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 IPXA10B60336Skin · damagedINSPECTION TYPE:C, DMI D419963-RT INBD FLAP T/E LWR SURFACE SKIN DAMAGED. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10 REPAIR 4, FIG 201, SHEET. 3 REV 56.SDR IPXA10B60337Skin · dentedINSPECTION TYPE:C, DMI D411229 - LT INBD MID FLAP BOTTOM SKIN DENT. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10, REPAIR 4, FIG 201, SHEET 3, REV 56.SDR UIEA2010052600007Rib · damagedDURING WALKAROUND, DAMAGE WAS FOUND TO THE TO THE LT WING T/E INBD MID FLAP OTBD T/E COVE RIB. THE REPAIR PER PART 1 OF THIS EO IS CATEGORY C AND REQUIRES REPETITIVE INSPECTION IAW PART 2 OF THIS EO AT 5 CYCLE INTERVALS AND REPLACEMENT AT THE NEXT A-CHECK AFTESDR UIEA2010052600137Skin · crackedRT WING INBD MID FLAP MOST OTBD T/E FOUND CRACKED (RT WING INBD MID FLAP MOST OTBD T/E LWR SURFACE COMPOSITE HOT BOND REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A. DETAIL REF HX PROCESS CARD SEQ NT EAX 500294-1)SDR UIEA2010052600138Skin · crackedLT WING INBD MID FLAP MOST OTBD T/E FOUND CRACKED. (LT WING INBD MID FLAP MOST OTBD T/E LWR SURFACE COMPOSITE HOT BOND REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A. DETAIL REF HX PROCESS CARD SEQ NR EAX 500344-1).SDR IPXA10B60061Skin · corrodedCORRISION AT FRAME 740 S-46L. REPAIRED IAW SRM 53-00-01 REPAIR 15, DETAIL 1,SDR UIEA2010052400002Skin · damagedDAMAGE WAS FOUND TO THE 65B23701-6 FUSELAGE SKIN AT BS 550 BETWEEN S-31L AND -32L AFTER A BURST EQUIPMENT COOLING EXHAUST VALVE STRUCK THE S-31L STRINGER AND SKIN. REFER TO EO 4453A363 FOR THE STRINGER REPAIR. ACCOMPLISH PART 1 OF THIS EO PRIOR TO FURTHER FLIGSDR UIEA2010052400003Stringer · damagedDAMAGE WAS FOUND TO THE 142U0086-198 STRINGER 31L AT BS 550 AFTER A BURST EQUIPMENT COOLING EXHAUST VALVE TRUCK THE S-31L STRINGER AND SKIN. REFER TO EO 4453A362 FOR THE SKIN REPAIR. THE 142U0086-198 STRINGER IS MADE FROM 0.050 INCH THICK 7075-0 SHEET PER QQ-ASDR IPXA10B60034Hmu · fluctuatesAT CRUISE, NR 2 ENGINE N1 VARIES BETWEEN 90.5 AND 91.0 EGT AND N2 NOTICEABLE FLUCTUATIONS AS WELL. C/O T/S FOR FRM CODE 730, 381 02 IAW FIM 73-03-00-812-839-J00. R & R HMU IAW AMM 73-21-14/401 LEAK CHECK WAS PERFORMED. NO LEAKS NOTED.SDR UIEA2010052000001Warning Message · false activationAIR TURN BACK DUE RUDDER RATIO MESSAGE DISPLAYED (SRM REPLACED AND SYS CHECKS NORMAL (MX WAS ABLE TO DUPLICATE PROBLEM ON GROUND AND CORRECTED AFTER SRM REPLACED, HOWEVER, AS PREC, REQUESTED PITOT STATIC TEST CHECKOUT OF SYS.)SDR UIEA201000187Floorboard · damagedMX FOUND DAMAGE/DELAMINATION TO THE MAIN DECK - FLOORBOARDS BS 385 LBL 3.75 & BS 410 LBL 4.0 (REFERENCE FIG 1). "DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS, INITIATE REPETITIVE DVIS AT EVERY 25 FC AND PERMANESDR UIEA201000186ASkin · crackedEO 4457A250: MX FOUND THE LT - OTBD MID FLAP LOWER SURFACE WITH A CRACK AND DELAMINATION MEASURING 6.56 FT LONG. DAMAGE IS BEYOND THE SRM LIMITS IAW THE SRM 57-53-01, FIG 101. (ALLOWABLE DAMAGE GENERAL). PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WOSDR UIEA201000186Flap · brokenDURING APPROACH, CREW SELECTED 25 DEGREE FLAPS AND LOUD THUMP FELT AND HEARD. ACFT ROLLED SLIGHTLY, CREW CORRECTED AND LANDING WAS UNEVENTFULL. ON POST-FLT WALKAROUND, FOUND LARGE SECTION OF RIGHT WING T/E, INBD FOREFLAP, OTBD END MISSSING (APPROX 12 FT.)SEPSDR IPXA10B59885Skin · damagedLT INBD AFT FLAP LOWER SKIN DAMAGED LOCATION OF DAMAGES NOTED IN EO B7 B747-5700-37548-A. REPAIRED IAW EO B747-5700-37548-B REF LOG PAGE 383520/1/2.SDR IPXA10B59876Skin · damagedLT INBD AFT FLAP L/E SKIN DAMAGED. REPAIRED LT INBD AFT FLAP IAW SRM 51-70-07 AND EO B747-5750-37683-A AN D AMM 51-24-11-7.SDR UIEA201000156Skin · delaminatedDURING MX WALKAROUND, THE NR4 LT FAN COWL INNER AND OUTER SKINS WERE FOUND WITH DELAMINATION. EO: 4471A055 - PART 1 - TIME LIMITED REPAIR THE PART 1 TIME LIMITED REPAIR INSTALLS THROUGH BOLTS TO RESTORE THE CAPABILITY OF THE DISBONDED AREA AND IS FAA APPROVED SDR IPXA10B59747Floor Panel · puncturedMCD FLOOR PANEL HAS 3 PUNCTURES AT FWD EDGE AND 1 IN MIDDLE OF PANEL REPAIRED IAW 747-400F, SRM 53-00-50-2R, REPAIR NR1.SDR UIEA201000155Skin · damagedON WALK AROUND INSP FOUND DAMAGE ON LT MID FLAP L/E (INBD FLAP). "EO 4457A247: DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS BY INSTALLING AN EXTERNAL REPAIR DOUBLER; SCHEDULE REPEAT INSPECTIONS AT EVERY 15 FC ASDR P5CA2010050601635Compressor · damagedMEMO MESSAGE "VVVVVV" DISPLAYED AT 1515Z AT FL 360, ENGINE 3 N2 VIBRATION AT 5.0. ALL OTHER PARAMETERS WERE NORMAL AND MONITORED. AT APPROXIMATELY 12,000 FT, NR 3 ENGINE FAILED. QRH PROCEDURES ACCOMPLISHED. INSPECTION OF TAILPIPE REVEALED NO METAL. BOROSCSDR IPXA10B59605Floor Panel · damagedDMG TO MAIN CARGO DECK FLOOR PANEL 21" FROM FWD EDGE 2.0" FROM OTBD EDGE. DMG IS APPROX 2.0" FORE/AFT AND 1.0" IN WIDTH AND .025 DEEP REF EO B747-5320-36566-A FOR DWG. REPAIRED IAW SRM 53-00-50-2R (4D).SDR IPXA10B59442Inlet · dentedON ASN FOUND DENT ON NR4 ENGINE INLET COWL AT 7 O'CLOCK POSITION. ITEM DEFERRED IAW EO B747-7110-37490A PARAGRAPH 6A. DEF NR 423771, DENT IS BEYOND SRM LIMITS. R & R NR 4 ENG INLET COWL IAW MM 71-11-01-4.SDR IPXA10B59154Skin · damagedLT INBD AFT FLAP LWR SKIN DAMAGED. DAMAGE LOCATED APPROX 188" FROM INBD END OF FLAP AND 4.25" FROM FWD EDGE OF PANEL. REPAIRED REF EOB747-57-50-37299SDR IPXA10B59081Skin · damaged2 DENTS ON LT AFT FLAP APPROX 89" OTBD OF INBD EDGE AND 7.5" FWD OF MID SEAM AND 92" OTBD OF INBD EDGE AND 10" FWD OF MID SEAM. REPAIRED IAW EO B747-5750-33005-E AND SRM 51-70-10-2R.SDR IPXA10B59079Skin · damagedLT INBD AFT FLAP LOWER SKIN DAMAGED. REPAIRED IAW EO B747-5750-33005-D.SDR UIEA201000108Stringer · crackedEO: 4454A096 DURING C-CHECK, A CRACK WAS FOUND IN THE 311U2420-83 PYLON STRINGER TEE AT APPROX NAC STA 300, WL 144.7 ON THE OTBD SIDE. THE CRACK WAS TRIMMED OUT AND A NEW SECTION OF TEE SPLICED IAW SRM 54-51-02, REPAIR 2 WITH MINOR DEVIATIONS IAW EGAT EI T2010SDR UIEA201000131Failsafe · crackedDURING C-CHECK, IN MARCH 2010, A CRACK WAS FOUND IN THE 65B09631-86 BS 1200, S-9L FRAME FAILSAFE CHORD CRACK COMMON TO THE TENSION TIE. A REPAIR ANGLE WAS INSTALLED IAW SRM 51-70-11, REPAIR 1 AND NRC 503951. THE 65B01753-369 FAILSAFE CHORD IS MADE FROM BAC1490SDR UIEA201000132Failsafe · crackedDURING C-CHECK, IN MARCH 2010, A CRACK WAS FOUND IN THE 65B01750-806 BS 1140, S-9R FRAME FAIL-SAFE CHORD CRACK COMMON TO THE TENSION TIE. REPAIR ANGLES WERE INSTALLED IAW SRM 51-70-12, REPAIR 1 AND NRC 503241. THE 65B01750-806 FAILSAFE CHORD IS MADE FROM BAC1SDR IPXA10B58855Seal · brokenSEAL BROKEN ON EMERGENCY DESCENT DEVICE. REPLACED DESCENT DEVICE IAW MM 25-61-01-2.SDR UIEA201000099Web · mismanufacturedEO4453A332, RS NR: R-53-00-36599: WHEN ACCOMPLISHING A MOD ON THE SUBJECT ACFT IAW REF E, REF C FOUND SEVERAL SEM FASTENER HOLES AS SHOWN IN FIG 1. THE MINIMUM EM IS FOUND TO BE 1.38D. FABRICATE NEW -1 WEB IDENTICAL TO EXISTING WEB 1456U1321-7 FROM 0.032" THSDR UIEA201000171Skin · dentedA DENT WAS FOUND IN THE FUSELAGE SKIN AT BS 1993 BETWEEN S-41L AND S-42L. THE DENT MEASURES 3.5 INCHES LONG BY 0.5 INCHES WIDE AND 0.020 INCHES DEEP."THE DENT WAS INSPECTED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL III BUT WITHIN LIMITS FSDR IPXA10B58097Compressor · stalledNR 2 ENGINE COMPRESSOR STALL ON TAKEOFF. CURRENTLY OOS. REMOVED AND REPLACED NR 2 ENGINE IAW TASK CARD 71-000-00-01, VERSION 13.SDR UIEA201000088Skin · delaminatedLT WING UPPER SURFACE OTBD, ALL OTBD AREA FOUND DELAMINATED. RT WING OTBD AIL UPPER SURFACE DELAMINATED AT SEVERAL LOCATION AS MARKED. LT WING UPPER SURFACE OTBD AILERON REPAIRED IAW SRM 51-70-07, FIG 5 AND REF HX PROCESS CARD, CONTROL SEQ NR: DJU 507013-1. SDR UIEA201000090Skin · delaminatedRT WING OTBD AFT FLAP L/E MID AREA FOUND DELAMINATED. RT WING - OTBD AFT FLAP REPAIRED IAW SRM 51-70-07 FIG 5 AND REF HX PROCESS CARD, CONTROL SEQ NR: DJU506866-1. EO 4457A224RA, 4457A225RA.SDR UIEA201000087Skin · delaminatedLT WING UPPER SURFACE OTBB AIL INBD AREA DELAMINATED AT SEVERAL LOCATIONS AS MARKED. RT WING - OTBD AILERON UPPER SURFACE REPAIRED IAW SRM 51-70-07, FIG 5 AND REF HX PROCESS CARD, CONTROL SEQ NT: DJU 504200-1, EO 4457A224RA AND 4457A225RA.SDR UIEA201000091Skin · dentedRT WING T/E OTBD AFT FLAP LWR SURFACE FOUND DENT AS MARKED. RT WING - OTBD AFT FLAP REPAIRED IAW SRM 51-70-10, REPAIR NR 4, FIG 201 AND REF HX PROCESS CARD, CONTROL SEQ NR: DJU505223. EO 4457A224RA, 4457A225RA.SDR UIEA201000095Skin · delaminatedRT WING T/E INBD FORE FLAP L/E FOUND DELAMINATION AS MARKED. RT WING - INBD FORE FLAP REPAIRED IAW SRM 51-70-07, FIG 5 AND REF HX PROCESS CARD, CONTROL SEQ NR: DJU 504747-1. EO 4457A224RA, 4457A225RA.SDR UIEA201000096Flap Track · erodedNR 7 FIX FLAP TRACK FAIRING L/E AREA ERODED. NR 7 FIX FAIRING RESIN REPAIRED IAW SRM 51-70-06, PARA 5.0, EO 4457A224RA, 4457A225RA.SDR UIEA201000093Skin · delaminatedEO 4457A224RA, 4457A225RA: RT WING INBD MID FLAP UPPER SURFACE 2 LOCATION FOUND DELAMINATED AS MARKED. RT WING INBD MID FLAP LWR SURFACE OTBD AFT CORNER SCRATCH AS MARKED. RT WING - INBD MID FLAP REPAIRED IAW SRM 51-70-07, FIG 5 AND REF HX PROCESS CARD, CONTSDR UIEA201000092Skin · delaminatedLT WING T/E OTBD FORE FLAP L/E FOUND DELAMINATION AT SEVERAL LOCATION AS MARKED. LT WING -OTBD FORE FLAP REPAIRED IAW SRM 51-70-07, FIG 5 AND REF HX PROCESS CARD, CONTROL SEQ MO: DJU 503665-1. EO 4457A224RA, 4457A225RA.SDR UIEA201000094Skin · delaminatedRT WING INBD AFT FLAP LWR SURFACE 1 LOCATION FOUND DELAMINATED AS MARKED. RT WING - INBD AFT FLAP REPAIRED IAW SRM 51-70-07, FIG 5 AND REF HX PROCESS CARD, CONTROL SEQ NR: DJU504176-1. EO 4457A224RA , 4457A225RA.SDR UIEA201000106Floorbeam · crackedM/DECK WEB CRACKED STA 380, RBL 80. M/D STA 380 RBL 80 FLOORBEAM CRACKED WEB TRIMMED OFF FROM RBL 77 TO RBL 88. HFEC INSPECTED, NO CRACK AFT TRIMMED OFF. FLOORBEAM WAS REPAIRED IAW SRM 53-00-51-2R-1 FIG 201 REPAIR 1. CATEGORY B. REF NON ROUTINE NR 50999.SDR UIEA201000100Floor Support · deformedBULK CARGO COMPT STA 1980 - 2000, RBL 50 FLOOR PANEL SUPPORT DEFORMED AS MARKED. BULK CARGO COMPT STA1980-2000 RBL50 FLOOR PANEL SUPPORT DEFORMED AREA TRIMMED OFF. HFEC INSPECTED, NO CRACK AFTER TRIMMED OFF. FLR SUPPORT REPAIRED IAW SRM 53-60-53-2R-1, FIG 2SDR UIEA201000101Floor Support · deformedBULK CARGO COMPT STA 2120-2130 LBL 30 FLOOR PANEL SUPPORT DEFORMED AS MARKED. BULK CARGO COMPT STA2120-2130 LBL30 FLOOR PANEL SUPPORT DEFORMED AREA TRIMMED OFF, HFEC INSPECTED, NO CRACK AFTER TRIMMED OFF FLR SUPPORT. REPAIRED IAW SRM 53-60-53-2R-1, FIG 201, RESDR UIEA201000104Floor Support · deformedBULK CARGO COMPT STA1980-2000 RBL46 FLOOR PANEL SUPPORT DEFORMED AREA TRIMMED OFF HFEC INSPECTED FREE OF CRACK. FLOOR SUPPORT REPAIRED IAW SRM 53-60-53-2R-1 FIG 201 REPAIR 1.SDR UIEA201000105Floor Support · deformedBULK CARGO COMPT STA 1950 -1970 BL0 FLOOR PANEL SUPPORT DEFORMED AS MARKED. BULK CARGO COMPT STA1950-1970 BL0 FLOOR PANEL SUPPORT DEFORMED AREA TRIMMED OFF, HFEC INSPECTED, NO CRACK AFTER TRIMMED OFF. FLR SUPPORT REPAIRED IAW SRM 53-60-53-2R-1, FIG 201, REPAISDR 2010FA0000019Valve · leakingDURING FUELING NOTED FUEL COMING FROM RT WING JETTISON TUBE. JETTISON VALVE LEAKING. FUELING STOPPED AND JETTISON NOZZLE CYCLED IAW MM TASK 28-31-00-715-068. LEAK STOPPED
SDR UIEA2009120800003Wedge · damagedTHE PURPOSE OF EO 4455A032 IS TO DOCUMENT A MAJOR REPAIR. WHILE PERFORMING A-CHECK INSP, MX REPORTED DAMAGED OF THE RT INBD HORIZ STAB ELEVATOR T/E MEASURING 2.750 IN LONG AND 3.0 IN INTO THE T/E WEDGE. (PERMANENT REPAIR ACCOMPLISHED IAW THE SRM 55-20-01 FIG 2SDR UIEA201000173Skin · delaminatedNR 4 RH T/R COWL WITH DELAMINATION DAMAGE TO THE OUTER SKIN FROM A PREVIOUS REPAIR, LOCATED AT APPROX 2:00 POSITION. DISPOSITION WAS MADE TO PERFORM A REPAIR BY FILLING THE DAMAGED AREA WITH BMS5-28 POTTING COMPOUND OR EQUIVALENT TO CONTOUR AND APPLY (2) LAYERSDR UIEA201000172Strip · missingTHE L/E STRIP ON THE NR 3 RT FAN COWL WAS FOUND WITH APPROX 20" MISSING. "DISPOSITION WAS TO APPLY 1 LAYER OF SPEED TAPE. DVI EVERY FLIGHT CYCLE AND REPLACEMENT OF THE FAN COWL AT THE NEXT "A" CHECK".SDR UIEA2009110300004Structure · damagedEO 4471A044, DURING THE A-CHECK INSP ON 11/3/2009, MX FOUND DAMAGE TO THE NR 2 ENG LT CORE COWL UPPER FWD CORNER. (DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS. SCHEDULE REPEAT INSPECTIONS AT EVERY A-CHECK AND
Back to GE CF6-80C2B1F