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 IPXA10661037Skin · misrepairedRT WING INBD AILERON EXISTING REPAIR PATCH NOT IAW SRM 57-60-01-2R1, TABLE 3 NOTE G. COMPOSITE WET LAY UP REPAIR CARRIED OUT AT EXISTING REPAIR PATCH AREA EO B767-5750-38681 AND RS R57-60-36772.SDR IPXA10660867Fitting · crackedINSPECTION TYPE:C, LT WING INBD MAIN FLAP INBD HINGE ARM FLANGE AREA FOUND CRACKED. LT WING INBD MAIN FLAP HINGE FTG AT IFS179.75 REPAIRED IAW SRM 57-53-02- 2R1, FIG201, ORG MATL IS 7075T73 FORGING, CRK LENGTH AT INBD FLANGE IS 1.5" & OTBD FLANGE IS 1.25", DASDR P5CA2010062101642Structure · damagedNR 4 ENGINE & NBSP; RIGHT CORE COWL DAMAGED DURING MAINTENANCE BY STAND. ACCOMPLISHED TIME LIMITED REPAIR PER ENGINEERING ORDER 4471A058, WITH FAA 8110-3 DATED 15 JUN 2010. DVI EVERY 2 FLIGHT CYCLES WITH PERMANENT REPAIR PRIOR TO 25 FLIGHT CYCLES.SDR IPXA0660660Skin · damagedRT OTBD AILERON HAS 4 OTHER AREAS OF LIGHTNING STRIKE DAMAGE ON UPPER SURFACE OF WEDGE MARKED. STARTED SANDING AREA, FWD LIMITS TO ENGR. FINISHED DAMAGE REMOVAL REF SRM 57-60-02-2R. STARTED NR 346819. REPAIR COMPLETE SEE NRC 346819 AND ECA 020462. THIS REPAISDR FDEA201006212097Skin · dentedLT WING - INBD LOWER SURFACE FOUND DENTS AT XIFH 146. LT WING INBD FLAP LOWER SKIN AND FILLER FABRICATED IAW SRM 57-50-01, FIG 201, REV 43. SKIN AND FILLER INSTALLED IAW SRM 51-35-01, REV 43. THIS REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.SDR FDEA201006192065Seat Track · corrodedCABIN SEAT TRACK 4L FROM FR 50 TO FR51 HAS APPROX. 8 SQ IN OF CORROSION. REMOVED CORROSION IAW SRM 51-74-10 P205. CHECKED FOUND OUT OF LIMITS IAW SRM 53-10-16 FIG 201. REPAIRED SEAT TRACK 4L IAW SRM 53-10-16, FIG 203.SDR FDEA201006192079Stringer · corrodedAFT CARGO COMPT HAS CORROSION AT STRINGER 31 RT FROM FRAME 54.1 TO FRAME 54.1, 12 IN TOTAL AREA APPROX 13 SQ IN. REMOVE CORROSION IAW SRM 51-74-10, CHECK FOUND OUT OF LIMIT IAW WITH SRM 53-10-00, PG 106. REPAIRED STRINGER 31RT IAW SRM 53-10-14.SDR FDEA201006182049Skin · crackedCRACK LINE-LT WING L/E ANTI ICE TELESCOPIC DUCT CUTOUT UPPER INBD CORNER EDGE. REPAIRED IAW SRM 57-40-01 REV 43, FIG 201. LT WING NR 3 SLAT ADJUSTMENT AND TEST CARRIED OUT IAW AMM 27-80-30-5, REV 66. FOUND SATISFACTORY. THIS REPAIR CLASSIFIED AS MINOR IAW SDR IPXA0660636Pneumatic System · inoperativeINSPECTION TYPE:ETOP, APU PNEUMATIC INOP; REF 427849 AND WAN NR 1631215. T/S IAW FIM 49-11-00 AND ECU TEST PASS IAW AMM 49-11-00-5, ITEM CLOSED. BOW COMPLETED.SDR WRLA20100618396Vane · brokenINBOARD FLAP VANE TRAILING EDGE BROKEN OF LT WING. THIS NRC HAS BEEN COVERED BY ERA: DOCUMENT NUMBER 10-57-029 REVISION 1. CONDITION CHECK NORMAL AND JOB COMPLETED.SDR WRLA20100617397Skin · corrodedEXFOLIATION CORROSION ON CUTOUT SKIN EDGE OF LAVATORY SERVICE ACCESS DOOR STA: Y=410.5, X=2 TO X=-5. REPAIR SKIN IAW EGAT EI W2010A53B-1328 REV 00 AND REV 01. CONDITION CHECK NORMAL AND JOB COMPLETED.SDR WRLA20100617398Longeron · corrodedCORROSION ON LONGERON 52 OF FWD CARGO COMPARTMENT STA: Y=939. REPAIR CORROSION AREA IAW SRM 53-00-05 REPAIR TYPE 1 OF FIG 201 AND FIG 202. CONDITION CHECK NORMAL AND JOB COMPLETED.SDR FDEA201006162021Seat Track · corrodedSURFACE CORROSION - SEAT TRACK STA 1069 X=-8 IN MAIN DECK CARGO. REPAIRED IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 43. THIS REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.SDR FDEA201006141984Frame · damagedUPPER FUSELAGE FRAME 34R FROM STR 13R TO 22R HAS NUMEROUS SMALL GOUGES AND BARE METAL APPROX 4 SQ IN THROUGHOUT ENTIRE FRAME ON INSIDE OF ACFT DEEPEST OF THE GOUGES IS APPROX .005" BLENDED OUT GOUGES ON FRAME 34R BETWEEN STR 13R TO 22R CHECK LIMITS FOUND OUT OSDR WRLA20100614384Longeron · corrodedLONGERON 46R CORROSION STA Y=6-90--6-96 OF CENTER ACCESSORY COMPARTMENT. REPAIRED LONGERON IAW EI W2010A53B-1330 REV 00,01. CONDITION CHECK NORMAL AND JOB COMPLETED.SDR WRLA20100614385Seat Track · corrodedCORROSION ON MAIN DECK SEAT TRACK STA:Y=6-50, X=-6 . REPAIRED SEAT TRACK IAW SRM 53-00-52 REPAIR 1 FIG 201 REV 43. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR WRLA20100614386Longeron · corrodedLONGERON 46R CORROSION OF CENTER CARGO LOWER SIDE AT STA 1721. ACCOMPLISH EI NO W2010A53B-1348 REV 00, 01, 02, 03, 04, COND CHECK SATISFACTORY.SDR FDEA201006101942Bearing · damagedNR 2 RUDDER HINGE ARM ON VERTICAL STAB END HAS 2 EA BAD BEARING. R & R 2 EA BEARINGS ON NR 2 RUDDER HINGE ARM IAW E.A.6-5540-135192.SDR WRLA20100610373Doubler · crackedCRACK ABOUT 2 INCHES ON CENTER L/G WHEEL WELL LT FORWARD OUTBOARD SIDE DOUBLER STA:Y=1384, X=31.5 (NRC:U05086). REPAIR THE DOUBLER OF STIFFENER AT CENTER GEAR WHEEL WELL LEFT KEEL WEB IAW EGAT EI: W2010A53B-1295. CONDITION CHECK NORMAL AND JOB COMPLETED.SDR IPXA10660600Wedge · crackedINSPECTION TYPE:C, LT WING OTBD T/E FLAP T/E WEDGE INBD AREA LWR SURFACE CRACKED. FIBERGLASS PREPREG LAYUP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5G, FIG 14, REV 47.SDR IPXA10660604Fairing · delaminatedINSPECTION TYPE:C, RT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATION FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05 PAR 5A (1) FIG 5 REV 47.SDR UIEA2010060800029Panel · brokenDURING A2-CHECK INSP, MX FOUND THE RT WBL 515 - OTBD MID FLAP L/E & AMP; RT WING FIXED T/E WITH CRACK/DAMAGE. WBL 515 - L/E OF RT OTBD MID FLAP BROKEN . THE DIMENSION IS 0.787 & .787 ) WBL 515 RT WING FIXED T/E FAIRING PANEL BROKEN AT WBL 515.. (1)PERMANENT RSDR WRLA20100608361Support Fitting · crackedCRACK - LT NLG SUPPORT FITTING CRACK 1 INCH AND RT NLG SUPPORT FITTING CRACK 0.75 INCH STA Y:595.SDR IPXA10660601Wedge · delaminatedINSPECTION TYPE:C, LT WING OTBD FLAP T/E LWR SURFACE AT 127" FROM OTBD EDGE DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A (1) FIG 9, REV 47.SDR IPXA10660606Wedge · delaminatedINSPECTION TYPE:C, LT WING OTBD FLAP T/E LWR SURFACE AT 54.5" FROM OTBD EDGE. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A (1) FIG 9, REV 47.SDR P5CA2010060801640Structure · damagedNUMBER 4 ENGINE LT & RT CORE COWLS DAMAGED AT FORWARD EDGE AT 6 O'CLOCK POSITION. TIME LIMITED REPAIR PART ONE ACCOMPLISHED PER ENGINEERING ORDER 4471A057, WITH FAA 8110-3 DATED 08 JUN 2010. DVI EVERY 15 FLIGHT CYCLES AND PERMANENT REPAIR PRIOR TO 50 FLIGHT CSDR IPXA10660605Skin · crackedINSPECTION TYPE:C, LT WING NR 4 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 4 SLAT L/B OTBD NOSE SKIN AT OSS641.9 AREA SKIN REPAIRED IAW SRM 57-43-01-22R FIG 201, ORG MATL IS CLAD7075T6-0.063IN, CRK LENGTH 0.244", DAMAGED CUTOUT IS 8.875" X 7.25"SDR FDEA201006061845Seat Track · corrodedSEAT TRACK 4 R BETWEEN FRAMES 74 AND 80/82 HAS 5 EA AREAS OF COROSION, DEFECTS MEASURE 5 SQ IN REMOVED COROSION IAW SRM 51-74-10, PAGE 5. CHECKED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, FIG 101. CUT OUT DAMAGED SECTION AND REPAIRED IAW SRM 53-10-16SDR UIEA2010060600026Floorboard · damagedDURING LOADING OUT PALLET CAUSED DAMAGE TO ROLLER CASTER TRAYS AND FLOORBOARD ON MAIN DECK LT SIDE & NBSP; STA 1600 & NBSP; & AMP; 1700 BETWEEN 18L AND 16L & NBSP; (IAW DDPG 25-53-01 CAT D ITEM TRANSFERRED TO MDDR 17366. ITEM EXPIRES 5 SEP 10. DAMAGED CASTER TSDR FDEA201006051843Stringer · corrodedBULK CARGO 4 IN AFT OF FR 65 ON STR 53 LT HAS AREA OF CORROSION,1 SQ INCH. REMOVED LEVEL 1 CORROSION. REMOVED DAMAGED STR SECTION AND INSTALLED STR REPAIR ON STR 53 LT BETWEEN FR 65 AND FR 66 IAW SRM 53-10-14, FIG 201.SDR UIEA2010060300024Skin · tornLT WING INBD T/E MID FLAP INBD FUSELAGE SEAL UPPER SURFACE TORN. REQUIRES REPLACEMENT. (EO 4457A263/ NON MEL MDDR 17280 RAISED FOR LW T/E INBD MID FLAP TEMP REPAIR PER PT 1 OF EO AND REPEAT INSP IAW PT 2 WITH PERM REPAIR TO BE CARRIED OUT AT THE NEXT A CHECKSDR UIEA2010060300025Actuator · leakingEO; 4455A041 IS TO DOCUMENT A MAJOR REPAIR. DURING REPLACEMENT OF UPPER RUDDER PCA (FOR LEAK), HIGH-LIFT CONTACTED RUDDER CAUSING DAMAGE TO RUDDER COMPOSITE STRUCTURE (REF FIGURE 1), MEASURING 12.0 IN. X 15.0 IN. DAMAGE IS BEYOND THE SRM LIMITS IAW THE SRM 55-SDR FDEA201005311743Stringer · corrodedFUSELAGE INTERNAL STRUCTURE ZONE 170, STR 44 R HAS SURFACE CORROSION BETWEEN FR 78-79, APPROX 4.50" X 1.75". REMOVED CORROSION IAW SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAM SRM 53-10-00 TABLE 102. REPAIRED STR 44R BETWEEN FR 78-79, IAW SRM 53-10-14, FIG 20SDR FDEA201005291708Floorbeam · corrodedAFT CARGO COMPT FLOORBEAM FR 66,28'' TO 44'' LT OF CTR LINE FWD FLANGE LWR HAS CORROSION IN AND AROUND FASTENER HOLES APROX 8 SQ IN. REMOVED CORROSION IAW SRM 51-74-10 CHECK AND FOUND FLOORBEAM AT FR 66 OUT OF LIMIT IAW SRM 53-10-00, TABLE 102. REPLACED BEAMSDR FDEA201005291709Seat Track · corrodedCABIN SEAT TRACK 3R FROM FRAME 46-54 HAS NUMOUROUS AREAS OF MODERATE TO SEVERE CORROSION AND AREAS OF BARE METAL APROX 125 SQ IN. REMOVED CORROSION IAW SRM 51-74-10 CHECK SEAT TRACK 3R LIMITS FOUND OUT OF LIMITS IAW SRM 53-10-16, FG 101. R & R SEAT TRACK 3R BSDR FDEA201005291711Skin Panel · crackedHFEC OPEN HOLE INSP. CARRIED OUT AND FOUND 02EA HOLES W/ CRACK INDICATION RT WING LWR SKIN PANEL OUTER WING ACCESS CUTOUT BTW XORS=683.4 AND XORS=713.6 AS MARKED. QTY 02 EA CRACK FASTENER HOLES ON RT WING LWR SKIN PNL FUEL TANK ACCESS DOOR CUTOUT 636AB BTW STSDR FDEA201005291730Frame · damagedCOMPLY WITH T CARD REPAIR IAW EA T 6-5310-113006 PART 2,WRI 53102241. ACCOMPLISHED REPAIR ON FUSELAGE FRAME 46 IAW EA 6-5310-113006C PART 2 - FUSELAGE - AD2009-18-16 - EO 6-5310-7-5020. FRAMES 44 TO 46 FOOT FITTINGS CRACKS -REPAIR.SDR FDEA201005281701Bearing · wornNR 2 RUDDER HINGE ARM ON VERT STAB END, 2 EA BRGS WITH SIDEPLAY. R & R 2 EA BRGS ON NR 2 RUDDER HINGE ARM IAW EA 6-5540-135192, RELEASE DATE MAY 06,2010.SDR FDEA201005281705Skin Panel · crackedHPEC OPEN HOLE INSP. CARRIED OUT AND FOUND 01 HOLE WITH CRACK INDICATION ON LT WING LWR SKIN PANELS, OUTER WING ACCESS DOOR BTW XORS=683.4 AND XORS=713.6 AS MARKED. QTY 01 EA CRACK FASTENER HOLE ON LT WING LOWER PNL FUEL TANK ACCESS DOOR CUTOUT 536AB BTW STA SDR FDEA201005271688Stiffener · crackedLWR FWD CARGO CEILING AREA FRAME 38 FLOOR BEAM, FWD SIDE 67" LT OF CTRLINE THE VERTICAL STIFFENER IS CRACKED AT THE TOP (CRACK LENGTH APPROX. .3750 IN. LONG) SMOOTH AND BLENDED CRACKED AREA IAW SRM 51-73-10. NDT CHECKED AND FOUND NO CRACKS. FABRICATED RSDR FDEA201005271689Stiffener · crackedLWR FWD CARGO CEILING FRAME 25 FLOORBEAM FWD SIDE 27" RT OF CTRLINE THE VERTICAL STIFFENER IS CRACKED AT THE TOP (APPROX. LENGTH IS 1/4IN) BLENDED CRACK AT FRME 25 IAW SRM 51-73-10. NDT VERIFIED REMOVAL OF CRACK. FABRICATED REPAIR ANGLE AND REPAIRED CROSSBEASDR CALA2010060100230Floor Support · corrodedMULT-25-3-0042 CABIN - BETWEEN LT STA 303 AND 325 LBL 25 FLOOR SUPPORT UPPER SURFACE FOUND CORROSION. FORM 44.0008 ATT FLOOR SUPPORT BETWEEN BS 303 & AMP; BS 325 LBL 25" REPLACED IAW SRM 51-10-02, FORM 44.0008 ITEMS 1-2 ACCOMPLISHED.SDR IPXA10660384Bracket · crackedINSPECTION TYPE:C RT WING L/E LES 675 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR BRACKET FOUND CRACKED. RT WING L/E LES 675 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR CLIP REPLACED AND INSTALLED IAW SRM 57-10-02 AND 51-40-02 REV 47.SDR FDEA201005251629Seat Track · corrodedSEAT TRACK 3L, BETWEEN FRAMES 14C & 15B, HAS 2 SQ. INCHES WITH EXFOLIATION CORROSION CHECKED MATERIAL LOSS IAW SRM 53-10-16 FIG 101 AND FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK IAW SRM 53-10-16.SDR FDEA201005251630Seat Track · corrodedMDCC, SEAT TRACK 3R, HAS 3 SQ. INCHES OF CORROSION AT FR 15B REMOVED CORROSION IAW A310 SRM 51-74-10. CHECKED LIMITS , FOUND OUT OF LIMITS IAW SRM 53-10-16 FIG 101. R & R SEAT TRACK 3R BETWEEN FR 15A TO FR 19 IAW SRM 53-10-16 AND SRM 51-72-10.SDR WRLA20100518357Longeron · corrodedCORROSION - DURING C01 CHECK, FOUND LONGERON CORROSION AT STA 6-90 L-47L, NRC U05051 ISSUED. REPAIRED THE CORROSION AREA AT STA 6-90 L47L IAW MD-11 SRM 53-00-05 REPAIR 1 FIGURE 202 REV 43, COND SATISFACTORY.SDR DL76G101309Lamp · inoperativeEMERGENCY PATH LIGHTING AT 22AB IS INOP. MX REPAIRED WIRE AT SEAT PLUG AND RE-LAMPED IT. SYS OPS IS NOW NORMAL.SDR FDEA201005171561Hinge · corrodedEXISTING REPAIR AT LT WING OTBD FLAP INBD HINGE LOWER PIVOT BORE HOLES. EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED IAW EA 1-5750-67544 TITLE: WINGS- OTBD T/E FLAPS- LT FLAP - REPAIR OF INBD AND OTBD HINGE. EO 1-5100-7-5001, A4 PART I TITLE: REPAIR CATALOGSDR 2010FA0000606Flap System · separated((F8ER)) ON APPROACH, THE RT INBD, FORE FLAP, OTBD SECTION SEPARATED FROM THE ACFT, STRIKING THE RT SIDE OF FUSELAGE AND PUNCTURING SEVERAL AREAS OF EXTERIOR SKIN CAUSING DAMAGE TO SEVERAL FUSELAGE FRAMES AND STRINGERS IN FUSELAGE SECTIOON 46 WITH DAMAGE BEINGSDR FDEA201005151543Seat Track · corrodedUPPER DECK SEAT TRACK 5R HAS CORROSION ON UPPER SURFACE BOTH FLANGES AND INSIDE SCALLOPS (APPROX 10 SQ IN TOTAL) FROM FRAME 18 TO FRAME 19. R & R SEAT TRACK 5R FROM FRAME 18 TO FRAME 19 IAW SRM 51-72-10. ALSO IAW SRM 53-12-16 PAGE 4G/4H.
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