# Service difficulty reports: N258UP

A list on [N258UP](https://openairdocs.org/aircraft/N258UP.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 10 · 493 reports

- [SDR IPXA2025082907090](https://openairdocs.org/sdr/IPXA2025082907090.md): Warning Message · illuminated · Aug 28, 2025 · N258UP · Doug MD11F · Fuel Indicating System
  > DIVERSION, LEVEL 2 FUEL QTY/USED CHK MESSAGE MULTIPLE TIMES IN FLIGHT WHEN FLT CREW ARRIVED THE A/C HAD 25.2 TOTAL ONBD. THE TANKS WERE WITHIN 200 LBS OF EA OTHER. PERF BITE OF FQBU & FOUND FMC FAULT FROM PREV LEG. NO CORRELATING FAULTS NOTED. CLEARED MEMORY
- [SDR IPXA2025071516005](https://openairdocs.org/sdr/IPXA2025071516005.md): Skin · gouged · Mar 18, 2025 · N258UP · Doug MD11F · Fuselage Main, Plate/Skin
  > DENT AND GOUGE FOUND ON LEFT SIDE OF AIRCRAFT AT STATION 1794.5, JUST ABOVE STRINGER 8. REMOVED THREE FASTENERS IN BLEND OUT AREA PER ENGINEERING REQUEST. TAPE AND MEASUREMENTS AT AFFECTED LOCATION REF [T3F18E006A182] ALL STEPS OF EO-93108-REQ3 COMPLETED ON SH
- [SDR IPXA2025012887953](https://openairdocs.org/sdr/IPXA2025012887953.md): Panel · dented · Jan 25, 2025 · N258UP · Doug MD11F · Fuselage Main, Plate/Skin
  > FOUND ON WAI DENT RH LOWER FUSELAGE FWD OF FWD LOWER CARGO DOOR OPERATING SWITCH PANEL DEFERED PER EO-92626-REQ1. OPEN
- [SDR IPXA2025012581071](https://openairdocs.org/sdr/IPXA2025012581071.md): Bottle · low · Jan 25, 2025 · N258UP · Doug MD11F · Escape Slide
  > R1 DOOR SLIDE LOW PRESSURE. VERIFIED SAFETY PIN REMOVED AND GIRTH BAR ENGAGED REF AMM 26-61-15.
- [SDR IPXA2024123016142](https://openairdocs.org/sdr/IPXA2024123016142.md): Handle · inoperative · Dec 20, 2024 · N258UP · Doug MD11F · Emergency Equipment
  > L1 DOOR WOULD NOT ARM SLIDE DURING MEL APPLICATION ATTEMPTED TO RESEAT DOOR, DOOR WOULD NOT CLOSE AFTER SLIDE WILLL NOT ARM DOOR OPEN. L1 DOOR DEFERRED PER MEL 52-10-3-1-2-1-2.
- [SDR IPXA2024122114951](https://openairdocs.org/sdr/IPXA2024122114951.md): Cable · failed · Dec 20, 2024 · N258UP · Doug MD11F · Passenger/Crew Doors
  > L1 DOOR CABLE SNAPPED. PERFORMED OPS CHK AT L1 DOOR IAW AMM 52-11-02, OPS CHK GOOD. REMOVED PLACARD THIS CLEARS DEFERRAL.
- [SDR IPXA2024122016142](https://openairdocs.org/sdr/IPXA2024122016142.md): Door · faulted · Dec 20, 2024 · N258UP · Doug MD11F · Passenger/Crew Doors
  > **SDR FILED OPEN**L1 DOOR WOULD NOT ARM SLIDE DURING MEL APPLICATION ATTEMPTED TO RESEAT DOOR, DOOR WOULD NOT CLOSE AFTER SLIDE WILLL NOT ARM DOOR OPEN. L1 DOOR DEFERRED PER MEL 52-10-3-1-2-1-2 ON BARCODE T3F18E005SQSU.
- [SDR IPXA2024110861381](https://openairdocs.org/sdr/IPXA2024110861381.md): Support Rod · chafed · Oct 10, 2024 · N258UP · Doug MD11F · Fuselage Main, Structure
  > APG, LEFT SIDE OVERWING FLOOR BEAM SUPPORT ROD AT STA 1275 X81 HAS SURFACE CORROSION AND IS CHAFFING ON UPPER BRACKET. SAA034 038 ATA 53-14.REMOVED 1EA BRACKET AND SUPPORT ROD AT LEFT SIDE OVERWING FLOOR BEAM SUPPORT ROD AT STA 1275 X81 IN REF MD11 SRM 51-31
- [SDR IPXA2024110861320](https://openairdocs.org/sdr/IPXA2024110861320.md): Floorbeam · chafed · Oct 10, 2024 · N258UP · Doug MD11F · Fuselage Main, Floor Beam
  > APG, LEFT SIDE OVERWING FLOOR BEAM SUPPORT ROD AT STA 1293 X81 HAS SURFACE CORROSION AND IS CHAFFING ON UPPER BRACKET. SAA034 037 ATA 53-14.REMOVED 1EA BRACKET AND SUPPORT ROD AT LEFT SIDE OVERWING FLOOR BEAM SUPPORT ROD AT STA 1293 X81 IN REF MD11 SRM 51-31
- [SDR IPXA2024110261392](https://openairdocs.org/sdr/IPXA2024110261392.md): Floor Support · corroded · Oct 10, 2024 · N258UP · Doug MD11F · Fuselage Miscellaneous Structure
  > LEFT SIDE OVERWING FLOOR BEAM SUPPORT ROD AT STA 1256 X81 HAS SURFACE CORROSION AND IS CHAFING ON UPPER BRACKET. SAA 039 ATA 53-14. INSTALLED FLOOR SUPPORT FITTING 1 EACH AND SUPPORT ROD 1 EACH AT LEFT SIDE OVERWING FLOOR BEAM SUPPORT ROD AT STA 1256 X81 IAW
- [SDR IPXA2024103107260](https://openairdocs.org/sdr/IPXA2024103107260.md): Skin · gouged · Oct 7, 2024 · N258UP · Doug MD11F · Wing, Plate/Skin
  > RH WING AT L/E UPPER SURFACE IS GOUGED AT APPX STA XORS 855 ATA 57-40 MARKED 84-12. REPAIR ACCOMPLISHED IAW: SRM 57-40-02-2R-3 REPAIR 3 (REV 71).
- [SDR IPXA2024102307597](https://openairdocs.org/sdr/IPXA2024102307597.md): Skin · gouged · Oct 7, 2024 · N258UP · Doug MD11F · Leading Edge Devices
  > LEFT WING O/B SLAT #3 TRAILING EDGE HAS GAULGE ABOVE SLAT TRACK #7. ATA 57-20 RD07 ACCOMPLISHED REPAIR PER EO-91801-REQ1 (VT-SAA EA 011-2780-01-B0297)
- [SDR IPXA2024102982061](https://openairdocs.org/sdr/IPXA2024102982061.md): Slide · unknown · Oct 5, 2024 · N258UP · Doug MD11F · Escape Slide
  > APG - NEED TO REPACK R1 DOOR EVACUATION SLIDE. INSTALLED EMERGENCY EVACUATION SLIDE ON R1 DOOR PER. MD-11 AMM 25-61-01-400-801. REVIEWED.
- [SDR IPXA2024100782061](https://openairdocs.org/sdr/IPXA2024100782061.md): Slide · unpacked · Oct 5, 2024 · N258UP · Doug MD11F · Escape Slide
  > *SDR FILED OPEN* APG - NEED TO REPACK R1 DOOR EVACUATION SLIDE ATA 25-61
- [SDR IPXA2023090794115](https://openairdocs.org/sdr/IPXA2023090794115.md): Battery · inoperative · Sep 7, 2023 · N258UP · Doug MD11F · Emergency Lighting
  > DURING PREFLIGHT EMER LIGHTS TEST LEVEL 1 EMER LT BAT 1 LO APPEARED. DEFERRED EMERGENCY LIGHTING SYS PER MEL 33-50-04 C/W DMP 33-50-4 PLACARD INSTALLEDR&R EMER. BATTERY, DMP REVERSED, PERFORMED OPS CHK. OPS CHK GOOD IAW 33-51-01. THIS ACTION CLEARS DEFERRAL M8
- [SDR IPXA2023072593736](https://openairdocs.org/sdr/IPXA2023072593736.md): Door · broken · Jul 25, 2023 · N258UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION TYPE:NAL1 DOOR DISARMED ANNUCIATOR BROKEN.REMOVED AND REPLACED ANNUCIATOR. OPS CHECK GOOD W/REF TO M/M 52-10-01
- [SDR IPXA2023072493713](https://openairdocs.org/sdr/IPXA2023072493713.md): Landing Gear · inoperative · Jul 22, 2023 · N258UP · Doug MD11F · Landing Gear Retraction/Extension System
  > INSPECTION TYPE:NA *** AIRTURN BACK *** L MAIN GEAR WOULD NOT COME UP ON DEPARTURE. CHKLT DID NOT GET GEAR UP. RESULTED IN ATB TO KONT NOTE: BOTH PRIMARY AND SECONDARY GEAR INDICATIONS WERE RED (UNSAFE) WITH THE GEAR HANDLE IN THE UP POSITION. BUFFET AND NOISE
- [SDR IPXA2023071993691](https://openairdocs.org/sdr/IPXA2023071993691.md): Light · inoperative · Jul 18, 2023 · N258UP · Doug MD11F · Emergency Lighting
  > EMERGENCY LIGHTS REQUIRES DEFERRAL REF ITEM 1 ABOVE. ITEM DEFERRED PER MEL 33-50-4 M 810483 ASSIGNED. PLACARD INSTALLED.L1 DOOR CEILING PANEL REPAIRED. C/W REF M810482 REACTIVATED EMERGENCY LIGHTING SYSTEM. REVERSE DMP 33-50-4 SYSTEM. OPS CHECK OK. CLEARS M810
- [SDR IPXA2023071993690](https://openairdocs.org/sdr/IPXA2023071993690.md): Door · inoperative · Jul 18, 2023 · N258UP · Doug MD11F · Passenger/Crew Doors
  > L1 DOOR REQUIRES DEFERRAL. REF ITEM 1 ABOVE. ITEM DEFERRED PER MEL 52-10-3-1-2-1-2. M810484 ASSIGNED. PLACARD INSTALLED.REF LOG PAGE 610079 ITEM 1 FOR REPAIR. L1 SLIDING CEILING PANEL REACTIVATED IAW MD-11 AMM 25-23-23-400-801. ACCOMPLISHED PERMANENT REPAIR. T
- [SDR IPXA2023071993692](https://openairdocs.org/sdr/IPXA2023071993692.md): Door · inoperative · Jul 18, 2023 · N258UP · Doug MD11F · Passenger/Crew Doors
  > L1 DOOR HAS CEILING PANEL DAMAGE. PANEL REMOVED AND REPLACED IN FPM ITEM DEFERRED PER EO MD11-2520-87659-A D 810482 ASSIGNED.ACCOMPLISHED PERMANENT REPAIR IAW MD-11 SRM 51-71-00-06-0 STEP 20 C. REACTIVATED SLIDING CEILING PANEL ASSY IAW MD-11 AMM 25-23-23-400
- [SDR IPXA2023011979980](https://openairdocs.org/sdr/IPXA2023011979980.md): Power Supply · no test · Jan 16, 2023 · N258UP · Doug MD11F · Emergency Lighting
  > EMERGENCY LIGHT BATTERY LOW ON PREFLT TEST. R & R EMERGENCY POWER LIGHTING POWER SUPPLY IAW AMM 33-51-01-400-802. OPS CHECK GOOD.
- [SDR IPXA2023011189795](https://openairdocs.org/sdr/IPXA2023011189795.md): Linkage · out of adjust · Jan 10, 2023 · N258UP · Doug MD11F · Landing Gear Steering System
  > ON LANDING ROLLOUT, UNABLE TO TAXI DUE TO NOSE WHEEL STEERING BYPASS PIN LEVER STUCK IN INTERMEDIATE POSITION. T/S AND FOUND BY-PASS LINKAGE IS OUT OF ADJUSTMENT. ADJUSTED BY-PASS LINKAGE IAW AMM 32-52-04. OPS TESTED THE STEERING BY-PASS VALVE ASSEMBLY IAW
- [SDR IPXA2022100886966](https://openairdocs.org/sdr/IPXA2022100886966.md): Hinge Fitting · corroded · Oct 8, 2022 · N258UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3CLH INBD FLAP FWD HINGE FITTING #3 LUG OTBD FACE HAS PITTINGACCOMPLISHED REPAIR ON LH INBD FLAP FWD HINGE FITTING #3 LUG OTBD FACE PER VT EA#011-5740-01A9716 REV I/R AND UPS EO MD11-5740-84883-A
- [SDR IPXA2022100886965](https://openairdocs.org/sdr/IPXA2022100886965.md): Hinge Bracket · corroded · Oct 8, 2022 · N258UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3CLH INBD FLAP AFT HINGE FITTING #7 LUG HOLE IS GOUGEDACCOMPLISHED REPAIR ON LH INBD FLAP OTBD HINGE BRACKET ASSY #7 LUG HOLE PER VT SAA EA#011-5740-01-A9720 I/R AND UPS EO MD11-5740-84955-A
- [SDR IPXA2022100886964](https://openairdocs.org/sdr/IPXA2022100886964.md): Hinge Bracket · corroded · Oct 8, 2022 · N258UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3CLH INBD FLAP AFT HINGE FITTING #6 LUG HOLEIS GOUGED. ACCOMPLISHED REPAIR ON LH INBD FLAP OTBD HINGE AFT OTBD HINGE BRACKET PER VT SAA EA#011-5740-01-A9720 REV I/R AND UPS EO MD11-5750-84955-A
- [SDR IPXA2022100886963](https://openairdocs.org/sdr/IPXA2022100886963.md): Hinge · corroded · Oct 8, 2022 · N258UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3CLH INBD FLAP FWD ING FITTING #3 LUG INBD FACE HAS PITTINGACCOMPLISHED REPAIR ON LH INBD FLAP OTBD FWD HINGE ASSY PER VT SAA EA#011-5740-01-A9716 REV I/R AND UPS EO MD11-5740-84883-A
- [SDR IPXA2022100886949](https://openairdocs.org/sdr/IPXA2022100886949.md): Hinge · corroded · Oct 8, 2022 · N258UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3CRH INBD FLAP HINGE FITTING #3 LUG INBD FACE HAS PITTINGACCOMPLISHED REPAIR ON RH INBD FLAP OTBD FWD HINGE ASSY INBD AND OTBD LUG FACE PER VT SAA EA#011-5740-01-A9717 REV I/R AND UPS EO MD11-5740-84884-A.
- [SDR IPXA2022100586875](https://openairdocs.org/sdr/IPXA2022100586875.md): Longeron · corroded · Oct 5, 2022 · N258UP · Doug MD11F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:3CCENTER CARGO COMPARTMENT BILGE AREA STA 1691 LONGERON 48L HAS CORROSIONACCOMPLISHED REPAIR ON CENTER CARGO COMPARTMENT LONGERON 48L STA 1691 PER VT SAA EA#011-5310-01-A9691 REV I/R AND UPS EO MD11-5310-84725-A
- [SDR IPXA2022100586873](https://openairdocs.org/sdr/IPXA2022100586873.md): Bushing · migrated · Oct 5, 2022 · N258UP · Doug MD11F · Wing Main, Frame Structure
  > INSPECTION TYPE:3C, LH INBD FLAP INBD TRACK UPPER ACTUATOR MOUNT FITTING OTBD LUG BUSHING IS MIGRATED. ACCOMPLISHED REPAIR ON LH WING INBD FLAP DRIVE LEVER ASSY UPPER TBD LUG PER VT SAA EA#011-5700-01-A9713 REV I/R AND UPS EO MD11-5740-84885-A
- [SDR IPXA2022092986722](https://openairdocs.org/sdr/IPXA2022092986722.md): Longeron · corroded · Sep 29, 2022 · N258UP · Doug MD11F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:3CCENTER CARGO COMP BILGE AREA STA 1526 LONGERON 43L HAS CORROSIONACCOMPLISHED REPAIR ON CENTER CARGO COMPARTMENT LONGERON 43L PER VT SAA EA# 011-5310-01-A9690 I/R AND UPS EO MD11- 5310-84692-A
- [SDR IPXA2022092986700](https://openairdocs.org/sdr/IPXA2022092986700.md): Door Frame · gouged · Sep 28, 2022 · N258UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:CUPPER DECK COMP MCD AFT FRAME HAS A GOUGE AND DENT AT MID LOCATIONREMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW EA# 011-5230-01-A9701, UPS EO # MD11-5230-84795-A
- [SDR IPXA2022092786654](https://openairdocs.org/sdr/IPXA2022092786654.md): Skin · corroded · Sep 27, 2022 · N258UP · Doug MD11F · Rudder, Plate/Skin
  > INSPECTION TYPE:3CUPPER RUDDER LOWER ROUND ACCESS AREA HAS CORROSION ON LIP AND SKINREMOVED AND REPLACED ASSY UPPER AFT RUDDER PER MD11 AMM 27-20-30
- [SDR IPXA2022092786653](https://openairdocs.org/sdr/IPXA2022092786653.md): Former · cracked · Sep 27, 2022 · N258UP · Doug MD11F · Wing Main, Frame Structure
  > INSPECTION TYPE:3CCRACKED FORMER AT LH WING L/E STA XOS584ACCOMPLISHED REPAIR ON LH WING L/E FORMER AT STA XOS 584 PER MD11 SRM 57-00-00 FIG 204
- [SDR IPXA2022091786336](https://openairdocs.org/sdr/IPXA2022091786336.md): None · cracked · Sep 17, 2022 · N258UP · Boeing 737 · Wing, Attach Fittings
  > INSPECTION TYPE:3CCRACKED BEADED DOUBLER ON LH WING L/E AT APROX XFS 590ACCOMPLISHED MAJOR REPAIR ON LH WING BEADED DOUBLER AT XFS 590 PER MD11 SRM 57-40-02 FIG 205 REPAIR 15
- [SDR IPXA2022100386780](https://openairdocs.org/sdr/IPXA2022100386780.md): Skin · corroded · Sep 11, 2022 · N258UP · Doug MD11F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:3CEMPENNAGE THRU ACCESS 311 INSIDE AREA UPPER FWD COMP L/H SIDE FUSELAGE SKIN HAS CORROSION NEAR AT NUT PLATE AT BETWEEN STA 1986.798 CANT STA 2014.982 AND BETWEEN L10L - L11L.REMOVED, REPAIRED CORRODED AFT SKIN BETWEEN STA 1986.798 AND CANT-
- [SDR IPXA2022100886961](https://openairdocs.org/sdr/IPXA2022100886961.md): Hinge · corroded · Sep 10, 2022 · N258UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3C, RT I/B FLAP AFT HINGE FITTING NR 6 LUG HOLE HAS PITTING AT STA XW=254, YW=495.96 AND ZW=-28.941. REPAIRED AFT HINGE FITTING HOLE IAW EA 011-5740-01-A9719 REV I/R, AND EO MD11-5750-84954-A.
- [SDR IPXA2022100886948](https://openairdocs.org/sdr/IPXA2022100886948.md): Hinge · corroded · Sep 10, 2022 · N258UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3C, RIGHT I/B FLAP FWD HINGE FITTING O/B FACE HAS PITTING AT STA XW=254, YW=495.961 & ZW=-28.941.REPAIRED FWD HINGE O/B FACE IAW EA 011-5740-01-A9717, AND EO MD11-5740-84884-A.
- [SDR IPXA2022100886959](https://openairdocs.org/sdr/IPXA2022100886959.md): Hinge · corroded · Sep 10, 2022 · N258UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3CR/H I/B FLAP AFT HINGE FITTING #7 HOLE HAS PITTING AT STA XW=254, YW=495.96 AND ZW=-28-941.REPAIRED THE AFT HINGE #7 HOLE IAW VT-SAA EA 011-5740-01-A9719 REV I/R DATED 10/07/22 AND UPS EO MD11-5750-84954-A DATED 10/07/22 AND FAA FORM 8100-9 S
- [SDR IPXA2022100286775](https://openairdocs.org/sdr/IPXA2022100286775.md): Spar Cap · corroded · Sep 10, 2022 · N258UP · Doug MD11F · Horizontal Stabilizer, Spar/Rib
  > INSPECTION TYPE:3CR/H HORIZONTAL STABLIZER T/E REAR SPAR LOWER IN/BD FLANGE IS CORRODED BEWTEEN STA XE=39 AND XE=72.REMOVED, REPAIRED CORRODED FLANGE IAW VT-SAA EA 011-5510-01-A9700 REV. IR AND UPS EO MD11-5510-84791-A DATED 09/23/2022 (MINOR)
- [SDR IPXA2022092686623](https://openairdocs.org/sdr/IPXA2022092686623.md): Skin · cracked · Sep 8, 2022 · N258UP · Doug MD11F · Wing, Plate/Skin
  > INSPECTION TYPE:3CR/H WING T/E LOWER SKIN SILL HAS A CRACKED AT STA. XORS= 455.REPLACED CRACKED SILL ON R/H WING T/E AT STA. XORS= 455. IAW SRM 51-33-01 (MINOR)
- [SDR IPXA2022092586576](https://openairdocs.org/sdr/IPXA2022092586576.md): Longeron Splice · cracked · Sep 8, 2022 · N258UP · Doug MD11F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:3CCTR CARGO BILGE AREA AT STA 1531 SPLICE FITTING CRACKED AT LONGERON 49L.REPLACED SPLICE FITTING IN CTR CARGO AT STA 1531 AT LONGERON 49L IAW SRM 51-33-01 (MINOR)
- [SDR IPXA2022100436821](https://openairdocs.org/sdr/IPXA2022100436821.md): Fitting · corroded · Sep 7, 2022 · N258UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:3CR1 DOOR AFT UPPER DOOR JAMB GUIDE FITTING EXFOLIATED CORROSION.REPLACED CORRODED GUIDE FITTING ON R1 AFT UPPER DOOR JAMB IAW SRM 51-31-01 (MINOR)
- [SDR IPXA2022100436820](https://openairdocs.org/sdr/IPXA2022100436820.md): Fitting · corroded · Sep 7, 2022 · N258UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:3C, R1 DOOR FWD UPPER DOOR JAMB GUIDE FITTING HAS EXFOLTATED CORROSION.REPLACED CORRODED GUIDE FITTING ON R1 DOOR IAW SRM 51-31-01 (MINOR)
- [SDR IPXA2022100436816](https://openairdocs.org/sdr/IPXA2022100436816.md): Fitting · cracked · Sep 7, 2022 · N258UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:3CL1 DOOR AFT UPPER DOOR JAMB GUIDE FITTING IS CRACKED.REPLACED CRACKED GUIDE FITTING IAW SRM 51-31-01 (MINOR)
- [SDR IPXA2022091986402](https://openairdocs.org/sdr/IPXA2022091986402.md): None · cracked · Sep 7, 2022 · N258UP · Boeing 737 · Leading Edge Devices
  > INSPECTION TYPE:3CCRACKED BEADED DOUBLER ON L/H WING L/E BETWEEN STA XOS=679.85,XOS=692.03.REMOVED,FAB, REPLACED CRACKED BEADED DOUBLER ON L/H WING L/E BETWEEN STA XOS=679.85, XOS=692.03 IAW SRM 57-40-02 REPAIR 15 FIG 205 REV 69. (MAJOR)
- [SDR IPXA2022100886950](https://openairdocs.org/sdr/IPXA2022100886950.md): Longeron · corroded · Sep 6, 2022 · N258UP · Doug MD11F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:3C, CTR CARGO BILGE AREA AT STA 1701 LONGERON 48R HAS CORROSION.REPAIRED CORRODED LONGERON 48R IN THE CTR CARGO AT BETWEEN STA Y=1690,Y=1710 IAW EA 011-5310-01-A9705 REV I/R DATED 10/05/22 AND EO MD11-5310-84807-A.
- [SDR IPXA2022100286778](https://openairdocs.org/sdr/IPXA2022100286778.md): Longeron · corroded · Sep 6, 2022 · N258UP · Doug MD11F · Fuselage Structure (General)
  > INSPECTION TYPE:3CCTR CARGO BILGE AREA AT STA 1541 LONGERON 48L HAS CORROSION.REPAIRED CORRODED LONGERON 48L IN THE CTR CARGO BILGE AREA AT STA 1541 IAW VT-SAA EA 011-5310-01-A9696 REV. I/R AND UPS EO MD11-5310-84871-A, FAA FORM 8100-9 SIGNED BY P. LAU (AR-83
- [SDR IPXA2022092186472](https://openairdocs.org/sdr/IPXA2022092186472.md): Support · cracked · Sep 6, 2022 · N258UP · Boeing 737 · Wing Structure
  > INSPECTION TYPE:3CR/H WING FIXED L/E SUPPORT STRUCTURE O/B END OF SLAT MECHANISM ACCESS DOOR IS CRACKED.REPLACED R/H FIXED L/E SUPPORT IAW SRM 51-35-01 (MINOR).
- [SDR IPXA2022100286773](https://openairdocs.org/sdr/IPXA2022100286773.md): Cover · missing · Sep 2, 2022 · N258UP · Doug MD11F · Wing, Plate/Skin
  > INSPECTION TYPE:3CL/H WING #7 SLAT CENTER TRACK COVER IS MISSING AND ATTACH BRACKETS BROKEN.FABRICATED,REPLACED #7 SLAT CENTER TRACK COVER AND ATTACH BRACKETS IAW SRM 51-31-01 AND AMM 27-80-30-820-802 (MINOR)
- [SDR IPXA2022062783536](https://openairdocs.org/sdr/IPXA2022062783536.md): Door · abnormal · Jun 26, 2022 · N258UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION TYPE:NASTARTED #3 ENGINE AND GOT LEVEL 1 MESSAGE CRG DR FWD DISAG. FOR ABOUT 2-3 SECONDS AND THEN IT WENT AWAY.PERFORMED OPERTION CHECK IN REF TO MD-11 52-70-00-700-801. NO DEFECTS NOTED VERIFIED FWD CARGO DOOR LATCHED AND LOCKED

Next page: https://openairdocs.org/aircraft/N258UP/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 = 'N258UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N258UP/reports

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