N602FE

Service difficulty reports · 506

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 = 'N602FE' 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 FDEA200901110132Skin · misrepairedFUSELAGE EXTERIOR SKIN AT STA 6-90 LONGERON 33L TO 34L FOUND WITH EXISTING DOUBLER REPAIR. EXISTING DOUBLER REPAIR AT FUSELAGE EXTERIOR SKIN AT STA 6-90 LONGERON 33L TO 34L EVALUATED AND FOUND NOT IN ACCORDANCE WITH SRM 53-20-00 FIGURE 2 VOLUME I. REPAIR CJan 11, 2009 · N602FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA200901110148Seat Track · corrodedMAIN DECK, FLOOR PANEL SEAT TRACK AT STA 1541, X = 8.5 FOUND WITH CORROSION. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG 1 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jan 11, 2009 · N602FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200901110146Bracket · corrodedRIGHT WING INBOARD FLAP OUTBOARD AFT HINGE OUTBOARD PIVOT BORE FOUND WITH CORROSION. REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-52-03. NEW BUSHING FABRICATED AND INSTALLED AS PER E.A. 1-5750-127721. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jan 11, 2009 · N602FE · Doug MD11F · Trailing Edge FlapsSDR FDEA200901110145Bracket · corrodedRIGHT WING INBOARD FLAP OUTBOARD AFT HINGE INBOARD PIVOT BORE FOUND WITH CORROSION. REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-52-03. NEW BUSHING FABRICATED AND INSTALLED AT RT WING INBOARD FLAP OUTBOARD AFT HINGE INBOARD PIVOT BORE AS PER E.A. 1-5750Jan 11, 2009 · N602FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200901110144Bracket · corrodedLEFT WING INBOARD FLAP OUTBOARD AFT HINGE OUTBOARD PIVOT BORE FOUND WITH CORROSION. OUTBOARD PIVOT BORE HOLE AT LEFT HAND WING INBOARD FLAP OUTBOARD AFT HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-52-03. NEW BUSHING FABRICATED AND INSTALLED AT LTJan 11, 2009 · N602FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200901110143Bracket · corrodedLEFT WING INBOARD FLAP OUTBOARD AFT HINGE INBOARD PIVOT BORE FOUND WITH CORROSION. INBOARD PIVOT BORE AT LT WING INBOARD FLAP OUTBOARD AFT HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-52-03. NEW BUSHING FABRICATED AND INSTALLED AS PER E.A. 1-575Jan 11, 2009 · N602FE · Doug MD11F · Trailing Edge FlapsSDR FDEA200901070074Skin · misrepairedLEFT WING INBOARD TRAILING EDGE FLAP INBOARD LOWER SEGMENT UPPER SURFACE FOUND AN EXISTING REPAIR AT OUTBOARD EDGE AREA. EXISTING REPAIR AT LEFT WING INBOARD TRAILING EDGE FLAP INBOARD LOWER SEGMENT UPPER SURFACE OUTBOARD EDGE AREA EVALUATED AND FOUND NOT CJan 7, 2009 · N602FE · Doug MD11F · Trailing Edge FlapsSDR FDEA200901070055Skin · misrepairedLEFT WING INBOARD TRAILING EDGE FLAP UPPER SURFACE FOUND WITH AN EXISTING REPAIR, LOCATION: 68 INCH FROM TRAILING EDGE AND 70 INCH FROM INBOARD EDGE OF FLAP. LEFT WING INBOARD TRAILING EDGE FLAP UPPER SURFACE EXISTING REPAIR EVALUATED AND FOUND NOT ACCOMPLIJan 7, 2009 · N602FE · Doug MD11F · Trailing Edge FlapsSDR FDEA200901070053Skin · misrepairedLEFT WING INBOARD TRAILING EDGE FLAP LOWER INBOARD SEGMENT UPPER SURFACE FOUND WITH AN EXISTING REPAIR, LOCATION: 12 INCH FROM TRAILING EDGE AND 88 INCH FROM INBOARD OF FLAP. EXISTING REPAIR AT LEFT WING INBOARD TRAILING EDGE FLAP LOWER INBOARD SEGMENT UPPER Jan 7, 2009 · N602FE · Doug MD11F · Trailing Edge FlapsSDR FDEA200901070078Seat Track · corrodedMAIN DECK, FLOOR PANEL SEAT TRACK FROM STA 5-20 TO STA 5-60, X = 8.5 FOUND CORROSIONS AT SEVERAL LOCATIONS, MAIN DECK, CORRODED SEAT TRACK FROM STA 5-20 TO STA 5-60, X = 8.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 5-0 TO STA 5-123, X = 8.5 AS PJan 7, 2009 · N602FE · Doug MD11F · Fuselage Main, StructureSDR FDEA200901070080Longeron · crackedAFT CARGO, WASTE COMPARTMENT STA 2007, LONGERON 47L, LONGERON SPLICE FITTING CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jan 7, 2009 · N602FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA200901070077Skin · chafedRIGHT WING DROOP LEADING EDGE INBOARD EDGE SKIN WITH CHAFE MARK. REPAIRED AS PER E.A. 1-5750-127877. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jan 7, 2009 · N602FE · Doug MD11F · Wing, Plate/SkinSDR FDEA200901070076Longeron · crackedCRACK INDICATION FOUND APPROXIMATELY 2.5 INCH DURING X-RAY INSPECTION AT STA 5-0, LONGERON 2R AFT SECTION EDGE. CRACKED LONGERON 2R AT STA 5-0 REPAIRED AS PER SRM 53-10-00 FIGURE 2 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jan 7, 2009 · N602FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA200901070073Stanchion · corrodedFORWARD CARGO, DURING POST OPEN UP FOR THRUST REVERSER MODIFICATION, STA 6-70, X = 50, AFT BULKHEAD STANCHION FOUND CORRODED. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. STANCHION FABRICATED PER DRAWING A6A7094. REPAIR CLASSIFIED AS MINOR PER GMM 6Jan 7, 2009 · N602FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA200901070050Mount · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE ACTUATOR MOUNT OUTBOARD BORE FOUND WITH CORROSION. COMPLIED WITH E.A. 1-5750-127715. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jan 7, 2009 · N602FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200901070049Mount · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE ACTUATOR MOUNT INBOARD BORE FOUND WITH CORROSION. COMPLIED WITH E.A. 1-5750-127715. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jan 7, 2009 · N602FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200901040025Door Frame · crackedCRACK INDICATION FOUND DURING HFEC OPEN HOLE INSP ON 0.460 INCH HOLES AT MAIN CARGO DOOR LWR JAMB NR 6 SUPPORT FITTING AT HOLES A, B, C AND D. REMOVED & REPLACED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jan 4, 2009 · N602FE · Doug MD11F · Cargo/Baggage DoorsSDR FDEA200901040024Door Frame · crackedCRACK INDICATION FOUND DURING HFEC OPEN HOLE INSP ON 0.460 INCH HOLES AT MAIN CARGO DOOR LWR JAMB NR 7 SUPPORT FITTING AT HOLES A, B , C AND D. REMOVED & REPLACED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jan 4, 2009 · N602FE · Doug MD11F · Cargo/Baggage DoorsSDR FDEA200901040023Support Fitting · damagedCRACK INDICATION FOUND DURING HFEC OPEN HOLE INSP ON 0.460 INCH HOLES AT MAIN CARGO DOOR LWR JAMB NR 5 SUPPORT FITTING AT HOLES A, B, C AND D. REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jan 4, 2009 · N602FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA200901040022Support Fitting · damagedCRACK INDICATION FOUND DURING HFEC OPEN HOLE INSP ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 4 SUPPORT FITTING AT HOLES A, B, C AND D. REPAIR CARRIED OUT AS PER SRM 53 -50-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jan 4, 2009 · N602FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA200901040021Support Fitting · damagedCRACK INDICATION FOUND DURING HFEC OPEN HOLE INSP ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 3 SUPPORT FITTING AT HOLES A, B, C AND D. REMOVED & REPLACED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jan 4, 2009 · N602FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA200901040020Support Fitting · crackedCRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 2 SUPPORT FITTING AT HOLES A, B, C AND D. SUPPORT FITTING REMOVED & REPLACED AS PER SRM 51-31-01 VOL II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-1Jan 4, 2009 · N602FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA200901040019Support Fitting · crackedCRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 1 SUPPORT FITTING AT HOLES A, B, C AND D. SUPPORT FITTING REMOVED & REPLACED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-1Jan 4, 2009 · N602FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA200901040018Mount · corrodedRIGHT WING OUTBOARD FLAP INBOARD FORWARD HINGE AFT LOWER MOUNT OUTBOARD BORE FOUND WITH CORROSION. COMPLIED WITH E.A. 1-5750-127716. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jan 4, 2009 · N602FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200901040017Mount · corrodedRIGHT WING OUTBOARD FLAP INBOARD FORWARD HINGE AFT LOWER MOUNT INBOARD BORE FOUND WITH CORROSION. COMPLIED WITH E.A. 1-5750-127716. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Jan 4, 2009 · N602FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200901040016Mount · corrodedLEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE AFT LOWER MOUNT NUT SIDE FACE FOUND CORROSION. REPAIRED AS PER E.A. 1-5750-127870, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jan 4, 2009 · N602FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200901040015Mount · corrodedLEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE INBOARD ACTUATOR MOUNT BORE FOUND WITH CORROSION. COMPLIED WITH E.A 1-5750-127714. CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100.Jan 4, 2009 · N602FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200901040014Bracket · corrodedLEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE AFT LOWER MOUNT OUTBOARD BORE FOUND WITH CORROSION. REPAIRED AS PER E.A. 1-5750-127870, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jan 4, 2009 · N602FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200901040013Bracket · corrodedLEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE AFT LOWER MOUNT INBOARD BORE FOUND WITH CORROSION. REPAIRED AS PER E.A. 1-5750-127870, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jan 4, 2009 · N602FE · Doug MD11F · Trailing Edge FlapsSDR 07FDEA02769Skin · crackedWITH REFERENCE TO EA NR 1-5710-90773 DURING ACCOMPLISHMENT OF ALI 57.23.01.2. TWO MOUNTING BORES THE TANKS ACCESS PLATE AT STA XORS = 713.6 GAVE A CRACK INDICATION. THE BORES WERE INCREASED TO 0.310" WHERE CRACK INDICATION CEASED. COMPLIED WITH FEDEX EA NR Aug 5, 2007 · N602FE · Doug MD11F · Wing, Plate/SkinSDR 07FDEA02659Longeron · crackedLONGERON 38R AT STA 1863 FOUND CRACKED. CARRIED OUT REPAIR AS PER SRM 53-10-00 FIGURE 2 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jul 29, 2007 · N602FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 07FDEA02658Longeron · damagedLONGERON 38R AT STA 1864 FOUND WITH HOLE DIAMETER AS 1/4" SIZE. REPAIR CARRIED OUT AS PER FEDEX EA 1-5310-114762. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jul 29, 2007 · N602FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 07FDEA02657Longeron · damagedLONGERON 37R AT STA 1841 FOUND WITH FASTENER HOLE AS 1/4" SIZE. REPAIR CARRIED OUT PER FEDEX EA 1-5310-114762. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jul 29, 2007 · N602FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 07FDEA02656Longeron · damagedLONGERON 39R AT STA 1857 FOUND WITH FASTENER HOLE ELONGATED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5310-114762, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jul 29, 2007 · N602FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 07FDEA02655Longeron · damagedLONGERON 38R AT STA 1865 FOUND WITH SHORT PITCHES. REPAIR CARRIED OUT AS PER FEDEX EA 1-5310-114762. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jul 29, 2007 · N602FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 07FDEA02660Skin · dentedFUSELAGE RT SIDE AT STA 1841-1855 BETWEEN X = 35 AND X = 36 FOUND DENTED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5310-114762. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jul 29, 2007 · N602FE · Doug MD11F · Fuselage Main, Plate/SkinSDR 07FDEA02533Seat Track · corrodedMAIN DECK CARGO ALONG CENTER STA 1521 TO 5-93 SEAT TRACK AROUND FASTENER HOLE AREA FOUND WITH CORROSION. [08-02-07] CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 6 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jul 20, 2007 · N602FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02532Skin · crackedCRACK INDICATIONS REVEALED IN 04 FASTENER HOLES TOWARDS EDGE OF ACCESS, CUTOUT IN RIGHT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS = 683.4 AND XORS = 713.6. [08-06-07] REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-112360, REPAIR CLASSIFIED AS MAJOR PER GJul 20, 2007 · N602FE · Doug MD11F · Wing, Plate/SkinSDR 07FDEA02531Skin · crackedCRACK INDICATIONS REVEALED IN 04 EACH FASTENER HOLES TOWARDS EDGE OF ACCESS CUTOUT IN LEFT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS = 683.4 AND XORS = 713.6. [08-06-07] REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-112359, REPAIR CLASSIFIED AS MAJOR PER Jul 20, 2007 · N602FE · Doug MD11F · Wing, Plate/SkinSDR 07FDEA02530Structure · corrodedCENTER ACCESSORY COMPARTMENT BILGE AREA AT LONGERON 51R BETWEEN STA 1139 AND STA 1159, FOUND CORROSION. [08-06-07] REMOVED AND REPLACED WITH NEW LONGERON AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jul 20, 2007 · N602FE · Doug MD11F · Fuselage Main, StructureSDR 07FDEA02529Seat Track · corrodedMAIN DECK CARGO ALONG CENTER STA 1501 TO 1521 SEAT TRACK AROUND FASTENER HOLE AREA FOUND WITH CORROSION. [07-30-07] CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 6 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jul 20, 2007 · N602FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02520Seat Track · damagedMAIN DECK CARGO CENTER STA 635 BETWEEN FLOOR PANELS NR 232FF AND NR 233GF, FOUND SEAT TRACK CROWN AREA CHIPPED OFF. CARRIED OUT REPAIR ON DAMAGED SEAT TRACK AT STA 625 TO STA 645 AS PER SRM 53-70-00 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jul 19, 2007 · N602FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02506Skin · dentedWITH REFERENCE TO WORK CARD NR T1-5310-96612 PT2, DENT FOUND IN FUSELAGE AT STA 1851 BETWEEN LONGERON 35R AND LONGERON 36R. [08-06-07] REPAIR CARRIED OUT AS PER FEDEX EA 1-5310-114762, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jul 17, 2007 · N602FE · Doug MD11F · Fuselage Main, Plate/SkinSDR 07FDEA02505Vane · delaminatedRIGHT WING OUTBOARD FLAP VANE UPPER SURFACE FOUND DELAMINATED. [07-30-07] COMPLIED WITH FEDEX E.A. 1-5750-112356. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jul 17, 2007 · N602FE · Doug MD11F · Trailing Edge FlapsSDR 07FDEA02504Slat Track · crackedFOUND CRACK, RIGHT WING SLAT TRACK NR 14 CUTOUT. [07-30-07] REPAIRED AS PER SRM 57-10-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jul 17, 2007 · N602FE · Doug MD11F · Leading Edge DevicesSDR 07FDEA02497Trunnion · crackedNOSE LANDING GEAR RIGHT TRUNNION FITTING FOUND CRACKED. [08-03-07] CARRIED OUT REPAIR AS PER SRM 53-40 -00 FIGURE 23 VOLUME I. REPETITIVE INSPECTION TO BE CARRIED OUT NOT EXCEEDING 1,500 LANDING INTERVALS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jul 16, 2007 · N602FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR 07FDEA02496Trunnion · crackedNOSE LANDING GEAR LEFT TRUNNION FITTING FOUND CRACKED. [08-03-07] CARRIED OUT REPAIR AS PER SRM 53-40- 00 FIGURE 23 VOLUME I. REPETITIVE INSPECTION TO BE CARRIED OUT NOT EXCEEDING 1,500 LANDING INTERVALS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jul 16, 2007 · N602FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR 07FDEA02495Stop Fitting · crackedLEFT WING OUTBOARD FLAP SECONDARY UP STOP FITTING FOUND CRACKED. [08-02-07] REMOVED CRACKED FITTING AND INSTALLED NEW FITTING AT LT WING OUTBOARD FLAP AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jul 16, 2007 · N602FE · Doug MD11F · Wing Miscellaneous StructureSDR 06FDEA1421Fire Warning · false activationAT APPROX 2000 AT DEPARTURE, GOT NR 3 ENGINE FIRE WARNING LIGHTS AND BELLS. INTERMITTENT AT FIRST 5-10 SEC AND STEADY AT 20 SEC PHASE 1 AND CHECKLIST COMPLIED WITH. SHUTDOWN ENGINE, DISCHARGED BOTTLE. NO FUEL DUMP. NO OTHER ABNORMAL ENGINE INDICATIONS. DIApr 12, 2006 · N602FE · Doug MD11 · Fire DetectionSDR 06FDEA1011Floor Support · corrodedMAIN DECK BAY FLOOR SUPPORT FOUND WITH CORROSION AT BS 1914 LBL 47-75. MAIN DECK BAY CORRODED FLOOR SUPPORT AT BS 1941 LBL 47-75 REMOVED AND REPLACED BY FABRICATION AS PER DRAWING AGA7085 AND INSTALLED AS PER SRM 51-31 -01 VOLUME II. REPAIR CLASSIFIMar 13, 2006 · N602FE · Doug MD11 · Fuselage Miscellaneous Structure
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