N259UP, cancelled Feb 20, 2026

Service difficulty reports · 528

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 = 'N259UP' AND deregistration_id = 'N259UP-2026-02-20'
  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 IPXA2025100196817Longeron Splice · corrodedCTR CARGO BILGE AREA STA 5-53 TO 5-73 LONGERON 48L HAS CORROSION. 74-049 ATA CODE 53 QC AUDIT C/WSep 9, 2025 · N259UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2025091596879Longeron · corrodedCENTER CARGO BILGE AREA STA 5-11 TO 5-32 LONGERON 49R HAS CORROSION. PERFORMED A DVI CENTER CARGO AREA BETWEEN STA 5-11 & 5-32 NO DEFECTS NOTED IAW EA 0115310-01-B0566 STEP 6.Sep 9, 2025 · N259UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2025091709687Stringer · crackedCENTER WING UPPER FUEL TANK LOWER STRINGER 41 CRACK AT XCW = -81 REQUIRES PERMANENT REPAIR PER EO 81811-REQ001 ATA 57-11 QC AUDIT C/WSep 4, 2025 · N259UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2025041154477Panel · openSLIDING PANEL ATTACHED TO L1 ENTRY DOOR INOP INSTALLED SPRING IAW AMM 25-23-23/401 AND IPC 25-23-04-15. OPS CHECK GOOD. SLIDING PANEL OPENS AND CLOSES WITH NORMAL DOOR OPERATION WITH NO ISSUES. THIS CLOSES DEFERRAL. PLACARD REMOVED.Apr 11, 2025 · N259UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2025021177655Bottle · emptyR1 DOOR ASSIST BOTTLE DEPLETED. REMOVED AND REPLACED R1 DOOR ASSIST BOTTLE CHARGE VALVE IAW AMM 52-11-04-400-801 (H)(J)(K). C/W SERVICING IAW 12-25-04-600-801Feb 11, 2025 · N259UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2023093011200Flap · gougedABSORB FOUND L/H WING I/B FLAP I/B ATTACHMENT MOUNT UPPER BOLT HOLE CUT-OUT IS GOUGED, DURING IN-PROCESS INSTALL VERIFIED STEP 1 AND 2Sep 30, 2023 · N259UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023092794262Attach Fitting · corrodedINSPECTION TYPE:2CL/W A/C SIDE I/B FLAP O/B HINGE # 3 LUG O/B FACE HAS CORROSION AT REF STA. XW=254 , YW= 495.961 AND ZW=-28.941ACCOMPLISHED REPAIR IAW VTSAA EA 011/5740-01-B0094 I/R DATED 09/25/2023 , UPS EO MD11-5740-88267-A 8100-9 SIGNED BY STEPHEN KANG AR-Sep 27, 2023 · N259UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023092794260Attach Fitting · corrodedINSPECTION TYPE:2CL/H WING A/C SIDE I/B FLAP O/B HINGE #3 LUG BORE HAS CORROSION AT REF STA. XW=254,YW=495.961 AND ZW=28.941ACCOMPLISHED REPAIR IAW VTSAA EA 011/5740-01-B0094 I/R DATED 09/25/2023, UPS EO MD11-5740-88267-A AND 8100-9Sep 27, 2023 · N259UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023092794264Attach Fitting · corrodedINSPECTION TYPE:2CL/H WING A/C SIDE I/B FLAP O/B HINGE #3 LUG I/B FACE HAS CORROSION AT REF STA.XW=254,YW=495.961 AND ZW=-28.941REPAIR ACCOMPLISHED IAW VTSAA EA 011/5740-01-B0094 I/R DATED 09/25/2023, UPS EO. MD11-5740-88267-A DATED 09/26/2023 AND 8100-9 SIGNESep 27, 2023 · N259UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023092494237Support Angle · crackedINSPECTION TYPE:2CAFT CARGO COMP STA 1954 UNDER FLOOR PANEL 187HF ANGLE SUPPORT HAS CRACKREPLACED ANGLE SUPPORT IAW MD11-SRM 51-35-01-0G-01. (MINOR)Sep 24, 2023 · N259UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2023092494236Bracket · crackedINSPECTION TYPE:2CUPPER CENTER TANK CRACKED BRACKET AT STA -81/STR52REPLACED BRACKET IAW MD11 SRM 51-31-01 AND SRM 51-33-01. MINORSep 24, 2023 · N259UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2023092494235Stiffener · gougedINSPECTION TYPE:2CTAIL CONE COMP RH PATIO DOOR FWD SIDE FRAME AND METAL PLATE HAS DEEP GOUGEDREPLACED SUPPORT ANGLE FRAME AT TAIL CONE COMP. R/H PATIO DOOR FWD SIDE FRAME AND METAL PLATE IN REF.MD11 SRM 51-35-01-0G-0 AND SRM 51-33-01-0G-0(MINOR)Sep 24, 2023 · N259UP · Doug MD11F · Aerodynamic FairingsSDR IPXA2023092494234Frame · gougedINSPECTION TYPE:2CTAIL CONE FWD HORIZONTAL FRAME HAS A GOUGE R/H SIDEREPAIRED WITH DOUBLER IAW SRM 53-00-00-2R-1 FIG. 201 AND 53-80-02-01-1 . (MINOR)Sep 24, 2023 · N259UP · Doug MD11F · Aerodynamic FairingsSDR IPXA2023092994306Lever · wornL/H WING I/B FLAP IB ACTUATOR UPPER LUG IS WORN AT STA XIFH=116.850, YIFH=43.493. REPAIRED WORN LUG ATTACHMENT AT THE L/H WING I/B FLAP I/B ACTUATOR UPPER LUG AT STA XIFH=116.80, YIFH=43.493 IAW VTSAA EA 011-5700-01-B0104 I/R, UPS EO MD11-5740-88219-A DATED 09Sep 14, 2023 · N259UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023092994304Hinge Bracket · corrodedR/H WING I/B FLAP SIDE O/B HINGE #14 LUG BORE HAS CORROSION AT STA XW=-254, YW=495.96. REPAIRED CORRODED HINGE BRACKET AT THE R/H WING I/B FLAP SIDE O/B HINGE AT STA XW=-254, YW=495.96 IAW VTSAA EA 011-5740-01-B0105 I/R, UPS EO MD11-5750-88271-A DATED 09/28/23Aug 31, 2023 · N259UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023092994302Hinge Bracket · corrodedR/H WING I/B FLAP SIDE O/B HINGE #13 LUG BORE HAS CORROSION AT STA XW=-254, YW=495.96. REPAIRED CORRODED HINGE-BRACKET AT THE R/H WING I/B FLAP SIDE O/B HINGE AT STA XW=-254, YW= 495.96 IAW VTSAA EA 011-5740-01-B0105 I/R, UPS EO MD11-5750-88271-A DATED 09/28/2Aug 31, 2023 · N259UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023092994301Hinge Bracket · corrodedR/H WING A/C SIDE I/B FLAP O/B HINGE #3 LUG O/B FACE HAS CORROSION AT STA XW=-254, YW=495.961. REPAIRED CORRODED HINGE-BRACKET AT THE R/H WING A/C SIDE I/B FLAP O/B HINGE AT STA XW=-254, YW=495.961 VTSAA EA 011-5740-01-B0095 I/R, UPS EO MD11-5740-88269-A DATEDAug 31, 2023 · N259UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023092994300Hinge Bracket · corrodedR/H WING A/C SIDE I/B FLAP O/B HINGE #3 LUG I/B FACE HAS CORROSION AT STA XW= .254, YW= 495.961. REPAIRED CORRODED HINGE BRACKET AT R/H WING I/B FLAP O/B HINGE AT STA XW=.254, YW=495.961 IAW VTSAA EA 011-5740-01-B0095 IR, UPS EO MD11-5750-75959-J DATED 09/27/2Aug 31, 2023 · N259UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023092994298Hinge Bracket · corrodedINSPECTION TYPE:2CR/H WING A/C SIDE I/B FLAP O/B HINGE #3 LUG BORE HAS CORROISON AT STA XW=-254, YW=495.961.REPAIRED CORRODED HINGE-BRACKET AT THE R/H WING I/B FLAP O/B HINGE AT STA XW=-254, YW=495.961 IAW VTSAA EA 011-5740-01-B0095 I/R, UPS EO MD11-5740-88269Aug 31, 2023 · N259UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023092994297Hinge Bracket · corrodedINSPECTION TYPE:2CR/H WING O/B FLAP O/B HINGE #13 LUG BORE HAS CORROSION AT STA XW=-638.305, YW=670.239.REPAIRED CORRODED HINGE BRACKET AT THE R/H WING O/B FLAP O/B HINGE AT STA XW=-638.305, YW=670.239 IAW EA 011-5740-01-B0106 I/R, UPS EO MD11-5750-88273-A.Aug 31, 2023 · N259UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023092994296Hinge Bracket · corrodedINSPECTION TYPE:2CR/H WING O/B FLAP I/B HINGE #13 LUG BORE HAS CORROISON AT STA XW=-486.403, YW=589.366.REPAIRED CORRODED HINGE-BRACKET AT THE R/H WING O/B FLAP I/B HINGE STA XW=-486.403, YW=589.366 IAW VTSAA EA 011-5740-01-B0100 I/R, UPS EO MD11-5750-88272-A.Aug 31, 2023 · N259UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023092894285Hinge Bracket · corrodedINSPECTION TYPE:2CL/H WING I/B FLAP O/B HINGE #14 LUG BORE HAS CORROSION AT STA XW=254, YW=495.96.REPAIRED CORRODED HINGE AT THE L/H WING I/B FLAP O/B HINGE AT STA XW=254, YW=495.96 IAW VTSAA EA 011-5740-01-B0101 I/R, UPS EO MD11-5750-88274-AAug 31, 2023 · N259UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023092894284Hinge Bracket · gougedINSPECTION TYPE:2CL/H WING I/B FLAP O/B HINGE #14 LUG BORE IS GOUGED AT STA XW=254, YW=495.96.REPAIRED L/H WING I/B FLAP O/B HINGE AT STA XW=254, YW=495.96 IAW VTSAA EA 011-5740-01-B0101 I/R, UPS EO MD11-5750-88274-AAug 31, 2023 · N259UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023092294226Hinge Bracket · corrodedINSPECTION TYPE:2CR/H WING O/B FLAP I/B HINGE #4 LUG BORE HAS CORROSION.REPLACED CORRODED HINGE-BRACKET AT THE R/H WING O/B FLAP I/B HINGE IAW AMM 57-53-01-400-801. (MINOR)Aug 31, 2023 · N259UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023092294225Hinge Bracket · corrodedINSPECTION TYPE:2CL/H WING O/B FLAP O/B HINGE-BRACKET #4 LUG BORE HAS CORROSION.REPLACED CORRODED HINGE-BRACKET AT THE L/H WING O/B FLAP O/B HINGE IAW AMM 57-53-01-400-801. (MINOR)Aug 31, 2023 · N259UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023091994196Seat Track · corrodedINSPECTION TYPE:2C*MAJOR REPAIR* MAIN CABIN R/H FLOOR SEAT TRACK AT STA Y=1541, X=-8.5 HAS CORROSION.REPAIRED CORRODED SEAT TRACK AT THE MAIN CABIN R/H FLOOR AREA STA Y=1541, X=-8.5 IAW SRM 53-00-52-2R-1 FIG. 201 REPAIR 1 (MAJOR)Aug 30, 2023 · N259UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2023091594161Splice · crackedINSPECTION TYPE:2CMAIN CABIN AT STA Y=1531, LONGERON 11L HAS A CRACKED PRODUCTION SPLICE.REPLACED CRACKED PRODUCTION SPLICE AT THE MAIN CABIN STA Y=1531, LONGERON 11L IAW SRM 51-33-01 (MINOR)Aug 30, 2023 · N259UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2023091594160Splice · crackedINSPECTION TYPE:2CMAIN CABIN AT STA Y=1531, LONGERON 12L HAS A CRACKED PRODUCTION SPLICE.REPLACED CRACKED PRODUCTION SPLICE AT THE MAIN CABIN STA Y=1531, LONGERON 12L IAW SRM 51-33-01 AND DWG AEA7633. (MINOR)Aug 30, 2023 · N259UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2023092594244Doubler · wornINSPECTION TYPE:2CTAIL CONE R/H UPPER FWD PRODUCTION DOUBLER IS WORN AT STA Y=2165, X=36.5.REPAIRED PRODUCTION DOUBLER AT THE TAIL CONE R/H UPPER FWD AT STA Y=2165, X=36.5 IAW UPS EO MD11-5350-66790-B APPENDIX B. (MINOR)Aug 29, 2023 · N259UP · Doug MD11F · Aerodynamic FairingsSDR IPXA2023090794114Doubler · crackedINSPECTION TYPE:2CL/H WING FIXED L/E BEADED DOUBLER AT STA XORS= 772 HAS A CRACKED.REPAIRED CRACKED BEADED DOUBLER AT THE L/H WING FIXED L/E AT STA XORS=772 IAW SRM 57-40-02 REPAIR 15 FIG 205 (MAJOR)Aug 29, 2023 · N259UP · Doug MD11F · Wing Miscellaneous StructureSDR IPXA2023091994191Stiffener · crackedINSPECTION TYPE:2CR/H MLG WHEEL WELL AREA O/B AFT SIDE WALL STIFFENER HAS A CRACKED.REPLACED CRACKED STIFFENER AT THE R/H MLG WHEEL WELL AREA O/B AFT SIDE IAW SRM 51-35-01 (MINOR)Aug 28, 2023 · N259UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2023092994305Skin · gouged*MAJOR REPAIR* L/H WING OUTBD L/E SKIN GOUGED DAMAGED BETWEEN STA XOS=1113 AND XOS=1132.5. REPAIRED GOUGED SKIN AT THE L/H WING OUTBD L/E BETWEEN STA XOS=1113 AND XOS=1132.5 IAW VTSAA EA 011-5730-01-B0098 I/R, UPS EO MD11-5750-88290-A DATED 09/28/23 AND FAA FOAug 25, 2023 · N259UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2023092894280Flap System · damagedINSPECTION TYPE:2CL/H WING OUT BOARD FLAP TRAILING EDGE UPPER SKIN WEDGE IS DAMAGED ATSTA XOF=498.367.REPLACED L/H WING O/B FLAP ASSY. IAW AMM 27-50-30-400-801 (MINOR)Aug 25, 2023 · N259UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023091994199Stringer · crackedINSPECTION TYPE:2C*MAJOR REPAIR* CENTER WING UPPER FUEL TANK STRINGER #41 CENTER WING AT STA XCW=-81 HAS A CRACKED REPAIR.REPAIRED CRACKED STRINGER 41 AT THE CENTER WING UPPER FUEL TANK AT STA XCW=-81 IAW VTSAA EA 011-5710-01-B0087 I/R , UPS EO MD11-5710-81811Aug 23, 2023 · N259UP · Doug MD11F · Fuel StorageSDR IPXA2023061693453Brake · inoperativeINSPECTION TYPE:NA*A/C WAS TOWED* LEVEL 2 TIRE FAIL.BLOCK TURN BACK REJECTED TAKEOFF AROUND 110KTS FOR UNKOWN DECELERATION.LEFT CENTER GEAR TIRE IMMEDIATELY HEATED TO OVER 700 DEGREES.FUSE PLUG RELEASED. LEVEL 2 BRAKE OVERHEAT DUE TO REJECTED TAKEOFF ON #1 MAIJun 14, 2023 · N259UP · Doug MD11F · Landing Gear Brake SystemSDR IPXA2023041892911Battery · dischargedINSPECTION TYPE:NA*SDR FILED OPEN* EMER LT BAT 1 LO. DEFERRED PER MEL 33-50-4. DMP C/W AND PLACARD INSTALLED. R&R EMERGENCY LIGHTING BATTERY SUPPLY IAW 33 51 01 THS CLEARS DMI M807148 PLACARD REMOVED.Apr 17, 2023 · N259UP · Doug MD11F · Emergency LightingSDR IPXA2022101287087Chiller · odorDURING DESCENT PASSING TRHOUGH A SMOKY HAZY LAYER ON ODER ENTERED THE FLIGHT DECK. DISSIPATED AFTER 30 SEC. AFTER ENG SHUTDOWN W/APU RUNNING & AIR SELECTED ON THE SMELL/ODOR REOCCRRED. APPEARS TO BE EMANATING FROM THE REFRIG. VERIFIED SMELL IS CONCENTRATED AT Oct 11, 2022 · N259UP · Doug MD11F · Air Distribution SystemSDR IPXA2022100186757Wedge · tornINSPECTION TYPE:SV, LT WING O/B FLAP REAR SPAR AND T/E WEDGE DAMAGED AT STAXOF=498.367.REPAIRED LIH WING O/B FLAP REAR SPAR AND T/E WEDGE AT STAXOF=498.367 IAW VTSAA EA 011-575301-A9718-IR AND UPS EO MD11-5750-84886-A.Sep 30, 2022 · N259UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2022032280353None · noneINSPECTION TYPE:NA**SUPPLEMENTAL SDR** SMELLED FUMES COMING FROM THE GALLEY AREA THEN NOTICE A SLIGHT SMOKEY AIR, TURNED REFRIG SWITCH OFF, PULLED BOTH REFRIG AND HOT POT/OVEN BREAKERS, CALLED FLT CONTROL AND PER MAINT CONTROLL PULLED GALLEY BREAKER, PERFORMEDMar 22, 2022 · N259UP · Doug MD11F · Buffet/GalleysSDR IPXA2021112276233None · noneINSPECTION TYPE:N/A** EMERGENCY DECLARED** A/C TOWED OFF RUNWAY** FAA NOTIFIED**ON LANDING UNDER 60 KIAS, TIRE FAILURE. TAXIED OFF RUNWAY AND STOPPED. #10 TIRE PRESSURE 0.R&R #10 TIRE DUE TO TIRE BLOW OUT IAW MD11 AMM 32-41-01 PB 401. P/N ON & OFF MD11MN. S/N Nov 20, 2021 · N259UP · Doug MD11F · Brake Anti-Skid SectionSDR IPXA2021110175497Pipe · rupturedINSPECTION TYPE:3CAPPX. 250 MILES FROM SDF DURING DECENT AP1 DISCONNECTED AND WE RECEIVED A LEVEL 1 HYD. 2 OFF ALERT, HYD 2 QUANATY WAS 2.6 GALLONS, REDUCED TO 2.1 DURING APPROACH.REMOVED AND REPLACED HYD. PRESSURE LINE IN L/H W/W, LEAK CHECK IS GOOD REF. AMM Oct 31, 2021 · N259UP · Doug MD11F · Hydraulic Power SystemSDR IPXA2021102975442None · noneINSPECTION TYPE:N/A**SUPPLEMENTAL SDR OPEN** L-1 DOOR ALERT OPES'T SHOWS CLOSED ON SECONDARY DISPLAY. DEFERRED PER MEL 52-40-1-1-0-1 STICKER INSTALLED. TRANSFERRED TO NRC 458794CHK & INSPECT L-1 DOOR FOUND BROKEN SUPPORT BACKET ASSY, R & R SUPPORT BACKET ASSY Oct 28, 2021 · N259UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2021102675335None · crackedINSPECTION TYPE:3CVERTICAL STABILIZER #4 BANJO FITTING R/H SIDE IS CRACKED.REPAIRED CRACKED VERTICAL STABILIZER #4 BANJO FITTING R/H SIDE IAW VT-SAA EA 011-5530-01-A9386 REV. I/R AND UPS EO MD11-5530-81955-A. (MAJOR) REF FAA FORM 8100-9 BY J. TOM (AR-605565) DOct 13, 2021 · N259UP · Doug MD11F · Vertical StabilizerSDR IPXA2021101975115Angle · corrodedINSPECTION TYPE:3C#2 PYLON SPAR ANGLE IS CORRODED AT STA. YID= 380.310 & ZID= 54.5.REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG. AVB7510 AND SRM 51-33-01. (MINOR)Oct 4, 2021 · N259UP · Doug MD11F · Standard Practices/StructuresSDR IPXA2021102575296Longeron · noneINSPECTION TYPE:3CMAIN CABIN LONGERON 11L CRACK BETWEEN STA.1331 AND STA.1361.REPAIRED CRACKED LONGERON 11L BETWEEN STA.1331 AND STA. 1361 IAW VT-SAA EA 011-5310-01-A9397 REV I/R AND UPS EO MD11-5310-81923-A (MAJOR) REF. FAA FORM 8100-9 BY S.KANG (AR-605677) DSep 26, 2021 · N259UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2021102075157Cap · noneINSPECTION TYPE:3CR/H WING REAR SPAR LWR CAP SUPPORT IS CORRORED AT STA-390.REMOVE, FABRICTED AND REPLACED CORRORED LWR CAP SUPPORT IAW DWG ARC3102 AND MD-11 SRM 51-33-01. (MINOR)Sep 25, 2021 · N259UP · Doug MD11F · Wing Main, Frame StructureSDR IPXA2021102675341Stringer · crackedINSPECTION TYPE:3CCENTER WIN TANK STRINGER #41 IS CRACKED AT SGTA. XCW= -81.REPAIRED CRACKED CENTER WING TANK STRINGER #41 BETWEEN STA. XCW= -69 TO XCW= -112 IAW VT-SAA EA 011-5710-01-A9389 REV. I/R AND UPS EO MD11-5710-81811-A. (MAJOR) REF FAA FORM 8100-9 BY Sep 23, 2021 · N259UP · Doug MD11F · Wing Main, Frame StructureSDR IPXA2021102275213Skin · chafedINSPECTION TYPE:3CR/H WING FIXED LE SKIN UPPER SURFACE FOUND MULTIPLE CHAFE DAMAGED BETWEEN STA XOS 832 TO STA XOS 889.REPAIRED CHAFE SKIN ON R/H FIXED L/E BETWEEN STA XOS 832 TO STA XOS 889 IAW VT-SAA EA 011-5730-01-A9394 REV I/R AND UPS EO MD11-5730-81868-A Sep 23, 2021 · N259UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2021102275204Stringer · crackedINSPECTION TYPE:3CCENTER UPPER AUX TANK STRINGER 42 HAS CRACKS BEWTEEN STA XCW=28.70 AND XCW=-57.REPAIRED CRACKED STRINGER 42 BEWTEEN STA XCW=28.70 AND XCW=-57 IAW DWG APB7471-1 AND MD-11 SRM 57-10-03 REPAIR 1 FIGURE201 REV 68. (MAJOR)Sep 23, 2021 · N259UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2021100774706Stringer · crackedINSPECTION TYPE:3CCENTER WING UPPER AUX TANK STRINGER 47 BETWEEN XCW 5.5 & XCW 28.5 IS CRACKED.REPAIRED CRACKED CENTER WING UPPER AUX TANK STRINGER 47 BETWEEN XCW 5.5 & XCW 28.5 IAW SRM 57-10-03, REPAIR 1, FIGURE 201. (MAJOR)Sep 23, 2021 · N259UP · Doug MD11F · Wing Main, Frame Structure
Back to N259UP, cancelled Feb 20, 2026