N608FE

Service difficulty reports · 370

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 = 'N608FE' 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 FDEA201304180803Skin · delaminatedRIGHT OTBD AILERON INBD T/E UPPER SURFACE FROM XOA 841 TO XOA 860 FOUND DELAMINATED. EA 1-5750-166115 AND SRM 57- 60-80 REPAIR 1 PARA. 4A HAS BEEN COMPLIED WITH. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 116.Apr 18, 2013 · N608FE · Doug MD11F · AileronsSDR FDEA201304180804Trunnion · crackedHIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON STOP DRILL IN THE LT NLG TRUNNION FITTING AND FOUND CRACK PROPAGATION FROM THE SLOT OUT APPROX .2500 INCHES IN LENGTH. TRUNNION REPAIRED IAW SRM 53-10-14, FIG 202, REPAIR 2, REV 52. REPAIR CLASSIFIED MAApr 18, 2013 · N608FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR FDEA201207252669Charger · malfunctionedEMERGENCY POWER TEST FAIL NOTED ON POST FLIGHT INSP. EPCU SHOWS BATTERY/INTFC UNDER CURRENT FAULTS AND LAST TWO FLIGHT LEGS. COMPLIED WITH FIM 24-30-03-00 BATTERY VOLTAGE FOUND TO BE WITHIN LIMITS. EMERGENCY POWER TEST ATTEMPTED THREE TIMES, TWO FAILED, PJul 25, 2012 · N608FE · Doug MD11F · Battery/Charger SystemSDR FDEA201112285448Warning Horn · false activationON DEPARTURE, AFTER FLAP RETRACTED, RECEIVED A MLG AURAL WARNING. RETRACTED SLATS & WARNING CONTINUED. CHECKED CONFIGURATION PAGE & ALL INDICATIONS OF SLATS/FLAPS & GEAR NORMAL. NO GEAR LIGHTS DISPLAYED. CYCLED GEAR & WARNING CONTINUED. CYCLED FLAPS TO 28 & Dec 28, 2011 · N608FE · Doug MD11F · Landing Gear Position and WarningSDR FDEA201112285449Pseu · failedAFTER T/O, RETRACTED GEAR AND FLAPS. WHEN FLAPS CAME UP GOT GEAR HORN. GEAR SHOWED UP AND SAFE. SLATS EXTENDED, FLAPS UP. RECYCLED GEAR AND FLAPS AND GOT SAME RESULT. R & R PSEU IAW MM 31-71-01-2-0 AND OPS CHECKED NORMAL.Dec 28, 2011 · N608FE · Doug MD11F · Landing Gear Position and WarningSDR FDEA201106022098Switch · inoperativeDURING MX PREFLIGHT, FOUND L1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST INDICATION INOPERATIVE. RELEASED FOR SERVICE IAW MEL: 25-61-02. REPLACED ITS BATTERIES AND BULBS, NO HELP. R & R TEST LAMP SWITCH IAW SMP. OPS CHECKED GOOD.Jun 2, 2011 · N608FE · Doug MD11F · Escape SlideSDR FDEA201105261991Hinge Fitting · wornUPPER CARGO DOOR HINGE FITTING ASSEMBLY ON FUSELAGE AT MOST FWD 03 EA HOLES WORN READ 0.425". REPAIR CARRIED OUT AS PER SRM 52-30-16 REV46. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV 112.May 26, 2011 · N608FE · Doug MD11F · Fuselage, Door HingeSDR FDEA201105261993Hinge Fitting · wornUPPER CARGO MOST FWD HINGE FITTING ASSEMBLY LOPE HOLES WORN, READ 0.430" UPPER CARGO DOOR MOST FWD HINGE FITTING ASSEMBLY WORN LOPE HOLES AREA REPAIRED AS PER EA1-5230-143587 TITLE: DOORS - MAIN DECK CARGO DOOR FORWARD HINGE SUPPORT - REPAIR. REPAIR CLASSIMay 26, 2011 · N608FE · Doug MD11F · Fuselage, Door HingeSDR FDEA201105251981Bracket · damagedCENTER CARGO FOUND STRUCK DAMAGE ON THE STA 1721 CEILING SUPPORT INSTALLATION AT STA 1741 AND 1761 RESPECTIVELY. DAMAGED BRACKET AT STA 1741 AND 1761 REMOVED AND REPLACED WITH NEW FABRICATED BRACKET IAW DWG APA0161-259 FOR STA 1741 AND APA 0161-227 FOR STA 17May 25, 2011 · N608FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201105161843Skin · crackedHFEC OPEN HOLE INSP CARRIED OUT AND FOUND 3 EA HOLES WITH CRACK INDICATION AT RT WING LOWER SKIN PANELS OUTER WING ACCESS DOOR CUT-OUT AT BTW XORS=683.400 AND XORS=713.600. REPAIR CARRIED OUT AT RT WING LOWER SKIN PANEL OUTER WING ACCESS DOOR CUTOUT AT BTW XORMay 16, 2011 · N608FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201105161842Skin · crackedHFEC OPEN HOLE INSP CARRIED OUT AND FOUND 7 EA HOLES WITH CRACKED INDICATION AT LT WING LOWER SKIN PANELS OUTER WING ACCESS DOOR CUT-OUT AT BTW XORS=683.400 AND XORS=713.600. REPAIR CARRIED OUT AT LT WING LWR SKIN PANEL OUTER WING ACCESS DOOR CUTOUT BETWEEN XOMay 16, 2011 · N608FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201105121818Seat Track · corrodedUPON REMOVAL OF FLOOR PANEL NR 282HF SEAT TRACK FOUND CORROSION AT STATION 1701 X=-75. REPAIRED SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1671 TO STA 1711 X=-75 AS PER SRM 53-00-52 FIG 201 REPAIR 1 REV 46. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.May 12, 2011 · N608FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201105121815Seat Track · damagedMAIN DECK SEAT TRACK CROWN DAMAGED AT STATION 635 X= 47.5. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 605 TO STA 645 X= 47.5 AS PER SRM 53-00-52 FIG 201 REPAIR 1 REV 46. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.May 12, 2011 · N608FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201105121810Seat Track · damagedMAIN DECK SEAT TRACK CROWN DAMAGED AT STATION 635 X= 27.5. REPAIRED BY SECTION SEAT TRACK REPLACEMENT FROM STA 625 TO STA 665 X= 27.5 AS PER SRM 53-00-52 FIG 201 REPAIR 1 REV 46. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 112.May 12, 2011 · N608FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201006021780Adc · malfunctionedDURING CRUISE FLIGHT AUTOPILOT CONNECTED RECEIVED STALL INDICATION (STICKSHAKER) AND RED IAS. IAS ON BOTH AIRSPEED TAPE READ APPROX 280KTS. STANBY AIRSPEED WAS 220 KTS. ACCOMPLISHED ERRACTIC AIRSPEED CHECKLIST AND FADEC ALT. CDG U PERFORMED STICK SHAKER AJun 2, 2010 · N608FE · Doug MD11F · Air Data ComputerSDR FDEA201001200197Line · rupturedDURING SLAT RETRACT GOT LEVE 1 "SLAT DISAG" WITH ROLLING MOTION TO THE RT. COMPLIED WITH RED TABS AND RETURNED TO DTW DECLARING EMERGENCY LANDING. ACFT TOWED OFF RUNWAY. FOUND RT SLAT ACT INBD LINE BROKEN. INSTALLED PERMANANT REPAIR TO SLAT HYD LINE IAW MMJan 20, 2010 · N608FE · Doug MD11F · Hydraulic System, MainSDR FDEA200908042889Frame · damagedAGING INSPECTION - MAIN DECK CARGO FRAME AT STA 1681 ABOVE LONGERON 12 LEFT FOUND WITH EXISTING DOUBLER REPAIR. EXISTING REPAIR AT MAIN DECK CARGO FRAME STA 1681 ABOVE LONGERON 12 LEFT EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED IN ACCORDANCE WITH SRM 53-3Aug 4, 2009 · N608FE · Doug MD11F · Fuselage Main, FrameSDR FDEA200908032874Hinge Bracket · corrodedRIGHT WING OUTBOARD FLAP FORWARD INBOARD HINGE FITTING LOWER INBOARD ATTACH HOLE SPOT FACE FOUND CORROSION. REWORKED AS PER E.A. 1-5750-132702, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.Aug 3, 2009 · N608FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200908032873Hinge Bracket · corrodedRT WING OTBD FLAP FWD INBD HINGE FITTING LWR OTBD ATTACH HOLE SPOT FACE FOUND CORROSION. REWORKED AS PER E.A. 1-5750-132702, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.Aug 3, 2009 · N608FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200907302836Floor Support · corrodedMAIN DECK CARGO - LT FLOOR SUPPORT ASSY FROM STA 1887 TO STA 2007 FOUND CORRODED. REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 41. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING AGA7081 REVISION P. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 1Jul 30, 2009 · N608FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA200907302835Floor Support · corrodedMAIN DECK CARGO - RT FLOOR SUPPORT ASSY FROM STA 1887 TO STA 2007 FOUND CORRODED. REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 41. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING AGA7080 REVISION F. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 1Jul 30, 2009 · N608FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA200907282809Skin · crackedHIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP CARRIED OUT. FOUND 07 EA HOLES WITH CRACKED INDICATION AT LT WING LWR SKIN OUTER WING FUEL TANK PANEL CUT OUT BETWEEN XORS 683.400 AND XORS 713.600. REPAIR CARRIED OUT AS PER E.A. 1-5710-132718, REPAIR CLASSIFIEJul 28, 2009 · N608FE · Doug MD11F · Wing, Plate/SkinSDR FDEA200907282808Skin · crackedHIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP CARRIED OUT. FOUND 02 EA HOLES WITH CRACKED INDICATION AT RT WING LWR SKIN OUTER WING FUEL TANK PANEL CUT OUT BETWEEN XORS 683.400 AND XORS 713.600. REPAIR CARRIED OUT AS PER E.A. 1-5710-132717, REPAIR CLASSIFIEDJul 28, 2009 · N608FE · Doug MD11F · Wing, Plate/SkinSDR FDEA200907282800Seat Track · corrodedMAIN DECK CARGO - SEAT TRACK FLANGE FROM STA 900 TO STA 935, X = -8.5 FOUND WITH MULTIPLE 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, REVIJul 28, 2009 · N608FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200907282798Seat Track · corrodedMAIN DECK CARGO - SEAT TRACK FLANGE FROM STA 1851 TO STA 1891, X = 8.5 FOUND WITH MULTIPLE 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, REVIJul 28, 2009 · N608FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200907282797Seat Track · corrodedMAIN DECK CARGO - SEAT TRACK FLANGE AT STA 1890, X = -27.5 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.Jul 28, 2009 · N608FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200907282796Seat Track · corrodedMAIN DECK CARGO - SEAT TRACK FLANGE AT STA 1845, X = 27.5 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.Jul 28, 2009 · N608FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200907282795Seat Track · corrodedMAIN DECK CARGO - SEAT TRACK FLANGE FROM STA 1851 TO STA 1891, X = 27.5 FOUND WITH MULTIPLE 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, REJul 28, 2009 · N608FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200907272767Seat Track · corrodedMAIN DECK CARGO - SEAT TRACK STA 785, X = 8.5 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.Jul 27, 2009 · N608FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200907272766Seat Track · corrodedMAIN DECK CARGO - SEAT TRACK STA 1621, X = -27.5 FOUND WITH SURFACE CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1591 TO STA 1631, X = -27.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME I, REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100,Jul 27, 2009 · N608FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200907272765Seat Track · corrodedMAIN DECK CARGO - SEAT TRACK STA 795, X = 8.5 FOUND WITH SURFACE CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 745 TO STA 800, X = 8.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME I, REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVJul 27, 2009 · N608FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200907272764Seat Track · corrodedMAIN DECK CARGO - SEAT TRACK STA 1229, X = -75.5 FOUND WITH SURFACE CORROSION. REPAIRED AS PER SRM 53-70-00 FIGURE 6 VOLUME I, REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.Jul 27, 2009 · N608FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200907272763Seat Track · corrodedMAIN DECK CARGO - SEAT TRACK STA 735, X = 8.5 FOUND WITH CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 685 TO STA 745, X = 8.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME I, REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISIONJul 27, 2009 · N608FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200907272762Vane · corrodedLT WING OTBD FLAP VANE NR 4 FROM INBD TRACK TEE FITTING ATTACH HOUSING FOUND CORROSION. REMOVED AND REPLACED AS PER AMM 27-50-32-4 REVISION 64. ADJUSTMENT AND TEST OF THE LT OUTBOARD FLAP VANE REFER TO WORK CARD E1-5750-7-5002 E2 PART 1.Jul 27, 2009 · N608FE · Doug MD11F · Trailing Edge FlapsSDR FDEA200907272761Vane · corrodedRT WING OTBD FLAP VANE NR 4 FROM INBD TRACK TEE FITTING ATTACH HOUSING, FOUND CORROSION. REMOVED AND REPLACED AS PER AMM 27-50-32-4 REVISION 64. ADJUSTMENT AND TEST OF THE RT OUTBOARD FLAP VANE REFER TO WORK CARD E1-5750-7-5002 E2 PART 2.Jul 27, 2009 · N608FE · Doug MD11F · Trailing Edge FlapsSDR FDEA200907272760Panel · crackedVERTICAL STABILIZER - NR 2 ENGINE INTAKE DUCT INTERNAL INBD SUPPORT PANEL STA ZID 2160 FOUND CRACKED. REPAIR CARRIED OUT AS PER SRM 55-20-00 VOLUME I FIGURE 2, REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.Jul 27, 2009 · N608FE · Doug MD11F · Vertical Stabilizer, Plate/SkinSDR FDEA200907272759Skin · corrodedRT WING UPPER SURFACE SKIN AT XORS 250 FOUND SURFACE CORROSION AT 3 LOCATIONS. CORROSION ON RIGHT HAND WING UPPER SURFACE SKIN AT XORS 250, REPAIRED CARRIED OUT AS PER SRM 57-00-01 VOLUME I FIGURE 6, REVISION 40. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100,Jul 27, 2009 · N608FE · Doug MD11F · Wing, Plate/SkinSDR FDEA200907252748Hinge Bracket · corrodedRT WING OTBD FLAP FWD INBD HINGE FITTING ACTUATOR OTBD ATTACH HOLE BORE FOUND CORROSION. RIGHT HAND WING OUTBOARD FLAP FORWARD INBOARD HINGE FITTING ACTUATOR OUTBOARD ATTACH HOLE BORE REWORKED AS PER E.A. 1-5750-132702, REPAIR CLASSIFIED AS MAJOR AS PER GMM Jul 25, 2009 · N608FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200907252747Hinge Bracket · corrodedRIGHT HAND WING OUTBOARD FLAP FORWARD INBOARD HINGE FITTING LOWER OUTBOARD ATTACH HOLE BORE FOUND CORROSION. RIGHT HAND WING OUTBOARD FLAP FORWARD INBOARD HINGE FITTING LOWER OUTBOARD ATTACH HOLE BORE REWORKED AS PER E.A. 1-5750-132702, REPAIR CLASSIFIED AS MJul 25, 2009 · N608FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200907252746Hinge Fitting · corrodedRIGHT HAND WING OUTBOARD FLAP FORWARD INBOARD HINGE FITTING LOWER INBOARD ATTACH HOLE BORE FOUND CORROSION. RIGHT WING OUTBOARD FLAP FORWARD INBOARD HINGE FITTING LOWER INBOARD ATTACH HOLE BORE REWORKED AS PER EA 1-5750-132702, REPAIR CLASSIFIED AS MAJOR AS Jul 25, 2009 · N608FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200907252745Hinge Bracket · corrodedRT WING OTBD FLAP FWD OTBD HINGE FITTING ACTUATOR OTBD ATTACH HOLE BORE FOUND CORROSION. RIGHT WING OUTBOARD FLAP FORWARD OUTBOARD HINGE FITTING ACTUATOR OUTBOARD ATTACH HOLE BORE REWORKED AS PER EA 1-5750-132704. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-Jul 25, 2009 · N608FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200907252744Hinge Bracket · damagedLEFT HAND WING OUTBOARD FLAP FORWARD INBOARD HINGE FITTING ACTUATOR OUTBOARD ATTACH BORE FOUND CORROSION. LEFT WING OUTBOARD FLAP FORWARD INBOARD HINGE FITTING ACTUATOR OUTBOARD ATTACH BORE REWORKED AS PER E.A. 1-5750-132701, REPAIR CLASSIFIED AS MAJOR AS PERJul 25, 2009 · N608FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200907252743Hinge Fitting · corrodedLT WING OTBD FLAP FWD OTBD HINGE FITTING ACTUATOR INBD ATTACH BORE FOUND CORROSION. REWORKED AS PER E.A. 1-5750-132703, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.Jul 25, 2009 · N608FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200907232714Hinge Fitting · damagedSCRATCH MARK, LT WING INBD FLAP AFT OUTBD HINGE INBD PIVOT BORE. REWORKED AS PER E.A. 1-5750-132705, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.Jul 23, 2009 · N608FE · Doug MD11F · Trailing Edge FlapsSDR FDEA200907232713Hinge Fitting · corrodedCORROSION RT WING INBD FLAP AFT OUTBD HINGE OUTBD PIVOT SPOT FACE. REWORKED AS PER E.A. NO. 1-5750-132706, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.Jul 23, 2009 · N608FE · Doug MD11F · Trailing Edge FlapsSDR FDEA200907232712Hinge Bracket · damagedRIGHT HAND WING INBOARD FLAP AFT OUTBOARD HINGE OUTBOARD PIVOT BORE FOUND CORROSION. RIGHT WING INBOARD FLAP AFT OUTBOARD HINGE OUTBOARD PIVOT BORE REWORKED AS PER EA 1-5750-132706, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.Jul 23, 2009 · N608FE · Doug MD11F · Trailing Edge FlapsSDR FDEA200907232711Hinge Bracket · damagedUNABLE TO CARRY OUT HFEC INSPECTION ON INBD PIVOT HOLE AT RT WING INBD FLAP OUTBD HINGE (FLAP SIDE) DUE TO HOLE CORROSION. REWORKED AS PER E.A. NO. 1-5750-132706, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.Jul 23, 2009 · N608FE · Doug MD11F · Trailing Edge FlapsSDR FDEA200907232710Seat Track · chafedDEEPLY CHAFED SEAT TRACK STA 1411 X=-47.5 IN MAIN DECK CARGO. 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.Jul 23, 2009 · N608FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200907222701Skin · damagedLOWER AFT FUSELAGE BELLY STA 1902 TO 1941, BETWEEN LONGERON 48 RIGHT AND LONGERON 48 LEFT FOUND WITH EXISTING SPLICE REPAIR. EXISTING REPAIR AT LOWER AFT FUSELAGE BELLY STA 1902 TO 1941, BETWEEN LONGERON 48 RIGHT AND LONGERON 48 LEFT EVALUATED AND FOUND PRJul 22, 2009 · N608FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA200907222700Skin · damagedCENTER CARGO DOOR CUT OUT AFT EDGE STA 1781, BETWEEN LONGERON 40 AND 41 RT FOUND WITH EXISTING DOUBLER REPAIR. EXISTING REPAIR AT CENTER CARGO DOOR CUT OUT AFT EDGE STA 1781, BETWEEN LONGERON 40 AND 41 RT EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED IAW SRM 5Jul 22, 2009 · N608FE · Doug MD11F · Fuselage Main, Plate/Skin
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