N610FE

Service difficulty reports · 497

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 = 'N610FE' 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 FDEA201003190929Skin · crackedCRACK - LT WING L/E DROOP UPPER SURFACE. LT DROOP LEADING EDGE REPLACED AS PER AMM 27-80-10-4 REV 64.Mar 19, 2010 · N610FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201003180866Seat Track · corrodedMAIN DECK CARGO - STA 5-33 TO STA 5-53 'X' = 75, SEAT TRACK OUTBOARD FLANGE FOUND WITH SURFACE CORROSION. MAIN DECK CARGO, STA 5-33 TO STA 5-53 'X' = 75, CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 5-0 TO STA 5-63 AS PER SRM 53-0Mar 18, 2010 · N610FE · Doug MD11F · Fuselage Floor PanelSDR FDEA201003180870Seat Track · corrodedMAIN DECK CARGO - STA 675 TO STA 735 'X' = -75, SEAT TRACK OTBD FLANGE FOUND WITH MULTIPLE SURFACE CORROSION. MAIN DECK CARGO, STA 675 TO STA 735 'X' = -75, SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-00-52 FIGURE 201 REPAIR 1, REVMar 18, 2010 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201003180869Skin · crackedHFEC OPEN HOLE INSP AT RT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STA XORS 690 AND XORS 700 FOUND CRACK INDICATION ON 09 EACH FASTENER HOLE. REPAIRED AS PER EA 1-5710-132384. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 109.Mar 18, 2010 · N610FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201003180868Skin · crackedHFEC OPEN HOLE INSP AT LT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STA XORS 690 AND XORS 700. FOUND CRACK INDICATION ON 02 EACH FASTENER HOLE. REPAIRED AS PER EA 1-5710-132383Mar 18, 2010 · N610FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201003180865Seat Track · corrodedMAIN DECK CARGO - STA 1481 TO STA 1501 'X' = 75, SEAT TRACK OTBD FLANGE FOUND WITH SURFACE CORROSION. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1471 TO STA 1531 IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 43. REPAIR CLASSIFIED AMar 18, 2010 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201003180864Seat Track · corrodedMAIN DECK CARGO - STA 1521 'X' =8, SEAT TRACK INBD AND OTBD FLANGE FOUND WITH SURFACE CORROSION. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1511 TO STA 1531 IAW SRM 53-00-52, FIGURE 201, REPAIR 1, REVISION 43. REPAIR CLASSIMar 18, 2010 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201003180863Seat Track · corrodedMAIN DECK CARGO - STA 1491 'X' = -8, SEAT TRACK OTBD FLANGE FOUND WITH SURFACE CORROSION. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1471 TO STA 1521 IAW SRM 53-00-52 FIGURE 201 REPAIR 1, REV 43. REPAIR CLASSIFIED AS MAJOR IAW GMar 18, 2010 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201003170846Seat Track · corrodedCABIN - STA 495, 'X' = -27.5 SEAT TRACK INBD FLANGE FOUND SURFACE CORROSION. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 458 TO STA 525 IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 43. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV Mar 17, 2010 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201003150823Skin · crackedRT WING L/E AT NR 5 SLAT TRACK CTR TRACK CUT OUT LOWER OTBD CORNER FOUND CRACKED. RT WING L/E NR 5 SLAT CTR TRACK LOWER OTBD CORNER TRIMMED OFF AND REPAIR CARRIED OUT IAW SRM 57-40-02 FIG 201 REV 43. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REVISION 109.Mar 15, 2010 · N610FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201003130806Skin Panel · unknownEXISTING REPAIR AT CENTER CARGO DOOR AFT JAMB. REPAIR AS PER SRM 53-00-15 FIG 202 REPAIR 8 REV 43 (MAJOR REPAIR).Mar 13, 2010 · N610FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201003130805Skin Panel · unknownEXISTING REPAIR AT CENTER CARGO DOOR FORWARD JAMB. REPAIR AS PER SRM 53-00-15 FIG 202 REPAIR 8 REV 43 (MAJOR REPAIR).Mar 13, 2010 · N610FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201003130804Skin · unknownEXISTING REPAIR AT FORWARD CARGO DOOR FORWARD JAMB. REPAIR AS PER SRM 53-00-15 FIG 202 REPAIR 8 REV 43 (MAJOR REPAIR).Mar 13, 2010 · N610FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201003130803Skin · chafedEXISTING REPAIR AT FORWARD CARGO AFT DOOR JAMB. REPAIR AS PER SRM 53-00-15 FIG 202 REPAIR 8 REV 43 (MAJOR REPAIR).Mar 13, 2010 · N610FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201003130801Skin · unknownEXISTING REPAIR AT LEFT WING INBOARD FLAP UPPER SURFACE STA XIFH 216. REPAIR AS PER SRM 57-00-01 FIG 201 REPAIR 1 REV 43 (MAJOR REPAIR).Mar 13, 2010 · N610FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201003130800Panel · damagedEXISTING REPAIR AT RIGHT WING DROOP LEADING EDGE LOWER SURFACE INBOARD EDGE. REPAIR AS PER EA 1-5740-132379 TITLE: "WINGS - RT DROOP LEADING EDGE SKIN, REPAIR" (MAJOR REPAIR).Mar 13, 2010 · N610FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201003130799Panel · damagedEXISTING REPAIR AT LEFT WING DROOP LEADING EDGE LOWER SURFACE INBOARD EDGE. LT DROOP LEADING EDGE REPLACED AS PER AMM 27-80-10-4 REV 64.Mar 13, 2010 · N610FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201003130802Skin · unknownEXISTING REPAIR AT LT WING INBD FLAP UPPER SURFACE STA XIFH 200. REPAIR AS PER SRM 57-00-01 FIG 201 REPAIR 1 REV43 (MAJOR REPAIR).Mar 13, 2010 · N610FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201003120793Rib · crackedLT WING - NR 16 L/E SLAT TRACK SUPPORT RIB FOUND CRACKED. R & R IAW SRM 51-33-01 REVISION 43. LT WING NR 7 AND NR 8 SLAT ADJUSTMENT AND TEST CARRIED OUT IAW AMM 27-80-30 REV 64 FOUND SATISFACTORY. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 109.Mar 12, 2010 · N610FE · Doug MD11F · Leading Edge DevicesSDR FDEA201003120792Fitting · crackedCRACK INDICATION FOUND DURING HFEC INSP ON THE LOWER VERTICAL STABILIZER NR 4 BANJO FITTING RT SIDE FWD. REPAIR AS PER SRM 55-30-02 FIG 201 DETAIL3 REV 43 AND EA1-5530-132364. (MAJOR REPAIR).Mar 12, 2010 · N610FE · Doug MD11F · Vertical Stabilizer, Attach FittingsSDR FDEA201002250529Strut · corrodedDURING SERVICE CHECK AT HANGAR, FOUND LT MLG OUTER SLEEVE GLAND THREADS ARE CORRODED ON INSIDE OF CYLINDER. SEVERE CORROSION OF ALL THREADS FOR 360 DEGREES. EXTREME EROSION OF THREADS OF UP TO 40 PERCENT FROM 4:00 TO 7:00 POSITION. REMOVED AND REPLACED LT MFeb 25, 2010 · N610FE · Doug MD11F · Main Landing Gear Strut/Axle/TruckSDR FDEA201002250523Strut · contaminatedWATER FOUND IN UPPER LT MLG STRUT "B" CHAMBER EXT WATER FOUND IN UPPER LT MLG STRUT "B" CHAMBER EXTENSION TUBE AREA. DURING SIGHT ROD ASSY. R & R. (REF NR0002) INVESTIGATE AS REQ. REPLACED NEW GEAR INSTALLED REF. W/C 32T1902Feb 25, 2010 · N610FE · Doug MD11F · Main Landing Gear Strut/Axle/TruckSDR FDEA201002250522Panel · damagedDURING POST FLIGHT WALK AROUND, FOUND PANEL ON RT LOWER HORIZONTAL STAB, FWD OF RT INBD ELEVATOR, NOT SEATED. INBD AND OUTBD ROLLERS ARE OUT OF INBD ELEVATOR TRACKS. INBD ROLLER BRACKET BENT. FWD OF INBD AND OUTBD ROLLER BRACKETS HAVE CRACKS. ACCOMPLISHEFeb 25, 2010 · N610FE · Doug MD11F · Elevator, Plate/SkinSDR FDEA200907162646Oil System · leakingNR 1 ENG OIL QTY TO ZERO IN FLIGHT QTY WAS 21 QTS AT START WENT TO 0 IN FLIGHT. ENG SHUTDOWN IN FLIGHT. COMPLIED WITH QRH.AT SHUTDOWN NR1 OIL PRESSURE 25PSI NR 1 OIL TEMP 150 DEGREES 31 OIL QTY 0. THIS ENGINE IS APPROVED FOR REMOVAL IAW ENGR. NR 1 ENGINE Jul 16, 2009 · N610FE · Doug MD11F · Turbine Engine Oil SystemSDR 08FDEA03570Skin · corrodedEMPENNAGE: UPON AFT FUSELAGE BODY FAIRING REMOVED, FOUND RIGHT HAND FUSELAGE SKIN FAIRING MATING SURFACE WITH MINOR SURFACE CORROSION. RIGHT FUSELAGE SKIN FAIRING MATING SURFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II AND FOUND OUT OF LIMIT AS PER SRM 5Aug 25, 2008 · N610FE · Doug MD11F · Fuselage Main, Plate/SkinSDR 08FDEA03569Skin · dentedAFT LOWER FUSELAGE EXTERNAL SKIN FOUND A DENT WITH DIMENSIONS: D=1"/ Y=0.064" AND SCRATCH 8" IN LENGTH AT FUSELAGE STA 1940. AFT LWR FUSELAGE EXTERNAL SKIN DENT CLASS II REPAIR CARRIED OUT AS PER SRM 53-20-00 VOLUME I FIGURE 2. REQUIRED INITIAL INSPECTION Aug 25, 2008 · N610FE · Doug MD11F · Fuselage Main, Plate/SkinSDR 08FDEA03539Skin · dentedRIGHT WING - INBOARD FLAP LOWER SURFACE FOUND DENT AT XIFH 255. RIGHT WING - INBOARD FLAP LOWER SURFACE DENT AT XIFH 255 DAMAGED CARRIED OUT REPAIR AS PER SRM 57-10-00 FIGURE 2 VOLUME I. THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Aug 22, 2008 · N610FE · Doug MD11F · Trailing Edge FlapsSDR 08FDEA03512Skin · cracked11 FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS= 690 AND STA XORS= 700. 11 EACH FASTENER HOLES CRACK AT RT WING LOWER SKIN ACCESS. REPAIR CARRIED OUT AS PER EA 1-5710-122425A, Aug 20, 2008 · N610FE · Doug MD11 · Wing, Plate/SkinSDR 08FDEA03511Skin · cracked15 EA FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT LH WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS= 690 AND STA XORS= 700. 15 EACH FASTENER HOLES ON LEFT HAND WING LOWER SKIN ACCESS BETWEEN XORS = 690 TO XORS = 700 REPAIAug 20, 2008 · N610FE · Doug MD11 · Wing, Plate/SkinSDR 08FDEA03519Skin · corrodedUPPER CARGO COMPARTMENT - CENTER WING TANK UPPER SKIN CORRODED AT STA 1232 LBL 17 UPPER CARGO COMPARTMENT. CENTER WING TANK UPPER SKIN AT STA 1232 LBL 17 CORRODED AREA REPAIRED AS PER FEDEX EA 1-5710-124344 TITLE: WINGS - BASIC WING STRUCTURE - CORROSION AT CAug 20, 2008 · N610FE · Doug MD11F · Wing, Center BoxSDR 08FDEA03517Skin · crackedLEFT WING - NR 6 LEADING EDGE SLAT OUTBOARD TRACK CUTOUT CORNER FOUND SUSPECTED CRACK. LEFT WING NR 6 LEADING EDGE SLAT OUTBOARD TRACK CUTOUT OUTBOARD CRACKED CORNER TRIMMED OFF AND REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIEDAug 20, 2008 · N610FE · Doug MD11 · Leading Edge DevicesSDR 08FDEA03516Skin · dentedLEFT WING - INBOARD FLAP LOWER SURFACE FOUND DENTS AT XIFH 249. LEFT WING INBAORD FLAP LOWER SURFACE DENT AREAS TRIMMED OFF AND REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 2 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Aug 20, 2008 · N610FE · Doug MD11F · Trailing Edge FlapsSDR 08FDEA03514Skin · dentedLEFT WING - INBOARD FLAP LOWER SURFACE FOUND DENT AT XIFH 130. LEFT WING INBOARD FLAP LOWER SURFACE DENT AREA TRIMMED OFF AND REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 3 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Aug 20, 2008 · N610FE · Doug MD11F · Trailing Edge FlapsSDR 08FDEA03518Longeron Splice · crackedTWO CRACKS FOUND DURING X-RAY INSPECTION AT STA 6-100, LONGERON 2R SPLICE. CRACK LENGTH APPROXIMATELY 1 INCH, AT STA 6-100, LONGERON 2R CRACKED STRINGER SPLICE REMOVED AND REPLACED AS PER SRM 51-21-01 VOLUME II. NEW SPLICE FABRICATED AS PER DWG A6A7112. RAug 20, 2008 · N610FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 08FDEA03492Structure · crackedLT MAIN LANDING GEAR DOOR SUSPECTED CRACKED AT I/B MOUNTING AREA (BELOW AFT BOLT). COMPLIED WITH EA 1-5280-124351, DOORS, MAIN LANDING GEAR DOOR, LT MLG DOOR CRACK REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Aug 18, 2008 · N610FE · Doug MD11F · Landing Gear DoorsSDR 08FDEA03496Skin · corrodedMAIN DECK CARGO COMPARTMENT, CENTER WING TANK UPPER SKIN CORRODED AT STA 1232, LBL 47. MAIN DECK CARGO COMPARTMENT CENTER WING TANK UPPER SKIN CORROSION AT STA 1232 LBL 47 REPAIRED AS PER FEDEX EA 1-5710-124343, TITLE: WINGS - BASIC WING STRUCTURE - CORROSIONAug 18, 2008 · N610FE · Doug MD11F · Wing, Center BoxSDR 08FDEA03495Beam · damagedL3 DOOR FWD BEAM NR 7 STOP BROKEN. L3 DOOR BROKEN BEAM REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Aug 18, 2008 · N610FE · Doug MD11F · Passenger/Crew DoorsSDR 08FDEA03494Seat Track · corrodedMAIN DECK SEAT TRACK CORRODED AT STA 655, RBL 8. MAIN DECK CORRODED SEAT TRACK AT STA 655 RBL 8 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 645 TO STA 765 RBL 8 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Aug 18, 2008 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA03493Stanchion · corrodedFWD CARGO: AFT BULKHEAD APPROXIMATE STA 6-73.5, LBL 8, STANCHION CORRODED. FORWARD CARGO AFT BULKHEAD APPROXIMATELY STA 6-73.5, LBL 8 STANCHION CORRODED AREA. CARRIED OUT REPAIRED AS PER SRM 53-00-01 FIGURE 8 VOLUME I. THIS REPAIR CLASSIFIED AS MAJOR PER GAug 18, 2008 · N610FE · Doug MD11F · Fuselage Main, StructureSDR 08FDEA03462Fitting · crackedDURING OPEN HOLE HFEC INSPECTION ON 0.460" DIAMETER HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 6 FOUND WITH CRACK INDICATIONS AT HOLES A AND B. MAIN CARGO DOOR LOWER JAMB CRACKED SUPPORT FITTING NR 6. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUMEAug 17, 2008 · N610FE · Doug MD11F · Fuselage Main, Attach FittingsSDR 08FDEA03459Fitting · crackedDURING OPEN HOLE HFEC INSPECTION ON 0.460" DIAMETER HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 2 FOUND WITH CRACK INDICATIONS AT HOLES C AND D. MAIN CARGO DOOR LOWER JAMB CRACKED SUPPORT FITTING NR 2 REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME IAug 17, 2008 · N610FE · Doug MD11F · Fuselage Main, StructureSDR 08FDEA03458Support Fitting · crackedDURING OPEN HOLE HFEC INSPECTION ON 0.460" DIAMETER HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NO. 1 FOUND WITH CRACK INDICATIONS AT HOLES A, B, C AND D. MAIN CARGO DOOR LOWER JAMB CRACK SUPPORT FITTING #1 REMOVED AND REPLACED AS PER SRM 51-31-0Aug 17, 2008 · N610FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA03463Support Fitting · crackedDURING OPEN HOLE HFEC INSPECTION ON 0.460" DIAMETER HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 FOUND WITH CRACK INDICATIONS AT HOLES C AND D. MAIN CARGO DOOR LOWER JAMB CRACKED SUPPORT FITTING NR 7 REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II. Aug 17, 2008 · N610FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA03461Support Fitting · crackedDURING OPEN HOLE HFEC INSPECTION ON 0.460" DIAMETER HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 4 FOUND WITH CRACK INDICATIONS AT HOLES A, AND C. MAIN CARGO DOOR LOWER JAMB CRACKED SUPPORT FITTING NR 4 REMOVED AND REPLACED AS PER SRM 51-31-01 VOL IIAug 17, 2008 · N610FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA03460Support Fitting · crackedDURING OPEN HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 3 FOUND WITH CRACK INDICATIONS AT HOLE A. MAIN CARGO DOOR LOWER JAMB CRACKED SUPPORT FITTING NR 3 REPAIRED AS PER SRM 53-50-00 FIG 10 VOL I . REPAIR Aug 17, 2008 · N610FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 07FDEA01385Seat Track · corrodedUPPER MAIN CARGO COMPARTMENT FOUND SEAT TRACK WITH CORROSION AT STA 1179 X= 8. [SUP 4-20-07] REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG.1 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Apr 10, 2007 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA01384Seat Track · corrodedCORROSION FOUND ON SEAT TRACK AT STA 1853 - 1887, X= 8.5, DISCOVERED AFTER REMOVAL OF FLOOR PANEL FOR ACCESS. [SUP 4-20-07] REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG.1 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Apr 10, 2007 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA01383Seat Track · corrodedCORROSION FOUND ON SEAT TRACK AT STA 1871 X = -8.5, DISCOVERED AFTER REMOVAL OF FLOOR PANEL FOR ACCESS. [SUP 4-20-07] REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG.1 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Apr 10, 2007 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA01378Seat Track · corrodedUPPER MAIN CARGO COMPARTMENT FOUND SEAT TRACK CORROSION ON STA 1179 TO 1199, X= -8.5. [SUP 4-20-07] REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG. 1 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Apr 8, 2007 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA01377Tank · corrodedUPPER AUX TANK FOUND WITH CORROSION BETWEEN STA 1219 TO 1235 X= -40, FOUND AFTER REMOVAL OF FLOOR PANEL TO FACILITATE NDT INSPECTION. [SUP 4-20-07] COMPLIED WITH FEDEX E.A. 1-5720-109847. CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100.Apr 8, 2007 · N610FE · Doug MD11F · Fuel Storage
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