# Rolls-Royce RB211-524D419

- Type: Engine model (FAA registry)
- Registry code: 54046
- Manufacturer (registry): ROLLS-ROYC
- Model: RB211-524D419
- Engine type: Turbo-fan
- Power: 51,980 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-rb211-524d419

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 2013-04-01](https://openairdocs.org/ad/2013-04-01): Thrust reverser units (TRUs) · Rolls-Royce RB211-524D4-19, RB211-524D4-39, RB211-524D4-B-19 and 11 more. Effective Mar 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 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 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 2000-18-03](https://openairdocs.org/ad/2000-18-03): Cold Stream Nozzle Assembly · Rolls-Royce RB211-524D4-19, RB211-524D4-B-19, RB211-524D4-B-39 and 2 more. Effective Sep 22, 2000
- [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 2011-13-01](https://openairdocs.org/ad/2011-13-01) (historical): Rivets · Rolls-Royce RB211-524D4-19, RB211-524D4-39, RB211-524D4-B-19 and 11 more. Effective Aug 12, 2011
- [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 (92, newest 50)

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

- [SDR 2020FA0000021](https://openairdocs.org/sdr/2020FA0000021), Oct 6, 2019: ACTUATOR. FAILED. WE EXPERIENCED A FAILURE OF THE RH BODY LANDING GEAR DOOR ACTUATOR IN FLIGHT WHICH CAUSED THE RELEASE OF NR 1 SYSTEM HYDRAULIC FLUID. THE ACTUATOR FAILED AT THE
- [SDR 0126200801](https://openairdocs.org/sdr/0126200801), Jan 26, 2008: ENGINE. MALFUNCTIONED. ON TAKEOFF ROLL, NR 3 ENGINE N2 WENT TO 114 PERCENT FOR LESS THAN 2 SECONDS, EPR WAS 1.4, ALL OTHER ENGINE GAGES NORMAL, AIRSPEED WAS 70 KTS. ABORTED TO, RETURN
- [SDR 0331200702](https://openairdocs.org/sdr/0331200702), Mar 31, 2007: ENGINE. BIRD INGESTION. AT ROTATION NR 2 ENG VIB ANNUNICATOR LIGHT & ENG VIB LIGHT FOR NR 2 ENG ILLUM, ACCOMPANIED BY VIB & ABNORMAL SOUND. NR 2 ENG SECURED IAW CHECKLIST, NO VIB NOTED
- [SDR 1023200603](https://openairdocs.org/sdr/1023200603), Oct 23, 2006: WARNING LIGHT. ILLUMINATED. ON DEPARTURE (GYD), JUST AFTER V1, NR 1 ENGINE VIBE LIGHT ILLUMINATED, VIBE METER NR 1 OFF SCALE HIGH, INCLUDING VIBRATION AS WELL. ENGINE SHUT DOWN, FUEL DUMP,
- [SDR 1017200602](https://openairdocs.org/sdr/1017200602), Oct 17, 2006: ENGINE. POWER LOSS. DURING CLIMB FROM (ELLX) AT AROUND FL 180 FT, NR 1 THROTTLE IS AT FORWARD STOP TO MAINTAIN CLIMB THRUST. IN CRUISE NR 1 THROTTLE IS AT 1.5 UNITS - (4) KNOBS AHE
- [SDR 0925200603](https://openairdocs.org/sdr/0925200603), Sep 20, 2006: COMPRESSOR. STALLED. DURING TO ROLL (SKBO), APPROX. 125 KTS., NR 4 ENGINE COMPRESSOR STALLED - ABORTED TO, RETURN TO GATE. FINDINGS - CORRECTIVE ACTIONS - TBD.
- [SDR 0808200601](https://openairdocs.org/sdr/0808200601), Aug 8, 2006: ENGINE. NONE. ON TAKEOFF AT SGES (AGT), NR 3 ENGINE BEGAN TO VIBRATE AND AMBER ENGINE VIB LIGHT CAME ON. ENGINE SHUTDOWN AND PROCEDURE TO COMPLETE THE HIGH ENGINE VIBRATION R
- [SDR AU510001639](https://openairdocs.org/sdr/AU510001639), Dec 12, 2005: FRAME. SCRATCHED. (AUS) FORWARD PRESSURE BULKHEAD AFT FACE OUTER CHORD SCRATCHED IN BEND RADIUS LOCATED AT LBL46/WL235 AND RBL24/WL268. SUSPECT A SHARP OBJECT WAS USED TO REMOVE 
- [SDR AU510002178](https://openairdocs.org/sdr/AU510002178), Dec 12, 2005: PANEL. MISSING. (AUS) NR 4 ENGINE VIGV ACCESS PANEL MISSING. INVESTIGATION ALSO FOUND THE LP COMPRESSOR ACOUSTIC LINING DAMAGED AT THE 6 O`CLOCK POSITION WITH A HOLE APPROXIMAT
- [SDR AUS20040443](https://openairdocs.org/sdr/AUS20040443), May 19, 2004: INDICATOR. FAULTY. (AUS) LT OB TRAILING EDGE FLAP INDICATOR FAILED.
- [SDR AUS20040390](https://openairdocs.org/sdr/AUS20040390), May 6, 2004: BOLT. INCORRECT. (AUS) LT WING LANDING GEAR TO LANDING GEAR DOOR TIE ROD BOLTS INCORRECTLY FITTED. BOLTS WERE FITTED UPSIDE DOWN. PERSONNEL/MAINTENANCE ERROR.
- [SDR AUS20040127](https://openairdocs.org/sdr/AUS20040127), Feb 24, 2004: BLANKET. DETERIORATED. (AUS) APU DUCT INSULATION BLANKET BURNED AND IN POOR CONDITION.
- [SDR AUS20031255](https://openairdocs.org/sdr/AUS20031255), Dec 1, 2003: BALLAST. FAILED. (AUS) LIGHTING BALLAST LOCATED AT SEAT 19JK FAILED.
- [SDR AUS20031205](https://openairdocs.org/sdr/AUS20031205), Nov 25, 2003: WIRE HARNESS. WORN. (AUS) WIRING LOOM LOCATED AT BS 1000 BEHIND OVERHEAD LOCKERS CHAFED THROUGH INSULATION BLANKET AND CONTACTED FUSELAGE FRAME CAUSING BURNING OF WIRES AND DAMAGE 
- [SDR AUS20030882](https://openairdocs.org/sdr/AUS20030882), Aug 31, 2003: TIRE. FAILED. (AUS) NR 5F TIRE TREAD SEPARATED FROM CASING. TIRE REMAINED INFLATED. NIL DAMAGE EVIDENT TO REST OF AIRCRAFT. SUSPECT CAUSED BY FAILURE OF TREAD TO BOND TO CASI
- [SDR AUS20030634](https://openairdocs.org/sdr/AUS20030634), Jun 19, 2003: SLIDE. FAILED. (AUS) DOOR NR 1 RT SLIDE RAFT FAILED.
- [SDR AUS20030518](https://openairdocs.org/sdr/AUS20030518), May 18, 2003: RADIO. FAILED. (AUS) DUAL HF SYSTEM FAILURE. ON ARRIVAL IT WAS REPORTED THAT NR 1 HF SYSTEM WANDERS OFF FREQUENCY AND BECOMES GARBLED. NR 2 HF WOULD NOT TUNE TO THE FREQUENCY 
- [SDR AUS20021287](https://openairdocs.org/sdr/AUS20021287), Nov 5, 2002: STATOR. DISINTEGRATED. (AUS) NR 4F BRAKE STATOR DISINTEGRATED CAUSING DAMAGE TO WHEEL.
- [SDR AUS20021270](https://openairdocs.org/sdr/AUS20021270), Nov 2, 2002: TIE ROD. BROKEN. (AUS) NR 3 ENGINE EXPERIENCED HIGH VIBRATION LEVELS. INSPECTION FOUND A NACELLE TIE ROD BROKEN AND FOULING ON A PIPE LOCATED ADJACENT TO THE AVM PICKUP. FAN BLA
- [SDR AUS20021244](https://openairdocs.org/sdr/AUS20021244), Oct 29, 2002: ENGINE. VIBRATES. (AUS) NR 4 ENGINE VIBRATION EXCESSIVE. ENGINE VIBRATION WAS ACCOMPANIEDBY A NOTICEABLE AIRFRAME VIBRATION.
- [SDR AUS20021149](https://openairdocs.org/sdr/AUS20021149), Oct 12, 2002: PUMP. FAILED. (AUS) NR 2 ENGINE DRIVEN FUEL PUMP FAILED.
- [SDR AUS20021065](https://openairdocs.org/sdr/AUS20021065), Sep 23, 2002: ENGINE. VIBRATES. (AUS) NR 4 ENGINE VIBRATION CAUSED INFLIGHT SHUTDOWN.
- [SDR AUS20021003](https://openairdocs.org/sdr/AUS20021003), Sep 7, 2002: PLATE. LEAKING. (AUS) NR 2 ENGINE HYDRAULIC PUMP BLANKING PLATE LEAKING ENGINE OIL. THE HYDRAULIC PUMP HAD BEEN REMOVED FROM THE ENGINE AND THE BLANKING PLATE FITTED.
- [SDR AUS20020994](https://openairdocs.org/sdr/AUS20020994), Sep 5, 2002: ENGINE. FAILED. (AUS) NR 1 ENGINE FAILED. EXCESSIVE VIBRATION INDICATIONS. INSPECTION FOUND METAL IN TAILPIPE.
- [SDR AUS20020743](https://openairdocs.org/sdr/AUS20020743), Jul 22, 2002: CONTROLLER. FAULTY. (AUS) NO1 ENGINE VIGV CONTROLLER FAULTY. CONTROLLER COULD NOT BE ADJUSTED TO BRING ENGINE PARAMETERS WITHIN LIMITS.
- [SDR AUS20020606](https://openairdocs.org/sdr/AUS20020606), Jun 18, 2002: PUSHROD. FAILED. (AUS) FORWARD CARGO DOOR FAILED TO OPEN. A LOUD NOISE WAS HEARD AND SEVERAL PUSHRODS HAD SHEARED.
- [SDR AUS20020406](https://openairdocs.org/sdr/AUS20020406), Apr 30, 2002: ENGINE. VIBRATES. (AUS) DURING CLIMB NR 4 ENGINE VIBRATION INDICATED 2.0. ON B' SELECTION THE INDICATION WENT OFF SCALE WITH AVM ALERT FLASHING. PRIOR TO SHUTDOWN A SLIGHT AIRFRA
- [SDR AUS20020380](https://openairdocs.org/sdr/AUS20020380), Apr 25, 2002: ENGINE. FAILED. (AUS) ON ROTATION A LOUD BANG WAS HEARD AND NR 4 EPR INDICATION DROPPED AND SPARKS WERE REPORTED FROM THE NR 4 ENGINE. THE ENGINE WAS SHUT DOWN.
- [SDR AUS20020305](https://openairdocs.org/sdr/AUS20020305), Apr 3, 2002: HANDLE. OUT OF ADJUST. (AUS) L5 DOOR HANDLE RIGGING OUT OF ADJUSTMENT.
- [SDR AUS20020281](https://openairdocs.org/sdr/AUS20020281), Mar 23, 2002: HOSE. RUPTURED. (AUS) NR 1 ADP PRESSURE HOSE LOCATED BETWEEN THE PUMP AND THE PRESSURE MODULE RUPTURED. LOSS OF HYDRAULIC FLUID.
- [SDR AUS20020153](https://openairdocs.org/sdr/AUS20020153), Mar 1, 2002: CONNECTOR. LOOSE. (AUS) CAPTAINS NR 1 WINDOW HEAT CONNECTION LOCATED IN THE LOWER LT CORNER LOOSE AND ARCING.
- [SDR AUS20020118](https://openairdocs.org/sdr/AUS20020118), Feb 17, 2002: ENGINE. STALLED. (AUS) NR 1 ENGINE STALLED. VIBRATION FELT AND ENGINE PARAMETERS DIFFERENT FROM OTHER ENGINES.
- [SDR AUS20020094](https://openairdocs.org/sdr/AUS20020094), Feb 10, 2002: COUPLING. SEPARATED. (AUS) NR 6 AND NR 7 LEADING EDGE FLAPS DISCONNECTED DUE TO THE OUTBOARD SPLINE COUPLING COMING ADRIFT. THERE WAS NO SIGN OF THE LOCKWIREOR ATTACHMENT SCREWS.
- [SDR AUS20020089](https://openairdocs.org/sdr/AUS20020089), Feb 8, 2002: ACTUATOR. FAULTY. (AUS) RUDDER RATIO ACTUATOR FAULTY.
- [SDR AUS20020067](https://openairdocs.org/sdr/AUS20020067), Jan 26, 2002: COUPLING. MISRIGGED. (AUS) FUEL TRANSFER SYSTEM COUPLING INCORRECTLY ASSEMBLED.
- [SDR AUS20020032](https://openairdocs.org/sdr/AUS20020032), Jan 17, 2002: CONTROL UNIT. FAULTY. (AUS) NR 2 ENGINE VIBRATION SIGNAL CONTROL UNIT SUSPECT FAULTY.
- [SDR AUS20011437](https://openairdocs.org/sdr/AUS20011437), Dec 30, 2001: BOLT. SHEARED. (AUS) H11 BOLT LOCATED AT STN 1241/LBBL 127/WL 163 SHEARED. FOLLOWING REMOVAL OF THE BOLT CORROSION WAS FOUND IN THE BULKHEAD FITTING BORE. FOUND DURING ULTRASO
- [SDR AUS20011381](https://openairdocs.org/sdr/AUS20011381), Dec 22, 2001: BOLT. LOOSE. (AUS) NR 1 ENGINE FUEL FLOW REGULATOR (FFR) TO FUEL PUMP PIPE LEAKING. INVESTIGATION FOUND A LOOSE PIPE RETAINING BOLT ON THE FFR.
- [SDR AUS20011217](https://openairdocs.org/sdr/AUS20011217), Nov 13, 2001: COMPUTER. FAILED. (AUS) UPPER YAW DAMPER COMPUTER FAULTY.
- [SDR AUS20011178](https://openairdocs.org/sdr/AUS20011178), Nov 6, 2001: LINE. DAMAGED. (AUS) HYDRAULIC LINE DAMAGED BY CONTACT FROM THE RT WING LANDING GEAR RETRACTION ACTUATOR. LOSS OF NR 4 HYDRAULIC SYSTEM FLUID.
- [SDR AUS20011132](https://openairdocs.org/sdr/AUS20011132), Oct 25, 2001: CONTROL CABLE. SEIZED. (AUS) NR 1 ENGINE THRUST LEVER PUSH/PULL CABLE SEIZED.
- [SDR AUS20010980](https://openairdocs.org/sdr/AUS20010980), Sep 8, 2001: ENGINE. VIBRATES. (AUS) NR 1 ENGINE VIBRATION. OIL QUANTITY SLOWLY DROPPED. METAL CONTAMINATION OF ENGINE OIL SYSTEM.
- [SDR AUS20010949](https://openairdocs.org/sdr/AUS20010949), Sep 1, 2001: CONNECTOR. BURNED. (AUS) SEAT 43AB VIDEO CONNECTOR PINS BURNT AND WIRING CHAFED.
- [SDR AUS20010928](https://openairdocs.org/sdr/AUS20010928), Aug 23, 2001: COVER. CRACKED. (AUS) LT AND RT ENGINE THRUST CABLE GUARD COVERS LOCATED IN AREABETWEEN BS960 TO BS1000 DETERIORATED AND CRACKED. FOUND DURING INSPECTION IAW EI 743-076-0002R02
- [SDR AUS20010910](https://openairdocs.org/sdr/AUS20010910), Aug 21, 2001: ACTUATOR. SHEARED. (AUS) NOSE LANDING GEAR DOOR ACTUATOR SHEARED. LOSS OF HYDRAULIC FLUID.
- [SDR AUS20010911](https://openairdocs.org/sdr/AUS20010911), Aug 19, 2001: PDU. FAULTY. (AUS) NR 3 LT LEADING EDGE FLAP PNEUMATIC DRIVE UNIT FAULTY.
- [SDR AUS20010883](https://openairdocs.org/sdr/AUS20010883), Aug 14, 2001: ENGINE. VIBRATES. (AUS) NR 2 ENGINE VIBRATION EXCESSIVE.
- [SDR AUS20010905](https://openairdocs.org/sdr/AUS20010905), Aug 13, 2001: ANTENNA. FAULTY. (AUS) WEATHER RADAR ANTENNA FAULTY.
- [SDR AUS20010839](https://openairdocs.org/sdr/AUS20010839), Jul 31, 2001: FUEL CONTROL. FAULTY. (AUS) NR 4 ENGINE FUEL FLOW REGULATOR FAULTY. AIRCRAFT IS FOREIGN REGISTRATION DQ-FJE.
- [SDR AUS20010801](https://openairdocs.org/sdr/AUS20010801), Jul 29, 2001: ROTOR. FAILED. (AUS) NR 7 MAIN BODY WHEEL BRAKE ROTOR SEGMENT FAILED.

All 92: https://openairdocs.org/engine/rolls-royce-rb211-524d419/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
- [3272542-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID199868990720230914183318.0001): Gearbox Ballscrew. Honeywell International Inc. · PMA PQ1222NM · Replaces 3272542-4 · Mar 23, 2023
- [3275514-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID199417040720230914183302.0001): Ballscrew. Honeywell International Inc. · PMA PQ1222NM · Replaces L922569 · Mar 23, 2023
- [3272626-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID199002416820230914183322.0001): Gearbox Pneumatic Interlock. Honeywell International Inc. · PMA PQ1222NM · Replaces 3272626-3 · Mar 23, 2023
- [3275514-6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID197842150320230914183254.0001): Screw Jack. Honeywell International Inc. · PMA PQ1222NM · Replaces 3275514-6 · Mar 23, 2023
- [3272546-9](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID196002878520230914183323.0001): Gearbox Lock. Honeywell International Inc. · PMA PQ1222NM · Replaces 3272546-9 · Mar 23, 2023
- [3272544-6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID190574240920230914183319.0001): Gearbox Ballscrew & Interlock. Honeywell International Inc. · PMA PQ1222NM · Replaces 3272544-6 · Mar 23, 2023
- [3500927-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID186632525220230914183317.0001): Flange Kit. Honeywell International Inc. · PMA PQ1222NM · Replaces 3500927-2 · Mar 23, 2023
- [979182-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID185788866820230914183318.0001): Shutoff Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces L901675 · Mar 23, 2023
- [3505010-11](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID181680563220230914183315.0001): Starter. Honeywell International Inc. · PMA PQ1222NM · Replaces 3505010-11 · Mar 23, 2023
- [3268844-9](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180064669820230914183307.0001): Air Motor. Honeywell International Inc. · PMA PQ1222NM · Replaces 3268844-9 · Mar 23, 2023
- [3272546-5](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID174785429020230914183310.0001): Gearbox. Honeywell International Inc. · PMA PQ1222NM · Replaces 3272546-5 · Mar 23, 2023
- [3272546-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID173993444620230914183309.0001): Gearbox. Honeywell International Inc. · PMA PQ1222NM · Replaces 3272546-3 · Mar 23, 2023
- [126704-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168778674520230914183331.0001): Air Motor. Honeywell International Inc. · PMA PQ1222NM · Replaces 126704-4 · Mar 23, 2023
- [3272626-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID167735334120230914183324.0001): Gearbox and Solenoid Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 3272626-2 · Mar 23, 2023
- [3272544-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165728732120230914183300.0001): Gearbox. Honeywell International Inc. · PMA PQ1222NM · Replaces 3272544-4 · Mar 23, 2023
- [126704-9](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID163461866120230914183322.0001): Motor, Air. Honeywell International Inc. · PMA PQ1222NM · Replaces 126704-9 · Mar 23, 2023
- [3505010-5](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID162409143320230914183313.0001): Starter. Honeywell International Inc. · PMA PQ1222NM · Replaces 3505010-5 · Mar 23, 2023
- [126704-10](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID159682858520230914183333.0001): Motor, Air. Honeywell International Inc. · PMA PQ1222NM · Replaces 126704-10 · Mar 23, 2023
- [3272546-7](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID158442911820230914183311.0001): Gearbox. Honeywell International Inc. · PMA PQ1222NM · Replaces 3272546-7 · Mar 23, 2023
- [3289520-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID158375557520230914183304.0001): Seq Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 3289520-3 · Mar 23, 2023
- [126704-6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID157251352420230914183328.0001): Air Motor. Honeywell International Inc. · PMA PQ1222NM · Replaces 126704-6 · Mar 23, 2023
- [121734-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149323116120230914183255.0001): Flex Drive. Honeywell International Inc. · PMA PQ1222NM · Replaces L922535 · Mar 23, 2023
- [126704-5](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID146846182620230914183332.0001): Air Motor. Honeywell International Inc. · PMA PQ1222NM · Replaces 126704-5 · Mar 23, 2023
- [126704-8](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145493761120230914183330.0001): Air Motor. Honeywell International Inc. · PMA PQ1222NM · Replaces 126704-8 · Mar 23, 2023
- [3272546-10](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID140263866820230914183321.0001): Gearbox Pneumatic Interlock. Honeywell International Inc. · PMA PQ1222NM · Replaces 3272546-10 · Mar 23, 2023
- [3505010-12](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139431046520230914183316.0001): Starter. Honeywell International Inc. · PMA PQ1222NM · Replaces 3505010-12 · Mar 23, 2023
- [3272554-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID135977668220230914183301.0001): Gearbox. Honeywell International Inc. · PMA PQ1222NM · Replaces 33272554-2 · Mar 23, 2023
- [3272542-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID135239425020230914183259.0001): Gearbox. Honeywell International Inc. · PMA PQ1222NM · Replaces L922533 · Mar 23, 2023
- [126704-11](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID134860136520230914183327.0001): Motor, Air. Honeywell International Inc. · PMA PQ1222NM · Replaces 126704-11 · Mar 23, 2023
- [3289520-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID128876189820230914183303.0001): Seq Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 3289520-2 · Mar 23, 2023
- [3268844-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID125091051920230914183306.0001): Air Motor. Honeywell International Inc. · PMA PQ1222NM · Replaces 3268844-4 · Mar 23, 2023
- [3289520-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID123439346320230914183308.0001): Seq Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 3289520-1 · Mar 23, 2023
- [3505010-9](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID122842235420230914183314.0001): Starter. Honeywell International Inc. · PMA PQ1222NM · Replaces 3505010-9 · Mar 23, 2023
- [126704-7](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID121500678720230914183329.0001): Air Motor. Honeywell International Inc. · PMA PQ1222NM · Replaces 126704-7 · Mar 23, 2023
- [121734-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID119019771420230914183258.0001): Flex Drive. Honeywell International Inc. · PMA PQ1222NM · Replaces L922546 · Mar 23, 2023
- [3272546-6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID117650587120230914183305.0001): Gearbox. Honeywell International Inc. · PMA PQ1222NM · Replaces 3272546-6 · Mar 23, 2023
- [3268844-10](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID114965935820230914183326.0001): Motor, Air & Valve Assy.. Honeywell International Inc. · PMA PQ1222NM · Replaces 3268844-10 · Mar 23, 2023
- [3272546-8](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID110977184520230914183301.0001): Gearbox. Honeywell International Inc. · PMA PQ1222NM · Replaces L922548 · Mar 23, 2023
- [121734-5](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID110187368520230914183325.0001): Shaft, Drive Flexible. Honeywell International Inc. · PMA PQ1222NM · Replaces 121734-5 · Mar 23, 2023
- [3275514-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID105187096920230914183312.0001): Screw & Nut Jack. Honeywell International Inc. · PMA PQ1222NM · Replaces 3275514-3 · Mar 23, 2023
- [121734-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID100424507620230914183256.0001): Flex Drive. Honeywell International Inc. · PMA PQ1222NM · Replaces L922536 · Mar 23, 2023
- [UL38922ACI](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168843985320260805175346.0001): Stop, Rear,FingerBracket. Wencor LLC (formerly Dixie Aerospace LLC) · PMA PQ1630CE · Replaces UL38922 · Jul 21, 2022
- [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

All of them: https://openairdocs.org/engine/rolls-royce-rb211-524d419/pma.md

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