# Service difficulty reports: Rolls-Royce RB211-524D419

A list on [Rolls-Royce RB211-524D419](https://openairdocs.org/engine/rolls-royce-rb211-524d419.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 92 reports

- [SDR 2020FA0000021](https://openairdocs.org/sdr/2020FA0000021.md): Actuator · failed · Oct 6, 2019 · N787RR · Boeing 747267B · Landing Gear Door Actuator
  > 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 END CAP/GLAND NUT THAT HOUSES THE SEAL FOR THE RAM. THE BREAK OF THE END CAP IS FROM SAFETY WIRE
- [SDR 0126200801](https://openairdocs.org/sdr/0126200801.md): Engine · malfunctioned · Jan 26, 2008 · N362FC · Boeing 747236B · Engine (Turbine/Turboprop)
  > 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, RETURNED TO RAMP.
- [SDR 0331200702](https://openairdocs.org/sdr/0331200702.md): Engine · bird ingestion · Mar 31, 2007 · N361FC · Boeing 747200B · Engine (Turbine/Turboprop)
  > 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 AFTER SHUTDOWN. FUEL JETTISON, ACFT RETURNED WITHOUT FURTHER INCIDENTS. ON POSTFLIGHT INSPECTIO
- [SDR 1023200603](https://openairdocs.org/sdr/1023200603.md): Warning Light · illuminated · Oct 23, 2006 · N361FC · Boeing 747200B · Engine (Turbine/Turboprop)
  > 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, AND RETURNED TO (GYD).CORRECTIVE ACTIONS, PENDING.
- [SDR 1017200602](https://openairdocs.org/sdr/1017200602.md): Engine · power loss · Oct 17, 2006 · N362FC · Boeing 747200B · Engine (Turbine/Turboprop)
  > 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 AHEAD OF ENGINES 2, 3, 4. NOTE ALL ENGINE PARAMETERS NORMAL AT LOW ALT, BELOW 189 THROTTLE POSITIONS
- [SDR 0925200603](https://openairdocs.org/sdr/0925200603.md): Compressor · stalled · Sep 20, 2006 · N362FC · Boeing 747200B · Engine (Turbine/Turboprop)
  > 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.md): Engine · none · Aug 8, 2006 · N362FC · Boeing 747200B · Engine (Turbine/Turboprop)
  > 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 RB211 CHECKLIST. DISCREPANCY DUE TO BIRDSTRIKE/INJESTION. PERFORMED CONDITIONAL ENGINE BIRDSTRIKE
- [SDR AU510001639](https://openairdocs.org/sdr/AU510001639.md): Frame · scratched · Dec 12, 2005 · Boeing 747338 · Fuselage Main, Frame
  > (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 SEALANT. FOUND DURING INSPECTION IAW AD/B747/159. SEE ATTACHMENT FOR INVESTIGATION DETAILS. (CASA N
- [SDR AU510002178](https://openairdocs.org/sdr/AU510002178.md): Panel · missing · Dec 12, 2005 · Boeing 747338 · Nacelle/Pylon, Plate/Skin
  > (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 APPROXIMATELY 150MM BY 100MM (6IN BY 4IN) IN THE SKIN. VIGV CONTROLLER PANEL SUPPORT STRUCTURE ALSO DAMAGED. (
- [SDR AUS20040443](https://openairdocs.org/sdr/AUS20040443.md): Indicator · faulty · May 19, 2004 · Boeing 747338 · Trailing Flap Position Indicating System
  > (AUS) LT OB TRAILING EDGE FLAP INDICATOR FAILED.
- [SDR AUS20040390](https://openairdocs.org/sdr/AUS20040390.md): Bolt · incorrect · May 6, 2004 · Boeing 747338 · Fasteners
  > (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.md): Blanket · deteriorated · Feb 24, 2004 · Boeing 747338 · Air Distribution System
  > (AUS) APU DUCT INSULATION BLANKET BURNED AND IN POOR CONDITION.
- [SDR AUS20031255](https://openairdocs.org/sdr/AUS20031255.md): Ballast · failed · Dec 1, 2003 · Boeing 747338 · Passenger Compartment Lighting
  > (AUS) LIGHTING BALLAST LOCATED AT SEAT 19JK FAILED.
- [SDR AUS20031205](https://openairdocs.org/sdr/AUS20031205.md): Wire Harness · worn · Nov 25, 2003 · Boeing 747338 · Fuselage Main, Bulkhead Fuselage wiring
  > (AUS) WIRING LOOM LOCATED AT BS 1000 BEHIND OVERHEAD LOCKERS CHAFED THROUGH INSULATION BLANKET AND CONTACTED FUSELAGE FRAME CAUSING BURNING OF WIRES AND DAMAGE TO THE INSULATION BLANKET AND FRAME. AREA OF DAMAGE TO FRAME WAS APPROXIMATELY 4.762MM BY 2.381MM(0.
- [SDR AUS20030882](https://openairdocs.org/sdr/AUS20030882.md): Tire · failed · Aug 31, 2003 · Boeing 747338 · Tire
  > (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 CASING DURING RETREAD.
- [SDR AUS20030634](https://openairdocs.org/sdr/AUS20030634.md): Slide · failed · Jun 19, 2003 · Boeing 747338 · Escape Slide
  > (AUS) DOOR NR 1 RT SLIDE RAFT FAILED.
- [SDR AUS20030518](https://openairdocs.org/sdr/AUS20030518.md): Radio · failed · May 18, 2003 · Boeing 747338 · HF Communications System
  > (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 SELECTED. THE NR 1 SYSTEM WAS RE-RACKED AND OPERATED NORMALLY. THE NR 2 SYSTEM TRANSCEIVER AND COUP
- [SDR AUS20021287](https://openairdocs.org/sdr/AUS20021287.md): Stator · disintegrated · Nov 5, 2002 · Boeing 747238B · Brake
  > (AUS) NR 4F BRAKE STATOR DISINTEGRATED CAUSING DAMAGE TO WHEEL.
- [SDR AUS20021270](https://openairdocs.org/sdr/AUS20021270.md): Tie Rod · broken · Nov 2, 2002 · Boeing 747238B · Nacelle/Pylon, Main Frame
  > (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 BLADES CLEANED AND LUBRICATED AND AN ENGINE RUN CARRIED OUT.
- [SDR AUS20021244](https://openairdocs.org/sdr/AUS20021244.md): Engine · vibrates · Oct 29, 2002 · Boeing 747238B · Engine (Turbine/Turboprop)
  > (AUS) NR 4 ENGINE VIBRATION EXCESSIVE. ENGINE VIBRATION WAS ACCOMPANIEDBY A NOTICEABLE AIRFRAME VIBRATION.
- [SDR AUS20021149](https://openairdocs.org/sdr/AUS20021149.md): Pump · failed · Oct 12, 2002 · Boeing 747338 · Engine Fuel Pump
  > (AUS) NR 2 ENGINE DRIVEN FUEL PUMP FAILED.
- [SDR AUS20021065](https://openairdocs.org/sdr/AUS20021065.md): Engine · vibrates · Sep 23, 2002 · Boeing 747238B · Engine (Turbine/Turboprop)
  > (AUS) NR 4 ENGINE VIBRATION CAUSED INFLIGHT SHUTDOWN.
- [SDR AUS20021003](https://openairdocs.org/sdr/AUS20021003.md): Plate · leaking · Sep 7, 2002 · Boeing 747238B · Turbine Engine Oil System
  > (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.md): Engine · failed · Sep 5, 2002 · Boeing 747338 · Engine (Turbine/Turboprop)
  > (AUS) NR 1 ENGINE FAILED. EXCESSIVE VIBRATION INDICATIONS. INSPECTION FOUND METAL IN TAILPIPE.
- [SDR AUS20020743](https://openairdocs.org/sdr/AUS20020743.md): Controller · faulty · Jul 22, 2002 · Boeing 747238B · Turbine Engine Air Inlet Section
  > (AUS) NO1 ENGINE VIGV CONTROLLER FAULTY. CONTROLLER COULD NOT BE ADJUSTED TO BRING ENGINE PARAMETERS WITHIN LIMITS.
- [SDR AUS20020606](https://openairdocs.org/sdr/AUS20020606.md): Pushrod · failed · Jun 18, 2002 · Boeing 747238B · Cargo/Baggage Doors
  > (AUS) FORWARD CARGO DOOR FAILED TO OPEN. A LOUD NOISE WAS HEARD AND SEVERAL PUSHRODS HAD SHEARED.
- [SDR AUS20020406](https://openairdocs.org/sdr/AUS20020406.md): Engine · vibrates · Apr 30, 2002 · Boeing 747238B · Engine (Turbine/Turboprop)
  > (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 AIRFRAME VIBRATION WAS FELT THROUGH THE AIRCRAFT.
- [SDR AUS20020380](https://openairdocs.org/sdr/AUS20020380.md): Engine · failed · Apr 25, 2002 · Boeing 747338 · Engine (Turbine/Turboprop)
  > (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.md): Handle · out of adjust · Apr 3, 2002 · Boeing 747338 · Passenger/Crew Doors
  > (AUS) L5 DOOR HANDLE RIGGING OUT OF ADJUSTMENT.
- [SDR AUS20020281](https://openairdocs.org/sdr/AUS20020281.md): Hose · ruptured · Mar 23, 2002 · Boeing 747238B · Hydraulic System, Main
  > (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.md): Connector · loose · Mar 1, 2002 · Boeing 747238B · Windshield/Door Rain/Ice Removal
  > (AUS) CAPTAINS NR 1 WINDOW HEAT CONNECTION LOCATED IN THE LOWER LT CORNER LOOSE AND ARCING.
- [SDR AUS20020118](https://openairdocs.org/sdr/AUS20020118.md): Engine · stalled · Feb 17, 2002 · Boeing 747338 · Engine (Turbine/Turboprop)
  > (AUS) NR 1 ENGINE STALLED. VIBRATION FELT AND ENGINE PARAMETERS DIFFERENT FROM OTHER ENGINES.
- [SDR AUS20020094](https://openairdocs.org/sdr/AUS20020094.md): Coupling · separated · Feb 10, 2002 · Boeing 747238B · Leading Edge Slat Control System
  > (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.md): Actuator · faulty · Feb 8, 2002 · Boeing 747338 · Rudder Actuator
  > (AUS) RUDDER RATIO ACTUATOR FAULTY.
- [SDR AUS20020067](https://openairdocs.org/sdr/AUS20020067.md): Coupling · misrigged · Jan 26, 2002 · Boeing 747338 · Aircraft Fuel Distribution System
  > (AUS) FUEL TRANSFER SYSTEM COUPLING INCORRECTLY ASSEMBLED.
- [SDR AUS20020032](https://openairdocs.org/sdr/AUS20020032.md): Control Unit · faulty · Jan 17, 2002 · Boeing 747338 · Engine Vibration Analyzer
  > (AUS) NR 2 ENGINE VIBRATION SIGNAL CONTROL UNIT SUSPECT FAULTY.
- [SDR AUS20011437](https://openairdocs.org/sdr/AUS20011437.md): Bolt · sheared · Dec 30, 2001 · Boeing 747338 · Wing Main, Frame Structure
  > (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 ULTRASONIC INSPECTION.
- [SDR AUS20011381](https://openairdocs.org/sdr/AUS20011381.md): Bolt · loose · Dec 22, 2001 · Boeing 747338 · Fuel Control/Turbine Engines
  > (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.md): Computer · failed · Nov 13, 2001 · Boeing 747SP38 · Autopilot Computer
  > (AUS) UPPER YAW DAMPER COMPUTER FAULTY.
- [SDR AUS20011178](https://openairdocs.org/sdr/AUS20011178.md): Line · damaged · Nov 6, 2001 · Boeing 747338 · Hydraulic System, Main
  > (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.md): Control Cable · seized · Oct 25, 2001 · Boeing 747338 · Power Lever
  > (AUS) NR 1 ENGINE THRUST LEVER PUSH/PULL CABLE SEIZED.
- [SDR AUS20010980](https://openairdocs.org/sdr/AUS20010980.md): Engine · vibrates · Sep 8, 2001 · Boeing 747238B · Engine (Turbine/Turboprop)
  > (AUS) NR 1 ENGINE VIBRATION. OIL QUANTITY SLOWLY DROPPED. METAL CONTAMINATION OF ENGINE OIL SYSTEM.
- [SDR AUS20010949](https://openairdocs.org/sdr/AUS20010949.md): Connector · burned · Sep 1, 2001 · Boeing 747238B · Passenger Compartment Equipment
  > (AUS) SEAT 43AB VIDEO CONNECTOR PINS BURNT AND WIRING CHAFED.
- [SDR AUS20010928](https://openairdocs.org/sdr/AUS20010928.md): Cover · cracked · Aug 23, 2001 · Boeing 747338 · Power Lever
  > (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.md): Actuator · sheared · Aug 21, 2001 · Boeing 747238B · Landing Gear Door Actuator
  > (AUS) NOSE LANDING GEAR DOOR ACTUATOR SHEARED. LOSS OF HYDRAULIC FLUID.
- [SDR AUS20010911](https://openairdocs.org/sdr/AUS20010911.md): Pdu · faulty · Aug 19, 2001 · Boeing 747SP38 · Leading Edge Slat Actuator
  > (AUS) NR 3 LT LEADING EDGE FLAP PNEUMATIC DRIVE UNIT FAULTY.
- [SDR AUS20010883](https://openairdocs.org/sdr/AUS20010883.md): Engine · vibrates · Aug 14, 2001 · Boeing 747338 · Turbine Engine Compressor Section
  > (AUS) NR 2 ENGINE VIBRATION EXCESSIVE.
- [SDR AUS20010905](https://openairdocs.org/sdr/AUS20010905.md): Antenna · faulty · Aug 13, 2001 · Boeing 747238B · Weather Radar System
  > (AUS) WEATHER RADAR ANTENNA FAULTY.
- [SDR AUS20010839](https://openairdocs.org/sdr/AUS20010839.md): Fuel Control · faulty · Jul 31, 2001 · Boeing 747238B · Fuel Control/Turbine Engines
  > (AUS) NR 4 ENGINE FUEL FLOW REGULATOR FAULTY. AIRCRAFT IS FOREIGN REGISTRATION DQ-FJE.
- [SDR AUS20010801](https://openairdocs.org/sdr/AUS20010801.md): Rotor · failed · Jul 29, 2001 · Boeing 747338 · Brake
  > (AUS) NR 7 MAIN BODY WHEEL BRAKE ROTOR SEGMENT FAILED.

Next page: https://openairdocs.org/engine/rolls-royce-rb211-524d419/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE engine_model_key = 'RB211524D419'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/rolls-royce-rb211-524d419/reports

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