA020201011), Jan 27, 2002: ENGINE. FAILED. (CAN) DURING FINAL APPROACH , FLAPS 33 DEGREES , 160KNOTS ON FLIGHT TSC 372 FROM YMX TO MCO THERE WAS A HIGH VIBRATION ON NR 1 ENGINE AT 3.8 UNITS ON CHANNELS A
- [SDR CA020117015](https://openairdocs.org/sdr/CA020117015), Jan 17, 2002: GEARBOX. SHEARED. (CAN) C1A CARGO DOOR, AFT LIFT GEARBOX SHEARED FROM ATTACHMENT DURING OPENING.
- [SDR CA020110016](https://openairdocs.org/sdr/CA020110016), Jan 7, 2002: UPLOCK SENSOR. OUT OF ADJUST. (CAN) GEAR DOWN APPROACH YYZ, HAD THREE GREEN & RED DOOR LIGHT, FLIGHT ENGINEER LT GEAR OR DOOR LIGHT. FOLLOWED ABNORMAL PROCEDURE 03:18:03 (ALL LIGHTS WENT NOR
- [SDR CA020117014](https://openairdocs.org/sdr/CA020117014), Dec 22, 2001: GYRO. FAILED. (CAN) ON DEPARTURE FROM AUA - YYZ, A MODERATELY STEADY LATERAL AIRFRAME OSCILLATION ( AT APPROXIMATE RATE OF TWO PER SECOND) STARTED AT 180 KNOTS / 2100 FT ABOV
- [SDR CA020117018](https://openairdocs.org/sdr/CA020117018), Dec 4, 2001: CONTROL VALVE. MALFUNCTIONED. (CAN) ON FERRY FLIGHT TSC 2257 FROM CUN-YMX , DURING TAKE OFF , SLAT SYSTEM LOCKED IN EXTEND POSITION , BUT FLAPS RAISED FULL UP. FLAP RED LIGHT WAS ILLUMINATED
- [SDR ARWA20011117](https://openairdocs.org/sdr/ARWA20011117), Nov 19, 2001: ENGINE. MAKING METAL. AT CRUISE 33,000; NR 3 ENGINE OIL PRESSURE DROPPED TO 30 PSI - MOVED THROTTLE TO IDLE, OIL PRESSURE REDUCED TO 20 PSI; COMPLETED ENGINE SHUTDOWN PROCEDURE AT 23
- [SDR CA020709002](https://openairdocs.org/sdr/CA020709002), Nov 18, 2001: ENGINE. VIBRATION. (CAN) VIBRATION INDICATION ON NR 1 ENGINE, 3.0 UNITS ON CHANNEL A AND B. THE ENGINE WAS SHUT DOWN IAW THE SOP. MAINTENANCE REMOVED THE LP FAN BLADES , CLEANED A
- [SDR ARWA20011103](https://openairdocs.org/sdr/ARWA20011103), Nov 13, 2001: ENGINE. VIBRATION. SHUTDOWN NR 2 ENGINE AFTER EXPERIENCING VIPS SPIKE 3.0 BOTH CHANNELS AT APPOX 2325Z.
- [SDR ARWA20020505](https://openairdocs.org/sdr/ARWA20020505), Nov 13, 2001: ENGINE. VIBRATION. (SUPPLEMENT TO: ARWA20011103) LOG PAGE # 22235. DISCREPANCY: SHUTDOWN NR # 2 ENGINE, AFTER EXPERIENCING VIPS SPIKE 3.0 BOTH CHANNELS AT APPOXIMATELY 2325 ZULU. 

All 102: https://openairdocs.org/engine/rolls-royce-rb211-524b402/reports.md

## STCs that may be installed (OpenAirDocs) (1)

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

## 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.

- [AAP-3502129-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID151538335920251125143637.0001): Bearing. Approved Air Parts, LLC · PMA PQ4173NE · Replaces Honeywell 3502129-1 · Nov 6, 2025
- [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
- [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
- [AAP-3502689-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID183644830020230331124834.0001): Bearing, Ball. Approved Air Parts Co Inc · PMA PQ4173NE · Replaces Honeywell P/N: 3502689-1 · Jun 2, 2021
- [AAP-3501171- 1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID106604782020230331124756.0001): Bearing, Ball. Approved Air Parts Co Inc · PMA PQ4173NE · Replaces Honeywell P/N: 3501171-1 · Jun 2, 2021
- [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
- [DEC92- 001-503](https://drs.faa.gov/browse/excelExternalWindow/5ECFAA2F69E7221586258629005AC7D3.0001): Plug, Machine. Turbine Kinetics Inc, A HEICO Aerospace Company · PMA PQ0816NE · Replaces 572-510-9004 A75M · 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
- [VL1370PE1-0860](https://drs.faa.gov/browse/excelExternalWindow/7335C9E5B3A94DE6862583D30067ED37.0001): Gasket, Seal. KAPCO · PMA PQ1383NM · Replaces 0860 and A0860 · Oct 9, 2018
- [VL1370PE1-0863](https://drs.faa.gov/browse/excelExternalWindow/0959035D5BC861DC862583D30067ED51.0001): Gasket, Seal. KAPCO · PMA PQ1383NM · Replaces 0863 and A0863 · Oct 9, 2018
- [VL1370PE1-0805](https://drs.faa.gov/browse/excelExternalWindow/0805EA6FC1442D33862583D30067ED15.0001): Gasket, Seal. KAPCO · PMA PQ1383NM · Replaces 0805 and A0805 · Oct 9, 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
- [3502689-1TA](https://drs.faa.gov/browse/excelExternalWindow/2A79CAB3069EF2E98625836A005030B7.0001): Bearing, Ball, Annular Supplement 129. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 3502689-1 · Sep 7, 2016
- [DEC92-001-503](https://drs.faa.gov/browse/excelExternalWindow/5A6D65283949B1EB86257F9A004D9918.0001): Plug, Machine. Turbine Kinetics Inc, A HEICO Aerospace Company · PMA PQ0816NE · Replaces 572-510-9004, A75M · Mar 29, 2016
- [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
- [GM6813](https://drs.faa.gov/browse/excelExternalWindow/D950D93C939D58E186257FAA0067F58D.0001): Transducer Fuel Flow. Kavlico Corporation · PMA PQ1186NM · Replaces ACS2280 · Jan 12, 2016
- [183824](https://drs.faa.gov/browse/excelExternalWindow/4FCB64D9D1B4EF9986257F16004F2E3B.0001): Nozzle Assy-Fuel Spray. Delavan Inc. · PMA PQ3405CE · Replaces 183824 · Dec 3, 2015

All of them: https://openairdocs.org/engine/rolls-royce-rb211-524b402/pma.md

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