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 FDEA201709122490Hinge Bracket · corrodedRIGHT WING OUTBD FLAP OUTBD HINGE (WING SIDE) LOWER MOUNT INBD HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335331, PART 1, STEP 2B, AND STEP 2.Sep 12, 2017 · N586FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201709122489Hinge Bracket · corrodedRIGHT WING OTBD FLAP OUTBD HINGE (WING SIDE) UPPER MOUNT OTBD HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335331, PART 1, STEP 2A.Sep 12, 2017 · N586FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201709122488Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) ACTUATOR OUTBD LUG HOLE BORE FOUND CORRODED. THE HOLE BORE WAS REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335322, PART 1, STEP 2D.Sep 12, 2017 · N586FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201709122487Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) BARREL NUT HOLE SPOT SURFACE FOUND CORRODED. SURFACE REWORKED IAW CMM 57-44-09. A REPAIR SHIM FABRICATED AND INSTALLED IAW CMM 57-44-09.Sep 12, 2017 · N586FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201709122486Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) ACTUATOR INBD LUG HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335322, PART 1, STEP 2D.Sep 12, 2017 · N586FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201709122485Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) BARREL NUT LOWER HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335322, PART 1, STEP 2C.Sep 12, 2017 · N586FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201709122484Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) BARREL NUT UPPER HOLE BORE FOUND CORRODED. BORE REWORKED AND FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335322, PART 1, STEP 2C.Sep 12, 2017 · N586FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201709122483Hinge Bracket · corrodedLEFT WING OUTBD FLAP OTBD HINGE (WING SIDE) LOWER MOUNT OTBD HOLE FWD AND AFT SURFACE FOUND CORRODED. MOUNT BORE, FWD AND AFT SURFACE REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335322, PART 1Sep 12, 2017 · N586FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201709122482Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) LOWER MOUNT INBD HOLE FWD AND AFT SURFACE FOUND CORRODED. BORE FWD AND AFT SURFACE REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335322, PART 1, STEPSep 12, 2017 · N586FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201709122481Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) LOWER MOUNT OUTBD HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335322, PART 1, STEP 2 AND 2A.Sep 12, 2017 · N586FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201709122480Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE ( WING SIDE ) LOWER MOUNT INBD HOLE BORE FOUND CORRODED., THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335322, PART 1, STEP 2 AND 2A.Sep 12, 2017 · N586FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201709122479Hinge Bracket · corrodedLEFT WING OUTBD FLAP OTBD HINGE ( WING SIDE ) UPPER MOUNT OTBD HOLE BORE FOUND CORRODED. BORE REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335322, PART 1, STEP 2B.Sep 12, 2017 · N586FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR IPXA2017091221658Drive Assy · failedR1 DOOR INTERCOSTAL DAMAGED DUE TO DRIVE MECHANISM FAILURE. REPAIRED IAW EO MD11-5310-65637-ASep 11, 2017 · N283UP · Doug MD11F · Service DoorsSDR IPXA2017091221663Guard · brokenR1 DOOR AFT CABLE DRUM AND SUPPORT ASSY ROLLER CHAIN GUARD BRACKET BROKEN. R & R THE CHAIN GUARD ASSY IAW MM 20-50-02.Sep 11, 2017 · N283UP · Doug MD11F · Service DoorsSDR FDEA201709112477Support Fitting · corrodedRIGHT WING OUTBOARD FLAP VANE NR 1 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORRODED. BORE REWORKED AND FOUND OUT OF LIMITS IAW SRM 57-50-02-2R, FIG 201. AN OVERSIZED WAS FABRICATED IAW EA 1-5750-T0335352, PART 1, STEP 3, TEST CARRIED OUT IAW AMM 27- 50-32Sep 11, 2017 · N586FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201709112476Support Fitting · corrodedLEFT WING OUTBOARD FLAP VANE NR 5 SUPPORT FITTING BORE FOUND CORRODED. BORE REWORKED AND FOUND OUT OF LIMITS IAW SRM 57-50-02-2R, FIG 201. AN OVERSIZED BUSHING WAS FABRICATED IAW EA1-5750-T0335345, PART 1, STEP 1A. INSTALLED IAW AMM 27-50-32-4. LT WING FLAPSep 11, 2017 · N586FE · Doug MD11F · Trailing Edge FlapsSDR IPXA2017091121546Skin · damagedINSPECTION TYPE: PS-1, APPROXIMATE 5 INCHE AREA OF DAMAGE, AFT OF FWD LWR CARGO DOOR ON FUSELAGE SKIN BS 1039 ABOVE LONGERON 38R. FABRICATED A REPAIR DOUBLER AND TRIPLER. INSTALLED THE REPAIR IAW EO MD-11-5330-65609A, PARA 6A.Sep 10, 2017 · N252UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2017091121611Girt Bar · obstructedL1 DOOR SLIDE INOPERATIVE. ADJUSTED THE DOOR LOWER COVER, FOUND SIGHT GLASS INTERFACING WITH THE GRIT BAR. CHECKED IAW AMM 52-10-01-700-803, AND AMM 25-23-07-000-802.Sep 10, 2017 · N292UP · Doug MD11F · Emergency EquipmentSDR IPXA2017090821474Insert · damagedCAPTAIN'S EVAS CONTAINER CAME LOOSE AND FELL ONTO THE COCKPIT FLOOR DURING TAKEOFF. REPAIRED THE INSERTS ON THE EVAS CONTAINER.Sep 7, 2017 · N257UP · Doug MD11F · Emergency EquipmentSDR FDEA201709062462Power Supply · failedDURING CA'S PREFLIGHT CHECKS RECEIVED "EMER LT BATT 1 LO" LVL1 ALERT. REMOVED AND REPLACED EMERG POWER SUPPLY REF 33-51-01-4.Sep 6, 2017 · N589FE · Doug MD11F · Emergency LightingSDR IPXA2017090721448Warning Message · false activationEMERGENCY LIGHT BATTERY 1 LOW ILLUMINATED DURING PREFLIGHT. PERFORMED AN EMERGENCY LIGHT SYS TEST. OPS TESTED NORMAL. OK FOR SERVICE IAW AMM 33-50-00/501.Sep 6, 2017 · N254UP · Doug MD11F · Emergency LightingSDR IPXA2017090721435Bulkhead Web · crackedA DENT AND CRACK FOUND ON THE AFT BULKHEAD AT BS 2033, 17 INCHES FROM BOTTOM OF WEB. INSTALLED A DOUBLER REPAIR IAW EO MD11-5310-65566-A.Sep 6, 2017 · N289UP · Doug MD11F · Fuselage Main, BulkheadSDR FDEA201709052458Cable · brokenL1 DOOR MAIN AFT DRIVE CABLE BROKEN. REF IPC 52-11-05-01, ITEM 312 IS UPPER CABLE THAT IS BROKEN. REMOVED AND REPLACED AFT UPPER L1 DOOR DRIVE CABLE REF AMM 52-11-03-4 UP TO AND INCLUDING STEP E(7).Sep 5, 2017 · N582FE · Doug MD11F · Passenger/Crew DoorsSDR IPXA2017091221646Structure · chafedINSPECTION TYPE: 3C, AREAS OF BLOCKER DOOR CONTACT, CHAFED NR 1 LT THRUST REVERSER INNER BARREL SKIN. REPAIRED IAW SREO M-7830-25334-G.Sep 2, 2017 · N274UP · Doug MD11F · Engine Thrust ReverserSDR FDEA201709022451Hinge Bracket · corrodedRIGHT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT OUTBOARD LUG HOLE BORE FOUND CORRODED. BORE REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-135692F, PART 5, STEP 2 AND 3. REPAIR CSep 2, 2017 · N586FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201709022450Hinge Bracket · corrodedRIGHT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT INBOARD LUG HOLE BORE FOUND CORRODED. BORE REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-135692F, PART 5, STEP 2 AND 3. REPAIR CLASSep 2, 2017 · N586FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201709022449Hinge Bracket · corrodedLEFT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT OUTBOARD LUG HOLE BORE FOUND CORRODED. BORE REWORKED AND FOUND OUT OF LIMITS CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-135691F, PART 5, STEP 2 & 3. REPAIR CLASSIFSep 2, 2017 · N586FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201709022448Hinge Bracket · corrodedLEFT WING INBOARD FLAP OUTBOARD HINGE (FLAP) PIVOT INBOARD LUG HOLE BORE FOUND CORRODED. BORE REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-135691F, PART 5, STEP 2 & 3. REPAIR CLASSIFIEDSep 2, 2017 · N586FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201709022447Hinge Bracket · corrodedRIGHT WING INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT HOLE BORE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-07. A NEW REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0330927 A, PART 1, STEP 1F. REPAIR CLASSIFIED AS MAJOR IASep 2, 2017 · N586FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201709022446Hinge Bracket · corrodedLEFT WING INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT HOLE BORE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-07. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0330926 B, PART 1, STEP 1F. REPAIR CLASSIFIED AS MAJOR IAW GMSep 2, 2017 · N586FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201709022445Skin · chafedLT WING LE DROOP SLAT OUTBOARD LE FOUND CHAFING. REPAIR CARRIED OUT AS PER EA 1-5730- T0335216-PT1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI 57305245.Sep 2, 2017 · N624FE · Doug MD11F · Leading Edge DevicesSDR FDEA201709022444Longeron · corrodedLOWER AFT CARGO WASTE TANK COMPARTMENT FOUND LONGERON 35R BETWEEN STA 1986-1997 WITH CORROSION AS MARKED. DAMAGED LONGERON REPAIR CARRIED OUT AS PER EA 1-5310-T0335215 PART:1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI #53105247 FOR JOB DETAIL.Sep 2, 2017 · N624FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2017090221251Slide · inoperativeUNABLE TO DISARM EMERGENCY SLIDE. LEVER WOULD NOT MOVE TO FULLY REAR POSITIONAFTER BEING EXPOSED TO TORRENTIAL RAINFALL DURING SDF STOPOVER DOOR WAS FROZEN. AFTER EXPOSURE TO 100 DEGREE AMBIENT TEMPERATURE IN ONT, DOOR OPS CHECKS NORMAL EMERGENCY SLIDE IS PINNSep 1, 2017 · N295UP · Doug MD11F · Escape SlideSDR FDEA201708312438Beam · crackedMAIN DECK R3 DOOR LOWER BEAM FORWARD STOPPER AREA FOUND CRACKED. THE BEAM WAS REMOVED AND REPLACED IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 31, 2017 · N586FE · Doug MD11F · Cargo/Baggage DoorsSDR FDEA201708312437Seat Track · damagedMAIN DECK SEAT TRACK AT BS 755, LBL 27.5 FOUND TO HAVE CROWN DAMAGE. THE SEAT TRACK WAS REPLACED FROM BS 725 TO 765 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 31, 2017 · N586FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201708312436Seat Track · damagedMAIN DECK SEAT TRACK AT BS 755, RBL 47.5 FOUND TO HAVE CROWN DAMAGE. THE SEAT TRACK WAS REPLACED FROM BS 725 TO 765 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 31, 2017 · N586FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201708312435Cargo Track · crackedMAIN DECK CARGO TRACK AT BS 755, RBL 8.5 FOUND CRACKED. THE CARGO TRACK WAS REPLACED BETWEEN BS 725 TO 765 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 31, 2017 · N586FE · Doug MD11F · Fuselage Floor PanelSDR FDEA201708312434Cargo Track · crackedMAIN DECK CARGO TRACK AT BS 638, RBL 8.5 FOUND CRACKED. THE CARGO TRACK WAS REPLACED BETWEEN BS 625 TO 705 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 31, 2017 · N586FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201708312433Cargo Track · crackedMAIN DECK CARGO TRACK AT BS 695, LBL 27.5 FOUND CRACKED. THE CARGO TRACK WAS REPLACED FROM BS 625 TO 745 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100Aug 31, 2017 · N586FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201708312432Cargo Track · crackedMAIN DECK CARGO TRACK AT BS 755, LBL 8.5 FOUND CRACKED. THE CARGO TRACK WAS REPLACED FROM BS 485 TO 745, IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 31, 2017 · N586FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201708312431Seat Track · damagedSEAT TRACK AT BS 755, RBL 27.5 FOUND WITH CROWN DAMAGE. THE SEAT TRACK WAS REPLACED BETWEEN BS 745 TO 785 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 31, 2017 · N586FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201708312430Seat Track · damagedSEAT TRACK AT BS 998, LBL 47.5 FOUND WITH CROWN DAMAGE. THE SEAT TRACK WAS REPLACED FROM BS 949 TO 1029, IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 31, 2017 · N586FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201708312427Seat Track · damagedSEAT TRACK AT BS 1681, LBL 47.5 FOUND THE CROWN DAMAGED. THE SEAT TRACK WAS REPLACED FROM BS 1631 TO 1731, LBL 47.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 31, 2017 · N586FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201708312426Seat Track · damagedSEAT TRACK AT BS 1681, LBL 27.5 FOUND WITH CROWN DAMAGE. THE SEAT TRACK WAS REPLACED FROM BS 1651 TO 1710, LBL 27.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 31, 2017 · N586FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201708312425Seat Track · damagedSEAT TRACK AT BS 755, LBL 47.5 FOUND THE CROWN DAMAGED. REPLACED THE SEAT TRACK AT EXISTING SPLICES FROM BS 725 TO 765, IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 31, 2017 · N586FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201708312424Cargo Track · crackedCARGO TRACK AT BS 775, LBL 75.5 CRACKED. REPLACED THE CARGO TRACK FROM BS 725 TO EXISTING SPLICE AT BS 765, IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 31, 2017 · N586FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201708312423Longeron Splice · crackedCROWN AREA LONGERON SPLICE AT STA 5-0, LONGERON 4L FOUND CRACKED. THE LONGERON SPLICE WAS REMOVED AND REPLACED IAW SRM 51-33-01-0G. A NEW LONGERON SPLICE WAS FABRICATED IAW DWG AEA 7634, REV B. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 31, 2017 · N586FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201708312422Skin · crackedLEFT WING DROOPED LEADING EDGE UPPER SKIN FOUND CRACKED AT XDLE 325. REPAIRED IAW SRM 57-40-01-2R, FIG 201, REPAIR 5. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 31, 2017 · N586FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201708312421Angle · damagedMAIN DECK, FUSELAGE FRAME AT BS A 535, LONGERON 24L FOUND A DAMAGED REPAIR ANGLE. THE REPAIR WAS REMOVED AND THE REPAIR REACCOMPLISHED IAW SRM 53-20-07-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 31, 2017 · N586FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201708312420Angle · damagedMAIN DECK FUSELAGE FRAME AT BS 535, LONGERON 19L FOUND A DAMAGED REPAIR ANGLE. DAMAGED REPAIR ANGLE REMOVED AND REPAIR REACCOMPLISHED IAW SRM 53-20-07-2R, FIG 202, REPAIR 1.Aug 31, 2017 · N586FE · Doug MD11F · Fuselage Main, Frame
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