Boeing MD-11F

Service difficulty reports · 31,320

Newest first. General aviation reporting is voluntary.

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 FDEA2019101762659Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE(#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57Oct 16, 2019 · N597FE · Doug MD11F · Wing, Control SurfacesSDR FDEA2019101762658Hinge · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 5Oct 16, 2019 · N597FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2019101762657Hinge · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44Oct 16, 2019 · N597FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2019101762662Frame · damagedMAIN DECK LEFT HAND FRAME AT STATION 535 LONGERON 24 LEFT , EXISTING REPAIR OUTER ANGLE FOUND DAMAGED . MAIN DECK LEFT HAND FRAME AT STATION 535 LONGERON 24 LEFT , EXISTING DAMAGED OUTER REPAIR ANGLE REMOVED AS PER SRM 51-33-01-0G AND REPAIRED AS PEROct 16, 2019 · N597FE · Doug MD11F · Fuselage Main, FrameSDR IPXA2019101877984Link · brokenINSPECTION TYPE:N/AAIR TURNBACK - ON GEAR RETRACTION VIBRATION INCREASING UNTIL VIOLENT SHAKING & VIBRATION AT FULL RETRACTION. EXTENDED GEAR NORMALLY W/VIB SUBSIDING, BUT STILL PRESENTFOUND L/H NLG DOOR LINK MECHANISM BROKEN. R/R DOOR LINK MECHANISM IAW MD11Oct 16, 2019 · N271UP · Doug MD11F · Landing Gear Door Retract SectionSDR FDEA201910152643Hinge · corrodedLEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) BARREL NUT HOLE SURFACE HAD CORROSION. CORROSION REWORKED AND FOUND TO EXCEED LIMITS. BASE THE DIFFERENCE BETWEEN DRAWING LIMITS AND CMM MAXIMUM REWORK LIMIT FOR BARREL NUT HOLE. REPAIR SHIM FABRICOct 15, 2019 · N601FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR IPXA2019102328183Stringer · crackedINSPECTION TYPE:2CLT WING FIXED L/E STRINGER IS CRACKED AT STA. XOS 667.REPAIRED CRACKED LT WING FIXED L/E STRINGER AT STA. XOS 667 IAW MD-11 SRM 57-40-03, REPAIR 2, FIGURE 202. (MAJOR)Oct 15, 2019 · N259UP · Doug MD11F · Wing, Longeron/StringerSDR FDEA201910142637Floorbeam · corrodedLOWER AFT CARGO COMPARTMENT FORWARD BULKHEAD 'L' ANGLE FLOORBEAM FOUND CORRODED AT BS 1841. CORROSION REMOVED AND FOUND TO EXCEED LIMITS IAW SRM 53-00-00-2R, FIGURE 205. FLOORBEAM REMOVED AND REPLACED IAW SRM 51-31-01-0G. THE REPAIR WAS CLASSIFIED AS MINOR Oct 14, 2019 · N601FE · Doug MD11F · Fuselage Main, Floor BeamSDR FDEA201910142638Skin · corrodedEMPENNAGE RIGHT UPPER FUSELAGE SKIN BS 2122 TO 2164, LONGERONS 33-35R, FOUND WITH SURFACE CORROSION. SURFACE CORROSION REMOVED IAW SRM 51-21-01-0G, AND FOUND OUT OF LIMITS IAW SRM 53-70-01-2R, FIGURE 201, REPAIR 3. REPAIRED IAW EA 1-5330-T0350371, PART 1. Oct 14, 2019 · N601FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201910142636Seat Track · corrodedCABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK FLANGE CORRODED, BS 1581 - 1621, LBL 8.5. CORROSION REMOVED AND FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIG 101. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT FROM BS 1571 TO 1631 IAW SRM 53-00-52-2,Oct 14, 2019 · N601FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201910132635Floor Panel · corrodedBOTTOM OF AIRCRAFT AFT OF CTR LANDING GEAR SUSPECT CORROSION MARKED WITH TAPE REMOVED AND INSTALLED 2 FLOOR PANELS IN CTR CARGO FWD IAW AMM 53-21-01-4.Oct 13, 2019 · N613FE · Doug MD11F · Fuselage Floor PanelSDR FDEA2019101432625Hinge Bracket · corrodedCORROSION AT WING, INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE NR 3 HOLE. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44- 07. OVERSIZED REPAIR BUSHING FABRICATED AND INSTALLED CMM 57-44-07 AND EA 1-5750-T0321647 F PART 3 STEP 1A Oct 13, 2019 · N601FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2019101432626Hinge Fitting · corrodedRIGHT WING, INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE CORRODED. THE CORROSION WAS REWORKED AND FOUND TO EXCEED LIMITS CMM 57-44- 07. AN OVERSIZED REPAIR BUSHING WAS FABRICATED AND INSTALLED CMM 57-44-07 AND EA 1-5750-T0321648 D PART 3,Oct 13, 2019 · N601FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2019101432628Rib · crackedRIGHT WING NR 1 LEADING EDGE SLAT INBOARD RIB FOUND CRACKED AT XIS 151. REPAIRED THE NR 1 SLAT INBOARD RIB IAW EA 1-5750-T0350046, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Oct 13, 2019 · N597FE · Doug MD11F · Leading Edge DevicesSDR FDEA2019101432627Rib · crackedLEFT WING NR 1 LEADING EGE SLAT INBOARD RIB FOUND CRACKED AT XIS 151. REPAIRED THE LEFT WING SLAT INBOARD RIB IAW EA 1-5750-T0350043, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Oct 13, 2019 · N597FE · Doug MD11F · Leading Edge DevicesSDR FDEA2019101432624Attach Fitting · corrodedLEFT MAIN LANDING GEAR RETRACT ACTUATOR UPPER ATTACH FITTING LOWER AFTER HOLE FOUND CORRODED. CORROSION REWORKED AND FOUND EXCEED TO LIMITS IAW SRM 57-20-14-2R, REPAIR 1. A REPAIR BUSHING WAS FABRICATED IAW SRM 57-20-14-2R, REPAIR 1, AND EA 1-5740-T0350144Oct 13, 2019 · N597FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR FDEA2019101432623Attach Fitting · corrodedLEFT MAIN LANDING GEAR RETRACT ACTUATOR UPPER ATTACH FITTING LOWER FORWARD HOLE FOUND CORRODED. CORROSION REWORKED AND FOUND TO EXCEED LIMITS IAW SRM 57-20-14-2R, REPAIR 1. A REPAIR BUSHING WAS FABRICATED IAW SRM 57-20-14-2R, REPAIR 1, AND EA 1-5740-T0350Oct 13, 2019 · N597FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR FDEA2019101432622Attach Fitting · corrodedLEFT HAND MAIN LANDING GEAR RETRACT ACTUATOR UPPER ATTACH FITTING , LOWER MATING SURFACE FOUND CORRODED. THE CORROSION WAS REWORKED AND FOUND TO EXCEED LIMITS IAW SRM 57-20-14-2R, REPAIR 1. REPAIRED IAW EA 1-5750-T0350145 P1, STEP 9. THE REPAIR WAS CLASSIOct 13, 2019 · N597FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR FDEA2019101432621Attach Fitting · corrodedLEFT MAIN LANDING GEAR, RETRACT ACTUATOR UPPER ATTACH FITTING UPPER MATING SURFACE FOUND CORRODED. ATTACH FITTING CORROSION REWORKED AND FOUND TO EXCEED LIMITS IAW SRM 57-20-14-2R REPAIR 1. REPAIRED IAW EA 1-5750-T0350145 P1, STEP 9. THE REPAIR WAS CLASSIFOct 13, 2019 · N597FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR FDEA2019101432620Floor Support · crackedMAIN DECK AFT FLOOR SUPPORT AT STATION 1887 - 2007 X = - 57 FOUND CRACKED . THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-31-01-0G . REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 .Oct 13, 2019 · N597FE · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2019101647910Spring · brokenINSPECTION TYPE:N/AREF M685305 L-1 PASS DOOR DRIVE CABLEREVERSED DMP. R&R BROKEN TENSION SPRING & INSTALLED NEW CABLE ASSY. REF AMM 52-11-03. OPS CK GOOD. THIS CLEARS M685305Oct 13, 2019 · N279UP · Doug MD11F · Passenger/Crew DoorsSDR FDEA2019101432635Longeron · corrodedBOTTOM OF AIRCRAFT AFT OF CTR LANDING GEAR SUSPECT CORROSION MARKED WITH TAPEOct 13, 2019 · N613FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 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 IPXA2019103098454Longeron · damagedINSPECTION TYPE:2CEXTERIOR FUSELAGE SKIN WAS TRIMMED OUT BETWEEN STA. 1641-1681 AND LONGERON'S 29R-30R TO ACCESS REPAIRS ON LONGERON'S 29R-30R.REPAIRED EXTERIOR FUSELAGE SKIN BETWEEN STA. 1641-1681 AND LONGERON'S 29R-30R IAW VT-SAA EA 011-5330-01-A7929 REV. I/Oct 12, 2019 · N259UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR 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 IPXA2019102878347Hinge · gougedINSPECTION TYPE:2CL/H I/B FLAP O/B HINGE FITTING IS GOUGED AT STA. XIFH=261.REPAIRED GOUGED L/H I/B FLAP O/B HINGR FITTING AT STA. XIFH=261. IAW VT-SAA EA 011-5750-01-A7937 REV. I/R AND UPS EO MD11-5740-74451-A.Oct 12, 2019 · N259UP · Doug MD11F · Trailing Edge FlapsSDR FDEA2019101422615Skin · corrodedAFT ACCESSORY COMPARTMENT HAS EVIDENCE OF CORROSION ON THE RT SIDEWALL. REPAIRED IAW SRM 53-70-01-2R, FIG 201.Oct 12, 2019 · N617FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201910112601Hinge Fitting · crackedLEFT WING - INBOARD AILERON ASSEMBLY INBOARD HINGE FITTING OUTBOARD EDGE CRACKED. REPAIRED PER EA 1-5750-T0350012 P1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Oct 11, 2019 · N586FE · Doug MD11F · AileronsSDR 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 IPXA2019103098430Intercostal · crackedINSPECTION TYPE:2CFWD. CARGO INTERCOSTAL IS CRACKED BETWEEN STA. 6-30 TO 6-50 AND ABOVE LONG. 43 R/H.REMOVED, FABRICATED AND REPLACED INTERCOSTAL BETWEEN STA. 6-30 TO 6-50 AND ABOVE LONG. 43 R/H IAW DWG. ACA7049 AND SRM 51-33-01. (MINOR)Oct 11, 2019 · N259UP · Doug MD11F · Fuselage Miscellaneous StructureSDR 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 IPXA2019102548248Shear Tie · crackedINSPECTION TYPE:2CUNDERWING BARREL (BLADDER AREA) FRAME TO BEAM SHEAR ANGLE IS CRACKED AT STA. Y=1278 R/H SIDE.REMOVED AND REPLACED ANGLE IAW SRM 51-33-01.(MINOR)Oct 11, 2019 · N259UP · Doug MD11F · Fuselage Internal Mounting StructureSDR IPXA2019102548239Stringer · crackedINSPECTION TYPE:2CCENTER WING TANK STRINGER #45 IS CRACKED AT STA. XCW=17 & XCW=46.5REPAIRED CRACKED CENTER WING TANK STRINGER # 45 BETWEEN STA. XCW= 4.5 TO XCW= 57.25 IAW SRM 57-10-03 REPAIR 1 FIG. 201. (MAJOR)Oct 11, 2019 · N259UP · Doug MD11F · Fuel StorageSDR FDEA201910112599Door Frame · crackedMAIN DECK L3 DOOR AFT JAMB LOWER WEB BOX AT STATION 1305.25 TO STATION 1315.42 L-26 LEFT TO L-27 LEFT FOUND CRACKED. REPAIRED AS PER SRM 53-40-15- 2R FIGURE 201 REPAIR 3 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .Oct 11, 2019 · N597FE · Doug MD11F · Fuselage Main, StructureSDR 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 Fittings
Back to Boeing MD-11F