GE CF6-50C2

Service difficulty reports · 719

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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 = 'CF650C2'
  ORDER BY difficulty_date DESC"

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SDR WRLA2007096Web · crackedDURING C-5 CHECK, CENTER CARGO AFT VERTICAL WALL AT STA 1841, THERE IS A DOUBLER REPAIR INSTALLED WITH BLIND RIVETS AND WITHOUT CRACK BLEND OUT. NR 67342. FAA FINDING. 10-12-07 PERFORM FINAL REPAIR PER SRM VOL.1 53-00-01 P.14.Sep 23, 2007 · N303WL · Doug DC1030F · Fuselage Miscellaneous StructureSDR WRLA2007095Skin · crackedDURING C-5 CHECK, NR 3 AIR CONDITION COMPARTMENT DOOR WAY AFT UPPER CORNER SKIN IS CRACKED. REF NR 67328. 10-12-07 REPAIRED REF DC10 SRM 53-50-00 FIG.3 REV.91.Sep 23, 2007 · N303WL · Doug DC1030F · Fuselage Main, Plate/SkinSDR WRLA2007092Spar · crackedDURING C-5 CHECK, FOUND CRACK FROM NR 3 PYLON LOWER SPAR LT SIDE BESIDE FAN AIR DUCT FEED THROUGH. REF NR 64879. 10-12-07 REPAIRED PER DC10 SRM VOL.1 54-20-00.Sep 23, 2007 · N303WL · Doug DC1030F · Nacelle/Pylon, Frame/Spar/RibSDR WRLA2007093Skin · unknownDURING C-5 CHECK, CUSTOMER REQUEST FOUND UNIDENTIFIED SKIN DOUBLER ON RIGHT HAND SIDE NOSE AT STA 453 LONGERON 41. NR 66431. 10-12-07 EC-INSP REF. NDT SPM PART G REV.13 RESULTS OK. REINSTALLED ORIGINAL DOUBLER CLASS 1 REPAIR REF SRM VOL.1 53-20-00 REV.91Sep 23, 2007 · N303WL · Doug DC1030F · Fuselage Main, Plate/SkinSDR WRLA2007091Skin · crackedDURING C-5 CHECK, FOUND RIGHT AIR CONDITION COMPARTMENT DOOR SKIN PLATE AND INBOARD INTERCOSTAL CRACKED. REF NR 64867. 10-12-07 REPAIR PER DC10 SRM 52-00-01 FIG.4 VOL.1 AND SRM 52-42-01 FIG.1 VOL.3 REV.91.Sep 23, 2007 · N303WL · Doug DC1030F · Air Conditioning DoorsSDR WRLA2007094Vertical Support · crackedDURING C-5 CHECK, RT WING FIXED TRAILING EDGE 1 EACH VERTICAL SUPPORT CRACKED AT STA XORS 164-192. N/R 66448. 10-12-07 REPAIRED ACCORDING TO DWG ARC0295.Sep 23, 2007 · N303WL · Doug DC1030F · Wing Miscellaneous StructureSDR WRLA2007100Seal · missingDURING C-CHECK FOUND THE LOWER CENTER CARGO COMP FIRE EXTINGUISHING LINE JOINT IS OPEN AND SEAL RING IS MISSING AT STA1441. N/R 66723. REINSTALL THE LINE JOINT WITH SEAL RING AND TEST THE DEPLOYMENT LINES REF DC10 AMM 26-22-03.201 REV 81.Sep 18, 2007 · N303WL · Doug DC1030F · Extinguishing SystemSDR G6OA200700006Engine · malfunctionedNR 2 ENGINE OIL PRESSURE STARTED TO DECREASE FOLLOWED BY LOW OIL PRESSURE LIGHT AND RAPID LOSS OF OIL QUANTITY. ENGINE WAS SHUTDOWN.Aug 16, 2007 · N606GC · Doug DC1030F · Engine (Turbine/Turboprop)SDR WRLA2007078Switch · lockedRME/BWI CENTER GEAR TOOK 30 SEC TO RETRACT DID NOT EXTEND NORMALLY, EMERGENCY EXTENSION RELEASED. GEAR EXTENDED IN APPROXIMATLEY 15 SEC. FOUND CENTER GEAR SWITCH ON F/O PANEL LOCKED IN UP POSITION, RETURNED TO NORMAL. DEFLATED CENTER GEAR STRUT, CYCLED CENTJul 1, 2007 · N14075 · Doug DC1030 · Landing Gear Retraction/Extension SystemSDR CNMA20070011Motor · bypassingL-2 DOOR AIR MOTOR IS BYPASSING AIR INTERNALLY DURING OPS CHECK.Jun 12, 2007 · N630AX · Doug DC1030 · Passenger/Crew DoorsSDR ARWA20070605Engine · low pressureDURING TAKEOFF ROLL, NR 3 ENGINE AT FIREWALL THRUST 98 PERCENT N1, N2, EGT AND FUEL FLOW LOW; ABORTED TAKEOFF. PERFORMED TROUBLESHOOTING IN ACCORDANCE WITH M/M 72-00-00; FLUSHED COMPRESSOR DISCHARGE SENSE LINE AND PERFORMED MPA RUN AT BLAST FENCE, ALL PARAMETJun 10, 2007 · N526MD · Doug DC1030 · Engine (Turbine/Turboprop)SDR WRLA2007075Support Fitting · corrodedDURING B-CHECK INSPECTION, CORROSION FOUND ON DIAMETER SUPPORT FITTING TIE BRACE ON LOWER INNER SURFACE IN CENTER LANDING GEAR WHEEL WELL RIGHT SIDE FS 1461. REPLACED SPLICE ANGLES AT FS 1461 PER SRM 51-33-01, SRM 53-14-01, SRM 53-00-01, SRM 51-21-01, SRM 51-May 30, 2007 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR WRLA2007072Longeron · corrodedDURING B-CHECK INSPECTION, CORROSION FOUND ON LOWER END OF LONGERON IN CENTER GEAR W/W RIGHT SIDE AT FS 1461. REMOVED CORRODED LONGERON FROM CENTER GEAR WHEEL WELL. FABRICATED A REPLACEMENT LONGERON FROM 7075-T6 511 AND INSTALLED IAW DC-10 SRM 51-38-01 PG 17May 29, 2007 · N14075 · Doug DC1030 · Fuselage Main, Longeron/StringerSDR WRLA2007074Doubler · corrodedDURING B-CHECK INSPECTION, CORROSION FOUND ON FWD LOWER CORNER OF UPPER CUTOUT SUPPORT DOUBLER FOR AFT HINGE ON CENTER GEAR RIGHT FWD DOOR IN CENTER W/W AT FS 1441. REMOVED DOUBLER, FABRICATED DOUBLER AND INSTALLED DOUBLER, TEE STIFFENER AND SUPPORT FITTING IMay 27, 2007 · N14075 · Doug DC1030 · Fuselage Main, Plate/SkinSDR WRLA2007073Stiffener · corrodedDURING B-CHECK INSPECTION, CORROSION FOUND ON LOWER AFT CORNER OF SUPPORT STRAP IN CENTER W/W RIGHT SIDE ABOVE AFT HINGE ON FWD GEAR DOOR AT FS 1442. REMOVED, FABRICATED, AND INSTALLED TEE STIFFENER IAW DC10 SRM VOL II 51-31-01 & 51-33-01.May 27, 2007 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR WRLA2007071Door Frame · corrodedDURING B-CHECK INSPECTION, RIGHT HAND OVERWING DOOR R-3, AFT LOWER CORNER (AT FLOOR LEVEL) STA 1305 EVIDENCE OF CORROSION UNDER DOOR SILL PLATE. [08-07-07] SILL PLATE SUPPORT CHANNEL FOUND CORRODED BEYOND LIMITS. REMOVED CHANNEL, FABRICATED NEW SUPPORT CHANMay 23, 2007 · N14075 · Doug DC1030 · Fuselage Main, StructureSDR AMTA200700237Slide · no testR4 DOOR SLIDE FAILED TO DEPLOY ON TEST (AUTO AND MANUAL). REINSTALLED SLIDE SN 004456 FOR EVACUATION TEST IAW MM 25-61-01. (K) REPLACED SLIDE IAW MM 25-61-01. (K)May 16, 2007 · N701TZ · Doug DC1030 · Escape SlideSDR ARWA20070501Blades · damagedJUST PRIOR TO ROTATION, DURING TAKEOFF ROLL, A/C SUDDENDLY BEGAN TO VIBRATE, AND DURING INITIAL CLIMB VIBRATION WAS DETERMINED TO BE COMING FROM NR 1 ENGINE. ENGINE WAS SHUTDOWN. [SUP 06-01-07] PERFORMED FULL BOROSCOPE INSPECTION AND FOUND COMPRESSOR SECTIOMay 3, 2007 · N450ML · Doug DC1030F · Turbine Engine Compressor SectionSDR ARWA20070502Tire · failedPOST FLIGHT FOUND NR 5 TIRE SHREDDED AND DAMAGE TO AIRCRAFT AND NR 1 ENGINE. [SUP 06-01-07] REMOVED AND REPLACED NR 6 MAIN WHEEL ASSEMBLY IN ACCORDANCE WITH DC-10 M/M 32-41-01.May 3, 2007 · N450ML · Doug DC1030F · TireSDR CNMA20070006Channel · corrodedBS 2007, RBL 20-23, CORROSION ON CHANNEL SUPPORT UNDERNEATH GALLEY. CORRODED PORTION REMOVED NEW FABRICATED M/F S2920883-12000 AND INSTALLED WITH EXISTING FASTNERS IAW SRM VOL 2 51-31-01 AND CHERRY-MAX MS 2885/6-4/08.Mar 18, 2007 · N270AX · Doug DC10 · Fuselage Miscellaneous StructureSDR XN0A1360Control Unit · malfunctionedRUDDER WILL ONLY GO .5 TO .6666 OR 20 UNITS TO THE LT DURING GROUND CONTROL CHECK. FOUND ARTIFICIAL FEEL AND TRIM UNIT CATCHING ON TRIM STOP. REMOVED AND REPLACED RUDDER ARTIFICIAL FEEL AND TRIM UNIT IAW AMM CHAPTER 27-23-11, OPS CHECKS GOOD IAW AMM CHAPTER 2Feb 3, 2007 · N472AS · Airbus A300B4203 · Rudder Tab Control SystemSDR XN0A1359Gcu · faultedNR 1 PITCH TRIM TRIPPED BEFORE TAXI. ALL COCKPIT LIGHTS STARTED FLASHING WITH POWER-UP FOR TAXI. LOST VSI INDICATORS TEMPORARILY. LOST TAWS INDICATIONS. FOUND NR 1 GCU CAUSING POWER INTERRUPTIONS. R/R NR 1 GCU AND DISCONNECTED NR 2 CSD, OPS CK GOOD IAW AMM Feb 1, 2007 · N472AS · Airbus A300B4203 · AC Generation SystemSDR CNMA20070002Wire Harness · damagedENG NR 3 FIRE WARNING LOOP A AND B ILLUMINATED AFTER TAKE OFF. EXTINGUISHED AT THRUST REDUCTION. REPLACED WIRE HARNESS IN NR 3 ENG IAW MM 20-30. OPS CK NORM. C/W INSP OF NR 3 ENG IAW 07-005 ENG RUN UP, OPS CHECK NORMAL IAW JRH.Jan 7, 2007 · N49082 · Doug DC1030 · Fire Protection System WiringSDR CNMA20060032Battery Pack · dischargedWHILE TESTING EMERGENCY LIGHTS MID-CABIN BATTERY FAILED. REMOVED AND REPLACED MID-CABIN EMERGENCY LIGHT BATTERY PACK OPS CHECK GOOD IAW MM 33-51.Dec 18, 2006 · N17085 · Doug DC1030 · Emergency LightingSDR ARWA20061201Bleed Valve · malfunctionedNR 3 PNEUMATIC TEMPERATURE HIGH, LIGHT ON; TEMP AT RED LINE. FOUND NR 3 ENGINE FAN AIR VALVE STICKING CLOSED; REMOVED AND REPLACED NR 3 ENGINE FAN AIR VALVE IN ACCORDANCE WITH M/M 36-13-03; ALSO REMOVED AND REPLACED HIGH STAGE TEMPERATURE SENSOR IN ACCORDANCEDec 5, 2006 · N478CT · Doug DC1030F · Compressor Bleed ValveSDR 06FDEA03962Pressure Switch · failedNR 3 MANIFOLD LT, ILLUMINATED PASSING 3000 WITH FE STANDARD PANEL SETUP. ENGINE WING ANTI-ICE ON PRESSURE WAS 60. FOLLOWED QRH AFTER PHASE ONE PRESSURE, REMAINED AT 40. THROTTLE BROUGHT TO IDLE, PRESS DROPPED TO 20 DURING RTB TO MEM FACT, 11NOV06 20:47 MENov 11, 2006 · N313FE · Doug DC1030 · Pneumatic Indicating SystemSDR 06FDEA03702Seat Track · corrodedFOUND MAIN CABIN SEAT TRACK CORRODED BETWEEN STA 842 AND STA 890 RBL 8. REMOVED CORROSION, FABBED AND INSTALLED SPLICE, LOCATED, DRILLED AND INSTALLED SEAT TRACK IAW MD/DC 10 SRM 53-70-00 FIGURE 1A PAGE 7, VOL I, AND 51-31-01 VOL II MAJOR REPAIR MECH 7593 QC3Oct 19, 2006 · N10060 · Doug DC1010 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA03703Longeron · corrodedCENTER CARGO BAY L52 STA.1521-1526, UPPER SURFACE IS CORRODED. REMOVED AND REPLACED CORRODED LONGERON, LOCATED, DRILLED AND INSTALLED LONGERON IAW DRAWING NEA 6076, REV AK, MD SRM 51-33-01 FIG 1, PAGE 1, VOL II. MAJOR REPAIR, MECH 7198 QC340.Oct 19, 2006 · N10060 · Doug DC1010 · Fuselage Main, Longeron/StringerSDR 06FDEA03704Seat Track · corrodedFOUND CABIN STA 1169-1249 RBL76 SEAT TRACK CORRODED. REMOVED, DRILLED AND INSTALLED SEAT TRACK AND SPLICE IAW 53-70-00, FIG,1 VOL I, MAJOR REPAIR MECH 4644 QC388.Oct 19, 2006 · N10060 · Doug DC1010 · Fuselage, Seat/Cargo Attach FittingsSDR WRNA200600036Axle · overtempAFTER LANDING, NR 4 BRAKE TEMPERATURE REACHED 600 DEGREES, FUSE PLUG DISCHARGED AFTER PARKING. PERFORMED BRAKE OVERHEAT INSPECTION IAW AMM 05-51-16, FOUND AXLE DISCOLORATION IN BEARING AREA OUT OF LIMITS. REPLACED AXLE IAW CMM REV.8 DATED 03/02/1998. A/C RETUOct 18, 2006 · N504TA · Airbus A300B4203 · Main Landing Gear Strut/Axle/TruckSDR WRNA200600037Cadc · dirtyAT START OF TAKEOFF, F/O AIR SPEED INDICATION RAPIDLY WENT TO 90 KNOTS, CAPT MOVED NORMALLY. TAKEOFF WAS ABORTED, RETURNED TO GATE. CLEANED AND RE-RACKED NR 2 CADC. OPS CHECKED OK IAW AMM 34-12-34, AIRCRAFT RETURNED TO SERVICE.Oct 16, 2006 · N821SC · Airbus A300B4203 · Airspeed/Mach IndicatorSDR WRLA2006099Attach Bracket · corrodedDURING "C" CHECK IN RME FOUND 5 EA ATTACH BRAKETS CORRODED ON RIGHT O/B FLAP VANE. INSTALLED 5 SERVICABLE ATTACH BRAKETS ON RIGHT FLAP VANE IAW DC10 MM 57-52-02.Oct 15, 2006 · N304 · Doug DC1030F · Trailing Edge FlapsSDR WRLA2006098Seat Track · corrodedITEM: DURING (C) CHECK IN RME FOUND RT OB TRACK HAS EXFOLIATING CORROSION JUST AFT OF R1 DOOR LAV AREA FUSELAGE STA 466.500. REMOVED RT OB TRACK ON MAIN DECK AND REPLACED AS REQUIRED IAW SRM 53-70-00.Oct 4, 2006 · N304WL · Doug DC1030F · Fuselage, Seat/Cargo Attach FittingsSDR WRLA2006097Door · missingDURING WALKAROUND FOUND MISSING PRESSURE RELIEF DOOR FROM NR 1 ENG LT HAND SIDE CORE COWL, DOOR HINGE DAMAGED AND COWLING SKIN CRACKED ABOUT .875 INCH FORWARD OF DOOR HINGE AREA; CHECKED WING FUSELAGE AND TAIL, NO DAMAGE NOTED. REPAIRED AS PE 14-121-379 BOEINOct 1, 2006 · N14075 · Doug DC1030 · Engine Cowling SystemSDR WRLA2006077Stiffener · corrodedDURING C-CHECK IN GSO FOUND LT WHEEL WELL BS1521 OB STIFFNER ANGLE HAS SECTION MISSING DUE TO CORROSION. REMOVED AND REPLACED STIFFNER WITH A NEW FABRICATED STIFFNER IAW DAC DWG AEA0025, ALODINED, PRIMED AND PAINTED IAW SRM 51-21-01 VOL II.Sep 5, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR WRLA2006078Angle · corrodedDURING "C" CHECK IN GSO, FOUND LEFT WHEEL WELL BS1521 INBOARD BULKHEAD ANGLE CORRODED. REMOVED AND REPLACED WITH A NEW FABRICATED ANGLE IAW DAC DWG AEA0025, ALODINED, PRIMED AND PAINTED IAW DC10 SRM 51-21-01 VOL II.Sep 5, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR WRLA2006079Pressure Panel · corrodedDURING C-CHECK IN GSO FOUND LT WHEEL WELL BS1521 LOWER WEB HAS SEVERE INTERGRANUALAR CORROSION. REMOVED AND REPLACED WITH A NEW FABRICATED INTERCOASTAL IAW DAC DWG AEA7163, ALODINED, PRIMED AND PAINTED IAW SRM 51-21-01 VOL II.Sep 5, 2006 · N14075 · Doug DC1030 · Fuselage Main, BulkheadSDR WRLA2006054Channel · corrodedITEM: DURING "C" IN GSO FOUND HAT CHANNEL HAS SURFACE CORROSION AROUND FASTENER HOLE AT STA 1921 BL0. REMOVED AND REPLACED HAT CHANNEL IAW SRM 51-31-01 VOL II.Aug 11, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR WRNA200600034Engine · making metalNR 1 ENGINE STALLED 3 TO 4 TIMES, EGT 909 C. REDUCED POWER TO IDLE AND RETURNED TO FIELD FOR SAFE LANDING. POST FLIGHT INSPECTION FOUND METAL IN TAIL PIPE, ENGINE WAS REPLACED IAW 71-00-00 AND AIRCRAFT RETURNED TO SERVICE.Aug 10, 2006 · N506TA · Airbus A300B4203 · Engine (Turbine/Turboprop)SDR WRLA2006050Floor Support · corrodedITEM: DURING "C" IN GSO FOUND FLOOR BOARD SUPPORT CHANNEL HAS SURFACE CORROSION AT STA 1877 - 2007 RBL26. REMOVED AND REPLACED FLOOR SUPPORT CHANNEL IAW SRM 51-31-01 VOL II.Aug 10, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR WRLA2006053Floor Support · corrodedITEM: DURING "C" IN GSO FOUND FLOOR BOARD SUPPORT CHANNEL CORRODED ON UPPER SURFACE APPROX STA 1915. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT IAW SRM 51-31-01 VOL II.Aug 10, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR WRLA2006056Seat Track · corrodedITEM: DURING "C" IN GSO FOUND SEAT TRACK CORRODED AT LBL28 STA 420-457. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-31-01 VOL II.Aug 10, 2006 · N14075 · Doug DC1030 · Fuselage, Seat/Cargo Attach FittingsSDR WRLA2006063Floorbeam · crackedDURING C-CK IN GSO FOUND MAIN CABIN FLOORBEAM CRACKED AT STA 1482 B/N LBL 107 AND LBL 80. FABRICATED FLOOR SUPPORT IAW DC 10 DWG. INSTALLED FLOOR SUPPORT.Aug 10, 2006 · N14075 · Doug DC1030 · Fuselage Main, Floor BeamSDR WRLA2006042Intercostal · corrodedITEM: DURING "C" IN GSO FOUND CABIN ZONE 220 UNDER FLOOR AREA STA 475 BL95R CORRODED INTERCOSTAL. FABRICATED INTERCOSTAL IAW DC10 DRWG 7186-502. ALODINED & PRIMED IAW DC10 SRM 51-21-01 VOL II. INSTALLED FLOOR SUPPORT IAW SRM 51-31-01.Aug 9, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR WRLA2006064Web · crackedDURING C-CK IN GSO FOUND WEB AT STA 1960-1986 AT RBL 50 CRACKED AROUND FASTENER HOLES. REMOVED WEB IAW DC10 SRM 51-31-01 COL II. FABRICATED DOUBLER IAW DC10 SRM 53-16-01 VOL III. ALIGNED, PRIMED, AND PAINTED, IAW DC10 SRM 51-21-01 VOL I. INSTALLED DOUBLER Aug 9, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR WRLA2006041Floor Support · corrodedITEM: DURING "C" CHECK IN GSO FOUND MAIN CABIN AT STA 828 AT BL-0 FLOOR SUPPORT CORRODED. REPLACED FLOOR SUPPORT BEAM IAW DC10 SRM 51-31-01 VOL II.Aug 8, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR WRLA200637Smoke · detectedFEW SECONDS AFTER NR 3 ENG STARTER WAS ACTIVATED (BUTTON LOCKED) AND LIGHT ILLUMINATED; NOTICED SMOKE WAS COMING OUT OF THE OVERHEAD ANNUNCIATOR PANEL. ABORTED START AND START BUTTON PULLED. ALL POWER WAS TURNED OFF AND SMOKE CEASED.Aug 7, 2006 · N303 · Doug DC1030F · Standard Practices/StructuresSDR WRLA2006048Floor Support · corrodedITEM: DURING "C" IN GSO FOUND MAIN CABIN AT STA 832 AT APPROX RBL46 TO LBL46 FLOOR SUPPORT CORRODED. REMOVED AND REPLACED FLOOR SUPPORT BEAM IAW SRM 51-31-01 VOL II.Aug 7, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR WRLA2006043Floor Support · corrodedITEM: DURING "C" CHECK IN GSO FOUND CABIN ZONE 220 UNDER FLOOR AREA STA 450 BL35L SCALLOPED BEAM CAP CORRODED. REMOVED AND FABRICATED NEW FLOOR SUPPORT IAW DOUGLAS DWG ABA8306 REV K. INSTALLED FLOOR SUPPORT IAW SRM 51-35-01 VOL II.Aug 5, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR WRLA2006028Seat Track · corrodedDURING ACCOMPLISHEMENT OF CARGO MOD J/C SP11530505-7014, FOUND TRACK P/N AFA7795-11 CORRODED (REF STA 1811-1871, X=-8.5). TRACK SECTION REMOVED AND REPLACED WITH TRACK P/N WSP0826-527 IWA DWG SP11530505-7013.Aug 4, 2006 · N279 · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
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