# Service difficulty reports: Rolls-Royce RB211-524B-02 A list on [Rolls-Royce RB211-524B-02](https://openairdocs.org/engine/rolls-royce-rb211-524b-02.md). Newest first. General aviation reporting is voluntary. - [SDR ARWA0010715](https://openairdocs.org/sdr/ARWA0010715.md): Engine · vibration · Jul 3, 2001 · N308GB · Lkheed 1011385115 · Engine (Turbine/Turboprop) > AT TOP OF CLIMB NR 1 ENGINE VIBRATION SPIKED AT 3.0 BOTH CHANNELS IN-FLIGHT SHUT DOWN AND RETURN TO KMIA. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 ENGINE - PER MM L1011 FORM 7104A, OPS CHECK OK IAW MM L1011 - 7102B; RUN UP IAW MM 71-00-00. - [SDR ARWA0010404](https://openairdocs.org/sdr/ARWA0010404.md): Engine · vibration · Apr 17, 2001 · N308GB · Lkheed 1011385115 · Turbine Engine Compressor Section > NR3 ENGINE VIBRATION UNITS WENT ABOVE 2.5 SHORTLY AFTER LEVEL OFF IN CRUISE. 04:50Z SHUTDOWN ENGINE IN ACCORDANCE WITH ABNORMAL VIBRATION CHECKLIST. HIGH VIBRATION READING WAS ONLY IN THE LOW SELECTION ALL OTHER READINGS WERE NORMAL.CORRECTIVE ACTION: PERFORME - [SDR ARWA0010401](https://openairdocs.org/sdr/ARWA0010401.md): Engine · vibration · Apr 1, 2001 · N260FA · Lkheed 1011385114 · Engine (Turbine/Turboprop) > NR 2 ENGINE VIBRATION EXCEEDED 2.5 UNITS IN BOTH A & B VIBRATION SELECTIONS. ENGINE SHUT DOWN PLUS RETURNED TO MIA TIME 00:35Z. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED CHIP DETECTORS, EXHAUST COLLECTOR NO DEFECT NOTED. LUBED CLAPPERS. PERFORMED BOROSCO - [SDR ARWA0010301](https://openairdocs.org/sdr/ARWA0010301.md): Engine · vibration · Mar 3, 2001 · N308GB · Lkheed 1011385115 · Engine (Turbine/Turboprop) > NR 1 ENGINE SHUTDOWN IN FLIGHT AND RETURNED TO MIAMI DUE TO 2.5 SPIKE ON VIBRATION, BOTH CHANNELS IN THE LOW RANGE. REMOVED AND INSPECTED MASTER INTERNAL GEARBOX CHIP DETECTORS IAW 72-01-00, NO EVIDENCE OF INTERNAL FAILURE FOUND. VISUALLY INSPECTED AIR INLET - [SDR ARWA981213](https://openairdocs.org/sdr/ARWA981213.md): Fuel Control · out of adjust · Dec 21, 1998 · N306GB · Lkheed 10113851 · Fuel Controlling System > NR 3 ENGINE SLOW TO SPOOL, ABOVE 1.3 EPR. DURING TAKEOFF ROLL IN DTW ABORTED TAKEOFF. AFTER FURTHER RUN-UP ON THE TAXI WAY, ENGINE OPERATED NORMALLY. ADJUSTED FUEL CONTROL IAW M/M 73-21-00. - [SDR CKSA98353](https://openairdocs.org/sdr/CKSA98353.md): Clamp · loose · Jun 27, 1998 · N102CK · Lkheed 1011385115 · Pneumatic Distribution System > AFTER TAKEOFF, NR 3 ENGINE FIRE DET LOOP B ILLUMINATED, SWITCHED TO A LOOP AND FULL FIRE WARNING EXPERIENCED. WHEN PULLING THROTTLE BACK ALL INDICATIONS EXTINGUISHED. FHB EMERGENCY PROCEDURES C/W, ENGINE SHUTDOWN. FOUND NR 3 ENGINE HIGH PRESSURE VALVE CLAMP - [SDR CKSA98500](https://openairdocs.org/sdr/CKSA98500.md): Fire Loop · out of adjust · Jun 21, 1998 · N104CK · Lkheed 1011385115 · Fire Detection > DURING CLIMB, B FIRE LOOP LIGHT NR 2 ENGINE CAME ON STEADY. TEST SHOWED A LOOP OK. A FIRE LOOP SELECTED. AFTER ABOUT 2 MIN, A FIRE LOOP CAME ON. SELECTED BOTH, AND A AND B, LOOP LIGHT BOTH CAME ON. FOUND A AND B SENSOR TOUCHING ENGINE CASE AT 6:00 POS. R - [SDR CKSA98091](https://openairdocs.org/sdr/CKSA98091.md): Blade · damaged · Feb 12, 1998 · N103CK · Lkheed 1011385115 · Turbine Engine Compressor Section > AFTER TAKEOFF, NR 2 ENG HAD A LARGE COMPRESSOR STALL WITH A 40 FT TO 50 FT. REPORTED FLAME OUT THE TAIL, OBSERVED BY TOWER, OTHER ACFT AND GROUND PERSONNEL. TGT = 860, ALL OTHER PARAMETERS WITHIN LIMITS. FIRM 71-23-17-02. PERFORMED BORESCOPE INSPECTION ON - [SDR CKSA98011](https://openairdocs.org/sdr/CKSA98011.md): Engine · flamed out · Feb 4, 1998 · N103CK · Lkheed 1011385115 · Engine (Turbine/Turboprop) > PER CREW REPORT, NR 3 ENGINE FLAMED OUT DURING FLIGHT THRU HAIL STORM. ALL MCD INSPECTION, INLET AND EXHAUST AREAS CHECKED FOR DAMAGE. NO DAMAGE NOTED, ENGINE GROUND RUN PERFORMED, ALL PARAMETERS NORMAL IAW 71-00-00. - [SDR CKSA97571](https://openairdocs.org/sdr/CKSA97571.md): Plug · missing · Nov 14, 1997 · N103CK · Lkheed 1011385115 · Engine (Turbine/Turboprop) > THE A AND B FIRE DETECTION LOOP LIGHTS NR 2 ENGINE ON INTERMITTENTLY WITH POWER REDUCED ON FINAL RECEIVED FULL FIRE INDICATION AND ACCOMPLISHED FIRE SHUTDOWN PROCEDURES. FOUND BLEED AIR LEAK. INSTALLED BORESCOPE PLUG, CLEANED A AND B FIRE DETECTOR CONTROLLER - [SDR CKSA97560](https://openairdocs.org/sdr/CKSA97560.md): Module Gearbox · sheared · Oct 25, 1997 · N106CK · Lkheed 1011385115 · Turbine Engine Accessory Drive > NR 3 ENGINE FLAME-OUT LEVEL FLT FL350, NO APPARENT REASON ALL PARAMETERS NORMAL. AIRSTART UNSUCCESSFUL. FUEL PUMP GEAR FOUND INOP. REMOVED AND REPLACED 06 MODULE GEARBOX. LEAK AND OPS CHECK OK IAW RB211 EM 72-00-06. - [SDR ARWA970903](https://openairdocs.org/sdr/ARWA970903.md): Gearbox · failed · Sep 10, 1997 · N306GB · Lkheed 1011385115 · Turbine Engine Reduction Gear > NR 1 ENG SHUT DOWN (ON IT'S OWN) AT 4,000 AS 210KTS 15 MI FROM AIRPORT. UNABLE TO MOTOR ENGINE DUE TO SHARED SHAFT IN GEAR BOX, DISCOVERED CHIPS ON ACC GEARBOX PLUG. REMOVED AND REPLACED ENG DRIVEN GEARBOX. REMOVED AND REPLACED SCAVENGE OIL FILTER, OPS CHEC - [SDR CKSA97316](https://openairdocs.org/sdr/CKSA97316.md): Fire Light · illuminated · Jul 5, 1997 · N102CK · Lkheed 1011385115 · Fire Detection > NR 1 ENGINE B-FIRE DETECTOR LOOP LIGHT ILLUMINATED STEADY IN FLIGHT. A-LOOP TESTED GOOD. SELECTED A-LOOP AND CONTINUED OK, 26-71-10-01. - [SDR CKSA97276](https://openairdocs.org/sdr/CKSA97276.md): Fire Contl Unit · malfunctioned · Jun 12, 1997 · N108CK · Lkheed 1011385115 · Fire Detection > FIRE DETECT LOOP ON PILOTS CAUTION AND WARN PNL ILLUM WITH ENG NR 3 B LOOP ON FIRE DETECT PNL ILLUM ALSO. C/W EMERG HANDBOOK PROCEDURE PG 3-3-4, A LOOP DIDN'T TEST, EMERG CHECKLIST C/W. BOTH BOTTLES DISCHARGED, FIRE IND WENT OUT APPROX 2 MINS LATER. HYD PUM - [SDR CKSA97071](https://openairdocs.org/sdr/CKSA97071.md): Control Unit · shorted · Mar 13, 1997 · N107CK · Lkheed 1011385115 · Fire Detection > ENGINE NR 1B LOOP COMES ON DURING FLIGHT. FOLLOWED ABNORMAL PROCEDURE 3-3-3 AFM (FOM). REMOVED AND REPLACED DETECTOR CONTROL UNIT IAW MM 26-11-08, OPS CHECKS NORMAL. - [SDR CKSA96135](https://openairdocs.org/sdr/CKSA96135.md): Fire Warning · activated · Sep 10, 1996 · N103CK · Lkheed 1011385115 · Fire Detection > KMIA - FLT 78614 - NR 2 ENGINE A-LOOP LIGHT CAME ON WHILE SETTING CLIMB THRUST AFTER TAKEOFF. SELECTED LOOP B AND TESTED OK. WENT BACK TO BOTH POSITIONS AND A AND B LOOPS WERE ON WITH LIGHTS AND BELL. RAN ENGINE FIRE AND SEVERE DAMAGE CHECKLIST ALONG WITH L - [SDR CKSA96061](https://openairdocs.org/sdr/CKSA96061.md): Fire Loop · malfunctioned · Jun 20, 1996 · N103CK · Lkheed 1011385115 · Fire Detection > NR 2 ENGINE A-FIRE DETECTION LOOP CAME ON STEADY IN CLIMB. SWITCHED TO B-LOOP AND TEST IAW OPS MANUAL CHECKED GOOD. APPROXIMATELY 5 MINUTES LATER FIRE WARNING SOUNDED ON B-LOOP, SHUT NR 2 ENGINE DOWN IAW OPS MANUAL. INSPECTED NR 2 ENGINE, NO DEFECTS FOUND. ## 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 = 'RB211524B02' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/engine/rolls-royce-rb211-524b-02/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.