Boeing MD-11F

Service difficulty reports · 31,320

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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 aircraft_model_key = 'MD11F'
  ORDER BY difficulty_date DESC"

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SDR FDEA201211194093Hinge Bracket · corrodedRIGHT WING INBD FLAP, OTBD AFT HINGE BRACKET PIVOT OTBD LUG BORE OTBD SPOT FACE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 74. EXISTING THICKNESS: 0.263", MATERIAL REMOVED: 0.078", REMAINING THICKNESS: 0.185", MINIMUM THICKNESS: 0.Nov 19, 2012 · N579FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201211184070Landing Gear · unknownLANDING GEAR DID NOT CYCLE TO GREEN INDICATION. RECYCLED NORMAL GEAR EXTENSION: GREEN. GEAR HANDLE RESISTANCE STIFF, PERFORMED A GENERAL VISUAL INSPECTION OF ALL GEAR DOORS AND ALL LANDING GEAR, ALL FIND NORMAL IAW SMP CLEANED AND INSPECT LANDING GEAR CONTRNov 18, 2012 · N613FE · Doug MD11F · Landing Gear Position and WarningSDR FDEA201211174062Bracket · corrodedLEFT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET ACTUATOR ATTACH INBD LUG BORE FOUND CORRODED. FOUND EXCEEDED LIMITS AS PER CMM 57-44-09 REVISION 74. EXISTING HOLE DIAMETER = 1.224 INCH, FINAL HOLE DIAMETER = 1.228 INCH, MAXIMUM HOLE DIAMETER = 1.220 INCH. RNov 17, 2012 · N579FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201211174065Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FORWARD HINGE BRACKET ACTUATOR ATTACH OTBD LUG BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS AS PER CMM 57-44-08 REVISION 74. REPAIRED PER EA 1-5750-163540 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.Nov 17, 2012 · N579FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201211174064Hinge Bracket · corrodedLT WING OTBD FLAP, INBD FORWARD HINGE BRACKET ACTUATOR ATTACH INBD LUG BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08 REVISION 74. REPAIRED PER EA 1-5750-163540 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.Nov 17, 2012 · N579FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201211174063Bracket · corrodedLT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET ACTUATOR ATTACH OTBD LUG BORE FOUND CORROSION. FOUND EXCEEDED LIMIT AS PER MD-11 CMM 57-44-09 REVISION 74. EXISTING HOLE DIAMETER = 1.223 INCH, FINAL HOLE DIAMETER = 1.226 INCH, MAXIMUM HOLE DIAMETER = 1.220 INov 17, 2012 · N579FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201211174061Longeron · crackedX-RAY INSPECTION FOUND CRACKED INDICATION APPROX 2" IN LENGTH AT CABIN, STATION 5-123, LONGERON 3 LT AFT SECTION EDGE. REPAIRED AS PER SRM 53-00-05 FIGURE 202 REPAIR 1 REVISION 51. NEW LONGERON SEGMENT FABRICATED AS PER DRAWING AFA7771 REVISION C AND INSTNov 17, 2012 · N579FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR WRNA201200015Control Unit · malfunctionedWHILE IN FLIGHT, LEVEL 2 "GEN BUS 3 FAULT" ILLUMINATED. DEPLOYED ADG AND RETURNED TO FIELD (MIA) FOR SAFE LANDING. REPLACED EPCU IAW AMM 24-08-01, GROUND RUN ENGINES, NO DEFECTS NOTED. STOWED ADG IAW AMM 24-25-01. AIRCRAFT RETURNED TO SERVICE.Nov 16, 2012 · N953AR · Doug MD11F · AC Power Distribution SystemSDR WRNA201200014Engine · bird ingestionAFTER TAKEOFF FROM SUMU, HAD HIGH VIBRATION NR 3 ENGINE. DUMPED FUEL TO MAX LANDING WEIGHT AND RETURNED TO FIELD FOR A SAFE LANDING. AFTER LANDING ENGINE NR 3 WAS SHUT DOWN AS PRECAUTION. ON POST FLIGHT INSPECTION, FOUND 6 DAMAGED FAN BLADES WITH EVIDENCE ONov 16, 2012 · N952AR · Doug MD11F · Engine (Turbine/Turboprop)SDR FDEA201211164055Skin · misrepairedLT WING NR 2 SLAT INNER SKIN AT XIS 275 MISREPAIRED. REPAIRED PER SRM 57-40-01 FIGURE 201 REPAIR 1 REVISION 51 AND EA 1-5750-163553. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.Nov 16, 2012 · N579FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201211164052Skin · misrepairedLT WING INBD FLAP UPPER SURFACE CENTER BOX BETWEEN XIFH 281 AND XIFH 288 MISREPAIRED. REPAIRED IAW SRM 57-00-01 FIGURE 201 SHEET 2 REPAIR 1 REVISION 51 AND EA 1-5750-163534 STEP 2 PART 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.Nov 16, 2012 · N579FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201211164051Vane · delaminatedRT WING INBD FLAP VANE LOWER SURFACE FOUND DELAMINATED. REMOVED AND REPLACED AS PER AMM 27-50-22-4 REVISION 74.1. ADJUSTMENT AND TEST CARRIED OUT PER AMM 27-50-00-5 REVISION 74.1 FOUND SATISFACTORY. REPAIR CLASSIFIED MINOR PER GMM 6-2-100 REVISION 115.Nov 16, 2012 · N579FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201211164050Skin · misrepairedLT WING INBD FLAP LOWER SURFACE LOWER SKIN BETWEEN XIFH 269 AND XIFH 288 MISREPAIRED. REPAIRED IAW SRM 57-50-01 FIGURE 201 REPAIR 1 REVISION 51 AND EA 1-5750-163534 STEP 11 PART 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.Nov 16, 2012 · N579FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201211164049Skin · misrepairedLT WING INBD FLAP UPPER SURFACE LOWER SKIN BETWEEN XIFH 269 AND XIFH 293 MISREPAIRED. REPAIRED IAW SRM 57-00-01 FIGURE 201 REPAIR 2 REVISION 51 AND E.A. 1-5750-163534 STEP 7 PART 1.Nov 16, 2012 · N579FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201211164047Seat Track · corrodedBS 1890, X = -3 SEAT TRACK FOUND CORRODED. R & R IW SRM 51-31-01, REV 51. SEAT TRACK FABRICATED IAW DWG AGA7080 REVISION S. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.Nov 16, 2012 · N579FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201211164046Seat Track · corrodedLEFT BS 1890, X = 3 SEAT TRACK FOUND CORRODED.Nov 16, 2012 · N579FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201211154033Frame · misrepairedFRAME MISREPAIRED AT CABIN LT BS 535, 9G NET LOWER SUPPORT YOKE AT LONGERON 24 LT. CARRIED OUT REPAIR IAW SRM 53-20-07, FIG 201, REPAIR 1, REV 51. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 115.Nov 15, 2012 · N579FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201211154032Frame · misrepairedFRAME MISREPAIRED AT CABIN LT BS 535, 9G NET UPPER SUPPORT YOKE AT LONGERON 18 LT. REPAIRED IAW SRM 53-20-07, FIG 202, REPAIR 1, REV 51. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 115.Nov 15, 2012 · N579FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201211154031Skin · crackedRT WING NR 8 SLAT LOWER SURFACE FOUND CRACKED. REPAIRED IAW SRM 57-40-01, FIG 201 REPAIR 3, REV 51 AND EA 1-5750-163529. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.Nov 15, 2012 · N579FE · Doug MD11F · Leading Edge DevicesSDR FDEA201211154030Skin · misrepairedLT WING NR 3 SLAT ASSY UPPER SKIN XOS 429.446 MISREPAIRED. REPAIRED IAW EA 1-5750-163527. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 115.Nov 15, 2012 · N579FE · Doug MD11F · Leading Edge DevicesSDR FDEA201211154037Support Fitting · damagedLEFT WING NR 8 L/E SLAT INBD SUPPORT FITTING FWD HOLE OTBD SIDE SURFACE FOUND STEPPED. SUPPORT FITTING REMOVED AND REPLACED IAW SRM 51-31-01, REV 50. REPAIR CLASSIFIED AS MAJOR IAW GENERAL MM 6-2-100, REV 115.Nov 15, 2012 · N588FE · Doug MD11F · Leading Edge DevicesSDR FDEA201211154023Union · leakingAT 118 INTO FLIGHT AT FL 320 GOT LVL 1 "HYD 3 ELEV OFF" ALERT. FLUID LEVEL IN NR 3 WAS 4.3 GALS AND STARTED DECREASING AT A RATE OF .1 GAL EVERY 3 MINUTES. WHEN 3.5 WAS REACHED;, TURNED HYD SYSTEM TO MANUAL AND TURNED OFF HYD 3 LT AND RT PUMPS AND ALSO THENov 15, 2012 · N615FE · Doug MD11F · Hydraulic System, MainSDR FDEA201211144010Seat Track · corrodedBS 1351 'X' = 8.5 SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.Nov 14, 2012 · N579FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201211144012Seat Track · corrodedBS 1611 'X' = 8.5 SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52, FIGURE 201, REPAIR 1, REVISION 51. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 115.Nov 14, 2012 · N579FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201211144011Seat Track · corrodedBS 1805 'X' = -8.5 SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52, FIGURE 201, REPAIR 1, REVISION 51. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 115.Nov 14, 2012 · N579FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201211144009Seat Track · corrodedBS 1611 'X' = -8.5 SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52, FIGURE 201, REPAIR 1, REVISION 51. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 115.Nov 14, 2012 · N579FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201211144006Support Fitting · chafedLEFT WING NR 8 L/E SLAT, INBD SUPPORT FITTING, AFT HOLE, BOTH SIDES SURFACES FOUND CHAFED. FOUND DURING LT OTBD SLAT DRIVE CABLES TENSION CHECK. SUPPORT FITTING REMOVED IAW STRUCTURAL REPAIR MANUAL 51-31-01 REV 50. HOLES PICKED UP ON NEW SUPPORT FITTING IAW SNov 14, 2012 · N588FE · Doug MD11F · Leading Edge DevicesSDR FDEA201211103935Idg · inoperativeRAN NR 3 ENG FOR IDG DISCONNECT IDG CAME APART DURING RUN. ENGINE NR 3 FIRE INDICATION IN FLIGHTDECK AND 1EA FIRE BOTTLE DISCHARGED, AFTER FURTHER INSPECTION IDG FOUND CRACKED AND INSPECTION ON WIRING AND GEARBOX INWORK. R & R IDG, AIR/OIL HEAT EXCHANGER FLUNov 10, 2012 · N615FE · Doug MD11F · AC Generator-AlternatorSDR FDEA201211093918Skin · crackedLEFT WING INBD FLAP UPPER SKIN PANEL ASSY CRACKED AT XIFH 171.3. REPAIRED IAW SRM 57-00-01 REPAIR 1 FIGURE 201 REVISION 50 AND EA 1-5750-163526Nov 9, 2012 · N588FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201211093915Seat Track · corrodedMAIN DECK SEAT TRACK CLIP NUT HOLE AT BS 5-55, "X" = -107.25 FOUND CORRODED. REPAIRED IAW SRM 53-00-52, FIG 201, REPAIR 5, REV 50. REPAIR PARTS FABRICATED IAW SRM 53-00-52, FIG 201, REPAIR 5, REV 50. REPAIR PARTS INSTALLED IAW SRM 53-00-52, FIG 201, REPAIR Nov 9, 2012 · N588FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201211083909Splice · crackedCENTER LANDING GEAR WHEEL WELL RT UPPER FORWARD SPLICE JOINT FOUND CRACKED. SPLICE REMOVED AND REPLACED WITH WITH NEW SPLICE IAW SRM 51-33-01 REVISION 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.Nov 8, 2012 · N588FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201211083908Slat Track · crackedRT WING L/E NR 10 SLAT TRACK CUT OUT INBD CORNER FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02 FIGURE 201, REPAIR 7, REVISION 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.Nov 8, 2012 · N588FE · Doug MD11F · Leading Edge DevicesSDR FDEA201211083907Doubler · crackedLEFT WING L/E COMPARTMENT BEADED DOUBLER AT XOS 666 FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02 FIGURE 203, REPAIR 15, TYPE A, REVISION 50. REPAIR CLASSIFIED AS MAJOR GMM REVISION 115.Nov 8, 2012 · N588FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201211073896Seat Track · corrodedMAIN DECK SEAT TRACK BS 1372, "X" = -8.5 FOUND CORRODED. SEAT TRACK REMOVED IAW SRM 53-00-52, FIG 201. REPAIR 1, REV 50. NEW SEAT TRACK SEGMENT REWORKED IAW SRM 53-00-52, FIG 201, REPAIR 1 REV 50. NEW SEAT TRACK SEGMENT INSTALLED IAW SRM 53-00-52, FIG 201, RENov 7, 2012 · N588FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201211073895Seat Track · corrodedMAIN DECK SEAT TRACK BS 1861, "X" = -27.5 FOUND CORRODED. REPAIRED IAW SRM 53-00-52, FIG 201 REPAIR 5, REV 50. REPAIR PARTS FABRICATED IAW SRM 53-00-52, FIG 201, REPAIR 5, REV 50. REPAIR PARTS INSTALLED IAW SRM 53-00-52, FIG 201, REPAIR 5, REV 50. REPAIR CLANov 7, 2012 · N588FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201211073892Frame · dentedDENT FOUND FRAME AT BS 1741, L11R. REPAIRED IAW SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.Nov 7, 2012 · N588FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201211073891Frame · dentedDENT FOUND AT RT SIDE FRAME AT BS 1761, NEAR L11R. REPAIRED IAW SRM 53-00-07 FIGURE 201, REPAIR 2, REVISION 50. REPAIR CLASSIFIED AS MAJOR GMM 6-2-100 REVISION 115.Nov 7, 2012 · N588FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201211073890Frame · dentedDENT FOUND ON RT SIDE OF CABIN FUSELAGE FRAME AT BS 1641, NEAR L11R. REPAIR CARRIED OUT IAW SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.Nov 7, 2012 · N588FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201211063867Door Frame · crackedUPPER CENTER CARGO DOOR FRAME, BS 1743 BETWEEN LONGERON 28 - 29R, "X" = 106 FOUND CRACKED. APPROX 1.25" IN LENGTH. REPAIRED IAW EA 1-5310-163524. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.Nov 6, 2012 · N588FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201211063863Spar Cap · crackedRT WING T/E REAR SPAR LOWER CAP XORS 433 FOUND CRACKED. REMOVED AND REPLACED WITH NEW SILL AS PER SRM 51-34-01 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.Nov 6, 2012 · N588FE · Doug MD11F · Wing SparSDR FDEA201211063865Vane · delaminatedRT WING INBD FLAP VANE LOWER SURFACE FOUND DELAMINATED. REMOVED AND REPLACED AS PER AMM 27-50-22-4 REVISION 74. FLAP VANE ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-22-5 REVISION 74. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 115.Nov 6, 2012 · N588FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201211063878Longeron Splice · crackedCENTER CARGO BAY BS 5-123, L44L LONGERON SPLICE FOUND CRACKED. LONGERON SPLICE REMOVED IAW SRM 51-31-01 REVISION 50 AND INSTALLED WITH NEW FABRICATED LONGERON SPLICE IAW SRM 51-33-01 REVISION 50. LONGERON SPLICE FABRICATED IAW DRAWING A5A7116 REVISION D. RENov 6, 2012 · N588FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201211063877Longeron Splice · crackedCENTER CARGO BAY BS 5-123 L45R LONGERON SPLICE FOUND CRACKED. LONGERON SPLICE REMOVED IAW SRM 51-31-01 REVISION 50 AND INSTALLED WITH NEW FABRICATED LONGERON SPLICE IAW SRM 51-33-01 REVISION 50. LONGERON SPLICE FABRICATED IAW DRAWING A5A7116 REVISION D. RENov 6, 2012 · N588FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201211063876Skin · crackedDURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN XORS 683.4 AND XORS 713.6. FOUND CRACK INDICATIONS AT FASTENER HOLES. REPAIRED IAW SRM 57-20-02 REPAIR 5 FIGURE 201 REVISION 50. REPAIR CLASSIFIED AS MANov 6, 2012 · N588FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201211063874Skin · crackedDURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN XORS 683.4 AND 713.6. FOUND CRACKED INDICATION AT FASTENER HOLES. FASTENER HOLES CRACKED AT RIGHT WING LOWER SKIN ACCESS DOOR COUTOUT REPAIRED IAW SRM 5Nov 6, 2012 · N588FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201211063872Longeron Splice · crackedCENTER CARGO BAY BS 5-123, L46L LONGERON SPLICE FOUND CRACKED. LONGERON SPLICE REMOVED IAW SRM 51-31-01 REVISION 50 AND INSTALLED WITH NEW FABRICATED LONGERON SPLICE IAW SRM 51-33-01 REVISION 50. LONGERON SPLICE FABRICATED IAW DRAWING A5A7114 REVISION J. REPANov 6, 2012 · N588FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201211063871Longeron Splice · crackedCENTER CARGO BAY BS 5-123, L41L LONGERON SPLICE FOUND CRACKED. LONGERON SPLICE REMOVED IAW SRM 51-31-01 REVISION 50 AND INSTALLED WITH NEW FABRICATED LONGERON SPLICE IAW SRM 51-33-01 REVISION 50. LONGERON SPLICE FABRICATED IAW DRAWING A5A7115 REVISION D. RNov 6, 2012 · N588FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201211063870Longeron Splice · crackedCENTER CARGO BS BS 5-123, LONGERON 40L LONGEORN SPLICE FOUND CRACKED. LONGERON SPLICE REMOVED IAW SRM 51-31-01 REVISION 50 AND INSTALLED WITH NEW FABRICATED LONGERON SPLICE IAW SRM 51-33-01 REVISION 50. LONGERON SPLICE FABRICATED IAW DRAWING A5A7114 REVISIONNov 6, 2012 · N588FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201211063869Longeron Fitting · crackedCENTER CARGO COMPARTMENT BS 5-123, LONGERON 44 RT SPLICE FITTING FOUND CRACKED. LONGERON SPLICE REMOVED IAW SRM 51-31-01 REVISION 50 AND INSTALLED WITH NEW FABRICATED LONGERON SPLICE IAW SRM 51-33-01 REVISION 50. LONGERON SPLICE FABRICATED IAW DRAWING A5A7114Nov 6, 2012 · N588FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201211063868Longeron Splice · crackedCENTER CARGO COMPARTMENT BS 5-123, LONGERON 37 RT SPLICE FITTING FOUND CRACKED. LONGERON SPLICE REMOVED AS PER SRM 51-31-01 REVISION 50 AND INSTALLED WITH NEW FABRICATED SPLICE AS PER SRM 51-33-01 REVISION 50. SPLICE FABRICATED IAW DRAWING A5A7114 REVISION J.Nov 6, 2012 · N588FE · Doug MD11F · Fuselage Main, Longeron/Stringer
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