# Service difficulty reports: N254UP

A list on [N254UP](https://openairdocs.org/aircraft/N254UP.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 7 · 345 reports

- [SDR IPXA2025080145238](https://openairdocs.org/sdr/IPXA2025080145238.md): Proximity Sensor · faulted · Aug 1, 2025 · N254UP · Doug MD11F · Landing Gear Position and Warning
  > DESCENDING THROUGH 17000 W/SPEED EXTENDED, THE RIGHT GEAR HANDLE RED WARNING LIGHT CAME ON,AND STAYED ON. RE-ADJUSTED RH MLG GEAR UP AND DOOR LATCHED PROXIMITY SENSOR IAW AMM 32-61-15. PERFORMED BITE TEST IAW AMM 32-61-15-741-802. TEST GOOD.
- [SDR IPXA2025070795201](https://openairdocs.org/sdr/IPXA2025070795201.md): Skin · cracked · Jun 24, 2025 · N254UP · Doug MD11F · Wing, Plate/Skin
  > LEFT WING / FOUND CRACKED LE SKIN AT SLAT TRACK #14. 040-28, ATA 51-00.HFEC SURFACE INSP. (ASST.#20-1204, CAL. DUE: 12/11/25) OF LH WING LE SKIN AT SLAT TRACK #14 CUTOUT PER NDT SPM 06-10-01.001. CRACK DETECTED AT IB EDGE OF TRACK CUTOUT TO NEAR EDGE AFT.FABR
- [SDR IPXA2025070534130](https://openairdocs.org/sdr/IPXA2025070534130.md): Fuel Tank · corroded · Jun 20, 2025 · N254UP · Doug MD11F · Fuel Storage
  > FOUND CORROSION AT FUEL TANK UPPER SKIN M. CABIN STA 1239 XCW=-81.00 ATA 53-10.REMOVED 6EA FASTENERS AND REMOVED CORROSION AT FUEL TANK UPPER SKIN M. CABIN STA. 1239 XCW=-81.00 PER MD11 SRM 57-10-01-1A-1 FIG. 101. ACCOMPLISHED ON E.A.# 011-5730-01-B0525 REV. P
- [SDR IPXA2025070734130](https://openairdocs.org/sdr/IPXA2025070734130.md): Fuel Tank · corroded · Jun 20, 2025 · N254UP · Doug MD11F · Fuel Storage
  > FOUND CORROSION AT FUEL TANK UPPER SKIN M. CABIN STA 1239 XCW=-81.00 ATA 53-10 VERIFIED STEP 27 VERIFIED REPAIR ACCOMPLISHED IN ACCORDANCE WITH EO-94206-REQ1 AND VT-SAA EA 011-5730-01-B0525 REV IR
- [SDR IPXA2025070873830](https://openairdocs.org/sdr/IPXA2025070873830.md): Doubler · cracked · Jun 17, 2025 · N254UP · Doug MD11F · Wing Main, Frame Structure
  > RIGHT WING LE COVE HAS A CRACKED BEADED DOUBLER AT APPROX XOS=740.8 TO XOS=734.75 49-075. CUT OUT DAMAGED BEADED DOUBLER AT RH WING LE AT APPROX STA XORS 633 IAW MD-11 SRM 57-40-02-2R-15 REPAIR 15 DIMENSIONS CUT OUT 12.25" X 6.2".LOCATED AND DRILLED BEADED DO
- [SDR IPXA2025070771804](https://openairdocs.org/sdr/IPXA2025070771804.md): Seat Track · cracked · Jun 17, 2025 · N254UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO SEAT TRACK CRACKED AT BOTTOM SIDE VEIWED FROM CENTER CARGO STA 1681 LBL 8.5. FABRICATED 2 EA SEAT TRACK SPLICES REPAIR REF SRM 53-00-52-2R-1.FABRICATED 2EA REPAIR SPLICE PLATES REF SRM 53-00-52-2R-1. INSTALLED EWIS AT MAIN CARGO STA 1681 LBL8.5 RE
- [SDR IPXA2025070751852](https://openairdocs.org/sdr/IPXA2025070751852.md): Longeron Splice · corroded · Jun 16, 2025 · N254UP · Doug MD11F · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND AT CENTER CARGO BLIGE AREA RH LONGERON 48 SPLICE BETWEEN STA 5-53 TO 5-73. REMOVED DAMAGE SPLICE FROM CTR CGO BLIGE AREA RH LONGERON 48 BETWEEN STA 5-53 TO 5-73 IAW SRM 51-33-01. FABRICATED SPLICE PN AEA7653-1SAAU FOR LONGERON 48 RT CTR CARGO
- [SDR IPXA2025070742098](https://openairdocs.org/sdr/IPXA2025070742098.md): Beam · cracked · Jun 16, 2025 · N254UP · Doug MD11F · Fuselage Main, Structure
  > RIGHT OVER WING DOOR HAS A CRACK BEAM P/N ADA3750-1. REMOVED THE DAMAGED DOOR BEAM ON R-3 OVERWING DOOR REF SRM 51-33-01-0G-0 AND SRM 51-35-01-0G-0.FABRICATED BEAM EA011-5212-01-B0519-1 FOR RT WING DOOR, PLATE WITH 10% PART THICKNESS IN ALL DIRECTIONS WHILE
- [SDR IPXA2025070835259](https://openairdocs.org/sdr/IPXA2025070835259.md): Intercostal · cracked · Jun 15, 2025 · N254UP · Doug MD11F · Fuselage Miscellaneous Structure
  > STR- RH A/C BAY HAS A CRACKED INTERCOSTAL JUST AFT OF A/C BAY DOOR APPROX STRINGER S31. <BR>49-032 ATA 53-00.REMOVED INTERCOSTAL AT A/C R/H COMP APPROX STRINGER S31 REF MD11 SRM 51-35-01 AND 51-33-01.FABRICATED INERCOSTAL WEB PN ACA3804-27SAAU FOR RH AC BAY DO
- [SDR IPXA2025040275223](https://openairdocs.org/sdr/IPXA2025040275223.md): Stick Shaker · inoperative · Apr 1, 2025 · N254UP · Doug MD11F · Stall Warning System
  > **ATB** CAPT/S STICK SHAKER, PLI SHOWING STALL FO STICK SHAKER PLI NORMAL. REMOVED AND REPLACED #1 AOA VANE PER AMM 27-35-02. OPS CHECK NORMAL.
- [SDR IPXA2025012221486](https://openairdocs.org/sdr/IPXA2025012221486.md): Handle · out of position · Jan 22, 2025 · N254UP · Doug MD11F · Passenger/Crew Doors
  > L1 EXTERNAL DOOR HANDLE ROTATED TO THE EMERGENCY POSITION BY DE-ICE EMPLOYEE. DOOR IS STUCK IN THE PARTIALLY OPENED POSITION. DOOR HANDLE STUCK IN THE EMERGENCY POSITION. RESET L1 DOOR PNEUMATIC SYSTEM IAW AMM 52-11-04-700-801.<BR>SERVICED L1 DOOR PNEUMATIC BO
- [SDR IPXA2024112792263](https://openairdocs.org/sdr/IPXA2024112792263.md): Skin · dented · Nov 25, 2024 · N254UP · Doug MD11F · Passenger/Crew Doors
  > ENTRY DOOR DENT/BENT TOP LEFT APPROX. 2 1/4 IN BY 1 1/4 IN. INSTALLED L1 DOOR IAW AMM 52-11-02. OPS CHECK GOOD. DOOR SLIDE PIN REMOVED AND STOWED.
- [SDR IPXA2024112692263](https://openairdocs.org/sdr/IPXA2024112692263.md): Skin · dented · Nov 25, 2024 · N254UP · Doug MD11F · Passenger/Crew Doors
  > ENTRY DOOR DENT/BENT TOP LEFT APPROX. 2 1/4 IN BY 1 1/4 IN
- [SDR IPXA2024102909839](https://openairdocs.org/sdr/IPXA2024102909839.md): Battery · no test · Oct 28, 2024 · N254UP · Doug MD11F · Emergency Lighting
  > LOW LVL 1EMERGANCYLT BATTERY LOW WON€™T PASS TEST PERFORMED OPS CHECK PER AMM: 33-51-01, NO FAULT
- [SDR IPXA2024102286629](https://openairdocs.org/sdr/IPXA2024102286629.md): Battery · discharged · Oct 22, 2024 · N254UP · Doug MD11F · Emergency Lighting
  > LVL1 EMERGENCY LT BAT LOW ON PREFLIGHT R/R EMERGENCY POWER SUPPLY BATTERY REF AMM 33-51-01. OPS CHECK GOOD. REVERSED DMP. REMOVED PLACARD. THIS CLEARS DEFERRAL.
- [SDR IPXA2024092129171](https://openairdocs.org/sdr/IPXA2024092129171.md): Battery Pack · inoperative · Sep 21, 2024 · N254UP · Doug MD11F · Escape Slide
  > L1 EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST INDICATOR NOT ILLUMINATING. REMOVED AND REPLACED BATTERY AND LIGHT BULBS IAW AMM 25-61-04. OPS. CHECK GOOD. THIS CLEARS DEFERRAL.PLACARD REMOVED. NO DISABLING DMP APPLIED.
- [SDR IPXA2024091007025](https://openairdocs.org/sdr/IPXA2024091007025.md): Slide · unsecure · Sep 10, 2024 · N254UP · Doug MD11F · Escape Slide
  > CREW ENTRY L1 DOOR EVACUATION SLIDE NOT SECURED. COMPLETED L1 EVACUATION SLIDE INSTALL REF AMM 25-62-02-400 THIS CLEARS MEL PLACARD REMOVED
- [SDR 2024F00181](https://openairdocs.org/sdr/2024F00181.md): Door Frame · cracked · Jul 31, 2024 · N254UP · Doug MD11F · Fuselage Main, Plate/Skin
  > UPPER LEFT CORNER AFT PACK NO.3 ACCESS 114AR VISUAL CRACK FOUND APPROX..75 IN PICS ATTACHED. VERIFIED ALL INSP STEPS COMPLIED WITH ON EO-90589-PRELIM1 RIGHT-SIDE AIR-CONDITIONING DOOR JAMB CORNER SKIN CRACK- PRELIMINARY REPAIR NO. 1
- [SDR IPXA2024030591110](https://openairdocs.org/sdr/IPXA2024030591110.md): Battery · discharged · Mar 5, 2024 · N254UP · Doug MD11F · Emergency Lighting
  > EMERG LIGHTS BATT 1 LO R/R EMERG POWER SUPPLY BATTERY PER AMM33-51-01-400-802 OPS CHECKS GOOD
- [SDR IPXA2023121528319](https://openairdocs.org/sdr/IPXA2023121528319.md): Unknown · unknown · Dec 15, 2023 · N254UP · Doug MD11F · Fuselage Miscellaneous Structure
  > *SDR FILED OPEN* CENTER PIT CEILING DAMAGE, UPPER GILLINER ATTACH ANGLE INBOARD OF THE FWD DOOR ACTUATOR ARM. INSTALLED CTR CARGO COMPT CEILING LINER IAW AMM 25-56-07
- [SDR IPXA2023083194060](https://openairdocs.org/sdr/IPXA2023083194060.md): Cover · missing · Aug 30, 2023 · N254UP · Doug MD11F · Emergency Lighting
  > INSPECTION TYPE:NAR1 DOOR EMERGENCY LT COVER MISSING ABOVE GALLEY.INSTALLED GROMMETS AND BEZEL ADDY REF IPC 33-52-55-01-05,20.
- [SDR IPXA2023071093629](https://openairdocs.org/sdr/IPXA2023071093629.md): Aileron Sys · warning message · Jul 9, 2023 · N254UP · Doug MD11F · Aileron Control System
  > INSPECTION TYPE:NA*SDR FILED OPEN* *ATB* EMERGENCY DECLARED* AFT START CONFIGURED ACFT & RCVD LVL 2 AIL DEFLECT DISAG MSG RAN CK LIST & SYS RESET AFT TKOFF MSG RTRND FO SLATED AC WANTED TO ROLL LEFT BUT MAINTAINED ACFT CONTROL RAN CK LIST AND LIGHT REMAINED IL
- [SDR IPXA2023062693523](https://openairdocs.org/sdr/IPXA2023062693523.md): Spar · corroded · Jun 26, 2023 · N254UP · Doug MD11F · Wing Spar
  > INSPECTION TYPE:C3CORROSION FOUND R/WING ON LOWER SPAR CAP VERTICAL FLANGE STA XW 486REMOVED CORROSION AND REPAIRED IAW VT-SAA EA 011-5710-01-A9978 I/R AND UPS EO MD11-5710-87379-A. MINOR REPAIR
- [SDR IPXA2023062893530](https://openairdocs.org/sdr/IPXA2023062893530.md): Seat Track · corroded · Jun 16, 2023 · N254UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C3*MAJOR REPAIR* MAIN CABIN SEAT TRACK AT STA Y=6.70 AND Y=6.80, X=27.50 HAS CORROSION.REPAIRED CORRODED SEAT TRACK AT THE MAIN CABIN STA Y=6.70 AND STA Y=6.80, X=27.50 IAW 53-00-52-2R FIG 201 REPAIR 1. (MAJOR)
- [SDR IPXA2023062893534](https://openairdocs.org/sdr/IPXA2023062893534.md): Tee Angle · cracked · Jun 14, 2023 · N254UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3CR/H WING O/B FLAP O/B HINGE LWR TEE SUPPORT ANGLE IS CRACKED.REPLACED CRACKED TEE AT THE R/H WING O/B FLAP O/B HINGE LWR SUPPORT ANGLE IAW SRM 51-31-01 (MINOR)
- [SDR IPXA2023063093551](https://openairdocs.org/sdr/IPXA2023063093551.md): Hinge · corroded · Jun 13, 2023 · N254UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3CL/H WING A/C SIDE O/B FLAP I/B HINGE #3 LUG BORE HAS CORROSION ATSTA XW=486.403.REPAIRED CORRODED HINGE ASSY. #3 LUG BORE AT THE L/H WING A/C SIDE O/B FLAP I/B HINGE AT STA XW=486.403 IAW VTSAA EA 011-5710-01-A9987 I/R AND UPS EO MD11-5740-87
- [SDR IPXA2023062693516](https://openairdocs.org/sdr/IPXA2023062693516.md): Splice · unknown · Jun 13, 2023 · N254UP · Doug MD11F · Fuselage Structure (General)
  > INSPECTION TYPE:3C*MAJOR REPAIR* FOUND EXISTING REPAIR SPLICE FITTING AT STA Y=6-80 LONGERON 46L WITH NO HISTORY.REPLACED EXISTING REPAIR SPLICE FITTING AT STA Y= 6-80 LONGERON 46L IAW SRM 53-00-05 FIG 201 REPAIR 1. (MAJOR)
- [SDR IPXA2023062893535](https://openairdocs.org/sdr/IPXA2023062893535.md): Hinge · corroded · Jun 9, 2023 · N254UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3CR/H WING A/C SIDE O/B FLAP O/B HINGE #2 LUG BORE HAS CORROSION AT STA XW=-638.305.REPAIRED CORRODED #2 LUG BORE AT THE R/H WING A/C SIDE O/B FLAP O/B HINGE AT STA XW=-638.305 IAW VTSAA EA 011-5710-01-A9985 I/R AND UPS EO MD11-5740-87383-A DAT
- [SDR IPXA2023062893536](https://openairdocs.org/sdr/IPXA2023062893536.md): Hinge · corroded · Jun 9, 2023 · N254UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3CR/H WING A/C SIDE O/B FLAP O/B HINGE #3 LUG BORE HAS CORROSION AT STA XW=-638.305.REPAIRED CORRODED #3 LUG BORE AT THE R/H WING A/C SIDE O/B FLAP O/B HINGE AT STA XW=-638.305 IAW VTSAA EA 011-5710-01-A9985 I/R AND UPS EO MD11-5740-87383-A DAT
- [SDR IPXA2023063093549](https://openairdocs.org/sdr/IPXA2023063093549.md): Hinge · corroded · Jun 8, 2023 · N254UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3CL/H WING O/B FLAP I/B FWD HINGE AFTER REMOVAL OF BUSHING FOUND INCOMING #1 LUG BORE OUT OF LIMITS.REPAIRED HINGE ASSY. #1 LUG BORE AT THE L/H WING O/B FLAP I/B FWD HINGE IAW VTSAA EA 011-5710-01-A9987 I/R AND UPS EO MD11-5740-87381-A DATED 06
- [SDR IPXA2023062993544](https://openairdocs.org/sdr/IPXA2023062993544.md): Longeron · corroded · Jun 6, 2023 · N254UP · Doug MD11F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:3C*MAJOR REPAIR* FOUND CORROSION UNDERNEATH OF THE END SPLICE OF LONGERON 50 R/H CTR CARGO AT STA Y=5-2.21 - Y=5-11.00.REPAIRED CORRODED LONGERON 50R AT THE R/H SIDE CTR CARGO STA Y=5-2.21 - Y=5-11.00 IAW VTSAA EA 011-5310-01-A9976 I/R AND UPS
- [SDR IPXA2023062693515](https://openairdocs.org/sdr/IPXA2023062693515.md): Longeron · corroded · Jun 4, 2023 · N254UP · Doug MD11F · Fuselage Structure (General)
  > INSPECTION TYPE:3C*MAJOR REPAIR* CAC COMP. BILGE AREA LONGERON 46L HAS CORROSION AT STA Y=6-75.REPAIRED CORRODED LONGERON 46L SECTION AT THE CAC COMP. BILGE AREA AT STA Y=6-75 IAW SRM 53-00-05 FIG 201 REPAIR 1. (MAJOR)
- [SDR IPXA2023062993545](https://openairdocs.org/sdr/IPXA2023062993545.md): Beam · cracked · Jun 3, 2023 · N254UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:3C*MAJOR REPAIR* MAIN CABIN R3 DOOR LWR HORIZONTAL BEAM FWD SIDE IS CRACKED BETWEEN STA Y=793 - Y=838.REPAIRED CRACKED HORIZONTAL BEAM AT THE MAIN CABIN R3 DOOR FWD SIDE BETWEEN STA Y=793 - Y=838 IAW VTSAA EA 011-5210-01-A9970 I/R AND UPS EO MD
- [SDR IPXA2023062093483](https://openairdocs.org/sdr/IPXA2023062093483.md): Web · cracked · Jun 3, 2023 · N254UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C3MAIN CABIN R/H FLOOR WEB IS CRACKED AT STA 1986.REMOVED, FABRICATED AND REPLACED CRACKED FLOOR WEB IAW SRM 51-35-01 AND DWG AGA7145. (MINOR)
- [SDR IPXA2023062093488](https://openairdocs.org/sdr/IPXA2023062093488.md): Skin · corroded · Jun 3, 2023 · N254UP · Doug MD11F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:3CEMPENNAGE R/H FUSELAGE BODY FAIRING SKIN HAS SURFACE CORROSION AT STA 1941-2122.REPAIRED CORRODED SKIN AT THE EMPENNAGE R/H FUSELAGE AREA AT STA 1941-2122 IAW SRM 51-21-01 DWG AJC7060. (MINOR)
- [SDR IPXA2023062093486](https://openairdocs.org/sdr/IPXA2023062093486.md): Tee Fitting · cracked · Jun 3, 2023 · N254UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:3CUPPER CENTER AUXILIARY TANK FWD BULKHEAD TEE BRACKET IS CRACKED BETWEEN STA XCW=46 AND XCW=81.REMOVED, FABRICATED AND REPLACED CRACKED TEE BRACKET AT THE UPPER CENTER AUXILIARY TANK FWD BULKHEAD BETWEEN STA XCW=46 AND XCW=81 IAW SRM 51-33-01
- [SDR IPXA2023061693454](https://openairdocs.org/sdr/IPXA2023061693454.md): Stringer · cracked · Jun 3, 2023 · N254UP · Doug MD11F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:3C*MAJOR REPAIR* UPPER CENTER AUXILIARY TANK HAS A CRACKED EXISTING REPAIR BETWEEN STA XCW=-17 AND XCW=-46.REPAIRED CRACKED EXISTING REPAIR AT THE UPPER CENTER AUXILIARY TANK BETWEEN STA XCW=-17 AND XCW=-46 IAW SRM 57-10-03 FIG 201 REPAIR 1. (
- [SDR IPXA2023063093553](https://openairdocs.org/sdr/IPXA2023063093553.md): Hinge · corroded · Jun 2, 2023 · N254UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3CL/H WING A/C SIDE O/B FLAP O/B HINGE #3 LUG BORE HAS CORROSION AT STA XW=638.305.REPAIRED CORRODED HINGE ASSY. #3 LUGE BORE AT THE L/H WING A/C SIDE O/B FLAP O/B HINGE AT STA XW=638.305 IAW VTSAA EA 011-5740-01-A9986 I/R AND UPS EO MD11-5740-
- [SDR IPXA2023063093552](https://openairdocs.org/sdr/IPXA2023063093552.md): Hinge · corroded · Jun 2, 2023 · N254UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3CL/H WING A/C SIDE O/B FLAP I/B HINGE #2 LUG BORE HAS CORROSION AT STA XW=486.403.REPAIRED HINGE ASSY. #2 LUG BORE AT THE L/H WING A/C SIDE O/B FLAP I/B HINGE AT STA XW=486.403 IAW VTSAA EA 011-5710-01-A9987 I/R AND UPS EO MD11-5740-87381-A DA
- [SDR IPXA2023063093555](https://openairdocs.org/sdr/IPXA2023063093555.md): Stringer · cracked · Jun 2, 2023 · N254UP · Doug MD11F · Wing, Longeron/Stringer
  > INSPECTION TYPE:3C*MAJOR REPAIR* R/H WING #3 TANK UPPER STRINGER 1 IS CRACKED BETWEEN STA XORS=1012.55 AND 1042.350.REPAIRED CRACKED STRINGER 1 AT THE R/H WING #3 TANK UPPER SIDE BETWEEN STA XORS=1012.55 AND XORS=1042.350 IAW VTSAA EA 011-5710-01-A9977 I/R AND
- [SDR IPXA2023062893533](https://openairdocs.org/sdr/IPXA2023062893533.md): Stiffener · cracked · Jun 1, 2023 · N254UP · Doug MD11F · Cargo Compartments
  > INSPECTION TYPE:3CAFT CARGO COMP STA 1841 R/H SIDE 1EA STIFFENER HAS A CRACKED.REPLACED CRACKED STIFFENER AT THE AFT CARGO COMP AT STA 1841 IAW SRM 51-33-01 (MINOR)
- [SDR IPXA2023062893532](https://openairdocs.org/sdr/IPXA2023062893532.md): Angle · broken · Jun 1, 2023 · N254UP · Doug MD11F · Leading Edge Devices
  > INSPECTION TYPE:3CR/H WING FUEL QUANTITY CONTROL UNIT HAS A BROKEN O/B ATTACHMENT ANGLE.REPLACED BROKEN ANGLE AT THE R/H WING FUEL QUANTITY CONTROL UNIT ATTACHMENT IAW 51-33-01 AND DWG ARB2382. (MINOR)
- [SDR IPXA2023062693513](https://openairdocs.org/sdr/IPXA2023062693513.md): Splice · corroded · Jun 1, 2023 · N254UP · Doug MD11F · Fuselage Structure (General)
  > INSPECTION TYPE:3CCTR CARGO BILGE AREA AT STA Y=1701 - Y=1721 SPLICE ON LONGERON 52 HAS CORROSION.REPAIRED CORRODED SPICE AT THE CTR CARGO BILGE AREA AT STA Y=1701 - Y=1721 ON LONGERON 52 IAW SRM 51-33-01 AND DWG AFA7102. (MINOR)
- [SDR IPXA2023062093485](https://openairdocs.org/sdr/IPXA2023062093485.md): Angle · corroded · Jun 1, 2023 · N254UP · Doug MD11F · Fuselage Structure (General)
  > INSPECTION TYPE:3CCTR CARGO STA 1721-1741 LONGERON 52 INTERCOSTAL WEB ANGLE SUPPORT HAS CORROSION.REMOVED, FABRICATED AND REPLACED THE CORRODED SUPPORT TEE AT THE CTR CARGO STA 1721-1741, LONGERON 52 IAW SRM 51-33-01 AND DWG ACA7673. (MINOR)
- [SDR IPXA2023061693455](https://openairdocs.org/sdr/IPXA2023061693455.md): Spar Cap · corroded · May 31, 2023 · N254UP · Doug MD11F · Wing Spar
  > INSPECTION TYPE:C3*MAJOR REPAIR* R/H WING REAR SPAR AREA ABOVE O/B FLAP O/B HINGE FITTING HAS CORROSION BETWEEN STA XORS=724 AND XORS=730.REPAIRED CORRODED R/H WING REAR SPAR AREA ABOVE O/B FLAP O/B HINGE FITTING BETWEEN STA XORS=724 AND XORS=730 IAW VTSAA EA
- [SDR IPXA2023062093484](https://openairdocs.org/sdr/IPXA2023062093484.md): Stiffener · cracked · May 30, 2023 · N254UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:3CVERTICAL STIFFENER FROM FRONT OF R/H WHEEL WELL AFT CUTOUT IS CRACKED.REMOVED, FABRICATED AND REPLACED CRACKED VERTICAL STIFFENER AT THE R/H WHEEL WELL AFT CUTOUT IAW SRM 51-35-01 AND DWG ANB7203. (MINOR)
- [SDR IPXA2023032792290](https://openairdocs.org/sdr/IPXA2023032792290.md): Door · inoperative · Mar 25, 2023 · N254UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION TYPE:NAL1 "DOOR DISARM') LIGHT SWITCH BROKENREMOVED & REPLACED LENS ASSY IAW MD11 AMM 20-30-10
- [SDR IPXA2023032492198](https://openairdocs.org/sdr/IPXA2023032492198.md): Door · inoperative · Mar 23, 2023 · N254UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION TYPE:NADOOR 1R DISARM LIGHT INOP.SECURED DISARM LIGHT IAW AMM, 52-10-00.
- [SDR IPXA2022112288349](https://openairdocs.org/sdr/IPXA2022112288349.md): Girt Bar · out of position · Nov 21, 2022 · N254UP · Doug MD11F · Emergency Equipment
  > L1 ENTRY DOOR WILL NOT ARM PHYSICAL BLOCK, WHEN TRYING TO MOVE ARMING LEVER AFTER CLOSING. FOUND GORT BAR OUT OF POSITION REST REF AMM 52 10 01
- [SDR IPXA2022110887971](https://openairdocs.org/sdr/IPXA2022110887971.md): Door · malfunctioned · Nov 7, 2022 · N254UP · Doug MD11F · Passenger/Crew Doors
  > UNABLE TO ARM L1 DOOR AFTER CLOSING REPOSITIONED QIRT BW ON L1 DOOR OPENED THE SEVERAL CYCLES REF MD11 MM 25-61-01 OPENEDS NORMALLY

Next page: https://openairdocs.org/aircraft/N254UP/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 = 'N254UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N254UP/reports

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