GE CF6-80 series

Service difficulty reports · 1,092

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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 = 'CF680'
  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.

SDR AU510002059Lug · broken(AUS) VERTICAL STABILIZER ACCESS LADDER UPPER ATTACHMENT LUGS BROKEN. SUSPECT CAUSED BY POOR SHIMMING OF THE UPPER ATTACHMENT FITTINGS. SEE ATTACHMENT FOR INVESTIGATION DETAILS. (CASA NR 510002059)Dec 12, 2005 · Airbus A330* · Vertical Stabilizer Miscellaneous StructureSDR 05FDEA04216Skin · debondedSMIS 424 51-00 0007102 27SEP05 MC1 CLOSE R MOD TYPE Y MOD NR 9-AGING-INSP REV NO. PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1 ENT BY: 067708 INFO 30NOV05 21:26 MC1 R DISCREPANCDec 10, 2005 · N424FE · Airbus A310 · Elevator, Plate/SkinSDR 05FDEA04217Structure · corrodedSMIS 424 51-00 0007102 27SEP05 MC1 CLOSE R MOD TYPE Y MOD NR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NO. POS PT1 ENT BY: 067708 INFO 30NOV05 21:26 MC1 R DISCREPANCYDec 10, 2005 · N424FE · Airbus A310 · Passenger/Crew DoorsSDR 05FDEA04218Track · crackedSMIS 424 51-00 0007102 27SEP05 MC1 CLOSE R MOD TYPE Y MOD NR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1 ENT BY: 067708 INFO 30NOV05 21:26 MC1 R DISCREPANCDec 10, 2005 · N424FE · Airbus A310 · Fuselage Miscellaneous StructureSDR 05FDEA04241Generator · failedREMOVED AND REPLACED NR1 GCU I/A/W M.M 24-22-12-4, PERFORMED ENG RUN NR 1 GEN. OPS CHECKS GOOD. R/I 10DEC05 07:13 PHL R R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG 764067A SRL A115 ON MFG 764067A SRL 0359.Dec 9, 2005 · N662FE · Airbus A300* · AC Generation SystemSDR 05FDEA04054Floorbeam · nonePREVIOUS REPAIRS ON MAIN DECK CARGO FLOORBEAMS AT FS 34, FS 35, AND FS 36, RT OF CENTER, NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. EVALUATION DETERMINED REPAIRS TO BE IAW EA 6-5310-29466. NO FURTHER ACTION REQUIRED. MINOR REPDec 1, 2005 · N423FE · Airbus A310203 · Fuselage Main, Floor BeamSDR UPS05M45850Control Panel · defectiveN/A DIVERSION - ALL 3 VHF COMMS INOPERATIVE. REMOVED AND REPLACED NR 3 COMM PANEL IAW MM 23-10-01-4 AND TEST IAW 23-11-01-2 AND 23-11-01-2 AND 23-12-01-2 OPS CK NORMAL.Dec 1, 2005 · N255UP · Doug MD11F · VHF Communications SystemSDR 05FDEA04010Engine · bird ingestionON DEPARTURE BIRD STRIKE LT NR 1 ENGINE. ENGINE VIB MAX APPROX 3.7 AT 85 PERCENT. AT IDLE APPROX 1.6; EGT NORMAL, N1 + N2 NORMAL OTHERWISE. REDUCED POWER FOR APPROACH. ENGINE HAS BEEN APPROVED FOR REMOVAL (DAMAGE) NEW ENGINE EXPECTED OMA 12/05/05 (THIS Nov 29, 2005 · N401FE · Airbus A310203 · Engine (Turbine/Turboprop)SDR 05FDEA03987Repair · improperPREVIOUS REPAIR EXT DOUBLER INSTALLED ON L1 DOOR AFT UPPER CORNER NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA REF N00722. REMOVED AND REPLACED COVER DUE TO NONCONFORMITY IAW SRM 52-10-00 FIG 203. MINOR REPAIR IAW GMM 6-2-100.Nov 28, 2005 · N423FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR 05FDEA03989Repair · properPREVIOUS REPAIR INSTALLED ON FUSELAGE RT SIDE AFT OF STATIC PORT EXT DOUBLER AT FR 34 BETWEEN STR 39 RT AND 40 RT NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFACATION AND REPAIR DATA REF N00717. REPAIR FOUND TO BE IAW EA 6-5310-7952, MINOR IAW EA 6-5310-7952.Nov 28, 2005 · N423FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR 05FDEA03994Skin · puncturedPUNCTURE AND DENT IN SKIN APPROX FR 44 RT STRINGERS 6-7. DAMAGE APPROX 5.00 IN X 3.2 IN. CUT OUT DAMAGE IAW A310-200 SRM 53-27-00. NDT FOR CRACKS IAW NTM 51-10-08. NO CRACKS NOTED. INSTALLED REPAIR DOUBLER IAW A310-200 SRM 53-10-12 FIG. 228. WORK DOCUMNov 28, 2005 · N405FE · Airbus A310 · Fuselage Main, Plate/SkinSDR CALA0500390Electrical Box · overheatedFLIGHT CREW REPORTED SMOKE COMING FROM BELOW SEAT 19E WHILE ENROUTE FROM AMS TO EWR. THE SMOKE LASTED FOR ONLY ABOUT 15 SECONDS. AN EMERGENCY DECLARED AND AIRCRAFT LANDED AT EWR W/O INCIDENT. MECHANIC FOUND THE DSEB (DIGITAL SEAT ELECTRONIC BOX) AT SEAT GROUNov 7, 2005 · N68061 · Boeing 767424ER · Entertainment SystemSDR AU510001601Aspirator · failedSLIDERAFT FAILED FLAT FIRE TEST. INSPECTION OF THE INFLATABLE ASSEMBLY FOUND THREE HOLES AND ONE INDENTATION COMMON TO THE LOWER INFLATION TUBE. THIS SLIDERAFT ASSEMBLY WAS FITTED WITH P/N 4A3791-3 PLASTIC PRESSURE RELIEF VALVES (PRV) ON BOTH THE UPPER AND LNov 7, 2005 · Airbus A330* · Escape SlideSDR CALA0500383Rib · crackedINSPECTION FOUND A 0.025 INCH CRACK IN RT WING IB AILERON IB HINGE RIB SUPPORT AT AFT HI-LOK AREA, WS 467.8. THE CRACKED AREA WAS TRIMMED OUT AND A REPAIR WAS INSTALLED IAW ECRA 5740-02094.Nov 3, 2005 · N59053 · Boeing 767424ER · Wing, Rib/BulkheadSDR AALA20050719Battery Pack · inoperativeMIA - EMERGENCY EXIT LIGHTING AT LEFT FIRST CLASS SEAT INOPERATIVE. REPLACED BATTERY PACK AT 110WL1 FOR EMERGENCY EXIT LIGHTING AT LEFT FIRST CLASS SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION.Nov 1, 2005 · N11060 · Airbus A300B4605R · Emergency LightingSDR DL76G050651Engine · smokeCREW REPORTS SMOKE OIL SMELL HAZE IN CRUISE. DONNED MASK AND MADE AN EMERGENCY LANDING. SMOKE DETECTORS IN CABIN WENT OFF. ENGINE USED 5 PINTS OF OIL. ENGINE CHANGED.Oct 24, 2005 · N1611B · Boeing 767332 · Engine (Turbine/Turboprop)SDR UPS05645551A/C Pack · malfunctionedINSPECTION TYPE: ETOP IN FLT FL350 M80 AFTER AND DURING TRANSMITTING NOTICE ACRID ODOR IN COCKPIT, NO OTHER INDICATIONS NOTED. COULD NOT ISOLATE OR IDENTIFY SOURCE OF ODOR 1 PACK OPS, PRIOR TO COAST OUT HF COULD NOT BE OPERATED FOR 45 MINS EVENTUALLY TO WORKOct 4, 2005 · N324UP · Boeing 767300 · Cabin Cooling SystemSDR 05FDEA02917Seat Track · corrodedMDCC SEAT TRACK IS CORRODED. REMOVED CORRODED TRACK AND INSTALLED NEW TRACK IAW SRM53-10-16, 51-40-21, AND51- 23-10.Sep 14, 2005 · N425FE · Airbus A310 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA02918Seat Track · nickedMDCC SEAT TRACK HAS NICKS. REMOVED NICKED SEAT TRACK AND INSTALLED NEW TRACK IAW SRM 53-10-16, 51-27-00,51-40- 40,AND 51-21-00.Sep 14, 2005 · N425FE · Airbus A310 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA02919Seat Track · damagedMDCC SEAT TRACK HAS DAMAGED LUGS. REMOVED DAMAGED TRACK AND INSTALLED NEW TRACK IAW SRM 51-40-21, 51-21-10, AND 53-10-16.Sep 14, 2005 · N425FE · Airbus A310 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA02920Seat Track · corrodedMDCC SEAT TRACK BETWEEN FR. 51 ,52 LBL 56 HAS CORROSION . REMOVED AND REPLACED SEAT TRACK DUE TO OUT OF LIMITS CORROSION IAW SRM 53-10-16 AND 51-40-21.Sep 14, 2005 · N425FE · Airbus A310 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA02905Floor Panel · delaminatedMDCC FLOOR PANEL 242EK IS DELAMINATED. FABED NEW FLOOR PANEL.Sep 14, 2005 · N425FE · Airbus A310 · Fuselage Floor PanelSDR 05FDEA02906Floor Panel · crackedMDCC FLOOR PANEL 232TG IS CRACKED. FABED NEW FLOOR PANEL.Sep 14, 2005 · N425FE · Airbus A310 · Fuselage Floor PanelSDR 05FDEA02907Floor Panel · crackedMDCC FLOOR PANEL 231VG-2 IS CRACKED. FABED NEW FLOOR PANEL.Sep 14, 2005 · N425FE · Airbus A310 · Fuselage Floor PanelSDR 05FDEA02909Floor Panel · puncturedMDCC FLOOR PANEL 231VG IS PUNCTURED. FABED NEW FLOOR PANEL.Sep 14, 2005 · N425FE · Airbus A310 · Fuselage Floor PanelSDR 05FDEA02910Floor Panel · crackedMDCC FLOOR PANEL 231TG CRACKED. FABED NEW FLOOR PANEL.Sep 14, 2005 · N425FE · Airbus A310 · Fuselage Floor PanelSDR 05FDEA02911Floor Panel · crackedMDCC FLOOR PANEL 231KH IS CRACKED. FABED NEW FLOOR PANEL.Sep 14, 2005 · N425FE · Airbus A310 · Fuselage Floor PanelSDR 05FDEA02912Floor Panel · crackedMDCC FLOOR PANEL 231JH CRACKED. FABED NEW FLOOR PANEL.Sep 14, 2005 · N425FE · Airbus A310 · Fuselage Floor PanelSDR 05FDEA02913Floor Panel · crackedMDCC FLOOR PANEL 231JG IS CRACKED. FABED NEW FLOOR PANEL.Sep 14, 2005 · N425FE · Airbus A310 · Fuselage Floor PanelSDR 05FDEA02914Floor Panel · delaminatedMDCC FLOOR PANEL 232NG DELAMINATED. FABED NEW FLOOR PANEL.Sep 14, 2005 · N425FE · Airbus A310 · Fuselage Floor PanelSDR 05FDEA02915Floor Panel · crackedMDCC FLOOR PANEL 241WH IS CRACKED. FABED NEW FLOOR PANEL.Sep 14, 2005 · N425FE · Airbus A310 · Fuselage Floor PanelSDR 05FDEA02916Floor Panel · delaminatedMDCC FLOOR PANEL 232EG IS DELAMINATED. FABED NEW FLOOR PANEL.Sep 14, 2005 · N425FE · Airbus A310 · Fuselage Floor PanelSDR DL76S050543Engine · leakingODOR DETECTED AND SEVERAL SMOKE DETECTORS WENT OFF. ODOR DISSIPATED WITH UTILITY BUSSES OFF, BUT RETURNED WHEN POWER LEVERS ADVANCED. OIL LEAK NR 1 ENGINE. REPLACED NR 1 BEARING MANIFOLD PKNGS, PERF SAME INSPECTION ON NR 2 ENGINE CKS OK. RAN AT HIGH PWR WISep 13, 2005 · N122DL · Boeing 767332 · Turbine Engine Oil SystemSDR AU510001600Valve · leakingLOW PRESSURE FUEL VALVE LEAKING. INVESTIGATION CONTINUING.Sep 7, 2005 · Airbus A330* · Fuel Selector/Shut-Off ValveSDR 05FDEA02716Fire Detector · false indicationDURING CLIMB-OUT AT 20,000 FT, NR 2 ENGINE INDICATED A FIRE: LIGHT IN FIRE CRC AND LIGHT IN FUEL SHUTOFF HANDLE. NO OTHER ANOMALIES NOTED EITHER ON ANALOG GAUGES OR ECAM PAGE. ALL CHECKLISTS COMPLETED TO INCLUDE PULLING FIRE HANDLE & DISCHARGING BOTH BOTTLEAug 30, 2005 · N652FE · Airbus A300B4605R · Fire DetectionSDR 05FDEA02691Engine · fluctuatesNR 2 ENGINE DISPLAYED GRADUAL OIL LOSS TO AN INDICATION OF 1 QT JUST BEFORE DESCENT TO KIX. OIL PRESSURE BEGAN TO FLUCTUATE A LITTLE AND DURING DESCENT AN ALERT "OIL PRESS LO" DISPLAYED. PRECAUTIONARY SHUTDOWN PER QRH. NR 2 OIL PRESSURE WAS AROUND 35 PSI WIAug 25, 2005 · N616FE · Doug MD11 · Engine (Turbine/Turboprop)SDR 2005FA0001279Water Heater · failedFA COMPLAINED ABOUT NO HOT WATER AT GALLEY SINK SHORTLY BEFORE LANDING. ONCE ON GROUND, MAINTENANCE EXPOSED WATER HEATER, GOT HEAVY BURNED SMELL. REMOVED FALSE PANEL COVERING WATER HEATER, NOTED THAT NO CB EITHER ON UNIT OR ON GALLEY CB PANEL HAD TRIPPED. DAug 24, 2005 · N767A · Boeing 7672AX · Wash Water SystemSDR DL76G050433Apu · contaminatedAPU FAULT ON START OF LEFT ENGINE. APU WOULD NOT RESTART. REMOVED PLASTIC BAG FROM INLET AND REPLACED SURGE VALVE.Aug 7, 2005 · N1612T · Boeing 767332 · APU Core EngineSDR DL764050443Engine · wornFAILED OPN 5039 11TH STAGE BORO. REPLACED ENGINE.Aug 7, 2005 · N841MH · Boeing 767432ER · Engine (Turbine/Turboprop)SDR 05FDEA02226Powerplant · crackedW/O 29493, NR N00177, ENGINE NR 1 AT FORWARD INBOARD LOWER HOIST POINT, THE FLANGE IS CRACKED AT IT'S BASE. FPI IAWM NTM 51-91-00 CRACK IS CONTAINED BY STOP DRILL. SWAB ETCHED DAMAGED AREA IAW TASK 70-24-01-110-34 PER GESPM STOP DRILL ACCEPTABLE PER EAAug 3, 2005 · N671FE · Airbus A300F4605R · Engine (Turbine/Turboprop)SDR 05FDEA02227Service difficultyNR 1 ENG FAN CASE HAS 2 PREVIOUSLY STOP DRILLED CRACK ON AFT DOLLY MOUNT AT APPROX 8 O'CLOCK POSITION. FPI IAW NTM 51-91-00 CRACK CONTAINED BY STOP DRILL. SWAB ETCHED DAMAGED AREA IAW TASK 70-24-01-110-34 OF SPM. STOP DRILLS ACCEPTABLE PER EA 6-7223-82106-NAug 3, 2005 · N671FE · Airbus A300F4605R · Engine (Turbine/Turboprop)SDR 05FDEA02228Service difficultyNR 1 ENG FAN CASE HAS 2 PREVIOUSLY STOP DRILLED CRACKS ON FWD DOLLY MOUNTS AT APPROX 8 O'CLOCK. FPI IAW NTM 51-91-00 CRACK IS CONTAINED BY STOP DRILL. SWAB ETCHED DAMAGED AREA IAW TASK 70-24-01-110-34 SPM. STOP DRILL ACCEPTABLE PER EA 6-7223-82106 AND PER AAug 3, 2005 · N671FE · Airbus A300F4605R · Engine (Turbine/Turboprop)SDR 05FDEA01707Engine · failedAFTER TAKEOFF AT SMF NR 1 ENG RPM ROLLED BACK TO 42 PERCENT EGT TO 992 AN HAD SEVERE VIBRATION. SHUTDOWN NR 1 IAW QRH. NOTE HAD NO FIRE WARNING IND. 1 FIRE BOTTLE USED- GND WITNESS OBS FLAMES FROM CENTER OF ENG. EXHAUST REMOVED AND REPLACED #1 ENG NR 1 FIRJun 27, 2005 · N565FE · Doug MD1010F · Engine (Turbine/Turboprop)SDR 05FDEA01677Torque Ring · crackedNR 3 ENG, RIGHT FORWARD FRAME UPPER TORQUE RING CRACKED APPROXIMATELY 5 INCHES IN LENGTH. THRUST REVERSER REMOVED AND INSTALLED AS PER WORK CARD 78T3003-R AND WORK CARD 78T3903-R FOR WORK DETAILS. THRUST REVERSER ADJUSTMENT AND OPERATION CHECK CARRIED OJun 24, 2005 · N619FE · Doug MD11 · Engine (Turbine/Turboprop)SDR DL76S050277Idg · malfunctionedDURING CLIMB-OUT AT 8000 FT, THE LEFT GENERATOR WENT OFF LINE, TRIED TO RESET ONCE BUT DID NOT COME BACK. DIVERT INTO JFK DUE TO SINGLE GENERATOR OPERATION. REPLACED LEFT IDG AND APU EXCITER.May 17, 2005 · N118DL · Boeing 767332 · AC Generator-AlternatorSDR AU510001651Display · failedCAPTAIN`S LT AND FIRST OFFICER`S DISPLAY UNITS READ `DATA INVALID` FOR APPROXIMATELY 20 SECONDS AND THEN RETURNED TO NORMAL DISPLAY.May 7, 2005 · Airbus A330* · Navigation SystemSDR DL76G050244Idg · unreliableLEFT ENGINE DRIVE LIGHT ON AT CRUISE. FOUND OVERSERVICED, SERVICED SAME, CHECKS GOOD.Apr 28, 2005 · N16065 · Boeing 767332 · AC Generation SystemSDR 05FDEA01107Filter · contaminatedDURING TAKEOFF, APPROACHING 80 KTS, FUEL CLOG LIGHT, ECAM AND SINGLE CHIME FOR 1 ENGINE; REJECTED TAKEOFF AND ACCOMPLISHED RTO CHECKLIST. PULLED FUEL FILTER, FOUND DEBRIS IN FILTER. REPLACED FILTER, RAN ENGINE 15 MINS, REMOVED AND INSPECTED FILTER, NO DEBRApr 23, 2005 · N430FE · Airbus A310203 · Engine Fuel DistributionSDR UIEA200500052Skin · dentedSTA 1980-2000, STR 42-44, RT (2 EA) DENT (A) AND (B) WERE FOUND ON THE EXT FUSELAGE. DENT (A) STA 1980-2000, STR 42-43, RT D=0.09, W=1.15 INCH, L=3.8 INCH. DENT (B) STAT 1980-2000, STR 43-44, RT D=0.051, W=1.18, L=1.54. THE DAMAGED AREA TRIMMED OUT. A REPApr 20, 2005 · N412MC · Boeing 74747UF · Fuselage Main, Plate/SkinSDR CALA050110Engine · failedON TAKEOFF, AT APPROXIMATELY 90 KNOTS, RT ENGINE FAILED. REPLACED ENGINE.Apr 18, 2005 · N67158 · Boeing 767224 · Engine (Turbine/Turboprop)
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