Boeing MD-11F

Service difficulty reports · 31,317

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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 IPXA2020101061140Bracket · crackedINSPECTION TYPE: 2C RT MLG WHEEL WELL SYSTEM NR 1 HYD ACCUMULATOR LOWER SUPPORT BRACKET CRACKED AT BOTH ENDS. REMOVED CRACKED BRACKET, FABRICATED, AND INSTALLED IN RT MLG WHEEL WELL BELOW SYSTEM NR 1 ACCUMULATOR, IAW SRM 51-31-01 (MINOR).Aug 25, 2020 · N253UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2020101061138Angle · crackedINSPECTION TYPE: 2C RT MLG WW CUTOUT AT FWD END HAS A CRACKED ANGLE. REMOVED CRACKED ANGLE, FABRICATED, AND INSTALLED IN RT MLG WW FWD END CUT OUT, IAW SRM 51-35-01. MINORAug 25, 2020 · N253UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2020092060410Floorbeam · crackedINSPECTION TYPE: 2C LOWER FWD CARGO FLOOR BEAM IS CRACKED AT STA 6-70 AND X=57.50. REPAIRED CRACKED FLOOR BEAM AT STA 6-70 AND X=57.50, IAW VT-SAA EA 011-5340-01-A8529 REV. I/R AND UPS EO MD11-5340-77877-A (MAJOR).Aug 25, 2020 · N290UP · Doug MD11F · Fuselage Main, Floor BeamSDR IPXA2020091436161Beam · crackedINSPECTION TYPE: 2C LOWER FWD CARGO HORIZ BEAM IS CRACKED AT STA 6-73 ABOVE L43R. REMOVED, FABRICATED, AND REPLACED BEAM, IAW DWG ADA 7667 AND SRM 51-33-01 (MINOR).Aug 25, 2020 · N290UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2020091436159Intercostal · crackedINSPECTION TYPE: 2C LOWER FWD CARGO INTERCOSTAL IS CRACKED AT STA 6-50 AT L43R. REMOVED, FABRICATED, AND REPLACED INTERCOSTAL, IAW DWG ACA7049 AND SRM 51-35-01 (MINOR).Aug 25, 2020 · N290UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2020091416121Skin · corrodedINSPECTION TYPE: 2C EXTERIOR FUSELAGE SKIN HAS CORROSION BETWEEN STA 2154-2163.8 AND L12R TO 13R. REPAIRED CORRODED EXTERIOR FUSELAGE SKIN BETWEEN STA 2154-2163.8 AND L12R TO 13R, IAW SRM 53-70-01 REPAIR 3 FIG. 201 (MAJOR).Aug 25, 2020 · N290UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2020091416119Skin · corrodedINSPECTION TYPE:2C EXTERIOR FUSELAGE SKIN HAS CORRROSION BETWEEN STA 2148-2155 AND L33R TO 35R. REPAIRED CORRODED EXTERIOR FUSELAGE SKIN BETWEEN STA 2148-2155 AND L33R TO 35R, IAW SRM 53-70-01 REPAIR 3 FIG. 201 (MAJOR).Aug 25, 2020 · N290UP · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA202008252013Beam · crackedCABIN, MAIN DECK CARGO COMPARTMENT LEFT 3 DOOR NUMBER 1 (UPPER) BEAM AFT DOOR STOP NUMBER 1 FOUND CRACKED AT STATION 838.330, Z=51.367. CABIN, MAIN DECK CARGO COMPARTMENT LEFT 3 DOOR NUMBER 1 (UPPER) BEAM AFT DOOR STOP NUMBER 1 STATION 838.330, Z=51.367. REMAug 25, 2020 · N585FE · Doug MD11F · Fuselage Main, StructureSDR FDEA2020082652017Bracket · corrodedRT WING, WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT RT WING, WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (NR 4 HOLE). REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-Aug 25, 2020 · N625FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2020082652016Bracket · corrodedRT WING, WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT RT WING, WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (NR 4 HOLE). REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. Aug 25, 2020 · N625FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2020082652015Bracket · corrodedLT WING, WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LT WING, WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (NR 4 HOLE). REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-Aug 25, 2020 · N625FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2020082652014Bracket · corrodedLT WING, WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LT WING, WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (NR 4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. RAug 25, 2020 · N625FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2020082652012Beam · crackedCABIN, MAIN DECK CARGO COMPARTMENT RIGHT 3 DOOR NR 1 (UPPER) BEAM AFT DOOR STOP NR1 FOUND CRACKED AT STATION 838.330 , Z= - 51.367. CABIN, MAIN DECK CARGO COMPARTMENT RIGHT 3 DOOR NR 1 (UPPER) BEAM AFT DOOR STOP NR 1 STATION 838.330, Z= -51.367. REMOVED AND Aug 25, 2020 · N585FE · Doug MD11F · Fuselage Main, StructureSDR IPXA2020092060409Longeron · corrodedINSPECTION TYPE:2CLONGERON 50 L/H IS CORRODED BETWEEN STA. 6-70 TO 6-80.REPAIRED CORRODED LONGERON 50 L/H BETWEEN STA. 6-40 TO 6-80 IAW VT-SAA EA 011-5340-01-A8525 REV. I/R AND UPS EO MD11-5340-77874-A. (MAJOR)Aug 24, 2020 · N290UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2020091760342Seat Track · corrodedINSPECTION TYPE: 2C MAIN CABIN SEAT TRACK IS CORRODED BETWEEN STA 459.227 TO 485.227 AND X=50 TO X=63. REPAIRED CORRODED MAIN CABIN SEAT TRACK BETWEEN STA 459.227 TO 485.227 AND X=50 TO X=63, IAW VT-SAA EA 011-5310-01-A8521 REV I/R AND UPS EO MD11-5310-77862-Aug 24, 2020 · N290UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2020091460184Floor Panel · corrodedINSPECTION TYPE: 2C MAIN CABIN FLOOR PANEL IS CORRODED BETWEEN STA X= -8.5 TO -27.5 AND Y=392-440. REMOVED, FABRICATED, AND REPLACED FLOOR PANEL IAW DWG WSP0668 AND SRM 51-33-01 (MINOR).Aug 24, 2020 · N290UP · Doug MD11F · Fuselage Floor PanelSDR IPXA2020091436169Floor Panel · corrodedINSPECTION TYPE: 2C MAIN CABIN FLOOR PANEL NR WSP 0709-501 HAS CORROSION. REPAIRED CORRODED FLOOR PANEL, IAW VT-SAA EA 011-5320-01-A8535 REV I/R AND UPS EO MD11-5320-77799-A (MINOR).Aug 24, 2020 · N290UP · Doug MD11F · Fuselage Floor PanelSDR IPXA2020091436162Stiffener · crackedINSPECTION TYPE: 2C VERTICAL STIFFNER IS CRACKED AT STA 1841 AND LBL=20. REMOVED, FABRICATED, AND REPLACED STIFFNER IAW DWG. AGA7170 AND SRM 51-33-01 (MINOR).Aug 24, 2020 · N290UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2020091416117Skin · gougedINSPECTION TYPE:2C LT WING FIXED LEADING EDGE UPPER SKIN IS GOUGED AT STA XOS 1185.65. REPAIRED GOUGED LT WING FIXED LEADING EDGE SKIN AT STA XOS 1185.65, IAW SRM 57-40-01 REPAIR 16 FIG 201 (MAJOR).Aug 24, 2020 · N290UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2020091160098Seat Track · corrodedINSPECTION TYPE: 2C MAIN CABIN SEAT TRACK IS CORRODED BETWEEN STA 440-515 AND X= -36. REMOVED AND REPLACED SEAT TRACK BETWEEN STA 440-515 AND X= -36, IAW DWG WSP0826 AND SRM 51-31-01 (MINOR).Aug 24, 2020 · N290UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2020090960022Stringer · crackedINSPECTION TYPE: 2C CENTER WING TANK STRINGER NR 47 IS CRACKED IN 3 PLACES, CXW=17, XCW= 46.5, AND XCW= -17.0. REPAIRED CRACKED CENTER WING TANK STRINGER NR 47 BETWEEN STA XCW= -34.0 TO XCW= 58.5, IAW SRM 57-10-03 REPAIR 1 FIG 201 (MAJOR).Aug 24, 2020 · N290UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2020090960020Stringer · crackedINSPECTION TYPE: 2C CENTER WING TANK STRINGER NR 45 IS CRACKED AT STA XCW= -17.0. REPAIRED CRACKED CENTER WING TANK STRINGER NR 45 BETWEEN STA XCW= -4.250 TO XCW= -29.5, IAW SRM 57-10-03 REPAIR 1 FIG. 201 (MAJOR).Aug 24, 2020 · N290UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2020090859973Hinge · gougedINSPECTION TYPE:2C RT WING INBOARD AILERON NR 3 HINGE FITTING INBOARD AND OUTBOARD SIDE HAS GOUGES AT BOTTOM. REPAIRED GOUGED HINGE FITTING ON RT WING TRAILING EDGE NR 3 INBOARD AILERON HINGE FITTING IAW EA 011-5740-01-A8527 AND EO MD11-5740-77739-A. (MINOR)Aug 24, 2020 · N286UP · Doug MD11F · AileronsSDR IPXA2020090865901Skin · crackedINSPECTION TYPE:2C WHILE PERFORMING TASK CARD 7633 CRACKS WERE DETECTED AT 6EA FASTENER HOLES AT LOWER WING SKIN AT ACCESS CUTOUT 536AB XORS 696.730. REPAIRED 6EA CRACKED HOLES ON LT LOWER WING SKIN AT 536AB CUTOUT XORS 696.730 IAW SRM 57-20-02 REPAIR 5. (MIAug 24, 2020 · N286UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2020090219767Skin · crackedINSPECTION TYPE:2C WHILE PERFORMING TASK CARD 7682. CRACKS WERE DETECTED AT (7EA) FASTENER HOLES AT LOWER RIGHT WING SKIN PANEL AT ACCESS DOOR 638AB CUT OUT. REPAIRED RT WING LOWER SKIN 7EA FASTENER HOLES AROUND 638AB ACCESS DOOR CUT OUT IAW SRM 57-20-02 REPAAug 24, 2020 · N286UP · Doug MD11F · Wing, Plate/SkinSDR FDEA202008242009Engine · damagedPDIS 593 72-51 3549 24AUG20 MEM OPEN U LOGPAGES:3355273 PASSING FL 310 FOR 340 ON INITIAL CLIMBOUT, AIRCRAFT SUDDENLY STARTED VIBRATING CONSIDERABLY #3 ENG EVM SHOWED AMBER BOX 5.0 BUT ALL OTHER INDICATIONS NORMAL. REDUCED POWER, VIBRATION IAug 24, 2020 · N593FE · Doug MD11F · Turbine SectionSDR IPXA2020082659488Battery · faultedEMERG BATT 1 FAULTR & R EMERG BATTERY POWER SUPPLY PER MM33-51-01-400-802 OPS CHECKS GOODAug 24, 2020 · N259UP · Doug MD11F · Emergency LightingSDR IPXA202009160268Floorbeam · corrodedINSPECTION TYPE: 2C CENTER CARGO FLOOR BEAM HAS CORROSION AT STA 1781 X=-58. REPAIRED CORRODED FLOOR BEAM IN CENTER CARGO STA 1781 X= -58, IAW EA 011-5310-01-A8538 REV IR AND EO MD11-5310-77782-A (MAJOR).Aug 23, 2020 · N286UP · Doug MD11F · Fuselage Main, Floor BeamSDR IPXA2020091436164Skin · crackedINSPECTION TYPE:2C LT INBOARD AILERON LT LOWER SKIN BENT OUTWARD AND CRACKED AT OUTBOARD CORNER. REPLACED CRACKED LT INBOARD AILERON ASSY AND INSTALLED ON EO MD11-2700-74700, (MINOR).Aug 23, 2020 · N286UP · Doug MD11F · AileronsSDR IPXA2020091160105Doubler · crackedINSPECTION TYPE: 2C LT WING FIXED LEADING EDGE BEADED DOUBLER IS CRACKED BETWEEN STA XOS 753.1 TO 759.1. REPAIRED CRACKED LT WING FIXED LEADING EDGE BEADED DOUBLER BETWEEN STA XOS 753.1 TO 759.1, IAW SRM 57-40-02 REPAIR 15 FIG 205 (MAJOR).Aug 23, 2020 · N290UP · Doug MD11F · Wing Main, Frame StructureSDR IPXA2020091160104Doubler · crackedINSPECTION TYPE: 2C LT WING FIXED LEADING EDGE BEADED DOUBLER IS CRACKED BETWEEN STA XOS 667.6 TO 673.7. REPAIRED CRACKED LT WING FIXED LEADING EDGE BEADED DOUBLER BETWEEN STA XOS 667.6 TO 673.7, IAW SRM 57-40-02 REPAIR 15 FIG 201 (MAJOR).Aug 23, 2020 · N290UP · Doug MD11F · Wing Main, Frame StructureSDR IPXA2020090960024Skin · crackedINSPECTION TYPE: 2C RT WING FIXED LEADING EDGE LOWER SKIN IS CRACKED AT STA XOS 490.850. REPAIRED CRACKED RT WING FIXED LEADING EDGE LOWER SKIN AT STA XOS 490.850, IAW SRM 57-40-01 REPAIR 17 FIG. 201 (MAJOR).Aug 23, 2020 · N290UP · Doug MD11F · Wing, Plate/SkinSDR FDEA2023012321982Sensor · failedAPPROX 1 SECOND AFTER ADVANCING POWER FOR TAKEOFF RECIEVED LEVEL 1 TIRE DIFF PRESS ALERT. REJECTED TAKEOFF. ALERT CLEARED ITSELF SHORTLY THEREAFTER, ALTHOUGH NR 3 TIRE PRESSURE CONTINUED TO FLUXUATE. ALL TIRE PRESSURES REMAINED IN LIMMITS FOR SECOND TAKEOAug 22, 2020 · N586FE · Doug MD11F · Landing Gear Position and WarningSDR FDEA2023012321980Smoke Warning · false activationAT FLT 360, RECEIVED CABIN SMOKE LEVEL 3 ALERT. ALERT WAS INTERMITTENT ON & OFF. ELECTED TO DIVERT TO KTUL ALERT WENT OUT DURING DESCENT. CREW REPORTED THERE WAS NO SMOKE PRESENT ONLY INTERMITTENT INDICATION ON OVERHEAD PANEL & EAD. PERFORMED SMOKE DETEAug 22, 2020 · N596FE · Doug MD11F · Smoke DetectionSDR IPXA2020090859971Truss Fitting · crackedINSPECTION TYPE:2C CENTER ACCY COMP RT SIDE TRUSS ABOVE CENTER TANK FWD BULKHEAD IS CRACKED AT LONG 27R STA 1159. REMOVED CRACKED TRUSS, FABRICATED AND INSTALLED IN CENTER ACCY COMP ABOVE CENTER TANK BULKHEAD AT LONG 27R BETWEEN STA 1139 - 1159 IAW SRM 51-33-Aug 22, 2020 · N286UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2020090869904Stiffener · crackedINSPECTION TYPE:2C NOSE WHEEL AVIONICS COMPARTMENT UNDER PRESSURE DOOR STA 475 AND 3 INCHES RT OF LONG 52 J ANGLE HAS CORROSION. REMOVED CORRODED STIFFENER, FABRICATED AND INSTALLED FWD AVIONICS COMP STA 475 LONG 52 IAW DWG NCA6042 AND SRM 51-33-01. (MINOR)Aug 22, 2020 · N286UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2020090459846Support Angle · crackedINSPECTION TYPE:2C CENTER CARGO HAS A CRACKED LOWER SIDEWALL SUPPORT ANGLE AT LT SIDE AT STA 1761 BETWEEN LONG 38L - 41L. REMOVED CRACKED ANGLE, FABRICATED AND INSTALLED IN CENTER CARGO LT SIDE STA 1761 BETWEEN LONG 38L - 41L. IAW DRWG ADA0130 AND SRM 51-33-0Aug 22, 2020 · N286UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2020090231709Floor Support · crackedINSPECTION TYPE:2C CENTER CARGO COMPARTMENT FLOOR PANEL LANDING CRACKED AT STA 1521 RBL18. REMOVED CRACKED SUPPORT. FABRICATED AND INSTALLED IN CENTER CARGO COMPARTMENT STA 1521 RBL36 TO LBL36 IAW SRM 51-35-01 (MINOR).Aug 22, 2020 · N286UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2020090219707Floor Support · crackedINSPECTION TYPE: 2C CENTER CARGO COMPARTMENT FLOOR PANEL LANDING CRACKED STA 1521 LBL30. REMOVED CRACKED SUPPORT, FABRICATED AND INSTALLED IN CENTER CARGO STA 1521 LBL30 IAW SRM 51-35-01. MINOR.Aug 22, 2020 · N286UP · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA2020082521982Warning Message · illuminatedAPPROX 1 SECOND AFTER ADVANCING POWER FOR TAKEOFF RECIEVED LEVEL 1 TIRE DIFF PRESS ALERT. REJECTED TAKEOFF. ALERT CLEARED ITSELF SHORTLY THEREAFTER, ALTHOUGH NR 3 TIRE PRESSURE CONTINUED TO FLUXUATE. ALL TIRE PRESSURES REMAINED IN LIMITS FOR SECOND TAKEOFFAug 22, 2020 · N586FE · Doug MD11F · Landing Gear Position and WarningSDR FDEA2020082521980Smoke Warning · false activationAT FLT 360, RECEIVED CABIN SMOKE LEVEL 3 ALERT. ALERT WAS INTERMITTENT ON AND OFF. WE ELECTED TO DIVERTED, ALERT WENT OUT DURING DESCENT. CREW REPORTED THERE WAS NO SMOKE PRESENT, ONLY INTERMITTENT INDICATION ON OVERHEAD PANEL AND EAD. PERFORMED SMOKE DAug 22, 2020 · N596FE · Doug MD11F · Smoke DetectionSDR IPXA2020092060408Cap · damagedINSPECTION TYPE: 2C LT WING LOWER T/E CAP HAS GOUGES ON HORZ FLANGE BETWEEN STA XW=120.630 TO XW=146.618. REPAIRED DAMAGED LT WING LOWER T/E CAP HORZ FLANGE BETWEEN SGTA XW=120.630 TO XW=146.618, IAW EA 011-5710-01-A8546 REV I/R AND EO MD11-5710-77871-A (MAJAug 21, 2020 · N290UP · Doug MD11F · Wing Main, Frame StructureSDR IPXA2020091436163Hinge · chafedINSPECTION TYPE: 2C NR 1 ENG OUTBOARD FAN COWL FWD HINGE IS CHAFED. REPAIRED NR 1 ENG OUTBOARD FAN COWL FWD HINGE, IAW VT-SAA EA 011-7110-01-A8528 REV I/R AND UPS EO MD11-7110-77740-A (MINOR).Aug 21, 2020 · N290UP · Doug MD11F · Nacelle/Pylon, Main FrameSDR IPXA2020090960030Longeron Splice · crackedINSPECTION TYPE: 2C UPPER CARGO COMPARTMENT LONGERON 4L SPLICE CRACK AT STA 1129. REMOVED CRACKED LONGERON SPLICE, FABRICATED AND INSTALLED IN UPPER CARGO LONGERON 4L AT STA 1129, IAW DWG AGA7112 (MINOR).Aug 21, 2020 · N286UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2020090960028Web · crackedINSPECTION TYPE: 2C L3 DOOR FWD JAMB TORQUE BOX WEB CRACK AT LIGHTNING HOLE APPX STA 1255. REPAIRED CRACKED WEB AT L3 DOOR JAMB AROUND LIGHTNING HOLE AT STA 1256, IAW SRM 53-40-15 REPAIR 3 FIG 201 REV 67.Aug 21, 2020 · N286UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2020090869907Beam · crackedINSPECTION TYPE:2C RT WING OUTBOARD FLAP INBOARD FWD HINGE FAIRING OUTBOARD LOWER TEE ANGLE IS CRACKED AT AFT END. REMOVED CRACKED TEE ANGLE BEAM, FABRICATED AND INSTALLED AT RT WING OUTBOARD FLAP INBOARD HINGE IAW SRM 51-31-01. (MINOR)Aug 21, 2020 · N286UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2020090439812Panel · crackedINSPECTION TYPE:2C RT WING TRAILING EDGE BLISTER PANEL JUST AFT OF MLG TRUNNION IS CRACKED. REMOVED CRACKED BLISTER PANEL, FABRICATED AND INSTALLED IN RT WING TRAILING EDGE JUST AFT OF MLG TRUNNION IAW DRWG ARC2841 AND SRM 51-35-01. (MINOR)Aug 21, 2020 · N286UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2020090219768Angle · crackedINSPECTION TYPE:2C LT WING OUTBOARD FLAP INBOARD HINGE Z-ANGLE IS CRACKED. REPAIRED CRACKED ANGLE, FABRICATED AND INSTALLED AT LT OUTBOARD FLAP INBOARD HINGE IAW SRM 51-33-01. (MINOR)Aug 21, 2020 · N286UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2020090239712Tee Fitting · crackedINSPECTION TYPE:2C UPPER CARGO COMPARTMENT LONG 15R T FITTING CRACKED AT STA 1341. REMOVED CRACKED T FITTING, FABRICATED AND INSTALLED IN UPPER CARGO LONG 15R AT STA 1341 IAW SRM 51-33-01. (MINOR)Aug 21, 2020 · N286UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2020090259711Tee Fitting · crackedINSPECTION TYPE:2C UPPER CARGO COMPARTMENT LONG 15L T FITTING CRACKED AT STA 1341. REMOVED CRACKED T FITTING, FABRICATED AND INSTALLED IN UPPER CARGO COMPARTMENT LONG 15L AT STA 1341 IAW SRM 51-33-01. (MINOR)Aug 21, 2020 · N286UP · Doug MD11F · Fuselage Main, Attach Fittings
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