GE CF6-80 series

Service difficulty reports · 1,092

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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"

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SDR FDEA201009233693Frame · damagedFRAME 72 HAS 0.25 INCH PUNCTURE ON OUTER FLANGE AT STRG 55L REPAIRED FR 72 AT STR 55L IAW SRM 53-10-13, FIG 101.Sep 23, 2010 · N445FE · Airbus A310203 · Fuselage Main, StructureSDR FDEA201009233694Seat Track · wornMAIN CARGO DECK SEAT TRACK NR 1 FRAME 61 HAS ONE EACH SCALLOP ON SEAT TRACK OUT OF ROUND MEASURES .8750 INCH. REPAIRED SEAT TRACK NR1 IAW SRM 53-10-16 BY REPLACING DAMAGED SECTION OF SEAT TRACK FROM FR 58 TO FR 61.9.Sep 23, 2010 · N445FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2010092300164Cdu · malfunctionedDURING TAKEOFF ROLL CAPT CDU BLANKED , THUS THE CAPTAIN LOSSING T/O SPEEDS(MX SWAPPED LT CDU TO CTR POSITION, LT IRU TO CTR AND SWAPPED LT FMC TO RT AND DEFERRED THE CTR CDU, CTR IRU AND THE RT FMC. ALL SYS OPS NORMAL.Sep 23, 2010 · N409MC · Boeing 74747UF · Attitude Gyro and Indicating SystemSDR IPXA10662787Skin · damagedON ARRIVAL FOUND DAMAGE TO OTBD FLAP L/E SKIN PANEL 666FT, 3.5"X0.75" LOCATED 1.5" FROM L/E OF PANEL AND 1.5" FROM OTBD EDGE OF PANEL. REPAIRED IAW SRM 57-53-01-2R FIG 201 AND SRM 51-70-03.Sep 23, 2010 · N324UP · Boeing 76734AF · Trailing Edge FlapsSDR UIEA2010092200162Cowling · damagedTHE PURPOSE OF THIS EO IS TO DOCUMENT A MAJOR REPAIR. DURING WALK-AROUND INSP, MX FOUND THE NR1 LT T/R TRANSLATING COWL WITH DELAMINATION DAMAGE TO THE OUTER SKIN, MEASURING 5.0 IN. X 2.0 IN LOCATED APPROX AT 10 O'CLOCK POSITION (REF FIG 1) AND A CRACK MEASURISep 22, 2010 · N493MC · Boeing 74747UF · Engine Thrust ReverserSDR DALA1023891816Acm · seizedSULFUR TYPE SMELL THROUGHOUT CABIN AND FLIGHT DECK, SMOKE, HAZE OBSERVED BY F/A ON LANDING AN EICAS MESSAGE ABOUT THE LT ACM SHOWED UP. MX FOUND THE LT ACM SEIZED.Sep 22, 2010 · N840MH · Boeing 767432ER · Cabin Cooling SystemSDR UIEA201000230Nozzle · crackedEO 4478A138: DURING MX WALKAROUND, MX FOUND 1EA CRACK ON THE NR2 ENGINE EXHAUST NOZZLE OUTER SLEEVE, AT APPROX THE 9 O'CLOCK POSITION. THE CIRCUMFERENTIAL CRACK IS APPROX 4.5 IN LONG. IAW SRM 54-41-30 THE LENGTH OF THE CRACK IS OUT OF LIMITS. DISPOSITION IS TOSep 20, 2010 · N493MC · Boeing 74747UF · Engine Collector/Tailpipe/NozzleSDR FDEA201009203566Idg · crackedON TAXI OUT MEM LEVEL NR 2 "GEN DRIVE 2 FAULT " WARNING DISCONNECT IDG NR 2 CDG U IN WORK. REMOVED AND REPLACED ENGINE NR 2 IDG.Sep 20, 2010 · N606FE · Doug MD11F · AC Generator-AlternatorSDR FDEA201009203588Stringer · corrodedAVIONICS COMPT. - STRINGER 44L, FOUND CORRODED AT FR16A-18 BLENDED OUT CORROSION IAW SRM 51-74-10. REMAINING THINKNESS IS 0.110" IAW NTM 51-10-04. NO CRACK FOUND IAW NTM 51-10-18 AND NTM 51-10-08 WITHIN ALLOWABLE DAMAGE LIMIT IAW EA6-5310-141616 RESTOREDSep 20, 2010 · N410FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201009203589Frame · corrodedAVIONICS COMPT- FRAME 17, STRINGER 45L-44L FRAME LOWER FLANGE FOUND CORROSION BLENDED OUT, CORROSION IAW SRM 51-74-10. REMAINING THINKNESS IS 0.195" IAW NTM 51-10-04 NO CRACK FOUND IAW NTM 51-10-18 AND NTM 51-10-08 WITHIN ALLOWABLE DAMAGE LIMIT IAW EA 6-531Sep 20, 2010 · N410FE · Airbus A310203 · Fuselage Main, FrameSDR FDEA201009203568Floorboard · damagedFWD CARGO COMPARTMENT FLOORBOARD 131NG HAS EDGE DAMAGE, BOTTOM SKIN DAMAGE AND CORE DAMAGE IN MULTIPLE PLACES. FABRICATED NEW FLOOR PANEL 131NG IAW DWG SRZ 25-005, REV "H".Sep 20, 2010 · N672FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201009203569Floorboard · damagedFWD CARGO FLOORBOARD 132 RG HAS ONE CORNER BROKEN. FABRICATED NEW FLOORBOARD 132 RG IAW DWG SRZ 25-005, REV "H".Sep 20, 2010 · N672FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201009203570Floorboard · damagedFWD CARGO COMPARTMENT FLOORBOARD 131 MG HAS BOTTOM SKIN DAMAGE AT MULTIPLE PLACES. FABRICATED NEW FLOORBOARD IAW DWG SRZ 25-005, REV "H".Sep 20, 2010 · N672FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201009203580Floor Panel · crackedAFT CARGO COMPARTMENT FLOOR PANEL 151 XF IS CRACKED IN 2 LOCATIONS. FABRICATED NEW AFT CARGO FLOOR PANEL 151 RF IAW DWG SRZ 25-005, REV "H".Sep 20, 2010 · N672FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201009203582Floor Panel · damagedAFT CARGO COMPARTMENT FLOOR PANEL 152 PF CORNER IS DAMAGED. FABRICATED NEW AFT CARGO FLOOR PANEL 152 PF IAW DWG SRZ 25-005, REV "H".Sep 20, 2010 · N672FE · Airbus A300F4605R · Fuselage Floor PanelSDR HALA2010091800424Warning Message · illuminatedETOPS SIGNIFICANT SYS - RUDDER RATIO EICAS MESSAGE CAME ON AFTER TAKEOFF. ACCOMP FIM 27-21-0 FIG 104. TEST OK.Sep 18, 2010 · N594HA · Boeing 767332 · Rudder Control SystemSDR IPXA10662653Floor Panel · damagedD424529 MAIN CARGO POS 5 L FLOOR PANEL 2ND FROM OTBD HAS .5" HOLE. REMOVED AND MFG NEW FLOOR PANEL IAW B767-5320-9693G.Sep 18, 2010 · N314UP · Boeing 76734AF · Fuselage Floor PanelSDR DALA1023470128Wire · damagedEMERGENCY LIGHTS AT SEATS 27AB AND 27FG ARE INOPERATIVE. MX REPAIRED THE POWER CONNECTION AT SEAT 27A. SYS OPS IS NORMAL.Sep 18, 2010 · N128DL · Boeing 767332 · Light System WiringSDR HALA2010091600421Selector Valve · leakingETOPS SIGNIFICANT SYS - ON ARRIVAL, FOUND HYD LEAKING RT GEAR WHEEL WELL. R & R MAIN GEAR SELECTOR VALVE IAW AMM TASK 32-31-02-004-001 AND TASK 32-31-02-404-008. OPS AND LEAK CKD OK.Sep 16, 2010 · N594HA · Boeing 767332 · Landing Gear Retraction/Extension SystemSDR FDEA201009163512Sensor · failedAT SLATS RETRACT, 250KTS .538M, FL 160 THE UPPER FOOT WOULD NOT MOVE UP FROM 258 KTS AND ALLOW THE ACFT TO ACCELERATE, IMMEDIATELY GOT STICK SHAKER, THEN REDEPLOYED THE SLATS. ACFT WAS ON A/P 1 AT TIME OF SLAT RETRACTION, DISCONNECTED AUTOPILOT WHEN STICK SHSep 16, 2010 · N590FE · Doug MD11F · Leading Edge Slat Position Indicating SystemSDR DALA1023161809Fuse · failedEMERGENCY LIGHTS AT SEATS 6A-10A ARE INOPERATIVE. MX REPLACED A FUSE IN M7235. SYS OPS IS NORMAL.Sep 15, 2010 · N833MH · Boeing 767432ER · Emergency LightingSDR UIEA201000204Seat Track · damagedPURPOSE OF THIS EO IS TO DOCUMENT A MAJOR REPAIR (CATEGORY A) THAT WAS ACCOMPLISHED DURING D-CHECK. DURING D-CHECK INSP OF DATUM ACFT, EGAT FOUND DAMAGE (WORN) ON SEAT TRACK CROWN AREA BETWEEN STA 1840 AND 1860, LBL 11.33.EGAT PERFORMED REPAIR IAW SRM 53-00-52Sep 15, 2010 · N497MC · Boeing 74747UF · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201009153497Seat Track · crackedMAIN DECK CARGO COMPARTMENT - SEAT TRACK CRACKED AT STATION 1541 LBL 47. MAIN DECK CARGO COMPARTMENT - SEAT TRACK REMOVED AND REPLACED AS PER SRM 53-00-52 FIGURE 201 REVISION 44 FROM STA 1531 TO STA 1571 , X= 47.25. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER Sep 15, 2010 · N603FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201009153498Seat Track · corrodedMAIN DECK CARGO SEAT TRACK RBL 106 CORRODED AT STATION 1701 TO STATION 1785. CORROSION REMOVED AS PER SRM 51-21-01 REVISION 44. ORIGINAL THICKNESS= 0.080"; MATERIAL REMOVED= 0.050"; MATERIAL REMAINED= 0.030" FOUND EXCEEDED LIMIT AS PER SRM 53-00-52 FIGURESep 15, 2010 · N603FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201009153499Seat Track · corrodedMAIN DECK CARGO, AFTER REMOVAL OF FLOOR PANEL (282GF) WITH CORRODED FERRULES FOUND SEAT TRACK FLANGE CORRODED AT STA 1598 X= 107.25. CORROSION REMOVED AS PER SRM 51-21-01 REVISION 44. FOUND EXCEEDED LIMIT AS PER SRM 53-00-52 FIGURE 101 REVISION 44. DAMSep 15, 2010 · N603FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201009153500Seat Track · corrodedMAIN DECK CARGO - AFTER REMOVAL OF FLOOR PANEL (282GF) WITH CORRODED FERRULES FOUND SEAT TRACK FLANGE CORRODED AT STATION 1610 TO STATION 1750 X= -75. CORROSION REMOVED AS PER SRM 51-21-01 REVISION 44. FOUND EXCEEDED LIMIT AS PER SRM 53-00-52 FIGURE 101 REVISep 15, 2010 · N603FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR HALA2010091400422Structure · damagedETOPS SIGNIFICANT SYS - RT WING OTBD FLAP L/E SUSTAINED DAMAGE APPROX IN LINE W W/S 746.2. ACCOMPLISHED HAL-M105 FILE NR597114 REV A. OK FOR SERVICE.Sep 14, 2010 · N597HA · Boeing 767332 · Trailing Edge FlapsSDR UIEA201000200Floor Panel · damagedDURING D-CHECK INSP OF DATUM ACFT, DAMAGES (GOUGE) WERE FOUND ON BULK CARGO FLOOR PANELS BETWEEN BS 2040 AND BS 2160. THE DAMAGE AREAS WERE REPAIRED IAW SRM 51-70-13, FIG 201.Sep 14, 2010 · N497MC · Boeing 74747UF · Fuselage Floor PanelSDR UIEA201000201Skin · dentedDURING D-CHECK INSP OF DATUM ACFT, A DENT WAS FOUND ON LT APU DOOR OUTER SKIN AT STA 2684 BETWEEN WL 276 - WL 286. THE DAMAGE AREA WAS REPAIRED IAW SRM 52-00-01, REPAIR 7.Sep 14, 2010 · N497MC · Boeing 74747UF · Auxiliary Power Unit (APU) DoorsSDR UIEA201000202Skin · dentedDURING D-CHECK INSP OF DATUM ACFT, A DENT WAS FOUND ON LT APU DOOR OUTER SKIN AT STA 2693 BETWEEN WL 276 - WL 286. THE DAMAGE AREA WAS REPAIRED IAW SRM 52-00-01, REPAIR 7.Sep 14, 2010 · N497MC · Boeing 74747UF · Auxiliary Power Unit (APU) DoorsSDR UIEA201000205Skin · dentedDURING THE D02 PLUS C03, DENT DAMAGE ON THE LOWER SKIN WAS DETECTED AT STAB STA 156.0 OF THE LOWER SKIN 65B03500-143 AND DOCUMENTED IAW EGAT NRC 390. THE ACTION REQUIRED TO CLOSE EGAT NRC 390 WAS TO CUT THE DAMAGE OUT AND TO INSTALL A FLUSH REPAIR IAW REPAIR SSep 14, 2010 · N497MC · Boeing 74747UF · Horizontal Stabilizer, Plate/SkinSDR UIEA201000207Skin · dentedDURING D-CHECK INSP OF DATUM ACFT, A DENT WAS FOUND ON LT APU DOOR SKIN (PN:65B02771-190) AT STA 2661 (THE DETAIL LOCATION AND DIMENSION ARE SHOWN IN FIG 1).Sep 14, 2010 · N497MC · Boeing 74747UF · Auxiliary Power Unit (APU) DoorsSDR FDEA201009133366Skin · crackedHFEC OPEN HOLE CARRIED OUT AND FOUND 04 EA HOLES WITH CRACK INDICATION AT LT WING OUTER WING ACCESS DOOR CUTOUT AT BETWEEN STA XORS= 683.4 AND XORS= 713.6. REPAIRED HOLES AS PER SRM 57-20-02 REVISION 44 REPAIR 4 AND DRAWING SG11570004 REVISION A. THIS REPAIRSep 13, 2010 · N603FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201009133367Skin · crackedHFEC OPEN HOLE CARRIED OUT AND FOUND 02 EA HOLES WITH CRACK INDICATION AT RT WING OUTER WING ACCESS DOOR CUTOUT AT BETWEEN STATION XORS= 683.4 AND XORS= 713.6. REPAIRED HOLES AS PER SRM 57-20-02 REVISION 44 REPAIR 4 AND DRAWING SG11570004 REVISION A. THIS Sep 13, 2010 · N603FE · Doug MD11F · Wing, Plate/SkinSDR HALA2010091200416Module · malfunctionedETOPS SIGNIFICANT SYS - CAPT'S DESCENDING THROUGH 24,000 RA FLAG APPEARED FOLLOWED BY GEAR NOT DOWN EICAS MG & CONFIG DISCREET LIGHT. RA FLAG DISAPPEARED & SO DID ALL OTHER EICAS MSG SUSPECT RADIO ALT PROBLEM. BOTH RA R/T GROUND OPS CHECKED OK IAW FIM34-33-0Sep 12, 2010 · N594HA · Boeing 767332 · Landing Gear SystemSDR UIEA201000203Skin · dentedDAMAGE WAS FOUND TO THE RT OTBD MID FLAP - WBL763 T/E WITH A DENT (1.0 IN. X 1.0 IN. DIAM. AFTER DAMAGE REMOVAL). DISPOSITION WAS MADE TO PERFORM A PERMANENT REPAIR IAW EGAT NRC 659; PERFORMED IAW THE SRM 57-53-01, FIG 201, REPAIR 1 IAW SRM 51-70-06 (WET LAYUPSep 10, 2010 · N497MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA201000216Skin · dentedLT OTBD AFT FLAP WBL424 INBD SIDE UPPER SKIN DENT, REPAIRED IAW SRM 57-53-01 FIG 201, REPAIR 1 IAW SRM 51-70-10 REF. EGAT NRC 361, RAM FORM 073).Sep 10, 2010 · N497MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA201000217Skin · debondedLT OTBD AFT FLAP WBL666 TE UPPER SKIN DISBOND, REPAIRED IAW SRM 57-53-01 FIG 201, REPAIR 1 IAW SRM 51-70-06, FIG 5 (REF. EGAT NRC 375, RAM FORM 074).Sep 10, 2010 · N497MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA201000219Skin · damagedLT INBD FORE FLAP WBL143-159 TOP PANEL UPPER SKIN NICK, PUNCH & BEND, REPAIRED IAW SRM 57-53-01 FIG 201, REPAIR 1 IAW SRM 51-70-10, REPAIR 4 (REF EGAT NRC 722, RAM FORM 076).Sep 10, 2010 · N497MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA201000221Skin · damagedLT INBD MID FLAP WBL241.5 LWR PANEL INNER SKIN TOOL MARK/NICK, REPAIRED IAW SRM 57-53-01 FIG 201, REPAIR 1 IAW SRM 51-70-10.Sep 10, 2010 · N497MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA201000222Skin · dentedLEFT INBD MID FLAP WBL180 & WBL201 LWR PANEL INNER SKIN DENT, REPAIRED IAW SRM 57-53-01 FIG 201, REPAIR 1 IAW SRM 51-70-10, REPAIR 2 (REF. EGAT NRC 773, RAM FORM 068).Sep 10, 2010 · N497MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA201000223Skin · dentedLEFT INBD MID FLAP WBL223 & WBL374 TE UPPER SKIN DENT, REPAIRED IAW SRM 57-53-01 FIG 201, REPAIR 1 IAW SRM 51-70-06, FIG 5 (REF. EGAT NRC 180, RAM FORM 066).Sep 10, 2010 · N497MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA201000224Skin · dentedLEFT INBD MID FLAP WBL281 & WBL355 LWR PANEL INNER SKIN DENT, REPAIRED IAW SRM 57-53-01 FIGURE 201, REPAIR 1 IAW SRM 51-70-10, REPAIR 4 (REF. EGAT NRC 775, RAM FORM 069).Sep 10, 2010 · N497MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA201000225Skin · dentedLEFT OTBD MID FLAP WBL 554.5 & WBL 570 L/E SKIN DENT & DISBOND, REPAIRED IAW SRM 57-53-01 FIG 201, REPAIR 1 IAW SRM 51-70-07, FIG 5 (REF. EGAT NRC 991, RAM FORM 072).Sep 10, 2010 · N497MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA201000226Skin · debondedRIGHT INBD FORE FLAP WBL 254.5-335.5 L/E SKIN DISBOND, REPAIRED IAW SRM 57-53-01 FIG 201, REPAIR 1 IAW SRM 51-70-07, FIG 5 (REF EGAT NRC 992, RAM FORM 080).Sep 10, 2010 · N497MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA201000227Skin · dentedRIGHT OTBD FORE FLAP WBL 557 & WBL 695 L/E SKIN DENT, REPAIRED IAW SRM 57-53-01 FIG 201, REPAIR 1 IAW SRM 51-70-07, FIG 5 (REF. EGAT NRC 043, RAM FORM 065).Sep 10, 2010 · N497MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA201000228Skin · dentedRIGHT OTBD AFT FLAP WBL 217 TOP PANEL DENT, REPAIRED IAW SRM 57-53-01 FIG 201, REPAIR 1 IAW SRM 51-70-10.Sep 10, 2010 · N497MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA201000229Skin · chafedRIGHT OTBD AFT FLAP WBL820 L/E SKIN CHAFED, REPAIRED IAW SRM 57-53-01 FIG 201, REPAIR 1 IAW SRM 51-70-06, FIG 5.Sep 10, 2010 · N497MC · Boeing 74747UF · Trailing Edge FlapsSDR IPXA10662538Floor Panel · damagedINSPECTION TYPE:C, MCD STA 930 TO 975 LBL 11" TO RBL 11" FLOOR PANEL, FOUND 1 DAMAGED, 1 GOUGE & 10 DENT MARKS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Sep 8, 2010 · N331UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10662573Panel · crackedINSPECTION TYPE:C, RT WING NR7 SLAT CLOSURE PANEL EXISTING REPAIR PATCH CRACKED. COMPOSITE REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5H, FIG 15, REV 47.Sep 8, 2010 · N331UP · Boeing 76734AF · Wing, Plate/Skin
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