N577FE, cancelled Mar 2, 2024

Service difficulty reports · 256

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 = 'N577FE' AND deregistration_id = 'N577FE-2024-03-02'
  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 FDEA201310022380Window · looseLEFT SIDE COCKPIT ESCAPE ROPE VIEWING DOOR GLASS IS LOOSE. CORRECTLY INSTALLED VIEWING GLASS.Oct 2, 2013 · N577FE · Doug MD11F · Emergency EquipmentSDR FDEA201204241541Skin · misrepairedRT WING NR 5 SLAT AFT SURFACE OTBD LOWER CORNER STA XORS 682 MISREPAIRED. REPAIRED IAW EA 1-5750-160032. CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 114.Apr 24, 2012 · N577FE · Doug MD11F · Leading Edge DevicesSDR FDEA201204241539Skin · misrepairedRT WING NR 8 SLAT UPPER SURFACE STATION XORS 995 MISREPAIRED. REPAIRED IAW EA 1-5750-160031 PART 1. CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 114.Apr 24, 2012 · N577FE · Doug MD11F · Leading Edge DevicesSDR FDEA201204191487Skin · misrepairedNR 2 PYLON EXTERIOR APPROX STA Y = 2334 FOUND MISREPAIRED. REPAIRED IAW EO E1-5100-7-5001B PT1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Apr 19, 2012 · N577FE · Doug MD11F · Nacelle/Pylon, Plate/SkinSDR FDEA201204171449Skin · misrepairedLT WING SKIN AT NR 3 SLAT LOWER SURFACE XORS 372. REPAIRED IAW EA1-5750-159830. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.Apr 17, 2012 · N577FE · Doug MD11F · Leading Edge DevicesSDR FDEA201204161431Skin · misrepairedSKIN AT BS 2147 - 2160, L33L MISREPAIRED. REPAIRED IAW SRM 53-70-01 FIGURE 201 REPAIR 3 REVISION 49 & EO E1-5100-7-5001B PT1. MAJOR REPAIR.Apr 16, 2012 · N577FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201204141399Attach Fitting · crackedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION AROUND STOP DRILL HOLE OF LT NOSE LANDING GEAR TRUNNION FITTING FOUND ONE NEW ADDITIONAL CRACK PROPAGATED FROM THE STOP DRILL HOLE TOWARDS THE LOWER EDGE, APPROX 0.25". REPAIR CARRIED OUT AT LT NLG TRUNNION FITTINApr 14, 2012 · N577FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR FDEA201204121373Longeron · crackedFOUND LONGERON 49 LT FASTENER HOLE (COMMON TO NLG TRUNNION FITTING) CRACKED , APPROX 0.025". LONGERON REMOVED IAW SRM 51-31-01, REV 49. NEW LONGERON FABRICATED IAW DWG ACA 3796 REV A. NEW FABRICATED LONGERON INSTALLED IAW SRM 51-31-01, REV 49. REPAIR CLASSApr 12, 2012 · N577FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201204101337Frame · misrepairedFRAME STA 535 AT LONGERON 19 LT MISREPAIRED. REPAIRED IAW SRM 53-20-07, FIG 202, REPAIR 1, REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Apr 10, 2012 · N577FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201204101335Skin · misrepairedRT WING INBD FLAP UPPER SURFACE MISREPAIRED. REPAIRED IAW SRM 57-00-01, FIG 201, REPAIR 1, REV 49.Apr 10, 2012 · N577FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201204101334Frame · misrepairedCABIN AT FRAME BS 535, LONGERON 23L FOUND MISREPAIRED. REPAIRED IAW SRM 53-20-07, FIG 201 REPAIR 1, REV 49. CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.Apr 10, 2012 · N577FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201204101344Skin · corrodedMAIN DECK UPPER CARGO COMPARTMENT UNDER FLOOR AT CENTER WING TANK BETWEEN BS 1219 TO 1239, "X" = -90 TO "X" = -107.5 FOUND SURFACE CORROSION AT FASTENERS AREA. CORROSION REMOVED IAW SRM 51-21-01, REV 49. ORIGINAL MATERIAL THICKNESS = 0.180", REMAINING THICKNEApr 10, 2012 · N577FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201204101343Skin · corrodedMAIN DECK UPPER CARGO COMPARTMENT UNDER FLOOR AT CENTER WING TANK BETWEEN BS 1219 TO 1239, "X" = -75.25 TO "X" = -90 FOUND SURFACE CORROSION AT FASTENERS AREA. CORROSION REMOVED IAW SRM 51-21-01, REV 49. ORIGINAL MATERIAL THICKNESS = 0.168", REMAINING THICKNApr 10, 2012 · N577FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201204101342Skin · corrodedMAIN DECK UPPER CARGO COMPARTMENT UNDER FLOOR AT CENTER WING TANK BETWEEN STATION 1219 TO STATION 1239, "X" = -75.25. FOUND SURFACE CORROSION AT FASTENERS AREA. CORROSION REMOVED IAW SRM 51-21-01, REV 49. ORIGINAL MATERIAL THICKNESS = 0.171", REMAINING TApr 10, 2012 · N577FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201204101341Skin · corrodedMAIN DECK UPPER CARGO COMPARTMENT, UNDER FLOOR AT CENTER WING TANK BETWEEN STATION 1219 TO STATION 1239, "X" = -27.5 FOUND SURFACE CORROSION AT FASTENERS AREA. CORROSION REMOVED IAW SRM 51-21-01, REV 49. ORIGINAL MATERIAL THICKNESS = 0.175", REMAINING THApr 10, 2012 · N577FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201204101340Skin · corrodedMAIN DECK UPPER CARGO COMPARTMENT, UNDER FLOOR AT CTR WING TANK BETWEEN BS 1219 TO 1239, "X" = -8.5 TO "X = -27.5. FOUND SURFACE CORROSION AT FASTENERS AREA. CORROSION REMOVED IAW SRM 51-21-01, REV 49. ORIGINAL MATERIAL THICKNESS = 0.182", REMAINING THICKNApr 10, 2012 · N577FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201204101339Longeron · corrodedCENTER CARGO COMPARTMENT, BILGE AREA BS 1646 LONGERON 50 LT FOUND WITH SURFACE CORROSION. REPAIR CARRIED OUT AT CENTER CARGO COMPARTMENT BILGE AREA STA 1646, LONGERON 50L IAW EA 1-5310-159838. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.Apr 10, 2012 · N577FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201204101338Longeron · corrodedCENTER CARGO COMPARTMENT BS 1676 LONGERON 51 LT FOUND WITH SURFACE CORROSION. REPAIRED IAW SRM 53-00-05, FIG 201, REPAIR 1, REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.Apr 10, 2012 · N577FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201204101333Skin · crackedLOWER VERTICAL STABILIZER FOUND RT SIDE REAR CENTER SPAR TO REAR SPAR LOWER PANEL CRACKED. REPAIR CARRIED OUT IAW SRM 55-30-02, FIG 201, REPAIR 2, REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114. NR 2 ENGINE FIRE DETECTION CONTROL UNIT CARRIEDApr 10, 2012 · N577FE · Doug MD11F · Vertical Stabilizer, Plate/SkinSDR FDEA201204101332Skin · corrodedAFT ACCESSORY COMPARTMENT, FOUND CORROSION ON RT SKIN BS 2163 BODY FAIRING CUTOUT LOCATION. CORROSION REMOVED IAW SRM 51-21-01, REV 49. ORIGINAL THICKNESS: 0.95", MATERIAL REMOVED: 0.80", REMAINING 0.015" AND FOUND EXCEED LIMIT IAW SRM 53-70-01, FIG 201, REApr 10, 2012 · N577FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201204091326Longeron · corrodedCENTER ACCESSORY COMPARTMENT STA 6-95, LONGERON 43 RT FOUND WITH CORROSION. REPAIRED IAW EA 1-5310-157171, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.Apr 9, 2012 · N577FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201204091324Bushing · wornRT WING (FLAP SIDE) OTBD FLAP, OTBD HINGE, OTBD PIVOT HOLE BUSHING FOUND WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED DIAMETER 1.152" AND FOUND EXCEED LIMIT IAW CMM 57-52-04, REV 72. MAXIMUM ALLOWABLE DIAMETER 1.150". REPAIR ACCOMPLISHEDApr 9, 2012 · N577FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201204091323Hinge Fitting · corrodedRT WING (WING SIDE) OTBD FLAP, OTBD HINGE, OTBD ACTUATOR HOLE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09, REV 72. EXISTING BORE DIAMETER 1.222". FINAL BORE DIAMETER 1.246", MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR CARRIED OUT EA 1-Apr 9, 2012 · N577FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201204091322Hinge Fitting · corrodedRT WING (WING SIDE) OTBD FLAP, OTBD HINGE, INBD ACTUATOR HOLE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72. EXISTING BORE DIAMETER = 1.2215", FINAL BORE DIAMETER 1.246", MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR ACCOMPLISHED EApr 9, 2012 · N577FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201204091321Hinge Fitting · corrodedRT WING (WING SIDE) OTBD FLAP, OTBD HINGE, LOWER MOUNT, OTBD HOLE FOUND CORRODED. BUSHING REMOVED IAW CMM 20-20-07, REV 72. OTBD BORE REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72. EXISTING BORE DIAMETER = 0.597", FINAL BORE DIAMETER 0.612", MApr 9, 2012 · N577FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201204091320Hinge Fitting · corrodedRT WING (WING SIDE) OTBD FLAP, OTBD HINGE LOWER MOUNT, INBD HOLE FOUND CORRODED. BUSHING REMOVED IAW CMM 20-20-07, REV 72. INBOARD HOLE REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72. EXISTING BORE DIAMETER = 0.581", FINAL BORE DIAMETER 0.612",Apr 9, 2012 · N577FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201204091319Hinge Fitting · corrodedLT WING (WING SIDE) OTBD FLAP, INBD HINGE, OTBD ACTUATOR HOLE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08, REV 72. ORIGINAL BORE DIAMETER = 1.2295", FINAL BORE DIAMETER 1.236", MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR ACCOMPLISHED EApr 9, 2012 · N577FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201204091318Bushing · wornLT WING (WING SIDE) OTBD FLAP, INBD HINGE, INBD ACTUATOR HOLE BUSHING FOUND WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED, DIAMETER = 1.231" AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08, REV 72. MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR ACCOMPApr 9, 2012 · N577FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201204091317Hinge Fitting · corrodedLT WING (WING SIDE) OTBD FLAP, INBD HINGE LOWER MOUNT OTBD HOLE FOUND CORRODED. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08, REV 72. EXISTING HOLE DIAMETER :0.707", FINAL HOLE DIAMETER 0.713", MAXIMUM ALApr 9, 2012 · N577FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201204091316Hinge Fitting · corrodedLT WING (WING SIDE) OTBD FLAP, INBD HINGE SIDE LOAD FITTING SURFACE FOUND CORRODED. REWORKED IAW CMM 20-11-02, REV 72. UPPER EXISTING THICKNESS: 0.400", MATERIAL REMOVED: 0.004", REMAINING THICKNESS: 0.396". LOWER EXISTING THICKNESS: 0.387", MATERIAL REMOVApr 9, 2012 · N577FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201204091314Bushing · wornLT WING (WING SIDE) OTBD FLAP, OTBD HINGE, INBD ACTUATOR HOLE BUSHING WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE DIAMETER 1.251" AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72. MAXIMUM ALLOWABLE DIAMETER: 1.220". REPAIR ACCOMPLISHED EA 1-5750-Apr 9, 2012 · N577FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201204091312Hinge Fitting · corrodedLT WING (WING SIDE) OTBD FLAP, OTBD HINGE SIDE LOAD FITTING SURFACE FOUND CORROSION. REWORKED IAW CMM 20-11-02, REVISION 72. UPPER EXISTING THICKNESS: 0.425", MATERIAL REMOVED: 0.009", REMAINING THICKNESS: 0.416". LOWER EXISTING THICKNESS: 0.413", MATERIALApr 9, 2012 · N577FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201204091311Hinge Fitting · corrodedLT WING (WING SIDE) OTBD FLAP, OTBD HINGE, SIDE LOAD FITTING LOWER HOLE FOUND CORRODED. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE REWORKED AND FOUND EXCEEDED LIMIT CMM 57-44-09, REV 72. EXISTING HOLE DIAMETER 0.389", FINAL HOLE DIAMETER 0.408", MAXIMUMApr 9, 2012 · N577FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201204091310Hinge Fitting · corrodedLT WING (WING SIDE) OTBD FLAP, OTBD HINGE SIDE LOAD FITTING UPPER HOLE FOUND CORRODED. BUSHING REMOVED IAW CMM 20-20-07, REV 72. UPPER HOLE REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72. EXISTING HOLE DIAMETER 0.389", FINAL HOLE DIAMETER 0.408",Apr 9, 2012 · N577FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201204091309Hinge Fitting · corrodedLT WING (WING SIDE) OTBD FLAP, OTBD HINGE LOWER MOUNT, OTBD HOLE FOUND CORRODED. BUSHING REMOVED IAW CMM 20-20-07, REV 72. OTBD BORE REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72. EXISTING HOLE DIAMETER 0.581", FINAL HOLE DIAMETER 0.596", MAXIMApr 9, 2012 · N577FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201204091308Hinge Fitting · corrodedLT WING (WING SIDE) OTBD FLAP, OTBD HINGE LOWER MOUNT INBD HOLE FOUND CORRODED. BUSHING REMOVED IAW CMM 20-20-07, REV 72. INBD BORE REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72. EXISTING HOLE DIAMETER 0.580", FINAL HOLE DIAMETER 0.5975", MAXIApr 9, 2012 · N577FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201204091307Bushing · wornRT WING (WING SIDE) OTBD FLAP, INBD HINGE, OTBD ACTUATOR HOLE BUSHING WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED, DIAMETER 1.252" FOUND EXCEED LIMIT IAW CMM 57-44-08, REV 72. MAXIMUM ALLOWABLE DIAMETER: 1.220". REPAIR ACCOMPLISHED IAW Apr 9, 2012 · N577FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201204091306Hinge Fitting · damagedRT WING (WING SIDE) OTBD FLAP, INBD HINGE, INBD ACTUATOR HOLE BUSHING WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED DIAMETER 1.253" AND FOUND EXCEED LIMIT IAW CMM 57-44-08, REV 72. MAXIMUM ALLOWABLE DIAMETER 1.220", REPAIR ACCOMPLISHED IAW EApr 9, 2012 · N577FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201204091305Hinge Fitting · corrodedRT WING (WING SIDE) OTBD FLAP, INBD HINGE LOWER MOUNT INBD HOLE FOUND CORRODED. BUSHING REMOVED IAW CMM 20-20-07, REV 72. LOWER MOUNT INBD BORE REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08, REV 72. EXISTING BORE DIAMETER 0.705", FINAL BORE DIAMETER 0.7Apr 9, 2012 · N577FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201204091304Hinge Fitting · corrodedRT WING (WING SIDE) OTBD FLAP, INBD HINGE LOWER MOUNT OTBD HOLE, FOUND CORRODED. BUSHING REMOVED IAW CMM 20-20-07, REV 72. LOWER MOUNT OTBD BORE REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08, REV 72. EXISTING BORE DIAMETER 0.708", FINAL BORE DIAMETER 0.7Apr 9, 2012 · N577FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201204091303Hinge Fitting · corrodedRT WING (WING SIDE) OTBD FLAP, INBD HINGE SIDE LOAD FITTING SURFACE, FOUND CORRODED. REWORKED IAW CMM 20-11-02 REV 72. UPPER EXISTING THICKNESS: 0.412", MATERIAL REMOVED: 0.005", REMAINING THICKNESS: 0.407". LOWER EXISTING THICKNESS: 0.403", MATERIAL REMOApr 9, 2012 · N577FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201204091301Hinge Fitting · damagedLEFT WING (FLAP SIDE), INBD FLAP OTBD HINGE, OTBD PIVOT HOLE, FOUND STEP HOLE. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED, OTBD LUG DIAMETER 1.254", OTBD STRAP DIAMETER 1.190" AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72. MAXIMUM ALLOWABLE DApr 9, 2012 · N577FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201204091300Hinge Fitting · damagedLEFT WING (FLAP SIDE) INBD FLAP, OTBD HINGE, INBD PIVOT HOLE, FOUND STEP HOLE. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURE, INBD LUG, DIAMETER 1.283", INBD STRAP DIAMETER 1.217" AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72. MAXIMUM ALLOWABLE DIApr 9, 2012 · N577FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201204091299Hinge Fitting · damagedRT WING (FLAP SIDE) INBD FLAP, OTBD HINGE, OTBD PIVOT HOLE, FOUND STEP HOLE. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED, OTBD LUG DIAMETER 1.250", OTBD STRAP DIAMETER 1.21" AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72. MAXIMUM ALLOWABLE DIAMApr 9, 2012 · N577FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201204091298Hinge Fitting · damagedRT WING (FLAP SIDE) INBD FLAP, OTBD HINGE, INBD PIVOT HOLE FOUND STEP HOLE. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURE, INBD LUG DIAMETER 1.252 IN, INBD STRAP DIAMETER 1.218" AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72. MAXIMUM ALLOWABLE DIAApr 9, 2012 · N577FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201204071285Skin · crackedHIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP ON LT WING FUEL TANK LOWER ACCESS DOOR PANEL NR 536AB CUTOUT AND FOUND CRACK INDICATION ON 04 EACH FASTENER HOLES. REPAIR CARRIED OUT IAW EA 1-5710-157169 PART 1. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REVISION 11Apr 7, 2012 · N577FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201204071284Skin · crackedHIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP ON RT WING FUEL TANK LOWER ACCESS DOOR PANEL NR 636AB CUTOUT AND FOUND CRACK INDICATION ON 06 EACH FASTENER HOLES. REPAIR CARRIED OUT IAW EA 1-5710-157168 PART 1. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REVISION 11Apr 7, 2012 · N577FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201204061275Skin · crackedRIGHT WING LOWER FIXED L/E AT REFUELING PANEL CUTOUT INBD FORWARD CORNER AREA FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02. REPAIR 7 FIG 201 REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 114.Apr 6, 2012 · N577FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201204051266Skin · misrepairedLT WING DROOP L/E UPPER SURFACE FOUND MISREPAIRED IAW SRM 57-40-01, REPAIR 5, FIGURE 201. REPAIRED IAW EA 1-5730-159836, CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.Apr 5, 2012 · N577FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201204051270Skin · crackedRT WING FIXED L/E LOWER SURFACE AT NR 14 SLAT TRACK LOWER CUTOUT FOUND CRACKED. REPAIR CARRIED OUT AT RT WING FIXED L/E LOWER SURFACE AT NR 14 SLAT TRACK LOWER CUTOUT IAW SRM 57-40-02. REPAIR 7, FIG 201, REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REApr 5, 2012 · N577FE · Doug MD11F · Wing, Plate/Skin
Back to N577FE, cancelled Mar 2, 2024