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 FDEA200902230644Seat Track · corrodedMAIN DECK, SEAT TRACK AT STA 1880, X= -8.5, FOUND 01 CORROSION IN THE CHANNEL. REPAIRED AS PER SRM 53-70-00 FIG 1 VOL. I. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Feb 23, 2009 · N582FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200902230639Seat Track · corrodedMAIN DECK, SEAT TRACK AT STA 1326, X= -8.5, UNDER FLOOR PANEL NR 263LF FOUND 02 CORROSION NEAR FASTENER HOLES. REPAIRED FROM STA. 1310 TO STA 1370, X= -8.5 AS PER SRM 53-70-00 FIG.I VOL. I. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Feb 23, 2009 · N582FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200902230637Skin · corrodedRT WING, UPPER SKIN CORROSION AT APPROX XORS= 260, STRINGER 31. REPAIRED AS PER SRM 51-00-01 FIG 6 VOL. I. THIS REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Feb 23, 2009 · N582FE · Doug MD11F · Wing, Plate/SkinSDR FDEA200902230636Longeron · crackedMAIN DECK, BELOW NR 3R DOOR SILL AREA AT STA 1293, LONGERON 27R FOUND 01 SUSPECT CRACK AT THE RADIUS. REMOVED AND REPLACED AS PER SRM 51-31-00 VOL. II. REPAIR CLASSIFIED AS PER MAJOR AS PER GMM 6- 2-100.Feb 23, 2009 · N582FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA200902230634Seat Track · corrodedCABIN, LT STATION 415 TO 475, X=107 SEAT TRACK FOUND CORROSION. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED AS PER MAJOR AS PER GMM 6-2-100.Feb 23, 2009 · N582FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200902230633Frame · dentedCABIN, RT STATION 1681, LONGERON 11 TO LONGERON 13 FRAME FOUND DENT. REPAIRED AS PER SRM 53-30-00 FIG. I VOL I. REPETITIVE INSPECTION REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00 FIG. I VOL I. REPAIFeb 23, 2009 · N582FE · Doug MD11F · Fuselage Main, FrameSDR FDEA200902230632Frame · dentedCABIN, LT STATION 1641, LONGERON 11 TO LONGERON 13 FRAME FOUND DENT. REPAIRED AS PER SRM 53-30-00 FIG. I VOL I. REPETITIVE INSPECTION REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00 FIG. I VOL I. REPAIFeb 23, 2009 · N582FE · Doug MD11F · Fuselage Main, FrameSDR FDEA200902230631Frame · dentedCABIN, RT STATION 1721, LONGERON 11 TO LONGERON 13 FOUND DENT. REPAIRED AS PER SRM 53-30-00 FIG. I VOL. I. REPETITIVE INSPECTION REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00 FIG. I VOL. I. REPAIRFeb 23, 2009 · N582FE · Doug MD11F · Fuselage Main, StructureSDR FDEA200902230630Frame · dentedCABIN, RT STATION 1701, LONGERON 11 TO LONGERON 13 FOUND DENT. REPAIRED AS PER SRM 53-30-00 FIG. I VOL. I. REPETITIVE INSPECTION REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00 FIG. I VOL. I. REPAIR Feb 23, 2009 · N582FE · Doug MD11F · Fuselage Main, StructureSDR FDEA200902200619Hinge Bracket · corrodedLT WING, OTBD FLAP INBD FWD HINGE BRACKET ACTUATOR ATTACH INBD BORE FOUND WITH CORROSION. COMPLIED WITH EA 1-5750-127460. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Feb 20, 2009 · N582FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200902200618Hinge Bracket · corrodedLT WING, OTBD FLAP OUTBD FWD HINGE BRACKET LOWER ATTACH OTBD BORE FOUND WITH CORROSION. COMPLIED WITH EA 1-5750-127462. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Feb 20, 2009 · N582FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200902200610Stop Fitting · crackedLT WING OTBD FLAP SECONDARY UP STOP CRACKED. CRACKED FITTING REMOVED AND REPLACED NEW FITTING AT LT WING OUTBD FLAP AS PER SRM 51-33-01 VOL. II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Feb 20, 2009 · N582FE · Doug MD11F · Trailing Edge FlapsSDR FDEA200902200609Hinge Bracket · corrodedRT WING, OTBD FLAP OTBD FORWARD HINGE BRACKET LOWER ATTACH BORE FORWARD FACE FOUND WITH CORROSION. COMPLIED WITH EA 1-5750-128580. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Feb 20, 2009 · N582FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200902200608Support Fitting · crackedCRACK INDICATION FOUND ON 1ST LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520 INCH HOLE AT MAIN CARGO DOOR NR 4 LOWER JAMB AT HOLE D. COMPLIED WITH EA 1-5310-127432. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Feb 20, 2009 · N582FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA200902200607Support Fitting · crackedCRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTING AT HOLES A, B, C AND D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG. 10 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-10Feb 20, 2009 · N582FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA200902200606Support Fitting · crackedCRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 6 SUPPORT FITTING AT HOLES A, B, C AND D. SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-00 VOL. II. NEW SUPPORT FITTING FABRICATED AS PER DRAFeb 20, 2009 · N582FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA200902200605Support Fitting · crackedCRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 5 SUPPORT FITTING AT HOLES A, B, C AND D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG. 10 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-10Feb 20, 2009 · N582FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA200902200604Support Fitting · crackedCRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 4 SUPPORT FITTING AT HOLES A, B, C AND D. REMOVED AND REPLACED REFER TO EA 1-5310-127432. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Feb 20, 2009 · N582FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA200902200603Support Fitting · crackedCRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 3 SUPPORT FITTING AT HOLES A, B, C AND D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG. 10 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-10Feb 20, 2009 · N582FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA200902200602Support Fitting · crackedCRACK INDICATION FOUND DURING HFEC OPEN HOLE ISPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 2 SUPPORT FITTING A, B, C AND D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG. 10 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Feb 20, 2009 · N582FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA200902200601Support Fitting · damagedCRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 1 SUPPORT FITTING AT HOLES A, B, C AND D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG. 10 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-10Feb 20, 2009 · N582FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA200902170559Vane · delaminatedLEFT WING INBOARD FLAP VANE FOUND DELAMINATION ON LOWER SURFACE. REMOVED AND REPLACED AS PER AMM 27-50-22-4. ADJUSTMENT AND TEST CARRIED OUT FOUND SATISFACTORY AS PER AMM 27-50-22-5.Feb 17, 2009 · N582FE · Doug MD11F · Trailing Edge FlapsSDR FDEA200902170558Skin · damagedLEFT WING LEADING EDGE SKIN AT NR 3 SLAT FOUND WITH CUT MARK. REPAIR CARRIED AT LT WING LEADING EDGE SKIN AT NR 3 SLAT TRACK AS PER SRM 57-10-00 FIG 24 VOL I. REPAIR CLASSIFIED AS PER GMM 6-2-100.Feb 17, 2009 · N582FE · Doug MD11F · Leading Edge DevicesSDR FDEA200902040454Gcu · failedEPGS FAULT FOLLOWED BY NR 3 GEN OFF PASSING 5000 FT ON DEP. RAN NR 3 ENG PER MD-11 JRH SEVERAL TIMES. COULDN'T DUPLICATE B FAULT. COMPARED WITH NR 1 ENG, ALL INDICATION NML. OPERATED EPCU IN MANUAL MODE, TURN "GEN RELAY" AND BUS TIE RELAY" OFF THEN ON. AFeb 4, 2009 · N582FE · Doug MD11F · AC Generator-AlternatorSDR 07FDEA03161Bracket · damagedRIGHT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) FORWARD SUPPORT INBOARD AFT BORE EXISTING DIAMETER = 0.5INCH. COMPLIED WITH FEDEX EA 1-5750-115159.Aug 28, 2007 · N582FE · Doug MD11F · Wing Main, Frame StructureSDR 07FDEA03141Seat Track · crackedFORWARD CARGO COMPARTMENT, MAIN DECK CARGO SEAT TRACK LBL 47.5 FOUND CRACK. 09-04-07 MAIN DECK CARGO SEAT TRACK FROM STA 625 TO STA 665 LBL 47.5 REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG. 1 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Aug 27, 2007 · N582FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA03138Strut · corrodedRIGHT WING, OUTBOARD FLAP OUTBOARD HINGE AFT FAIRING STRUT 1 FASTENER HOLE FOUND CORROSION. 09-04-07 COMPLIED WITH FEDEX E.A. 1-5750-115158, CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100.Aug 27, 2007 · N582FE · Doug MD11F · Trailing Edge FlapsSDR 07FDEA03137Strut · corrodedRIGHT WING, OUTBOARD FLAP INBOARD HINGE AFT FAIRING STRUT 1 FASTENER HOLE FOUND CORROSION. 09-04-07 COMPLIED WITH FEDEX E.A. 1-5750-115157, CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100.Aug 27, 2007 · N582FE · Doug MD11F · Trailing Edge FlapsSDR 07FDEA03136Hinge · corrodedRIGHT WING, OUTBOARD FLAP INBOARD HINGE AFT FAIRING SUPPORT 1 FASTENER HOLE FOUND CORROSION. 09-04-07 COMPLIED WITH FEDEX E.A. 1-5750-115156, CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100.Aug 27, 2007 · N582FE · Doug MD11F · Trailing Edge FlapsSDR 07FDEA03081Panel · crackedRIGHT WING REFUELING PANEL CUT OUT INBOARD CORNER FOUND WITH CRACK. 09-04-07 RT WING REFUELLING PANEL CUT OUT INBOARD CORNER REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG. 21 VOL. I. REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100.Aug 24, 2007 · N582FE · Doug MD11F · Wing Main, Frame StructureSDR 07FDEA02974Support Fitting · crackedCRACK FOUND ON OUTBOARD FASTENER HOLE OF LOWER ROW FASTENERS OF ARC4009 RIGHT OUTBOARD FLAP HINGE SUPPORT FITTING. 09-04-07 RT OUTBOARD FLAP ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-00-830-805, FOUAug 19, 2007 · N582FE · Doug MD11F · Trailing Edge FlapsSDR 07FDEA02973Skin · crackedCRACK INDICATIONS REVEALED IN FASTENER HOLES TOWARDS EDGE OF ACCESS CUTOUT IN LHW LOWER SKIN ACCESS DOOR, BETWEEN STA XORS=683.400 TO STA XORS=713.600. 09-04-07 COMPLIED WITH FEDEX E.A. 1-5710-115154, CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.Aug 19, 2007 · N582FE · Doug MD11F · Wing, Plate/SkinSDR 07FDEA02972Skin · crackedCRACK INDICATIONS REVEALED IN FASTENER HOLES TOWARDS EDGE OF ACCESS CUTOUT IN RT WING LOWER SKIN ACCESS DOOR, BETWEEN STA XORS=683.400 TO STA XORS=713.600. 09-04-07 COMPLIED WITH FEDEX EA 1-5710-115155, CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.Aug 19, 2007 · N582FE · Doug MD11F · Wing, Plate/SkinSDR 07FDEA02960Support Fitting · brokenLEFT WING, NR 3 LEADING EDGE SLAT OUTBOARD SUPPORT FITTING BROKEN. 09-04-07 REMOVED & REPLACED AS PER AMM 27-80-30. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-80-30, FOUND SATISFACTORY.Aug 17, 2007 · N582FE · Doug MD11F · Leading Edge DevicesSDR 07FDEA02958Structure · crackedRIGHT WING, ANTI-ICE TELESCOPING DUCT DOOR CUTOUT CORNER FOUND CRACK. 09-04-07 COMPLIED WITH FEDEX EA 1-5710-115161, CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100.Aug 17, 2007 · N582FE · Doug MD11F · Wing Main, Frame StructureSDR 07FDEA02957Structure · crackedLEFT WING, LEADING EDGE TELESCOPING DUCT CUTOUT OUTBOARD CORNER FOUND CRACK. 09-04-07 COMPLIED WITH FEDEX E.A. 1-5710-115160, CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100.Aug 17, 2007 · N582FE · Doug MD11F · Wing Main, Frame StructureSDR 07FDEA02956Structure · crackedLEFT WING, LEADING EDGE SLAT DROOP LOWER SURFACE FOUND CRACK. 09-04-07 LT WING LEADING EDGE SLAT DROOP ASSY REMOVED AND REPLACED AS PER AMM 27-80-10. ADJUSTMENT CARRIED OUT AS PER AMM 27-80-10, FOUND SATISFACTORY.Aug 17, 2007 · N582FE · Doug MD11F · Wing Main, Frame StructureSDR 07FDEA02793Wire · damagedPASSING FL 270 ON CLIMB A/P TRIPPED OFF FOLLOWED BY MULTIPLE OTHER ALERTS. ENGINE NR 3 FLAMED OUT WITH "0" FUEL FLOW. FOLLOWED CHECKLIST FOR RESTART WITH NO SUCCESS. TANK NR 3 PUMPS WERE UNPOWERED. ENG NR 3 WAS SUCTION FEEDING. ATTEMPTED RESTART WITH FUAug 8, 2007 · N582FE · Doug MD11F · Electrical Power System WiringSDR 07FDEA00153Valve · failedON DEPARTURE WHEN WING ANTI-ICE SELECTED ON GOT WING ANTI-ICE DISAGREE AND MOMENTARILY MANIFOLD FAIL. PERFORMED QRH PROCEDURE, REMAINED CLEAR OF ICING CONDITION. WING DISAGREE INDICATION REMAINED. TROUBLE SHOT CARRIED OUT PRECAUTIONARY MEASURE DELTA P SENSOJan 23, 2007 · N582FE · Doug MD11 · Ice DetectionSDR 06FDEA1683Skin · dentedFUSELAGE - EXTERIOR SKIN WHILE CARRYING OUT REPETITIVE INSPECTION ON DENTED MARK AT STA 640 STRINGER 38L TO 39L FOUND REQUIRE REPAIR. FORWARD CARGO STA 640 STRINGER 38L TO 39L DENTED MARK CARRIED OUT REPAIR AS PER SRM 53-20-00 FIGURE 16 VOLUME I. REPAIR CLASMay 3, 2006 · N582FE · Doug MD11 · Fuselage Main, Plate/SkinSDR 06FDEA1682Skin · dentedFUSELAGE - EXTERIOR SKIN WHILE CARRYING OUT REPETITIVE INSPECTION ON DENTED MARK 3 FEET AFT OF CENTER CARGO DOOR FOUND REQUIRE REPAIR. THREE FEET AFT OF CENTER CARGO DOOR DENTED SKIN CARRIED OUT REPAIR AS PER SRM 53-20-00 FIGURE 6 VOLUME I. REPAIR CLASSIFIEDMay 3, 2006 · N582FE · Doug MD11 · Fuselage Main, Plate/SkinSDR 06FDEA1629Seat Track · corrodedSNRM N01239: MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STA 1795 RBL 27. SNRM N01239: MAIN DECK COMPARTMENT SEAT TRACK AT STA 1795 RBL 27 CARRIED OUT. REPAIR IAW SRM 53-70-00 FIG1, VOL 1. REPAIR CLASSIFIED AS MAJOR IAW MFG GMM 6-2-100.Apr 27, 2006 · N582FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA1557Trunnion · corrodedDURING THE CORROSION REMOVAL OF CENTER LANDING GEAR LEFT TRUNNION SUPPORT FITTING FOUND FORWARD BOLT HOLE TOP SPOTFACE AREA WITH CRACK. REPAIRED AS PER FEDEX EA NR 1-5340-95821.Apr 20, 2006 · N582FE · Doug MD11 · Fuselage, Landing Gear Attach FittingsSDR 06FDEA1515Door Frame · corrodedR3 DOOR JAMB AREA FOUND WITH CORROSION. R3 DOOR JAMB AREA CARRIED OUT REPAIR AS PER SRM 53-50-00 FIG 17 VOL I. THIS REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Apr 19, 2006 · N582FE · Doug MD11 · Fuselage Main, StructureSDR 06FDEA1491Skin · corrodedMAIN DECK COMPARTMENT CENTER WING TANK TOP SURFACE FOUND CORROSION BETWEEN STRINGER 14 AND STRINGER 15 LBL 66. MAIN DECK COMPARTMENT CENTER WING TANK TOP SURFACE CORROSION BETWEEN STRINGER 14 AND STRINGER 15 LBL 66. REMOVED AS PER SRM 51-21-01 VOL II ORIG THApr 18, 2006 · N582FE · Doug MD11 · Fuselage Main, Plate/SkinSDR 06FDEA1492Skin · corrodedMAIN DECK COMPARTMENT CENTER WING TANK TOP SURFACE FOUND WITH CORROSION, STRINGER 19 LBL 104. MAIN DECK COMPARTMENT CENTER WING TANK TOP SURFACE CORROSION AT STRINGER 19 LBL 104 REMOVED AS PER SRM 51-21-01 VOL II ORIG THICKNESS: 0.150"; THICKNESS REMAINING:Apr 18, 2006 · N582FE · Doug MD11 · Fuselage Main, Plate/SkinSDR 06FDEA1480Fuel Tank · corrodedMAIN DECK COMPARTMENT CENTER WING TANK TOP SURFACE FOUND WITH CORROSION AT STRINGER 15 RBL 75 TO RBL 104. REMOVED AS PER SRM 51-21-01 VOLUME II. REWORKED AREA MEASURED: MATERIAL THICKNESS = 0.164", THICKNESS REMAINED = 0.147", THICKNESS REMOVED = 0.017" FOApr 17, 2006 · N582FE · Doug MD11F · Fuel StorageSDR 06FDEA1479Fuel Tank · corrodedMAIN DECK COMPARTMENT CENTER WING TANK TOP SURFACE FOUND WITH CORROSION AT STRINGER 16 RBL 79. REMOVED AS PER SRM 51-21-01 VOLUME II. REWORKED AREA MEASURED: MATERIAL THICKNESS = 0.194", THICKNESS REMAINED = 0.158", MATERIAL REMOVED = 0.036". FOUND WITHINApr 17, 2006 · N582FE · Doug MD11F · Fuel StorageSDR 06FDEA1484Longeron · crackedLONGERON 48L FOUND CRACKED AFTER SPLICE REMOVAL FOR REPAIR, FORWARD OF STA 5 -113, CENTER CARGO COMPARTMENT. REMOVED AND REPLACED WITH NEW LONGERON IAW SRM 51-33-01 VOL.II. REPAIR CLASSIFIED AS MAJOR IAW FEDEX GMM 6-2-100.Apr 17, 2006 · N582FE · Doug MD11 · Fuselage Main, Longeron/StringerSDR 06FDEA1483Longeron · crackedLONGERON 52 STA 979 FOUND CRACKED AFTER FASTENERS REMOVED FOR CORROSION CLEAN UP ON CAP ANGLE FORWARD CARGO. COMPLIED WITH FEDEX EA 1-5330-95835.Apr 17, 2006 · N582FE · Doug MD11 · Fuselage Main, Longeron/Stringer
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