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 FDEA201307301696Rib · damagedAFTER REMOVAL OF EXISTING REPAIR, FOUND L/E RIB DAMAGED AT ZFS =603.132. CRACKED RIB REMOVED IAW SRM 51-35-01, REV 53. NEW RIB FABRICATED IAW DWG AMC7130, REV E. RIB INSTALLED IAW SRM 51-35-01, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 30, 2013 · N521FE · Doug MD11F · Vertical Stabilizer, Spar/RibSDR FDEA201307301695Rib · damagedAFTER REMOVAL OF EXISTING REPAIR, FOUND L/E RIB DAMAGED AT ZFS =596.972. CRACKED RIB REMOVED IAW SRM 51-35-01, REV 53. NEW RIB FABRICATED IAW DWG AMC7130, REV E. RIB INSTALLED IAW SRM 51-35-01, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 30, 2013 · N521FE · Doug MD11F · Vertical Stabilizer, Spar/RibSDR FDEA201307251661Skin · crackedEIGHT FASTENER HOLES FOUND WITH CRACK INDICATIONS DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION. REPAIRED IAW SRM 57-20-02, REPAIR 5, FIG 201, REV 53, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 25, 2013 · N521FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201307251660Skin · crackedSEVEN FASTENER HOLES FOUND WITH CRACK INDICATIONS. DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=690 AND STA XORS=700. REPAIRED IAW SRM 57-20-02, REPAIR 5, FIG 201, REV 53. REPAIR CJul 25, 2013 · N521FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201307241655Rib · damagedRT WING NR 8 LEADING SLAT TRACK RIB DRIVE ATTACH LUG BORE HOLES XOS 1113.252 FOUND DAMAGED. REPAIRED IAW EA1-5750-16614. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 24, 2013 · N521FE · Doug MD11F · Wing, Rib/BulkheadSDR FDEA201307241652Skin · dentedRIGHT WING L/E NR 8 SLAT FWD INBD AREA DENTED. REPAIRED IAW EA 1-5750-166141. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 24, 2013 · N521FE · Doug MD11F · Leading Edge DevicesSDR FDEA201307241651Rib · damagedAFTER RT WING L/E NR 8 SLAT LOWER INNER SKIN REMOVAL, FOUND INTERNAL NR 5 RIB DAMAGED AT XOS 1030.5. REPAIRED IAW EA 1-5750-166142. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 24, 2013 · N521FE · Doug MD11F · Leading Edge DevicesSDR FDEA201307241650Rib · damagedAFTER RT WING L/E NR 8 SLAT LOWER INNER SKIN REMOVAL, FOUND INTERNAL NR 4 RIB DAMAGED AT XOS 1025. REPAIR IAW EA 1-5750-166142. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 24, 2013 · N521FE · Doug MD11F · Leading Edge DevicesSDR FDEA201307241649Rib · damagedAFTER RT WING L/E NR 8 SLAT LOWER INNER SKIN REMOVAL, FOUND INTERNAL NR 1 RIB, DAMAGED AT XOS 1010.5. REPAIRED IAW EA 1-5750-166142. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 24, 2013 · N521FE · Doug MD11F · Leading Edge DevicesSDR FDEA201307231642Rib · damagedON REMOVAL OF RIGHT WING L/E NR 8 SLAT LOWER SKIN, NR 2 RIB FROM INBD WAS FOUND DAMAGED AT APPROX XOS 1015. REPAIRED IAW EA 1-5750-166142. CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 23, 2013 · N521FE · Doug MD11F · Leading Edge DevicesSDR FDEA201307221626Structure · corrodedLEFT WING OTBD FLAP, INBD FORWARD (WING SIDE) HINGE ACTUATOR INBD BORE CORRODED. BORE REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-44-08, REV 76. REPAIR CARRIED OUT IAW EA 1-5750-166143, STEP 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 22, 2013 · N521FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201307221625Structure · corrodedLEFT WING OTBD FLAP, INBD FORWARD (WING SIDE) HINGE UPPER MOUNT OTBD BORE CORRODED. BORE REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-44-08, REV 76. REPAIR CARRIED OUT IAW EA 1-5750-166143, STEP 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 22, 2013 · N521FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201307221624Structure · corrodedLEFT WING OTBD FLAP INBD FORWARD (WING SIDE) HINGE BARREL NUT HOLE SURFACE CORRODED. BARREL NUT BORE SURFACE REWORKED IAW CMM 20-10-6, REV 76. REPAIR SHIM FABRICATED AND INSTALLED IAW CMM 57-44-08, REV 76. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 22, 2013 · N521FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201307221623Structure · corrodedRIGHT WING OTBD FLAP, INBD FORWARD (WING SIDE) HINGE UPPER MOUNT INBD BORE CORRODED. BORE REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08, REV 76, REPAIRED IAW EA 1-5750-T0301348, PART 1 STEP 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 22, 2013 · N521FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201307221622Structure · corrodedRIGHT WING OTBD FLAP, INBD FWD (WING SIDE) HINGE UPPER MOUNT OTBD BORE CORRODED. BORE REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08, REV 76. REPAIRED IAW EA 1- 5750-T0301348, PART 1, STEP 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 22, 2013 · N521FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201307221621Structure · corrodedRIGHT WING OTBD FLAP, INBD FWD (WING SIDE) HINGE ACTUATOR INBD BORE CORRODED. BORE REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08, REV 76. REPAIRED IAW EA 1-5750-T0301348, PART 1, STEP 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 22, 2013 · N521FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201307221617Structure · corrodedRIGHT WING OTBD FLAP, OTBD FWD (WING SIDE) HINGE BARREL MOUNT LOWER BORE CORRODED. BORE NR 7 REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 76. REPAIRED IAW EA 1- 5750-T0301349, PART 1, STEP 2. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 22, 2013 · N521FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201307221615Structure · corrodedRIGHT WING OTBD FLAP, OTBD FWD (WING SIDE) HINGE BARREL MOUNT UPPER BORE CORRODED. BORE NR 7 REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 76. REPAIRED IAW EA 1- 5750-T0301349, PART 1, STEP 2. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 22, 2013 · N521FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201307221614Hinge Fitting · corrodedRT WING OTBD FLAP, OTBD FORWARD (WING) HINGE UPPER MOUNT INBD BORE CORRODED. REPAIRED IAW EA 1- 5750-T0301349 PART 1 STEP 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 116.Jul 22, 2013 · N521FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201307221632Tee Fitting · corrodedLT OTBD FLAP VANE TEE FITTING "B" MOUNTING HOLE CORRODED. REWORKED AND FOUND EXCEEDED LIMITS IAW SRM 57-50-02 REPAIR 5 FIG.201 REV 53. REPAIRED IAW EA 1-5750-T0301579 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 116.Jul 22, 2013 · N521FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201307221631Tee Fitting · corrodedRT OTBD FLAP VANE TEE FITTING "F" MOUNTING HOLE CORRODED. FOUND EXCEEDED LIMIT IAW SRM 57-50-02, REPAIR 5, FIG 201, REV 53. REPAIRED IAW EA 1-5750-T0301580, PART 1 STEP 1.B. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 22, 2013 · N521FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201307221630Tee Fitting · corrodedRIGHT OTBD FLAP VANE TEE FITTING "C" MOUNTING HOLE CORROSION. FOUND EXCEEDED LIMITS IAW SRM 57-50-02, REPAIR 5, FIG 201, REV 53. REPAIRED IAW EA1-5750-T0301580, PART 1 STEP 1.A. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 22, 2013 · N521FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201307221629Hinge Fitting · corrodedRT WING OTBD FLAP, OTBD AFT (FLAP) HINGE PIVOT HOLE INBD BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-52-04, REV 76. REPAIRED IAW EA 1-5750-166144. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 22, 2013 · N521FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201307221628Bushing · wornRIGHT WING FLAP OTBD HINGE (FLAP SIDE), PIVOT OTBD BUSHING FOUND WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 76 AND FOUND EXCEEDED LIMITS IAW CMM 57-52-03, REV 76. NEW BUSHING FABRICATED BY MACHINING AND INSTALLED EA 1-5750-102153C, PART 3, STEP 2. REPAIRJul 22, 2013 · N521FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201307221627Bushing · wornRIGHT WING: RT INBD FLAP OTBD HINGE (FLAP SIDE) , PIVOT INBD BUSHING FOUND WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 76. FOUND EXCEEDED LIMIT IAW CMM 57-52-03, REV 76. NEW BUSHING FABRICATED BY MACHINING AND INSTALLED IAW EA 1-5750-102153C, PART 3, STEP Jul 22, 2013 · N521FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201307221619Bushing · wornRT WING OTBD FLAP, OTBD FORWARD (WING) HINGE ACTUATOR, OUTBOARD BORE BUSHING WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 76. FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 76. NEW BUSHING AND REPAIR WASHER FABRICATED AND INSTALLED IAW EA 1-5750-T0301349, PART 1Jul 22, 2013 · N521FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201307221618Bushing · wornRT WING OTBD FLAP, OTBD FORWARD (WING) HINGE ACTUATOR INBD BORE BUSHING WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 76. FOUND EXCEEDED LIMITS IAW CMM 57-44-09, REV 76. NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0301349, PART 1, STEP 3. REPAIR CLAJul 22, 2013 · N521FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201307221616Hinge Fitting · corrodedRT WING OTBD FLAP, OTBD FORWARD (WING) HINGE BARREL MOUNT HAS SURFACE CORROSION. REWORKED IAW CMM 20-10-6, REV 76. FOUND WITHIN DWG NR ARC0503 AND CMM 57-44-09, REV 19, TABLE 601 LIMITS. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 116.Jul 22, 2013 · N521FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201307191590Hinge Fitting · crackedRIGHT WING T/E OTBD FLAP INBD FORWARD HINGE BRACKET SIDE LOAD FITTING CRACKED. R & R IAW SRM 51-33-01, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 19, 2013 · N521FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201307191588Support Fitting · crackedDURING HIGH FREQUENCY EDDY CURRENT FOR OPEN HOLE INSPECTION FOUND TWO CRACK INDICATIONS ON NR 1 MAIN DECK CARGO DOOR LOWER FRAME SUPPORT FITTING AT HOLE "C" AND "D". R & R IAW SRM 51-31-01, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REVISION 116.Jul 19, 2013 · N521FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201307191591Stop Fitting · crackedLEFT WING OTBD FLAP STOP FITTING CRACKED. STOP FITTING REMOVED IAW SRM 51-31-01, REV 53, HOLES PICKED UP ON NEW STOP FITTING IAW DWG ARC4125, REV G AND SRM 51-31-02 REV 53 NEW STOP FITTING INSTALLED IAW SRM 51-33-01, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6Jul 19, 2013 · N521FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201307191589Web · canningCENTER LANDING GEAR WHEEL WELL, OIL CANNING FOUND AT RT KEELBEAM WEB, ABOVE FORWARD DOOR HINGE LINE. REPAIRED IAW EA 1-5310-T0301311, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 19, 2013 · N521FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201307171578Beam · crackedMAIN DECK CARGO L3 DOOR AFT UPPER CORNER DOOR STOP FOUND CRACKED. R & R IAW SRM 51-31-01, REV 53 REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 17, 2013 · N521FE · Doug MD11F · Passenger/Crew DoorsSDR FDEA201307161572Longeron Splice · crackedCENTER CARGO LONGERON SPLICE FITTING AT STATION 5-123, LONGERON 45L FOUND CRACKED. SPLICE FABRICATED IAW DWG A5A7116, REVISION D. R & R WITH NEW FABRICATED SPLICE IAW SRM 51-33-01, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 16, 2013 · N521FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201307161571Longeron Splice · crackedCENTER CARGO LONGERON SPLICE FITTING AT STATION 5-123, LONGERON 49L FOUND CRACKED. SPLICE FABRICATED IAW DWG A5A7114, REV J. R & R WITH NEW FABRICATED SPLICE IAW SRM 51-33-01, REV 53, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 16, 2013 · N521FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201307161570Longeron Splice · crackedCENTER CARGO LONGERON SPLICE FITTING AT STATION 5-123, LONGERON 51L FOUND CRACKED. SPLICE FABRICATED IAW DWG A5A7114 REVISION J. R & R WITH NEW FABRICATED SPLICE IAW SRM 51-33-01, REV 53 REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 16, 2013 · N521FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201307161569Longeron Splice · crackedCENTER CARGO LONGERON SPLICE FITTING AT STATION 5-123, LONGERON 50L FOUND CRACKED. SPLICE FABRICATED IAW DWG A5A7114, REV J. R & R WITH NEW FABRICATED SPLICE IAW SRM 51-33-01, REV 53 REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 16, 2013 · N521FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201307161568Longeron Splice · crackedCENTER CARGO LONGERON SPLICE FITTING AT BS 5-123 LONGERON 49R FOUND CRACKED. SPLICE FABRICATED IAW DWG A5A7114, REV J. R & R WITH NEW FABRICATED SPLICE IAW SRM 51-33-01, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 16, 2013 · N521FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201307161567Longeron Splice · crackedCENTER CARGO LONGERON SPLICE FITTING AT BS 5-123, LONGERON 40R FOUND CRACKED. R & R WITH NEW FABRICATED SPLICE IAW SRM 51-33-01, REV 53. SPLICE FABRICATED IAW DWG A5A7114, REV J. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 16, 2013 · N521FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201307161566Longeron Splice · crackedCENTER CARGO LONGERON SPLICE FITTING AT BS 5-123, LONGERON 39R FOUND CRACKED. R & R WITH NEW FABRICATED SPLICE IAW SRM 51-33-01, REV 53. SPLICE FABRICATED IAW DWG A5A7114, REV J. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 16, 2013 · N521FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201307161565Longeron Splice · crackedCENTER CARGO LONGERON SPLICE AT BS 5-123, LONGERON 37R FOUND CRACKED. R & R WITH NEW FABRICATED SPLICE IAW SRM 51-33-01, REV 53. SPLICE FABRICATED IAW DWG A5A7114, REV J. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 16, 2013 · N521FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201307161564Seat Track · bulgedMAIN DECK CARGO BS 1229, X= 8.5 SEAT TRACK FOUND BOTTOM SURFACE BULGING. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT BS 1209 - 1248 IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 16, 2013 · N521FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201307161563Trunnion · crackedNOSE LANDING GEAR RT TRUNNION FITTING FOUND CRACKED AT BS 595. REPAIRED IAW SRM 53-10-14, REPAIR 2, FIG 202, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 16, 2013 · N521FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR FDEA201307161562Trunnion · crackedNOSE LANDING GEAR LT TRUNNION FITTING FOUND CRACKED AT BS 595. REPAIRED IAW SRM 53-10-14, REPAIR 2, FIG 202, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 16, 2013 · N521FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR FDEA201306061205Line · crackedRAMP REPORTED, WHEN CLOSING THE MAIN CARGO DOOR, HEARD A POP FOLLOWED BY A MIST IN THE AIR. FOUND MAIN CARGO DOOR ACTUATOR "CLOSED" LINE CRACKED AT UPPER FITTING. MCD DOOR ACTAUTOR FLEX LINE INSTALLED.Jun 6, 2013 · N521FE · Doug MD11F · Hydraulic System, MainSDR FDEA201301220155Wire · shortedDURING TROUBLESHOOTING, FWD CARGO FAN ASSY FOUND WIRES SHORTED AT S3-380 TERMINAL 17XJ. 15 THRU 21. R & R FWD CARGO FAN RELAY R2-78 IN REF TO WDM 21-43-01 PG 1, SH 1.Jan 22, 2013 · N521FE · Doug MD11F · Air Conditioning System WiringSDR FDEA201107252930Spar · crackedNR 2 ENGINE RT AIR INTAKE SPAR INTERIOR SUPPORT STRUCTURE FOUND WITH CRACKED. REPAIRED AS PER SRM 55-30-02 FIG 201 REPAIR 2 REV 47. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.Jul 25, 2011 · N521FE · Doug MD11F · Nacelle/Pylon, Main FrameSDR FDEA201107212872Longeron Splice · crackedFWD CARGO COMPARTMENT/ SPLICE DOUBLER AT STATION 758, LONGERON 45 LT FOUND CRACKED. REMOVED AND REPLACED WITH NEW LONGERON SPLICE AS PER SRM 51-33-01 REV 47. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.Jul 21, 2011 · N521FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201107202830Vane · delaminatedRT WING INBD FLAP VANE LOWER SURFACE FOUND DELAMINATED. REMOVED AND REPLACED AS PER AMM 27-50-22-4 REV 70.0. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-22-5 REV 70.0 FOUND SATISFACTORY. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REV 112.Jul 20, 2011 · N521FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201107202829Seat Track · corrodedCABIN BS 5-95 X=-77.25 RIGHT, SEAT TRACK FOUND CORRODED. REMOVED AND REPLACED AS PER SRM 51-31-01 REV 47. SEAT TRACK FABRICATED AS PER DRAWING A6A7083 REV NEW, REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.Jul 20, 2011 · N521FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
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