N617FE

Service difficulty reports · 467

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 = 'N617FE' 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 FDEA201609203314Wedge · delaminatedRIGHT WING OTBD FLAP INBD TRAILING EDGE WEDGE DELAMINATED. WEDGE REPAIRED AND SMOOTHED AS PER SRM 57-50-80 REPAIR 1 PARA 4A1B. REFER TO WR1 57504399 FOR WORK DETAIL. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 20, 2016 · N617FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201609183306Seat Track · corrodedCABIN, MAIN DECK CARGO COMPARTMENT SEAT TRACK FLANGE CORROSIONS AT RT STA 475, X = -75.25. SEAT TRACK REPAIRED PER SRM 53-00-52-2R FIG 201 REPAIR 5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 18, 2016 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201609183307Hinge · corrodedRIGHT WING OTBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT INBD HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-04. A REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0328400 PART 1 STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Sep 18, 2016 · N617FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201609183305Seat Track · corrodedCABIN, MAIN DECK CARGO COMPARTMENT SEAT TRACK CORROSIONS AT RT STA 615, X = -8.5. SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 585 TO EXISING SPLICE AT STA 625 X= -8.5 PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GSep 18, 2016 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201609183304Hinge · corrodedLEFT WING OTBD FLAP INBD AFT HINGE, FLAP SIDE, PIVOT INBD HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-04. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0328382, PART 1, STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-1Sep 18, 2016 · N617FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201609183303Hinge · corrodedLEFT WING INBD FLAP OTBD AFT HINGE, FLAP SIDE, PIVOT INBD HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM57-52-03. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-75300C P5, STEP 1A & STEP 1C. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2Sep 18, 2016 · N617FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201609183302Hinge · corrodedLEFT WING INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT OTBD HOLE BORE CORRODED. REWORKED AND FOUND TO BE OUT OF LIMITS IAW CMM 57-52-03. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-75300C P5, STEP 1A & STEP 1C. CLASSIFIED AS MAJOR IAW GMM 6-2Sep 18, 2016 · N617FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201609183301Hinge · corrodedRIGHT WING INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT OTBD HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-75312C PART 5 STEP 2 & STEP 4. REPAIR CLASSIFIED AS MAJOR IAW GMM Sep 18, 2016 · N617FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201609183300Hinge · corrodedRIGHT WING INBD FLAP OTBD AFT HINGE, FLAP SIDE, PIVOT INBD HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-75312C PART 5 STEP 4 & STEP 4.Sep 18, 2016 · N617FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201609183299Hinge · corrodedLEFT WING OTBD FLAP INBD FWD HINGE, WING SIDE, PIVOT HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0328351 PART 1 STEP 1A.Sep 18, 2016 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201609183298Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE. LOWER MOUNT OTBD HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0328351 PART 1 STEP 1B.Sep 18, 2016 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201609183297Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0328351 PART 1 STEP 1B AND STEP 1.Sep 18, 2016 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201609183296Hinge · corrodedLEFT WING OTBD FLAP INBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR BUSHING WAS FABRICATED AND INSTALLED EA 1-5750-T0328351 PART 1 STEP 1C.Sep 18, 2016 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201609183295Hinge · corrodedLEFT WING OTBD FLAP INBD FWD HINGE, WING SIDE, ACTUATOR INBD HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0328351 PART 1 STEP 1C.Sep 18, 2016 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201609183294Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0328319 PART 1 STEP 1A AND STEP 1.Sep 18, 2016 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201609183293Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0328319 PART 1, STEP 1A AND STEP 1.Sep 18, 2016 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201609163269Angle · dentedCABIN - MAIN DECK CARGO COMPARTMENT FRAME EXISTING REPAIR ANGLE DENTED AT LT STA 1701, LONGERON 12L. FRAME REPAIR ANGLE REMOVED PER SRM 51-33-01-0G AND REPAIRED PER SRM 53-00-07-2R FIG 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 16, 2016 · N617FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201609163283Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER BARREL NUT HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0328319 PART 1, STEP 1C.Sep 16, 2016 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201609163282Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, UPPER BARREL NUT HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0328319 PART 1, STEP 1C.Sep 16, 2016 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201609163281Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, FWD MOUNT OTBD HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR WAS BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0328319 PART 1, STEP 1B.Sep 16, 2016 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201609163280Hinge · corrodedRIGHT WING OTBD FLAP, INBD FORWARD HINGE, WING SIDE LOWER MOUNT INBD HOLE BORE CORRODED. REWORKED AND FOUND TO BE OUT OF LIMITS IAW CMM 57-44-08. FABRICATED A REPAIR BUSHING AND INSTALLED IAW EA 1-5750-T0328311 PART 1 STEP 1.Sep 16, 2016 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201609163279Hinge Bracket · corrodedRIGHT WING OTBD FLAP INBD FWD HINGE, WING SIDE LOWER MOUNT OTBD HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE: DIA 0.707", FINAL HOLE: DIA 0.729", MAXIMUM ALLOWABLE HOLE: DIA 0.709". REPAIR BUSHING FABRICATED ANDSep 16, 2016 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201609163278Hinge · corrodedRIGHT WING OTBD FLAP, INBD FORWARD HINGE, WING SIDE ACTUATOR INBD HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE: DIA 1.246", FINAL HOLE: DIA 1.250", MAXIMUM ALLOWABLE HOLE: DIA 1.220". REPAIR BUSHING FABRICATED ASep 16, 2016 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201609163277Hinge · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE ACTUATOR OTBD HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE: DIA 1.220", FINAL HOLE: DIA 1.224", MAXIMUM ALLOWABLE HOLE: DIA 1.220". REPAIR BUSHING FABRICATED ANSep 16, 2016 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201609163276Hinge · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE ACTUATOR INBD HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE: DIA 1.249", FINAL HOLE: DIA 1.252", MAXIMUM ALLOWABLE HOLE: DIA 1.220". REPAIR BUSHING FABRICATED AND ISep 16, 2016 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201609163275Hinge · corrodedRT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE LOWER BARREL NUT HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE: DIA 0.406", FINAL HOLE: DIA 0.421", MAXIMUM ALLOWABLE HOLE: DIA 0.391". REPAIR BUSHING FABRICATED AND ISep 16, 2016 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201609163274Hinge Bracket · corrodedRT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE UPPER BARREL NUT HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE: DIA 0.406", FINAL HOLE: DIA 0.421", MAXIMUM ALLOWABLE HOLE: DIA 0.391". REPAIR BUSHING FABRICATED ANSep 16, 2016 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201609163273Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE LOWER MOUNT, OTBD HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE: DIA 0.582", FINAL HOLE: DIA 0.598", MAXIMUM ALLOWABLE HOLE: DIA 0.584". REPAIR BUSHING FABRICATESep 16, 2016 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201609163272Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE LOWER MOUNT INBD HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE: DIA 0.582", FINAL HOLE: DIA 0.598", MAXIMUM ALLOWABLE HOLE: DIA 0.584". REPAIR BUSHING FABRICATEDSep 16, 2016 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201609163271Door Frame · crackedR3 DOOR AFT LOWER FUSELAGE FRAME WEB CRACKED AT BS 1310, BETWEEN LONGERONS 2R AND 27R. REPAIRED IAW SRM 53-40-15-2R, FIG 201, REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Sep 16, 2016 · N617FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201609163270Angle · dentedCABIN, MAIN DECK CARGO COMPARTMENT FRAME EXISTING REPAIR ANGLE DENTED AT RT STA 1681, LONGERON 12R. FRAME ANGLE REMOVED PER SRM 51-33-01-0G AND REPAIRED PER SRM 53-00-07-2R FIG 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 16, 2016 · N617FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201609163268Frame · dentedCABIN MAIN DECK CARGO COMPARTMENT FRAME DENTED AT LT STA 1059, LONGERON 12L. FRAME REPAIRED PER SRM 53-00-07-2R FIG 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 16, 2016 · N617FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201609163267Frame · dentedCABIN, MAIN DECK CARGO COMPARTMENT FRAME DENTED AT LT STA 5-11, LONGERON 12L. FRAME REPAIRED PER SRM 53-00-07-2R FIG 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 16, 2016 · N617FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201609153261Seat Track · corrodedSEAT TRACK FLANGE FOUND CORRODED AT BS 1964 - 2000, X -107. REPAIR AS PER EA 1-5310-T0328362 P1. SEAT TRACK AT X=-107.5 - SPLICE REPAIR FROM STA 1831 TO STA 2007. REFER TO WRI: 53104412 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 15, 2016 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201609153260Seat Track · corrodedSEAT TRACK FLANGE FOUND CORRODED AT BS 1818 - 1872, LBL 47.5. REPAIRED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Sep 15, 2016 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201609153259Seat Track · corrodedSEAT TRACK FLANGE FOUND CORRODED AT BS 1818, RBL 47.5. REPAIRED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Sep 15, 2016 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201609153257Seat Track · corrodedSEAT TRACK FLANGE FOUND WITH CORROSION AT BS 1811, X 27.5. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1771 TO STA 1811 X= 27.5 PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 15, 2016 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201609153256Seat Track · damagedMAIN DECK SEAT TRACK CROWN AREA DAMAGED AT BS 775, X 75.25. SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 816 TO EXISTING SPLICE AT STA 765 X= 75.25 PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 15, 2016 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201609153255Seat Track · damagedMAIN DECK SEAT TRACK CROWN AREA DAMAGED AT BS 6-10, X 8.5. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 6-40 TO EXISTING SPLICE AT STA 6-10 X= 8.5 PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 15, 2016 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201609153254Former · crackedRIGHT WING LEADING EDGE CAVITY AT OUTBOARD OF SLAT TRACK NR 16 FORMER FOUND CRACKED. FORMER REMOVED PER SRM 51-31-01-0G AND FABRICATED NEW FORMER PER DWG ARB2920 REVISION BB. INSTALLED FORMER AT RT WING L/E CAVITY AT O/B OF SLAT TRACK 16 AT XOS 1025.289 PER Sep 15, 2016 · N617FE · Doug MD11F · Wing Main, Frame StructureSDR FDEA201609153253Skin · crackedHFEC INSPECTION CARRIED OUT ON LEFT WING FIXED LEADING EDGE AT CORNER 11, FUEL ACCESS DOOR FWD INBD CORNER AND FOUND ONE CRACK PROPAGATE FROM THE FASTENER HOLE APPROX. 3/8 INCH IN LENGTH, AT XOS 605.844. REPAIR CARRIED OUT PER SRM 57-40-01-2R FIG 201 REPAIRSep 15, 2016 · N617FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201609153252Seat Track · damagedMAIN DECK SEAT TRACK CROWN AREA DAMAGED AT BS 755, X 75.25. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 725 TO EXISTING SPLICE AT STA 765 X= 75.25 PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 15, 2016 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201609153251Seat Track · damagedMAIN DECK SEAT TRACK CROWN AREA DAMAGED AT BS 1290, X 47.5. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1266 TO STA 1331 X= 47.5 AS PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 15, 2016 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201609153250Seat Track · damagedMAIN DECK SEAT TRACK CROWN AREA DAMAGED AT BS 5-11, X -27.5. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 5-63 TO EXISTING SEAT SPLICE AT STA 5.0 X= -27.5 PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 15, 2016 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201609153249Seat Track · damagedMAIN DECK SEAT TRACK CROWN AREA DAMAGED AT BS 5-10, X -47.5. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 5-63 TO EXISTING SPLICE AT STA 5-0 X= -47.5 PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 15, 2016 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201609153248Cargo Track · damagedMAIN DECK SEAT TRACK CROWN AREA DAMAGED AT BS 5-113, X 8.5. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 5-83 TO STA 5-123 X= 8.5 PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 15, 2016 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201609153247Cargo Track · damagedMAIN DECK SEAT TRACK CROWN AREA DAMAGED AT BS 1411, X -8.5. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1391 TO STA 1431 X= -8.5 PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 15, 2016 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 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 FDEA201606242136Wire Harness · chafedDURING APPROACH, AFTER ALL CHECKLISTS COMPLETED, WE HAD A GREEN BOX ON DU NR 3, BUT THEN, LANDING GEAR, BEGAN FLICKERING IN SIDE THE BOX INTERMITTENTLY. WE LOOKED AT THE LANDING GEAR SYNOPTIC. THE LT GEAR INDICATED RED FOR UNSAFE. WENT AROUND CYCLED GEAR FJun 24, 2016 · N617FE · Doug MD11F · Landing Gear System WiringSDR FDEA201603301119Power Supply · inoperativeEMERGENCY LIGHT BATTERY 1 LOW. R & R EMER EXIT LIGHTS POWER SUPPLY IAW 33-51-01-5. OPERATIONS CHECKED NORMAL AT THIS TIME. OK FOR SERVICE.Mar 30, 2016 · N617FE · Doug MD11F · Emergency Lighting
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