Boeing MD-11F

Service difficulty reports · 31,320

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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"

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SDR FDEA201607042253Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK FLANGE LOWER SIDE FOUND CORROSION AT STA 1821-1854, X=-8, INBD. SEAT TRACK REPAIRED PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jul 4, 2016 · N602FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201607042252Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK FLANGE LOWER SIDE FOUND CORROSION AT STA 1820, X=-8, OTBD. SEAT TRACK REPAIRED PER SRM 53-00-52-2R FIG 201 REPAIR 1. REFER TO SNRM N00987 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jul 4, 2016 · N602FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201607042251Skin · dentedLEFT WING NR 4 SLAT UPPER SURFACE FOUND DENTED AT STA XOS 554.894 TO STA 560.200. DENT EXCEEDED LIMIT OF ALLOWABLE SRM 57-40-02-2R FIG 201 REPAIR 6. DAMAGED AREA TRIM OUT AND REPAIR DOUBLER INSTALLED PER EA 1-5750-T0326476. REPAIR CLASSIFIED AS MAJOR PER GMJul 4, 2016 · N602FE · Doug MD11F · Leading Edge DevicesSDR FDEA201607042269Seat Track · crackedMAIN DECK RT FLOOR SEAT TRACK AT STA 635, X=-47.5 FOUND CRACKED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 625-STA 645X= -47.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 4, 2016 · N582FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201607042268Seat Track · crackedMAIN DECK LT FLOOR SEAT TRACK AT STA 755, X= 8.5 FOUND CRACKED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 745-STA 785 X= 8.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 4, 2016 · N582FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201607042267Seat Track · crackedMAIN DECK LT FLOOR SEAT TRACK AT STA 755, X=47.5 FOUND CRACKED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-52-2R, FIG 201, REPAIR NR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 4, 2016 · N582FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201607042266Seat Track · corrodedMAIN DECK RT FLOOR SEAT TRACK AT STA 778, X=-74.5 FOUND CORROSION AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 765-STA 818 X= -74.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. COMPLIED WITH EA 1-5320-T0326733 P1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-Jul 4, 2016 · N582FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201607042265Seat Track · damagedMAIN DECK LT FLOOR SEAT TRACK AT STA 770, X= 74.5 FOUND CROWN DAMAGED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 765-STA 783 X=74.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 4, 2016 · N582FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201607042264Seat Track · crackedMAIN DECK LT FLOOR SEAT TRACK AT STA 635, X= 47.5 FOUND CRACKED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 625 TO STA 665X=47.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 4, 2016 · N582FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201607042263Seat Track · crackedMAIN DECK LT FLOOR SEAT TRACK AT STA 635, X= 8.5 FOUND CRACKED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 625 TO STA 645 X=8.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 4, 2016 · N582FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201607042262Seat Track · crackedMAIN DECK RT FLOOR SEAT TRACK AT STA 635, X=-8.5 FOUND CRACKED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 625-STA 645 X= -8.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 4, 2016 · N582FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201607042261Seat Track · damagedMAIN DECK RT FLOOR SEAT TRACK AT STA 1425, X=-47.5 FOUND CROWN DAMAGED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1390 TO STA 1431 X = -47.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 4, 2016 · N582FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201607042259Seat Track · damagedMAIN DECK RT FLOOR SEAT TRACK AT STA 1285, X=-8.5 FOUND CROWN DAMAGED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1264 TO STA 1311 X= -8.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR GMM 6-2-100.Jul 4, 2016 · N582FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201607042258Seat Track · corrodedMAIN DECK LT FLOOR SEAT TRACK AT STA 1643, X= 8.5, FOUND CORROSION AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1570 TO STA 1651 X=8.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 4, 2016 · N582FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201607042257Seat Track · damagedMAIN DECK LT FLOOR SEAT TRACK AT STA 5-5, X= 27.5, FOUND CROWN DAMAGED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 5-0 TO STA 5-63 X=27.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 4, 2016 · N582FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201607042256Seat Track · damagedMAIN DECK RT FLOOR SEAT TRACK AT STA 5-5, X= -27.5 FOUND CROWN DAMAGED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 5-0 TO STA 5-63 X= -27.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 4, 2016 · N582FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201607042255Beam · crackedCABIN-L3 DOOR PLUG NR 7 FWD STOP FITTING BEAM FOUND CRACKED. R & R WITH NEW STOP FITTING BEAM IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 4, 2016 · N582FE · Doug MD11F · Passenger/Crew DoorsSDR FDEA201607042247Floor Support · corrodedMAIN DECK, AFT CABIN RT FLOOR SUPPORT AT STA 1887 - STA 2007, X=-25, FOUND CORROSION AS MARKED. R & R WITH NEW FABRICATED FLOOR SUPPORT IAW SRM 51-31-01-0G. NEW FLOOR SUPPORT FABRICATED IAW DWG AGA7087, REV P. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 4, 2016 · N582FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201607042246Web · crackedMAIN DECK L3 DOOR AFT JAMB LOWER WEB BOX AT STA 1305.25 TO 1315.42, LONGERON L26L TO L27L FOUND CRACKED AS MARKED. CARRIED OUT REPAIR IAW SRM 53-40-15-2R, FIG 201 REPAIR NR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 4, 2016 · N582FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201607042245Web · crackedMAIN DECK L3 DOOR FWD JAMB LOWER WEB BOX AT STA 1250.75 TO 1256.75, LONGERON L26L TO L27L, FOUND CRACKED AS MARKED. CARRIED OUT REPAIR IAW SRM 53-40-15-2R, FIG 201. REPAIR NR 3 AND EA 1-5310-T0326798A, PT 1 TITLE: FUSELAGE MAIN FRAME, CENTER FUSELAGE, OVERWIJul 4, 2016 · N582FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201607042244Web · crackedMAIN DECK R3 DOOR FWD JAMB LOWER WEB BOX AT STA 1250.75 TO 1256.75, LONGERON L26R-L27R, FOUND CRACKED AS MARKED. CARRIED OUT REPAIR IAW SRM 53-40-15-2R, FIG 201. REPAIR NR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 4, 2016 · N582FE · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2016070405361Skin · damagedL-1 DOOR OUTER SKIN DAMAGED, REF EO MD11-5210-61106-B FOR REPAIR.Jul 4, 2016 · N279UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2016070405369Skin · damagedLOWER AFT RUDDER SKIN RT SIDE AT STA ZAR 302.089, 8" AFT OF FWD SPAR HAS A .3750" DIAMETER CHIP IN SKIN COMPLETELY THRU TO INTERNAL DOUBLER. R & R LOWER AFT RUDDER AND COMPLETED SATISFACTORY RANGE ON MOVEMENT CHECK IAW AMM 27-20-20-400-801 AND 27-20-00-710-80Jul 4, 2016 · N293UP · Doug MD11F · Rudder, Plate/SkinSDR FDEA201607032241Bushing · corrodedLEFT WING OTBD FLAP VANE FITTING F, BUSHING HOLE, CORRODED. BUSHING HOLE CORROSION REWORKED PER SRM 57-50-02-2R FIGURE 201 AND FOUND EXCEED LIMIT. EXISTING HOLE SIZE 0.860" X 0.5655", FINAL HOLE SIZE: 0.9565" X 0.6585", MAXIMUM ALLOWABLE LIMIT: 0.940" X 0.67Jul 3, 2016 · N602FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201607032240Web · crackedMAIN DECK R3 DOOR AFT JAMB LOWER WEB BOX AT STA 1305.25-STA 1315.42, LONGERON L26R-L27R FOUND CRACKED AS MARKED. WEB BOX REPAIRED PER SRM 53-40-15-2R FIG 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jul 3, 2016 · N602FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201607032239Seat Track · crackedMAIN DECK LT FLOOR SEAT TRACK AT STA 755, X= 27.5 FOUND CRACKED AS MARKED. SEAT TRACK REPAIRED PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jul 3, 2016 · N602FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201607032238Seat Track · crackedMAIN DECK LT FLOOR SEAT TRACK AT STA 755, X=47.5 FOUND CRACKED AS MARKED. SEAT TRACK REPAIRED PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jul 3, 2016 · N602FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201607032237Bushing · corrodedLT WING OUTBOARD FLAP VANE FITTING 'B' BUSHING HOLE CORROSION. BUSHING HOLE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201. EXISTING HOLE SIZE 0.935" X 0.650", FINAL HOLE SIZE: 1.0325" X 0.740", MAXIMUM ALLOWABLE LIMIT: 0.940" X 0.670". OJul 3, 2016 · N602FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201607032236Bushing · corrodedLEFT WING OTBD FLAP VANE FITTING C, BUSHING HOLE CORRODED. BUSHING HOLE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201. EXISTING HOLE SIZE 0.856" X 0.597", FINAL HOLE SIZE: 0.997" X 0.704", MAXIMUM ALLOWABLE LIMIT: 0.940" X 0.670". OVERSIJul 3, 2016 · N602FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201607032235Bushing · corrodedLT WING OTBD FLAP VANE FITTING D, BUSHING HOLE, CORRODED. BUSHING HOLE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201. EXISTING HOLE SIZE 0.876" X 0.580", FINAL HOLE SIZE: 0.953" X 0.660", MAXIMUM ALLOWABLE LIMIT: 0.940" X 0.670". OVERSIZJul 3, 2016 · N602FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201607032250Door · crackedLEFT FWD NOSE GEAR DOOR CRACKED THROUGH 3 RIVETS. APPROXIMATELY 6-8" FROM L/E OF DOOR. REMOVED LT FWD NOSE GEAR DOOR IAW AMM 32-23-03-4. SENT TO SHEETMETAL SHOP. REMOVED DAMAGE ON LT FWD NOSE GEAR DOOR AND REPAIRED IAW SRM 52-00-00-2R.Jul 3, 2016 · N617FE · Doug MD11F · Landing Gear DoorsSDR FDEA201607032243Light · brokenL1 DOOR FOLLOWER CEILING PANEL EMERGENCY EXIT LIGHT FRAME ASSY BROKEN.Jul 3, 2016 · N615FE · Doug MD11F · Emergency LightingSDR FDEA201607032234Beam · corrodedCABIN MAIN DECK CARGO COMPARTMENT. R3 DOOR PLUG NR 7 LOWER DOOR BEAM DAMAGED.Jul 3, 2016 · N602FE · Doug MD11F · Passenger/Crew DoorsSDR FDEA201607032233Floor Support · corrodedMAIN DECK, AFT CABIN RT FLOOR SUPPORT AT STA 1887 -STA 2007, X=-57 FOUND CORROSION AS MARKED.Jul 3, 2016 · N602FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201607032232Hinge Bracket · corrodedLEFT WING OTBD FLAP, FLAP SIDE, INBD AFT HINGE PIVOT INBD HOLE BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT CMM 57-52-04. EXISTING HOLE: DIA 1.154", FINAL HOLE: DIA 1.217", MAXIMUM ALLOWABLE HOLE: DIA 1.150". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA1Jul 3, 2016 · N602FE · Doug MD11F · Trailing Edge FlapsSDR IPXA2016071205744Door Frame · corrodedINSPECTION TYPE: 3C, AFT CARGO DOOR FRAME HAS CORROSION AT BS 1959 BETWEEN X 30 TO 40 AND Z 80. REPAIRED THE DOOR FRAME IAW EA 011-5310-A6351 REV. I/R AND EO MD11-5310-61221-A. (MINOR)Jul 1, 2016 · N285UP · Doug MD11F · Fuselage Main, StructureSDR FDEA201607012228Sensor · defectiveENGINE 2 ANTI-ICE DUCT FAIL, PASSING FL 200 TURNED ON ENGINE ANTI-ICE, RECEIVED NR 2 ENGINE DUCT FAILURE NR 2 ANTI-ICE DISAGREE. QRH INDICATED FAILURE OF NR 2 A/I DUCT. RETURNED TO PAN C WHERE ICING DID NOT EXIST. R & R ALL 3, NR 2 ENGINE COWL ANTI-ICE MANIJul 1, 2016 · N621FE · Doug MD11F · Air Intake Anti/De-Ice SystemSDR IPXA2016070505431Life Vest · openFOUND PASSENGER SEAT LIFE VEST SEAL BROKEN. R&R THE LIFE VEST IAW AMM 25-64-01-2 REV 85.03.Jul 1, 2016 · N272UP · Doug MD11F · Life JacketSDR FDEA201607012220Skin · crackedTWO CRACK INDICATIONS APPROXIMATE 2.0 INCHES IN LENGTH FOUND DURING X-RAY INSPECTION AT STA 6-0, LONGERON SPLICE 4R AFT SECTION EDGE.Jul 1, 2016 · N602FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201607012219Hinge · corrodedLEFT HAND WING OUTBOARD FLAP (WING SIDE) INBOARD FWD HINGE LOWER MOUNT OUTBOARD HOLE BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 0.706", FINAL HOLE DIA: 0.728", MAXIMUM ALLOWABLE HOLE DIA: 0.709". REPAIR BUSHING FABJul 1, 2016 · N602FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201607012218Hinge · corrodedLEFT WING OUTBOARD FLAP (WING SIDE) INBOARD FWD HINGE LOWER MOUNT INBOARD HOLE BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE: DIA 0.706", FINAL HOLE: DIA 0.728", MAXIMUM ALLOWABLE HOLE: DIA 0.709". REPAIR BUSHING FABRICATEDJul 1, 2016 · N602FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201607012214Hinge · corrodedRIGHT WING INBOARD FLAP (FLAP SIDE) OUTBOARD AFT HINGE PIVOT OUTBOARD HOLE BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE: DIA 1.330", FINAL HOLE: DIA 1.336", MAXIMUM ALLOWABLE HOLE: DIA 1.220". OVERSIZE BUSHING FABRICATED Jul 1, 2016 · N602FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201607012213Hinge · corrodedRIGHT WING INBOARD FLAP (FLAP SIDE) OUTBOARD AFT HINGE PIVOT INBOARD HOLE BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03. EXISTING HOLE: DIA 1.330", FINAL HOLE: DIA 1.336", MAXIMUM ALLOWABLE HOLE: DIA 1.220". OVERSIZE BUSHING FABRICATED IAW Jul 1, 2016 · N602FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201607012212Hinge · corrodedLEFT WING INBOARD FLAP (FLAP SIDE) OUTBOARD AFT HINGE PIVOT OUTBOARD HOLE BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.294", FINAL HOLE DIA: 1.327", MAXIMUM ALLOWABLE HOLE DIA: 1.220", OVERSIZE BUSHING FABRICATED ANDJul 1, 2016 · N602FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201607012211Hinge · corrodedLEFT WING INBOARD FLAP (FLAP SIDE) OUTBOARD AFT HINGE PIVOT INBOARD HOLE BORE CORRODED. HINGE REWORKED AND FOUND EXCEED LIMIT PER CMM57-52-03. EXISTING HOLE DIA: 1.294", FINAL HOLE DIA: 1.327", MAXIMUM ALLOWABLE HOLE DIA: 1.220". OVERSIZE BUSHING FABRICATEDJul 1, 2016 · N602FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201607012210Bracket · corrodedLEFT HAND WING INBOARD FLAP (FLAP SIDE) OUTBOARD AFT HINGE ACTUATOR OUTBOARD HOLE BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.219", FINAL HOLE DIA: 1.235" MAXIMUM ALLOWABLE HOLE DIA: 1.220". OVERSIZE BUSHING FABRICATJul 1, 2016 · N602FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201606302205Battery · dischargedR1 DOOR PRESS TO TEST SWITCH INOPERATIVE. REPLACED R-1 DOOR PRESS TO TEST SWITCH BATTERIES. OPS CK GOOD.Jun 30, 2016 · N583FE · Doug MD11F · Emergency EquipmentSDR FDEA201606302203Seat Track · corrodedMAIN DECK CARGO RT FLOOR SEAT TRACK AT STA 492, X=-27.5, FOUND CORROSION AS MARKED.Jun 30, 2016 · N602FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201606302202Seat Track · damagedMAIN DECK CARGO LT FLOOR SEAT TRACK AT STA 1801, X= 47.5. FOUND CROWN DAMAGED AS MARKED.Jun 30, 2016 · N602FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201606302201Seat Track · damagedMAIN DECK CARGO LT FLOOR SEAT TRACK AT STA 5-27, X= 47.5. FOUND CROWN DAMAGED AS MARKED.Jun 30, 2016 · N602FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
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