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 AALA20140603022Pump · malfunctionedCREW REPORTED RT CTR FUEL PUMP LIGHT ILLUMINATED WITH ASSOCIATED EICAS MSG. APPROX 30 MINUTES LATER RT ENG BEGAN SURGING. RT ENG BLEED LIGHT ILLUMINATED WITH EICAS MSG & STATUS MSG FOLLOWED, RT ENG SPEED CARD. EMER DECLARED RETURNED & LANDED WITHOUT INCIDENSDR U2RA201406020001Slide Raft · unserviceableRIGHT DOOR NR 1, SLIDE RAFT FOUND UNSERVICEABLE DUE TO THE RT SIDE BULGING OUT & BENDING RELEASE PINS.SDR U2RA201405270003Battery Pack · dischargedDURING ACCOMPLISHMENT OF TASK CARD 33-004-01-01, THE L2 DOOR EMER LIGHT FAILED THE EMER LIGHT TEST. FOUND BATTERY PACK DEPLETED.SDR USAA2014052100004Eec · faultyCLT FLT 1857 EN-ROUTE CLT TO MCO. DURING TAKEOFF RT ENG WOULD NOT DEVELOP TAKEOFF THRUST, RT ENG EEC LIGHT ON, REJECTED TAKEOFF APPROXIMATELY 80KTS. REPLACED RT ENG EEC. VENDOR SHOP FINDINGS, THIS EEC WAS EXCHANGED FOR ANOTHER AT THE VENDOR.SDR AALA20140513004Thrust Reverser · corrodedNUMBER 1 ENG OTBD THRUST REVERSER INNER UPPER AFT AREA HAS CORROSION. INSTALLED NEW SERVICEABLE NR 1 OTBD THRUST REVERSER IAW CARD 78-94-01.SDR USAA2014080100011Door · missingOIL FILL DOOR MISSING NR 1 ENG AFTER FLIGHT. REPLACED NR 1 ENG OIL SERVICE DOOR IAW SRM 51-40-02. OK FOR SERVICE.SDR CALA2014032100376Probe · faultyRT ENG PROBE HEAT REPLACED P1 PROBE IAW MM73-21-04-404-013-R-00.SDR CALA2014031700339Engine · surgesDURING CLIMB BETWEEN FL180 & FL230 RT ENG BEGAN SURGING 1.66 - 1.69 EPR. ALL ENG PARAMETERS FOLLOWED ACFT DUCT PRESS SPLIT 35R 50L. WHEN DUCT PRESS EVENED SURGE STOPPED FLUCTUATION 1.66 & 1.69 EPR. PERFORMED POWER PLANT INSP IAW MM 71-00-00-206-007-R00. NOSDR FDEA201402040254Target · out of adjustON TAKEOFF ROLL THE RT REVERSER ECAS MESSAGE CAME INTERMITTENT REJECT AT 80 KTS. REVERSER SECURED IN FWD THRUST POSITION. FOUND THE RIGHT LOCK PROX TARGET, TOO FAR AWAY FROM SENSOR. INSTALLED SHIMS ON RIGHT LOCK PROX SENSOR, PER AMM 78-30-00-5-4. GAP IS WISDR AALA20140127002O-Ring · tornDFW INFLIGHT LAX-GRU CREW REPORTED LT ENG OIL DECREASING AT ALTITUDE. EMERGENCY DECLARED FLIGHT DIVERTED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED TORN LT ENG OIL CAP O-RING. SYS GND CHECKED NORMAL OPERATION CLOSED.SDR AALA20130928008Engine · failedJFK CREW REPORTED LOSS OF LT ENGINE OIL PRESSURE. ASSOCIATED EICAS "OIL PRESSURE" MESSAGE. CREW SHUTDOWN ENGINE. EMERGENCY DECLARED FLIGHT RETURNED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LT ENGINE AT JFK ON 09/29/2013. SYSTESDR IPXA3577501Cowling · corrodedINSPECTION TYPE:C-10, NR 2 ENGINE OTBD T/R SKIN ACCESS PLATE AND FASTENERS CORRODED REMOVED AND REPLACED NR 2 OTBD T/R.SDR CA110721007Valve · brokenDURING MASTER MCD INSPECTION, ON REMOVAL OF THE MCD PROBE, THE SELF SEALING VALVE BROKE OFF AND FELL DOWN OIL TUBE. THE OIL TUBE WAS REMOVED TO RECOVER PARTS, THE MCD HSG WAS REPLACED (PN VA3509). PARTS BEING SENT TO ENGINEERING AND MFG ADVISED.SDR CA110707001Compressor Blade · damagedON POWER UP FOR TAKEOFF, CREW RECEIVED ECAM MESSAGE "ENGINE SURGE" FOLLOWED BY "ENG FAIL" MESSAGE. ACFT RETURNED TO GATE FOR INVESTIGATION. BOROSCOPE INSPECTION REVEALED MODERATE HP COMPRESSOR STAGE 5 BLADE DAMAGE AND SUBSTANTIAL HP COMPRESSOR STAGE 6 BLADE SDR CA110708010Idg · failedDUE IDG FAILURE AND UNABLE TO CONFIRM IDG DISCONNECTED CREW ELECTED TO RETURN TO DEPARTUE FOR OVER WEIGHT LANDING APRX 210.0 KG. ELEC IDG 1 OIL SYS FAULT. OIL PRESSURE LOW , IDG OIL TEMP RISING COULD NOT ASCERTAIN WETHER IDG WAS DISCONNECTED AFTER IDG P/B PUSDR HALA2011041000150Exciter · inoperativeETOPS SIGNIFICANT SYS - APU INFLIGHT START UNSUCESSFUL. T/S IAW 49-62-00 APU BITE SHOWS EXCITER IAW AMM 49-41-38. INSTALL NEW EXCITER IAW AMM CKS OK, SUCCESFUL APU START ON FIRST TRY.SDR FDEA201103231185Seat Track · gougedSEAT TRACK AT RBL24.75 FROM STA 1075-1180 HAS SEVERAL NICKS, GOUGES AND DAMAGED DOME NUTS, SEAT TRACK FROM BS 1075-1180, RBL 24.75 OUT OF LIMITS IAW SRM 53-00-52, FIG101, DETAIL 1, P.102. FABRICATED NEW SEAT TRACK, PN BAC 1520-792, BATCH NR 000194663 AND INSSDR FDEA201103231186Seat Track · gougedSEAT TRACK AT STA 1075-1180, RBL45.50 HAS SEVERAL NICKS, GOUGES AND DAMAGED DOME NUTS. SEAT TRACK FROM BS 1075-1180, RBL 45.5, OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 1, P 102. FABRICATED NEW SEAT TRACK, PN BAC 1520-792, BATCH NR 00019046632 AND INSDR AALA20110204JFK01Engine · malfunctionedJFK - CREW REPORTED MULTIPLE LAVATORY SMOKE ALARMS ON APPROACH. EMERGENCY DECLARED FLIGHT LANDED JFK WITHOUT INCIDENT. ALARMS WENT OUT WITH BLEEDS OFF ON THE GROUND. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED ENGINE RUNS AND OIL FUMES WERE IN THE CABIN. SDR HALA2011020200066Adiru · malfunctionedETOPS SIGNIFICANT SYS - BTB - ON TAXI, AUTOFLT, A/P OFF. REALIGNED ADIRU'S, IAW AMM 34-10-00-806-802. NO AUTOPILOT FAULTS NOTED. OK FOR SERVICE.SDR CA110210012Control Unit · burnedBRAKE SYS NR 2 FAULT ON ECAM. FOUND BSCU BURNING ODOR. CHANGED BSCU IAW AMM 32-42-34-400-801. UNIT NAME: BSCU PN C2029339C9C9CSDR CA110117005Check Valve · failedENROUTE, THE FLIGHT EXPERIENCED A YELLOW HYD SYS FAILURE. QRH WAS FOLLOWED AND A PHONE PATCH WAS ESTABLISHED WITH MX CONTROL. THE FLIGHT IS CONTINUING. SN OF CHECK VALVE: 2525, MFG: SAMM..SDR FDEA201101130169Skin · noneNR3 L/E SLAT UPPER SURFACE WS 509.5 HAS A TEMP REPAIR. (CURRENT SRM REQUIRES PERM REPAIR AT C-CHECK) REPAIRED NR3 SLAT ASSY IAW SRM 57-43-02, REPAIR NR1. FINAL REPAIR DIMENSIONS ARE 3" DIAMETER. THE SLAT PN IS: 114N4004-165A, SN: A1-0122. THE REPAIR WAS PSDR CA110110007Blades · failedDURING THE INITIAL TAKEOFF ROLL THE NUMBER 1 ENGINE STALLED AND FAILED. THE CREW REJECTED THE TAKEOFF AT APPROX 5 KNOTS AND TAXIIED BACK TO THE GATE. NR 1 ENG BORO CARRIED OUT AS PER AMM 72-00-00-200-813 - HP 5TH STAGE HAD APPROX 30 BLADES WITH TIP CURL - INSDR CA110104003Eec · failedDURING TAXI OUT TO DEPART, THE LEFT ENGINE STALLED THEN FAILED AFTER MINOR POWER UP. THE AIRCRAFT RETURNED TO THE GATE. REPLACED EEC AS PER AMM 73-21-34PB401. REPLACED ALL 7 (4IP/3HP) BLEED VALVES PER AMM 75-33-42/75-33-43. GROUND RUN CHECKED SERV. OTHER SDR DALA1052887001Light · brokenDURING EMERGENCY LIGHT TEST FOUND DOOR 1R EXIT LIGHT BROKEN, REPLACED LIGHT AND CHECKS OK.SDR IPXA10563881Door · bindingFWD ENTRY DOOR HANDLE DIFFICULT TO OPEN AND CLOSE. C/W AMM 52-12-00-5. TEST OF THE LATCH SYS 20 LBS TO LATCH AND MORE THAN 1 LB TO RELEASE LATCH. FORCES WITHIN LIMITS. OK FOR SERVICE.SDR HALA121700595Power Supply · inoperativeDURING EMERGENCY LIGHT TEST, DOOR 3 LT EXIT LIGHT WAS INOPERATIVE. THE EMERGENCY POWER SUPPLY UNIT (EPSU), BATTERY AND DOOR 3 EXIT SIGN WERE REPLACED AND TESTS OK.SDR 2010FA0001248Light · inoperativeR1 DOOR EXTERIOR LIGHT INOP. (EMERGENCY EXIT SLIDE LIGHT)SDR FDEA201012144664Skin · misrepairedEXISTING REPAIR ON R1 DOOR INNER SKIN , DOES NOT CONFORM TO PREVIOUS OPERATOR DATA (REF 8110-3 ). ACCOMPLISHED EA F-5210-146201. DOORS- CREW AND PASSENGER-- R1 ENTRY DOOR INNER SKIN REPAIR. THIS IS A CAT A. REPAIR MAJOR REPAIR WITH 8100-9.SDR FDEA201012064599Skin · dentedAFT CARGO DOOR EXTERNAL SKIN, HAS A DENT, APPROX BS 1435. EVALUATED DENT IAW SRM 52-30-01,DETAIL 6 AND FOUND OUT OF LIMITS IAW SRM 52-30-01, FIG 101, DETAIL 6; A/Y=20. HFEC NOTED NO CRACKS. CUT OUT SKIN IAW SRM 52-30-01,STEP 3. REMOVED FASTENERS IAW SRM 51-40SDR FDEA201011304521Skin · dentedLT FUSELAGE SKIN HAS A DENT AT BS 1715, S16L, ACCOMPLISHED EA F-5330-142297; "FUSELAGE-PLATES AND SKIN-SECTION 46-FUSELAGE SKIN, SMOOTH DENT REPAIR, BS 1715, S16L" REF FAA FORM 8110-3, DATED 11/18/2010; "FIRST STAGE APPROVAL", DTE PENDING NOT TO EXCEED 12 MONSDR FDEA201011264491Skin · delaminatedNR5 SLAT T/E LOWER SURFACE OTBD CORNER SIDE DELAMINATED. REPAIRED NR 5 SLAT IAW SRM 51-70-06. MAJOR REPAIR.SDR FDEA201011264493Skin · damagedRT WING NR 10 L/E SLAT T/E LOWER SURFACE PUNCTURED. REPAIRED RT WING NR 10 SLAT T/E WEDGE IAW SRM 51-70-10. MAJOR REPAIR.SDR FDEA201011234468Skin · dentedEXTERNAL FUSELAGE SKIN HAS DENT AT STA 1705 S-15L. ACCOMPLISHED ON EA F-5330-143215, STA 1705 SKIN REAPIR AT STR 15L CAT B, REPAIR OF FAA FORM 8100-9 JAN 6, 2011 A NEW FAA APROVAL WHICH MUST BE ISSUED FINDING COMPLIANCE WITH 14 CFR 26.43 (D) AND 25.571 PRIORSDR FDEA201011234469Skin · corrodedRT WING NR9 L/E SLAT, OTBD AREA, CORROSION RUNS UNDER BOTH FASTENERS. ACCOMPLISHED EA F-5740-141230; WING L/E SLAT NR9, NOSE SKIN CORROSION REPAIR. REF. FAA FORM 8100-9, DATED 11/12/2010. REPAIR ACCOMPLISHED ON SLAT ASSY. PN; 141N4003- 174, SN; A2-0122. COSDR FDEA201011224463Frame · corrodedCORROSION ON BOTTOM FRAME FROM LBL 10 TO LBL 23, STA 1040. WTB FRAME CONSIDERED SECONDARY STRUCTURE.SDR IPXA0563647Bulb · inoperativeEMERGENCY LIGHT ASSY HAS 4 BULBS INOP. RELAMPED INOP BULBS IN EMERGENCY LIGHT ASSY IAW AMM 33-51-01-2.SDR FDEA201011124327Stringer · corrodedFWD PITT, LT SIDEWALL, BS 755, S24L, CORROSION BETWEEN SKIN AND DOME NUT STRIP. REMOVED CORROSION FROM STRINGER IAW SRM 51-10-02. BLENDED AREA; L=2.5", W=1.1", D=.030", ORIG. MATL. .080", AFTER REWORK; .050" REMAINING, OUT OF LIMITS IAW SRM 53-00- 03, FIG 1SDR HALA2010111200536Monitor · odorREPLACED MONITOR DUE TO F/A REPORTED ELECTRICAL ODOR IAW 23-32-10, P4001.SDR IPXA0563606Gps · malfunctionedAFTER T/O REC'D FAULT GPWS ALERT INCLUDING TERR AND PULL UP ADVISORIES. CREW CONF FAULTY MESSAGE WHILE ENROUTE AND DETERMINED DATA WAS OK, BUT IRS DATA AND POS INFO WAS NOT OK. LT IRS AND FMC PPOS DISPLAYED CORRECT POSITION. GPWS OPS CK PERFORMED IAW AMM 34SDR IPXA0563605Window · failedF/O WINDOW UNABLE TO CLOSE WITHOUT USING 2 PEOPLE. REQUIRES FORCE TO CLOSE WINDOW EXTREMELY HIGH. ABLE TO CLOSE WINDOW AFTER 8 ATTEMPTS. ACCOMPLISHED ADJUSTMENT OF INBD/OTBD OF NR2 WINDOW IAW AMM 56-11-02-5 PARA (3). OPS CK NORMAL. OK FOR CONTINUED SERVICE.SDR CA101110011Connector · broken(CAN) FUEL LOW PRESSURE SWITCH CONNECTOR 4075KS-B FOUND WITH BROKEN BACKSHELL AND PINS NOT ENGAGING.SDR FDEA201011084283Skin · crackedR4 DOOR HAS TWO LIGHTENING STRIKES WITH CRACKS, BS 1260-1270, S16R. REPAIRED AND ACCOMPLISHED EA F-5210-141228; DOORS 2 EA CRACKS ON R4 DOOR INNER SKIN REPAIR. THIS IS A CAT"A" MAJOR REPAIR IAW FORM 8100-9, DATED 11/01/2010. DOOR ASSY PN: 146N6100-12, SN: 003SDR FDEA201011084284Floorbeam · corrodedMAIN CARGO COMPARTMENT FLOORBEAM UPPER CHORD HAS CORROSION BS 345 BLENDED UPPER CHORD STA 345 IAW SRM 51-10-02, ORIGINAL MATERIAL .125 AFTER REWORK .106 OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL III. EXCEEDS MAX MAT LOSS OF 10 PERCENT OF ORIGINAL MASDR IPXA10563574Skin · dentedFUSELAGE TAILCONE SKIN PANEL HAS DENT AFT OF FS.1941 18" LEFT OF BL."0. REPAIRED IAW EO B757-5330-40076-B.SDR IPXA10563476Skin · damagedFUSE SKIN BLENDOUT 1.25 X .600 .016 DEEP AT BS 620 BETWEEN STR 13L & 14L. REPAIRED IAW EO B757-5330-40378-A.SDR 2010F00228Battery Pack · dischargedFIRST CLASS SEATS MOUNTED EMERGENCY LIGHTS DIM ON TEST. LIGHT SYS TESTED GOOD AFTER REPLACED BATTERY PACK CPN NR BAT5016.SDR FDEA201010264172Skin · gougedL4 DOOR INTERNAL SKIN PANEL AT APPROX STA 1660, STR 13-L HAS A GOUGE. REMOVED DAMAGE IAW SRM51-10-02. REMOVED GOUGE BY BLENDING IAW 52-10-01 PG 104 FIG 101, DETAIL V, L=2.0 W=1.0 D=0.008. ORIG MAT 0.063, AFTER REWORK 0.055 -OUT OF LIMITS IAW SRM52-10-01 PGSDR FDEA201010154080Skin · misrepairedEXISTING EXTERNAL DOUBLER ON L-2 DOOR LOWER FWD HINGE CUTOFF DOES NOT MEET SRM REQUIEMENTS. ACCOMPLISHED EA F 5210-141214,DOORS L-2 DOOR OUTER SKIN EXISTING REPAIR REPLACEMENT, PN 143N6100-3, SN 000474. MAJOR REPAIR.
Back to Rolls-Royce RB-211 series