N521FE

Service difficulty reports · 471

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 = 'N521FE' 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 FDEA201107202828Frame · dentedCABIN BS 1681 L11L FRAME FOUND DENTED. DENT REPAIRED AS PER SRM 53-00-07 FIG 201 REV 47. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112. INITIAL INSPECTION AT 14,500 CYCLE AND REPETITIVE INSPECTION AT 9,500 CYCLE USING HFEC METHOD.Jul 20, 2011 · N521FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201004041051Engine · vibrationCREW DEBRIEF BIRD STRIKE ON FWD RADOME AND NR1 ENG VIBRATION READING 5.0 AMBER BOXED INDICATION. R & R NR 1 ENG IAW W/C 71T0001-PW,71T09 01-PW AND AMM 71-00-01-4 THEN RAN NR 1 ENG AT N2 80 PERCENT ALL PARAMETERS INDICATES WORKS NORMAL IAW JRH CH3 /5.CARRIEDApr 4, 2010 · N521FE · Doug MD11F · Engine (Turbine/Turboprop)SDR FDEA200909043258Skin · corrodedLEFT STA 1229 XCW= 97 TO XCW= 107 CTR WING UPPER PANEL FOUND CORROSION. REPAIRED IAW EA 1-5710-133850. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 107.Sep 4, 2009 · N521FE · Doug MD11F · Wing, Plate/SkinSDR FDEA200909043257Skin · corrodedCABIN - RT STA 1229 XCW=77 CTR WING UPPER PANEL FOUND CORROSION. COMPLIED WITH EA 1-5710-133850. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 107.Sep 4, 2009 · N521FE · Doug MD11F · Wing, Plate/SkinSDR FDEA200909023253Seat Track · corrodedCABIN - LT STA 1861 - STA 1901 X= 107 SEAT TRACK FOUND CORROSION. REMOVED AND REPLACED FROM STA 1831 TO STA 2007 X= 107 IAW SRM 51-31-01 REV 41. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV. 107.Sep 2, 2009 · N521FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200909023252Seat Track · corrodedCABIN - RT STA 1861 - STA 1901 X= -107 SEAT TRACK FOUND CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1831 TO STA 2007 X= -107 IAW SRM 53-00-52 FIG 201, REPAIR 1, REV 41 AND EA 1-5310-133861: WINGS- MAINFRAME - SEAT TRACK REPLACEMENT WITHSep 2, 2009 · N521FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200909013221Frame · dentedCABIN - RT STA 1741 LONGERON 11 - LONGERON 12 FRAME FOUND DENT. REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2 REV. 41. REPETITIVE INSP REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE INSP AT 9,500 CYCLES TO BE CARRIED OUT IAW SRM 53-00-07 FIG. 201, REPAIR 2Sep 1, 2009 · N521FE · Doug MD11F · Fuselage Main, FrameSDR FDEA200909013220Seat Track · corrodedCABIN - RT STA 6-90 X= -75.25 SEAT TRACK FOUND CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM ST 6-0 TO STA 6-123 X= -75.25 IAW SRM 53-00-52, FIG 201/ REPAIR 1 REV 41. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 107.Sep 1, 2009 · N521FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200909013219Seat Track · corrodedCABIN - RT STA 1371 TO STA 1391 X= -75.25 SEAT TRACK FOUND CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1371 TO STA 1411 X= -75.25 IAW SRM 53-00-52, FIG 201. REPAIR 1, REV. 41. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 107.Sep 1, 2009 · N521FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200909013218Seat Track · corrodedRIGHT STA 1411 X= -8 SEAT TRACK FOUND CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1391 TO STA 1431 X= -8 IAW SRM 53-00-52 FIG 201, REPAIR 1, REV 41. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 107.Sep 1, 2009 · N521FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200909013217Seat Track · corrodedLT STA 1525 X= 8 SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1491 TO STA 1531 X= 8 IAW SRM 53-00-52, FIG 201, REPAIR 1, REV. 41. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 107.Sep 1, 2009 · N521FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200908313167Doubler · crackedLT WING L/E ACCESS PANEL CUT-OUT XOS 543 FOUND CRACKED. CRACKED DOUBLER REMOVED AND FABRICATED NEW DOUBLER IAW DWG ARB2933, REV T. INSTALLED NEW DOUBLER AT LT WING L/E PANEL CUT-OUT XOS 543 IAW SRM 51-35-01, REV. 41 AND SRM 51-33-01 REV. 41. REPAIR CLASSIFAug 31, 2009 · N521FE · Doug MD11F · Wing, Plate/SkinSDR FDEA200908313166Support · crackedRT OTBD FLAP INBD FWD HINGE JACKET INBD LWR SUPPORT CRACKED. DAMAGED BEAM REMOVED AND REPLACED AT RT OUTBD FLAP INBD FWD HINGE JACKET INBD LWR AREA IAW SRM 51-31-01 REV 41. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 107.Aug 31, 2009 · N521FE · Doug MD11F · Wing Miscellaneous StructureSDR FDEA200908313164Former · crackedLT WING L/E INTERIOR COMPARTMENT XOS 1020 FORMER FOUND CRACKED. LT WING L/E INTERIOR FORMER REMOVED AND FABRICATED IAW DWG ARB2920, REV BB. LT WING L/E INTERIOR FORMER AT (XOS 1020) INSTALLED IAW SRM 51-35-01, REV 41 AND SRM 51-33-01 REV 41. REPAIR CLASSIFIAug 31, 2009 · N521FE · Doug MD11F · Wing Main, Frame StructureSDR FDEA200908313163Doubler · crackedCTR LANDING GEAR WHEEL WELL RT SIDE WALL WEB CUT-OUT DOUBLER FOUND CRACKED. CRACKED DOUBLER AT CTR LANDING GEAR WHEEL WELL RT SIDE WALL WEB CUT-OUT REMOVED IAW SRM 51-33-01 REV 41. NEW DOUBLER MACHINED IAW DWG AEA0526 REV NC AND INSTALLED IAW SRM 51-33-01, Aug 31, 2009 · N521FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA200908313161Bulkhead · crackedCTR LANDING GEAR WHEEL WELL LT WEB CUT-OUT DOUBLER FOUND CRACKED. DOUBLER AT CTR LANDING GEAR WHEEL WELL LT WEB CUT-OUT REMOVED IAW SRM 51-33-01, REV 41. NEW DOUBLER MACHINED IAW DWG AEA0526 REV, NC. NEW DOUBLER INSTALLED IAW SRM 51-31-01, REV 41. REPAIRAug 31, 2009 · N521FE · Doug MD11F · Fuselage Main, BulkheadSDR FDEA200908313159Frame · dentedCABIN - LT STA 1761 LONGERON 11 TO LONGERON 12 FRAME FOUND DENT. REPAIRED IAW SRM 53-00-07, FIG 20, REPAIR 2 REV 41. REPETITIVE INSP REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE INSP AT 9,500 CYCLES TO BE CARRIED OUT IAW SRM 53-00-07 FIG. 201, REPAIR 2Aug 31, 2009 · N521FE · Doug MD11F · Fuselage Main, FrameSDR FDEA200908313158Frame · chafedCABIN - LT STA 1741 LONGERON 11 TO LONGERON 12 FRAME FOUND CHAFED. REPAIRED IAW SRM 53-00-07, FIG. 201, REPAIR 2 REV. 41. REPETITIVE INSP REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE INSP AT 9,500 CYCLES TO BE CARRIED OUT IAW SRM 53-00-07 FIG. 201, REPAAug 31, 2009 · N521FE · Doug MD11F · Fuselage Main, FrameSDR FDEA200908313156Frame · dentedLEFT STA 1721 LONGERON 11 TO LONGERON 12 FRAME FOUND DENT. REPAIRED IAW SRM 53-00-07, FIG. 201. REPAIR 2 REV 41. REPETITIVE INSP REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE INSP AT 9,500 CYCLES TO BE CARRIED OUT IAW SRM 53-00-07 FIG. 201. REPAIR 2, RAug 31, 2009 · N521FE · Doug MD11F · Fuselage Main, FrameSDR FDEA200908313155Frame · dentedCABIN - LT STA 1701 LONGERON 11 TO LONGERON 12 FOUND DENT. REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2 REV 41. REPETITIVE INSP REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE INSP AT 9,500 CYCLES TO BE CARRIED OUT IAW SRM 53-00-07, FIG. 201, REPAIR 2, REVAug 31, 2009 · N521FE · Doug MD11F · Fuselage Structure (General)SDR FDEA200908313152Frame · dentedCABIN - RT STA LONGERON 11 TO LONGERON 12 FRAME FOUND DENT. REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2, REV. 41. REPETITIVE INSP REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE INSP AT 9,500 CYCLES TO BE CARRIED OUT IAW SRM 53-00-07 FIG 201, REPAIR 2, RAug 31, 2009 · N521FE · Doug MD11F · Fuselage Main, FrameSDR FDEA200908313151Frame · chafedCABIN - RT STA 1661 LONGERON 11 TO LONGERON 12 FRAME FOUND CHAFED. REPAIRED IAW SRM 53-00-07 FIG 201, REPAIR 2, REV. 41. REPETITIVE INSP REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE INSP AT 9,500 CYCLES TO BE CARRIED OUT IAW SRM 53-00-07 FIG 201, REPAIAug 31, 2009 · N521FE · Doug MD11F · Fuselage Main, FrameSDR FDEA200908313149Vane · delaminatedLT WING INBD FLAP VANE LWR MID EXTERIOR SURFACE FOUND DELAMINATION. COMPLIED WITH EA 1-5750-133837. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 107.Aug 31, 2009 · N521FE · Doug MD11F · Trailing Edge FlapsSDR FDEA200907062498Shaft · failedHYD 2 QTY LOW LVL 2 ALERT FOLLOWED BY HYD 2 OFF LVL 2 HYD QTY WENT TO 0. LANDED LAX WITHOUT INCIDENT. INSPECTED HYD FILTERS ON ENGINE FOUND AFT PUMP CASE DRAIN FILTER HAD LARGE QUANTITY OF METAL DEBRIS & DELTA P INDICATOR POPPED. FOUND SHAFT SHEARED ON AFT HJul 6, 2009 · N521FE · Doug MD11F · Hydraulic Pump (Electric/Engine), MainSDR 08FDEA01009Hinge Fitting · corrodedRIGHT WING, INBOARD FLAP AFT HINGE AFT INBOARD FASTENER HOLE FOUND CORROSION. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-116428. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Mar 18, 2008 · N521FE · Doug MD11F · Trailing Edge FlapsSDR 08FDEA00913Frame · dentedMAIN DECK LT FRAME AT STA 535 L20 FOUND DENTED. DENTED AREA REPAIRED AS PER DWG SRZ-53- 503. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Mar 12, 2008 · N521FE · Doug MD11F · Fuselage Main, FrameSDR 08FDEA00912Frame · dentedMAIN DECK LT FRAME AT STA 535 L24 FOUND DENTED. DENTED AREA REPAIRED AS PER DWG SRZ-53-503. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Mar 12, 2008 · N521FE · Doug MD11F · Fuselage Main, FrameSDR 08FDEA00911Frame · dentedMAIN DECK FRAME AT RT STA 1701 L12 FOUND DENTED. REPAIRED AS PER SRM 53-30-00 FIG. 1 VOL.I. INITIAL INSPECTION AT 14500 CYCLES AND REPETITIVE INSPECTION AT 9500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00 FIG.1 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-Mar 12, 2008 · N521FE · Doug MD11F · Fuselage Main, FrameSDR 08FDEA00910Frame · dentedMAIN DECK FRAME AT RT STA 1681 L12 FOUND DENTED. REPAIRED AS PER SRM 53-30-00 FIG. 1 VOL.I. INITIAL INSPECTION AT 14500 CYCLES AND REPETITIVE INSPECTION AT 9500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00 FIG.1 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER GMM Mar 12, 2008 · N521FE · Doug MD11F · Fuselage Main, FrameSDR 08FDEA00909Frame · dentedMAIN DECK FRAME AT RT STA 1661 L12 FOUND DENTED. REPAIRED AS PER SRM 53-30-00 FIG. 1 VOL.I. INITIAL INSPECTION AT 14500 CYCLES AND REPETITIVE INSPECTION AT 9500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00 FIG. 1 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER GMMar 12, 2008 · N521FE · Doug MD11F · Fuselage Main, FrameSDR 08FDEA00908Skin · gougedLEFT WING, INBOARD FLAP LOWER SURFACE FOUND GOUGE AT XIFH 191. REPAIRED AS PER SRM 57-10-00 FIG.2 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Mar 12, 2008 · N521FE · Doug MD11F · Trailing Edge FlapsSDR 08FDEA00864Rib · crackedLEFT WING, LEADING EDGE RIB FOUND CRACKED AT XOS 795. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. NEW RIB FABRICATED AS PER DRAWING ARB2922. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Mar 10, 2008 · N521FE · Doug MD11F · Wing, Rib/BulkheadSDR 08FDEA00863Seat Track · corrodedFOUND MAIN DECK SEAT TRACK AT STA 1521, X = -75.25, FOUND EXFOLIATION CORROSION. 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.Mar 10, 2008 · N521FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA00799Skin · crackedRING WING, LEADING EDGE TELESCOPIC DUCT CUTOUT DOOR OUTBOARD CORNER FOUND CRACKED. REPAIRED AS PER SRM 57-10-00 FIGURE 43 VOLUME I AND EA 1-5710-115329. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Mar 9, 2008 · N521FE · Doug MD11F · Wing Main, Frame StructureSDR 08FDEA00798Skin · crackedRT WING, DROOP LEADING EDGE SURFACE FOUND CRACKED AT FASTENER HOLE. REPAIRED AS PER SRM 57-10-00 FIGURE 30 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Mar 9, 2008 · N521FE · Doug MD11F · Wing, Plate/SkinSDR 08FDEA00797Skin · crackedLEFT WING, NR 3 LEADING EDGE SLAT TELESCOPIC DUCT CUTOUT INBOARD CORNER FOUND CRACK. REPAIRED AS PER SRM 57-10-00 FIGURE 43 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Mar 9, 2008 · N521FE · Doug MD11F · Wing, Plate/SkinSDR 07FDEA04188Selector Valve · malfunctionedRIGHT MAIN LANDING GEAR DID NOT RETRACT AFTER TAKEOFF. RED INDICATION IN BOTH MAIN LG DISPLAY AND CONFIG PAGE. REFERED TO QRH, RECYCLED GEAR, GOOD INDICATIONS (ALL UP) FOLLOWED. VISUALLY INSPECTED RT MAIN LDG GEAR AND AROUND OF SELECTOR VALVE, FOUND NORMAL.Sep 21, 2007 · N521FE · Doug MD11F · Landing Gear Retraction/Extension SystemSDR 07FDEA00735Handle · stuckAFTER T/O COULD NOT RAISE GEAR HANDLE. REPEATED ATTEMPTS. HANDLE FINALLY RAISED WITH RIGHT MAIN GEAR UNSAFE. RED LIGHT IN BOTH PRIMARY AND SECONDARY. LOWERED GEAR & LANDED FUEL DUMP APPROX 110,000 LBS FOUND RT MLG DOOR MOUNTED SENSOR TARGET DAMAGED. REPMar 9, 2007 · N521FE · Doug MD11F · Landing Gear SelectorSDR 06FDEA03626Uplock · overtorquedLEFT MAIN GEAR LIGHT UNSAFE AFTER TAKEOFF ON MAIN AND SECONDARY (CONFIG PAGE). CYCLED GEAR DOWN, GOOD INDICATION, GEAR HANDLE UP INDICATIONS WERE LEFT AND RIGHT MAIN GEAR UNSAFE. DURING DESCENT, RIGHT UNSAFE LIGHT WENT OUT. RETURNED TO MEM. LANDED UNEVEOct 12, 2006 · N521FE · Doug MD11 · Landing Gear Position and WarningSDR 06FDEA03476Attach Bracket · inoperativeUNABLE TO RETRACT GEAR IN FLIGHT AFTER SEVERAL NORMAL CYCLES, USING RETRACT OVERRIDE BUTTON NO HELP. POST TEST FLIGHT REVEALED DAMAGE TO LH MAIN GEAR SUPPORT BRACKET FOR CABLE AND HYDRAULIC. FOLLOWING DAMAGED PARTS WERE REPLACED AND FUNCTIONAL AND OPERATISep 29, 2006 · N521FE · Doug MD11 · Fuselage Main, Attach FittingsSDR 06FDEA03190Case · chafedENG NR 1 FAN CASE AT AFT 1:00 POS FOUND WITH CHAFE MARK AT 8 PLACES (P/N 51G478). CHAFE MARK MEASURED AND FOUND 3 AREAS OUT OF LIMIT PER AMM 72-33-06-6. REFER TO E.A.1-7233-103553. CLASSIFIED MAJOR REPAIR PER GMM 6-2-100.Sep 5, 2006 · N521FE · Doug MD11 · Turbine Engine Compressor SectionSDR 06FDEA03156Mount Fitting · corrodedPYLON NR 3 FWD ENG MOUNT FITTING WAS REPORTED WITH PITTING ON TRUSS P/N AUB7510-501 FWD AND AFT HOLES, AND ON TRUSS P/N AUB7510-502 FWD HOLES (FWD ENG MOUNT FITTING P/N AUB7508-1). CORROSION REMOVED AND FABRICATED BUSHINGS INSTALLED AS PER E.A.1-5450-102315, Aug 31, 2006 · N521FE · Doug MD11 · Engine Mount SectionSDR 06FDEA03154Hinge Bracket · corrodedLT WING OUTBD FLAP OUTBD HINGE (WING SIDE) SIDE LINK ATTACHMENT SPOT FACE FOUND CORROSION (HINGE BRACKET P/N ARC0503-11). CORROSION REMOVED AS PER CMM 57-44-09. REPAIR CARRIED OUT AS PER CMM 57-44-09 AND CLASSIFIED AS MINOR REPAIR PER GMM 6-2-100.Aug 30, 2006 · N521FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 06FDEA03153Hinge Bracket · corrodedLT WING OUTBD FLAP OUTBD HINGE (WING SIDE) ACTUATOR ATTACHMENT OUTBD BORE FOUND CORROSION. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-102161. CLASSIFIED MAJOR REPAIR PER GMM 6-2-100.Aug 30, 2006 · N521FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 06FDEA03152Hinge Bracket · corrodedLT WING OUTBD FLAP OUTBD HINGE (WING SIDE) ACTUATOR ATTACHMENT INBD BORE FOUND CORROSION. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. CLASSIFIED MAJOR REPAIR PER GMM 6-2-100.Aug 30, 2006 · N521FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 06FDEA03109Hinge Bracket · corrodedRT WING OUTBD FLAP OUTBD HINGE (WING SIDE) SIDE LINK ATTACHMENT SPOT FACE FOUND CORROSION. CORROSION REMOVED AS PER CMM 57-44-09. CLASSIFIED MAJOR REPAIR PER GMM 6-2-100.Aug 27, 2006 · N521FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 06FDEA03108Hinge Bracket · corrodedRT WING OUTBD FLAP OUTBD HINGE (WING SIDE) SIDE LINK ATTACHMENT FWD BORE FOUND CORROSION. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. BUSHING FABRICATED AND INSTALLED AS PER E.A.1-5750-102156. CLASSIFIED MAJOR REPAIR PER GMM 6-2-100.Aug 27, 2006 · N521FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 06FDEA03107Hinge Bracket · corrodedRT WING OUTBD FLAP OUTBD HINGE (WING SIDE) SIDE LINK ATTACHMENT AFT BORE FOUND CORROSION. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. BUSHING FABRICATED AND INSTALLED AS PER E.A.1-5750-102156. CLASSIFIED MAJOR REPAIR PER GMM 6-2-100.Aug 27, 2006 · N521FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 06FDEA03106Hinge Bracket · corrodedRT WING OUTBD FLAP OUTBD HINGE (WING SIDE) ACTUATOR ATTACHMENT OUTBD BORE FOUND CORROSION. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. BUSHING FABRICATED AND INSTALLED AS PER E.A.1-5750-102156. CLASSIFIED MAJOR REPAIR PER GMM 6-2-100.Aug 27, 2006 · N521FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 06FDEA03105Hinge Bracket · corrodedRT WING OUTBD FLAP OUTBD HINGE (WING SIDE) ACTUATOR ATTACHMENT INBD BORE FOUND CORROSION. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-102156. CLASSIFIED MAJOR REPAIR PER GMM 6-2-100.Aug 27, 2006 · N521FE · Doug MD11 · Wing, Control Surface Attach Fittings
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