N595FE

Service difficulty reports · 389

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 = 'N595FE' 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 FDEA201208072873Skin · misrepairedRT WING INBD FLAP UPPER SKIN MISREPAIRED. REPAIRED IAW EA 1-5750-160994. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.Aug 7, 2012 · N595FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201208012801Skin · misrepairedSKIN BS 495 TO 515 BETWEEN LONGERON 45 TO 46 LT MISREPAIRED. REPAIRED AS PER SRM 53-00-01 FIGURE 201 REPAIR 1 REV. 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.Aug 1, 2012 · N595FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201207302747Skin · misrepairedLT WING L/E TELSCOPIC DUCT CUTOUT MISREPAIRED. REPAIRED AS PER SRM 57- 40-01 REPAIR 10 FIGURE 201 REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.Jul 30, 2012 · N595FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201207282728Longeron Splice · crackedCENTER CARGO BETWEEN STA 5-113 AND STA 1561 LONGERON 47 LT SPLICE END, SUSPECTED CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 50. NEW SPLICE FABRICATED BY MACHINING AS PER DRAWING A5A7114 REVISION J. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-1Jul 28, 2012 · N595FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201207282727Longeron Splice · crackedCENTER CARGO LONGERON 38 LT BETWEEN STA 5-113 AND STA 1561 , FOUND LONGERON SPLICE CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.Jul 28, 2012 · N595FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201207282726Longeron Splice · crackedCENTER CARGO BETWEEN STA 5-113 AND STA 1561 LONGERON 43 LT SPLICE END, FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 50. NEW SPLICE FABRICATED BY MACHINING AS PER DRAWING A5A7116 REVISION D. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 RJul 28, 2012 · N595FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201207282725Longeron Splice · crackedCENTER CARGO BETWEEN STA 5-113 AND STA 1561, LONGERON 37 RT SPLICE END, SUSPECTED CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 50. NEW SPLICE FABRICATED BY MACHINING AS PER DRAWING A5A7114 REVISION: E. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-Jul 28, 2012 · N595FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201207282724Longeron Splice · crackedCENTER CARGO BETWEEN BS 5-113 AND 1561 LONGERON 41 RT SPLICE END, SUSPECTED CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 50 NEW SPLICE FABRICATED BY MACHINING AS PER DRAWING A5A7115 REVISION: D. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVIJul 28, 2012 · N595FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201207272715Skin · misrepairedAGING AIRCRAFT - EXISTING REPAIR AT RT FUSELAGE SKIN AT STA 1830 BETWEEN LONGERONS 37 AND 38 MISREPAIRED. REPAIRED IAW EA 1-5330-160992. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.Jul 27, 2012 · N595FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201207272718Skin · crackedLEFT WING L/E NR 8 SLAT LOWER SURFACE MID AREA FOUND CRACKED. REPAIRED AS PER SRM 57-40-01 FIGURE 201 REPAIR 3 REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.Jul 27, 2012 · N595FE · Doug MD11F · Leading Edge DevicesSDR FDEA201207272717Skin · corrodedRT FUSELAGE SKIN FROM STA 2027 TO 2024 (BENEATH FAIRING NR 341CF), FOUND CORROSION. CORROSION REMOVED IAW SRM 51-21-01, REV 50 ORIGINAL THICKNESS: 0.095 INCH, MATERIAL REMOVED: 0.085 INCH, REMAINING THICKNESS : 0.010 INCH AND FOUND EXCEEDED LIMIT IAW SRM 53Jul 27, 2012 · N595FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201207262699Skin · misrepairedAGING AIRCRAFT -EXISTING REPAIR AT RT FUSELAGE SKIN AT BS 488 BETWEEN LONGERONS 28 AND 29 MISREPAIRED. REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR 7, REV 50 EO 1-5100-7-5001B, PART 1. REPAIR CLASSIFIED MAJOR AS GMM 6-2-100, REV 115.Jul 26, 2012 · N595FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201207262698Frame · misrepairedBS 535 LONGERON 25LT FRAME MISREPAIRED. REPAIRED IAW SRM 53-20-07, FIG 201. REPAIR 1, REVISION 50 EO 1-5100-7-5001B PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 115.Jul 26, 2012 · N595FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201207262697Stringer · misrepairedBS 535, LONGERON 21L MISREPAIRED. REPAIRED IAW SRM 53-20-07, FIG 202, REPAIR 1, REV 50 EO 1-5100-7-5001B, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.Jul 26, 2012 · N595FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201207262696Frame · dentedFRAME BS 1701, LONGERON 12R FOUND DENTED. REPAIRED AS PER SRM 53-00-07, FIGURE 201, REPAIR 2, REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100, REVISION 115.Jul 26, 2012 · N595FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201207262695Frame · dentedFRAME BS 1721, LONGERON 12L FOUND DENTED. REPAIRED AS PER SRM 53-00-07, FIGURE 201, REPAIR 2, REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100, REVISION 115.Jul 26, 2012 · N595FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201207262694Frame · dentedFRAME BS 1641, LONGERON 12L FOUND DENTED. REPAIRED AS PER SRM 53-00-07, FIGURE 201, REPAIR 2, REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.Jul 26, 2012 · N595FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201207262693Trunnion · crackedNLG RT TRUNNION FITTING CRACKED. REPAIR CARRIED OUT AS PER SRM 53-10-14, FIGURE 202, REPAIR 2, REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115Jul 26, 2012 · N595FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR FDEA201207262692Trunnion · crackedNOSE LANDING GEAR LT TRUNNION FITTING CRACKED. REPAIR CARRIED OUT AS PER SRM 53-10-14, FIGURE 202, REPAIR 2, REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115Jul 26, 2012 · N595FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR FDEA201207262691Cargo Track · damagedMAIN DECK CARGO TRACK AT BS 1421, X=8 FOUND CROWN WITH A HOLE ELONGATED. REPAIRED BY SECTIONAL CARGO TRACK REPLACEMENT FROM BS 1411 TO 1471 X =8 AS PER SRM 53-00-52 FIGURE 201 REPAIR 1, REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100, REVISION 115Jul 26, 2012 · N595FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201207262690Seat Track · damagedMAIN DECK CARGO TRACK AT BS 1541, X=-8 FOUND CROWN HAS A HOLE ELONGATED. REPAIRED BY SECTIONAL CARGO TRACK REPLACEMENT FROM BS 1531 TO 1571 X =-8 AS PER SRM 53-00-52 FIGURE 201, REPAIR 1 REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.Jul 26, 2012 · N595FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201207262689Skin · crackedRIGHT WING OTBD L/E PANEL NR 619CB CUTOUT OTBD FORWARD CORNER FOUND CRACKED. REPAIR CARRIED OUT AT RIGHT HAND WING OUTBOARD LEADING EDGE PANEL 619CB CUTOUT OUTBOARD FORWARD CORNER AS PER SRM 57-40-02 REPAIR 7 FIGURE 201 REVISION 50 REPAIR CLASSIFIED MAJORJul 26, 2012 · N595FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201207262688Vane · delaminatedLT WING INBD FLAP VANE LOWER SURFACES BETWEEN INBD AND MID TRACKS, FOUND DELAMINATED. REMOVED AND REPLACED LEFT HAND WING INBOARD FLAP VANE AS PER AMM 27-50-22-4 REVISION 72.0. FLAP VANE ADJUSTMENTS AND TEST CARRIED OUT AS PER AMM 27-50-22-5 REVISION 72.0. Jul 26, 2012 · N595FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201206112181Holder · out of positionFOUND 1R DOOR EVACUATION SLIDE REMOTE PUSH TO TEST SWITCH INOPERATIVE. FOUND PRESSURE INDICATOR LIGHT HOLDER WAS OUT OF POSITION. INSTALLED LIGHT HOLDER AND OPS CHECKED NORMAL IAW MM 25-61-04-4, ACFT OK FOR SERVICE.Jun 11, 2012 · N595FE · Doug MD11F · Escape SlideSDR FDEA201010073971Control Panel · odorPROIR TO STARTUP F/O AND CAPT HEARD WHAT SOUNDED LIKE ELECTRICAL ARCING AND SPARKING. THEN SMELLED ELECTRICAL SMOKE IN THE COCKPIT. OVERHEAD SWITCH ONLY LIGHTING / CIRCUIT BREAKER WAS POPPED. RESET OVERHEAD PANEL LIGHTING CIRCUIT BREAKER. NO FAULTS NOTED OOct 7, 2010 · N595FE · Doug MD11F · Flight Compartment LightingSDR FDEA201009063298Frame · crackedUPPER AFT FUSELAGE FRAME CLIP AT CANT STATION Y = 2069.44, CRACKED APPROX 1 INCH IN LENGTH. R & R IAW SRM 51-31-01, REV 44. THIS REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.Sep 6, 2010 · N595FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201009043274Web · crackedLOWER VERTICAL STABILIZER AT PANEL NR 363QL INTERIOR AREA, WEB FOUND CRACKED. REPAIR CARRIED OUT AS PER SRM 55-30-02 FIGURE 201 REPAIR 2, REVISION 44 AND EA 1-5530-143725, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 111.Sep 4, 2010 · N595FE · Doug MD11F · Vertical StabilizerSDR FDEA201009033255Skin · crackedFUSELAGE EXTERIOR SKIN CUTOUT AROUND APU EXHAUST DOOR ACTUATOR FOUND CRACK ABOUT 0.5 INCH. FUSELAGE EXTERIOR SKIN CUTOUT AROUND APU EXHAUST DOOR ACTUATOR, WELDING REPAIR CARRIED OUT AS PER E.A. 1-5330-143414. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100, REVISep 3, 2010 · N595FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201009023252Skin · crackedLEFT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN XORS 683.4 AND XORS 713.6, 18 EACH FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION. LEFT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN XORS 683.4 AND XORS 713.6, 18 EACH FASTENER HOLES CASep 2, 2010 · N595FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201009023251Skin · crackedRIGHT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN XORS 683.4 AND XORS 713.6, 24 EACH FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION. CARRIED OUT REPAIR AS PER E.A. 1-5710-143728. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100, REVISION 1Sep 2, 2010 · N595FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201009023248Wedge · delaminatedLEFT WING OUTBOARD FLAP TRAILING EDGE WEDGE INBOARD EDGE LOWER SURFACE. FOUND DELAMINATION. REPAIRED AS PER E.A. 1-5750-132474. REPAIR CLASSISIFIED AS MINOR PER GMM 6-2-100, REVISION 111.Sep 2, 2010 · N595FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201008313213Seat Track · corrodedMAIN DECK CARGO - SEAT TRACK FROM STA 5-53 TO STA 5-73, "X" =8 FOUND SEVERAL LOCATIONS CORRODED. MAIN DECK CARGO - CORRODED SEAT TRACK FROM STA 5-53 TO STA 5-73, "X" =8 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 5-0 TO STA 5-123, "X" =8, AS PER Aug 31, 2010 · N595FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201008303202Skin · dentedRT WING - INBD FLAP LOWER SURFACE FOUND DENT AT XIFH 198. DENT AREA TRIMMED OUT AND FABRICATED NEW SKIN AND DOUBLER AS PER SRM 57-50-01, FIGURE 201 REPAIR 2, REVISION 44. NEW SKIN AND DOUBLER INSTALLED AS PER SRM 57-50-01 FIGURE 201, REVISION 44. REPAIRAug 30, 2010 · N595FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201008303201Skin · crackedRIGHT WING - NR 3 LEADING EDGE SLAT TELESCOPIC DUCT CUT-OUT INBOARD CORNER UPPER EXTERIOR SKIN FOUND CRACKED AT XOS 464. RIGHT HAND WING - NR 3 LEADING EDGE SLAT TELESCOPIC DUCT CUT-OUT INBOARD CORNER, CRACKED UPPER EXTERIOR SKIN AT XOS 464 TRIMMED OUT AS PAug 30, 2010 · N595FE · Doug MD11F · Leading Edge DevicesSDR FDEA200912044358Pseu · malfunctionedRT MAIN GEAR UNSAFE ON PRIMARY INDICATOR AFTER GEAR DOWN ON APPROACH AT MEM SECONDARY INDICATOR WAS GREEN. WENT MISSED APPROACH LEAVING GEAR DOWN AND RAN THE GEAR UNSAFE INDICATION WITH GEAR HANDLE DOWN, FOLLOWED BY NORMAL LANDING MEM RWY 36R. REMOVED ANDec 4, 2009 · N595FE · Doug MD11F · Landing Gear Position and WarningSDR FDEA200902060473Skin · damagedLEFT LOWER FUSELAGE EXTERIOR SKIN AT STA 759 TO STA 799, BETWEEN LONGERON 42L TO LONGERON 46L FOUND LIGHTNING STRIKE MARK. AREA REWORKED AND FOUND 2 CRACKS EVIDENT AFTER FPI CARRIED OUT. REPAIR CARRIED OUT AT CRACKED SKIN AS PER SRM 53-20-20-00 FIG.2 SHT 21Feb 6, 2009 · N595FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA200902060472Skin · crackedLEFT LOWER FUSELAGE EXTERIOR SKIN AT STA 735 TO STA 759, BETWEEN LONGERON 42L TO LONGERON 46L FOUND LIGHTNING STRIKE MARK. AREA FOUND CRACKED AFTER FPI WAS CARRIED OUT. REPAIR CARRIED OUT AT CRACKED SKIN AS PER SRM 53-20-00 FIGURE 2 SHEET 21 VOLUME I. REPAIRFeb 6, 2009 · N595FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA200902060471Fuel Tank · corrodedMAIN DECK, CENTER WING TANK AT STA 1230 X = -100 FOUND CORROSION. REPAIRED AS PER E.A. 1-5710-127758, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Feb 6, 2009 · N595FE · Doug MD11F · Fuel StorageSDR FDEA200902060470Fuel Tank · corrodedMAIN DECK, CENTER WING TANK AT STA 1230 X = -79 FOUND CORROSION. REPAIRED AS PER E.A.1-5710-127758, THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.Feb 6, 2009 · N595FE · Doug MD11F · Fuel StorageSDR FDEA200902060469Fuel Tank · corrodedMAIN DECK, CENTER WING TANK AT STA 1230 X = -65 FOUND CORROSION. REPAIRED AS PER E.A. 1-5710-127758, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Feb 6, 2009 · N595FE · Doug MD11F · Fuel StorageSDR FDEA200902040458Skin · delaminatedRIGHT WING, OUTBOARD AILERON TRAILING EDGE MIDDLE SECTION FOUND DELAMINATION. REPAIRED AS PER DRAWING SG11570003. WEIGHT AND BALANCE CARRIED OUT, ACTUAL = 31.00 IN-LBS, AS PER CMM 57-51-03. REFER TO WORKCARD 27C1306 FOR OPERATIONAL CHECK. REPAIR CLASSIFIEDFeb 4, 2009 · N595FE · Doug MD11F · AileronsSDR FDEA200902040457Skin · chafedFORWARD CARGO, DOOR CUT-OUT SKIN AT STA 888, LONGERON 40R FOUND CHAFED. REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG. 17 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Feb 4, 2009 · N595FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA200902030435Seat Track · crackedCABIN, SEAT TRACK AT STA 635 X = 47.5 FOUND CRACKED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Feb 3, 2009 · N595FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200902030434Seat Track · crackedCABIN, SEAT TRACK AT STA 635 X = 27.5 FOUND CRACKED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 625 TO STA 665, X = 27.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Feb 3, 2009 · N595FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200902030433Frame · dentedMAIN DECK, FRAME AT RIGHT STA 1661 LONGERON 12 FOUND WITH DENT. REPAIRED AS PER SRM 53-30-00 FIG.1 VOL I. REPETITIVE INSPECTION REQUIRED, INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE AT 9,500 CYCLES AS PER SRM 53-30-00 FIG.1 VOL.I. REPAIR CLASSIFIED ASFeb 3, 2009 · N595FE · Doug MD11F · Fuselage Main, FrameSDR FDEA200902030432Frame · dentedMAIN DECK, FRAME AT RIGHT STA 1681 LONGERON 12 FOUND DENTED. REPAIRED AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPETITIVE INSPECTION REQUIRED, INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES AS PER SRM 53-30-00 FIGURE 1 VOLUME I. RFeb 3, 2009 · N595FE · Doug MD11F · Fuselage Main, FrameSDR FDEA200902030431Vane · delaminatedLEFT WING, INBOARD FLAP VANE LOWER SURFACE INBOARD SIDE FOUND DELAMINATION. REMOVED AND REPLACED AS PER AMM 27-50-22-4. ADJUSTMENT CARRIED OUT AS PER AMM 27-50-22-5 FOUND SATISFACTORY.Feb 3, 2009 · N595FE · Doug MD11F · Trailing Edge FlapsSDR FDEA200902020428Hinge Bracket · corrodedLEFT WING, AIRCRAFT SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT FORWARD MOUNTING SURFACE FOUND CORROSION. REWORKED AS PER CMM 57-44-08 REPAIR 1-1. WITHIN DRAWING ARC0502 BLUE PRINT TOLERANCE = 0.436", 0.060" & - 0.015". NEW SHIM FABRICATED AND INSTALLED ASFeb 2, 2009 · N595FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200902020427Hinge Bracket · corrodedLEFT WING, AIRCRAFT SIDE OUTBOARD FLAP INBOARD HINGE LOWER BARREL NUT HOLE FOUND CORROSION. REPAIRED AS PER EA 1-5750-127444, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Feb 2, 2009 · N595FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200902020426Hinge Bracket · corrodedLEFT WING, AIRCRAFT SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE FOUND CORROSION. REPAIRED AS PER EA 1-5750-127444, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.Feb 2, 2009 · N595FE · Doug MD11F · Wing, Control Surface Attach Fittings
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