N582FE

Service difficulty reports · 370

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 = 'N582FE' 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 04FDEA1482Fuel Tank · corrodedFOUND MAIN DECK COMPARTMENT CENTER WING TANK TOP SURFACE FOUND WITH CORROSION BETWEEN STRINGER 14 AND STRINGER 15 RBL 46.Apr 17, 2006 · N582FE · Doug MD11 · Fuel StorageSDR 06FDEA1481Fuel Tank · corrodedFOUND MAIN DECK COMPARTMENT CENTER WING TANK TOP SURFACE FOUND WITH CORROSION BETWEEN STRINGER 14 AND STRINGER 15 RBL 81. COMPLIED WITH FEDEX EA 1-5710-95814.Apr 17, 2006 · N582FE · Doug MD11 · Fuel StorageSDR 06FDEA1458Trunnion · crackedUPON REMOVAL OF NOSE LANDING GEAR ASSEMBLY FOUND RIGHT TRUNNION FITTING LOWER AREA WITH CRACK. REPAIRED IAW SRM 53-40-00.Apr 15, 2006 · N582FE · Doug MD11 · Fuselage, Landing Gear Attach FittingsSDR 06FDEA1457Fitting · crackedUPON REMOVAL OF NOSE LANDING GEAR ASSEMBLY FOUND LEFT TRUNNION FITTING LOWER AREA WITH CRACK. REPAIRED IAW SRM 53-40-00.Apr 15, 2006 · N582FE · Doug MD11 · Fuselage, Landing Gear Attach FittingsSDR 06FDEA1456Fastener · misinstalledENGINE NR 1 PYLON AT RIGHT SIDE MATING TO THRUST REVERSER COWL FOUND CHAFING DUE WRONG FASTENER INSTALLED ON REVERSER. COMPLIED WITH FEDEX EA 1-5450-95813.Apr 15, 2006 · N582FE · Doug MD11 · Engine Thrust ReverserSDR 06FDEA1437Spar · corrodedFOUND LEFT WING, REAR SPAR AT ABOUT XORS 1042 CORRODED. CORRODED AREA AT LEFT HAND WING - REAR SPAR LOWER CHORD AT ABOUT XORS 1042 REPAIRED AS PER FEDEX E.A. #1-5710-95809, TITLE: WINGS - LEFT HAND REAR SPAR LOWER CAP AFT TANG UPPER SURFACE CORROSION Apr 13, 2006 · N582FE · Doug MD11 · Wing SparSDR 06FDEA1416Doubler · chafedFORWARD CARGO DOOR CUTOUT AFT DOUBLER APPROX FLOOR LEVEL EDGE CHAFED. FORWARD CARGO DOOR CUTOUT AFT DOUBLER CHAFING MARK REMOVED AND FOUND WITHIN LIMIT AS PER SRM 53-00-01 FIG 1A VOL.I.Apr 12, 2006 · N582FE · Doug MD11F · Fuselage Main, StructureSDR 06FDEA1404Longeron · corrodedCENTER CARGO RIGHT LONGERON 48R BETWEEN STA 1561 TO 1581 CORRODED. CENTER CARGO RIGHT SIDE STA 1561 TO STA 1581 LONGERON 48R SPLICE CORROSION REMOVED AND FOUND WITHIN LIMIT AS PER SRM 53-00-01 FIGURE 3 VOLUME I. ORIGINAL THICKNESS = 0.200", MATERIAL REMOVEApr 12, 2006 · N582FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 06FDEA1403Splice · corrodedCENTER CARGO LONGERON 48L BETWEEN STA 5-113 TO 1541 SPLICE CORRODED. CENTER CARGO LONGERON 48L BETWEEN STA 5-113 TO 1541 CORRODED SPLICE REMOVED AS PER SRM 51-33-01 VOL II. NEW SPLICE FABRICATED AS PER DWG NR A5A7125-501. NEW SPLICE INSTALLED AS PER SRM 5Apr 12, 2006 · N582FE · Doug MD11F · Fuselage Main, StructureSDR 06FDEA1415Doubler · chafedFORWARD CARGO DOOR CUTOUT FORWARD DOUBLER APPROX FLOOR LEVEL EDGE CHAFED. FWD CARGO DOOR CUTOUT FWD DAMAGED DOUBLERS REMOVED AS PER SRM 51-33-01 VOL II. NEW DOUBLERS FABRICATED AS PER SRM 53-50-00 FIG 16 VOL I. NEW DOUBLERS PROTECTED AS PER SRM 51-21-01 VOLApr 12, 2006 · N582FE · Doug MD11 · Fuselage Main, StructureSDR 06FDEA1417Seat Track · corrodedMAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STA 1795-1805 RBL 8. MAIN DECK COMPARTMENT SEAT TRACK AT STA 1795-1805 RBL 8 CARRIED OUT REPAIR AS PER SRM 53-70-00 FIG 1 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Apr 12, 2006 · N582FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA1418Doubler · crackedLEFT HAND WING - FIXED LEADING EDGE COMPARTMENT CANTED AREA FOUND FORMER DOUBLER AT STA XIS 562 WITH CRACKED. LEFT HAND WING - FIXED LEADING EDGE COMPARTMENT CANTED AREA AT STA XIS 562 CRACKED DOUBLER. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. NEWApr 12, 2006 · N582FE · Doug MD11 · Wing Main, Frame StructureSDR 06FDEA1402Spar Cap · corrodedRIGHT HAND WING - REAR SPAR UPPER SPAR CAP AT STA XORS 1062 FOUND CORROSION. CORROSION ON RIGHT HAND WING, REAR SPAR UPPER SPAR CAP AT STA XORS 1062 REMOVED AS PER SRM 51-21-01 VOLUME II AND FOUND WITHIN LIMIT AS PER SRM 57-20-00 FIGURE 16 VOLUME I. ORIGINALApr 12, 2006 · N582FE · Doug MD11 · Wing SparSDR 06FDEA1401Spar Cap · corrodedRIGHT HAND WING - REAR SPAR UPPER SPAR CAP AT STA XORS 1027 TO STA XORS 1045 FOUND CORROSION. REPAIR CARRIED OUT ON RIGHT HAND WING REAR SPAR UPPER SPAR CAP AT STA XORS 1027 TO XORS 1045 AS PER FEDEX EA 1-5710-95811, TITLE: WINGS - RIGHT HAND REAR SPAR CAP UPApr 12, 2006 · N582FE · Doug MD11 · Wing SparSDR 06FDEA1400Spar Cap · corrodedLEFT HAND WING - REAR SPAR UPPER SPAR CAP AT STA XORS 1025 TO STA XORS 1045 FOUND CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II AND FOUND EXCEEDED LIMIT AS PER SRM 57-20-00 FIGURE 16 VOLUME I. ORIGINAL THICKNESS = 0.145" MATERIAL REMOVED = 0.054Apr 12, 2006 · N582FE · Doug MD11 · Wing SparSDR 06FDEA1395Longeron · crackedEMPENNAGE AFT FUSELAGE APPROX STA 2007-2033 BETWEEN LONGERON 45R TO 46R, CAP SUSPECTED CRACKED. EMPENNAGE, AFT FUSELAGE APPROX STA 2007-2033 BETWEEN LONGERON 45R TO 46R END CAP REPAIRED AS PER FEDEX EA NR 1-5310-95817, TITLE: FUSELAGE LONGERON 45R CRACKED BApr 11, 2006 · N582FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 06FDEA1394Longeron · crackedEMPENNAGE AFT FUSELAGE APPROX STA 2007-2033 BETWEEN LONGERON 45L TO 46L, CAP SUSPECTED CRACKED. EMPENNAGE AFT FUSELAGE APPROX STA 2007-2033 BETWEEN LONGERON 45L TO 46L END CAP REPAIRED AS PER FEDEX EA NR 1-5310-95818, TITLE: FUSELAGE LONGERON 45L CRACKED BETWApr 11, 2006 · N582FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 06FDEA1376Block · corrodedCENTER LANDING GEAR REPLACEMENT, LEFT PILLOW BLOCK 3 OFF ATTACHMENT HOLES BORE SURFACE FOUND CORRODED. CENTER LANDING GEAR LEFT PILLOW BLOCK CORROSION REMOVED AND FOUND WITHIN LIMITS AS PER SRM 53-40-00 FIG 15 VOL I.Apr 11, 2006 · N582FE · Doug MD11F · Main Landing Gear Attach SectionSDR 06FDEA1375Block · corrodedCENTER LANDING GEAR REPLACEMENT RIGHT PILLOW BLOCK 3 OFF ATTACHMENT HOLES BORE SURFACE FOUND CORRODED. CENTER LANDING GEAR RIGHT PILLOW BLOCK ATTACHMENT HOLES CORROSION REMOVED AND FOUND WITHIN LIMIT AS PER SRM 53-40-00 FIG 15 VOL.I. REPAIR CLASSIFIED AS MINApr 11, 2006 · N582FE · Doug MD11F · Main Landing Gear Attach SectionSDR 06FDEA1371Support · corrodedCENTER LANDING GEAR REPLACEMENT LEFT PILLOW BLOCK ATTACHMENT BOTTOM MATING SURFACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5340-95821 FUSELAGE CENTER LANDING GEAR LT TRUNNION SUPPORT FITTING CORROSION REMOVAL AND REPAIR.Apr 11, 2006 · N582FE · Doug MD11F · Main Landing GearSDR 06FDEA1370Block · corrodedCENTER LANDING GEAR REPLACEMENT, RIGHT PILLOW BLOCK ATTACHMENT BOTTOM MATING SURFACE FOUND CORRODED. RT PILLOW BLOCK ATTACHMENT BOTTOM MATING SURFACE CORROSION REMOVED AND REPAIR CARRIED OUT AS PER SRM 53-40-00 FIG 15 VOL I. REPAIR CLASSIFIED AS MINOR AS PERApr 11, 2006 · N582FE · Doug MD11F · Emergency Flotation SectionSDR 06FDEA1373Seat Track · corrodedMAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STA 1581 RBL 8. MAIN DECK COMPARTMENT SEAT TRACK AT STA 1581 RBL 8 REPAIR CARRIED OUT AS PER SRM 53-70-00 VOL I FIG 1.Apr 11, 2006 · N582FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA1372Seat Track · corrodedMAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STA 1551 RBL 8. MAIN DECK COMPARTMENT SEAT TRACK AT STA 1551 RBL 8 CARRIED OUT. REPAIR AS PER SRM 53-70-00 FIG 1 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Apr 11, 2006 · N582FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA1396Frame · crackedRIGHT WING LEADING EDGE CANTED AREA FORMER AT STA XORS 480, SUSPECTED CRACKED. CRACK FORMER ON RT WING LEADING EDGE CANTED AREA AT STA XORS 480. REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II. NEW FORMER FABRICATED AS PER DWG ARB2931. REPAIR CLASSIFIED ASApr 11, 2006 · N582FE · Doug MD11 · Wing SparSDR 06FDEA1374Longeron Splice · crackedCENTER CARGO - LEFT HAND LONGERON 41 SPLICE AT STA 5-113 TO 1541 CRACKED. CRACKED SPLICE ON CENTER CARGO LEFT HAND LONGERON 41 AT STA 5-113 TO 1541 REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Apr 11, 2006 · N582FE · Doug MD11 · Fuselage Main, Longeron/StringerSDR 06FDEA1397Seat Track · corrodedMAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STA 1341-1361 RBL 75. MAIN DECK COMPARTMENT SEAT TRACK AT STA 1341-1361 RBL 75 CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE 1. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.Apr 11, 2006 · N582FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA1352Frame · dentedMAIN DECK COMPARTMENT FOUND FRAME WITH DENT AT STA 1721 LONGERON 12L. DENT ON FRAME OF M/D COMPARTMENT STA 1721 LONGERON 12L REPAIRED AS PER SRM 53-30-00 FIG.1 VOL.I. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. REPETITIVE INSPECTIONApr 10, 2006 · N582FE · Doug MD11 · Fuselage Main, FrameSDR 06FDEA1366Seat Track · crackedFOUND MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STA 5-20 RBL 27. CARRIED OUT REPAIR IAW SRM 53-70-00.Apr 10, 2006 · N582FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA1367Seat Track · corrodedFOUND MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STA 1805 LBL 8. CARRIED OUT REPAIR IAW SRM 53-70-00Apr 10, 2006 · N582FE · Doug MD11 · Fuselage Main, StructureSDR 06FDEA1368Fuel Cap · crackedLEFT LOWER WING ROOT STA Y1298 LOWER AUX TANK UPPER CAP FOUND WITH HAIR LINE CRACK MEASURED APPROX 4" IN LENGTH. COMPLIED WITH FEDEX EA 1-5310-95675, TITLE: FUSELAGE, CAP ANGLE LEFT UNDER WING BARREL STRUCTURE AT STATION Y=1298.6, XCW 46, CRACK ANGLE. FABRICApr 10, 2006 · N582FE · Doug MD11F · Fuel StorageSDR 06FDEA1369Fuel Cap · crackedFOUND RIGHT LOWER WING ROOT STA Y1288 TO 1298 LOWER AUX TANK UPPER CAP. FOUND WITH 1 HAIR LINE CRACK MEASURED APPROX 6" IN LENGTH. COMPLIED WITH FEDEX EA 1-5310-95676, TITLE: FUSELAGE CAP ANGLE RIGHT UNDER WING BARREL STRUCTURE AT STATION Y=1298.6, XCW 46, CApr 10, 2006 · N582FE · Doug MD11 · Fuel StorageSDR 06FDEA1353Seat Track · corrodedMAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STA 6-10 TO 6-30 LBL 8. MAIN DECK COMPARTMENT SEAT TRACK CORROSION AT STA 6-10 TO 6-30 LBL 8. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. REFApr 10, 2006 · N582FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA1345Intercostal · corrodedLT NR 1 AIR CONDITIONING COMPARTMENT APPROX. AT STA 575 INTERNAL FRAME INTERCOSTAL FOUND WITH SURFACE CORROSION. SURFACE CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II AND FOUND WITHIN LIMIT AS PER SRM 53-00-01 VOLUME I FIGURE 1A. ORIGINAL THICKNESS =Apr 9, 2006 · N582FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 06FDEA1342Stringer · crackedHFEC INSPECTION CARRIED OUT, FOUND CRACK ON LEFT WING STRINGER 14 END (CRACK LENGTH APPROX. 13"). CRACK ON LT WING STRINGER 14 END REPAIR CARRIED OUT AS PER SRM 57- 20-00 FIG 10 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Apr 9, 2006 · N582FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA1343Stringer · crackedHFEC INSPECTION CARRIED OUT ON LEFT WING STRINGER 40 END FOUND CRACK, CRACK LENGTH APPROX 1". CRACK ON LT WING STRINGER 40 END REPAIR CARRIED OUT AS PER SRM 57- 20-00 FIG 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Apr 9, 2006 · N582FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA1344Stringer · crackedHFEC INSPECTION CARRIED OUT ON RIGHT WING STRINGER 40 FOUND CRACK (CRACK LENGTH APPROX. 1"). CRACK ON RT WING STRINGER 40 END REPAIR CARRIED OUT AS PER SRM 57- 20-00 FIG 10 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Apr 9, 2006 · N582FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA1341Stringer · crackedHFEC INSPECTION CARRIED OUT, FOUND CRACK ON RIGHT WING STRINGER 13 END WITH CRACK LENGTH OF APPROX 12". FOUND CRACK ON RT WING STRINGER 13 END REPAIR CARRIED OUT AS PER SRM 57- 20-00 FIG 10 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Apr 9, 2006 · N582FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA1340Stringer · crackedHFEC INSPECTION CARRIED OUT ON RIGHT WING STRINGER 41 END FOUND CRACK (LENGTH APPROX. 1"). CRACK ON RT WING STRINGER 41 END REPAIR CARRIED OUT AS PER SRM 57- 20-00 FIG 10 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Apr 9, 2006 · N582FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA1346Seat Track · corrodedMAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STA 6-100 RBL 8. MAIN DECK COMPARTMENT SEAT TRACK AT STA 6-100 RBL 8 CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.Apr 9, 2006 · N582FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA1347Seat Track · corrodedMAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STA 6-88 TO 6-100 LBL 8. MAIN DECK COMPARTMENT SEAT TRACK AT STA 6-88 TO 6-100 LBL 8 CARRIED OUT. REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.Apr 9, 2006 · N582FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA02152Indication Sys · malfunctioned6 HOURS INTO FLIGHT GOT "FUEL MANF DRAIN" AND"TANK 2 FUEL QTY LO" LEVEL. FUEL READ 700 IN 1, 0IN 2, 700 IN 3, 500 AUX, 14000 IN TAIL. AFTER ACCOMPLISHING QRH PROCEDURE. MCDU INDICATED NR 19,000 FUEL REMAINING. RJAA 90 MILES AWAY. DECLARED EMERGENCY AND PRJul 31, 2005 · N582FE · Doug MD11 · Fuel Indicating SystemSDR 05FDEA00892Structure · corrodedSTABILIZERS - HORIZONTAL STABILIZER BARREL NUT BORES, CORROSION REMOVAL, COMPLY WITH EA 1-5510-71839. COMPLIED WITH EA 1-5510-71839.Apr 7, 2005 · N582FE · Doug MD11 · Horizontal Stabilizer Miscellaneous StructureSDR 05FDEA00891Structure · corrodedSTABILIZERS - HORIZONTAL STABILIZER BARREL NUT BORES, CORROSION REMOVAL COMPLY WITH EA 1-5510-71838. COMPLIED WITH EA 1-5510-71838.Apr 7, 2005 · N582FE · Doug MD11 · Horizontal Stabilizer Miscellaneous StructureSDR 05FDEA00886Spar Cap · crackedNACELLES/PYLONS - PYLON STRUCTURE - CRACK ON NR 2 ENGINE PYLON UPPER SPAR CAP COMPLY WITH EA 1-5450-76453. COMPLIED NR 2 ENG UPPER SPAR REPAIR PER EA 1-5450-81683.Apr 7, 2005 · N582FE · Doug MD11 · Nacelle/Pylon, Frame/Spar/RibSDR 05FDEA00768Flap · damagedLEFTHAND OUTBOARD FLAP; INBOARD HINGE ATTACH FITTING HAS 2.25 INCH CRACK ADJACENT TO ATTACH POINT. ACCESSED THRU PANEL 557GT. REMOVED & INSTALLED NEW FLAP P/N NRC6753-503,S/N LS0205 IAW MM 27-50-30-4. CHECKED & ADJUSTED O/B FLAP & VANE INW MM 27-50-32/27-5Mar 29, 2005 · N582FE · Doug MD11 · Wing, Attach FittingsSDR 04FDEA03110Plate · missingBOTH LT AND RT PRIMARY STATIC PORTS ARE MISSING THEIR RUB PLATES. REF: MD11 IPC CHAPTER 34-11-60-01, ITEM 322. DISCREPANCY FOUND DURING "C" CHECK MAINTENANCE. (OPEN)Nov 15, 2004 · N582FE · Doug MD11F · Pitot/Static SystemSDR 03FDEA01402Line · leakingAT BLOCK IN NUMBER 5 BRAKE LINE BROKE AND HYD FLUID SPRAYED ONTO HOT BRAKE CAUSING A FLAME WHICH QUICKLY WENT OUT. MEL 31AUG03 19:05 LCK R ACN RELEASED FOR SERVICE PER MEL/CDL: 32-43-02 CATEGORY: C EXPIRATION: 10SEP03 "MEL 32-43-02: NR 5 BRAKE HYD LINESep 2, 2003 · N582FE · Doug MD11 · Landing Gear Brake SystemSDR 03FDEA01090Structure · corrodedRT HORIZONTAL STABILIZER NR 34 BORE CORROSION EXCEEDED CONDITION "3". CORROSION ON RT HORIZONTAL STABILIZER NR 34 BORE REMOVED AND REPAIR CARRIED OUT IAW EA 1-5510-71839 (STABILIZERS - HORIZONTAL STABILIZER BARREL NUT BORES - CORROSION REMOVAL - BORE 34 RJul 11, 2003 · N582FE · Doug MD11 · Horizontal Stabilizer StructureSDR 03FDEA01089Barrel Nut · corrodedLT HORIZONTAL STAB NR 3 BORE CORROSION EXCEEDED LIMIT. LT HORIZONTAL STAB NR 3 BORE CORROSION REPAIR CARRIED OUT IAW EA 1-5510-71837, STABILIZERS- HORIZONTAL STAB BARREL NUT BORES- CORROSION REMOVAL- BORE 3 LEFT.Jul 9, 2003 · N582FE · Doug MD11 · Horizontal Stabilizer StructureSDR 03FDEA01072Structure · corrodedRT HORIZONTAL STABILIZER NR 36 BORE CORROSION EXCEEDED CONDITION "3". CORROSION ON RT HORIZONTAL STABILIZER NR 36 BORE REMOVED AND REPAIR CARRIED-OUT IAW EA 1-5510-71838 (STABILIZERS - HORIZONTAL STABILIZER BARREL NUT BORES - CORROSION REMOVAL BORE 36 RIJul 9, 2003 · N582FE · Doug MD11 · Horizontal Stabilizer Structure
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