N68059, cancelled Jul 29, 2013

Service difficulty reports · 74

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N68059' AND deregistration_id = 'N68059-2013-07-29'
  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.

SDR FDEA201105071778Battery Pack · dischargedEMERGENCY POWER BAT 1 LO ON PRE-FLIGHT. RELEASED FOR SERVICE IAW MEL: 33-50-02. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS POWER SUPPLY IN ACCORDANCE WITH MD10-10 AMM 33-51-01-4,5; OPERATIONAL TEST SATISFACTORY. ACFT. OKAY FOR SERVICE.May 7, 2011 · N68059 · Doug MD1010F · Emergency LightingSDR FDEA201105061765Latch · wornDURING CLIMBOUT ADG DEPLOYED ON ITS OWN. AUX PUMP ON/ADG ELECTRIC ON ALL NORMAL. SLOWED TO A SLOWER CRUISE SPEED. R & R OTBD UPLATCH SPRING, AMM 24-25-01-2. CHECKED ROLLER. CHECKED NORMAL. AWAITING UPLATCH HOOK.May 6, 2011 · N68059 · Doug MD1010F · AC Generation SystemSDR FDEA201105021688Control Unit · failedEMERGENCY POWER TEST INITIATES NORMALLY, AFTER 30SEC TEST APPEARS TO COMPLETE NORMALLY BUT EMERGENCY POWER TST FAIL ALERT APPEARS. DUE TO OTHER FAULTS NOTED ON ENG RUN ORDERED THE EPCU UNDER THE TSI. R & R EPCU OPS CHECK NORMAL. EMERGENCY POWER TEST ALSO CHMay 2, 2011 · N68059 · Doug MD1010F · AC InverterSDR FDEA201104281678Adg · unwanted deployPASSING FL14K, 320 KTS. NO TURBULANCE, THE ADG APPARENTLY DEPLOYED. HYD AUX PUMP LEVEL 0 ELEC CUE ON SD SHOWED GREEN ADG SYMBOL HYD CUE ON SD SHOWED AUX PUMP 1 ON. FULLY ENGAGED UPLOCK CLEVIS, AND STOWED ADG IAW MM 24-25-01-2 RII:036722.Apr 28, 2011 · N68059 · Doug MD1010F · AC InverterSDR FDEA201005261661Unknown · malfunctionedACFT LEFT AIRPORT WITH NR 1 TANK FUEL QTY DEFERRED. UPON ARRIVAL INTO ,CREW REPORTED THAT ON APPROACH THEY GOT THE NR 1 TANK FUEL QTY LOW FAULT. CHECKED NR 1 TANK FUEL LEVEL STICKS AND FOUND ONLY 1200 LBS IN TANK NR 1,14600LBS IN TANK NR 2 AND 9100 LBS IN TMay 26, 2010 · N68059 · Doug MD1010F · Fuel StorageSDR FDEA200904161317Wire · unknownCLIMBOUT PASSING 1000 FT RECEIVED ENG 2 EXCEEDANCE ALERT. RETARDED THROTTLE & N1 NOT EXCEEDED BUT HAD LARGE FLUCTUATIONS. ENG 2 N2 EGT NORMAL. PASSING 3000 FT RECEIVED ENG 2 RPM HI ALERT. ACCOMPLISHED CHECKLIST & ABLE TO KEEP NI RPM IN LIMITS WITH THROTTLEApr 16, 2009 · N68059 · Doug MD1010F · Engine Indicating System WiringSDR 08FDEA04420Cable · inoperativeNR 2 THROTTLE STUCK DURING CRUISE. ENGINE SHUTDOWN DURING DESCENT. NR 2 THROTTLE MOVED BACK ON SHORT FINAL AFTER LANDING NR 2 THROTTLE COULD BE MOVED TO IDLE. CABLE COMING FROM OAK. REPLACED #2 THROTTLE CABLE PER MM 76-11-01-2, OP'S CHEKS NORMAL. PERFORMEDOct 17, 2008 · N68059 · Doug DC1010F · Auto Throttle SystemSDR 08FDEA02120Skin · failedDURING REPAIR ASSESSMENT AN EXISTING REPAIR WAS FOUND AT FUSELAGE SKIN REPLACED EXISTING REPAIR IAW SRM53-50-00 FIG 9 BECAUSE IT IS NOT IN COMPLIANCE WITH APPROVED DATA.Jun 3, 2008 · N68059 · Doug DC1010F · Fuselage Main, Plate/SkinSDR 08FDEA02018Door Frame · misrepairedDURING REPAIR ASSESSMENT WAS FOUND AN EXISTING REPAIR AT CTR CARGO FUSELAGE DOOR JAMB REPAIR HAS BEEN REPLACED BECAUSE IT FOUND NOT IN CONFORMITY WITH APPROVED DATA.May 28, 2008 · N68059 · Doug DC1010F · Fuselage Main, StructureSDR 08FDEA02017Structure · misrepairedDURING REPAIR ASSESSMENT WAS FOUND AN EXISTING REPAIR AT CENTER FUSELAGE DOOR JAMB LT SIDE REPAIR HAS BEEN REPLACED BECAUSE IT FOUND NOT IN CONFORMITY WITH APPROVED DATA.May 28, 2008 · N68059 · Doug DC1010F · Fuselage Main, StructureSDR 08FDEA01900Skin · damagedDURING DC10 CARGO MODIFICATION TO ACF DURING INSPECTION FOUND ON THE CENTER LOWER CARGO DOOR LATERAL SKIN DAMAGE. REPAIRED CENTER CARGO DOOR PAN ASSEMBLY FOR SRM 52-10-00 FIG 3 VOL 1.May 20, 2008 · N68059 · Doug DC1010 · Cargo/Baggage DoorsSDR 08FDEA01833Skin · damagedEXISTING EXTERNAL REPAIR DOUBLER AT FIXED L/E STA XIS 150 REMOVE REPAIR AND ACCOMPLISH A NEW IAW SRM 57-10-00 FIG 40 BECAUSE REPAIR DETECTED WAS FOUND WITH A SIGNIFICANT LOSS OF MATERIAL DUE TO A LIP CONTACT.May 13, 2008 · N68059 · Doug DC1010F · Wing, Plate/SkinSDR 08FDEA01748Skin · damagedDURING REPAIR ASSESSMENT WAS FOUND AN EXISTING EXTERNAL REPAIR AT FUSELAGE SKIN STA 1019, LONG NR 37R REPAIR FOUND NOT IN CONFORMITY WITH APPROVED DATA AND HAS BEEN REPLACED WITH A NEW IAW SRM 53-20-00 FIG 6 SH 3 AND 4.May 5, 2008 · N68059 · Doug DC1010F · Fuselage Main, Plate/SkinSDR 08FDEA01698Web · crackedDURING MD10 ACF MODIFICATION IN UPPER FUSELAGE AT STA 1305 JAMB DOOR L3 FOUND CRACK 0.5 INCH LONG ON THE WEB UPPER SIDE. PERFORMED REPAIR FOR SRM 53-50-00 FIG 19 VOL. IApr 30, 2008 · N68059 · Doug DC1010F · Fuselage Miscellaneous StructureSDR 08FDEA01637Door Frame · crackedDURING MD10 ACF MODIFICATION IN UPPER FUSELAGE AT STA 1305 JAMB DOOR R3 FOUND CRACK 0.5 INCH LONG ON THE WEB. REPAIRED FOR SRM 53-50-00 FIG 19 VOL I.Apr 28, 2008 · N68059 · Doug DC1010F · Fuselage Main, StructureSDR 08FDEA01636Door Frame · crackedDURING MD10 ACF MODIFICATION ON UPPER FUSELAGE AT STA 1256 JAMB DOOR R3 FOUND N2 CRACK TO 2 INCH LONG ON THE WEB LOWER SIDE. REPAIRED FOR SRM 53-50-00 FIG 19 VOL I AND REPLACED CHANNEL P/N AEA0210-40.Apr 28, 2008 · N68059 · Doug DC1010F · Fuselage Main, StructureSDR 08FDEA01635Seat Track · corrodedDURING MD10 ACF MODIFICATION IN UPPER FUSELAGE ON SEAT TRACK AT STA 502 X= 63, FOUND CORROSION AND SCREW BROKEN. REPLACED TRACK AFA7789-521 FOR DWG AND SRM 53-70-00 FIG 1 VOL I.Apr 28, 2008 · N68059 · Doug DC1010F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA01633Door Frame · crackedDURING MD10 ACF MODIFICATION IN UPPER FUSELAGE AT STA 1256 JAMB DOOR R3 FOUND CRACK 0.5" LONG ON THE WEB UPPER SIDE REPAIRED FOR SRM 53-50-00 FIG 19 VOL I.Apr 28, 2008 · N68059 · Doug DC1010F · Fuselage Main, StructureSDR 08FDEA01631Seat Track · corrodedDURING MD10 ACF MODIFICATION IN UPPER FUSELAGE ON SEAT TRACK X -107 STA 1581 TO 1661 FOUND SEVERAL POINT OF CORROSION. REPAIRED FOR SRM 53-70-00 FIG 1 VOL I.Apr 28, 2008 · N68059 · Doug DC1010F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA01629Seat Track · wornDURING MD10 ACF MODIFICATION IN UPPER FUSELAGE ON SEAT TRACK STA 635- 615 X -28, FOUND USURED AND MISSING MATERIAL REPAIRED FOR SRM 53-70-00 FIG 1 VOL I.Apr 28, 2008 · N68059 · Doug DC1010F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA01478Seat Track · damagedDURING MD10 ACF MODIFICATION IN UPPER FUSELAGE AT STA 1273 AND X -47.250 FOUND MISSING MATERIAL ON SEAT TRACK. REPAIRED SEAT TRACK FOR SRM 53-10-00 FIG 1 VOL I.Apr 23, 2008 · N68059 · Doug DC1010F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA01477Frame · crackedDURING MODIFICATION IN CENTER ACCESSORY COMPARTMENT AT STA 1099 FROM LONGERON 49 TO LONGERON 48 RT SIDE FOUND LIGHT CORROSION AND CRACK LONG 0.5" ON CAP FRAME. REMOVED CORROSION FOR SRM 51-21-01 VOL II AND PERFORMED FRAME CAP REPAIR FOR SRM 53-30-00 FIG 8 VOLApr 23, 2008 · N68059 · Doug DC1010 · Fuselage Main, FrameSDR 08FDEA01441Seat Track · damagedDURING MD10 ACF MODIFICATION IN UPPER FUSELAGE AT STA 1209 X= 47.250 SEAT TRACK WITH MISSING MATERIAL. REPAIRED FOR SRM 53-70-00 FIG 1 VOL I.Apr 17, 2008 · N68059 · Doug DC1010F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA01440Seat Track · damagedDURING MD10 ACF MODIFICATION IN UPPER FUSELAGE FROM STA 1099 TO STA 1159 ON SEAT TRACK FOUND HOLES OVALIZED REPAIRED FROM SRM 53-70-00 FIG 1 VOL I.Apr 17, 2008 · N68059 · Doug DC1010F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA01439Seat Track · crackedDURING MD10 ACF MODIFICATION IN UPPER FUSELAGE AT STA 1341 X = -75.250 FOUND SEAT TRACK WITH CRACK .5" LONG REPAIRED FOR SRM 53-70-00 FIG 1 VOL I.Apr 17, 2008 · N68059 · Doug DC1010F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA01438Rib · damagedDURING MD10 ACF MODIFICATION ON SLAT NR 3 RT WING FOUND RIB P/N ARB1666-502 WITH HOLE OVALIZED REPLACED RIB FOR SRM 51-35-01 VOL II AND DWG NRB6027.Apr 17, 2008 · N68059 · Doug DC1010F · Wing, Rib/BulkheadSDR 08FDEA01424Skin · dentedDURING MD10 ACF MODIFICATION ON LOWER FUSELAGE EXTERNAL FOUND DENT 0.047" BY 2" BY 1.5 INCH LONG ON EXTERNAL SKIN STA 1049 RT SIDE LONGERON 46 TO LONGERON 47. REPAIRED FOR SRM 53-20-00 FIG 6 VOL I.Apr 16, 2008 · N68059 · Doug DC1010F · Fuselage Main, Plate/SkinSDR 08FDEA01423Rib · damagedDURING MD10 ACF MODIFICATION ON WING LT SIDE OUTBOARD SLAT NR 3 FOUND RIB P/N ARB1666-501 WITH EA 7 HOLES OVALIZED. REPLACED RIB FOR SRM 51-35-01 VOL II AND DWG ARB1666.Apr 16, 2008 · N68059 · Doug DC1010F · Wing, Rib/BulkheadSDR 08FDEA01401Frame · crackedDURING MD10 MODIFICATION TO ACF IN AVIONIC COMPARTMENT RT SIDE STA 469 X =-61 FOUND FRAME WITH CRACK 1 INCH REPAIRED FOR SRM 53-30-00 FIG 11 VOL I.Apr 14, 2008 · N68059 · Doug DC1010F · Fuselage Main, FrameSDR 08FDEA01400Floorbeam · damagedDURING MD10 MODIFICATION ACF FOUND IN AFT CARGO COMPT STA 1857 AT X 30 BEAM FLOOR WITH DOUBLE HOLE. REPAIRED FOR SRM 53-60-01 FIG 3 VOL I.Apr 14, 2008 · N68059 · Doug DC1010F · Fuselage Main, Floor BeamSDR 08FDEA01399Seat Track · damagedDURING MD10 ACF MODIFICATION IN UPPER FUSELAGE AT STA.939 X -47.50 FOUND SEAT TRACK WITH HOLE OVALIZED REPAIRED FOR SRM 53-70-00 FIG 1 VOL I.Apr 14, 2008 · N68059 · Doug DC1010F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA01331Skin · crackedDURING MD10 ACF MODIFICATION FOUND ON UPPER FUSELAGE AT STA 1305 JAMB DOOR R NR 3 NUMBER 2 CRACK 2 INCHES LONG ON THE WEB IN POSITION LOWER REPAIRED FOR SRM 53-50-00 FIG 19 VOL I.Apr 7, 2008 · N68059 · Doug DC1010F · Fuselage Main, Plate/SkinSDR 08FDEA01330Skin Panel · delaminatedDURING MD10 ACF MODIFICATION ON HORIZONTAL STABILIZER RT SIDE FOUND DISBONDING THE UPPER SKIN TIP OUTBOARD ELEVATOR REPLACED SKIN ASSY FOR SRM 51-35-01 AND DWG ALC7347,ALC7348, ALC7602.Apr 7, 2008 · N68059 · Doug DC1010F · Horizontal Stabilizer, Plate/SkinSDR 08FDEA01297Frame · crackedDURING MD10 ACF MODIFICATION ON UPPER FUSELAGE AT STA 1781 LT STRINGER 13 FOUND FRAME WITH CRACK 5 INCHES LONG. REPAIRED FOR SRM 53-30-00 FIG 5 SECT.Apr 4, 2008 · N68059 · Doug DC1010F · Fuselage Main, FrameSDR 08FDEA01209Skin · misrepairedDURING REPAIR ASSESSMENT AN EXISTING REPAIR AT FUSELAGE SKIN WAS FOUND NOT IN CONFORMITY WITH APPROVED DATA REPAIR HAS BEEN REPLACED WITH A NEW IAW SRM 53-50-00 FIG 26, VOL I.Mar 31, 2008 · N68059 · Doug DC1010F · Fuselage Main, Plate/SkinSDR 08FDEA01208Skin · misrepairedDURING REPAIR ASSESSMENT AN EXISTING REPAIR AT FUSELAGE SKIN WAS FOUND NOT IN CONFORMITY WITH APPROVED DATA REPAIR HAS BEEN REPLACED WITH A NEW IAW SRM 53-20-00 FIG 6, SH 3/4.Mar 31, 2008 · N68059 · Doug DC1010F · Fuselage Main, Plate/SkinSDR 08FDEA01187Fitting · corrodedDURING MD10 ACF MODIFICATION MAIN CARGO DOOR LOWER JAM SUPPORT FITTING AFTER INSPECTION FOUND BORE "B", "A" AND "D" OF FITTING NR 4 WITH CORROSION (DIAMETER .456") (REF EO FEDEX 8-5230-117635. PERFORMED REWORK HOLE FOR SRM 53-50-00 FIG 17, PERFORMED NDI ANMar 28, 2008 · N68059 · Doug DC1010F · Fuselage Main, StructureSDR 08FDEA01185Fitting · corrodedDURING MD10 ACF MODIFICATION MAIN CARGO DOOR LOWER JAM SUPPORT FITTING AFTER INSPECTION FOUND BORE "C" OF FITTING NR 1 WITH CORROSION (DIAMETER .456"), REF EO FEDEX 8-5230-117635. PERFORMED REWORK HOLE FOR SRM 53-50-00 FIG 17, PERFORMED NDI AND INSTALLED BUSHMar 28, 2008 · N68059 · Doug DC1010F · Fuselage Main, StructureSDR 08FDEA01183Fitting · corrodedDURING MD10 ACF MODIFICATION MAIN CARGO DOOR LOWER JAM SUPPORT FITTING AFTER INSPECTION FOUND BORE "B", "C" AND "D" OF FITTING NR 7 WITH CORROSION DIAMETER .456 INCH (REF.E.O. FEDEX 8-5230-117635). PERFORMED REWORK HOLE FOR SRM 53-50-00 FIG 17, PERFORMED NDIMar 28, 2008 · N68059 · Doug DC1010F · Fuselage Main, StructureSDR 08FDEA01182Fitting · corrodedDURING MD10 ACF MODIFICATION MAIN CARGO DOOR COVER JAM SUPPORT FITTING AFTER INSPECTION FOUND BORE "B" OF FITTING NR 3 WITH CORROSION (DIAMETER .58") (REF EO FEDEX 8-5230-117635). PERFORMED REWORK HOLE FOR SRM 53-50-00 FIG 17, PERFORMED NDI AND INSTALLED BUSMar 28, 2008 · N68059 · Doug DC1010F · Fuselage Main, StructureSDR 08FDEA01180Seat Track · corrodedDURING MD10 ACF MODIFICATION IN UPPER FUSELAGE AT STA 1099 BETWEEN SEAT TRACK X= -78 AND X=-81 FOUND CORROSION ON FLOOR SUPPORT REMOVED CORROSION IS OUT LIMIT THE REWORK. REPLACED SUPPORT FOR DWG ADA3615 AND SRM 51-35-01 VOL II.Mar 28, 2008 · N68059 · Doug DC1010F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA01151Hinge Bracket · corrodedDURING MODIFICATION MD10 ACF RT OUTBOARD FLAP INBOARD HINGE WITH RUST, BUSHING WITH PLAY AND SHIM WITH OXIDE. REPLACED HINGE FLAP P/N ARC0502-501 FOR DWG ARC0504.Mar 26, 2008 · N68059 · Doug DC1010F · Trailing Edge FlapsSDR 08FDEA01137Hinge Bracket · corrodedDURING MD10 ACF MODIFICATION FOUND RT OUTBOARD FLAP, OUTBOARD HINGE WITH RUT AND CORROSION. REPLACED BRACKET ASSY OUT FLAP FOR DWG ARC0503-502Mar 25, 2008 · N68059 · Doug DC1010 · Trailing Edge FlapsSDR 08FDEA01136Hinge Bracket · corrodedDURING MD10 ACF MODIFICATION, FOUND LT OUTBOARD FLAP OUTBOARD HINGE WITH ATTACH POINTS WITH OXIDE. REPLACED BRACKET ASSY P/N ARC0503-501 FOR DWG ARC0505.Mar 25, 2008 · N68059 · Doug DC1010F · Trailing Edge FlapsSDR 08FDEA01135Hinge Bracket · corrodedDURING MD10 ACF MODIFICATION, FOUND LT OUTBOARD INBOARD FLAP HINGE WITH ATTACH POINT (FWD) RUST AND BUSHING WITH PLAY. REPLACED BRACKET ASSY FOR DWG ARC0504.Mar 25, 2008 · N68059 · Doug DC1010F · Trailing Edge FlapsSDR 08FDEA00872Frame · crackedDURING MODIFICATION DC10 CARGO TO MD10 ACF, AT REMOVAL BRACKET IS NOTED CRACK 1.5 INCH LONG ON FRAME STA 1851 RT SIDE LONGERON 10 TO 11. PERFORMED REPAIR FOR EA FEDEX 8-5310-111515.Mar 11, 2008 · N68059 · Doug DC1010F · Fuselage Main, FrameSDR 08FDEA00774Bracket · damagedFOUND ON PYLON NR 3 ON STA YN=240 THE BRACKET WITH DAMAGED AND DO NOT INSTALLED FOR DWG REPLACE WEB FOR SRM 51-33-01 VOL II AND DWG AUB7027.Mar 7, 2008 · N68059 · Doug DC1010F · Nacelle/Pylon Miscellaneous StructureSDR 08FDEA00678Fitting · crackedDURING MODIFICATION DC10 FREIGHTER TO MD10 ACF, FOUND IN AIR CONDITION COMPARTMENT NR 3 RT SIDE STA 555 X= -96 Z=-37,50 THE END FITTING FRAME WITH CRACK. INSPECTED AREA AND REPLACED SUPPORT P/N ACA3137-1.Mar 3, 2008 · N68059 · Doug DC1010F · Fuselage Miscellaneous StructureSDR 06FDEA2434Unknown · unknownREPAIR DOUBLER STA 620 FWD LOWER CORNER MAIN CARGO DOOR CUT-OUT MARKED NR 73. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. COMPLIED WITH FEDEX EA 8-5330-100785, FUSELAGE, MAIN CARGO DOOR OJun 30, 2006 · N68059 · Doug DC1010 · Standard Practices/StructuresSDR 06FDEA2413Bolt · shearedRIGHT WING TRAILING EDGE INTERIOR STRUCTURE, OUTBOARD FLAP INBOARD TRACK SUPPORT FITTING LOWER OUTBOARD ATTACH BOLT SHEARED AT AFT SPAR. COMPLIED WITH E8-5710-100781 PT 1, LOWER ATTACH STUD BOLT REPLACED. MAJOR REPAIR.Jun 27, 2006 · N68059 · Doug DC1010 · Trailing Edge Flaps
Back to N68059, cancelled Jul 29, 2013