N578FE

Service difficulty reports · 364

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 = 'N578FE' 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 04FDEA02409Splice · crackedCENTER CARGO, RIGHT LONGERON SPLICE AT STA 5-113 TO 1541 LONGERON 47 CRACKED. REMOVED AND REPALCED PER SRM 51-33-01 VOLUME IIAug 9, 2004 · N578FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 04FDEA02408Splice · crackedCENTER CARGO, RIGHT LONGERON SPLICE AT STA 5-113 TO 1541 LONGERON 51 CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME III.Aug 9, 2004 · N578FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 04FDEA02407Splice · crackedCENTER CARGO, LT LONGERON SPLICE AT STA 5-113 TO 1541 LONGERON 50 CRACKED. LONGERON 50 REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME III.Aug 9, 2004 · N578FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 04FDEA02406Hinge · corrodedLEFT WING, INBOARD FLAP OUTBOARD AFT HINGE INBOARD PIVOT HOLE FLANGE CORRODED. CORROSION REMOVED PER CMM 57-52-03.Aug 9, 2004 · N578FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02405Hinge · corrodedLEFT WING, INBOARD FLAP OUTBOARD AFT HINGE INBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMITS PER CMM 57-52-03. CORROSION REMOVED AND FOUND EXCEEDED LIMITS PER CMM 57-52-03Aug 9, 2004 · N578FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02404Hinge · corrodedRT WING, INBOARD FLAP, OUTBOARD AFT HINGE OUTBOARD PIVOT HOLE FLANGE CORRODED. CORROSION REMOVED PER CMM 57-52-03. FOUND EXCEEDED LIMITS ORIGINAL THICKNESS = 0.562, MATERIAL REMOVED = 0.002, REMAINING THICKNESS = 0.560 COMPLIED WITH FEDEX EA 1-5750-76810, Aug 9, 2004 · N578FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02403Hinge · corrodedRT WING, INBOARD FLAP, OUTBOARD AFT HINGE OUTBOARD PIVOT HOLE CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.187 FINAL DIAMETER = 1.327 COMPLIED WITH FEDEX EA 1-5750-76810, WINGS - LT AND RT INBOARD TRAILING EDGE FLAP HINGE BRAug 9, 2004 · N578FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02402Hinge · corrodedRIGHT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE OUTBOARD ACTUATOR ROD END ATTACHING HOLE FLANGE CORRODED.Aug 9, 2004 · N578FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02401Hinge · corrodedRIGHT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE OUTBOARD ACTUATOR ROD END ATTACHING HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Aug 9, 2004 · N578FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02390Hinge · corrodedRT WING OUTBOARD FLAP INBOARD AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE OUTBOARD CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.395 MATERIAL REMOVED = 0.002 REMAINING THICKNESS = 0.393 COMPLIED WITH FEDEX EA 1-5750-7Aug 6, 2004 · N578FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02389Hinge · corrodedRT WING, OUTBOARD FLAP - INBOARD AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE INBOARD FLANGED CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.411 MATERIAL REMOVED = 0.005 REMAINING THICKNESS = 0.406 COMPLIED WITH FEDEX EA 1-Aug 6, 2004 · N578FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02388Hinge · corrodedRT WING OUTBOARD FLAP INBOARD AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE OUTBOARD CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.062 FINAL DIAMETER = 1.221 COMPLIED WITH FEDEX EA 1-5750-76807, WINGS - LT AND RT OUTBOARAug 6, 2004 · N578FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02387Hinge · corrodedRT WING, OUTBOARD FLAP - INBOARD AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE OUTBOARD CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.062 FINAL DIAMETER = 1.223 COMPLIED WITH FEDEX EA 1-5750-76807, WINGS - LT AND RT OUTBOARD Aug 6, 2004 · N578FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02386Hinge · corrodedRT WING OUTBOARD FLAP INBOARD AFT HINGE WITH PIVOT HOLE INBOARD FLANGE CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.497 MATERIAL REMOVED = 0.012 REMAINING THICKNESS = 0.485 COMPLIED WITH FEDEX EA 1-5750-76807, WINGS - LAug 6, 2004 · N578FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02385Hinge · corrodedRT WING OUTBOARD FLAP INBOARD AFT HINGE WITH PIVOT HOLE INBOARD CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.093 FINAL DIAMETER = 1.189 COMPLIED WITH FEDEX EA 1-5750-76807, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRAAug 6, 2004 · N578FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02384Hinge · corrodedRIGHT WING, OUTBOARD FLAP - INBOARD AFT HINGE WITH PIVOT HOLE OUTBOARD FLANGE CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.508 MATERIAL REMOVED = 0.002 REMAINING THICKNESS = 0.506 COMPLIED WITH FEDEX EA 1-5750-76807, WINGS Aug 6, 2004 · N578FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02383Hinge · corrodedRT WING, OB FLAP, IB AFT HINGE WITH PIVOT HOLE, OB CORRODED.**** S/D COMING ****Aug 6, 2004 · N578FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02381Hinge Bracket · corrodedLT WING, OB FLAP, IB AFT HINGE WITH ACTUATOR ROD END ATTACHING OB HOLE CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.062. FINAL DIAMETER = 1.203. COMPLIED WITH FEDEX EA 1-5750-76807, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINAug 5, 2004 · N578FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02380Hinge Bracket · corrodedLT WING, OB FLAP, IB AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE IB CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.412" MATERIAL REMOVED = 0.003. REMAINING THICKNESS = 0.409. COMPLIED WITH FEDEX EA 1-5750-76807, LEFT AND Aug 5, 2004 · N578FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02379Hinge Bracket · corrodedLT WING, OB FLAP, IB AFT HINGE WITH ACTUATOR ROD END ATTACHING T IB HOLE CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.062. FINAL DIAMETER = 1.199. COMPLIED WITH FEDEX EA 1-5750-76807, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HIAug 5, 2004 · N578FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02378Hinge Bracket · corrodedLT WING, OB FLAP, IB AFT HINGE WITH PIVOT IB HOLE FLANGE CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.502. MATERIAL REMOVED = 0.015. REMAINING THICKNESS = 0.487. COMPLIED WITH FEDEX EA 1-5750-76807, LEFT AND RIGHT OUTBOARD FAug 5, 2004 · N578FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02377Hinge Bracket · corrodedLT WING, OB FLAP, IB AFT HINGE WITH PIVOT HOLE IB CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.093 FINAL DIAMETER = 1.148. COMPLIED WITH FEDEX EA 1-5750-76807, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE Aug 5, 2004 · N578FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02376Hinge Bracket · corrodedLT WING, OB FLAP, IB AFT HINGE OB PIVOT HOLE FLANGE CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.502. MATERIAL REMOVED = 0.004 REMAINING THICKNESS = 0.498. COMPLIED WITH FEDEX EA 1-5750-76807, LEFT AND RIGHT OUTBOARD FLAAug 5, 2004 · N578FE · Doug MD11 · Wing Main, Frame StructureSDR 04FDEA02375Hinge Bracket · corrodedLT WING, OB FLAP IB AFT HINGE OB PIVOT HOLE FOUND CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.062 FINAL DIAMETER = 1.095. COMPLIED WITH FEDEX EA 1-5750-76807, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODAug 5, 2004 · N578FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02374Hinge Bracket · corrodedLT WING, OB FLAP, OB AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE IB FLANGE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.402, MATERIAL REMOVED = 0.006, REMAINING THICKNESS = 0.0.396 COMPLIED WITH FEDEX EA 1-5750-76808Aug 5, 2004 · N578FE · Doug MD11 · Wing Main, Frame StructureSDR 04FDEA02373Hinge Bracket · corrodedLT WING, OB FLAP, OB AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE IB CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.192 COMPLIED WITH FEDEX EA 1-5750-76808, WINGS - LEFT AND RIGHT OUTBOARD FLAP - Aug 5, 2004 · N578FE · Doug MD11 · Wing Main, Frame StructureSDR 04FDEA02372Hinge Bracket · corrodedLT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE OUTBOARD FLANGE CORRODED. CORROSION REMOVED AS PER CMM 20-11- 02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.402, MATERIAL REMOVED = 0.004, REMAINING THICKNESS = 0.398. COMPLIED WITH FEDEAug 5, 2004 · N578FE · Doug MD11 · Wing Main, Frame StructureSDR 04FDEA02371Hinge Bracket · corrodedLT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE OUTBOARD CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.192. COMPLIED WITH FEDEX EA 1-5750-76808, WINGS - LT AND RT OUTBOAAug 5, 2004 · N578FE · Doug MD11 · Wing Main, Frame StructureSDR 04FDEA02370Hinge Bracket · corrodedLT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE INBOARD PIVOT HOLE FLANGE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.500, MATERIAL REMOVED = 0.001, REMAINING THICKNESS = 0.0.499. COMPLIED WITH FEDEX EA# 1-5750-76808, WINGS Aug 5, 2004 · N578FE · Doug MD11 · Wing Main, Frame StructureSDR 04FDEA02368Hinge Bracket · corrodedLT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE WITH OUTBOARD PIVOT HOLE FLANGE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.502, MATERIAL REMOVED = 0.003, REMAINING THICKNESS = 0.0.499. COMPLIED WITH FEDEX EA 1-5750-76808, WAug 5, 2004 · N578FE · Doug MD11 · Wing Main, Frame StructureSDR 04FDEA02367Hinge Bracket · corrodedLT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE WITH OUTBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.071 COMPLIED WITH FEDEX EA 1-5750-76808, WINGS - LT AND RT OUTBOARD FLAP - OUTBAug 5, 2004 · N578FE · Doug MD11 · Wing Main, Frame StructureSDR 04FDEA02382Hinge · corrodedLT WING, OB FLAP, IB AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE OB HOLE CORRODED. *** S/D COMING ****Aug 5, 2004 · N578FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02369Hinge · corrodedLT WING, OB FLAP, OB AFT HINGE WITH IB PIVOT HOLE CORRODED**** S/D COMING ****Aug 5, 2004 · N578FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02358Seat Track · wornSEAT TRACK CROWN DAMAGED AT APPROXIMATE STA 839 RBL 8.5. TRIMMED OFF AS PER SRM 55-70-00 FIGURE 1 VOLUME I. NEW SEAT TRACK AND FABRICATED REPAIR SPLICE INSTALLED SRM 55-70-00 FIGURE 1 VOLUME I.Aug 3, 2004 · N578FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02357Longeron · crackedCENTER CARGO LT LONGERON SPLICE AT STATION 5-113 TO 1541 LONGERON 41 CRACKED. REMOVED PER SRM 51-33-01 VOLUME II. NEW SPLICE A5A7114-553 FABRICATED PER DWG A5A7114 AND PART MARKED PER GMM 7-0-1001. FABRICATED SPLICE FX A5A7114-553 INSTALLED PER SRM 51-33-01Aug 3, 2004 · N578FE · Doug MD11 · Fuselage Main, Longeron/StringerSDR 04FDEA02356Longeron · crackedCENTER CARGO LT HAND LONGERON SPLICE AT STATION 5-113 TO 1541 LONGERON 39 CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II.Aug 3, 2004 · N578FE · Doug MD11 · Fuselage Main, Longeron/StringerSDR 04FDEA02355Longeron · crackedCENTER CARGO LT LONGERON SPLICE AT STATION 5-113 TO 1541 LONGERON 37 CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II.Aug 3, 2004 · N578FE · Doug MD11 · Fuselage Main, Longeron/StringerSDR 04FDEA02354Fitting · corrodedLT WING, OB FLAP OB HINGE FORWARD FITTING AFT. IB HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.442, FINAL DIAMETER = 0.502 COMPLIED WITH FEDEX EA 1-5750-80364, WINGS - TRAILING EDGE FLAPS - LEFT OUTBOARD FLAP - HIAug 2, 2004 · N578FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02353Fitting · corrodedLT WING, OB FLAP OB HINGE FORWARD FITTING MIDDLE. OB HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.457, FINAL DIAMETER = 0.517 COMPLIED WITH FEDEX EA 1-5750-80364, WINGS - TRAILING EDGE FLAPS - LEFT OUTBOARD FLAP -Aug 2, 2004 · N578FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02352Fitting · corrodedLT WING, OB FLAP OB HINGE FORWARD FITTING. FORWARD IB HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.442, FINAL DIAMETER = 0.502. COMPLIED WITH FEDEX EA 1-5750-80364, WINGS - TRAILING EDGE FLAPS - LEFT OUTBOARD FLAP Aug 2, 2004 · N578FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02351Hinge · corrodedLT WING, OB FLAP IB HINGE FORWARD FITTING FORWARD. IB HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.567, FINAL DIAMETER = 0.627. COMPLIED WITH FEDEX EA 1-5750-80364, WINGS - TRAILING EDGE FLAPS - LEFT OUTBOARD FLAP Aug 2, 2004 · N578FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA01973Seal · tornDURING CLIMB-OUT PASSING FL250, A LOUD NOISE BEGAN FROM LEFT SLIDING WINDOW. NOISE CONTINUED AT VARIOUS ALTITUDES. TRIED ALL ALTITUDES FROM FL250 TO FL350. NOISE DIDN'T STOP UNTIL 9,000 FEET AND 245 KNOTS. DP, WHEN IT STOPPED WAS 3.7 CABIN ALTITUDE WAS 930Jul 6, 2004 · N578FE · Doug MD11F · Flight Compartment WindowsSDR 04FDEA01633Floorbeam · crackedFOUND LWR FLOORBEAM IN CENTER CARGO COMP AT APPROX FRAME STA 1701 AT APPROX 30 INCHES FROM CENTER LINE ON RT SIDE. NOTE: THERE IS ALSO DAMAGE TO LT SIDE.Jun 7, 2004 · N578FE · Doug MD11 · Fuselage Main, Floor BeamSDR 04FDEA01128Panel · missingPANEL ON TOP OF RIGHT WING MISSING. REPLACED WING PANEL USING APPROVED PARTS AND METHODS USING EA 1-5710-78268. PART NUMBER OF PANEL INSTALLED IS ARC0629-502 AND IS INK-STAMPED ACCORDINGLY REF MM CHAP 51 SRM. OK FOR SERVICE. INST ON A/C ONLY, NO REMOVAL OApr 27, 2004 · N578FE · Doug MD11 · Wing, Plate/SkinSDR 03FDEA01653Computer · inoperativeIMMEDIATELY AFTER TAKEOFF, FUEL AND MISC CUE ALERTS CAME ON. (FUEL ALERT, LEVEL 1 (TANK 3 FWD PUMP OFF). MISC CUE ALERT, LEVEL 1 (NO AUTOLAND). ADDITIONALLY, PFD AUTOPILOT BOX WENT AMBER, WITH (AP OFF) DISPLAYED. NEITHER AP WOULD ENGAGE AT 500 FT AGL, ASep 27, 2003 · N578FE · Doug MD11 · Autopilot SystemSDR 03FDEA01384Precooler · failedMOMENTARY INDICATION OF NR 2 BLEED MANF FAILURE. (RED LIGHT ON OVERHEAD AND RED LINE ON NR 2 BLEED MANF SYNOPTIC). ASC DEPRESSURIZED NR 2 MANF. QRH PROCEDURES ACCOMPLISHED. PHONE PATCH W/MEM GOC ADVISED TO CONTINUE TO NANDI. PERFORMED DECAY CHECK AND DECAAug 25, 2003 · N578FE · Doug MD11 · Pneumatic Distribution SystemSDR 03FDEA00727Manifold · damagedIN CRUISE (FL320) AFTER 5+30 FLIGHT, AIR MANF 2 FAIL WARNING ILLUMINATED, NR 2 PACK SHUTDOWN AUTOMATICALLY. DIVERTED TO NFFN. ACN RELEASED FOR SERVICE PER MEL/CDL: 36-10-02-A CATEGORY: C EXPIRATION: 22MAY03. MEL 36-10-02-A: PNEUMATIC SUPPLY SYS NR 2 - INOPMay 12, 2003 · N578FE · Doug MD11 · Pneumatic Indicating SystemSDR 03FDEA00112Rib · crackedRT HORIZONTAL STAB AT STA XE 122.594, FWD RIB, ONE HORIZONTAL MACHINED ANGLE FOUND A CRACKED, LINE MEASURED APPROX. 1 INCH IN LENGTH. HORIZONTAL STABILIZER UPPER FORWARD RIB XE 122.594 REPAIRED AS PER FEDEX EA 1-5510-63146 - STABILIZERS - HORIZONTAL STABFeb 6, 2003 · N578FE · Doug MD11F · Horizontal Stabilizer, Spar/RibSDR 03FDEA00075Spar Cap · corrodedCOMPLY WITH EA 1-5510-67532, HORIZONTAL STABILIZER, RT SPAR CAP, REPLACEMENT IAW SR DRAWING REPLACES EA 1-5510-64246 PART 3 AND IS TERMINATING ACTION. HORIZONTAL STABLIZER, RT SPAR CAP REMOVED AND REPLACED IAW EA 1-5510-67532. HORIZONTAL STABILIZER, RT SPJan 23, 2003 · N578FE · Doug MD11 · Horizontal Stabilizer, Spar/RibSDR 03FDEA00111Hinge Bracket · damagedRT WING O/B FLAP I/B HINGE ACTUATOR I/B ATTACHMENT HOLE FOUND WITH A GROOVE MARK. COMPLIED WITH FEDEX EA 1-5750-67561. WING TRAILING EDGE & TRAILING EDGE DEVICES, RT OUTBOARD FLAP, INBOARD HINGE BRACKET REPAIR.Jan 20, 2003 · N578FE · Doug MD11F · Trailing Edge Flaps
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