N601FE

Service difficulty reports · 546

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 = 'N601FE' 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 FDEA2019101422613Hinge Fitting · corrodedLEFT WING OUTBOARD FLAP, OUTBOARD AFTER HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE CORRODED. CORROSION REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-52-04. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-52-04, AND EA 1-5750-76649 A, PART 2, STOct 12, 2019 · N601FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2019101422610Hinge Fitting · corrodedRIGHT WING INBOARD FLAP, OUTBOARD AFTER HINGE (FLAP SIDE) OUTBOARD PIVOT HOLE BORE CORRODED. CORROSION REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-52-03, AND EA 1-5750-159802 G, PART 3,Oct 12, 2019 · N601FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2019101422609Hinge Fitting · corrodedRIGHT WING INBOARD FLAP, OUTBOARD AFTER HINGE (FLAP SIDE) INBOARD PIVOT HOLE BORE CORRODED. CORROSION REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-52-03, AND EA 1-5750-159802 G, PART 3, Oct 12, 2019 · N601FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2019101422608Hinge Fitting · corrodedLEFT WING INBOARD FLAP, OUTBOARD AFTER HINGE (FLAP SIDE) OUTBOARD PIVOT HOLE BORE CORRODED. CORROSION REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-52-03, AND EA 1-5750-159801 H, PART 3, SOct 12, 2019 · N601FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2019101422607Hinge Fitting · corrodedLEFT WING, INBOARD FLAP OUTBOARD AFTER HINGE (FLAP SIDE) INBOARD PIVOT HOLE BORE CORRODED. CORROSION REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-52-03, AND EA 1-5750-159801 H, PART 3, Oct 12, 2019 · N601FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201910112596Longeron · crackedLOWER CENTER CARGO COMPARTMENT BILGE AREA LONGERON 43 RIGHT FOUND CRACK AT STATION 1821. REMOVED AND INSTALLED FABRICATED LONGERON FITTING AS PER SRM 51-31-01-OG. LONGERON FITTING FABRICATED AS PER DOUGLAS DRAWING AGA 7369 REVISION H. REPAIR CLASSIFIED Oct 11, 2019 · N601FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201910112595Floorbeam · corrodedLOWER CENTER CARGO COMPARTMENT FLOOR BEAM FOUND WITH CORROSION AT STA 1701 X = -34. REPAIR CARRIED OUT AS PER SRM 53-50-51-2R FIGURE 201 REPAIR 1 AND EA # 1-5310- T0350373 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. LOWER CENTER CARGO COMPARTMENOct 11, 2019 · N601FE · Doug MD11F · Fuselage Main, Floor BeamSDR FDEA201910112594Longeron · corrodedLOWER CENTER CARGO COMPARTMENT BILGE AREA LONGERON 44 RIGHT FOUND CORROSION AT STATION 1661 TO 1681. CORROSION REMOVED AS PER SRM 51-21-01-OG AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIGURE 205. LONGERON 44 RIGHT CORROSION AREA CARRIED OUT REPAIR AS Oct 11, 2019 · N601FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201910112593Longeron · corrodedLOWER CENTER CARGO COMPARTMENT BILGE AREA LONGERON 47 RIGHT FOUND CORROSION AT STATION 1731. CORROSION REMOVED AS PER SRM 51-21-01-OG AND FOUND EXCEEDED LIMIT AS PER SRM 53- 00-00-2R, FIG 205. LONGERON 47 RIGHT AT STATION 1731 CARRIED OUT REPAIR AS PER SRMOct 11, 2019 · N601FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201910112597Bulkhead Web · crackedLOWER AFT CARGO COMPARTMENT BILGE AREA FORWARD BULKHEAD FOUND WEB SKIN PUNCTURED AT STA 1841 X = 17. REMOVED AS PER SRM 51-31-01-0G. NEW WEB FABRICATED AS PER DOUGLAS DRAWING AGA7170 REV R AND INSTALLED AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR POct 11, 2019 · N601FE · Doug MD11F · Fuselage Main, BulkheadSDR FDEA201910112598Longeron Splice · crackedLOWER CENTER CARGO COMPARTMENT BILGE AREA LONGERON 51 RIGHT SPLICE FITTING CRACK AT BETWEEN STATION 5-113 TO 1541. LONGERON SPLICE REMOVED AND INSTALLED A FABRICATED SPLICE IAW SRM 51-33-01-OG. SPLICE FITTING FABRICATED AS PER DOUGLAS DRAWING A5A7114 REVIOct 11, 2019 · N601FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201910102569Seat Track · corrodedMAIN DECK CARGO COMPARTMENT SEAT TRACK CORROSION AT BS 675, RBL 100. THE CORROSION WAS REMOVED AND FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101 ALLOWABLE DAMAGE 1. REPAIRED THE SEAT TRACK IAW SRM 53-00-52-2R, REPAIR 5, FIGURE 201, AND EA 1-5310-T0Oct 10, 2019 · N601FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201910102582Hinge Bracket · corrodedRIGHT WING, OUTBOARD FLAP, INBOARD FORWARD HINGE (WING SIDE), OUTBOARD ACTUATOR HOLE BORE CORRODED. THE CORROSION WAS REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0Oct 10, 2019 · N601FE · Doug MD11F · Wing, Control SurfacesSDR FDEA201910102581Hinge Bracket · corrodedRIGHT WING OUTBOARD FLAP, INBOARD FORWARD HINGE (WING SIDE), INBOARD ACTUATOR HOLE BORE CORRODED. THE CORROSION WAS REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T035Oct 10, 2019 · N601FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201910102580Hinge Bracket · corrodedRIGHT WING OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE CORRODED. THE CORROSION WAS REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0350048, PART 1, Oct 10, 2019 · N601FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201910102579Hinge Bracket · corrodedRIGHT WING OUTBOARD FLAP, OUTBOARD FORWARD HINGE (WING SIDE) OUTBOARD ACTUATOR HOLE BORE CORRODED. CORROSION REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350044, Oct 10, 2019 · N601FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201910102578Hinge Bracket · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) INBOARD ACTUATOR HOLE BORE CORRODED. CORROSION REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350044, PART 1, SOct 10, 2019 · N601FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201910102577Hinge Bracket · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) LOWER BARREL NUT HOLE BORE CORRODED. THE NR 7 NUT HOLE BORE WAS REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-57Oct 10, 2019 · N601FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201910102576Hinge Bracket · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) UPPER BARREL NUT HOLE BORE CORRODED. NUT HOLE NR 7 BORE REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T03500Oct 10, 2019 · N601FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201910102575Hinge Bracket · corrodedRIGHT WING OUTBOARD FLAP, OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT, OUTBOARD HOLE SURFACE CORRODED. OUTBOARD HOLE SURFACE REWORKED, AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. A REPAIR SHIM WAS FABRICATED, AND INSTALLED IAW CMM 57-44-09, AND EA 1-5Oct 10, 2019 · N601FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201910102574Hinge Bracket · corrodedRIGHT WING OUTBOARD FLAP, OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT, OUTBOARD NR 3 HOLE BORE CORRODED. THE HOLE BORE WAS REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-57Oct 10, 2019 · N601FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201910102573Hinge Bracket · corrodedRIGHT WING OUTBOARD FLAP, OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT INBOARD HOLE BORE CORRODED. HOLE NR 3 BORE REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T035004Oct 10, 2019 · N601FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201910102572Hinge Bracket · corrodedRIGHT WING OUTBOARD FLAP, OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE CORRODED. HOLE 4 BORE REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44- 09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44- 09, AND EA 1-5750-T0350044, PART 1, SOct 10, 2019 · N601FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201910102566Hinge Bracket · corrodedLEFT WING OUTBOARD FLAP INBOARD FORWARD HINGE, WING SIDE, LOWER MOUNT OUTBOARD HOLE SURFACE WAS CORRODED. HOLE SURFACE REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0350Oct 10, 2019 · N601FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201910102565Hinge Bracket · corrodedLEFT WING OUTBOARD FLAP, INBOARD FORWARD HINGE, WING SIDE LOWER MOUNT INBOARD HOLE SURFACE CORRODED. HOLE SURFACE REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0350113Oct 10, 2019 · N601FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201910102564Hinge Bracket · corrodedLEFT WING OUTBOARD FLAP INBOARD FORWARD HINGE PIVOT HOLE BORE FOUND CORRODED. REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08 AND EA 1-5750-T0350113, PART 1, STEP 1A, AND STEP 1. THOct 10, 2019 · N601FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201910102562Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE), OUTBOARD ACTUATOR HOLE BORE WAS CORRODED. THE CORROSION WAS REWORKED, AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-575Oct 10, 2019 · N601FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201910102560Hinge Bracket · corrodedLEFT WING OUTBOARD FLAP, INBOARD FORWARD HINGE (WING SIDE), INBOARD ACTUATOR HOLE BORE FOUND CORRODED. REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0350113, PART 1, Oct 10, 2019 · N601FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201910102559Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE), OUTBOARD FWD MOUNT HOLE BORE FOUND CORRODED. THE CORROSION WAS REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-57Oct 10, 2019 · N601FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201910102556Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP, INBOARD FORWARD HINGE (WING SIDE), INBOARD FWD MOUNT BORE WAS CORRODED. THE CORROSION WAS REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0Oct 10, 2019 · N601FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201910102555Hinge Bracket · corrodedLEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE), UPPER MOUNT, OUTBOARD HOLE BORE CORRODED. THE CORROSION WAS REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-TOct 10, 2019 · N601FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201910102554Hinge Bracket · corrodedLEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE), LOWER MOUNT OUTBOARD HOLE SURFACE CORRODED. SURFACE REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350013, PART 1,Oct 10, 2019 · N601FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201910102553Hinge Bracket · corrodedLEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE), LOWER MOUNT INBOARD HOLE SURFACE CORRODED. SURFACE REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350013, PART 1, Oct 10, 2019 · N601FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201910102552Hinge Bracket · corrodedLEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE), LOWER MOUNT OUTBOARD HOLE BORE CORRODED. CORROSION REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING WAS FABRICATED, AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350013, Oct 10, 2019 · N601FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201910102551Hinge Bracket · corrodedLEFT HAND WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT INBOARD HOLE BORE CORRODED. REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. SHOULDER BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350013, PART 1, STEP 1.Oct 10, 2019 · N601FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201910102550Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) BARREL NUT HOLE BORE WAS CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED, AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T035001Oct 10, 2019 · N601FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201910102549Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE), LOWER BARREL NUT HOLE BORE CORRODED. REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350013, PART 1, STEP 1Oct 10, 2019 · N601FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201910102548Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE), UPPER BARREL NUT HOLE BORE CORRODED. REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350013, PART 1, STEP Oct 10, 2019 · N601FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201910102547Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE), OUTBOARD ACTUATOR HOLE BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. OVERSIZED BUSHING FABRICATED, AND INSTALLED IAW CMM 57-44-09 AND EA 1-5750-T0350013 PART 1 STEP 1 . REPAIR Oct 10, 2019 · N601FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201910102546Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) INBOARD ACTUATOR HOLE BORE CORRODED. REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350013, PART 1, STEP 1. THE ROct 10, 2019 · N601FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201910102563Doubler · crackedRIGHT WING BEADED DOUBLER AT STA XOS 564 WAS FOUND CRACKED. THE BEADED DOUBLER WAS REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Oct 10, 2019 · N601FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201910102558Doubler · crackedRIGHT WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 643 WAS FOUND CRACKED. THE BEADED DOUBLER WAS REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Oct 10, 2019 · N601FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201910102571Seat Track · crackedMAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK WAS FOUND CRACKED BETWEEN BS 1581 - 1641, RBL 8.5. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT AT EXISTING SPLICE BS 1571 TO 1651 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED IAW Oct 10, 2019 · N601FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201910102570Seat Track · corrodedMAIN DECK CARGO COMPARTMENT SEAT TRACK FLANGE CORRODED BS 5-91, RBL 8.5. THE CORROSION WAS REMOVED AND FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101. THE SEAT TRACK WAS REPAIRED BY SECTIONAL AT EXISTING SPLICES BS 5-63 TO BS 1531, IAW SRM 53-00-52-Oct 10, 2019 · N601FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201910102568Doubler · crackedLEFT WING BEADED DOUBLER AT XOS 692 FOUND CRACKED. THE DOUBLER WAS REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Oct 10, 2019 · N601FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201910102567Doubler · crackedLEFT WING BEADED DOUBLER AT STA XOS 763 WAS FOUND CRACKED. THE BEADED DOUBLER WAS REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Oct 10, 2019 · N601FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201910102561Doubler · crackedLEFT WING BEADED DOUBLER AT STA XOS 795 FOUND CRACKED. THE BEADED DOUBLER WAS REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Oct 10, 2019 · N601FE · Doug MD11F · Wing, Plate/SkinSDR FDEA2019062081392Scuff Plate · damagedSCUFF PLATE DAMAGED OF THE LOWER FWD CARGO DOOR REPAIRED DAMAGE IN ACCORDANCE WITH EA 1-5330-T0347600 A, PS P2.Jun 18, 2019 · N601FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA2019060651224Duct · damaged#3 MANIFOLD FAILURE. SHGN 08JUN19 09:03 KIX INSTALLED NEW DUCT PER AMM 36-14-02-4 AND NO LEAK NOTED. ALSO #3 PNEUMATIC SYSTEM DECAY CHECK W/APU AIR SATISFACTORY PER MD11 JRH. MDC FLOOR BOARD AND SIDEWALL PANEL IN FWD CARGO COMPARTMENT BEING INSTALLED PEJun 5, 2019 · N601FE · Doug MD11F · Pneumatic Indicating SystemSDR FDEA201905181095Cable · shortedPDIS 601 26-10 0334 17MAY19 MEM OPEN U LOGPAGES:2723226 LVL 3 ENG 2 FIRE LIGHT PASSING FL 290. NR 2 ENG. FIRE LOOP "A" DEFERRED. COMPLIED W/ QRH FOUND RIGID CABLE BETWEEN DH7 AND DH8 SHORTED, ALSO FOUND UPP TUR RIGHT A AND B RAIL ASSEMBLY BROKE May 18, 2019 · N601FE · Doug MD11F · Fire Detection
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