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 IPXA10M60183Longeron Splice · crackedINSPECTION TYPE:4C, CTR CARGO BILGE LONGERON SPLICE CRACKED AT L50L STA 5-113 TO 1541. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SPLICE REF DWG A5A7114 & SRM 51-31-01, 51-33-01.SDR FDEA201005061473Skin · misrepairedEXISTING REPAIR - LT WING DROOP L/E UPPER SKIN. EXISTING REPAIR AT LT WING DROOP L/E UPPER SKIN FOUND NOT IAW SRM REPAIR. REPAIR AT LT WING DROOP L/E UPPER SKIN CARRIED OUT REPAIR IAW EA 1-5750-138495: REPAIR CLASSIFIED AS MINOR AS GMM 6-2-100, REV 110.SDR IPXA10M60101Rib · crackedINSPECTION TYPE:4C, RT WING FIXED L/E COMPT APPROX STA XORS 917 HAS ONE CRACKED RIB. REMOVED FABRICATED AND INSTALLED REPLACEMENT RIB REF DAC DWG ARB2920 AND SRM 51-33-01.SDR FDEA201005051456Skin · crackedRT WING - STA XORS 683.400 TO XORS 713.600 LOWER SKIN ACCESS DOOR CUT OUT 01 EACH FASTENER HOLES FOUND CRACKED DURING HFEC OPEN HOLE INSPECTION. REPAIRED IAW EA NR 1-5710-137992, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.SDR FDEA201005051457Rib · crackedRT WING - SLAT ASSY NR 6, XOS 863 RIB FOUND CRACKED. AFTER REMOVAL OF EXISTING REPAIR DOUBLER. RT WING - SLAT ASSY NR 6 R & R IAW AMM 27-80-30-4, REV 64. SLAT ADJUSTMENT AND TEST CARRIED OUT IAW AMM 27-80-30-4 REV 64. FOUND SATISFACTORY.SDR FDEA201005051458Skin · damagedLEFT HAND WING - FUEL TANK ACCESS PANEL NR 536AB CUT-OUT, 01 EACH FASTENER HOLE FOUND DAMAGED. COMPLIED WITH EA NR 1-5710-125559 REV A, PART 2. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 110.SDR IPXA10M59922Skin · crackedINSPECTION TYPE:4C, CRACKS FOUND AS MARKED AT UPPER SKIN WEB LT WING OTBD L/E COMPT BETWEEN SLAT TRACK 11 & 12 STA. XOS 753-763. FABRICATED & INSTALLED REPAIR REF SRM 57-40-02, FIG 203, REPAIR 9.SDR IPXA10M59923Skin · crackedINSPECTION TYPE:4C CRACK FOUND AS MARKED AT UPPER SKIN WEB OF LT WING OB LE COMPT STA. XOS 643-648. FABRICATED & INSTALLED REPAIR REF SRM 57-40-02, FIG 203, REPAIR 9.SDR FDEA201005041431Skin · damagedEXISTING REPAIR - STA 960 TO STA 994 APPROX 30 INCH FROM LOWER OF FWD CARGO DOOR EXTERIOR. EXISTING REPAIR ON LOWER FWD CARGO DOOR EXTERNAL SKIN STA 960 TO STA 994. REMOVED AND ACCOMPLISHED IAW EA 1-5230-138490, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, RESDR FDEA201004301407Wedge · delaminatedLT WING-OTBD FLAP, T/E WEDGE, INBD UPPER SURFACE FOUND DELAMINATED. LT WING - OTBD FLAP T/E WEDGE REPAIRED IAW EA 1-5750-137979, REPAIR CLASSIFIED AS MINOR REPAIR IAW GMM 6-2-100 REV 110.SDR FDEA201004301408Rib · crackedLT WING - L/E PERFORMANCE FILLET OTBD EDGE FORMER FOUND CRACKED. LT WING - L/E PERFORMANCE FILLET OTBD EDGE CRACKED RIB STOP DRILLED AND REPAIR AS IAW SRM 57-40-71 FIG 201, REPAIR 1, REVISION 43. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.SDR WRLA20100426354Panel · gougedDESC - FOUND THE PANEL 657LT 1EA BOLT HOLE SINK INTO PANEL, AT RT OUTBOARD FLAP OUTBOARD SIDE. NRC U05112 ISSUED FOR IT. REMOVED THE DAMAGED PANEL, FABRICATE A NEW IAW EI: W2010P57B-954 REV 00. INSTALLED THE NEW PANEL COND CHECK SATISFACTORY.SDR WRLA20100426355Panel · gougedDESC - GOUGE - FOUND LT WING 517 CB PANEL SURFACE GOUGED. NRC U05002 ISSUED FOR IT. REMOVED THE DAMAGED PANEL, FABRICATE A NEW PANEL IAW EI: W2010P57B-941 REV 00, INSTALLED THE NEW PANEL, COND CHECK SATISFACTORY.SDR FDEA201004221280Bolt · shearedLT WING / SIDE LOAD FITTING AFT INBD BOLT FOUND SHEARED AT THE SPAR INSIDE THE TANK. (FOUND WHILE CLEANING TANK FOR CLOSE). REMOVED BOLT IAW 51-40-21 PARA 5. PERFORMED BHEC INSP OF THE BOLT HOLE IAW NTM 51-10-01. NO CRACKS NOTED. INSTALLED NEW BOLT PART SDR FDEA201004151193Cargo Track · brokenMAIN CABIN TIE DOWN TRACK SCALLOP IS BROKEN FROM FRAME 65 TO FRAME 65; RBL 48 TO RBL 48. REMOVED TIE DOWN ADAPTER IAW SRM 51-72-10. LOCATED AND DRILL HOLES IN NEW TIE DOWN ADAPTER PART NR A5327828821200, PO NR 679551.1 IAW SRM 51-72-10. INSTALLED NEW TIE DOSDR FDEA201004151197Wedge · crackedRT WING INBD FLAP TAIL AT RIB 25A IS CRACKED. FABRICATED AND BONDED NEW WEDGE SKIN; DOUBLER; SPAR BRACKET AND CORE OF END FLAP TAIL WEDGE PN 57960014 IAW EA 6-5750-136642 "WING - RT INBD FLAP T/E WEDGE AT RIB 25A"; DWG A57960014 AND TPS 1001 REV "E".SDR FDEA201004141183Strip · crackedHORIZONTAL L/E PANEL 331 DB JOINT STRIP IS CRACKED AT RIB 33A. REMOVED JOINT STRIP IAW SRM 51-40-21, PARA 5. MATERIAL ID 2024-T3, 0.071, PO NR 618569.1. FOR THE DOUBLER AND 2024-T3 0.063, PO NR 652264.1 FOR THE FILLER IAW SRM 55-12-28. FABBED REPAIR IAW SRM SDR DL76S100908Battery Pack · inoperativeAFT EXTERIOR EMERGENCY LIGHTING ON RT AND LT SIDE OF FUSELAGE IS INOPERATIVE. MX REPLACED THE BATTERY PACK UNIT AND RE-LAMPED THE EXTERIOR LIGHTS. SYS OPERATION IS NOW NORMAL.SDR FDEA201004101129Skin · crackedLT WING - STA XORS 690 TO XORS 700 LOWER SKIN ACCESS DOOR CUT OUT 08 EACH FASTENER HOLES FOUND CRACKED DURING HFEC OPEN HOLE INSPECTION. LT WING - STA XORS 690 TO XORS 700 LOWER SKIN ACCESS DOOR CUT OUT 08 EACH. FASTENER HOLES REPAIRED IAW EA NR 1-5710-13SDR WRLA20100408352Skin · dentedMAIN CARGO DOOR CUTOUT DENTED BEYOND LIMITS AT LOWER FORWARD CORNER. CORRECTIVE ACTION SRM 53-00-15 REPAIR 8 FIG 203.SDR FDEA201004061060Frame · damagedDURING ACCOMPLISHMENT OF EO1-2620-7-5005 B PT1 STEP B2 DWG VA-FSS-26-2101 ARGON TANK INSTALLATION AT STA1461 L-1L TO L-2L AND L-3L TO L-4L FRAME DOUBLER PN VA-FSS-6158 AND VA-FSS-6159 WILL HAVE SHORT EDGE MARGIN WITH EXISTING PILOT HOLES ON NEW HANGAR PN VA-FSSDR HALA2010040500152Engine · malfunctionedETOPS SIGNIFICANT SYS - ACFT DIVERTED - APU FAULT LIGHT IN FLIGHT WITH APU SHUTDOWN. BITE CK FAULT MSG LOW OIL PRESS. R & R THE APU IAW HAL M266-767. OPS CHECK NORMAL,OK FOR SERVICE.SDR FDEA201004051056Seat Track · corrodedSEAT TRACK CORRODED ON THE FLANGE FROM FRAME 50 TO FRAME 51; RBL 26. REMOVED CORROSION IAW SRM 53-10-16, PG 101. MATERIAL LOSS 0.010. MATERIAL REMAINING 0.080 FOUND TO BE WITHIN LIMITS IAW SRM 53-10-16. ALODINED AND PRIMED IAW SRM 51-21-10. CORROSION ISDR FDEA201003311041Floorbeam · crackedFWD CARGO FRAME 30 UPPER FLOORBEAM BETWEEN S/T 2R AND 3R IS CRACKED ON FWD SIDE. PERFORMED CROSSBEAM REPAIR AT FWD FACE OF FLOORBEAM FRAME 30 BETWEEN SEAT TRACK 2R AND 3R BY REMOVING DAMAGE, FABRICATING, LOCATING AND DRILLING A FILLER AND REPAIR CHANNEL AND INSDR FDEA201003250989Seat Track · wornSEAT TRACK 3L HAS (2 EA) BROKEN SCALLOPS LOCATED 2 IN AFT OF FRAME 59, REMOVED DAMAGED SEAT TRACK. FABRICATED NEW SEAT TRACK AND SPLICE. REPROTECTED ALL PARTS IAW A300 FREIGHTER SRM 53-10-16 FIG 201.SDR FDEA201003250990Floorbeam · crackedFWD CARGO FR 31 UPPER FLOORBEAM BETWEEN 2R AND 3R CRACKED ON FWD SIDE CHEM MILL. ROUTED OUT CRACK, INSTALLED FILLER CHANNEL, APPLIED PROTECTIVE COATING IAW SRM 53-10-15, FIG 212.SDR WRLA20100316348Strut · damagedDUE TO HARD LANDING, INSP A PERFORMED AND FOUND CENTER LANDING GEAR STRUT DAMAGED. CENTER LANDING GEAR AND ADDITION BRAKES AND WHEELS REPLACED.SDR WRLA20100316349Vane · damagedDUE TO HARD LANDING, INSP A PERFORMED AND FOUND LT WING INBOARD FLAP-VANE AFT RT EDGE DAMAGED. DAMAGED SECTION TRIMMED OUT IAW BOEING APPROVAL REF SRE-WLD-10-0001-02B.SDR WRLA20100316350Bracket · damagedDURING HARD LANDING INSP FOUND DAMAGE/DENT IN FLAP TRACK BRACKET. PER BOEING REPAIR REF 57-ED-269679, SRE-WLD-10-0001-02B THE BRACKET IS STRUCTURALLY ACCEPTABLE FOR CONT IN SERVICE WITH HFEC INSP EVERY C-CHECK NOT TO EXCEED 24MONTHS.SDR WRLA20100315347Mount Fitting · corrodedENGINE PYLON FWD MOUNT TRUSS FITTING HAS CORROSION IN 2 AFT BOLT HOLES. REWORKED REPAIR IAW SERVICE GENERAL REPAIR DRAWING SG11540000.SDR WRLA20100307346Brake · fireA/C ARRIVED AT GATE WITH NR 5 BRAKE ON FIRE. REPLACED WHEEL AND BRAKE ASSY. PERFORMED AXLE INSP, FOUND NO DISCREPANCY.SDR IPXA10M58532Hmu · failedATB - CLIMBING THROUGH 2500 FT ENGINE FAIL LIGHT W/20 PERCENT RPM DROP ON NR 2 ENGINE. R&R NR 2 ENGINE HMU PER M/M 73-21-01-4. OPS CKS & LEAK CHECK GOOD.SDR CLCA02092010.1Warning System · activatedAFTER TAKEOFF (SBKP) LEVEL 2 DEFLECT AILERON DISAGREEMENT WARNING APPEARED ON EAD. PERFORMED CHECKLIST, WARNING REMAINED, RETURNED TO AIRPORT (SBKP). ENTERED ON DEFERRED MAINTENANCE ITEM (DMI) PER MEL 27-13-2, CAT "C", PLACARD INSTALLED, AIRCRAFT RELEASE BACSDR UIEA201000159Access Panel · crackedCRACKS WERE FOUND IN THE NR 3 PYLON INBD ACCESS PANEL 472FL AS SHOWN IN FIGURE 1. NR 3 PYLON ACCESS PANEL 452FL CRACKED AREA REPAIRED IAW EO 4454A095.SDR 2010F00023Control Cable · icedON ARRIVAL, CREW REPORTED STAB TRIM NO MOVEMENT IN NORM OR ALT MODES. ON INVESTIGATION STAB BAY FOUND TO HAVE ICE FORMATION APPROX 10 INCHES DEEP IN BILGE AREA. ICE FORMATION HAD PREVENTED POSITION MODULES AND FOLLOW UP CABLES FROM MOVING. THIS RESULTED IN CASDR CLCA01282010.1Warning System · activatedAFTER TAKEOFF (SBKP) EAD INDICATES LEVEL 2 AILERON DEFLECT DISAGREE. PERFORMED QRH CHECKLIST AND INDICATION STILL PRESENT. RETURNED TO AIRPORT. ENTERED ON DEFERRED MAINTENANCE ITEM (DMI) PER MEL 27-13-2, CAT "C", PLACARD INSTALLED, AIRCRAFT RELEASE BACK TO SDR FDEA201001140125Skin · cracked13 EA FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS = 690 AND STA XORS = 700. REPAIR CARRIED OUT IAW EA NR 1-5710-137538. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100 REVISION 109.SDR FDEA201001140126Skin · cracked14 EACH FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSP AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS = 690 AND STA XORS = 700. REPAIR CARRIED OUT IAW EA NR 1-5710-137539. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REVISION 109.SDR FDEA201001140128Skin · crackedRT WING LOWER SKIN SURFACE IS CRACKED AT ACCESS PANEL 613 AB. REMOVED ACCESS PANEL ADJACENT TO THE REPAIR ON THE FWD SPAR IAW SRM 51-40-02, PARA 5. FABRICATED -1 AND -3 REPAIR DOUBLERS IAW SRM 53-15-63, FIG 201. ALODINED REPAIR IAW SRM 51-21-10, PARA 2-B(C)SDR FDEA201001130112Hinge Bracket · corrodedCORROSION - ACTUATOR INBD HOLE AT RT WING OTBD FLAP INBD FWD HINGE (WING SIDE). REPAIR CARRIED OUT IAW EA NR 1-5750-137535. THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 109.SDR FDEA201001130115Hinge Bracket · corrodedCORROSION - PIVOT HOLE AT RT WING OTBD FLAP INBD FWD HINGE (WING SIDE). REPAIR CARRIED OUT IAW EA NR1-5750-137535. THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 109.SDR FDEA201001130117Hinge Bracket · corrodedCORROSION - PIVOT INBD HOLE AT LT WING INBD FLAP OTBD AFT HINGE (FLAP SIDE). REPAIR CARRIED OUT IAW EA NR 1-5750-137532. THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 109.SDR FDEA201001130118Hinge Bracket · wornWORN - BARREL NUT NR10 HOLE BUSHING AT LT WING OTBD FLAP OTBD FWD HINGE (WING SIDE). REPAIR CARRIED OUT IAW EA NR 1-5750-137531. THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 109.SDR FDEA201001130119Hinge Bracket · corrodedCORROSION - ACTUATOR OTBD HOLE AT LT WING OTBD FLAP INBD FWD HINGE (WING SIDE). REPAIR CARRIED OUT IAW EA NR 1-5750-137534. THIS REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 109.SDR FDEA201001130120Hinge Bracket · corrodedCORROSION - ACTUATOR INBD HOLE AT LT WING OTBD FLAP INBD FWD HINGE (WING SIDE). REPAIR CARRIED OUT IAW EA NR 1-5750-137534. THIS REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 109.SDR FDEA201001130121Hinge Bracket · corrodedCORROSION - LOWER MOUNT INBD HOLE AT LT WING OTBD FLAP INBD FWD HINGE (WING SIDE). REPAIR CARRIED OUT IAW EA NR 1-5750-137534. THIS REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 109.SDR FDEA201001130122Hinge Bracket · corrodedCORROSION - BARREL NUT HOLE SURFACE AT LT WING OTBD FLAP INBD FWD HINGE (WING SIDE). REPAIR CARRIED OUT IAW EA NR 1-5750-137534. THIS REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 109.SDR FDEA201001130123Hinge Bracket · corrodedCORROSION - PIVOT HOLE AT LT WING OTBD FLAP INBD FWD HINGE (WING SIDE). REPAIR CARRIED OUT IAW EA NR 1-5750-137534. THIS REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 109.SDR DL764092040Idg · failedRTB DUE TO LT IDG FAILED MIP. REMOVED AND REPLACED NR 1 IDG IAW AMM OPS AND LEAK CHECK OKC/W ETOPS PDC. CATEGORY 'E': PROBLEMS WITH SYS CRITICAL TO ETOPS.SDR HALA2009122400601Sensor · malfunctionedETOPS SIGNIFICANT SYS - CLIMB POWER UNATTAINABLE ON LT ENG WITH THRUST LEVEL FULL FWD BTW FL 340 & 360, 2 1/2 KNOB DIFFERENCE. MAX NI 106.0. LT ENG: 103.4 NI, 773 EGT, 99.2 N2, 7.3 FF. RT ENG: 106.0 N1, 790 EGT, 99.9 N2, 7.7 FF. ACCOMPLISHED FIM73-21-00 FIG11
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