N643FE

Service difficulty reports · 350

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 = 'N643FE' 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 FDEA201410313433Warning Light · false activationSLIDE LIGHT ILLUMINATED. ON ACFT ARRIVAL FOUND SLIDE CYLINDER PRESS IS IN GREEN BAND & MICRO JACK WAS CONNECTED. SLIDE RAFT CYLINDER PRESS TESTED OK IAW AMM 25-61-06-5. ACFT OK FOR SERVICE.Oct 31, 2014 · N643FE · Doug MD11F · Emergency EquipmentSDR FDEA201406221507Handle · lack of lubeAFTER TAKEOFF WITH GEAR LEVER UP & IN THE FOUR GEAR INDICATOR LIGHTS ADJACENT TO GEAR HANDLE & ON CONFIG PAGE REMAINED ILLUMINATED RED. GEAR HANDLE RECHECKED UP & IN BUT NO CHANGE. ACCOMPLISHED QRH PROCEDURE, LOWERED GEAR WITH FOUR GREEN THEN RETRACTED GEAR.Jun 22, 2014 · N643FE · Doug MD11F · Landing Gear SelectorSDR FDEA201404280869Gcu · inoperativeCLIMBING THRU FL 260, NR 1 GENERATOR OFF ILLUMINATED. WHILE WORKING THAT PROBLEM, NR 3 GENERATOR ALERT ILLUMINATED, FOLLOWED BY TR 1 FAIL & BATTERY DISCHARGING ALERTS. DIVERTED. R & R NR 3 TR IAW AMM 24-31-01-2.Apr 28, 2014 · N643FE · Doug MD11F · AC Generator-AlternatorSDR FDEA201309132204Skin · crackedSIX FASTENER HOLES FOUND TO HAVE CRACK INDICATIONS, DURING OPEN-HOLE HFEC INSPECTION ON RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS 690 AND XORS 700. REPAIRED IAW EA 1-5710-T0302389 PART 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 117.Sep 13, 2013 · N643FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201309132203Skin · crackedTHREE FASTENER HOLES FOUND TO HAVE CRACK INDICATIONS DURING OPEN-HOLE HFEC INSPECTION ON LT WING LOWER SKIN ACCESS DOOR CUTOUT, BETWEEN XORS 690 AND XORS 700. REPAIRED IAW EA 1-5710-T0302390B PART 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 11Sep 13, 2013 · N643FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201309122187Frame · dentedFRAME FOUND DENTED AT BS 1641, LONGERON 12 RIGHT. REPAIRED IAW SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 53. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 117.Sep 12, 2013 · N643FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201309072155Attach Bracket · corrodedRIGHT WING INBD FLAP, INBD DRIVE LINK ATTACH BRACKET BORE, FLAP SIDE, FOUND CORRODED. DRIVE LINK ATTACH BRACKET BORE (FLAP SIDE) REWORKED IAW SRM 51-21-01 REVISION 53. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 117.Sep 7, 2013 · N643FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201309072154Attach Bracket · corrodedLEFT WING INBD FLAP, INBD DRIVE LINK, ATTACH BRACKET BORE, FLAP SIDE, FOUND CORRODED. REWORKED CORROSION IAW SRM 51-21-01REVISION 53. REPAIRED IAW EA 1-5750-T0302436 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 117.Sep 7, 2013 · N643FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201309072153Hinge Fitting · corrodedRT WING INBD FLAP AFT HINGE BRACKET PIVOT INBD LUG BORE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMITS IAW CMM 57-52-03 REVISION 76. BLEND OUT CARRIED OUT IAW SRM 57-00-00 REVISION 53. REPAIRED IAW EA 1-5750-T0302386 PART 1 STEP 1,3,4,5,7 AND 8. REPAIR Sep 7, 2013 · N643FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201309072152Hinge Fitting · corrodedRT WING INBD FLAP AFT HINGE BRACKET PIVOT OTBD LUG BORE FOUND CORRODED. FOUND EXCEED LIMITS IAW CMM 57-52-03 REVISION 76. BLEND OUT CARRIED OUT IAW SRM 57-00-00 REVISION 53. REPAIRED IAW EA 1-5750- T0302386 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2Sep 7, 2013 · N643FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201309062145Hinge Fitting · corrodedLEFT WING INBD FLAP, AFT HINGE BRACKET PIVOT INBD LUG BORE FOUND CORRODED. REPAIRED IAW EA 1- 5750-T0302385 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 117.Sep 6, 2013 · N643FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201309062144Hinge Fitting · wornLEFT WING INBD FLAP, AFT HINGE BRACKET PIVOT OTBD LUG BORE FOUND DAMAGED. FLAP AFT HINGE BRACKET PIVOT OUTBOARD LUG BORE REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03 REVISION 76. REPAIRED IAW EA 1-5750-T0302385 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMSep 6, 2013 · N643FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201309062143Frame · dentedFRAME BS 1661 LONGERON 12 LT, FOUND DENTED. REPAIRED IAW SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 53. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 117.Sep 6, 2013 · N643FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201309062141Frame · dentedFRAME BS 1641, LONGERON 12 LT, FOUND DENTED. REPAIRED IAW SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 117.Sep 6, 2013 · N643FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201309062142Frame · dentedFRAME BS 1641, LONGERON 12 LT, FOUND DENTED. REPAIRED IAW SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 117.Sep 6, 2013 · N643FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201309062140Frame · dentedFRAME BS 1681, LONGERON 12R FOUND DENTED. REPAIRED IAW SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 53. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 117.Sep 6, 2013 · N643FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201309062139Frame · dentedBS 1661, LONGERON 12R. FRAME FOUND DENTED. REPAIRED IAW SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 53. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 117.Sep 6, 2013 · N643FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201309052124Seat Track · damagedBS 1124, X = -47.5 SEAT TRACK CROWN FOUND DAMAGED. REPAIRED BY SECTIONAL REPLACEMENT FROM BS 1089 TO 1129 IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 53. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 117.Sep 5, 2013 · N643FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201305020898Fmu · faulted"FADEC ALT" MANUAL THROTTLES AT T/O NR 2 WOULD NOT ACHIEVE "MAX POWER" AT FADEC BAR, BOTH EPR & N1 NOTED BELOW NR 1 & 3 ENG. FADEC MODE IN NORMAL AND ALT. ALL ENGINE PARAMETERS WITHIN SPECIFIED LIMITS OUTLINED IN JRH. PERFORMED MAX POWER ASSURANCE RUN. NOTMay 2, 2013 · N643FE · Doug MD11F · Fuel Controlling SystemSDR FDEA201304080744Engine · failedON DOWN WIND DTW 4000, 190 KTS HEARD BANG AND FELT VIBRATIONS NR 3 RPM LO ALERT DISPLAYED" N1 18 PERCENT, EGT 540 N2 :45 PERCENT COMPLIED WITH ENG RPM LO CHECKLIST AND SHUTDOWN ENGINE. R & R NR 3 ENGINE. EA 1-7100-167353 COMPLIED WITH. OPS CHECKED GOOD.Apr 8, 2013 · N643FE · Doug MD11F · Engine (Turbine/Turboprop)SDR FDEA201303090531Tank · overheatedDURING, PERFORMED MX "A" CHECK ITEM 11,B) FOUND EVIDENCE OF BURNED CARGO FOAM STORAGE TANK SURROUNDING COVER, PROBABLY HEATING COIL WAS SHORTED. DETAILED INSPECTION OF NR 2 GENERATOR FEEDER LINE, CARGO FOAM HEATER CIRCUIT BREAKER (NOT TRIPPED) AND OTHER WIRMar 9, 2013 · N643FE · Doug MD11F · Extinguishing SystemSDR FDEA201301110068Spar Cap · cracked1.625" CRACK RT WING AT STATION XROS 1042. REMOVED AND TEMP INSTALLED TANK PLATE 639EB. REQUIRES HFEC SURFACE PROBE INSPECTION OF R/S CAP HORIZONTAL AND VERTICAL FLANGES FOR DISCONTINUITIES. REPORT TO ENGINEERING IF ANY FINDINGS. PERFORMED HFEC REF SIDJan 11, 2013 · N643FE · Doug MD11F · Wing SparSDR FDEA201205302017Control Panel · burnedSHORTLY AFTER TAKE OFF, HAD AN UNCOMMANDED LIGHT ON EFB 1 (CAPTS) POWER START STOP SWITCH. IT WAS NOT SELECTED AS IT WAS ALREADY DEFERRED, POWER LIGHT WENT ON/OFF MOMENTARILY FOR ONLY FEW SEC'S. FAINT ACRID/ELECTRICAL ODOR NOTED FOR BRIEF TIME. NOTED NO SMay 30, 2012 · N643FE · Doug MD11F · Central WarningSDR FDEA201202280702Control Handle · dirtyON APPROACH, COULD NOT OBTAIN SAFE GEAR INDICATION. ALL GEAR INDICATED UNSAFE ON BOTH THE GEAR HANDLE & CONFIG DISPLAY. EXECUTED MISSED APPROACH. RECYCLED & WERE FINALLY ABLE TO OBTAIN A SAFE GEAR INDICATION ON BOTH THE GEAR HANDLE & CONFIG DISPLAY. PERFORFeb 28, 2012 · N643FE · Doug MD11F · Landing Gear SelectorSDR FDEA201110224619Skin · dentedLT WING SLAT NR 12 FOUND TOP SURFACE NICKED DURING GROUND CREW CHECK NR1 SLAT (LT) NR B6224-509, SN 48476, SRM 57-00-00, FIGURE 202, LT WING NR 1 SLAT XIS 188 NICK BLENDOUT TO 1.0" RADIUS. DEEPEST MEASURED 0.033" AND REPROTECTED IAW SRM 51-21-01, REV 47. ACOct 22, 2011 · N643FE · Doug MD11F · Leading Edge DevicesSDR FDEA201110214605Access Panel · unknownACFT SUMP PANEL PHYSICAL CONFIG FOUND DIFFERENT FRM AMM 06-00-00 FIGURE. ACCOMPLISHED EA 1-5330-153383, . CLASSIFIED AS MAJOR ALTERATION IAW GMM 6-2-100, REV 113.Oct 21, 2011 · N643FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201110164537Attach Bracket · corrodedFORWARD CARGO BETWEEN STA 959 AND 979, X = -46, ROLLER FOUND CORRODED AFTER PIVOT BRACKET ATTACHMENT REMOVAL. CORROSION REMOVED IAW SRM 51-21-01 REV 47 AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-00 REV 47, FIGURE 205. ORIGINAL MATERIAL THICKNESS 0.109 INCH, Oct 16, 2011 · N643FE · Doug MD11F · Fuselage Main, Attach FittingsSDR FDEA201110164536Channel · corrodedFORWARD CARGO ROLLER TRAY CHANNEL AT BS 1059-6-0, X -25 FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-00 REV 47, FIGURE 205 REPAIR CARRIED OUT AS PER EA 1-2550-153365, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 113.Oct 16, 2011 · N643FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201110164535Channel · corrodedFORWARD CARGO ROLLER TRAY CHANNEL AT BS 979-1059, X -25 FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-00 REV 47, FIGURE 205. ORIGINAL MATERIAL THICKNESS 0.109 INCH, MATERIAL REMOVED 0.049 INCH, MATERIAL REMAINED 0.060 INCH. REPOct 16, 2011 · N643FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201110164534Channel · corrodedFORWARD CARGO ROLLER TRAY CHANNEL AT BS 806-899, X -25 FOUND CORRODED. CORROSION REMOVED, DEEPEST DEPTH 0.10 INCH, ORIGINAL MATERIAL THICKNESS 0.109 INCH, MATERIAL REMAINED 0.099 INCH, FOUND WITHIN LIMITS IAW SRM 53-00-00 REV 47 FIGURE 205. REPAIR CLASSIOct 16, 2011 · N643FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201110164533Channel · corrodedFWD CARGO BAY ROLLER TRAY CHANNEL AT BS 1130 -6-70, X = -25.0 FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-00 REV 47, FIGURE 205. ORIGINAL MATERIAL THICKNESS 0.109 INCH, MATERIAL REMOVED 0.040 INCH, MATERIAL REMAINED 0.069 INCH. Oct 16, 2011 · N643FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201110164532Channel · corrodedFORWARD CARGO, PARTIAL LOAD LATCH CHANNEL AT BS 780 TO 795, X = -25.0 CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMITS IAW SRM 51-21-01 REV 47 FIGURE 205. ORIGINAL MATERIAL THICKNESS 0.109 INCH, MATERIAL REMOVED 0.040 INCH. MATERIAL REMAINING 0.069Oct 16, 2011 · N643FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201110014260Fitting · corrodedLT WING NR3 SLAT MIDDLE ATTACHMENT FITTING FOUND CORRODED AFTER SLAT REMOVAL. REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 SRM 57-40-02 REV 47, FIGURE 201. ORIGINAL DIAMETER = 0.5015 INCH, REWORKED DIAMETER = 0.5785 INCH, MAXIMUM DIAMETER = 0.625 INCH. REPAOct 1, 2011 · N643FE · Doug MD11F · Leading Edge DevicesSDR FDEA201110014253Panel · corrodedCORROSION ON CENTER WING AUX TANK TOP PANEL SURFACE AT STA 1229 TO 1239, X = 8 TO X = 27.5. CORROSION REMOVED AS PER SRM 51-21-01 REV 47. ORIGINAL MATERIAL THICKNESS = 0.172 INCH; MATERIAL REMOVED = 0.052 INCH; MATERIAL REMAINED = 0.120 INCH - FOUND EXCEEDED Oct 1, 2011 · N643FE · Doug MD11F · Fuel StorageSDR FDEA201110014252Panel · corrodedCOROSION ON CTR WING AUX TANK TOP PANEL SURFACE AT STA 1229 TO STA 1239, X = 8 TO X = -8. CORROSION REMOVED AS PER SRM 51-21-01 REV 47. ORIGINAL MATERIAL THICKNESS = 0.172 INCH; MATERIAL REMOVED = 0.035 INCH; MATERIAL REMAINED = 0.137 INCH - FOUND EXCEEDED LIOct 1, 2011 · N643FE · Doug MD11F · Fuel StorageSDR FDEA201110014248Panel · corrodedCOROSION ON CENTER WING AUX TANK TOP PANEL SURFACE AT STA 1229 TO 1239, X = -75 TO X = -107. CORROSION REMOVED AS PER SRM 51-21-01 REV 47. ORIGINAL MATERIAL THICKNESS = 0.172 INCH; MATERIAL REMOVED = 0.027 INCH; MATERIAL REMAINED = 0.142 INCH - FOUND EXCEEDEDOct 1, 2011 · N643FE · Doug MD11F · Fuel StorageSDR FDEA201110014242Panel · corrodedCOROSION ON CENTER WING AUX TANK TOP PANEL SURFACE AT STA 1256 TO 1273, X = -98 TO X = -107. COROSION REMOVED AS PER SRM 51-21-01 REV 47. ORIGINAL MATERIAL THICKNESS = 0.285 INCH; MATERIAL REMOVED = 0.012 INCH; MATERIAL REMAINED = 0.273 INCH - FOUND EXCEEDEDOct 1, 2011 · N643FE · Doug MD11F · Fuel StorageSDR FDEA201110014241Panel · corrodedCABIN - COROSION ON CENTER WING AUX TANK TOP PANEL SURFACE AT STA 1219 TO 1239, X = 75 TO X =107. COROSSION REMOVED AS PER SRM 51-21-01 REV 47. ORIGINAL MATERIAL THICKNESS = 0.172 INCH; MATERIAL REMOVED = 0.132 INCH; MATERIAL REMAINED = 0.040 INCH - FOUND EXOct 1, 2011 · N643FE · Doug MD11F · Fuel StorageSDR FDEA201110014258Fuel Cell · corrodedCOROSION ON CENTER WING TANK TOP PANEL SURFACE AT STA 1210 , X = -8 TO X = - 27.5. CORROSION REMOVED AS PER SRM 51-21-01, REV 47. ORIGINAL MATERIAL THICKNESS = 0.170 INCH; MATERIAL REMOVED = 0.011 INCH; MATERIAL REMAINED = 0.159 INCH - FOUND WITHIN LIMIT AOct 1, 2011 · N643FE · Doug MD11F · Fuel StorageSDR FDEA201110014257Structure · corrodedCORROSION ON CTR WING TANK TOP PANEL SURFACE AT STA 1210 , X = -8 TO X = 8. CORROSION REMOVED AS PER SRM 51-21-01 REV 47. ORIGINAL MATERIAL THICKNESS = 0.172 INCH; MATERIAL REMOVED = 0.008 INCH; MATERIAL REMAINED = 0.112 INCH - FOUND EXCEEDED LIMIT AS PER MDOct 1, 2011 · N643FE · Doug MD11F · Fuel StorageSDR FDEA201110014246Skin · crackedRT WING FIXED L/E LOWER SURFACE AT REFUELLING ACCESS DOOR INBD SIDE FOUND CRACKED. CRACK TRIMMED OUT AS PER SRM 57-40-02 REV 47, FIGURE 201 REPAIR 7. REPAIR FILLER AND DOUBLER FABRICATED AND INSTALLED AS PER SRM 57-40-02 REV 47, FIGURE 201 REPAIR 7. REPAIOct 1, 2011 · N643FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201110014259Panel · corrodedCORROSION ON CTR WING TANK TOP PANEL SURFACE AT STA 1210 , X = -47.5TO X = -75. CORROSION REMOVED AS PER SRM 51-21-01 REV 47. ORIGINAL MATERIAL THICKNESS = 0.170 INCH; MATERIAL REMOVED = 0.011 INCH; MATERIAL REMAINED = 0.159 INCH - FOUND EXCEEDED LIMIT AS PEROct 1, 2011 · N643FE · Doug MD11F · Fuel StorageSDR FDEA201110014256Panel · corrodedCORROSION ON CTR WING TANK TOP PANEL SURFACE AT STA 1210 , X =47.5 TO X =75. CORROSION REMOVED AS PER SRM 51-21-01 REV 47. ORIGINAL MATERIAL THICKNESS = 0.170 INCH; MATERIAL REMOVED = 0.010 INCH; MATERIAL REMAINED = 0.160 INCH - FOUND EXCEEDED LIMIT AS PER SROct 1, 2011 · N643FE · Doug MD11F · Fuel StorageSDR FDEA201110014255Panel · corrodedCORROSION ON CTR WING AUX TANK TOP PANEL SURFACE AT STA 1229 TO 1239, X = 75 TO X = 107. CORROSION REMOVED AS PER SRM 51-21-01 REV 47. ORIGINAL MATERIAL THICKNESS = 0.172 INCH; MATERIAL REMOVED = 0.024 INCH; MATERIAL REMAINED = 0.148 INCH - FOUND EXCEEDED LIMOct 1, 2011 · N643FE · Doug MD11F · Fuel StorageSDR FDEA201110014254Panel · corrodedCOROSION ON CENTER WING AUX TANK TOP PANEL SURFACE AT STA 1229 TO 1239, X = 27.5 TO X = 47.5. CORROSION REMOVED AS PER SRM 51-21-01 REV 47. ORIGINAL MATERIAL THICKNESS = 0.172 INCH; MATERIAL REMOVED = 0.043 INCH; MATERIAL REMAINED = 0.129 INCH - FOUND EXCEEDEOct 1, 2011 · N643FE · Doug MD11F · Fuel StorageSDR FDEA201110014251Panel · corrodedCOROSION ON CTR WING AUX TANK TOP PANEL SURFACE AT STA 1229 TO 1239, X = -8 TO X = -27.5. CORROSION REMOVED AS PER SRM 51-21-01 REV 47. ORIGINAL MATERIAL THICKNESS = 0.172 INCH; MATERIAL REMOVED = 0.031 INCH; MATERIAL REMAINED = 0.141 INCH - FOUND EXCEEDED LIOct 1, 2011 · N643FE · Doug MD11F · Fuel StorageSDR FDEA201110014250Panel · corrodedCOROSION ON CTR WING AUX TANK TOP PANEL SURFACE AT STA 1229 TO 1239, X = -27.5 TO X = -47.5. CORROSION REMOVED AS PER SRM 51-21-01 REV 47. ORIGINAL MATERIAL THICKNESS = 0.172 INCH; MATERIAL REMOVED = 0.041 INCH; MATERIAL REMAINED = 0.131 INCH - FOUND EXCEEDEOct 1, 2011 · N643FE · Doug MD11F · Fuel StorageSDR FDEA201110014249Panel · corrodedCOROSION ON CTR WING AUX TANK TOP PANEL SURFACE AT STA 1229 TO 1239, X = -47.5 TO X = -75. COROSION REMOVED AS PER SRM 51-21-01 REV 47. ORIGINAL MATERIAL THICKNESS = 0.176 INCH; MATERIAL REMOVED = 0.015 INCH; MATERIAL REMAINED = 0.161 INCH - FOUND EXCEEDED LIOct 1, 2011 · N643FE · Doug MD11F · Fuel StorageSDR FDEA201110014247Panel · corrodedCOROSION ON CTR WING AUX TANK TOP PANEL SURFACE AT STA 1229 TO 1239, X =47.5 TO X =75. CORROSION REMOVED AS PER SRM 51-21-01 REV 47. ORIGINAL MATERIAL THICKNESS = 0.172 INCH; MATERIAL REMOVED = 0.027 INCH; MATERIAL REMAINED = 0.145 INCH - FOUND EXCEEDED LIMITOct 1, 2011 · N643FE · Doug MD11F · Fuel StorageSDR FDEA201110014245Panel · corrodedCOROSION ON CENTER WING AUX TANK TOP PANEL SURFACE AT STA 1209 TO 1219, X =107. COROSION REMOVED AS PER SRM 51-21-01 REV 47. ORIGINAL MATERIAL THICKNESS = 0.193 INCH; MATERIAL REMOVED = 0.031 INCH; MATERIAL REMAINED = 0.162 INCH - FOUND EXCEEDED LIMIT AS PER Oct 1, 2011 · N643FE · Doug MD11F · Fuel Storage
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