Boeing MD-11F

Service difficulty reports · 31,320

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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 aircraft_model_key = 'MD11F'
  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 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 IPXA2019103098440Longeron · corrodedINSPECTION TYPE:2CLONGERON 28 R/H SIDE IS CORRODED BETWEEN STA. 1288-1295.REPAIRED CORRODED LONGERON 28 R/H SIDE BETWEEN STA. 1288-1295 IAW VT-SAA EA 011-5310-01-A7935 REV. I/R AND UPS EO MD11-5310-74445-A. (MAJOR)Oct 10, 2019 · N259UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2019102878346Longeron · crackedINSPECTION TYPE:2CCENTER CARGO LONGERON 29R IS CRACKED BETWEEN STA. 1641-1651.REPAIRED CRACKED CENTER CARGO LONGERON 29R BETWEEN STA. 1641-1681 IAW SRM 53-00-05 REPAIR 1 FIG. 201 & 202. (MAJOR)Oct 10, 2019 · N259UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR 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 IPXA2019102538218Longeron · corrodedINSPECTION TYPE:2CCENTER FUSELAGE LONGERON 28L BETWEEN STA Y=1266 - 1297 HAS CORROSION.REPAIRED CORRODED CENTER FUSELAGE LONGERON 28L BETWEEN STA Y=1266 - 1297 IAW VT-SAA EA 011-5310-01-A7933 REV. IR AND UPS EO MD11-5310-74408-A. (MINOR)Oct 10, 2019 · N259UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR 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 IPXA2019102328178Support · corrodedINSPECTION TYPE:2CR/H WING T/E SPOILER PANEL SILL HAS CORROSION BETWEEN STA. XOFH=453.931 AND XOSP=544.75.REPAIRED CORRODED R/H WING SPOILER PANEL SILL BETWEEN STA. XOFH=453.931 TO XOSP=544.75 IAW SRM 57-50-02 REPAIR 10 FIG. 201. (MAJOR)Oct 10, 2019 · N259UP · Doug MD11F · SpoilersSDR FDEA201910102557Floor Support · corrodedFORWARD CABIN FLOOR SUPPORT AT STATION 445, RBL 95 FOUND CORROSION. THE FLOOR SUPPORT WAS FOUND EXFOLIATED AND EXCEEDED LIMITS IAW SRM 53-00-00-2R, FIGURE 206 ALLOWABLE DAMAGE. A NEW FLOOR SUPPORT WAS FABRICATED IAW DRAWING ABA 7341, REVISION C . THE FLOOOct 10, 2019 · N597FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201910102545Skin · delaminatedRIGHT WING OTBD AILERON COMPOSITE STRUCTURE, TOP SURFACE AT LOWER INBD. NEAR T/E SHOWING DELAMINATION. REPAIRED THE RT OTBD AILERON COMPOSITE STRUCTURE IAW SRM 57-60-80-2R AND DRAWING ARC7311.Oct 10, 2019 · N528FE · Doug MD11F · AileronsSDR FDEA2020032792541Actuator · damagedPDIS 603 78-30 6952 09OCT19 PHX OPEN U LOGPAGES:3159490 ON CLIMBOUT RECIEVED LEVEL ONE ALERT "REV 2 PRESS FAULT" AND RED U/L ALERT. SHGN 09OCT19 15:20 PHX U ON ARRIVAL VISUAL CHECK OF REVERSER SHOWS FULLY STOWED, PER CREW DEBRIEF WHEN THE Oct 9, 2019 · N603FE · Doug MD11F · Engine Thrust ReverserSDR IPXA2019102868317Fitting · gougedINSPECTION TYPE:2CRT WING REFUEL ADAPTER FITTING IS GOUGED ON INSIDE.REPAIRED GOUGED RT WING REFUEL ADAPTER FITTING IAW VT-SAA EA 011-5720-01-A7931 REV. IR AND UPS EO MD11-5700-74425-A. (MINOR)Oct 9, 2019 · N259UP · Doug MD11F · Wing Main, Frame StructureSDR FDEA2019101092526Doubler · crackedLEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 754 FOUND CRACKED. REPAIRED THE BEADED DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Oct 9, 2019 · N597FE · Doug MD11F · Wing, Plate/SkinSDR FDEA2019101092525Doubler · crackedLEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 701 FOUND CRACKED. REPAIRED THE BEADED DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Oct 9, 2019 · N597FE · Doug MD11F · Wing, Plate/SkinSDR FDEA2019101092524Seat Track · corrodedFORWARD CABIN SEAT TRACK AT BS 430, RBL 27.5 WAS FOUND WITH CORROSION. THE SEAT TRACK WAS REWORKED IAW DRAWING ABA7684, REVISION G, AND THE CORROSION WAS FOUND EXFOLIATED AND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACOct 9, 2019 · N597FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2019101092515Seat Track · corrodedMAIN DECK FLOOR CURVED SEAT TRACK AT BS 455, RBL 107.25 FOUND CORRODED. THE SEAT TRACK CORROSION WAS FOUND EXFOLIATED , EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. COMPLIED WITH EA 1-5321-T0350175 P1. REPAIR CLASSIFIED AS MAJOR IAWOct 9, 2019 · N597FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2019101092514Doubler · crackedLEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 695 CRACKED. REPAIRED THE BEADED DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Oct 9, 2019 · N597FE · Doug MD11F · Wing, Plate/SkinSDR FDEA2019101092513Doubler · crackedLEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 664 CRACKED. REPAIRED THE BEADED DOUOBLER IAW SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Oct 9, 2019 · N597FE · Doug MD11F · Wing, Plate/SkinSDR FDEA2019101092511Doubler · crackedLEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 640 FOUND CRACKED. REPAIRED THE LEFT WING FIXED LEADING EDGE BEADED DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Oct 9, 2019 · N597FE · Doug MD11F · Wing, Plate/SkinSDR FDEA2019101092510Doubler · crackedLEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 544 CRACKED. REPAIRED THE LT WING FIXED LEADING EDGE BEADED DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Oct 9, 2019 · N597FE · Doug MD11F · Wing, Plate/SkinSDR FDEA2019101092508Doubler · crackedLEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 539 CRACKED. REPAIRED THE LT WING FIXED LEADING EDGE BEADED DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Oct 9, 2019 · N597FE · Doug MD11F · Wing, Plate/SkinSDR IPXA2019101877996Doubler · crackedINSPECTION TYPE:2CLT WING FIXED L/E BEADED DOUBLER CRACK REPAIR BETWEEN STA. XOS. 621 TO XOS. 636 REQUIRES PERMANENT REPAIR.ACCOMPLISHED PERMANENT REPAIR OF LT WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 621 - XOS. 636 IAW MD-11 SRM 57-40-02, REPAIR 15, FIOct 9, 2019 · N259UP · Doug MD11F · Wing, Plate/SkinSDR FDEA2019101092522Seat Track · damagedMAIN DECK SEAT TRACK AT BS 1541, LBL 47.5 WAS FOUND WITH CROWN DAMAGE. DAMAGE EVALUATED AND FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT FROM BS 1571 TO EXISTING SPLCE BS 153Oct 9, 2019 · N597FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2019101092521Seat Track · damagedMAIN DECK SEAT TRACK AT BS 1541, LBL 8.5 FOUND WITH CROWN DAMAGE. DAMAGE EVALUATED AND FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT FROM BS 1571 TO EXISTING SPLICE BS 1531 IAOct 9, 2019 · N597FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2019101092520Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT BS 5-113 X = 8.5 FOUND WITH CORROSION. FOUND EXFOLIATED AND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT FROM STATION 5-83 TO EXISTING SPLICE STATOct 9, 2019 · N597FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2019101092519Seat Track · corrodedMAIN DECK SEAT TRACK AT BS 5-113, RBL 8.5 WAS FOUND WITH CORROSION. FOUND EXFOLIATED AND EXCEEDS LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT BS 5-63 TO 5-123 / 1531 IAW SRM 53-00-52-2R, FOct 9, 2019 · N597FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2019101092518Seat Track · damagedMAIN DECK SEAT TRACK AT BS 5-60, LBL 47.5 FOUND WITH CROWN DAMAGE. DAMAGE EVALUATED AND FOUND TO EXCEED THE LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1 . THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT FROM BS 5- 63 TO EXISTING SPLICE BS Oct 9, 2019 · N597FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
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