N585FE

Service difficulty reports · 491

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 = 'N585FE' 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 FDEA201407141757Doubler · crackedLEFT WING LE COMPARTMENT BEADED DOUBLER AT STATION XOS 753 - 759. FOUND CRACKED DURING OTBD SLAT DRIVE CABLES INSPECTION & TENSION CHECK. CRACKED BEADED DOUBLER REPAIRED AS PER SRM 57-40-02 FIGURE 203 REPAIR 15 REVISION 56 REPAIR. CLASSIFIED MAJOR AS PER GJul 14, 2014 · N585FE · Doug MD11F · Wing Miscellaneous StructureSDR FDEA201308131870Fire Warning · false activationAT TAKE OFF, APROX 110 KTS. RECEIVED RED MASTER WARNING AND LEVEL 3 NR 3 ENG FIRE ALERT. REJECTED TAKEOFF AT POWER REDUCTION ON REJECT ALERT WENT AWAY. NO FIRE BELL. MAX PWR TAKEOFF.Aug 13, 2013 · N585FE · Doug MD11F · Fire DetectionSDR FDEA201307171577Wire Harness · damagedON DEPARTURE, RECEIVED A LEVEL 3 "ENG 3 FIRE" ALERT. APPEARED FOR APPROX 30 SECONDS THEN WENT OUT, THEN ONE MINUTE LATER RETURNED. SHUTDOWN ENGINE IAW QRH. FIRE WARNING CAME ON THREE MORE TIMES. FIRED SECOND BOTTLE, DECLARED EMERGENCY. R & R BOTH LOOPS AJul 17, 2013 · N585FE · Doug MD11F · Fire Protection System WiringSDR FDEA201210263752Unknown · unknownCENTER GEAR LIGHT DID NOT ILLUMINATE WITH GEAR DOWN. SECONDARY SHOWED DOWN AND LOCKED. RECYLED & LIGHT ILLUMINATED. PSCU HAS NO FAULT MEMORY STORED. FOLLOWED FIM 31-71-04-00 AND VISUALLY INSPECTION ALSO CLEANED CLG LOCKED SENSOR, NO DEFECT FOUND. THEN CLOct 26, 2012 · N585FE · Doug MD11F · Landing Gear Position and WarningSDR FDEA201210113594Floor Support · corrodedMAIN DECK FLOOR SUPPORT FOUND WITH CORROSION AT BS 1922, 1937 AND 1976, X= -58.5. REMOVED AND REPLACED AS PER AMM 20-50-02-4 REVISION 72.1. FLOOR SUPPORT MACHINED AS PER DRAWING AGA7551 REVISION G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6- 2-100 REVISION 115.Oct 11, 2012 · N585FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201210053557Hinge · wornMAIN DECK UPPER CARGO DOOR HINGE LOBES 04 PLACES WORN FORWARD HINGE AREA. REPAIRED IAW CMM 52-34-04 REVISION 74. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.Oct 5, 2012 · N585FE · Doug MD11F · Cargo/Baggage DoorsSDR FDEA201209253428Longeron · crackedDURING X-RAY INSPECTION, AT CABIN STATION 5-0, LONGERON 1R, FORWARD SECTION INBD ROW FROM EDGE TO NR 2 HOLE HAS A CRACK INDICATION APPROX 2.25" IN LENGTH. REPAIRED AS PER SRM 53-00-05 FIGURE 202 REPAIR 1 REVISION 50. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-Sep 25, 2012 · N585FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201209253427Longeron · crackedDURING X-RAY INSPECTION AT CABIN STATION 5-0, LONGERON 2L, FORWARD SECTION INBD ROW FROM EDGE CRACK INDICATION FOUND APPROX .3750" IN LENGTH. REPAIRED IAW SRM 53-00-05 FIGURE 202 REPAIR 1 REVISION 50. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 11Sep 25, 2012 · N585FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201209253426Longeron · crackedDURING X-RAY INSP AT CABIN STATION 5-0, LONGERON 2R STRINGER FORWARD SECTION OTBD ROW FROM EDGE CRACK INDICATION FOUND APPROX .3750" IN LENGTH. REPAIRED IAW SRM 53-00-05 FIGURE 202 REPAIR 1 REVISION 50. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION Sep 25, 2012 · N585FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201209243418Hinge · damagedDURING FPI ON RT INBD FLAP, OTBD HINGE (FLAP SIDE) PIVOT INBD HOLE FOUND DAMAGED. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03 REVISION 74. REPAIRED IAW EA 1-5750-162593 PART 1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.Sep 24, 2012 · N585FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201209233408Bushing · wornLEFT INBD FLAP, OTBD AFT (FLAP SIDE) HINGE PIVOT INBD BUSHING WORN. WORN BUSHING REMOVED AS PER CMM 20-20-07 REVISION 74. FOUND EXCEED LIMITS AS PER CMM 57-52-03 REVISION 74. NEW BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-162592 PART 1. REPAIR CLSep 23, 2012 · N585FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201209233407Hinge · corrodedLEFT OTBD FLAP, OTBD FORWARD (WING) HINGE ACTUATOR OTBD HOLE FOUND CORRODED. REPAIRED IAW EA 1-5750-162588. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.Sep 23, 2012 · N585FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201209233405Hinge · corrodedLEFT OTBD FLAP, OTBD FORWARD (WING) HINGE ACTUATOR INBD HOLE FOUND CORRODED. REPAIRED IAW EA 1-5750-162588. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.Sep 23, 2012 · N585FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201209233402Hinge · corrodedRT OTBD FLAP, INBD FORWARD (WING) HINGE ACTUATOR OTBD HOLE FOUND CORRODED. REPAIRED IAW EA 1-5750-162587 PART 1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115Sep 23, 2012 · N585FE · Doug MD11F · Wing Main, Frame StructureSDR FDEA201209233400Hinge · corrodedRT OTBD FLAP, INBD FORWARD (WING) HINGE ACTUATOR, INBD HOLE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 REVISION 74. EXISTING HOLE DIAMETER 1.249", FINAL HOLE DIAMETER 1.254", MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR ACCOMPLISHED AS PESep 23, 2012 · N585FE · Doug MD11F · Wing Main, Frame StructureSDR FDEA201209233411Bushing · wornRIGHT INBD FLAP, OTBD AFT (FLAP SIDE) PIVOT OTBD BUSHING WORN. WORN BUSHING REMOVED IAW CMM 20-20-07, REV 74. HOLE MEASURED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 74. EXISTING HOLE DIAMETER 1.258", MAXIMUM HOLE DIAMETER 1.220". NEW BUSHING FABRICATEDSep 23, 2012 · N585FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201209233410Bushing · wornRT INBD FLAP OTBD AFT (FLAP SIDE) HINGE PIVOT INBD BUSHING WORN. WORN BUSHING REMOVED IAW CMM 20-20-07 REV 74. HOLE MEASURED AND FOUND EXCEED LIMIT IAW CMM 57-52-03 REV 74. EXISTING HOLE DIAMETER 1.255", MAXIMUM HOLE DIAMETER 1.220". NEW BUSHING FABRICATEDSep 23, 2012 · N585FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201209233409Bushing · wornLEFT INBD FLAP, OTBD AFT (FLAP SIDE) HINGE PIVOT OTBD BUSHING WORN. REMOVED IAW CMM 20-20-07, REV 74. HOLE MEASURED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 74. EXISTING HOLE DIAMETER 1.254", MAXIMUM HOLE DIAMETER 1.220". NEW BUSHING FABRICATED AND INSSep 23, 2012 · N585FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201209233404Hinge Fitting · corrodedLEFT OTBD FLAP, INBD FORWARD (WING SIDE) HINGE ACTUATOR INBD HOLE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08, REV 74. EXISTING DIAMETER 1.228", FINAL DIAMETER 1.232", MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR ACCOMPLISHED IAW EA 1-575Sep 23, 2012 · N585FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201209213382Beam · crackedCENTER CARGO DOOR ACTUATOR MOUNTING BEAM FOUND CRACKED AT BS 1746 TO 1750. REPAIRED AS PER EA 1-5310-162594. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.Sep 21, 2012 · N585FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201209213380Longeron · corrodedCENTER CARGO COMPARTMENT LONGERON 49 LEFT CORRODED AT BS 1531 TO 1541. REPAIRED IAW EA 1-5310-162591. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.Sep 21, 2012 · N585FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201209213379Longeron Splice · crackedCENTER CARGO COMPARTMENT LONGERON SPLICE CRACKED AT LONGERON 49L BETWEEN BS 5-113 TO 1541. REMOVED AND REPLACED SPLICE IAW SRM 51-31-01 REVISION 50.Sep 21, 2012 · N585FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201209213381Longeron Splice · crackedLONGERON SPLICE, 47L, CRACKED AT BS 5-113 TO 1541. LONGERON SPLICE REMOVED AS PER SRM 51-31-01 REVISION 50. LONGERON SPLICE FABRICATED IAW DRAWING A5A7114 REVISION E AND INSTALLED IAW SRM 51-31-01 REVISION 50. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100Sep 21, 2012 · N585FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201209213378Longeron Splice · crackedCENTER CARGO COMPARTMENT LONGERON SPLICE AT 43RH BETWEEN STA 5-113 TO STA 1541 FOUND CRACKED. LONGERON SPLICE REMOVED AS PER SRM 51-31-01 REVISION 50. LONGERON SPLICE FABRICATED IAW DRAWING A5A7114 REVISION E. INSTALLED AS PER SRM 51-31-01 REVISION 50. REPSep 21, 2012 · N585FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201209213377Hinge Fitting · corrodedRT OTD FLAP, OTBD FORWARD WING HINGE ACTUATOR OTBD HOLE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09, REV 74 EXISTING HOLE DIAMETER 1.215", FINAL DIAMETER 1.221", MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR ACCOMPLISHED IAW EA 1-5750-162586, PASep 21, 2012 · N585FE · Doug MD11F · Wing Main, Frame StructureSDR FDEA201209213376Hinge Fitting · corrodedRT OTBD FLAP, OTBD FORWARD WING HINGE ACTUATOR INBD HOLE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09 REV 74. EXISTING HOLE DIAMETER 1.249", FINAL DIAMETER 1.254", MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR ACCOMPLISHED IAW EA 1-5750-162586 PASep 21, 2012 · N585FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201209203361Attach Fitting · corrodedRT WING T/E PANEL NR 641JB SUPPORT ATTACHMENT FOUND CORRODED. REPAIRED IAW EA1-5710-162382. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.Sep 20, 2012 · N585FE · Doug MD11F · Wing, Attach FittingsSDR FDEA201209203360Attach Fitting · corrodedLEFT WING PANEL ATTACHMENTS FOUND CORROSION. REPAIRED IAW EA 1-5710-162381. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.Sep 20, 2012 · N585FE · Doug MD11F · Wing, Attach FittingsSDR FDEA201209183346Skin · dentedLT OTBD SLAT NR 8 SKIN DENTED. R & R NR 8 SLAT ASSY ON LT WING IAW AMM 27-80-30-4, REV 74.0. CARRIED OUT ADJUSTMENT & TEST AND SLAT RANGE OF MOVEMENT IAW 27-80-30-5, REV 74.0 AND AMM 27-80-00-5, REV 74.0 FOUND SATISFACTORY. REPAIR CLASSIFIED AS MINOR IAW Sep 18, 2012 · N585FE · Doug MD11F · Leading Edge DevicesSDR FDEA201209183345Doubler · crackedCENTER LANDING GEAR COMPARTMENT LT BULKHEAD SPOILER CONTROL ROD CUTOUT SUPPORT DOUBLER FOUND CRACKED. DOUBLER REMOVED IAW SRM 51-31-01, REV 50. NEW DOUBLER FABRICATED BY MACHINING IAW DWG AEA0526 REVISION D AND INSTALLED IAW SRM 51-31-01, REV 50. REPAIR Sep 18, 2012 · N585FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201209183344Tee Fitting · crackedCENTER LANDING GEAR COMPARTMENT LT BULKHEAD TEE FITTING FOUND CRACKED. TEE FITTING REMOVED IAW SRM 51-31-01, REV 50. TEE FITTINGFABRICATED BY MACHINING IAW DWG APB7158 REV C AND INSTALLED IAW SRM 51-31-01, REV 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100,Sep 18, 2012 · N585FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201209183343Tee Fitting · crackedCENTER LANDING GEAR WW RT FORWARD BULKHEAD TEE FITTING CRACKED. R & R IAW SRM 51-31-01, REV 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.Sep 18, 2012 · N585FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201209183342Skin · damagedCENTER CARGO DOOR CUT-OUT FORWARD JAMB DOUBLER REPAIR EDGE FOUND BLENDED BY ABOUT .5" AT LONGERON 40RT. R & R IAW SRM 53-00-15, FIG 202, REPAIR 8, REV 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 115.Sep 18, 2012 · N585FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201207202628Landing Gear · malfunctionedAFTER TAKE OFF, RETRACTED LANDING GEAR, CENTER GEAR CUBE FLASHED RED (UNSAFE) RAN QRH CONFIG SYNOPTIC SHOWED CTR GEAR SAFE. FLASHING CENTER GEAR LIGHT APPROXIMATELY 25 MIN THEN STOPPED. NO FURTHER INDICATION PROBLEMS. ON EXTENSION OF GEAR FOR LANDING. THRU RJul 20, 2012 · N585FE · Doug MD11F · Landing Gear Position and WarningSDR FDEA201103140968Proximity Sensor · out of adjustUNSAFE LT MAIN GEAR UP ON DEPARTURE, COMPLIED WITH QRH AND COMFIRMED INDICATION WITH CONFIG PAGE. ALL MLG DOOR CLOSED ON ARRIVAL. PERFORMED T/S IAW FIM 32-30, PAGE 121. PERFORMED SELF TEST ON PSEU MM 31-71-01-2, NO FAULT. PERFORMED VISUAL INSP, NO DEFFECMar 14, 2011 · N585FE · Doug MD11F · Landing Gear Position and WarningSDR FDEA201101240337Light · inoperativeR1 DOOR PRESS TO TEST LIGHT DOESN'T WORK. RELEASED FOR SERVICE IAW MEL: 25-61-02, R & R REMOTE PRESSURE INDICATOR PER MM 25-61-04-4-0 , OPS CHECKED OK.Jan 24, 2011 · N585FE · Doug MD11F · Emergency EquipmentSDR FDEA201010063966Skin · cracked03 EACH FASTENER HOLES FOUND CRACK INDICATION DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT RIGHT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS= 683.4 AND STATION XORS=713.6. REPAIR CARRIED OUT AT RIGHT HAND WING LOWER SKIN ACCOct 6, 2010 · N585FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201010063965Skin · cracked06 EACH FASTENER HOLES FOUND CRACK INDICATION DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS= 683.4 TO STATION XORS= 713.6. REPAIR CARRIED OUT AT LEFT HAND WING LOWER SKIN ACCESS DOct 6, 2010 · N585FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201010063964Seat Track · corrodedMAIN DECK CARGO - SEAT TRACK FLANGE AT STATION 5-0 TO STATION 5-53 X= 8.5 FOUND WITH SURFACE CORROSION. SEAT TRACK REMOVED AND AND NEW SEAT TRACK INSTALLED IAW SRM 51-33-01 REV 44. NEW SEAT TRACK FABRICATED IAW DWG REV B. EXISTING SPLICE REMOVED AND RE-Oct 6, 2010 · N585FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201010063963Seat Track · corrodedMAIN DECK CARGO - SEAT TRACK FLANGE AT STA 5-53 TO STA 5-83 X= -8.5 FOUND WITH SURFACE CORROSION. SEAT TRACK R & R IAW SRM 51-33-01, REV 44. NEW SEAT TRACK FABRICATED IAW DWG A5A7082-1, REV B. EXISTING SPLICE REMOVED AND RE-INSTALLED IAW SRM 51-33-01, REVOct 6, 2010 · N585FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201010063962Seat Track · corrodedMAIN DECK CARGO - SEAT TRACK FLANGE AT STA 5-0 X= -8.5 FOUND WITH SURFACE CORROSION. SEAT TRACK R & R IAW SRM 51-33-01, REV 44. NEW SEAT TRACK FABRICATED IAW DWG A5A7082-1 REV B EXISITING SPLICE REMOVED AND RE-ISTALLED IAW SRM 51-33-01, REV 44. REPAIR COct 6, 2010 · N585FE · Doug MD11 · Fuselage Miscellaneous StructureSDR FDEA201010063961Seat Track · crackedMAIN DECK CARGO - SEAT TRACK FLANGE AT STA 1521 X=75 FOUND CRACKED. TRIMMED OUT IAW SRM 53-00-52, FIG 201, REVISION 44. CRACK SEAT TRACK REMOVED IAW SRM 51-33-01 REV 44. REPAIR SEAT TRACK AND SPLICE FABRICATED AND INSTALLED IAW SRM 53-00-52, FIG 201, REV 44.Oct 6, 2010 · N585FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201010053919Longeron · crackedWASTE TANK COMPARTMENT BILGE AREA STATION 1982 LONGERON L-47L CRACKED. REPAIRED IAW SRM 53-00-05 FIGURE 202, REV 44. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.Oct 5, 2010 · N585FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201010043898Frame · damagedFRAME AT STATION 1681 LONGERON 12L FOUND DEFORMED AT EXISTING DOUBLER REPAIR. EXISTING DOUBLER REPAIR REMOVED AND NEW REPAIR ANGLE INSTALLED AS PER SRM 51-33-01 REVISION 44. NEW REPAIR ANGLE FABRICATED AS PER SRM 53-00-07 FIGURE 201 REVISION 44. THIS REPAIROct 4, 2010 · N585FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201010043896Frame · deformedMAIN DECK CARGO - FRAME AT STATION 1701 LONGERON 12R FOUND DEFORMED. REPAIR ANGLE REMOVED AND NEW REPAIR ANGLE INSTALLED AS PER SRM 51-33-01 REVISION 44. NEW REPAIR ANGLE FABRICATED AS PER SRM 53-00-07 FIGURE 201 REVISION 44. THIS REPAIR IS CLASSIFIED AOct 4, 2010 · N585FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201010043893Skin · crackedRIGHT WING LEADING EDGE LOWER CUTOUT AT SLAT TRACK NR 14 FOUND CRACKED. REPAIR CARRIED OUT AT RT WING LEADING EDGE LOWER CUTOUT AT SLAT TRACK NR 14 AREA AS PER SRM 57-40-02 FIGURE 201 REVISION 44 REPAIR 7. THIS REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6-2-10Oct 4, 2010 · N585FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201010043892Skin · crackedLEFT WING LEADING EDGE CUTOUT AT SLAT TRACK NR 14 FOUND CRACKED. REPAIR CARRIED OUT AT LT WING LEADING EDGE LOWER CUTOUT AT SLAT TRACK NR 14 AS PER SRM 57-40-02 FIGURE 201 REVISION 44. THIS REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.Oct 4, 2010 · N585FE · Doug MD11F · Leading Edge DevicesSDR FDEA201010043897Frame · deformedMAIN DECK CARGO - FRAME AT STATION 1741 LONGERON 12LH FOUND DEFORMED. TRIMMED OUT IAW SRM 53-00-07, FIG 201, REVISION 44. REPAIR ANGLE FABRICATED AND INSTALLED IAW SRM 53-00-07, FIG 201 REVISION 44. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.Oct 4, 2010 · N585FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201010043895Frame · deformedMAIN DECK CARGO - FRAME AT STATION 1661 LONGERON 12R FOUND DEFORMED. TRIMMED OUT IAW SRM 53-00-07, FIG 201 REVISION 44. REPAIR ANGLE FABRICATED AND INSTALLED IAW SRM 53-00-07, FIG 201 REVISION 44. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.Oct 4, 2010 · N585FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201010043894Frame · deformedMAIN DECK CARGO - FRAME AT STATION 1641 LONGERON 12R FOUND DEFORMED. TRIMMED OUT IAW SRM 53-00-07, FIG 201 REV 44. REPAIR ANGLE FABRICATED AND INSTALLED IAW SRM 53-00-07, FIG 201, REV 44. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.Oct 4, 2010 · N585FE · Doug MD11F · Fuselage Main, Frame
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