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 IPXA201906143240Longeron · corrodedINSPECTION TYPE:2CCENTER CARGO BILGE AREA HAS CORROSION ON LONGERON 48L SPLICE BETWEEN STA. 1541 - 1561.REPAIRED CORRODED CENTER CARGO LONGERON 48L SPLICE BETWEEN STA. 1541 - 1561 IAW MD-11 SRM 53-00-05 REPAIR 1 FIGURE 202. (MAJOR)May 26, 2019 · N283UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2019061243190Stiffener · crackedINSPECTION TYPE:2C, AFT CARGO STA. 1841 LBL 30 BELOW FLOOR HAS A CRACKED VERTICAL STIFFENER.REMOVED AND REPLACED CRACKED VERTICAL STIFFENER AT STA. 1841 LBL 30 BELOW AFT CARGO FLOOR IAW MD-11 SRM 51-33-01. (MINOR)May 26, 2019 · N283UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2019061243189Stiffener · crackedINSPECTION TYPE:2CAFT CARGO AT STA. 1841 BL 0 BELOW FLOOR HAS A CRACKED VERTICAL STIFFENER.REMOVED AND REPLACED CRACKED VERTICAL STIFFENER AT STA. 1841 BL 0 BELOW AFT CARGO FLOOR IAW MD-11 SRM 51-33-01. (MINOR)May 26, 2019 · N283UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2019061243128Stiffener · crackedINSPECTION TYPE:2C, AFT CARGO AT STA.1841 RBL 30 HAS A CRACKED VERTICAL STIFFENER BELOW FLOOR.REMOVED AND REPLACED CRACKED AFT CARGO VERTICAL STIFFENER AT STA. 1841 RBL 30 BELOW FLOOR IAW MD-11 SRM 51-33-01. (MINOR)May 26, 2019 · N283UP · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA2019052861169Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED BUSHING FABRMay 26, 2019 · N598FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2019052861168Bracket · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#3 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRICATEMay 26, 2019 · N598FE · Doug MD11F · Trailing Edge FlapsSDR IPXA2019061043072Angle · gougedINSPECTION TYPE:2C CENTER CARGO STA. 1781 RT SIDE JUST AFT OF CARGO DOOR AFT JAMB. VERTICAL STANCHION (ANGLE) HAS 2 GOUGES.REMOVED AND REPLACED GOUGED VERTICAL STANCHION (ANGLE) AT CENTER CARGO STA, 1781 R/H SIDE IAW MD-11 SRM 51-35-01. (MINOR)May 26, 2019 · N293UP · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA2019052861167Skin · crackedHFEC INSPECTION CARRY OUT AND FOUND CRACK APPROXIMATELY 1/4" IN LENGTH AT LEFT HAND SIDE CORNER NUMBER 11 FUEL ACCESS DOOR FORWARD INBOARD CORNER. REPAIR CARRIED OUT AT LEFT HAND SIDE CORNER NO.11 FUEL ACCESS DOOR FORWARD INBOARD CORNER AT XOS 586 AS PER SMay 26, 2019 · N598FE · Doug MD11F · Wing, Plate/SkinSDR FDEA2019052861166Former · crackedLEFT HAND WING FIXED LEADING EDGE COMPARTMENT STATION XOS 939 FORMER FOUND CRACKED. CRACKED FORMER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED FORMER AS PER DOUGLAS DRAWING ARB1292 REVISION G. INSTALLED FORMER AT LEFT HAND WING FIXED LEADING EDGE COMPAMay 26, 2019 · N598FE · Doug MD11F · Wing SparSDR FDEA201905261165Doubler · crackedRIGHT HAND WING FIXED LEADING EDGE COMPARTMENT STATION XOS 605 LOWER STRINGER DOUBLER FOUND CRACKED. CRACKED DOUBLER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED DOUBLER AS PER DOUGLAS DRAWING ARB2933 REVISION AJ. INSTALLED DOUBLER AT RIGHT HAND WING FIXEMay 26, 2019 · N598FE · Doug MD11F · Wing Main, Frame StructureSDR FDEA2019052861164Doubler · crackedLEFT HAND WING FIXED LEADING EDGE COMPARTMENT LOWER STATION XOS 546 STRINGER DOUBLER FOUND CRACKED. CRACKED DOUBLER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED DOUBLER AS PER DOUGLAS DRAWING ARB2933 REVISION AJ. INSTALLED FABRICATED DOUBLER AT LEFT HAND May 26, 2019 · N598FE · Doug MD11F · Wing Main, Frame StructureSDR IPXA2019052642498Structure · damagedINSPECTION TYPE:N/A AFT BULK CARGO DOOR LWR CORNER DMG'ED AFT OF EXISTING PREVIOUS REPAIR. REPAIRED PER EO MD11-5230-71174-B.May 26, 2019 · N259UP · Doug MD11F · Cargo/Baggage DoorsSDR IPXA2019062194518Floorbeam · crackedINSPECTION TYPE:3CFWD LOWER CARGO FLOOR BEAM IS CRACKED AT STA. 6-70 ABOVE LONGERON 43 RT.REPAIRED CRACKED FWD LOWER CARGO FLOOR BEAM AT STA. Y=6-70, X=-57.5 AND Z=-98 IAW MD-11 SRM 53-40-51 REPAIR 1, FIGURE 202. (MAJOR)May 25, 2019 · N271UP · Doug MD11F · Fuselage Main, Floor BeamSDR IPXA201906143239Lug · gougedINSPECTION TYPE:2C#3 ENG. L/H T/R UPPER LUG IS GOUGED.REPAIRED GOUGED #3 L/H T/R UPPER BEAM AFT CASCADE RING LUG IAW VT-SAA EA 011-7830-01-A7793 REV. IR AND UPS EO MD11-7830-72915-A. (MINOR)May 25, 2019 · N283UP · Doug MD11F · Engine Thrust ReverserSDR IPXA2019061043071Beam · crackedINSPECTION TYPE:2C, FWD LOWER CARGO STA. 6-73 ABOVE LONGERON 43 L/H HORIZONTAL BEAM IS CRACKED AND CORRODED.REMOVED AND REPLACED CRACKED & CORRODED FWD LOWER CARGO HORIZONTAL BEAM AT STA. 6-73 ABOVE LONGERON 43L IAW MD-11 SRM 51-35-01 & 51-33-01. (MINOR)May 25, 2019 · N283UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2019060742946Floor Support · crackedINSPECTION TYPE:2CCENTER CARGO AT STA. 1741 AND LONG. 41 L/H, FLOOR SUPPORT ANGLE IS CRACKED.REMOVED, FABRICATED AND REPLACED FLOOR SUPPORT ANGLE AT STA. 1741 AND LONG. 41 L/H IAW DWG. ADA0130 AND SRM 51-33-01. (MINOR)May 25, 2019 · N283UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2019060742945Floor Support · crackedINSPECTION TYPE:2CCENTER CARGO AT STA. 1781 AND LONG. 41 L/H, FLOOR SUPPORT ANGLE IS CRACKED.REMOVED, FABRICATED AND REPLACED FLOOR SUPPORT ANGLE AT STA. 1781 AND LONG. 41 L/H IAW DWG. AFA7295 AND SRM 51-33-01. (MINOR)May 25, 2019 · N283UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2019060742944Floor Support · crackedINSPECTION TYPE:2CCENTER CARGO AT STA. 1751 AND LONG. 41 L/H, FLOOR SUPPORT ANGLE IS CRACKED.REMOVED, FABRICATED AND REPLACED FLOOR SUPPORT ANGLE AT STA. 1751 AND LONG. 41 L/H IAW DWG. ADA0130 AND SRM 51-33-01. (MINOR)May 25, 2019 · N283UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2019060762911Skin · crackedINSPECTION TYPE:3C, R/H OUTERWING LOWER ACCESS DOOR CUT-OUT PANEL LANDING BETWEEN STA. XORS.=683.4 TO XORS.=713.6 HAS 5 FASTENER HOLES CRACKED.REPAIRED R/H OUTERWING LOWER ACCESS DOOR CUTOUT PANEL LANDING BETWEEN STA. XORS.=683.4 TO 713.6 IAW SRM 57-20-02 REPAMay 25, 2019 · N271UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2019060542826Skin · crackedINSPECTION TYPE:2CR/H WING LOWER SURFACE AT PANEL #636AB, PANEL LANDING HAS 13 CRACKS AT FASTENER HOLES ( STA. XORS.=683.4-713.65)REPAIRED CRACKED R/H WING LOWER SURFACE PANEL LANDING BETWEEN STA. XORS. 683.4- 713.65 IAW SRM 57-20-02 REPAIR 5 FIG. 201.(MINOR)May 25, 2019 · N283UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2019060542839Skin · crackedINSPECTION TYPE:2CL/H WING LOWER SKIN AT ACCESS PANEL LANDING STA. XORS.= 683.4- 713.650 HAS 6 CRACKED FASTENER HOLES.REPAIRED CRACKED L/H WING LOWER SKIN AT ACCESS PANEL LANDING BETWEEM STA. XORS.= 683.4- 713.650 IAW SRM 57-20-02 REPAIR 5 FIG. 201. (MINOR)May 25, 2019 · N283UP · Doug MD11F · Wing, Plate/SkinSDR FDEA2019052851158Pump · leakingIN FLIGHT GOT LEVEL 1 "HYDRA. 2 OFF" ALERT. COMPLIED WITH QRH PROCEDURE AND ALSO REVIEWED THE REFERENCED "HYD. 2 FAIL" QRH PROCEDURE. THE "HYDR. 2 FAIL" ALERT APPEARED DURING CONFIG ON APPROACH. SINCE WE ALREADY REVIEWD THE PROCEDURE, AND WE HAD NO DEGRAMay 25, 2019 · N603FE · Doug MD11F · Hydraulic Pump (Electric/Engine), MainSDR IPXA2019062843838Skin · corrodedINSPECTION TYPE: 3C, UPPER CENTER SKIN WAS CORRODED BETWEEN STA. XCW=-101 TO XCW=-110 AND ABOVE STRINGER 12. REPAIRED THE SKIN IAW EA 011-5730-01-A7794, REV I/R, AND EO MD11-5730-72977-A. MAJOR.May 24, 2019 · N271UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2019062643759Longeron · crackedINSPECTION TYPE:3CMAIN CABIN LONGERON 27R IS CRACKED AT STA. 1256 UNDER R3 DOOR.REMOVED AND REPLACED CRACKED MAIN CABIN LONGERON 27R BETWEEN STA. 1256 - 1305 IAW MD-11 SRM 51-31-01, 51-33-01 AND 51-35-01. (MINOR)May 24, 2019 · N271UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2019062194516Stringer · crackedINSPECTION TYPE:3CCENTER WING TANK STRINGER 52 BETWEEN X=-17 &X=-46 IS CRACKED. REPAIRED CRACKED CENTER WING TANK STRINGER 52 BETWEEN STA. XCW=0.00 & XCW=-32 IAW MD-11 SRM 57-10-03 REPAIR 1, FIGURE 201. (MAJOR)May 24, 2019 · N271UP · Doug MD11F · Hydraulic System, MainSDR IPXA2019061983420Panel · gougedINSPECTION TYPE:2CR/H WING LOWER L/E PANEL 615DB HAS TOOLING MARKS AROUND FASTENER HOLES.REPAIRED DAMAGED R/H WING L/E PANEL 615DB IAW VT-SAA EA 011-5730-01-A7798 REV. IR AND UPS EO MD11-5720-72921-A. (MINOR)May 24, 2019 · N283UP · Doug MD11F · Wing, Plate/SkinSDR FDEA201905241151Hinge Bracket · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE OUTBOARD LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE OUTBOARD LUG HOLE BORE (A AND B HOLES) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57May 24, 2019 · N598FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201905241150Hinge Bracket · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE INBOARD LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE INBOARD LUG HOLE BORE (G AND F HOLES) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-5May 24, 2019 · N598FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201905241149Hinge Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE OUTBOARD LUG HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE OUTBOARD LUG HOLE BORE (A AND B HOLES) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-5May 24, 2019 · N598FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201905241148Hinge Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE INBOARD LUG HOLE BORE (G AND F HOLES) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52May 24, 2019 · N598FE · Doug MD11F · Trailing Edge FlapsSDR IPXA2019061754293Stringer · crackedINSPECTION TYPE:3CCENTER WING FUEL TANK LOWER STRINGER 42 IS CRACKED AT XCW 42.REPAIRED CRACKED CENTER WING FUEL TANK LOWER STRINGER 42 BETWEEN XCW=-34.0 TO XCW=-58.0 IAW MD-11 SRM 57-10-03 REPAIR 1, FIGURE 201. (MAJOR)May 24, 2019 · N271UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2019061243153Vane · damagedINSPECTION TYPE:2CR/H O/B FLAP VANE O/B LOWER EDGE IS DAMAGED.REPAIRED DAMAGED R/H O/B FLAP VANE O/B LOWER EDGE IAW MD-11 SRM 57-50-80, REPAIR 2, PARA. 2.A(2)(A)(5). (MAJOR)May 24, 2019 · N283UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2019061243073Brace · brokenINSPECTION TYPE:2C, RT WING T/E VERTICAL SUPPORT (BRACE) JUST AFT OF MLG AT APPROX. XOS 247 IS BROKEN.REMOVED AND REPLACED RT WING T/E VERTICAL SUPPORT (BRACE) JUST AFT OF MLG AT APPROX. XOS 247 IAW MD-11 SRM 51-31-01 & 51-33-01. (MINOR)May 24, 2019 · N283UP · Doug MD11F · Wing Miscellaneous StructureSDR FDEA201905241147Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE SURFACE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44- May 24, 2019 · N598FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201905241146Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE SURFACE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44- 08May 24, 2019 · N598FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201905241144Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57May 24, 2019 · N598FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201905241142Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM May 24, 2019 · N598FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201905241140Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57May 24, 2019 · N598FE · Doug MD11F · Trailing Edge FlapsSDR IPXA2019061074950Floorboard · damagedINSPECTION TYPE:3C MAIN CABIN FLOOR BOARD # 263BF HAS EDGE DAMAGE.FABRICATED REPLACEMENT FLOOR BOARD # 263BF IAW UPS EO MD11-5320-27386-C. (MAJOR)May 24, 2019 · N271UP · Doug MD11F · Fuselage Floor PanelSDR FDEA201905241152Frame · chafedMAIN DECK LEFT HAND FRAME AT STATION 535 LONGERON 24 LEFT FOUND EXISTING REPAIR OUTER ANGLE CHAFFED . MAIN DECK LEFT HAND FRAME AT STATION 535 LONGERON 24 LEFT , CHAFFED MARK AT EXISTING OUTER REPAIR ANGLE REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00May 24, 2019 · N598FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201905241145Door Frame · separatedCENTER GEAR LH GEAR DOOR AFT DOOR JAMB AREA HAS SEPERATION CAUSED FROM DOOR DEPARTING THE AC IN FLIGHT. AFTER CONSULTATION WITH ENGINEERING, IT WAS DETERMINED THAT THIS AREA IS A FAIRING ATTACHED TO THE JAMB AND IS NOT STRUCTURAL. PRIOR TO ATTACHING THE AFMay 24, 2019 · N624FE · Doug MD11F · Landing Gear DoorsSDR FDEA201905241143Wire Harness · damaged"FIRE DET 1 FAIL" LEVEL 1 ALERT DURING CRUISE FLIGHT. INTERROGATED #1 FDCU. FOUND #1 ENG. UPPER RIGHT TURBINE A LOOP FAULTED. WITH B LOOP ALREADY DEFERRED. REMOVED AND REPLACED #1 ENG. UPPER RIGHT TURBINE A LOOP AND HARNESS BETWEEN DH4 AND DH23. FDCU RTSMay 24, 2019 · N572FE · Doug MD11F · Detection SystemSDR FDEA201905241141Bolt · seizedDID NOT RECEIVE AN UP & LOCKED INDICATION ON THE RIGHT MAIN GEAR AFTER T/O ON BOTH PRIMARY & SECONDARY DISPLAY. RAN THE CHECKLIST,CYCLED THE GEAR,GOOD DOWN AND LOCKED,NEGATIVE RIGHT MAIN UP AND LOCKED. FELT A SLIGHT VIBRATION AT 16K,230KTS WITH GEAR HANDLMay 24, 2019 · N575FE · Doug MD11F · Landing Gear DoorsSDR IPXA2019060542861Web · crackedINSPECTION TYPE:2CL-3 DOOR JAMB LOWER AFT WEB IS CRACKED AT STA. 1307 AND Z=-18.REPAIRED CRACKED L-3 DOOR JAMB LOWER AFT WEB AT STA. 1307 AND Z=-18 IAW SRM 53-40-15 REPAIR 3 FIG. 201. (MAJOR)May 24, 2019 · N283UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2019060542828Fairing · crackedINSPECTION TYPE:3C#1 ENG. PYLON STINGER FAIRING 438ELHAS A CRACKE THRU FASTENER HOLE.REPAIRED #1 ENG. PYLON STINGER FAIRING #438EL IAW SRM 54-55-01 REPAIR 2. (MINOR)May 24, 2019 · N271UP · Doug MD11F · Nacelle/Pylon Miscellaneous StructureSDR IPXA2019062874810Skin · corrodedINSPECTION TYPE: 3C, SKIN WAS CORROSION AT STA. IXCW=17.0, STRINGERS 14 & 15. REPAIRED THE SKIN IAW EA 011-5730-01-A7795, REV I/R, AND EO MD11-5710-72976-A. MAJOR.May 23, 2019 · N271UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2019062653743Stringer · crackedINSPECTION TYPE:3CRT WING #15 STRIMGER HAS 2 CRACKES.REPAIRED CRACKED RT WING #15 STRINGER BETWEEN XORS=433 & XORS=455 IAW MD-11 SRM 57-20-03 REPAIR 3 FIGURE 201. (MAJOR)May 23, 2019 · N271UP · Doug MD11F · Wing, Longeron/StringerSDR IPXA2019062443669Stringer · crackedINSPECTION TYPE:3CL/H WING UPPER STRINGER #15 IS CRACKED BETWEEN STA. XORS.=433 TO 455.REPAIRED CRACKED L/H WING UPPER STRINGER #15 BETWEEN STA. XORS.=433-455 IAW SRM 57-20-03 REPAIR 3 FIG. 201. (MAJOR)May 23, 2019 · N271UP · Doug MD11F · Wing, Longeron/StringerSDR IPXA2019061983422Cap · crackedINSPECTION TYPE:2C, R/H UNDER WING CANTED PANEL UPPER CAP IS CRACKED AT STA. 1236.8.REPAIRED CRACKED R/H UNDER WING CANTED PANEL UPPER CAP AT STA. 1236.8 IAW UPS EO MD11-5310-72747-A. (MAJOR)May 23, 2019 · N283UP · Doug MD11F · Wing Main, Frame StructureSDR IPXA201906143243Skin · crackedINSPECTION TYPE:2CR/H WING FIXED L/E SKIN IS CRACKED AT #9 SLAT TRACK CUTOUT.REPAIRED CRACKED R/H WING FIXED L/E SKIN AT XOS=610.8437 IAW MD-11 SRM 57-40-01 REPAIR 18, FIGURE 202. (MAJOR)May 23, 2019 · N283UP · Doug MD11F · Wing, Plate/Skin
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