GE CF6-80 series
Service difficulty reports · 1,092
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 = '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.
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
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 BB05022Lockout · faultyPHL FL 1237, CREW RECEIVED THE EICAS MESSAGES (AIL LOCKOUT) AND (RUDDER RATIO), AND THE ASSOCIATED LIGHTS. CREW WAS ALSO HAVING PROBLEMS WITH THE AUTO THROTTLES DISENGAGING REPEATEDLY. FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCESDR UPS05M44132Engine · leakingNR 1 ENGINE SHUTDOWN IN FLIGHT DUE TO LOW OIL QTY. ATB. ONE AUTO FUEL CHANNEL WLD NOT MAINTAIN FUEL BALANCE. SECOND AUTO FUEL CHANNEL MAINTAINED BALANCE. DUMPED FUEL T O MAINTAIN BALANCE. PERFORMED FSC R-T-S SYSTEM TEST PASSED ON GROUND. NO MSG AND FAULT FOSDR DL767050067Engine · failedWHILE RUNNING APU ON GND WITH PACKS ON MTC NOTICED SMOKE IN THE CABIN AND SMOKE OUT OF APU EXHAUST. FOUND APU COMPRESSOR OUTLET DRIPPING OIL. REPLACED APU.SDR 05FDEA00127Warning Light · illuminatedENGINE NR 2 REV PRESSURIZED ECAM WARNING ON TAKEOFF ROLL. DISCONTINUED TAKEOFF. NO REV OR REV UNLOCK LIGHTS. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATEGORY: C EXPIRATION: 28JAN05 MEL 78-30-01-A: ENGINE (IDENTIFY 1 OR 2) 2 THRUST REVERSER INOP. SDR 05FDEA00107Filter · cloggedTAKEOFF REJECTED AT 90 KTS FOR NR 1 FUEL ENG FUEL CLOG ECAM & WARNING. REMOVED AND REPLACED MAIN FUEL FILTER AS PER MM 73-12-02-4F. NO CONTAMINATION FOUND. ENG RUN AND LEAK CHECK GOOD. OK FOR SERVICE. FILTER CPN 41823.SDR DL764050030Engine · wornNR 2 ENGINE REPLACED ATL 1/13/05 FOR VANE WEAR.SDR 05FDEA00056Structure · corrodedLT WING, TRAILING EDGE UPPER CHORD AT XORS= 1042 FOUND CORRODED. REPAIR CARRIED OUT AT LEFT HAND WING, TRAILING EDGE UPPER CHORD AT XORS= 1042 AS PER FEDEX EA 1-5710-81589, FOUND EXCEEDED LIMITS AS PER SRM 57-20-00 VOLUME I, FIGURE 16.SDR 05FDEA00023Engine · leakingAPPROACHING LEVEL OFF AT FL330 THE NR 2 OIL QUANTITY ON BOTH THE DIAL AND ECAM WAS 4 GALLONS. OVER THE NEXT TWO MINUTES BOTH INDICATORS DROPPED SLOWLY TO ZERO (WITH ENGINE ADVISORY). THEN THE OIL PRESSURE ON THE NR 2 ENGINE DROPPED FROM 36 TO 24 PSI AND STARSDR 04FDEA03236Tube · brokenDURING CRUISE AT F330 LEVEL 2, ALERT"ENG 2 OIL PRESS LOW" OBSERVED OIL PRESS READING 4 IN RED. ALSO, OBSERVED OIL QTY ZERO (0) ON ENG 2. COMPLIED WITH APPROPRIATE QRH PROCEDURES. AFTER SHUT DOWN N1 26.1 EGT 7 N2 22 .1 ENG SHUT DOWN AT 1350Z, LANDED AT 160SDR 04FDEA02953Yoke · damagedMAIN CARGO DECK STA 535 LT 9G NET YOKE ASSY HAS DAMAGE, TRANSVERSE FRAME. MAIN CARGO DECK STA 535 LT 9G NET YOKE ASSY ATTACHED TRANSVERSE FRAME, FLANGE DAMAGED AREAS AT 02 LOCATIONS, TRIMMED AND REPAIR CARRIED OUT AS PER DWG SRZ-53-503.SDR 04FDEA02657Engine · leakingAFTER START NR 2 ENG OIL WAS APPROX 15 QTYS. AFTER 1 37 OIL QTY DECREASED TO 10 QTYS. MONITORED AND SLOW LEAK OVER THE NEXT 45 MIN DOWN TO 4 QTYS. NR 2 ENG SHUT DOWN AT 6 QTYS. OIL TEMP AND PRESS NORMAL DURING THE LEAK. FND OIL TUBE ASSY P/N 1800M14G01 BROKESDR DL764040812Engine · wornPERFORM WIGGLE CHECK INSP OF NR 1 ENGINE 5TH STG VSV LEVER ARMS. DUE NR 2 ENGINE CHANGE FOR VSV REPAIR.SDR AALA20040819Light · inoperativeEMERGENCY EXIT LIGHT AT COCKPIT DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT COCKPIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)SDR DL76G040741Engine · failedDIVERSION INTO PHX, NR 1 ENGINE COMPRESSOR STALL AT CRUISE. PHX MAINTENANCE FOUND METAL IN TAIL PIPE. REPLACED ENGINE.SDR AALA20040808Pump · inoperativeENROUTE, AIR INTERRUPTED ON ACCOUNT OF FUEL FEED PROBLEMS. LANDED WITHOUT INCIDENT. TROUBLESHOOTING IN PROGRESS. --OPEN--SDR DL764040722Pressure Switch · failedRT ENGINE FUEL FILTER MSG ON T/O CLIMB. T/S PER FIM. NO CONTAMINATION FUEL FILTER. REPLACED FUEL DIFF PRESS SW BORROWED FROM CAL. OPERATED ENG PER PFHB, NO DISCREPANCIES.SDR DL764040716Generator · inoperativeLEFT GEN DRIVE LIGHT CAME ON AFTER TAKEOFF AND IDG WAS SUBSEQUENTLY DISCONNECTED ACCORDING TO THE QRH. BPCU FAULTED LEFT GEN OVER FREQ CODE 24-355-01 AND 24-314-11 OVER FREQ. REPLACED LEFT GCU. RAN ENGINE, LEFT ENG GEN SYS CHECK NORMAL.SDR 04FDEA02343Stringer · crackedLT WING, THRU FUEL TANK ACCESS PANEL CUT-OUT 536 CB, UPPER STRINGER NR 10, STRINGER END FOUND WITH CRACK OF ABOUT 10 INCHES LONG. REPAIR CARRIED OUT AT LEFT HAND WING FUEL TANK ACCESS PANEL CUTOUT 536CB, UPPER STRINGER NR 10 AS PER SRM 57-20-00 FIG 10, VOSDR 04FDEA02344Damper · failedAFTER TAKEOFF, GEAR WOULD NOT RETRACT, RETURNED. REMOVED AND REPLACED LT LANDING GEAR PITCH DAMPER REF MM 32-11-15-4 RII:233985, ENT BY: 274911 RPT BY: 274911, R/I 02AUG04 04:39 IAH R, FACT 02AUG04 10:38 IAH U GEAR SWING REQUIRED, JACKED A/C FOR GEAR SWING SDR 04FDEA02336Panel · dentedRT WING OB T/E PANEL ZONE 691 HAS 100 DENTS, OF WHICH 40 ARE DELAMINATED (TOP AND BOTTOM OF PANEL) ( AREA 2 INCHES X 12INCHES ) REMOVED DAMAGED T/E PNL AND INSTALLED NEW T/E PNL IAW A310/200 DWG 57243876.SDR 04FDEA02337Seat Track · corrodedREF. SNRM N00381, MDC BETWEEN FR15A AND FR19 SEAT TRACK 4L HAS (LEVEL 2) CORROSION 12 INCHES FWD OF FR17. REMOVED AND REPLACED SEAT TRACK IAW A310/200 SRM 53-12-16 AND DWG A53610798SDR 04FDEA02339Stringer · crackedLT WING FUEL TANK ACCESS CUT-OUT 538AB, INTERIOR, UPPER STRINGER 9, STRINGER END FOUND WITH ABOUT 10 INCH LONG CRACK. REPAIR CARRIED OUT AT LEFT WING, FUEL TANK ACCESS CUT-OUT 538AB, INTERIOR, UPPER STRINGER 9, AS PER SRM 57-20-00 FIG 10 VOL I. FABRICATED SDR 04FDEA02340Stringer · crackedRT WING THRU FUEL TANK ACCESS PANEL 635 BT CUT-OUT AT MOST UPPER STRINGER NR 12 FOUND STRINGER END WITH CRACK OF ABOUT 10 INCH LONG. FABRICATED REPAIR ANGLES AS PER SRM 57-20-00, FIGURE 10, VOLUME I AND INSTALLED REPAIR ANGLES AT RT FUEL TANK PANEL NR 635BT SDR 04FDEA02341Stringer · crackedRT WING, THRU FUEL TANK ACCESS PANEL CUT-OUT 636AB, UPPER STRINGER NR 11 STRINGER END FOUND WITH CRACK OF ABOUT 8 INCHES LONG. FABRICATED REPAIR ANGLES AS PER SRM 57-20-00, FIGURE 10, VOLUME I AND INSTALLED REPAIR ANGLES AT RT WING FUEL TANK ACCESS PANEL CUT SDR 04FDEA02342Stringer · crackedRT WING, THRU FUEL ACCESS PANEL CUT-OUT 636CB MOST FORWARD, UPPER STRINGER NR 10, STRINGER END FOUND CRACK OF ABOUT 10 INCHES LONG. FABRICATED REPAIR ANGLES AS PER SRM 57-20-00, FIGURE 10, VOLUME I AND INSTALLED REPAIR ANGLES AT RT WING FUEL TANK ACCESS PANSDR 04FDEA02333Bracket · corrodedRT WING, IB FLAP OB HINGE (FLAPSIDE) PIVOT HOLE NR 1 OB BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMITS AS PER CMM 57-52-03.SDR 04FDEA02334Bracket · corrodedRT WING, IB FLAP OB HINGE (FLAPSIDE) PIVOT HOLE NR 1 IB BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMITS AS PER CMM 57-52-03.SDR 04FDEA02331Skin Panel · corrodedRT HORIZONTAL STABILIZER NR 3R BARREL NUT BORE FOUND WITH CORROSION, CLEAN UP OF CORROSION FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-80289.SDR 04FDEA02332Skin Panel · corrodedRT HORIZONTAL STABILIZER NR 35R BARREL NUT BORE FOUND WITH CORROSION, CLEANED UP AND FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-80293.SDR 04FDEA02330Connector · damagedON TAKE OFF ROLL APPROX 60 KTS ECAM MOMENTARALY CAME ON. NR 2 ENG REV PRESSURIZED- INDICATION WENT OUT ABOUT 100 KTS AND CONTINUED NORMAL TAKE OFF. APPROX 800 AGL INDICATION RETURNED TO ECAM AND STAYED ON. PROCEDURE WAS FOLLOWED TO PULL NR 2 THROTTLE TO IDLESDR 04FDEA02300Barrel Nut · corrodedLT NR 32 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79832, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 32L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-551SDR 04FDEA02364Sensor · failed429 77-15 0006235 30JUL04 IAH CLOSE R THREE TIMES DURING CLIMB NR2 ENG, SURGED A/C YAWED TO LT N1 CLIMB LIMIT EXCEEDED (ECAM) CL N' 100 PERCENT SURGE TO 115 PERCENT A/THR TRIPPED OFF LEVEL AT FL 290 CRUISE. ENG. N1 SURGE CR N1 91 PERCENT SURGED TO 1SDR 04FDEA02329Case · crackedNR 2 ENG LT FAN CASE MOST AFT FRAME FOUND CRACKED AT 10 O'CLOCK POSITION. STOP DRILL AS PER AMM 72-33-00-81 AND CONFIRMED CRACK TERMINATED BY STOP DRILL BY FLOURESCENT PENETRANT INSPECTION (FPI) AS PER AMM 70- 10-05-21.SDR DL764040693Battery · dischargedBATTERY PACK WILL NOT HOLD A CHARGE. REMOVED AND REPLACED BATTERY PACKS. ETOPS CATEGORY (E) : PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.SDR 04FDEA02158Reservoir · lowDURING CRUISE FLIGHT AT FL 330 .80 MACH ECAM ALERTED-INDICATING LOSS OF BLUE HYD SYSTEM (HYD RSVR LO LEVEL) - ECAM SYSTEM PAGE SHOWED BLUE HYD SYSTEM RESEVIOR WAS LOW. ECAM PROCEDURE FOR HYD RSVR LO LEVEL ACCOMPLISHED. REMAINING HYD SYSTEMS NORMAL. FOUND SDR DL767040679Wedge · delaminatedIB AFT FLAP TE WEDGE WAS FOUND WITH DAMAGE TO THE LOWER SKIN AND CORE. REPAIRED IAW ERA 091685-14.SDR DL767040678Skin · crackedRT LOWER WING SKIN SIDE LINK FITTING ATTACH FASTENER FOUND CRACKED. REPAIRED IAW ERA 091372-14AD.SDR USA2004F00083Warning Light · illuminatedENROUTE, THE FORWARD EQUIPMENT COOLING LIGHT ILLUMINATED AND WOULD NOT EXTINGUISH IN THE STANDBY MODE. FLIGHT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED GROUND AND FLIGHT MODE TESTS OF THE EQUIPMENT COOLING SYSTEM AND COULD NOT DUPLISDR 04FDEA02148Slide · deployedUNINTENTIONAL CAPTIVE. RAMP PERSON OPENED DOOR AFTER PUSHBACK. (R.FWD DOOR) SLIDE DEPLOYED, BUT FAILED TO DEPLOY. ACN RELEASED FOR SERVICE IAW MEL/CDL: 52-11-01-02 ATTN: MX; FLT SAFETY HAS REQUESTED THE SLIDE THAT FA ILED TO DEPLOY BE SENT TO MATT DUKSDR USA2004F00084Overheat Loop · faultyCLIMBING THROUGH 12,000 FT, CREW RECEIVED EICAS MESSAGE (R ENG OVHT) AND ASSOCIATED LIGHT. AFTER PERFORMING QRH PROCEDURE, LIGHT AND MESSAGE REMAINED. ENGINE WAS SECURED AND THE FLT RETURNED TO DEPARTURE AIRPORT. (SET APPROX 15 MIN) MAINTENANCE REPLACED BOSDR UIEA200400115Skin · dentedFOUND NOSE CARGO DOOR DENTED. AREA APPROX 8 INCHES IN LENGTH 6 INCHES WIDE AND .1875 INCH DEEP ON THE BOTTOM OF THE DOOR, 4 INCHES FROM THE AFT EDGE. EXTERNAL PATCH REPAIR CARRIED OUT IAW SRM.SDR USA2004F00074Battery · dischargedFOUND L1 DOOR EPSU INOPERATIVE. MAINTENANCE REPLACED THE BATTERY.SDR AALA20040594Connector · looseEMERGENCY LIGHT AT SEAT 35H INOPERATIVE. FOUND LOOSE CONNECTOR. TIGHTENED AND SECURED EMERGENCY LIGHT CONNECTOR AT SEAT 35H. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR DL76S040472Ecu · malfunctionedMCO - APU STARTER CONTINUOUSLY POWERED CAUSING OVERHEATING AND SMELL IN APU AIR. REPLACED ECU AND K117 CONTACTOR.SDR DL767040463Stiffener · crackedCRACKS WERE NOTED IN THE RADIUS OF THE RBL AND LBL 10 VERTICAL STIFFENERS OF THE CENTER SECTION FRONT SPAR. CRACKS WERE LOCATED APPROXIMATELY 5 INCHES FROM TOP OF STIFFENER. DAMAGE WAS REMOVED AND SPLICE INSTRUCTIONS PROVIDED VIA ERA 090218-14.SDR 04FDEA01475Hinge · corrodedRT WING, OB FLAP AFT OB HINGE, FOUND IB ACTUATOR HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.062, FINAL DIAMETER =1.190. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76723, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICSDR 04FDEA01476Hinge · corrodedLT WING - OB FLAP AFT IB HINGE, FOUND IB ACTUATOR HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.062, FINAL DIAMETER =1.190. REPAIRED AS PER FEDEX EA 1-5750-76716, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - L/HSDR 04FDEA01477Hinge · corrodedLT WING OB FLAP AFT IB HINGE, FOUND IB ACTUATOR HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS= 0.400, MATERIAL REMOVED= 0.002, REMAINING THICKNESS= 0.398. COMPLIED WITH FEDEX EA 1-5750-76716, WINGS - TRAILINGSDR 04FDEA01489Hinge · corrodedLT WING OB FLAP AFT OB HINGE, FOUND OB ACTUATOR HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PG. 2-4. ORIG. DIAM.: 1.062, FINAL DIAM.: 1.196, REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76722 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUSDR 04FDEA01490Hinge · corrodedLT WING, OB FLAP AFT OB HINGE, FOUND IB ACTUATOR HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIG. THK. OF LUG: 0.402, MATERIAL REMOVED: 0.002, REMAINING THK.OF LUG: 0.400. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76722 - WINGS
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