N605FE

Service difficulty reports · 508

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 = 'N605FE' AND registry_match = 'registration'
  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 FDEA201211264156Seat Track · corrodedCENTER CARGO COMPARTMENT, ABOVE CEILING AREA, AT BS 1661, "X"= 75, SEAT TRACK FLANGE FOUND CORRODED. SEAT TRACK REPLACED FROM BS 1651 TO 1711, IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 51. REPAIR CLASSIFIED AS MAJOR, IAW MM 6-2-100, REV 115.Nov 26, 2012 · N605FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201211264155Seat Track · corrodedCENTER CARGO COMPARTMENT, ABOVE CEILING AREA AT BS 1701, "X" = 75, SEAT TRACK FLANGE FOUND CORRODED. SEAT TRACK REPLACED FROM BS 1651 TO 1711, IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 51. REPAIR CLASSIFIED AS MAJOR IAW MM 6-2-100, REV 115.Nov 26, 2012 · N605FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201211244147Skin · crackedLT WING L/E LOWER SURFACE ACCESS PANEL 518FB CUT-OUT CORNER FOUND CRACKED. REPAIRED IAW SRM 57-40-02, FIG 202, REPAIR 7, REV 51. REPAIR CLASSIFIED AS MAJOR IAW MM 6-2-100, REV 115.Nov 24, 2012 · N605FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201211244146Skin · crackedRT WING L/E FOUND LOWER FIXED PANEL NR 11 SLAT TRACK CUT-OUT SKIN EDGE CORNER CRACKED. REPAIRED IAW SRM 57-40-02, FIGURE 201, REPAIR 7, REVISION 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.Nov 24, 2012 · N605FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201211244145Cargo Track · corrodedMAIN DECK CARGO TRACK BS 1827, X= 8.5 FOUND WITH SURFACE CORROSION. CARGO TRACK REPLACEED FROM BS 1791 TO 1887, IAW SRM 53-00-52 FIGURE 201, REPAIR 1, REVISION 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.Nov 24, 2012 · N605FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201211244144Cargo Track · corrodedMAIN DECK CARGO TRACK BS 1661, X= -8.5 FOUND WITH SURFACE CORROSION. CARGO TRACK REPLACEED FROM BS 1531 TO 1671, IAW SRM 53-00-52 FIGURE 201, REPAIR 1, REVISION 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.Nov 24, 2012 · N605FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201211244143Cargo Track · corrodedMAIN DECK CARGO TRACK BS 1841, X= -27 FOUND WITH SURFACE CORROSION. CARGO TRACK REPLACED FROM BS 1791 TO 1887, IAW SRM 53-00-52 FIGURE 201, REPAIR 1, REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.Nov 24, 2012 · N605FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201211244142Cargo Track · corrodedMAIN DECK CARGO TRACK BS 1541, X= -8.5 FOUND WITH SURFACE CORROSION. CARGOTRACK REPLACED FROM BS 1531 TO 1671, IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 51. REPAIR CLASSIFIED AS MAJOR IAW MM 6-2-100, REV 115.Nov 24, 2012 · N605FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201211244141Cargo Track · corrodedMAIN DECK CARGO TRACK, BS 1745, X= -27 FOUND WITH SURFACE CORROSION. REPAIRED IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 51. REPAIR CLASSIFIED AS MAJOR IAW MM 6-2-100, REV 115.Nov 24, 2012 · N605FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201211244140Cargo Track · corrodedMAIN DECK CARGO TRACK BS 1541, X= -27 FOUND WITH SURFACE CORROSION. CARGO TRACK REPLACED FROM STATION 1531 TO 1571, IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 51. REPAIR CLASSIFIED AS MAJOR IAW MM 6-2-100, REV 115.Nov 24, 2012 · N605FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201211244139Skin · crackedLEFT WING NR 11 L/E SLAT TRACK CUT-OUT FOUND CRACKED AT XOS 720. REPAIRED IAW SRM 57-40-02, FIG 201, REPAIR 7, REV 51. REPAIR CLASSIFIED AS MAJOR IAW MM 6-2-100, REV 115.Nov 24, 2012 · N605FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201211244138Skin · crackedRT WING L/E NR 8 SLAT OTBD INNER SKIN FOUND CRACKED. REPAIRED IAW EA 1-5750-165172, PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.Nov 24, 2012 · N605FE · Doug MD11F · Leading Edge DevicesSDR FDEA201211234130Cargo Track · damagedMAIN DECK CARGO TRACK AT BS 1092, "X"= 47, FOUND CROWN ELONGATED. CARGO TRACK REPLACED FROM BS 1009 TO 1109, "X"= 47, IAW SRM 53-00-52 FIGURE 201, REPAIR 1, REVISION 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.Nov 23, 2012 · N605FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201211234129Cargo Track · damagedMAIN DECK CARGO TRACK AT BS 1035, "X"= 47", FOUND CROWN ELONGATED. REPAIRED IAW SRM 53-00-52 FIGURE 201, REPAIR 1, REVISION 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.Nov 23, 2012 · N605FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201211234131Access Panel · corrodedLEFT WING, T/E LOWER ACCESS PANEL NR 541JB CUTOUT FORWARD EDGE LOWER CAP. LOWER SURFACE FOUND CORRODED. CUTOUT FORWARD EDGE LOWER CAP DAMAGED. R & R WITH NEW CAP IAW SRM 51-31-01, REV 51. REPAIR CLASSIFIED AS MAJOR IAW MM 6-2-100, REV 115.Nov 23, 2012 · N605FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201211234128Cargo Track · corrodedMAIN DECK CARGO TRACK AT BS 873, "X"=-8.5", FOUND CORRODED. REPAIRED IAW SRM 53-00-52 FIGURE 201, REPAIR 1, REVISION 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.Nov 23, 2012 · N605FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201211234127Seat Track · corrodedMAIN DECK CARGO TRACK AT BS 873, "X"= 8.5, FOUND WITH CORROSION. REPAIRED IAW SRM 53-00-52 FIGURE 201, REPAIR 1, REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.Nov 23, 2012 · N605FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201211224124Door Frame · crackedCENTER CARGO DOOR, UPPER DOOR FRAME BEAM AT BS 1743, "X" =-106 CRACKED. REPAIRED IAW EA 1-5310-165169. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.Nov 22, 2012 · N605FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201211224123Vane · delaminatedLEFT WING, INBD FLAP VANE LOWER SURFACE FOUND DELAMINATED. REMOVED AND REPLACED IAW MM 27-50-22-4, REVISION 74.1. ADJUSTMENT CARRIED OUT IAW MM 27-50-22-830-801, REVISION 74.1 AND FOUND SATISFACTORY. FLAP OPS TEST CARRIED OUT IAW MM 27-50-00-860-801, REVISINov 22, 2012 · N605FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201210013527Power Supply · inoperativePRE-DISPATCH CHECK FOUND EMERGENCY LIGHT TEST FAILED. R & R THE EMERGENCY LIGHTING BATTERY POWER SUPPLY, OPS TEST PASSED .Oct 1, 2012 · N605FE · Doug MD11F · Emergency LightingSDR FDEA201206032067Battery · inoperativeDURING PREFLIGHT DISCOVERED DOOR R-1 EMERGENCY ESCAPE SLIDE PRESS TO TEST INDICATOR DID NOT ILLUMINATE WHEN PRESSED. REPLACED BATTERIES IAW SMP, OPS CHECKED NORMAL, OK FOR SERVICE.Jun 3, 2012 · N605FE · Doug MD11F · Escape SlideSDR FDEA201205021706Lamp · failedDOOR EVAC SLIDE PRESS TO TEST INDICATOR SWITCH INOPERATIVE. RELAMPED R1 DOOR REMOTE PRESSURE INDICATOR WITH CORRECT LAMPS IAW SMP. PERFOREMD OPS CHECK IAW AMM 25-61-04-5-0 WITH NO DEFECTS NOTED. ACFT OK FOR CONTINUED SERVICE AT THIS TIME.May 2, 2012 · N605FE · Doug MD11F · Escape SlideSDR FDEA201201190259Bulb · inoperativeR1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS TO TEST INOPERATIVE. REPLACED PUSH SWITCH LIGHT BULB ASSY AND OPS CHECKED NORMAL IAW MM 25-61-04-4.Jan 19, 2012 · N605FE · Doug MD11F · Escape SlideSDR FDEA201201170209Light · inoperativeR1 SLIDE CONTINUITY PRESS TO TEST LIGHT INOPERATIVE ON PRE-FLIGHT. CAN RT R & R TEST LIGHT BATTERY IAW SMP. PERFORMED OPS TEST IAW MM 25-61-04-5,CHECK.Jan 17, 2012 · N605FE · Doug MD11F · Escape SlideSDR FDEA201110224621Power Supply · failedEMER LT TEST FAILS, GET EMER LT BAT 1 ALERT DURING TEST. R & R EMERERGENCY LIGHTING BATTERY POWER SUPPLY REF MM 33-51-01-4-0. OK FOR SERVICE.Oct 22, 2011 · N605FE · Doug MD11F · Emergency LightingSDR FDEA201108083141Lamp · inoperativeLT MAIN ENTRY DOOR EVACUATION SLIDE PRESSURE WONT TEST. RELAMPED L1 EVACUATION SLIDE PACK PRESSURE INDICATION SWITCH IAW AMM 25-61-04-5-0, CHECKED GOOD.Aug 8, 2011 · N605FE · Doug MD11F · Escape SlideSDR FDEA201102200635Light · illuminatedEMERGENCY POWER ON LIGHT CAME ON DURING FLIGHT - FOLLOWED QRH IT WENT OUT. ADJUSTMENT TEST POWER SYS EMERGENCY IAW AMM 24-24-00-5. OPS CHECKED GOOD, ACFT OK FOR SERVICE AT THIS TIME. FINAL CLOSED.Feb 20, 2011 · N605FE · Doug MD11F · AC InverterSDR FDEA201101080081Longeron · crackedMAIN DECK STA 5-123, LONGERON 6 RT, LONGERON SPLICE CTR SECTION FOUND 2 EA CRACKED, APPROX 0.625 INCH LONG DURING X-RAY INSP. REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 45. LONGERON SPLICE FABRICATED AS PER DRAWING A5A7112 REVISION D. THIS REPAIR IJan 8, 2011 · N605FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201101080080Longeron · crackedMAIN DECK STA 5-0, LONGERON 1 LT, AFT SECTION EDGE FOUND 1 EACH CRACKED, APPROX 0.25 INCH LONG DURING X-RAY INSP. REPAIRED AS PER SRM 53-00-05 FIGURE 202 REVISION 45. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.Jan 8, 2011 · N605FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201101080079Longeron · crackedMAIN DECK STA 5-0, LONGERON 1, RT FWD SECTION EDGE FOUND 1 EA CRACKED, APPROX 0.25 INCH LONG DURING X-RAY INSP. REPAIRED AS PER SRM 53-00-05 FIGURE 202 REPAIR 1 REVISION 45. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.Jan 8, 2011 · N605FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201101080078Longeron · crackedMAIN DECK STA 5-0, LONGERON 1, LT FWD EDGE FOUND 1 EACH CRACKED, APPROX 1.25 INCH LONG DURING X-RAY INSP. REPAIRED AS PER SRM 53-00-05 FIGURE 202 REPAIR 1 REVISION 45. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.Jan 8, 2011 · N605FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201101070070Skin · crackedLT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN XORS 683.4 AND XORS 713.6, FOUND 03 EACH FASTENER HOLES WITH CRACKED INDICATION DURING HFEC OPEN HOLE INSP. REPAIR CARRIED OUT AS PER DRAWING SG11570004 REVISION A. THIS REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6Jan 7, 2011 · N605FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201101070069Skin · crackedRT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN XORS 683.4 AND XORS 713.6, FASTENER HOLES 12 EA. FOUND CRACKED INDICATION DURING HFEC OPEN HOLE INSP. REPAIR CARRIED OUT AS PER DRAWING SG11570004 REVISION A. THIS REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6-2Jan 7, 2011 · N605FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201101060020Vane · delaminatedRT WING INBD T/E FLAP VANE LOWER SURFACE DELAMINATED BETWEEN VANE CTR AND OTBD TRACK. VANE REMOVED AND REPLACED AS PER AMM 27-50-22-4 REVISION 69.0. FLAP VANE ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-22-5 REVISION 69.0 FOUND SATISFACTORY.Jan 6, 2011 · N605FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201101050018Fitting · crackedLT MLG DOOR UPLATCH FITTING FOUND CRACKED. FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 45. FITTING FABRICATED AS PER DRAWING ANB7089 REVISION A. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.Jan 5, 2011 · N605FE · Doug MD11F · Main Landing GearSDR FDEA201101050017Fitting · crackedRT MLG DOOR UPLATCH FITTING FOUND CRACKED. FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 45. FITTING FABRICATED AS PER DRAWING ANB7089 REVISION A. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.Jan 5, 2011 · N605FE · Doug MD11F · Main Landing GearSDR FDEA201101050012Slat Track · crackedRT WING SLAT TRACK NR8 CUT OUT OTBD AREA CRACKED. REPAIRED AS PER E.A. 1-5740-143499. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.Jan 5, 2011 · N605FE · Doug MD11F · Leading Edge DevicesSDR FDEA201101050011Rib · crackedRT WING L/E INBD RIB NR16 CRACKED. RIB REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 45 AND DRAWING ARB7565 REVISION C. THIS REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.Jan 5, 2011 · N605FE · Doug MD11F · Wing, Rib/BulkheadSDR FDEA200904161325Skin · misrepairedFUSELAGE EXISTING SKIN DOUBLER REPAIR (02 LAYER) FOUND AT STATION 621 LONGERON 26 LEFT. FUSELAGE EXISTING SKIN DOUBLER REPAIR AT STATION 621, LONGERON 26 LEFT EVALUATED AND FOUND NOT IN ACCORDANCE WITH SRM REPAIR. EXISTING DOUBLER REPAIR (02 LAYER) AT FUSELApr 16, 2009 · N605FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA200904131271Access Panel · cracked01 FASTENER HOLE FOUND CRACKED INDICATION DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT LEFT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 690 AND STA XORS 700. FASTENER HOLE FOUND CRACKED INDICATION DURING HIGH FREQUENCY EDDY CURRENT OPEApr 13, 2009 · N605FE · Doug MD11F · Wing, Plate/SkinSDR FDEA200904131270Access Panel · cracked04 FASTENER HOLES FOUND CRACKED INDICATION DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION, AT RIGHT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 690 AND STA XORS 700. FASTENER HOLES FOUND CRACKED INDICATION DURING HIGH FREQUENCY EDDY CURRENTApr 13, 2009 · N605FE · Doug MD11F · Wing, Plate/SkinSDR FDEA200904131269Spar Cap · crackedCRACK INDICATION APPROXIMATELY 1 INCH LENGTH FOUND ON RIGHT SIDE OF THE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP. CRACK INDICATION APPROXIMATELY 1 INCH LENGTH FOUND ON RIGHT HAND SIDE OF THE LOWER VERTICAL STABILIZER FORWARD FLANGE Apr 13, 2009 · N605FE · Doug MD11F · Vertical Stabilizer, Spar/RibSDR FDEA200904111265Seat Track · corrodedMAIN DECK CARGO STA 1175 TO STA 1257, X = -75.5 SEAT TRACK FOUND WITH SURFACE CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I, REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.Apr 11, 2009 · N605FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200904111264Seat Track · corrodedMAIN DECK CARGO STA 1301 TO STA 1381, X = 75.5 SEAT TRACK FOUND WITH SURFACE CORROSION.Apr 11, 2009 · N605FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200904111263Seat Track · corrodedMAIN DECK CARGO STA 1276 TO STA 1361, X = -75.5 SEAT TRACK FOUND WITH SURFACE CORROSION.Apr 11, 2009 · N605FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200904111262Longeron Splice · crackedMAIN DECK CARGO STA 1651 LONGERON 13 RIGHT SPLICE DOUBLER FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II, REVISION 40. NEW SPLICE FABRICATED AS PER AFA7181 REVISION E. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.Apr 11, 2009 · N605FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA200904111261Hinge Bracket · corrodedRIGHT WING INBOARD FLAP OUTBOARD HINGE (FLAP MOUNTED) PIVOT ATTACHMENT INBOARD LUG BORE FOUND CORROSION. REPAIRED AS PER EA 1-5750-127827, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.Apr 11, 2009 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200904111260Hinge Bracket · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE (WING MOUNTED) LOWER ATTACHMENT OUTBOARD BORE FOUND CORROSION. REPAIRED AS PER EA 1-5750-127826, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.Apr 11, 2009 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200904111259Hinge Bracket · corrodedLEFT WING OUTBOARD FLAP INBOARD HINGE (WING MOUNTED) PIVOT POINT BORE FOUND CORROSION. REPAIRED AS PER EA 1-5750-127825, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.Apr 11, 2009 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200904111258Hinge Bracket · corrodedLEFT WING OUTBOARD FLAP INBOARD HINGE (WING MOUNTED) ACTUATOR ATTACHMENT OUTBOARD LUG BORE FOUND CORROSION. REPAIRED AS PER E.A. NO. 1-5750-127825, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.Apr 11, 2009 · N605FE · Doug MD11F · Wing, Control Surface Attach Fittings
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