# Service difficulty reports: N295UP, cancelled Jul 23, 2025

A list on [N295UP, cancelled Jul 23, 2025](https://openairdocs.org/deregistered/N295UP-2025-07-23.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 · 322 reports

- [SDR IPXA2023120733928](https://openairdocs.org/sdr/IPXA2023120733928.md): Unknown · unknown · Dec 6, 2023 · N295UP · Doug MD11F · Passenger/Crew Doors
  > LATCH FOR COCKPIT DOOR WILL NOT KEEP DOOR LATCHED OPEN REPLACED LATCH, OP CKS NORMAL. DOCUMENT REFERENCE: 25-00-00
- [SDR IPXA2023120633928](https://openairdocs.org/sdr/IPXA2023120633928.md): Unknown · unknown · Dec 6, 2023 · N295UP · Doug MD11F · Passenger/Crew Doors
  > LATCH FOR COCKPIT DOOR WILL NOT KEEP DOOR LATCHED OPEN REPLACED LATCH, OP CKS NORMAL.
- [SDR IPXA2023100939811](https://openairdocs.org/sdr/IPXA2023100939811.md): Unknown · unknown · Oct 6, 2023 · N295UP · Doug MD11F · Nacelle/Pylon Structure
  > WHILE OPENING ENG #2 FAN COWL TO FOM FOUND R/H FAN COWL DELAMINATED (SEE ATTACHMENT) R+R #2 ENGINE R/H FAN COWL PER AMM 71-12-01. REFERENCE HYUNG CHOE LABOR ROW, FAN COWL WAS REPLACED. ADDED FAN COWL TO FAULT.
- [SDR IPXA2023100639811](https://openairdocs.org/sdr/IPXA2023100639811.md): Unknown · unknown · Oct 6, 2023 · N295UP · Doug MD11F · Nacelle/Pylon, Main Frame
  > *** SDR FILED OPEN *** WHILE OPENING ENG #2 FAN COWL TO FOM FOUND R/H FAN COWL DELAMINATED (SEE ATTACHMENT)
- [SDR IPXA2022112488399](https://openairdocs.org/sdr/IPXA2022112488399.md): Doubler · damaged · Nov 24, 2022 · N295UP · Doug MD11F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:N/AFUSELAGE SKIN PREVIOUS REPAIR DOUBLER DAMAGED AT PLANE 25, BL 0REPLACED DOUBLER IAW E.O. MD11-553-85332-A
- [SDR IPXA2022101487140](https://openairdocs.org/sdr/IPXA2022101487140.md): Battery · discharged · Oct 14, 2022 · N295UP · Doug MD11F · Emergency Lighting
  > INSPECTION TYPE:N/AEMERGENCY LIGHT BATTERY TESTS LOWR2 EMERGENCY LIGHT BATTERY IAW AMM 33-51-01. OPS TEST GOOD
- [SDR IPXA2022091486256](https://openairdocs.org/sdr/IPXA2022091486256.md): Skin Panel · punctured · Sep 14, 2022 · N295UP · Boeing 737 · Wing, Control Surfaces
  > INSPECTION TYPE:SVTRANSFERRED FROM LOGPAGE 439463 ITM 1 RH WING OTBD FLAP LOWER SKIN IS PUNCTURED.ACCOMPLISHED PERMANENT MAJOR REPAIR ON RH WING OTBD FLAP LOWER SKIN PANEL PER MD11 EA# 011-5700-01-A9695 I/R AND UPS EO MD11-5750-84718-A AND FAA APPROVED FORM 81
- [SDR IPXA2022033080667](https://openairdocs.org/sdr/IPXA2022033080667.md): Former · cracked · Mar 16, 2022 · N295UP · Doug MD11F · Wing Miscellaneous Structure
  > INSPECTION TYPE:C1L/H O/B WING L/E HAS A FORMER THAT IS CRACK JUST I/B OF THE #9 SLAT TRACK.REMOVED, FAB, REPLACED CRACK FORMER IAW DWG ARB2931 AND SRM 51-33-01. (MINOR)
- [SDR IPXA2022032780562](https://openairdocs.org/sdr/IPXA2022032780562.md): Doubler · cracked · Mar 16, 2022 · N295UP · Doug MD11F · Wing, Attach Fittings
  > INSPECTION TYPE:1CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 537.2 TO 547.5.REPAIRED CRACKED R/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 537.2 TO 547.5 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)
- [SDR IPXA2022032180309](https://openairdocs.org/sdr/IPXA2022032180309.md): Stiffener · cracked · Mar 14, 2022 · N295UP · Doug MD11F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:1CRT MLG W/W 3RD STIFFENER CRACK AT LOWER END O/B AFT.REMOVED AND REPLACED CRACK STIFFENER IAW SRM 51-35-01 AND 51-35-02 (MINOR).
- [SDR IPXA2022012478222](https://openairdocs.org/sdr/IPXA2022012478222.md): None · dented · Jan 24, 2022 · N295UP · Doug MD11F · Wing, Control Surfaces
  > INSPECTION TYPE:N/ASMALL DENT ON RIGHT WING INBOARD FLAP LOWER SURFACE T/E AREA BETWEEN STA XIFH 124 AND XW 291MAJOR REPAIR COMPLETED PER E.O. MD11-575080336-A SEE NR 676429 FOR DETAIL PERTAINING TO REPAIR THIS CLEARS D715183
- [SDR IPXA2021082873233](https://openairdocs.org/sdr/IPXA2021082873233.md): Door · inoperative · Aug 28, 2021 · N295UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION TYPE:N/AUPON ENTERING A/C FOUND L1 DOOR ELECTRIC ACTUATION TO BE INTERMITTENTT/S IAW FIM 34-46-00 & AMM 34-46-00. OPS TEST GOOD AT THIS TIME. THIS CLEARS M754915
- [SDR IPXA2021090173373](https://openairdocs.org/sdr/IPXA2021090173373.md): Pulley · inoperative · Aug 24, 2021 · N295UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION TYPE:N/AL1 DOOR FWD TOP DRIVE CABLE IDLER PULLEY DAMAGEDR&R LA DOOR FWD TOP DRIVE CABLE IDLER PULLEY REF AMM 52-11-03, BOEING DRAWING ABA7788, & BOEING AEPL
- [SDR IPXA2021082473097](https://openairdocs.org/sdr/IPXA2021082473097.md): Pulley · damaged · Aug 23, 2021 · N295UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION TYPE:N/AL1 DOOR AFT TOP CABLE TENSION PULLEY DAMAGED.INSTALLED NEW PULLEY IN TRUNION. AWAITING PART IN ITEM 2 THIS LOG FOR REINSTALLATION. REF MM 52 11 03 CF 3194937 8-22-21/ R&R WITH NEW ROD ASSY ITEM 2. INSTALLED TRUNNION & PULLY WITH TOP AFT L2 D
- [SDR IPXA2021081322676](https://openairdocs.org/sdr/IPXA2021081322676.md): Cable · broken · Aug 12, 2021 · N295UP · Doug MD11F · Passenger/Crew Doors
  > FUELING SUPERVISOR REPORTED L1 DOOR WOULD NOT CLOSE INSPECT L1 DOOR AND FOUND AFT LIFT. LOWERING CABLES BROKEN. INSTALLED LOWER L1 DOOR CABLE UP TO AND INCLUDING STEP AMM 52-11-03 E(1) (B) INSTALLED L1 DOOR TOP & BOTTOM AFT CABLES THROUGH SETP E.9 AMM 52-11-0
- [SDR IPXA2021060870293](https://openairdocs.org/sdr/IPXA2021060870293.md): Battery Pack · inoperative · Jun 8, 2021 · N295UP · Doug MD11F · Emergency Lighting
  > EMERGENCY LIGHTING IN COURIER AREA REMAINS PARTIALLY ILLUMINATED WITH EMERGENCY LIGHT. TEST PASSED ANE WITHOUT INDICATION EAD. DEFERRED EMERGENCY LIGHTS PER MEL 33-50-4 DMP C/W PLACARD INSTALLED.R/R'D EMERGENCY BATTERY PWR SUPPLY PER MM 33-51-01 PG BLK 401.
- [SDR IPXA2021012564839](https://openairdocs.org/sdr/IPXA2021012564839.md): Roller · lack of lube · Jan 25, 2021 · N295UP · Doug MD11F · Passenger/Crew Doors
  > L1 DOOR DOES NOT CLOSE/SEAL COMPLETELY ON FORWARD SIDE. THE DOOR DOES NOT OPERATE SMOOTHLY DURING THE LAST HALF OF THE CLOSING EITHER. ITEM DEFERRED PER MEL 52-10-3-1-2-1 PLACARD INSTALLED. DI# M733638 ASSIGNED. AIRCRAFT OK TO CONT. CRV.CLEANED AND LUBED TRACK
- [SDR IPXA2020050154778](https://openairdocs.org/sdr/IPXA2020050154778.md): Support Fitting · cracked · Apr 29, 2020 · N295UP · Doug MD11F · Fuselage, Landing Gear Attach Fittings
  > INSPECTION TYPE:2C CRACK ON NLG LH TRUNNION SUPPORT FITTING AT FUSELAGE STA Y=582.5, Z= -114 & X = 24.00.REPAIRED CRACKED LH NLG TRUNNION SUPPORT FITTING AT FUSELAGE STA Y= 582.5, Z= -114 & X=24.0. IAW SRM 53-10-14 REPAIR 2 FIGURE 202. ( MAJOR)
- [SDR IPXA2020042954772](https://openairdocs.org/sdr/IPXA2020042954772.md): Longeron · corroded · Apr 29, 2020 · N295UP · Doug MD11F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:2CCORROSION ON LONGERON 52 AT FWD EXTENDED FUSELAGE SECTION STA Y=6-73.ACCOMPLISHED SPLICE REPAIR ON LONGERON 52 BETWEEN Y= 6-60.00 - Y= 6-80 IAW SRM 53-00-05 REPAIR 1. FIGURE 201 & 202. (MAJOR)
- [SDR IPXA2020051555288](https://openairdocs.org/sdr/IPXA2020051555288.md): Bulkhead · corroded · Apr 13, 2020 · N295UP · Doug MD11F · Nacelle/Pylon, Bulkhead/Firewall
  > INSPECTION TYPE:2C#3 ENG. PYLON AFT BULKHEAD ASSY. HAS CORROSION COMMON TO THE INNER BORE LUG OF BULKHEAD P/N AUB7502-507 & AUB 7502-509.REPAIRED #3 ENG. PYLON AFT BULKHEAD ASSY. IAW VT-SAA EA 011-5410-01-A8166 REV. I/R AND UPS EO MD11-5410-76449-A. (MINOR).
- [SDR IPXA2020051855346](https://openairdocs.org/sdr/IPXA2020051855346.md): Stringer · cracked · Apr 8, 2020 · N295UP · Doug MD11F · Wing, Longeron/Stringer
  > INSPECTION TYPE:4CR/H WING TANK AT STA XORS 330.890, STRINGER # 41 IS CRACKED.ACOMPLISHED REPAIR TO R/H WING TANK AT STA XORS 330.890, STRINGER # 41 IAW VT-SAA EA 011-5710-01-A8138-IR AND UPS EO MD11-5710-76538-A.
- [SDR IPXA2020051155098](https://openairdocs.org/sdr/IPXA2020051155098.md): Mount Fitting · damaged · Apr 7, 2020 · N295UP · Doug MD11F · Ailerons
  > INSPECTION TYPE:4CRT I/B AILERON #2 MOUNT BOTH I/B AND O/B BUSHINGS ARE MIGRATED.REPAIRED DAMAGED RT I/B AILERON #2 MOUNT FITTING I/B AND O/B LUG BUSHING BORES IAW VT-SAA EA 011-5740-01-A8150 REV. IR AND UPS EO MD11-5740-76427-A. (MINOR)
- [SDR IPXA2020051555324](https://openairdocs.org/sdr/IPXA2020051555324.md): Barrier · corroded · Apr 6, 2020 · N295UP · Doug MD11F · Cargo Compartments
  > INSPECTION TYPE:2CRIGID CARGO BARRIER WALL HAS CORROSION ON LOWER FACE.REMOVED AND REPLACED RIGID CARGO BARRIER WALL IAW AMM 25-59-13-00-801 AND 25-59-13-400-801. (MINOR)
- [SDR IPXA2020051355030](https://openairdocs.org/sdr/IPXA2020051355030.md): Seat Track · corroded · Apr 6, 2020 · N295UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:4CMAIN CABIN SEAT TRACK AT X=-47.5 BETWEEN STA. 475 AND STA. 488 HAS CORROSION.REPAIRED CORRODED MAIN CABIN SEAT TRACK AT X=-47.5 BETWEEN STA. 475 AND STA. 488 IAW VT-SAA EA 011-5310-01-A8146 REV. IR AND UPS EO MD11-5310-76344-A. (MINOR)
- [SDR IPXA2020051355214](https://openairdocs.org/sdr/IPXA2020051355214.md): Seat Track · corroded · Apr 6, 2020 · N295UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:2CMAIN CABIN SEAT TRACK IS CORRODED BETWEEN STA. 459-485 AND X=50 TO X=62.REPAIRED CORRODED SEAT TRACK MBETWEEN STA. 459-485 AND X=50 TO X=62 IAW VT-SAA EA 011-5310-01-A8139 REV. I/R AND UPS EO MD11-5310-76476-A. (MAJOR)
- [SDR IPXA2020051355266](https://openairdocs.org/sdr/IPXA2020051355266.md): Seat Track · corroded · Apr 6, 2020 · N295UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:4CMAIN CABIN SEAT TRACK HAS CORROSION BETWEEN STA. 440 - 488 AT X=19.0.REPAIRED CORRODED MAIN CABIN SEAT TRACK BETWEEN STA. 440 - 488 AT X=19.0 IAW VT-SAA EA 011-5310-01-A8145 REV. IR AND UPS EO MD11-5310-76338-A. (MINOR)
- [SDR IPXA2020051355210](https://openairdocs.org/sdr/IPXA2020051355210.md): Seat Track · corroded · Apr 6, 2020 · N295UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:2CMAIN CABIN SEAT TRACK HAS CORROSION BETWEEN STA. 459-480 AND X=77REMOVED AND REPLACED SEAT TRACK AT SAID LOCATION IAW SRM 51-31-01. (MINOR)
- [SDR IPXA2020051355034](https://openairdocs.org/sdr/IPXA2020051355034.md): Floor Panel · corroded · Apr 6, 2020 · N295UP · Doug MD11F · Fuselage Floor Panel
  > INSPECTION TYPE:4CMAIN CABIN FLOOR PANEL AT STA 475 AND X=75.25 HAS CORROSION.REPAIRED CORRODED MAIN CABIN FLOOR PANEL AT STA 475 AND X=75.25 IAW VT-SAA EA 011-5320-01-A8152 REV IR AND UPS EO MD11-5320-76347-A. (MINOR)
- [SDR IPXA2020051355035](https://openairdocs.org/sdr/IPXA2020051355035.md): Floor Panel · corroded · Apr 6, 2020 · N295UP · Doug MD11F · Fuselage Floor Panel
  > INSPECTION TYPE:4CMAIN CABIN FLOOR PANEL AT STA 475 AND BETWEEN X=47.5 TO X=75.25 HAS CORROSION.REPAIRED CORRODED MAIN CABIN FLOOR PANEL AT STA 475 AND BETWEEN X=47.5 TO X=75.25 IAW VT-SAA EA 011-5320-01-A8151 REV IR AND UPS EO MD11-5320-76349-A. (MINOR)
- [SDR IPXA2020050655022](https://openairdocs.org/sdr/IPXA2020050655022.md): Floor Panel · corroded · Apr 6, 2020 · N295UP · Doug MD11F · Fuselage Floor Panel
  > INSPECTION TYPE:4CMAIN CABIN FLOOR PANEL AT STA. 475 BETWEEN X=-47.5 TO X=-72.25 HAS CORROSION.REPAIRED CORRODED MAIN CABIN FLOOR PANEL AT STA. 475 BETWEEN X=-47.5 TO X=-72.25 IAW VT-SAA EA 011-5320-01-A8154 REV. IR AND UPS EO MD11-5320-76313-A. (MINOR)
- [SDR IPXA2020050655021](https://openairdocs.org/sdr/IPXA2020050655021.md): Floor Panel · corroded · Apr 6, 2020 · N295UP · Doug MD11F · Fuselage Floor Panel
  > INSPECTION TYPE:4CMAIN CABIN FLOOR PANEL AT STA 475 BETWEEN X=-27.5 TO X=-36 HAS CORROSION.REPAIRED CORRODED MAIN CABIN FLOOR PANEL AT STA 475 BETWEEN X=-27.5 TO X=-36 IAW VT-SAA EA 011-5320-01-A8153 REV. IR AND UPS EO MD11-5320-76348-A. (MINOR)
- [SDR IPXA2020050654983](https://openairdocs.org/sdr/IPXA2020050654983.md): Seat Track · corroded · Apr 6, 2020 · N295UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:4CSEAT TRACK AT X=-27.5 BETWEEN STA 437 AND STA 479 HAS CORROSION.REPAIRED CORRODED SEAT TRACK AT X=-27.5 BETWEEN STA 437 AND STA 479 IAW VT-SAA EA 011-5310-01-A8147 REV IR AND UPS EO MD11-5310-76311-A. (MINOR)
- [SDR IPXA2020050654986](https://openairdocs.org/sdr/IPXA2020050654986.md): Floorbeam · corroded · Apr 6, 2020 · N295UP · Doug MD11F · Fuselage Main, Floor Beam
  > INSPECTION TYPE:4CFLOOR SUPPORT AT STA 421.578 BETWEEN X=-65 & X=-78 HAS CORROSION.REMOVED AND REPLACED CORRODED FLOOR SUPPORT AT STA 421.578 BETWEEN X=-65 & X=-78 IAW MD-11 SRM 51-33-01 AND 51-31-01. (MINOR)
- [SDR IPXA2020050154808](https://openairdocs.org/sdr/IPXA2020050154808.md): Seat Track · corroded · Apr 6, 2020 · N295UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:2CMAIN CABIN SEAT TRACK HAS CORROSION BETWEEN STA. 459-475 AT X= 36.0.REPAIRED CORRODED SEAT TRACK BETWEEN STA. 459-475 AT X= 36.0 IAW VT-SAA EA 011-5310-01-A8144 REV. I/R AND UPS EO MD11-5310-76302-A. (MINOR)
- [SDR IPXA2020050154807](https://openairdocs.org/sdr/IPXA2020050154807.md): Seat Track · corroded · Apr 6, 2020 · N295UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:2CMAIN CABIN SEAT TRACK HAS CORROSION BETWEEN STA. 440-488 AT X= -17.REPAIRED CORRODED SEAT TRACK BETWEEN STA 440-488 AT X= -17 IAW VT-SAA EA 011-5310-01-A8141 REV. I/R AND UPS EO MD11-5310-76306-A. (MINOR)
- [SDR IPXA2020050154806](https://openairdocs.org/sdr/IPXA2020050154806.md): Seat Track · corroded · Apr 6, 2020 · N295UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:2CMAIN CABIN SEAT TRACK HAS CORROSION BETWEEN STA. 421.578-488 AT X=0.REPAIRED CORRODED SEAT TRACK BETWEEN STA. 421.578-488 AT X=0 IAW VT-SAA EA 011-5310-01-A8140 REV. I/R AND UPS EO MD11-5310-76290-A. (MINOR)
- [SDR IPXA2020050154805](https://openairdocs.org/sdr/IPXA2020050154805.md): Seat Track · corroded · Apr 6, 2020 · N295UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:2CMAIN CABIN SEAT TRACK HAS CORROSION BETWEEN STA. 440-488 AT X= -36.REPAIRED CORRODED SEAT TRACK BETWEEN STA. 440-488 AT X= -36 IAW VT-SAA EA 011-5310-01-A8142 REV. I/R AND UPS EO MD11-5310-76312-A. (MINOR)
- [SDR IPXA2020050154804](https://openairdocs.org/sdr/IPXA2020050154804.md): Seat Track · corroded · Apr 6, 2020 · N295UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:2CMAIN CABIN SEAT TRACK HAS CORROSION BETWEEN STA. 475-515 AT X= 47.5.REPAIRED CORRODED SEAT TRACK BETWEEN STA. 475-515 AT X=47.5 IAW VT-SAA EA 011-5310-01-A8143 REV. I/R AND UPS EO MD11-5310-76303-A. (MINOR)
- [SDR IPXA2020051355253](https://openairdocs.org/sdr/IPXA2020051355253.md): Longeron · cracked · Apr 5, 2020 · N295UP · Doug MD11F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:2CCENTER CARGO LONGERON # 52 IS CRACKED BETWEEN STA. 1681-1701.REPAIRED CRACKED CENTER CARGO LONGERON # 52 BETWEEN STA. 1641 TO 1701 IAW VT=SAA EA 011-5310-01-A8157 REV. I/R AND UPS EO MD11-5310-76494-A. (MAJOR)
- [SDR IPXA2020051355211](https://openairdocs.org/sdr/IPXA2020051355211.md): Door Frame · chafed · Apr 5, 2020 · N295UP · Doug MD11F · Landing Gear Doors
  > INSPECTION TYPE:2CCENTER LANDING GEAR R/H DOOR UPPER AFT CORNER FRAME IS CHAFED.REMOVED FABRICATED AND REPLACED DOOR FRAME IAW DWG. ANB7384 AND SRM 51-31-01. (MINOR)
- [SDR IPXA2020051355037](https://openairdocs.org/sdr/IPXA2020051355037.md): Longeron · cracked · Apr 4, 2020 · N295UP · Doug MD11F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:4CMAIN CABIN INTERUPTED LONGERON 16L IS CRACKED BETWEEN STA. 1139 - 1159.REMOVED AND REPLACED CRACKED MAIN CABIN INTERUPTED LONGERON 16L BETWEEN STA. 1139 - 1159 IAW MD-11 SRM 51-33-01. (MINOR)
- [SDR IPXA2020051355268](https://openairdocs.org/sdr/IPXA2020051355268.md): Stringer Splice · cracked · Apr 4, 2020 · N295UP · Doug MD11F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:4CCENTER CARGO LONGERON 29R SPLICE IS CRACKED BETWEEN STA. 1661 AND 1681.REMOVED AND REPLACED CRACKED CENTER CARGO LONGERON 29R SPLICE BETWEEN STA. 1661 AND 1681 IAW MD-11 SRM 51-33-01. (MINOR)
- [SDR IPXA2020051355065](https://openairdocs.org/sdr/IPXA2020051355065.md): Splice · cracked · Apr 4, 2020 · N295UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:4CCENTER CARGO R/H TUNNEL UPPER AREA SPLICE AT L28R HAS 2 CRACKS.REMOVED AND REPLACED CRACKED CENTER CARGO LONGERON 28R SPLICE AND CRACKED LONGERON SECTION BETWEEN STA. 1651 AND 1701 IAW MD-11 SRM 53-00-05, REPAIR 1, FIGURE 201 & 202. (MAJOR)
- [SDR IPXA2020051155097](https://openairdocs.org/sdr/IPXA2020051155097.md): Support Angle · cracked · Apr 4, 2020 · N295UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:4CCENTER CARGO SLOPE PANEL SUPPORT ANGLE AT STA. 1951 IS CRACKED.REMOVED AND REPLACED CRACKED CENTER CARGO SLOPE PANEL SUPPORT ANGLE AT STA. 1951 IAW MD-11 SRM 51-35-01. (MINOR)
- [SDR IPXA2020050654991](https://openairdocs.org/sdr/IPXA2020050654991.md): Longeron · cracked · Apr 4, 2020 · N295UP · Doug MD11F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:2CCENTER CARGO LONGERON # 42 R/H IS CRACKED BETWEEN STA. 1641-1661.REPAIRED CRACKED CENTER CARGO LONGERON # 42 R/H BETWEEN STA. 1630 TO 1650.130 IAW SRM 53-00-05 REPAIR 1 FIG. 201 & 202. (MAJOR)
- [SDR IPXA2020050654990](https://openairdocs.org/sdr/IPXA2020050654990.md): Longeron · cracked · Apr 4, 2020 · N295UP · Doug MD11F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:2CCENTER CARGO LONGERON # 38 R/H IS CRACKED BETWEEN STA. 1661-1681.REPAIRED CRACKED CENTER CARGO LONGERON # 38 R/H BETWEEN STA. 1641 TO 1681 IAW SRM 536-00-05 REPAIR 1 FIG. 201 & 202. (MAJOR)
- [SDR IPXA2020050654989](https://openairdocs.org/sdr/IPXA2020050654989.md): Longeron · cracked · Apr 4, 2020 · N295UP · Doug MD11F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:2CCENTER CARGO LONGERON # 37 R/H IS CRACKED BETWEEN STA. 1661-1681.REPAIRED CRACKED CENTER CARGO LONGERON # 37 R/H BETWEEN STA. 1641 TO 1681 IAW SRM 53-00-05 REPAIR 1 FIG. 201 AND 202. (MAJOR)
- [SDR IPXA2020050454884](https://openairdocs.org/sdr/IPXA2020050454884.md): Longeron · cracked · Apr 4, 2020 · N295UP · Doug MD11F · Aerodynamic Fairings
  > INSPECTION TYPE:2CTAIL CONE R/H UPPER LONGERON BEAM IS CRACKED AT THE FWD. END.REPAIRED TAIL CONE R/H UPPER LONGERON BEAM IAW UPS EO MD11-5350-66790-A. (MINOR)
- [SDR IPXA2020050154830](https://openairdocs.org/sdr/IPXA2020050154830.md): Doubler · worn · Apr 4, 2020 · N295UP · Doug MD11F · Aerodynamic Fairings
  > INSPECTION TYPE:2CTAIL CONE LH UPPER LONGERON @ PRODUTION DOUBLER IS WORN THRU.REPAIRED TAILCONE LONGERON / INTERNAL DOUBLER IAW EO MD11-5350-66790-A. (MINOR)
- [SDR IPXA2020050154829](https://openairdocs.org/sdr/IPXA2020050154829.md): Frame · cracked · Apr 4, 2020 · N295UP · Doug MD11F · Aerodynamic Fairings
  > INSPECTION TYPE:2CTAIL CONE FWD. R/H FRAME IS CRACKED AT THE CENTER GUIDE PIN HOLE.REPAIRED TAIL CONE FRAME IAW SRM 53-80-07 REPAIR 1 FIG. 201. (MINOR)

Next page: https://openairdocs.org/deregistered/N295UP-2025-07-23/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 = 'N295UP' AND deregistration_id = 'N295UP-2025-07-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N295UP-2025-07-23/reports

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