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 05FDEA04212Fitting · corrodedUPON REMOVAL OF CLG SHOCK STRUT ASSY FOUND WHEEL WELL SIDE LT TRUNNION FITTING LOWER MATING SURFACE WITH CORROSION. LT TRUNNION FITTING LOWER MATING SURFACE CORROSION REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA1-5340-90705, TITLE: FUSELAGE CENTER LANDING Dec 9, 2005 · N578FE · Doug MD11 · Fuselage, Landing Gear Attach FittingsSDR 05FDEA04194Hinge Bracket · corrodedLEFT HAND WING OUTBOARD FLAP INBOARD AFT HINGE BRACKET FORWARD FITTING ATTACH HOLE AT OUTBOARD AFT POSITION FOUND CORRODED. CORROSION REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-90702.Dec 8, 2005 · N578FE · Doug MD11 · Trailing Edge FlapsSDR 05FDEA04193Hinge Bracket · corrodedRIGHT HAND WING OUTBOARD FLAP INBOARD AFT HINGE BRACKET AFT FITTING FORWARD ATTACH HOLE FOUND CORRODED. CORROSION REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-90699.Dec 8, 2005 · N578FE · Doug MD11 · Trailing Edge FlapsSDR 05FDEA04192Hinge Bracket · corrodedRT WING OUTBOARD FLAP INBOARD AFT HINGE BRACKET FORWARD FITTING ATTACH HOLE AT OUTBOARD AFT POSITION FOUND CORRODED. CORROSION REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-90700.Dec 8, 2005 · N578FE · Doug MD11 · Trailing Edge FlapsSDR 05FDEA04191Hinge Bracket · corrodedRIGHT HAND WING OUTBOARD FLAP INBOARD AFT HINGE BRACKET FORWARD FITTING ATTACH HOLE AT INBOARD AFT POSITION FOUND CORRODED. CORROSION REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-90701.Dec 8, 2005 · N578FE · Doug MD11 · Trailing Edge FlapsSDR 05FDEA04190Longeron · corrodedCAC COMPARTMENT RIGHT HAND BILGE AREA LONGERON 48R STATION 1139 FOUND EDGE WITH CORROSION. REPAIR CARRIED OUT AS PER FEDEX EA 1-5310-94573 (TITLE: FUSELAGE- MAINFRAME- BODY STATION Y=1134.000, THROUGH Y=1142.000 / LONGERON 48 (RH) SPLICE CORROSION REWORK & Dec 8, 2005 · N578FE · Doug MD11 · Fuselage Main, Longeron/StringerSDR 05FDEA04165Longeron · corrodedCENTER CARGO COMPARTMENT STATION 1571 LONGERON 48 RIGHT HAND FOUND CORRODED AROUND FASTENER AREA. CORROSION REMOVED AT CENTER CARGO COMPARTMENT STATION 1571 LONGERON 48 RIGHT FOUND EXCEEDED LIMIT AS PER SRM 53-00-01 FIGURE 3 VOLUME I. ORIGINAL THICKNESS=0.10Dec 7, 2005 · N578FE · Doug MD11 · Fuselage Main, Longeron/StringerSDR 05FDEA04164Door Frame · corrodedUPON REMOVAL OF LOOSE SEALANT AFT DOOR JAMB FORWARD CORNER FOUND CORRODED, SNRM N1260: AFT CARGO COMPARTMENT: AFT DOOR JAMB FORWARD CORNER, CORRODED AREA FOUND CRACKED. CARRIED OUT REPAIR AS PER FEDEX EA NR 1-5350-90711, TITLE: "FUSELAGE - AFT CARGO DOOR JAMBDec 6, 2005 · N578FE · Doug MD11 · Fuselage Main, StructureSDR 05FDEA04162Door · crackedRT MLG FLIPPER DOOR FORWARD HINGE AREA SUSPECTED WITH A HAIR LINE CRACK. REPAIR CARRIED OUT AT RT MLG FLIPPER DOOR FORWARD HINGE. CRACKED AREA IAW SRM 52-10-00 FIGURE 18 VOLUME I. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Dec 6, 2005 · N578FE · Doug MD11 · Landing Gear DoorsSDR 05FDEA04161Support · corrodedUPON REMOVAL OF CLG SHOCK STRUT ASSEMBLY, FOUND WHEEL WELL SIDE RIGHT TRUNNION FITTING LOWER MATING SURFACE WITH CORROSION. RIGHT HAND TRUNNION FITTING LOWER MATING SURFACE CORROSION. REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA#1-5340-90704, TITLE:"FUSEDec 6, 2005 · N578FE · Doug MD11 · Fuselage, Landing Gear Attach FittingsSDR 05FDEA04163Door Frame · corrodedSNRM N1259: AFT CARGO COMPARTMENT: UPON REMOVAL OF LOOSE SEALANT AFT DOOR JAMB STA 1935 ADJACENT TO FWD LATCH FOUND CORRODED.**S/D COMING**Dec 6, 2005 · N578FE · Doug MD11 · Fuselage Main, StructureSDR 05FDEA04149Latch · corrodedSNRM N0539: RT WING LEADING EDGE ACCESS PANEL 617CB INTERIOR FRONT, SPAR LOWER CAP, UPPER SURFACE FOUND CORROSION AT LATCH CONTACT AREA.** S/D COMING**Dec 5, 2005 · N578FE · Doug MD11 · Wing Miscellaneous StructureSDR 05FDEA04148Floorbeam · chafedFOUND CENTER CARGO DOOR WAY CEILING AREA STA 1721, X=-98 MAIN DECK FLOORBEAM LOWER SIDE FOUND CHAFED. REPAIR CARRIED OUT AT CENTER CARGO DOOR WAY CEILING AREA AT STA 1721, X=-98 MAIN DECK FLOOR BEAM LOWER SIDE AS PER FEDEX EA 1-5310-90708, TITLE: "FUSELAGEDec 5, 2005 · N578FE · Doug MD11F · Fuselage Main, Floor BeamSDR 05FDEA04125Support Fitting · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING FOUND CORROSION AT OUTBOARD NR 3 BOLT HOLE. RT WING OUTBD FLAP REMOVED & REPLACED AS PER AMM 27-50-30-4. VANE ADJUSTMENT CARRIED OUT AS PER AMM 27-50-32-5 FOUND SATIS. OUTBD FLAP OPERATIONAL TEST & Dec 5, 2005 · N578FE · Doug MD11F · Trailing Edge FlapsSDR 05FDEA04124Support Fitting · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING FOUND CORROSION AT OUTBOARD NR 2 BOLT HOLE. REFER TO SNRM NO. N0830 FOR RIGHT HAND WING OUTBOARD FLAP REPLACEMENT.Dec 5, 2005 · N578FE · Doug MD11 · Trailing Edge FlapsSDR 05FDEA04123Hinge Fitting · corrodedFOUND RIGHT WING OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING FOUND CORROSION AT INBOARD NR 2 BOLT HOLE. REFER TO SNRM NR N00830 FOR RIGHT HAND WING OUTBOARD FLAP REPLACEMENT.Dec 5, 2005 · N578FE · Doug MD11 · Trailing Edge FlapsSDR 05FDEA04122Hinge Fitting · corrodedFOUND LEFT WING OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING FOUND CORROSION AT OUTBOARD NR 3 BOLT HOLE.Dec 5, 2005 · N578FE · Doug MD11 · Trailing Edge FlapsSDR 05FDEA04119Structure · crackedFOUND FORWARD CARGO STATION 1129 L52 FOUND CRACKED. CARRIED OUT REPAIR AT CRACKED LONGERON 52 LOCATED AT FORWARD CARGO STATION 1129 AS PER SRM 53-10-00 FIGURE 1 VOLUME I.Dec 4, 2005 · N578FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 05FDEA04118Splice · crackedFORWARD CARGO STATION 1119 TO STATION 6-10 L52 SPLICE FOUND CRACKED. FORWARD CARGO STATION 1119 TO STATION 6-10 L52 SPLICE REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Dec 4, 2005 · N578FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 05FDEA04117Door · crackedFOUND LEFT HAND MAIN LANDING GEAR FLIPPER DOOR FORWARD HINGE FOUND WITH A CRACKED APPROXIMATELY 1.0" IN LENGTH. REPAIR CARRIED OUT AT LEFT HAND MAIN LANDING GEAR FLIPPER DOOR FORWARD HINGE CRACKED AREA AS PER SRM 52-10-00 FIGURE 18 VOLUME I. REPAIR CLASSIFDec 4, 2005 · N578FE · Doug MD11 · Landing Gear DoorsSDR 05FDEA04116Skin · chafedCENTER CARGO DOOR CUTOUT STA 1708 L40R TO L41R EXTERIOR SKIN EDGE FOUND CHAFED. REPAIR CARRIED OUT AT CENTER CARGO DOOR CUTOUT STA 1708 L40R TO L41R EXTERIOR SKIN EDGE CHAFFED AREA AS PER SRM 53-50-00 FIGURE 16 VOLUME I AND FEDEX EA # 1-5350- 90710, TIDec 4, 2005 · N578FE · Doug MD11 · Fuselage Main, Plate/SkinSDR 05FDEA04084Hinge Bracket · crackedLEFT WING OUTBOARD FLAP INBOARD FORWARD HINGE BRACKET AFT UPPER LINK FOUND CRACKED. COMPLIED WITH FEDEX EA 1-5750-90703 (TITLE: WINGS LEFT HAND WING TRAILING EDGE FLAP, INBOARD HINGE, TENSION STRAP - COMPLIANCE WITH BOEING S/B 57- 10). REPAIR CLASSIFIED Dec 2, 2005 · N578FE · Doug MD11 · Trailing Edge FlapsSDR 05FDEA04083Skin · corrodedLEFT HAND WING UPPER TRAILING EDGE PANEL FOUND BULGING AT XORS 1036. REMOVED CORROSION AT LEFT HAND WING UPPER TRAILING EDGE PANEL, XORS 1036 AS PER SRM 51-21-011 VOLUME II. ORIGINAL THICKNESS=0.140, MATERIAL REMOVED 0.100, REMAINING THICKNESS=0.040", FOUNDec 2, 2005 · N578FE · Doug MD11 · Wing, Plate/SkinSDR 05FDEA04071Stringer · crackedDURING HFEC INSPECTION, FOUND CRACK ON RIGHT WING STRINGER 14. REPAIRED AS PER SRM 57-20-00 FIG. 10 VOL. I. AND CLIP REMOVED & REPLACED AS PER SRM 51-33-01 VOL.II. FABRICATED CLIP AS PER FEDEX EA 1-5720-90712 - WINGS - STRINGER 14 RH REPAIR PER SRM VOL.I Dec 2, 2005 · N578FE · Doug MD11 · Wing, Longeron/StringerSDR 05FDEA04070Stringer · crackedDURING HFEC INSPECTION, FOUND CRACK ON RIGHT WING STRINGER 13. REPAIRED AS PER SRM 57-20-00 FIG. 10 VOL. I. AND CLIP REMOVED & REPLACED AS PER SRM 51-33-01 VOL.II. FABRICATED CLIP AS PER FEDEX EA 1-5720-90713 - WINGS - STRINGER 13 RH REPAIR PER SRM VOL.I Dec 2, 2005 · N578FE · Doug MD11 · Wing, Longeron/StringerSDR 05FDEA04069Stringer · crackedDURING HFEC INSPECTION, FOUND CRACK ON RIGHT WING STRINGER 43. REPAIRED AS PER SRM 57-20-00 FIG. 10 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Dec 2, 2005 · N578FE · Doug MD11 · Wing, Longeron/StringerSDR 05FDEA04068Skin · corrodedMAIN DECK COMPARTMENT R3 DOOR CUTOUT BOTTOM FOUND CORRODED. REMOVED AS PER SRM 51-21-01 VOLUME II. ORIGINAL THICKNESS = 0.270", MATERIAL REMOVED = 0.057", MATERIAL REMAINING = 0.213" AND FOUND WITHIN LIMIT AS PER SRM 53-00-01 VOLUME I. REPAIR CLASSIFDec 2, 2005 · N578FE · Doug MD11 · Fuselage Main, Plate/SkinSDR 05FDEA04067Stringer · crackedHFEC INSP CARRIED OUT AND CRACK FOUND ON RIGHT WING STRINGER S7. REPAIRED AS PER SRM 57-20-00 FIG. 10 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Dec 1, 2005 · N578FE · Doug MD11 · Wing, Longeron/StringerSDR 05FDEA04066Structure · crackedHFEC INSPECTED CARRIED OUT AND CRACK FOUND ON LOWER LEFT HAND WING STRINGER S44. REPAIR CARRIED OUT ON CRACK FOUND AT LEFT HAND WING STRINGER 44 AS PER FEDEX EA 1-5720-90707, TITLE: "WINGS - STRINGER 44 LEFT HAND CRACK AT WING STATION XORS=508 - REPADec 1, 2005 · N578FE · Doug MD11 · Wing Main, Frame StructureSDR 05FDEA04065Angle · crackedFOUND CENTER TANK LEFT LOWER CAP ANGLE AT STA 1298.6 SUSPECT CRACK. CTR TANK LT LOWER CAP ANGLE AT STA 1298.6 AREA REPAIRED AS PER FEDEX EA 1-5310-90694 (FUSELAGE - CAP ANGLE LT UNDERWING BARREL STRUCTURE AT STA 1298.6, XCW 46, CRACK - ANGLE FABRICATION &Dec 1, 2005 · N578FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 05FDEA04043Skin · crackedRIGHT WING FIXED LEADING EDGE FOUND CRACKED AT TELESCOPE DUCT UPPER CUTOUT. REPAIR CARRIED OUT AT RIGHT HAND WING FIXED LEADING EDGE TELESCOPING DUCT UPPER SKIN CUTOUT AS PER FEDEX EA 1-5730-90693, TITLE "WINGS - RT WING LEADING EDGE SKIN CRACKS AT TENov 30, 2005 · N578FE · Doug MD11F · Wing, Plate/SkinSDR 05FDEA03797Engine · malfunctionedABOUT 2-3 MIN AFTER BLEED SHUTDOWN, CREW GOT STICK SHAKER, A/S ALT LOSS WITH NR 3 ENG VIBRATION. BROUGHT NR 3 THROTTLE TO IDLE AND VIBRATION REDUCED BUT STILL NOTICEABLE & NR 3 EVM TURB MONITOR WAS CLIMBING THRU 4 TOWARDS 5. ELECTED TO SHUTDOWN NR 3 ENG & VINov 14, 2005 · N578FE · Doug MD11F · Engine (Turbine/Turboprop)SDR 05FDEA02659Sensor · defectiveAPPROX 2:40 HOURS INTO FLIGHT, LEVEL THREE AIR MANIFOLD 2 FAIL ALERT ILLUMINATED. CLEARED MASTER WARNING AND RAN APPROPIATE QRH LIST. SYSTEM 2 ON THE AIR SYNOPTIC DISPLAYED AS A RED LINE. MANIFOLD 2 MAINTAINED AIR PRESSURE THROUGHOUT REMAINDER OF FLT AND "BAug 23, 2005 · N578FE · Doug MD11 · Pneumatic Indicating SystemSDR 04FDEA02591Longeron · corrodedCENTER CARGO, CORROSION OBSERVED ON LONGERON 51R BETWEEN STA Y= 1681 AND STA Y= 1701. CENTER CARGO, BETWEEN STA Y= 1681 AND STA Y= 1701, CORRODED LONGERON 51R REMOVED PER SRM 51-33-01 VOLUME I. LONGERON SPLICE FABRICATED PER SRM 53-10-00 FIGURE 2 VOLUME I ANSep 1, 2004 · N578FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 04FDEA02588Fitting · crackedCAC COMPARTMENT, BETWEEN STA Y= 6-90 AND STA Y= 6-100 LONGERON 43R END SPLICE FITTING FOUND CRACKED. CAC COMPARTMENT - STA Y= 6-90 AND STA Y= 6-100 CRACKED SPLICE AT LONGERON 43R. REMOVED PER SRM 51-31-01 VOLUME II. NEW SPLICE FITTING FABRICATED PER DWG AGAug 31, 2004 · N578FE · Doug MD11F · Fuselage Main, Attach FittingsSDR 04FDEA02589Longeron · crackedMAIN DECK, LT SIDE STA Y= 6-90 TO STA Y= 1130 LONGERON 13L FOUND CRACKED. MAIN DECK, LEFT SIDE STA Y= 6-90 TO STA Y= 1130 LONGERON 13L CUT AND REMOVED PER SRM 51-31-01 VOLUME II. LONGERON SPLICE FABRICATED PER SRM 53-10-00 TYPE 1 VOLUME I. REPAIR PARTS ANAug 31, 2004 · N578FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 04FDEA02550Longeron · crackedRT SIDE STA 5-113-1541, LONGERON 25 FOUND CRACKED. REMOVED AND FABRICATED PER SRM 53-10-00 TYPE 1 VOLUME I. FABRICATED REPAIR PARTS AND EXISTING SPLICE INSTALLED PER SRM 53-10-00 TYPE 1 VOLUME I AND SRM 53-33-01 VOLUME II.Aug 23, 2004 · N578FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 04FDEA02546Longeron · corrodedCENTER CARGO, CORROSION OBSERVED ON LONGERON 48R SPLICE DOUBLER AT STA 5-116 TO STA 1541. DOUBLERS REMOVED PER SRM 51-33-01 VOLUME II. SPLICE DOUBLERS AFA7124-1, AFA7124-2, A5A7125-501 FABRICATED PER DWG AFA7124 AND A5A7125. PART MARKED AS PER FEDEX GMMAug 22, 2004 · N578FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 04FDEA02545Longeron · corrodedCENTER CARGO CORROSION OBSERVED ON LONGERON 51R SPLICE BETWEEN AT STA 1701 TO STA 172. LONGERON 51R AND SPLICE REMOVED PER SRM 53-10-00 FIGURE 2 VOLUME 1. LONGERON AND SPLICE FABRICATED PER SRM 53-10-00 FIGURE 2 VOLUME 1 AND INSTALLED PER SRM 51-33-01 VOLUMAug 22, 2004 · N578FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 04FDEA02544Longeron · corrodedCENTER CARGO, CORROSION OBSERVED ON LONGERON 48L SPLICE DOUBLER AT STA 5-113 TO STA 1541. REMOVED PER SRM 51-33-01 VOLUME II. THREE (3) EACH SPLICE DOUBLERS P/N A5A7124-1, A5A7124-2 AND A5A7125-501 FABRICATED PER DWG A5A7124 AND A5A7125; AND PART MARKEAug 22, 2004 · N578FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 04FDEA02524Spar · corrodedRT WING, REAR SPAR, LOWER CHORD AT XORS= 600 TO XORS= 620 FOUND WITH CORROSION. RT WING, REAR SPAR, LOWER CHORD AT XORS= 600 TO XORS= 620 CORROSION REMOVED PER SRM 51-31-01 VOLUME II COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR Aug 19, 2004 · N578FE · Doug MD11F · Wing SparSDR 04FDEA02523Spar · corrodedRT WING, REAR SPAR, UPPER CHORD AT XORS= 585 FOUND WITH CORROSION. RT WING, REAR SPAR, UPPER CHORD AT XORS= 585 CORROSION. REMOVED PER SRM 51-31-01 VOLUME II COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB, CORROSION ANAug 19, 2004 · N578FE · Doug MD11F · Wing SparSDR 04FDEA02522Spar · corrodedRT WING, REAR SPAR, UPPER AND LOWER CHORD AT XORS= 550 FOUND WITH CORROSION. RT WING, REAR SPAR, UPPER AND LOWER CHORD AT XORS= 550 CORROSION. REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX E NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAAug 19, 2004 · N578FE · Doug MD11F · Wing SparSDR 04FDEA02521Spar · corrodedRT WING, REAR SPAR, FROM XORS= 917 TO XORS= 1042 FOUND WITH CORROSION. RT WING, REAR SPAR, FROM XORS= 917 TO XORS= 1042 CORROSION. REMOVED PER SRM 51-31-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB, COAug 19, 2004 · N578FE · Doug MD11F · Wing SparSDR 04FDEA02520Spar · corrodedRT WING, REAR SPAR, UPPER CHORD AT ABOUT XORS= 598 FOUND WITH CORROSION. RT WING, REAR SPAR, UPPER CHORD AT XORS= 598 CORROSION. REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB, CORRAug 19, 2004 · N578FE · Doug MD11F · Wing SparSDR 04FDEA02519Spar · corrodedRT WING, REAR SPAR, UPPER CHORD AT ABOUT XORS= 720 FOUND WITH CORROSION. RT WING, REAR SPAR, UPPER CHORD AT XORS= 720 CORROSION. REMOVED PER SRM 51-31-01 VOLUME II COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB, CORROSAug 19, 2004 · N578FE · Doug MD11F · Wing SparSDR 04FDEA02518Spar · corrodedRT WING, REAR SPAR, UPPER CHORD AT ABOUT XORS= 703 FOUND WITH CORROSION. RT WING, REAR SPAR, UPPER CHORD AT ABOUT XORS= 703 CORROSION REMOVED PER SRM 51-21-01 VOLUME II COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB, Aug 19, 2004 · N578FE · Doug MD11F · Wing SparSDR 04FDEA02517Spar · corrodedRT WING, REAR SPAR, UPPER CHORD AT XORS= 633 FOUND WITH CORROSION. RT WING, REAR SPAR, UPPER CHORD AT XORS= 633 CORROSION REMOVED PER SRM 51-21-01 VOLUME II COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB, CORROSION ANAug 19, 2004 · N578FE · Doug MD11F · Wing SparSDR 04FDEA02516Spar · corrodedRT WING, REAR SPAR, LOWER CHORD AT XORS= 622 TO XORS= 642 FOUND WITH CORROSION. RT WING, REAR SPAR, LOWER CHORD AT XORS= 622 TO XORS= 642 CORROSION. REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWERAug 19, 2004 · N578FE · Doug MD11F · Wing SparSDR 04FDEA02515Spar · corrodedLEFT WING, REAR SPAR, XORS= 1020 FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 1020 AREA CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, LEFT UPPER AND LOWER REAR SPAR, CORROSION AND CRACK REPAIR.Aug 19, 2004 · N578FE · Doug MD11F · Wing Spar
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