Rolls-Royce RB-211 series
Service difficulty reports · 353
Newest first. General aviation reporting is voluntary.
Query with SQL
duckdb -csv -c "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 = 'RB211' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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 = 'RB211' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR USAA060145Frame · dentedSTA 1466 STR 26L, ACTION: TRIM OUT DAMAGE AND INSTALLED REPAIR PARTS IAW EA 95421A DEFECT SIZE: 2 INCH.SDR AMTA200600033Attach Angle · corrodedC-1 DOOR LWR BEAM ATTACH ANGLE AT STA 600 CORRODED. REMOVED CORROSION AND FOUND TO BE OF LIMITS IAW SRM. REMOVED AND ANGEL FABRICATED NEW AND INSTALLED IAW SRM. PRIMED TREATED AND PAINTED IAW SRM. (K)SDR CA060104005Oven · shortedFWD GALLEY OVEN FIRE EXTINGUISHED WITH 2 FIRE EXT BOTTLES ACTION. FWD GALLEY NR1/NR 2 OVENS REPLACED. FUNCT CHKD SERV NR 1 OFF HK76R5 NR 2 OFF 8203-17-000 S/N 9403-6150. NR 1 ON 8203-17-000, S/N 96-11-7934 NR 2 ON 568K81.SDR 2005AP02002Guide Vane · crackedENGINE NR 3 LP TURBINE STAGE 3, NOZZLE GUIDE VANE APPROX 6:10 O'CLOCK POSITION ROOT AREA WITH CRACK.SDR CA051208001Tire · blownAFTER T/O FROM YYC, A LARGE PIECE OF TIRE RUBBER WAS FOUND ON RUNWAY, NO UNUSUAL INDICATIONS IN COCKPIT. LANDED IN LHR WITH EMERG SERVICES IN STANDBY, TIRE IS SHREDDED. ACCOMPLISHED INSPECTION AFTER TIRE BLOWN AS PER AMM 05-51-12, REF L4044129 FOR FINDINGS. SDR CA051205005Engine · making metalPRELIMINARY INVESTIGATION AND TROUBLESHOOTING HAS NOTED UNUSUALLY HIGH N3 INDICATION DURING A GROUND START ATTEMPT, WHICH SUGGESTS THAT THE ACCESSORY GEARBOX MAY HAVE LOST COUPLING TO THE N3 ROTOR. AS FURTHER SUPPORTING EVIDENCE, THE MASTER CHIP DETECTOR WAS SDR CA051202005Steering Sys · malfunctionedDURING LEVELING A/C FOR WEIGHT AND BALANCE PURPOSES, GREEN SYS ELECT HYD PUMP WAS TURNED ON TO POSITION HORIZ STAB, A/C WAS BEING LEVELED USING 5 LANDING GEAR AXLE JACK POINTS, N/G STEERING SWITCH WAS SELECTED OFF AND N/G STEERING BY-PASS PIN INSTALLED. AT THSDR USAA051415Skin · gougedSTA 1300 STR 29R GOUGED. CUT OUT DAMAGE AND REPAIRED IAW EA 97045. DEFECT SIZE: .15 INCH, L X .10 INCH, W X .031 INCH D.SDR USAA051414Skin · gougedSTA 1337 STR 30 GOUGED. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 53-00-01 REPAIR 2. DEFECT SIZE: 1.0 INCH, L X .080 INCH, W X .017 INCH D.SDR ANCF200400061Actuator · failedBOTH FLAP POINTERS ARE ON HALF POSITION WITH THE FLAP LEVER UP. L/E SLAT DISAGREE LIGHT ILLUMINATED. L/E SLAT DISAGREE DISPLAY ON EICAS. VOICE RECORDER CB WAS PULL OUT AS SB REQUEST. IAW AMM 27-58-01 PAGE 501 ACCOMPLISHED RIGGING ON TRANSMITTER POSITION SLASDR AMTA200501026Wire · disconnectedEMERGENCY FLOOR PATH LIGHTING INOPERATIVE AT ROW 28, EXIT MARKER AND 2 LIGHT AT LAV D. RECONNECTED LIGHT ASSY WIRES. OPS CHECK GOOD. (K)SDR BB05096Controller · failedON DESCENT, VIBRATIONS WERE FELT FROM THE LEFT ENGINE. MAINTENANCE REPLACED THE NR 1 BLEED VALVE CONTROLLER.SDR AALA20050715Battery Pack · inoperativeSFO EMERGENCY LIGHTS AFT OF SEAT 28 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AFT OF SEAT 28. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)SDR AMTA200500711Fire Loop · malfunctionedRT ENGINE FIRE LP 2 DISPLAYED. PERFORMED FIM 26-11-00, FIG 103 BITE PROCEDURE. NO FAULTS FOUND COULD NOT DUPLICATE. INSPECTED ENG LOOPS FOR DEFECTS. NONE FOUND. OK FOR SERVICE. (K)SDR AMTA200500602Skin · damagedNOTICED SCRAPE ON LOWER TAIL SKIN DURING WALK AROUND. COMPLIED WITH ERA. (K)SDR P9RA20050082Odor · detectedEN ROUTE, FLT LEVEL 360, ELECTRICAL FUMES IN COCKPIT AND CABIN. HAD ENGINE ANTI ICE ON AND CONT IGNITION ON. SMELL DISSIPATED WHEN THESE ITEMS WERE SELECTED OFF. PERFORMED INSPECTIONS OF ENGINES, AIR CONDITIONING PACKS, IGNITION SYSTEMS. GROUND RAN AIRCRAFT SDR AMTA200500420Shim · migratedATTACH FITTING, HORIZONTAL STABILIZER LT PIVOT FITTING HAS MIGRATING SHIMS AT ATTACHMENT TO BS 1862.7 BULKHEAD - 3 LOCATIONS. COMPLIED WITH PART 1: TIME LIMITED REPAIR OF ERA NR 757-53R-58-73IR. (K)SDR AMTA200500421Shim · migratedATTACH FITTING, HORIZONTAL STABILIZER RT PIVOT FITTING HAS MIGRATING SHIMS AT ATTACHMENT TO BS 1862.7, BULKHEAD, 1 LOCATION. COMPLIED WITH PART 1: TIME LIMITED REPAIR OF ERA 757-53R-587-3IR FOR THE HORIZONTAL STABILIZER RT PIVOT FITTING. (K)SDR DL777050136Engine · making metalMETAL DISCOVERED IN MCD AND SCAVAGE FILTER NR 2 ENGINE. REPLACED ENGINE.SDR CA050127001Odor · detected(CAN) IN CRUISE LOUD GRINDING NOISE HEARD MID GALLEY, AFT J CLASS. AIRCRAFT FILLED WITH ACRID SMELL. AFT AND MID CABINS FILLED WITH SMOKE. SMELL AND SMOKE LASTED ONE TO TWO MINUTES. ALL SYSTEMS INDICATED NORMAL. PACK FLOW SET TO HIGH FOR 15 MINS. SMELSDR ANCF200400038Radio · inoperativeRECEPTION ON L VHF COMM INOPERATIVE, TRANSMISSION O.K. AND R VHF INOPERATIVE AND DEFERRED. AFTER LANDING 2 VHF COMM BECOME NORMAL. IAW WDM 23-12-02 AND 23-12-02 VHF COMM CONTROL PANEL WIRING WAS CHECKED AND OPERATIONAL TEST WAS PERFORMED IAW AMM 23-12-00 PAGESDR AMTA200401398Wire · disconnectedL2 DOOR EGRESS LIGHTS INOPERATIVE AT ROW 9 R/SIDE (2 EA). RECONNECTED WIRING AT ROW 8 AND 9. OPS CHECK, OK.SDR P9RA20040038Warning Light · inoperativeAIRCRAFT IN MAINTENANCE; ORD. 4R DOOR SLIDE ARMED LIGHT INOPERATIVE. REMOVED AND REPLACED DOOR ARM LIGHT ASSEMBLY.SDR 750WL0008Battery Pack · inoperativeEMERGENCY LIGHTS AT 2LT ARE INOPERATIVE. REPLACED BATTERY PACK IAW MM. OPS CHECKS OK.SDR ANCF200400026Slat · out of adjustEICAS MESSAGE LT SLAT DISAGREE DISPLAYED. WITH THE FLAP LEVER IN 1 BOTH FLAP POINTERS INDICATE .5. LT SLAT DISAGREE CHECK LIST ACCOMPLISHED AND MESSAGE REMAINED ON AFTER PROCEDURE COMPLETED. PERFORMED FIM PROCEDURE 27-81-00 PAGE 116 BLOCKS 1 AND 27 AND ADJUSDR AWXA200400747Connector · wornON TAKEOFF ROLL NR 2 ENG WOULD NOT REACH TAKEOFF EPR WITH THRUST LEVER FULL FORWARD & ENGINE LIMITER OFF, ENGINE PARAMETERS NORMAL FOR LOW EPR, REJECTED TAKEOFF 90 KTS. MX RAN ENGINES TO TAKEOFF POWER 3 TIMES, ALL INDICATIONS NORMAL. ISSUED MEL 73-21-09 COND. SDR AMTA200400847Battery Pack · inoperativeNUMEROUS EMERGENCY EXIT LIGHTS INOPERATIVE. INSTALLED BATTERY PACK, OPS CHECK OK IAW MM 33-51-07.SDR USAABB04063Bleed Valve · failedMIA - FLT 1463 - WITH THE LEFT PACK ON MEL, DESCENDING FROM FL350, THE RIGHT BLEED SYSTEM BLEED LIGHT ILLUMINATED. THE BLEED SYSTEM WAS RESET, BUT TRIPPED OFF AGAIN. THE CABIN ALTITUDE BEGAN TO CLIMB. THE AIRCRAFT DESCENDED TO 10,000 FEET AND DIVERTED TO MISDR USA2004F00067Charger · inoperativeFOUND EMERGENCY LIGHTS FOR RT SIDE OF ROWS 1 THROUGH 7 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER AND BATTERIES.SDR AMTA200400583Connector · disconnectedEMERGENCY EGRESS LIGHT, ROW 35 AFT GALLEY INOPERATIVE. RECONNECTED EGRESS LIGHT AT ROW 35, OPS CHECK OK.SDR AMTA200400570Idg · disconnectedGEN DRIVE AND DRIVE WARNING LIGHT FLICKERS. IDG WAS DISCONNECTED. REMOVED AND REPLACED NR 1 ENG IDG IAW M57-24-01.SDR AMTA200400555Charger · malfunctionedRT AFT PWR PACK FOR EMERGENCY LIGHT DOES NOT FLASH. LIGHT IS ON SOLID. REMOVED AND REPLACED POWER PACK IAW MM. OPERATION NORMAL AT THIS TIME.SDR AMTA200400440Controller · malfunctionedON TAKEOFF LT ENGINE BLEED OFF LIGHT ILLUMINATER. RESET UPON ARRIVAL AT KMDW SYSTEM NORMAL . REMOVED AND REPLACED REVERSE FLOW CHECK CONTROLLER IAW AMMSDR USA2004F00022Odor · detectedCREW NOTED A BURNING ODOR IN THE AFT GALLERY. MAINTENANCE COULD NOT FIND A PROBLEM. AN ENGINE RUN WAS PERFORMED. THE CONDITION COULD NOT BE DUPLICATED.SDR USA2004F00021Static Line · looseCREW HAD DIFFICULTY IN ARMING THE R1 DOOR. MAINTENANCE FOUND THE SLIDE STATIC LINE LOOSE AND RESECURED THE END LOOP AROUND THE GIRT BAR.SDR AWXA200400261Tpu · malfunctionedDURING DESCENT INTO LAS, WITH IDLE THRUST LEVERS THE NR 1 ENGINE SHUTDOWN. ENGINE RESTARTED AND OPERATED NORMALLY, RECEIVED STATUS MESSAGE LT ENG LP PUMP WITH ENGINE FAILURE FRM 73-11-05-01. DECLARED EMERGENCY, AND LANDED WITH NO FURTHER DIFFICULTIES. MAINTSDR AMTA200400241Warning Light · false activationEICAS MSG. RT EMERGENCY DOOR. COULD NOT DUPLICATE FAULT, OPENED DOOR AND INSPECTED SWITCH. COMPLIED WITH NR3 DOOR WARNING SYSTEM TEST. N O DEFECTS NOTED. RESECURED DOOR AND SLIDE. REF MM 52-71-00 AND W/C 222R2509.SDR USA2004F00015Apu · leakingENROUTE, CREW RECEIVED THE EICAS MESSAGE (R GEN DRIVE) AND THE ASSOCIATED LIGHT. THE IDG WAS DISCONNECTED. THE APU WAS BROUGHT ON LINE, BUT SUBSEQUENTLY PERFORMED AND AUTO SHUTDOWN. THE FLIGHT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLASDR USA2004F00005Odor · detectedDURING MAINTENANCE FERRY FLIGHT, CREW REPORTED A SMOKE ODOR IN THE FLIGHT DECK. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RAN PERFORMED AN ENGINE RUN WITH THE PACKS ON. THE CONDITION COULD NOT BE DUPLICATED.SDR USA2004F00006Slide · deflatedDURING THE OPERATIONAL CHECK OF THE RIGHT FRONT PASSENGER DOOR SLIDE, THE SLIDE DEPLOYED BUT DID NOT HOLD PRESSURE. THE LOWER SUPPORT CHAMBERS DID NOT RECEIVE ENOUGH PRESSURE, AND THE ENTIRE SLIDE HAD LOST MOST OF ITS PRESSURE WITHIN FIVE MINUTES OF BEING DEPSDR AMTA200400200Sensor · malfunctionedRT ENGINE NR 2 WENT TO O/S 103.4 4SEC. REMOVED AND REPLACED TPSU IAW AMM. OPS CHECK IAW 71-00-00-5 TEST 3. OK FOR SERVICE.SDR USA2004F00016Slide · leakingDURING ANNUAL SLIDE OPERATIONAL CHECK, THE R1 DOOR SLIDE DEPLOYED PROPERLY, BUT FAILED TO HOLD PRESSURE. MAINTENANCE ACTION PENDING.SDR AWXA200400186Light · brokenDURING INSPECTION EMERGENCY ESCAPE PATH LIGHT LENS AT SEAT ROW 16 LT WAS FOUND MISSING. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 16 LT, OPERATIONAL CHECK WAS GOOD.SDR USA2004F00003Cable · brokenIT WAS REPORTED THAT CATERING HAD ATTEMPTED TO OPEN THE L4 DOOR FROM OUTSIDE. OPENING OF DOOR DID NOT FEEL CORRECT SO ATTEMPTED TO OPEN DOOR WAS ABORTED. WHEN DOOR WAS CHECKED FROM INSIDE, ARMING LEVER WAS FOUND TO BE IN ARMED POSITION. MAINTENANCE FOUND ASDR AALA20040055Line · leakingORD T2095/11 CARGO REPORTED EVIDENCE OF FLUID LEAK FROM THE RIGHT HAND ENGINE UPON ARRIVAL AT GATE. INVESTIGATION REVEALED LP FUEL PUMP LINE HAD CHAFED AGAINST THE HYDRAULIC LINE CAUSING A HOLE IN THE FUEL PUMP LINE. REPLACED FUEL LINE ON NR 2 ENGINE. LEAKSDR AMTA200301524Circuit Card · malfunctionedSTATUS MSG RT ENG OH LP 2. SWAPPED LP 2 CARD WITH THE LP1 CARD ON ENG 2. PERFORMED BITE TEST. NO MESSAGE ON STATUS PAGE OR MECHANIC PAGE.SDR ANCF200300031Seal · out of positionDURING TAKEOFF ROLL A STRONG NOISE CAME IN TO COCKPIT, LT SIDE WINDOW, WAS NOT FUSELAGE. SEAL WAS REPOSITIONED IAW AMM 56-11-00 PAGE 401.SDR AALA20031260Tpu · failedAPPROX 1 HOUR AFTER DEPARTURE AT COMPLETION OF CLIMB TO FL 380, THE THROTTLES RETARD TO 1.35 EPR A POSSIBLE COMPRESSOR STALL HAPPENED AT THAT POINT AS WE HEARD A POP AND THE AIRCRAFT BOUNCED. NEITHER PILOT WAS LOOKING AT ENGINE INSTRUMENTS TO SEE ANY INDICATISDR P9R2003F00000Lamp · burned outL1 DOOR SLIDE LIGHT INOPERATIVE. REMOVED AND REPLACED LAMPS IAW BMM 33-00. (K)SDR P9R2003F00001Slide · dislodgedL1 DOOR SLIDE-RAFT OUT OF CASING. INSTALLED L1 SLIDE-RAFT IAW BMM 52-11. HARNESS ASSEMBLY PN 416N25035.(K)
Back to Rolls-Royce RB-211 series