N586FE

Service difficulty reports · 500

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 = 'N586FE' 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 08FDEA02436Skin · corrodedSKIN UNDER RIGHT BODY FAIRING NR 347DF, 01 EACH SURFACE CORROSION FOUND NEAR FASTENER HOLE AT STATION 2155. CORROSION REMOVED AS PER SRM 51-21-01 VOL.II. EXCEEDED LIMITS AS PER SRM 53-00-01, FIG. 2, VOL.I. REPAIR CARRIED OUT AS PER SRM 53-20-00, FIG.Jun 25, 2008 · N586FE · Doug MD11F · Fuselage Main, Plate/SkinSDR 08FDEA02381Stringer · crackedRIGHT WING LEADING EDGE STRINGER AT XOS 672 FOUND CRACKED OFF. REPAIR CARRIED OUT AS PER EA 1-5720-122505, REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100.Jun 23, 2008 · N586FE · Doug MD11F · Wing, Longeron/StringerSDR 08FDEA02380Longeron · crackedCRACK INDICATION FOUND DURING X-RAY INSPECTION AT STATION 6-100, LONGERON-3 RIGHT FORWARD SECTION EDGE. CRACK LENGTH APPROXIMATELY 0.3 INCH. REPAIR CARRIED OUT AS PER EA 1-5310-122735, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Jun 23, 2008 · N586FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 08FDEA02379Longeron · crackedDURING HFEC INSPECTION, MULTIPLE CRACKS (05 EACH, TOTAL LENGTH APPROX 1.2 INCH) FOUND AT FASTENER HOLE OF LONGERON ADJACENT TO NOSE LANDING GEAR LEFT TRUNNION FITTING. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2Jun 23, 2008 · N586FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 08FDEA02378Bulkhead · crackedCENTER LANDING GEAR WHEEL WELL STATION 1391 LEFT WEB CORNER DOUBLER FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Jun 23, 2008 · N586FE · Doug MD11F · Fuselage Main, BulkheadSDR 08FDEA02351Vane · delaminatedLEFT WING INBOARD FLAP VANE LOWER SURFACE FOUND DELAMINATED FROM STATION XIFH 156 TO XIFH 206. LEFT WING INBOARD FLAP VANE ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-22-4. ADJUSTMENT AND TEST CARRIED OUT FOUND 'SATIS' AS PER AMM 27-50-22-5.Jun 20, 2008 · N586FE · Doug MD11F · Trailing Edge FlapsSDR 08FDEA02344Support Fitting · crackedMAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 UPPER WEB SECOND LAYER FOUND WITH CRACK INDICATION (APPROXIMATELY 10 O'CLOCK POSITION) AT HOLE NR C. CARRIED OUT REPAIR AS PER EA 1-5310-122506, PART 1. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jun 19, 2008 · N586FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA02343Support Fitting · crackedMAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 UPPER WEB SECOND LAYER FOUND WITH CRACK INDICATION (APPROXIMATELY 4 O'CLOCK POSITION) AT HOLE NR D. CARRIED OUT REPAIR AS PER EA 1-5310-122506, PART 1. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jun 19, 2008 · N586FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA02342Support Fitting · crackedMAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 6 UPPER WEB SECOND LAYER FOUND WITH CRACK INDICATION (APPROXIMATELY 1 O'CLOCK POSITION) AT HOLE NR D. CARRIED OUT REPAIR AS PER EA 1-5310-122506, PART 1. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jun 19, 2008 · N586FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA02341Support Fitting · crackedMAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 6 UPPER WEB SECOND LAYER FOUND WITH CRACK INDICATION (APPROXIMATELY 4 O'CLOCK POSITION) AT HOLE NR C. CARRIED OUT REPAIR AS PER EA 1-5310-122506, PART 1. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jun 19, 2008 · N586FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA02340Support Fitting · crackedMAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 5 UPPER WEB SECOND LAYER FOUND WITH CRACK INDICATION (APPROXIMATELY 8 O'CLOCK POSITION) AT HOLE NR C. CARRIED OUT REPAIR AS PER EA 1-5310-122506, PART 1. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jun 19, 2008 · N586FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA02339Support Fitting · crackedMAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 4 UPPER WEB SECOND LAYER FOUND WITH CRACK INDICATION (APPROXIMATELY 2 O'CLOCK POSITION) AT HOLE NR C. CARRIED OUT REPAIR AS PER EA 1-5310-122506, PART 1. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jun 19, 2008 · N586FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA02338Trunnion · crackedNOSE LANDING GEAR LEFT TRUNNION FITTING FOUND CRACKED. AREA TRIMMED OUT AND REPAIRED AS PER SRM 53-40-00, FIG.23, VOL.I. PER SRM 53-40-00, FIG.23, VOL.I, OPTION 2: REPETITIVELY INSPECT FOR CRACK GROWTH AT NOT TO EXCEED 1,500 LANDING INTERVALS. THIS REPAIR CLAJun 19, 2008 · N586FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR 08FDEA02337Skin · cracked03 EACH FASTENER HOLES FOUND CRACK INDICATIONS DURING OPEN-HOLE HFEC INSPECTION AT RIGHT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 690 AND STATION XORS = 700. CARRIED OUT REPAIR AS PER EA 1-5710-122497 PART 1. THIS REPAIR CLASSIFIED AS MIJun 19, 2008 · N586FE · Doug MD11F · Wing, Plate/SkinSDR 08FDEA02336Skin · cracked02 EACH FASTENER HOLES FOUND CRACK INDICATIONS DURING OPEN-HOLE HFEC INSPECTION AT LEFT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 690 AND STATION XORS = 700. CARRIED OUT REPAIR AS PER EA 1-5710-122496 PART 1. THIS REPAIR CLASSIFIED AS MINJun 19, 2008 · N586FE · Doug MD11F · Wing, Plate/SkinSDR 08FDEA02335Support Fitting · crackedMAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 FOUND WITH CRACK INDICATIONS AT HOLES NR A, NR B, NR C AND NR D (THIRD LAYER). MAIN CARGO DOOR LOWER JAMB, CRACKED NR 7 SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01, VOL.II. NEW FITTING FABRICATED ASJun 19, 2008 · N586FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA02334Support Fitting · crackedMAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 6 FOUND WITH CRACK INDICATIONS AT HOLES NR A , NR B , NR C AND NR D (THIRD LAYER). MAIN CARGO DOOR LOWER JAMB, CRACKED NR 6 SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01, VOL.II. NEW FITTING FABRICATED Jun 19, 2008 · N586FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA02333Support Fitting · crackedMAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 5 FOUND WITH CRACK INDICATIONS AT HOLES NR B, NR C AND NR D (THIRD LAYER). REMOVED AND REPLACED AS PER SRM 51-31-01, VOL.II. NEW FITTING FABRICATED AS PER EA 1-5300-122494, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6Jun 19, 2008 · N586FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA02332Support Fitting · crackedMAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 4 FOUND WITH CRACK INDICATIONS AT HOLE NR C (THIRD LAYER). REMOVED AND REPLACED AS PER SRM 51-31-01, VOL.II. NEW FITTING FABRICATED AS PER EA 1-5300-122494, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jun 19, 2008 · N586FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA02331Fitting · crackedMAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 3 FOUND WITH CRACK INDICATIONS AT HOLE NR D (THIRD LAYER). REMOVED AND REPLACED AS PER SRM 51-31-01, VOL.II. NEW FITTING FABRICATED AS PER EA 1-5300-122494, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jun 19, 2008 · N586FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA02330Fitting · crackedMAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 2 FOUND WITH CRACK INDICATIONS AT HOLES NR C AND NR D (THIRD LAYER). REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II. NEW FITTING FABRICATED AS PER EA1-5300-122494, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jun 19, 2008 · N586FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA02329Fitting · crackedMAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 1 FOUND WITH CRACK INDICATIONS AT HOLES NR A AND NR C (THIRD LAYER). REMOVED AND REPLACED AS PER SRM 51-31-01 VOL. II. NEW FITTING FABRICATED AS PER EA 1-5300-122494, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-10Jun 19, 2008 · N586FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 07FDEA00623Cap · corrodedLT WING, REAR SPAR UPPER CHORD AT STA 1035-1043 FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5710-105616, CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.Mar 1, 2007 · N586FE · Doug MD11 · Wing Main, Frame StructureSDR 07FDEA00622Spar Cap · corrodedFOUND LT WING, REAR SPAR LOWER CHORD AT STA 1063 - 1075 CORROSION. LT WING, REAR SPAR LOWER CHORD AT STA 1063 - 1075 REPAIRED AS PER FEDEX EA NR 1- 5710- 105615, WINGS, LEFT WING LOWER SPAR CAP AFT FLANGE CORROSION BETWEEN XORS=1063 AND XORS=1075 - REPAIR. Mar 1, 2007 · N586FE · Doug MD11 · Wing SparSDR 07FDEA00611Relay · burnedELECTRICAL ARCING AT NR 1 EPC BAY LT TOP SIDE RELAY R2-53, R2-57, R2-102 AND R2-252 AFFECTED. REMOVED AND REPLACED 4 RELAYS R2-53, R2-57, R2-102 AND R2-252 AS PER STANDARD WIRING PRACTICES MANUAL. WIRINGS SPLICE REPAIRED AS PER STANDARD WIRING PRACTICES MANFeb 27, 2007 · N586FE · Doug MD11 · Aircraft Fuel Filter/StrainerSDR 07FDEA00475Longeron · corrodedFORWARD CARGO COMPARTMENT: BILGE AREA LONGERON 52 AT STA 979 UPPER FLANGE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5330-105625, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Feb 14, 2007 · N586FE · Doug MD11 · Fuselage Main, Longeron/StringerSDR 07FDEA00451Longeron · crackedAFT CARGO COMPARTMENT RT TUNNEL AREA, LONGERON 38R AT STA 1863 FOUND CRACKED. REPAIRED AS PER SRM 53-10-00 VOLUME I, FIGURE 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Feb 12, 2007 · N586FE · Doug MD11 · Fuselage Main, StructureSDR 07FDEA00448Longeron · corrodedCENTER CARGO COMPARTMENT BILGE AREA LONGERON 52 AT STA 1531 FOUND CORRODED REPAIR CARRIED OUT PER FEDEX EA 1-5310-105623, FUSELAGE, LONGERON L52 AT STA 5-102, SRM SPLICE CLASSIFICATION. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Feb 12, 2007 · N586FE · Doug MD11 · Fuselage Main, Longeron/StringerSDR 07FDEA00450Longeron Splice · crackedAFT CARGO COMPARTMENT, RIGHT TUNNEL AREA LONGERON 38R SPLICE AT STA 1863 FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II. THIS REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100.Feb 12, 2007 · N586FE · Doug MD11 · Fuselage Main, Longeron/StringerSDR 07FDEA00449Longeron · corrodedCENTER CARGO COMPARTMENT, BILGE AREA LONGERON 50L AT FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5310-105620, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Feb 12, 2007 · N586FE · Doug MD11 · Fuselage Main, Longeron/StringerSDR 07FDEA00447Longeron · corrodedWASTE TANK COMPARTMENT, LONGERON 43R END FITTING AT STA 2007 FOUND CORRODED. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Feb 12, 2007 · N586FE · Doug MD11 · Fuselage Main, Longeron/StringerSDR 07FDEA00389Skin · crackedLOWER FUSELAGE EXTERIOR, NR 1 AIRCON EXHAUST CUTOUT CORNER FOUND CRACKED. REPAIRED AS PER SRM 53-50-00 VOLUME I, FIGURE 16. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Feb 9, 2007 · N586FE · Doug MD11 · Fuselage Main, Plate/SkinSDR 07FDEA00374Stringer · crackedCRACK FOUND AT STRINGER END 9R (XORS 819), APPROX 11 INCHES LENGTH ON RIGHT WING TANK DURING HFEC INSPECTION. CRACK ON RT WING AT STRINGER END 9R (XORS 819) REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Feb 8, 2007 · N586FE · Doug MD11F · Wing, Longeron/StringerSDR 07FDEA00373Stringer · crackedCRACK FOUND AT STRINGER END 10R (XORS 760), APPROX 12 INCHES LENGTH ON RIGHT WING TANK DURING HFEC INSPECTION. REPAIRED AS PER SRM 57-20-00 VOLUME I, FIGURE 10. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Feb 8, 2007 · N586FE · Doug MD11F · Wing, Longeron/StringerSDR 07FDEA00372Stringer · crackedCRACK FOUND AT STRINGER END 11R (XORS 704), APPROX 13 INCHES LENGTH ON RIGHT WING TANK DURING HFEC INSPECTION. CRACK ON RT WING AT STRINGER END 11R (XORS 704) REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Feb 8, 2007 · N586FE · Doug MD11F · Wing, Longeron/StringerSDR 07FDEA00371Stringer · crackedCRACK FOUND AT STRINGER END 14L (XORS 521), APPROX 13 INCHES LENGTH ON LT WING TANK DURING HFEC INSPECTION. CRACK ON LT WING AT STRINGER END 14L (XORS 521) REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Feb 8, 2007 · N586FE · Doug MD11F · Wing, Longeron/StringerSDR 07FDEA00366Stringer · crackedCRACK FOUND AT STRINGER END 12R (XORS 642), APPROX 13 INCHES LENGTH ON RIGHT HAND WING TANK DURING HFEC INSPECTION. CRACK ON RIGHT HAND WING (XORS 642) AT STRINGER END 12R REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2Feb 7, 2007 · N586FE · Doug MD11 · Wing, Longeron/StringerSDR 07FDEA00370Stringer · crackedCRACK FOUND AT STRINGER END 13L (XORS 577), APPROX 13 INCHES LENGTH ON LEFT HAND WING TANK DURING HFEC INSPECTION. CRACK ON LT HAND WING AT STRINGER END 13L (XORS 577) REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-1Feb 7, 2007 · N586FE · Doug MD11F · Wing, Longeron/StringerSDR 07FDEA00369Stringer · crackedCRACK FOUND AT STRINGER END 12L (XORS 642), APPROX 12 INCHES LENGTH ON LT WING TANK DURING HFEC INSPECTION. CRACK ON LT WING AT STRINGER END 12L (XORS 642) REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Feb 7, 2007 · N586FE · Doug MD11F · Wing, Longeron/StringerSDR 07FDEA00368Stringer · crackedCRACK FOUND AT STRINGER END 14R (XORS 521), APPROX 14.5 INCHES LENGTH ON RIGHT WING TANK DURING HFEC INSPECTION. CRACK ON RIGHT HAND WING AT STRINGER END 14R (XORS 521) REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-Feb 7, 2007 · N586FE · Doug MD11F · Wing, Longeron/StringerSDR 07FDEA00367Stringer · crackedCRACK FOUND AT STRINGER END 13R (XORS 577), APPROX 13.5 INCHES LENGTH ON RIGHT WING TANK DURING HFEC INSPECTION. CRACK ON RIGHT HAND WING AT STRINGER END 13R (XORS 577) REPAIRED AS PER SRM 57-20- 00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-Feb 7, 2007 · N586FE · Doug MD11F · Wing, Longeron/StringerSDR 06FDEA04017Unknown · malfunctionedON APPROACH, BEFORE AND AFTER SLATS EXT, RUDDER PEDALS WERE EXTREMELY LOOSE. TRAVEL BETWEEN PEDALS WAS - 3-4" EACH WITH NO RUDDER MOVEMENT. ALSO NO RESISTANCE IN THE FIRST 3-4" OF PEDAL TRAVEL. VERIFIED 3-4" OF RUDDER PEDAL MOVEMENT BEFORE ANY MOVEMENT ONov 15, 2006 · N586FE · Doug MD11 · Rudder Control SystemSDR 06FDEA3055Wire · damagedFOUND WIRE BUNDLE DAMAGED IN RT AFT SPAR AREA INBD OF RT MAIN GEAR. WIRE NR" SE201-21-16A, E201-22-16B AND E201-23-16C BURNED THRU ABOUT 1 TO 2 FT INBD OF T-STRIP S3-375. WIRES ARE 3 PHASE WIRES FOR R AFT FUEL PUMP M1-1108. PULLED AND COLLARED AFFECTED C/B.Aug 22, 2006 · N586FE · Doug MD11F · Fuel System WiringSDR 06FDEA1152Controller · malfunctionedRCVD LEVEL 2 AVIONICS AIR FLOW OFF, THEN AVIONICS FAN O'VRD CAME ON. NO -ESC- CURRENT FAULTS NOTED, -ESC- FAULT REVIEW INDICATES NO FAULTS LAST LEG, -EC- SENSOR READOUTS NORMAL. PERFORMED -ESC- RETURN TO SERVICE CK, SYS PASS. REMOVED AND REPLACED ENV SYSTEMar 19, 2006 · N586FE · Doug MD11 · Air Distribution SystemSDR 05FDEA02579Fitting · corrodedEVIDENCE OF MINOR SURFACE CORROSION FOUND ON CENTER LANDING GEAR LEFT TRUNNION FITTING LOWER MATING SURFACE AREA. CORROSION MACHINED OFF AND FOUND WITHIN LIMIT AS PER SRM 53-40-00.Aug 19, 2005 · N586FE · Doug MD11 · Fuselage, Landing Gear Attach FittingsSDR 05FDEA02578Fitting · corrodedEVIDENCE OF SURFACE CORROSION FOUND ON CENTER LANDING GEAR RIGHT TRUNNION FITTING LOWER MATING SURFACE AREA. SURFACE CORROSION ON CENTER LANDING GEAR RIGHT HAND TRUNNION FITTING LOWER MATING SURFACE AREA REMOVED AS PER SRM 51-21-01 VOLUME II PAGE 27. ORIGINALAug 19, 2005 · N586FE · Doug MD11 · Fuselage, Landing Gear Attach FittingsSDR 05FDEA02510Seat Track · corrodedMAIN DECK SEAT TRACK AT STATION Y1092, -X8.5 FOUND CORRODED. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE I VOLUME I AT STATION Y1009 TO STATION Y1129, -X8.5.Aug 18, 2005 · N586FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA02509Seat Track · corrodedCABIN SEAT TRACK AT STATION Y1019, -X8.5 FOUND CORRODED. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE I VOLUME I AT STATION Y1009 TO STATION Y1129, -X8.5.Aug 18, 2005 · N586FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA02512Seat Track · corrodedMAIN DECK SEAT TRACK AT STATION Y1124, -X8.5 FOUND CORRODED. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE I VOLUME I AT STATION Y1009 TO STATION Y1129, -X8.5.Aug 18, 2005 · N586FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA02507Seat Track · corrodedCABIN SEAT TRACK AT STATION Y1049, -X8.5 FOUND CORRODED. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE I VOLUME I AT STATION Y1009 TO STATION Y1129, -X8.5.Aug 18, 2005 · N586FE · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
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