GE CF6-80C2B7F
Service difficulty reports · 405
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 = 'CF680C2B7F' 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 = 'CF680C2B7F' 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 P5CA2017011200014Link · wornFOUND NR 2 ENG LEFT LPT ACC DUCT SUPPORT LINK AT FWD AND AFT FLANGE UPPER SIDE WORN OUT. REPLACED IAW AMM 70-50-00-912-001 REV 120 AND ALL CONDITION CHECKED NORMAL.SDR UIEA2017010100001Start Valve · failedRT ENGINE STARTER EICAS MESSAGE DURING ENGINE START. CONFIRMED THE START VALVE NOT OPENING. PERFORMED MANUAL START. REMOVED & REPLACED THE NR 2 START VALVE IAW AMM 80-11-02, OPS CHECKED GOOD. MESSAGE NO LONGER DISPLAYED.SDR P5CA2016121000322Warning Message · false activationLEFT AND RIGHT BLEED VALVE EICAS MESSAGES ILLUMINATED INTERMITTENTLY IN FLIGHT AND ON THE GROUND. CHECKED AND NO MESSAGES SHOW IAW AMM 36-23-00. ASCS BITE TEST PASSED, NO FAULTS SHOW.SDR UIEA2016120600974Controller · malfunctionedNR 1 ENG PRV CONTROLLER FOR PRESSURE WAS NOT BETWEEN 40-67. REMOVED AND REPLACED THE NR 1 ENG PRV CONTROLLER IAW AMM 36-11-19.SDR UIEA2016112200879Blade · damagedNR 2 ENGINE FAN BLADE NR 23 SMALL NICK LE ONE INCH FROM TIP. REMOVED THE NICK ON THE BLADE IAW AMM 72-31-02-308-045-H00, FOUND TO BE WITHIN LIMITS IAW AMM 72-31-02-308-045H00 FIG 801.SDR UIEA2016120200961Warning Message · false activationDURING DESCENT, ENGINE ANTI-ICE EICAS RT HPSOV WENT AWAY AFTER A COUPLE OF MINUTES STATUS MSG R ENG HPSOV CLEARED MESSAGE PERFORMED BITE TEST NO FAULTS NOTED , GROUND TEST OK IAW AMM 36-11-00.SDR UIEA2016113000920Tube · damagedNR 2 ENGINE FUEL HEATER TUBE DAMAGED. REPLACED THE TUBE IAW MM 79-21-01.SDR P5CA2016112000294Exciter · failedRIGHT ENGINE IGNITER NR 2 STATUS MESSAGE. FOUND NR 2 EXCITER FAILED. REMOVED AND REPLACED THE EXCITER IAW AMM 74-11-01. SYSTEM TEST ACCOMPLISHED IAW AMM 74-00-00.SDR P5CA2016111400292Eec · inoperativeRIGHT EEC B CHANNEL INOPERATIVE. REMOVED AND REPLACED THE RT ENGINE EEC IAW AMM 73-21-15. OPS CHECKED NORMAL IAW AMM 71-00-00.SDR P5CA2016111200290Ecu · failedRIGHT ENGINE CONTROL STATUS & EICAS MESSAGE. REMOVED AND REPLACED THE RT ENGINE EEC IAW AMM 73-21-15. PERFORMED RT ENGINE RUN IAW AMM 71-00-00. OPS CHECKED NORMAL , NO EICAS MESSAGE.SDR P5CA2016110600286Warning Message · illuminatedAFTER LANDING RIGHT ENGINE CONTROL EICAS MESSAGE. FOLLOWED FIN TASK 73-21 TREE 878. RT ENGINE CONTROL. PIMU CHECK AND FOUND CHANNEL A & B DATA BUSS INOPERATIVE. CYCLE RT PIMU CIRCUIT BREAKER AND RT ENGINE PIMU. TEST PASSED, THEN RT ENG. RUN CHECK OK IAW AMMSDR P5CA2016111300291Ecu · failedRT ENGINE CONTROL STATUS MESSAGE. REPLACED THE RT ENGINE ECU IAW AMM 73-21-14. PERFORM ENGINE MOTORING AND ACTUATOR TEST. IDLE LEAK CHECK, CHECKED NORMAL. NO LEAK FOUND IAW AMM 71-00-00.SDR P5CA2016091900260Compressor Blade · damagedRIGHT ENGINE FAN BLADE TIP NR 34 HAS CURL. RT ENGINE FAN BLADE NR 34 TIP NO CURL, FOUND NR 33 HAS CURL, REPLACED NR 33 IAW AMM 72-31-02. OPS IAW AMM 71-00-00, VIB SURVEY CHECKED WITH IN LIMITS.SDR P5CA2016092100266Pilot Valve · faultyFOUND NR 1 ENGINE T/R STATUS MESSAGE IAW AMM TASK 78-34-01-004-003-H00/404-014-H00, REV 119. REPLACED NR 1 ENGINE DIRECTIONAL PILOT VALVE AND CONDITION CK NORMAL. NR 1 ENGINE T/R SYS TEST C/W IAW AMM TASK 71-00-00-700-807-H03, REV 119.SDR P5CA2016092100267Screw · looseFOUND NR 1 ENG ACOUSTICAL LINER SEGMENT SCREW LSN. RETORQUED NR 1 ENGINE ACOUSTICAL LINER SEGMENT SCREW AND CONDITION CHECK NORMAL IAW AMM 72-33-01-404-011-H00, REV 119.SDR P5CA2016092100268Screw · looseFOUND NR 2 ENGINE ACOUSTICAL LINER SEGMENT SCREW LOOSENED. RETORQUED NR 2 ENGINE ACOUSTICAL LINER SEGMENT SCREW AND CONDITION CHECK NORMAL IAW AMM 72-33-01-404-011-H00, REV 119.SDR P5CA2016091900263Eec · malfunctionedRIGHT ENGINE CONTROL, EICAS, MESSAGE DURING TAXI OUT. CHECK RT ENGINE CHANNEL B SAME DATA MISSING IN EPCS PAGE 2. REPLACED RT ENGINE,
ELECTRONIC ENGINE CONTROL IAW AMM 73-21-15. PERFORMED POWER PLANT TEST NR 11 ELECTRONIC ENGINE CONTROL STATIC TEST AND NR SDR P5CA2016092000264Hmu · malfunctionedRIGHT ENGINE CONTROL, EICAS MSG IAW AMM 73-21-14 REPLACE RT ENGINE HMU IAW AMM 71-00-00-401, CONFIGURATION 3. PFM RT ENGINE DRY MOTOR AND ECU GROUND ACTUATOR TEST AND ALL CONDITIONS SATISFACTORY, NO MSG SHOWS.SDR P5CA2016070500161Strut · inoperativeRIGHT ENGINE, LEFT FAN COWLING FWD STRUT ASSY INOPERATIVE IAW IPC 71-11-11-51, ITEM 595. REPLACED RT ENGINE, LT FAN COWLING FWD STRUT ASSY AND CHECK NORMAL IAW AMM 71-11-11-212-001.SDR P5CA2016061400135Bonding Wire · brokenFOUND NR 2 ENGINE HPSOV JUMPER WIRE BROKEN. REPLACED JUMPER WIRE IAW AMM 70-50-00-912-001-H00, REV 118.SDR P5CA2016061400137Clamp · brokenFOUND NR 1 ENG HPSOV SENSING TUBE SUPPORT CLAMP BROKEN. REPLACED CLAMP IAW AMM 70-50-00-912-001-H00, REV 118.SDR P5CA2016060900132Bonding Wire · brokenFOUND NR 1 JUMPER ENGINE HPSOV, 1 JUMPER WIRE BROKEN. R & R NR 1 ENGINE HPSOV JUMPER WIRE IAW AMM 70-50-00-912-001-H00, REV 18.SDR P5CA2016060900131Clamp · brokenFOUND NR 1 ENGINE HPSOV SENSING TUBE SUPPORT CLAMP BROKEN. R & R CLAMP IAW AMM 70-50-00-912-001-H00, REV 118.SDR P5CA2016031700070Warning Message · false activationDURING DESCENT, EICAS MESSAGE, IDLE DISAGREE, LEFT ENGINE 47 PERCENT, RT ENG 40 PERCENT IN IDLE. ACCOMPLISHED MAINTENANCE PROCEDURE IAW AMM 73-00-00/001. TESTED LT & RT PIMU BITE MSG/ECS MAINTENANCE , NO FAULTS FOUND IAW AMM 77-35-00, P201.SDR UIEA2015122200790Skin · delaminatedFOUND DAMAGE TO INTERIOR OF ENG NR 2 LT COWL. ACCOMPLISHED EO 6771A013 & ENG COWLING NR 2 ENG & LT FAN COWL INTERNAL SKIN DELAMINATED. DAMAGE REPAIR COMPLETED PART 1.SDR UIEA2015110400610Oil System · leakingNUMBER 1 ENG OIL QTY DECREASED 10QTS IN 29 MIN, LARGEST QTY INDICATED WAS 10 QTS INCREASED DURING DESCENT. PERFORMED FIM 79-11 TREE 800 STEPS 1 - 6 & STEPS 6 - 15 SCAVENGE OUT PORT SCREEN NO DEBRIS FOUND IAW MCC & POWER PLANT ENGINEERING. PERFORMED FIM 79-31SDR CA151028006Disc · cracked(CAN) DURING TAXI, AFTER LANDING TOWER ADVISED CREW SMOKE COMING FROM THE RT MAIN GEAR. ENGINES WERE SHUTDOWN. APPLIED WATER AND CREW WAS GIVEN A THUMBS UP. MAINTENANCE ADVISED THE NR 8 BRAKE WAS DAMAGED AND FLUID LEAKED ON THE BRAKE BUT THERE WAS NO FIRESDR P5CA2015101300163Blade · damagedBIRD STRIKE DURING CLIMBOUT, FOUND NR 2 ENGINE FAN BLADE NR 33 DISTORTION. LENGTH 2.5 CORD WIDTH 1.125 DISTORTION .5, 4" FROM TIP OF BLADE. PERFORMED BLEND OUT IAW AMM 72-31-02-226-012-400. AFTER BLEND OUT DIMENSION LENGTH 3.5, CHORD .55, WIDTH .25 DISTORTISDR UIEA2015091100517Line · looseNR 1 ENG OIL LEAK PUDDLING BY IDG. FOUND LOOSE LINE ON THE IDG. TIGHTENED LINE IAW 20-11-00. LEAK & OPS CHECKED GOOD.SDR P5CA2015082700107Support Bracket · crackedCRACK, NR 1 ENGINE LT STARTER DUCT SUPPORT BRACKET CRACK AT LOWER LINK SIDE. AMM 70-50-001, REV 112, REPLACE NR 2 ENGINE LT STARTER DUCT SUPPORT BRACKET WITH SERVICEABLE PARTS. CONDITION CHECK NORMAL.SDR P5CA2015082700106Clamp · damagedDAMAGE, NR 2 ENGINE RT AFT LOWER SIDE D, SUMP OIL PRESSURE TUBE SUPPORT CLAMP DAMAGE IAW AMM 70-50-00-912-001, REV 112, NR 2 ENGINE, RT D, SUMP OIL PRESSURE TUBE CLAMP. CONDITION CHECK NORMAL.SDR P5CA2015082700104Adapter · wornWORN, NR 1 ENGINE LT AND RT CORE COWL HOLD OPEN ROD BEARING AND ADAPTER WORN IAW AMM 70-50-00-912-001 -001, REV 112, REPLACED NR 1 ENGINE LT AND RT CORE COWL HOLD OPEN ROD END AND ADAPTER. CONDITION CHECK NORMAL.SDR P5CA2015082700103Sealant · misinstalledNR 1 ENGINE INLET LIP SEALANT VOID IAW CMM 71-11-16. REPAIR 5, REV 42 APPLY A1 ENG INLET LIP SEALANT. CONDITION CHECK NORMAL.SDR P5CA2015082700101Rod End · wornWORN NR 2 ENGINE LT AND RT CORE COWL SUPPORT ROD END WORN AMM 70-50-00-912-001, REV 112. REPLACED NR 2 ENGINE LT AND RT CORE COWL SUPPORT ROD END. CONDITION CHECK NORMAL.SDR P5CA2015081800092Exciter · malfunctionedLT ENGINE IGNITER 1, ERASED STATUS MESSAGE, LT ENGINE IGNITER 1 AUDIBLE CHECK. REPLACED LT ENGINE IGNITOR 1 EXCITER. IAW AMM 74-00-00, PERFORMED LT ENGINE IGNITOR SYS AUDIBLE TEST, CONDITION SATISFACTORY.
SDR P5CA2015042400023Structure · damagedFOUND LT ENG OTBD THRUST REVERSER COWL T/E AT 7 O'CLOCK POSITION AND RT ENG OTBD THRUST REVERSER; COWL T/E AT 3 O'CLOCK POSITION; EVIDENCE OF LIGHTNING STRIKE. PERFORMED PART 1, TEMPORARY REPAIR AND APPLIED SPEED TAPE IAW EO 6778A030, PART 2.SDR P5CA2014112800055Exciter · malfunctionedSTATUS MESSAGE, LT ENGINE IGNITOR 2" IAW AMM 74-21-02, REPLACED LT ENGINE IGNITOR 2 PLUG IAW AMM 74-11-01. REPLACED NR 2 EXCITER IAW AMM 74-00-00 PRM SUITABLE TEST, FUNCTION NORMAL. NO MORE MSG SHOWING.SDR UIEA2014070100296Status Message · false activationRIGHT IDG VLV STATUS MSG, BPCU SHOWS NO FAULT DEFECT, ERASE MSG IAW FIM 24-20 FT 802.SDR UIEA2014061500234Actuator · malfunctionedDURING SECOND ENG START THE DUCT PRESS BOTH LT & RT STARTED TO FLUCTUATE BETWEEN 30PSI & 5PSI. N2 ROTATION SLOWER THAN NORMAL. EGT DURING START WAS HIGHER THAN FIRST ENG START BUT WITHIN LIMITS. TROUBLE SHOT IAW FIM 36-11 FT831 & 841, NO TROUBLE FOUND. INDSDR UIEA2014060900229Retainer · crackedNUMBER 1 ENG RT C DUCT FWD TORQUE BOX OUTER RING RETAINER FOUND CRACKED AT 1 OCLOCK POSITION. NR 1 ENG RT C DUCT FWD TORQUE BOX OUTER RING RETAINER CRACKED AREA REPAIRED IAW MRAS CF6-80C2 TR CMM 78-32-02 REPAIR 024.SDR NOCA2014020526Light · inoperativeFLT DECK EMERGENCY LIGHT DID NOT ILLUMINATE. R & R LIGHT ASSY IAW MM 33-51-01. OPS CHECKED NORMAL.SDR NOCA2014010623Battery Pack · dischargedIN CABIN EMERGENCY LIGHTS OVERHEAD AFT LT SIDE AISLE WILL NOT ILLUMINATE. R & R BATTERY PACK AT M739 IAW AMM 33-51-01 AND OPS CHECKED OK.SDR NOCA2014010322Battery Pack · dischargedCEILING EMERGENCY EXIT LIGHT FWD & AFT OF R2 DOOR VERY DULL. R & R BATTERY PACK M1209 IAW AMM 33-51-07 & AMM 33-51-00. OPS CHECKED GOOD.SDR NOCA2013120419Contact · wrong partFIRST TWO SECTIONS OF LT SIDE FLOOR PATH LIGHTING INOPERATIVE. R & R INCORRECT CONTACTS ON FLOOR PATH LIGHTS IAW SWPM 20-60-02, RELAMPED AND TESTED GOOD IAW 33-51-00.SDR NOCA2013120320Wire · brokenEXTERIOR EMERGENCY EXIT LIGHT AT R4 DOOR INOPERATIVE. REPLACED TERMINAL OF WIRE IAW SWPM 20-30-11.SDR NOCA2013112518Battery Pack · inoperativeF/A EMERGENCY FLASHLIGHT AT LT OVER WING EXIT NOT BLINKING. R & R BATTERY PACK IAW AMM 25-64-00. OPS CHECKED NORMAL.SDR NOCA2013112316Battery Pack · inoperativeF/A FLASHLIGHT BY R2 DOOR INOPERATIVE. REPLACED FLASHLIGHT BATTERY, OPS CHECKED NORMAL IAW MM 25-54-00.SDR NOCA2013112317Battery Pack · inoperativeF/A EMERGENCY FLASHLIGHT IN AFT GALLEY RED LIGHT NOT BLINKING. R & R FLASHLIGHT BATTERY PACK IN AFT GALLEY CENTER FLT ATTEND STATION. OPS CHECKED NORMAL IAW AMM 25-64-00.SDR NOCA2013102615Circuit Breaker · openL/E SLAT DISAGREE STATUS MESSAGE AT FL 350. FOUND CIRCUIT BREAKER DC STANDBY A2 ON P6-1 PANEL OPENED. RESET CIRCUIT BREAKER IAW AMM 20-60-01 ACCOMPLISHED FIM TASK 27-51-00, FIG 104. NO FAULTS FOUND.SDR UIEA2013101100517Igniter · warning messageSTATUS MESSAGE FOR RT ENGINE IGNITER 2. R & R RT ENGINE SYS 2 IGNITER PLUG IAW AMM 74-21-02, PERFORMED ENG 2 IGNITION SYS AUDIBLE TEST NORMAL IAW AMM 74-00-00. PERFORMED RIGHT ENGINE IDLE RUN IAW AMM 71-00-00, OPS CHECKED NORMAL.
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