GE CF6-80C2B1F
Service difficulty reports · 768
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 = 'CF680C2B1F' 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 = 'CF680C2B1F' 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 UIEA2019111985929Oil System · abnormal#4 ENGINE OIL QTY DECREASED TO 4 QTS, PRECAUTIONARY ENGINE SHUTDOWN. (<P>REMOVED AND REPLACED #4 ENGINE IAW AMM 71-00-02 AND MCS PACKAGE 59263. LEAK AND OPS CHECK GOOD PER AMM 71-00-00.</P>)SDR U2RA201910220001Valve · stuckDURING REFUELING, THE RIGHT HAND SURGE TANK STARTED VENTING FUEL. - FOUND NUMBER 4 MAIN TANK REFUEL VALVE STICKING IN THE PARTIALLY OPEN POSITION. EXERCISED THE VALVE MANUALLY AND SYSTEM OPERATIONAL CHECK WAS NORMAL IN ACCORDANCE WITH B747-400 AIRCRAFT MAINTESDR U2RA201908160001Spoiler · damagedPARTS DEPARTING AIRPLANE REPORTING - NUMBER 6 SPOILER PANEL FOUND DAMAGED, WITH PIECES MISSING. - NUMBER 6 SPOILER PANEL WILL BE REPLACED, PRIOR TO NEXT DEPARTURE.SDR UIEA2019081215000Engine · stalledENG 4 COMPRESSOR SURGE OR STALL ABOVE 48% N1, NR 4 ENGINE HIGH VIBRATION, AND HIGH EGT. CHECKED CMC 74576. PERFORMED FIM 71-00 . ALL INSPECTION CHECKS FOUND OUT OF SERVICE LIMITATIONS. REMOVED AND REPLACED THE NR 4 ENGINE ASSEMBLY AND OPERATIONAL CHECK NORMSDR UIEA2019080604956Case · corrodedCORROSION ON OUTER CASE, NR 2 ENG FAN CASE ON 12 O'CLOCK TO 6 O'CLOCK, 8 O'CLOCK TO 12 O'CLOCK POSITION ON NAC STA 163. ACCOMPLISHED FAN CASE CORROSION REPAIR IAW ENG MANUAL GEK92451 ESM 72-23-01-220-572 REV. 88. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR P5CA2019080650162Oil System · lowLOW OIL QUANTITY NR 1 ENGINE. REMOVED AND REPLACED THE NR 1 ENGINE. C/W PER WORK CARD 71044-02-01. OPS CK NORMAL.SDR U2RA201908090002Support Angle · crackedSUPPORT ANGLE PN 65B07430-97 FOR WING TO BODY PANEL 293HL CRACKED AND HOLES MISALIGNED WITH CHORD PN 65B15823-7. REMOVED AND REPLACED SUPPORT ANGLE ASSEMBLY P/N 65B07430-97 AND PERFOMED REPAIR TO CHORD P/N 65B15832-7 IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTISDR U2RA201907180001Life Raft · low pressureUPPER DECK LIFE RAFT REMOVED DUE TO LOW PRESSURE - INSTALLED SERVICEABLE LIFE RAFT PER AIRCRAFT MAINTENANCE MANUAL 25-62-01.SDR U2RA201908100001Skin · crackedNR 1 PYLON SKIRT FAIRING FORWARD INBOARD, OUTER SKIN HAS SHEETMETAL HOLE DAMAGE AND TWO CRACKS. REPAIRED NUMBER 1 PYLON SKIRT FAIRING FORWARD INBOARD OUTER SKIN WITH SPLICE AND DOUBLER REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC. ENGINEERING ORDESDR U2RA201908090005Beam · elongatedLEFT WING TRAILING SUPPORT BEAM AT APPROXIMATE WING STATION 268.192 ATTACHING FITTING BEARING IS MISSING. INSTALLED NEW OVERSIZE BEARINGIN ATTACH FITTING PER FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER 19343.SDR U2RA201908090003Support Beam · damagedLEFT WING TRAILING EDGE SUPPORT BEAM UPPER CHORD P/N 65B11614-15, INBOARD END AT APPROXIMATE WBL 130 HAS 3 EACH ELONGATED HOLES AND CORROSION ON UPPER SURFACE. REMOVED CORROSION AND REMAINING MATERIAL THICKNESS FOUND TO BE WITHIN LIMITS PER B747-400SF SRM 57-5SDR U2RA201908090004Attach Angle · crackedFOUND ONE EACH BREATHER ANGLE P/N 69B13824-11 CRACKED COMMON TO LEFT WING FIXED TRAILING EDGE PANEL OUTBOARD SIDE BETWEEN INBOARD AILERON AND NUMBER FIVE SPOILER. REMOVED AND REPALCED BREATHER ANGLE PER SRM 51-40-02.SDR U2RA201907070001Skin Panel · dentedLEFT FUSELAGE SKIN AT BODY STATION 1430, BETWEEN STRINGER 28 LEFT AND STRINGER 29 LEFT HAS DENT WITH APPARENT CREASE. REPAIRED LEFT FUSELAGE SKIN AT BODY STATION 1430 BETWEEN STRINGER 28 LEFT AND 29 LEFT IN ACCORDANCE WITH SRM 53-00-01 REPAIR 1.SDR U2RA201906120001Window · brokenON POST FLIGHT INSPECTION FOUND WINDOW OUTER PANE ON RIGHT SIDE AT STATION 750 BROKE. REMOVED AND REPLACED MIDDLE AND OUTER WINDOW PANES IN ACCORDANCE WITH B747-400 AMM 56-21-01.SDR P5CA2019060600118Compressor · stalledAT TAKEOFF, ENGINE 1 OR 2 COMPRESSOR STALL, YAW TO LEFT, SEVERAL LOUD BANGS. #1 ENG ACCELERATED MORE QUICKLY THAN OTHERS. ABORTED TAKEOFF WITH NO LIMITS EXCEEDED. INSPECTED BOTH ENGINE 1 AND 2 FOR DEFECTS. NO DEFECTS FOUND FOR ENGINE 2. FOUND METAL AND DEBRISSDR U2RA201905140001Flap · missingON TAKE-OFF AIRCRAFT TRIED TO ROLL TO THE LEFT. DURING FLAP RETRACTION AT APPROXIMATE 10 DEGREE AILERON CONTROL RETURNED TO NORMAL. AIRCRAFT WAS OPERATED TO DESTINATION STATION PHIK AND HAD AN UNEVENTFUL LANDING. ON POST FLIGHT FOUND LEFT WING INBOARD FORE FLASDR UIEA201904223913Warning Message · false activationIN CRUISE, FLIGHT EICAS MESSAGE "ENG 4 OIL FILTER". RETARTED THRUST LEVER TO IDLE BUT MESSAGE STAYED, SHUTDOWN ENG 4.(<P>PERFORMED FIM TASK 71-00 TASK A07. INSPECTED MCD'S AND OIL FILTER, NO DEFECTS NOTED. PERFORMED POST WIND MILL INSPECTION, NO DEFECTS NOTED.SDR U2RA2018123129001Battery Pack · dischargedRIGHT UPPERDECK EMERGENCY EXIT DOOR BATTERY FOUND WITH LOW VOLTAGE. - REMOVED AND REPLACED RIGHT UPPERDECK EMERGENCY EXIT DOOR POWER SUPPLY BATTERY IN ACCORDANCE WITH B747-400 AMM 33-51-06. OPERATTIONAL TEST FOUND SATISFACTORY.SDR P5CA2018112630356Engine · not reportedRTO RUNWAY 25L, @ 80 KTS. DOUBLE POP ON #3 ENGINE, EGT 736 AT IDLE, TAXI TO THE GATE. OIL PRESSURE NORMAL.(<P>REMOVED AND REPLACED #3 ENGINE IAW EO WORK CARDS 71-099-02-01, LEAK AND RUN UP CHECKS WERE NORMAL</P>)SDR P5CA201811200351Shaft · sheared#3 ENGINE OIL PRESSURE DECREASED TO 98 PSI IN FLIGHT, AND THEN 38 PSI AT IDLE. "ENG 3 OIL FILTER" EICAS MESSAGE. RAN QRH PROCEDURE, AND SHUT DOWN ENG 3. (<P>COMPLIED WITH POST WINDMILL INSPECTION IAW B747 AMM 72-00-00-206-059-J00, AND FIM TASK 71-00 A07 "ENG 3SDR U2RA201811180001Panel · delaminatedRIGHT WING LEADING EDGE PANEL FOUND DELAMINATED. REMOVED AND REPLACED RIGHT WING LEADING EDGE PANEL IAW SRM 51-40-02.SDR U2RA201811120001Adc · faultyRIGHT TRANSPONDER ALTITUDE REPORTING IN ERROR, AS REPORTED BY AIR TRAFFIC CONTROL. TROUBLESHOOTING REVEALED THE ERROR WAS CAUSED BY THE BY THE LEFT DIGITAL AIR DATA COMPUTER. THE LEFT DIGITAL AIR DATA COMPUTER WAS FOUND TO BE READING 250 FOOT HIGH. THE LEFT DSDR U2RA201811090001Stringer · crackedNUMBER 20 VARIABLE CAMBER FLAP ATTACHMENT STRINGER HAS 1 EACH CRACK. REPLACED CRACKED STRINGER PER STRUCTURAL REPAIR MANUAL 51-10-02 AND 51-40-02.SDR U2RA201811090002Stringer · crackedNUMBER 7 VARIABLE CAMBER FLAP ATTACHMENT STRINGER HAS 1 EACH CRACK. REPLACED VARIABLE CAMBER FLAP ASSEMBLY PER AIRCRAFT MAINTENANCE MANUAL 27-81-02.SDR U2RA201810240001Rib · crackedRIGHT HAND LEADING EDGE SUPPORT RIB FOUND CRACKED 0.70 INCHES AT ILES 330. REPLACED RIB PER STRUCTURAL REPAIR MANUAL 51-10-02 AND 51-40-05.SDR U2RA201809280001Stiffener · crackedLEFT HAND WING INTERIOR OF PANEL 511CTA, INBOARD CORNER VERTICAL STIFFENER HAS 1.5 INCH CRACK. REPLACED VERTICAL STIFFENER PER STRUCTURAL REPAIR MANUAL 51-10-02 AND 51-40-05.SDR U2RA201809280002Rib · crackedRIGHT HAND WING LANDING GEAR INBOARD WHEEL WELL DOOR, FORWARD EDGE FOUND 1 EACH 1.2 INCH CRACK. REPAIRED PER DRAWING 52-18298-1 REVISION NEW, DATED OCTOBER 08, 2018.SDR U2RA201809270001Doubler · crackedDURING ACCOMPLISHMENT OF SERVICE BULLETIN 747-53A2651 REVISION 1 STATION 2403.6 TO STATION 2524.4, UPPER LOBE DOUBLER AT THE FUSELAGE VERTICAL STABILIZER ATTACH FITTINGS INSPECTION, A 2 INCH CRACK WAS DISCOVERED ON THE RIGHT HAND SIDE, FROM STATION 2519 TO 252SDR U2RA201809270002Web · crackedRIGHT HAND LEADING EDGE SUPPORT WEB LOWER FLANGE FOUND CRACKED 0.50 INCHES AT WING LEADING EDGE STATION 330.0. REPLACED WEB PER STRUCTURAL REPAIR MANUAL 51-40-02.SDR U2RA201809270003Strap · crackedDURING ACCOMPLISHMENT OF SERVICE BULLETIN 747-53A2839 REVISION ORIGINAL, ON THE LEFT HAND ENTRY DOOR NUMBER 5 AFT UPPER CORNER CUTOUT, 1 EACH 0.125 INCH CRACK WAS DISCOVERED. ACCOMPLISHED SERVICE BULLETIN 747-53A2839 REVISION ORIGINAL PART 5 - PREVENTIVE MODIFSDR U2RA201809270004Strap · crackedDURING ACCOMPLISHMENT OF SERVICE BULLETIN 747-53A2839 REVISION ORIGINAL, ON THE RIGHT HAND ENTRY DOOR NUMBER 5 AFT UPPER CORNER CUTOUT, 2 EACH 0.125 INCH CRACKS WERE DISCOVERED. ACCOMPLISHED SERVICE BULLETIN 747-53A2839 REVISION ORIGINAL PART 5 - PREVENTIVE MOSDR U2RA201809270005Filler · crackedDURING ACCOMPLISHMENT OF SERVICE BULLETIN 747-53A2839 REVISION ORIGINAL, ON THE RIGHT HAND ENTRY DOOR NUMBER 5 AFT UPPER CORNER CUTOUT, 3 EACH 0.10 INCH CRACKS WERE DISCOVERED ON FILLER. ACCOMPLISHED SERVICE BULLETIN 747-53A2839 REVISION ORIGINAL PART 5 - PREVSDR U2RA201809270006Skin · deformedRIGHT HAND WING LEADING EDGE SKIN OUTBOARD OF LANDING LIGHT HAS TILTED FASTENERS. REPAIRED PER STRUCTURAL REPAIR MANUAL 57-41-01-2R-5.SDR U2RA201809250001Power Supply · inoperativeUPPER DECK RIGHT HAND DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY SUPPLY ASSEMBLY PER AIRCRAFT MAINTENANCE MANUAL 31-31-04. LIGHT OPERATES NORMAL.SDR U2RA201809250002Power Supply · inoperativeEMERGENCY LIGHTS L1853, L1854, AND L5735 ARE INOPERATIVE (MAIN DECK LEFT DOOR). REPLACED EMERGENCY LIGHT BATTERY PACK ASSEMBLY PER AIRCRAFT MAINTENANCE MANUAL 33-51-04. LIGHTS OPERATE NORMAL.SDR U2RA201809250003Skin · damagedRIGHT HAND WING LEADING EDGE SKIN RIVETS LOOSE AND HOLES ELONGATED AT ILES 693.5. REPAIRED PER FLIGHT VEHICLES CONSULTING DRAWING NUMBER 57-18290-1 DATED 10/05/2018.SDR U2RA201809250004Skin · wornLEFT HAND BODY LANDING GEAR INBOARD STRUT DOOR INTERIOR SKIN FOUND TO HAVE RIVETS LOOSE AND HOLES ENLARGED. REPAIRED PER DRAWING 52-18303-1.SDR U2RA201809250005Skin · damagedRIGHT HAND BODY LANDING GEAR INBOARD STRUT DOOR INTERIOR SKIN FOUND TO HAVE RIVETS LOOSE AND HOLES ENLARGED. REPAIRED PER DRAWING 52-18315-1.SDR U2RA201809250006Stringer · crackedNUMBER 20 VARIABLE CAMBER FLAP LOWER CENTER STRINGER CRACKED. REPLACED CRACKED STRINGER PER STRUCTURAL REPAIR MANUAL 51-10-02 AND 51-40-02.SDR U2RA201809250007Stringer · crackedNUMBER 7 VARIABLE CAMBER FLAP LOWER CENTER STRINGER CRACKED. REPLACED CRACKED STRINGER PER STRUCTURAL REPAIR MANUAL 51-10-02 AND 51-40-02.SDR U2RA201809250008Attach Bracket · crackedRIGHT HAND WING TRAILING EDGE CAVITY PANEL SUPPORT BEAM AFT END ATTACH BRACKET CRACKED. REPLACED BRACKET PER STRUCTURAL REPAIR MANUAL 51-10-02 AND 51-40-02.SDR U2RA201809250009Skin Panel · corrodedRIGHT HAND WING TRAILING EDGE OUTBOARD FORE FLAP HAS 2 EACH AREAS OF CORROSION ON LOWER SKIN PANEL. CORROSION CLEANUP OUTSIDE OF STRUCTURAL REPAIR MANUAL LIMITS. REPLACED RIGHT HAND WING TRAILING EDGE OUTBOARD FORE FLAP PER AIRCRAFT MAINTENANCE MANUAL 27-51-0SDR U2RA201809240002Reservoir · low pressureRIGHT HAND UPPER DECK DOOR SLIDE RESERVOIR HAS LOW PRESSURE. RESERVOIR REPLACED PER AIRCRAFT MAINTENANCE MANUAL 25-68-02.SDR KCSA2018091731806Engine · unserviceableENGINE 3 OIL FILTER ILLUMINATED. REMOVED AND REPLACED NR 3 ENGINE IAW AMM 71-00 AND TASK CARD 71-001-00-00. PERFORMED TEST NUMBER 3 AND TEST NUMBER 10 IAW AMM 71-00-00. NO DEFECTS NOTED AT THIS TIME.SDR U2RA201807220001Frame · crackedDURING ACCOMPLISHMENT OF SERVICE BULLETIN 747-53A2494 REVISION 2 FOUND FRAME AFT INNER CHORD AT STATION 2230 RT R5 DOOR CRACKED. ACCOMPLISHED FRAME INNER CHORD CRACK REPAIR IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL CHAPTER 53-60-07 REPAIR 7.SDR U2RA201807260002Door Frame · crackedDURING ACCOMPLISHMENT OF SERVICE BULLETIN 747-53A2494 REVISION 2 FOUND FRAME AFT INNER CHORD AT STATION 2231 LEFT HAND R5 DOOR CRACKED. ACCOMPLISHED FRAME INNER CHORD CRACK REPAIR IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL CHAPTER 53-60-07 REPAIR 7.SDR U2RA201807230001Support Frame · crackedLEFT SIDE AIRCONDITIONING BAY, AFT UPPER BODY FAIRING SUPPORT FRAME IS CRACKED AT THE ANGLE. REPAIRED FAIRING SUPPORT FRAME IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL 53-00-71-2R-1 AND 51-70-11.SDR U2RA201807260001Support Rib · crackedLEFT WING TRAILING EDGE SUPPORT RIB WEB AT WBL 255.692 INBOARD OF THE NR 6 SPOILER IS CRACKED. REMOVED CRACKED WEB, FABRICATED NEW LAMINATED WEB IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL 57-51-02-01-1 IDENTIFICATION AND INSTALLED NEW WEB IN ACCORDANCE WITH SDR U2RA201803250001Hose · leakingDURING DECENT TO APPROACH, THE NR 1 HYDRAULIC SYSTEM FAILED DUE TO FLUID LEAK. FOUND THE NR 1 HYDRAULIC SYSTEM AIR DRIVEN DEMAND HYDRAULIC PUMP PRESSURE HOSE LEAKING. REMOVED AND REPLACED THE HYDRUALIC PRESSURE HOSE IIAW MM 29-11-17, 29-11-23, AND 20-1SDR UIEA2018030200312Engine · failedNR 1 ENGINE OIL QUANTITY FELL TO ZERO AND OIL PRESSURE DROPPED BELOW RED LINE. EICAS MESSAGE FOR THE NR 1 ENGINE OIL PRESSURE. ENGINE SHUTDOWN IN FLIGHT. REMOVE AND REPLACED THE NR 1 ENGINE.
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