# Service difficulty reports: N272UP, cancelled Jul 13, 2025 A list on [N272UP, cancelled Jul 13, 2025](https://openairdocs.org/deregistered/N272UP-2025-07-13.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 · 318 reports - [SDR IPXA2024011794581](https://openairdocs.org/sdr/IPXA2024011794581.md): Winglet · damaged · Jan 17, 2024 · N272UP · Doug MD11F · Wing Main, Frame Structure > RAMP REPORTED LOADER DAMAGED FWD TIP RIGHT LOWER WINGLET DAMAGE IS APPROX 2IN X 1 IN SM26/LMX4. REINSTALLED R/H LOWER WINGLET AFTER REPAIRS. REF:AMM 57-31-02-400-801. THIS CLEARED CDL DEFERRAL. PLACARD REMOVED. - [SDR IPXA2023120243400](https://openairdocs.org/sdr/IPXA2023120243400.md): Unknown · unknown · Dec 1, 2023 · N272UP · Doug MD11F · Aircraft Fuel System > *** SUPPLEMENTAL SDR *** AT CRUISE 30 MINUTES INTO FLIGHT LEVEL 2 FUEL QTY FAULT WITH TANK 2 FUEL QTY "X"-ED. #2 FUEL QTY REGAINED ON FINAL APPROACH **OII 2** **DD 12/04** R/R #2 TANK L/H MJP REF AMM 28-41-40-401 OPS AND LEAK CHECK GOOD PLACARD REMOVED DMP RE - [SDR IPXA2023120143400](https://openairdocs.org/sdr/IPXA2023120143400.md): Unknown · unknown · Dec 1, 2023 · N272UP · Doug MD11F · Fuel Indicating System > *SDR FILED OPEN* AT CRUISE 30 MINUTES INTO FLIGHT LEVEL 2 FUEL QTY FAULT WITH TANK 2 FUEL QTY "X"-ED. #2 FUEL QTY REGAINED ON FINAL APPROACH - [SDR IPXA2023101838691](https://openairdocs.org/sdr/IPXA2023101838691.md): Power Supply · faulted · Oct 18, 2023 · N272UP · Doug MD11F · Emergency Lighting > EMER LTS BAT 1 LO MESSAGE DURING TEST REVERSED DMP. R&R'D EMER LIGHT BATTERY POWER SUPPLY PER AMM 33-51-01. OPS CHECK GOOD. DEFERRAL CLEARED. - [SDR IPXA2023100254435](https://openairdocs.org/sdr/IPXA2023100254435.md): Unknown · unknown · Oct 2, 2023 · N272UP · Doug MD11F · Wing, Attach Fittings > DAMAGE FOUND ON RH WING NO. 3 SLAT, STATION XOS 402. INADVERTENLY CLOSED. C/W EO-88327-REQ1. CHKS GOOD. OK TO CONT. - [SDR IPXA2023100254914](https://openairdocs.org/sdr/IPXA2023100254914.md): Unknown · unknown · Oct 2, 2023 · N272UP · Doug MD11F · Wing, Attach Fittings > DAMAGE FOUND AT RH NO. 4 SLAT TRAILING EDGE, OUTBOARD, UPPER SURFACE. COMPLETED #4 SLAT INSTALLATION PER MM 27-80-30-400-802 ITEM IS CLOSED. - [SDR IPXA2023072893755](https://openairdocs.org/sdr/IPXA2023072893755.md): Bottle · blown · Jul 28, 2023 · N272UP · Doug MD11F · Doors > INSPECTION TYPE:NAL1 DOOR BOTTLE BLOWN TO EXIT AC.RESERVICED L1 DOOR BOTTLE PER AMM 12-25-04. - [SDR IPXA2023072893752](https://openairdocs.org/sdr/IPXA2023072893752.md): Panel · fumes · Jul 28, 2023 · N272UP · Doug MD11F · Lighting System > INSPECTION TYPE:NA*** EMERGENCY DECLARED *** ON DESCENT SDF HEARD ELECTRICAL ARC SOUND AND FLASH FROM ELECTRICAL PANEL BEHIND F.O. IMMEDIATELY SMELLED ELECTRICAL FUMES OVERHEAD PANEL LIGHTS WENT OUT.FOUND OVERHEAD/ OBSERVER STATION INSTRUMENT LIGHTING DIMMER S - [SDR IPXA2023060693379](https://openairdocs.org/sdr/IPXA2023060693379.md): Cable · broken · Jun 5, 2023 · N272UP · Doug MD11F · Passenger/Crew Doors > INSPECTION TYPE:NA *SDR FILED OPEN* L1 DOOR BOUNCES WHILE CLOSING UPPER AFT CABLE IS EXCESSIVELY LOOSE WHEN THE DOOR IS UP AND THE LOWER AFT CABLE IS EXCESSIVELY LOOSE WHEN THE DOOR IS DOWN. UPPER AFT CABLE HAS MULTI BROKEN STRANDS ALSO CABLE ORD ON REQ #45083 - [SDR IPXA2023042092930](https://openairdocs.org/sdr/IPXA2023042092930.md): Sign · detached · Apr 19, 2023 · N272UP · Doug MD11F · Emergency Lighting > INSPECTION TYPE:NAEXIT SIGN ON DOOR 1L FELL OFF WHILE DOOR WAS IN TRANSIT REPEAT WRITE FROM PAGE 295518.R&R L1 EXIT SIGN ASSY OPS GOOD PER MM 33-27-05 ESR IPC 33-27-01-05 #130K. - [SDR IPXA2022102987604](https://openairdocs.org/sdr/IPXA2022102987604.md): Support Bracket · cracked · Oct 18, 2022 · N272UP · Doug MD11F · Fuselage Miscellaneous Structure > INSPECTION TYPE:1CCAC AVI COMPARTMENT R/H SIDE AVI RACK HAS BRACKET SUPPORT THAT IS CRACKED AT STA 1139.REPLACED CRACKED SUPPORT IN THE CAC AVI COMPARTMENT AVI RACK IAW SRM 51-31-01 (MINOR) - [SDR IPXA2022110187710](https://openairdocs.org/sdr/IPXA2022110187710.md): Skin · dented · Oct 17, 2022 · N272UP · Doug MD11F · Trailing Edge Flaps > INSPECTION TYPE:1C, LEFT WING I/B FLAP SURFACE HAS A DENT AT STA YIFH=70.5, XIFH=177.320.REPAIRED L/H WING I/B FLAP AT STA YIFH=70.5, XIFH=177.320 IAW EA 011-5753-01-A9741 REV I/R AND MD11-5750-85123-A AND FAA FORM 8100-9. MAJOR - [SDR IPXA2022103187691](https://openairdocs.org/sdr/IPXA2022103187691.md): Skin · gouged · Oct 17, 2022 · N272UP · Doug MD11F · Fuselage Main, Plate/Skin > INSPECTION TYPE:1CFWD CARGO DOOR AFT LWR SILL AREA EXISTING REPAIR HAS A GOUGE.REPAIRED FWD CARGO DOOR AFT LWR SILL AREA EXISTING REPAIR IAW VT-SAA EA 011-5330-01-A9740 REV I/R AND UPS EO MD11-5330-85131-A DATED 10/28/2022 (MINOR) - [SDR IPXA2022103187689](https://openairdocs.org/sdr/IPXA2022103187689.md): Bracket · corroded · Oct 17, 2022 · N272UP · Doug MD11F · Trailing Edge Flaps > INSPECTION TYPE:1CL/H WING I/B FLAP O/B FWD FITTING PANEL BRACKET O/B SIDE HAS CORROSION.REPLACED TEE BRACKET ON THE L/H WING I/B FLAP O/B FWD FITTING O/B SIDE IAW SRM 51-33-01 (MINOR) - [SDR IPXA2022103187688](https://openairdocs.org/sdr/IPXA2022103187688.md): Bracket · corroded · Oct 17, 2022 · N272UP · Doug MD11F · Trailing Edge Flaps > INSPECTION TYPE:1CL/H WING I/B FLAP O/B FWD FITTING PANEL BRACKET I/B SIDE HAS CORROSION.REPLACED TEE BRACKET ON THE L/H WING I/B FLAP I/B SIDE IAW SRM 51-31-01 (MINOR) - [SDR IPXA2022110287742](https://openairdocs.org/sdr/IPXA2022110287742.md): Frame · cracked · Oct 14, 2022 · N272UP · Doug MD11F · Instrument Panel > INSPECTION TYPE:1CCAPT AND FIRST OFFICER LOWER INSTRUMENT PANEL FRAME IS CRACKED.REPAIRED CRACKED INSTRUMENT PANEL FRAME IAW UPS EO MD11-2510-82425-C DATED 10/27/2022. (MINOR) - [SDR IPXA2022110187732](https://openairdocs.org/sdr/IPXA2022110187732.md): Stiffener · chafed · Oct 14, 2022 · N272UP · Doug MD11F · Fuselage Main, Bulkhead > INSPECTION TYPE:1CAFT BODY STA 2163.685 BULKHEAD R/H SIDE STIFFENER HAS CHAFE DAMAGEDREPAIRED STIFFENER AT STA 2163.685 BULKHEAD R/H SIDE IAW SRM 53-00-00 (MINOR) - [SDR IPXA2022110187719](https://openairdocs.org/sdr/IPXA2022110187719.md): Trunnion · cracked · Oct 14, 2022 · N272UP · Doug MD11F · Fuselage, Landing Gear Attach Fittings > INSPECTION TYPE:1CR/H NLG TRUNION FITTING APPEARS TO BE CRACKED FROM FASTENER TO FASTENER AT STA Y=582.5, Z=-114, X=-24.00.REPAIRED R/H NLG TRUNION FITTING AT STA Y=582.5, Z=-114, X=-24.00 IAW SRM 53-10-14 REPAIR 2 FIG 202 REV. 69.01. (MAJOR) - [SDR IPXA2022061383071](https://openairdocs.org/sdr/IPXA2022061383071.md): Door · inoperative · Jun 13, 2022 · N272UP · Doug MD11F · Passenger/Crew Doors > INSPECTION TYPE:NADOOR L1 "DOOR DISARMED" LIGHT HOUSING KEEPS FALLING OUT OF BULKHEADR&R DOOR DISARMED LIGHT INDICATOR PER AMM 20-50-00 AND WPM 52-11-01. OPS CHECKS GOOD PER AMM 52-11-02-010-801 STEP C. (1). ESR: IPC 52-11-70-01 ITEM 170 - [SDR IPXA2022041181048](https://openairdocs.org/sdr/IPXA2022041181048.md): None · none · Apr 8, 2022 · N272UP · Doug MD11F · Fuel Controlling System > INSPECTION TYPE:NA"ENG 1 FADEC MAINT" MSG 1:30 INTO FLIGHT AT FL390REMOVED & REPLACED #1 ENGINE CONTROL STATORALTERNATOR IAW MD11 AMM 73-21-21-401 CONFIG2. PERFORMED EEC IDLE TEST 06 NO FAULTS LOGGED. - [SDR IPXA2021111075841](https://openairdocs.org/sdr/IPXA2021111075841.md): None · none · Nov 9, 2021 · N272UP · Doug MD11F · Passenger/Crew Doors > INSPECTION TYPE:NAL-1 UPPER DOOR COVER AFT SIDE PIN LANYARD BROKEN.R/R LANYARD REF AMM 52-11-02-000-801. - [SDR IPXA2021110975821](https://openairdocs.org/sdr/IPXA2021110975821.md): None · damaged · Nov 9, 2021 · N272UP · Doug MD11F · Passenger/Crew Doors > INSPECTION TYPE:N/AL1 DOOR PIN LANYARD FORWARD UPPER FOR SLIDE DAMAGEDREPLACED LANYARD REF AMM 52-11-02-000-801. - [SDR IPXA2020122963931](https://openairdocs.org/sdr/IPXA2020122963931.md): Battery Pack · discharged · Dec 29, 2020 · N272UP · Doug MD11F · Emergency Lighting > INSPECTION TYPE: NA CREW REPORTED EMERGENCY LIGHT BAT 1 LO. DEFERRED EMERGENCY LIGHT SYSTEM, IAW MEL 33-50-4. PLACARD INSTALLED C/W DMP 33-50-4 CBS OPENED OVERHEAD PANEL F24 E67 G23 LOWER MAIN ILLEG G13 F13 ILLEG M731047 ASSGNED. REPLACED EMERGENCY POWER SU - [SDR IPXA2020111762509](https://openairdocs.org/sdr/IPXA2020111762509.md): Pan · gouged · Nov 9, 2020 · N272UP · Doug MD11F · Cargo/Baggage Doors > INSPECTION TYPE: 4C UPPER CARGO DOOR FWD LOWER PAN IS GOUGED.REMOVED AND REPLACED GOUGED UPPER CARGO DOOR FWD LOWER PAN IAW MD-11 SRM 51-33-01 AND 51-35-01. (MINOR) - [SDR IPXA2020112262659](https://openairdocs.org/sdr/IPXA2020112262659.md): Beam · cracked · Nov 7, 2020 · N272UP · Doug MD11F · Trailing Edge Flaps > INSPECTION TYPE: 2C RT OUTBOARD FLAP INBOARD HINGE FAIRING BEAM CRACK. REMOVED AND REPLACED CRACKED BEAM AT RT OUTBOARD FLAP INBOARD HINGE, IAW SRM 51-35-01,51-33-01 AND DWG ARC2151. (MINOR) - [SDR IPXA2020112262661](https://openairdocs.org/sdr/IPXA2020112262661.md): Bracket · corroded · Nov 6, 2020 · N272UP · Doug MD11F · Trailing Edge Flaps > INSPECTION TYPE: 2C RT WING OUTBOARD FLAP INBOARD HINGE LUG HOLES CORRODED. REPAIRED RT OUTBPARD FLAP INBOARD HINGE CORRODED LUG HOLES, IAW VT-SAA EA 011-5740-01-A8716 REV I/R AND UPS EO MD11-5750-78565-A. (MINOR). - [SDR IPXA2020112162618](https://openairdocs.org/sdr/IPXA2020112162618.md): Fitting · damaged · Nov 6, 2020 · N272UP · Doug MD11F · Ailerons > INSPECTION TYPE: 4C LT WING INBOARD AILERON ACTUATOR MOUNT FITTING INBOARD LUG ANTI-ROTATION TAB IS DAMAGED. REPAIRED DAMAGED LT WING INBOARD AILERON ACTUATOR MOUNT FITTING INBOARD LUG ANTI-ROTATION TAB, IAW VT-SAA EA 011-5751-01-A8719 REV IR AND UPS EO MD11- - [SDR IPXA2020112162613](https://openairdocs.org/sdr/IPXA2020112162613.md): Fitting · migrated · Nov 6, 2020 · N272UP · Doug MD11F · Elevator Structure > INSPECTION TYPE: 4C RT HORIZONTAL STABILIZER TRAILING EDGE NR 2 HINGE FITTING AT STA XE 108 INBOARD & OUTBOARD BUSHINGS ARE MIGRATED. REPAIRED MIGRATED RT HORIZONTAL STABILIZER TRAILING EDGE NR 2 HINGE FITTING AT STA XE 108 INBOARD & OUTBOARD BUSHINGS, IAW VT - [SDR IPXA2020112162617](https://openairdocs.org/sdr/IPXA2020112162617.md): Fitting · damaged · Nov 5, 2020 · N272UP · Doug MD11F · Ailerons > INSPECTION TYPE: 4C RT WING INBOARD AILERON ACTUATOR MOUNT FITTING INBOARD LUG ANTI-ROTATION TAB IS DAMAGED. REPAIRED DAMAGED RT WING INBOARD AILERON ACTUATOR MOUNT FITTING INBOARD LUG ANTI-ROTATION TAB, IAW VT-SAA EA 011-5751-01-A8720 REV IR AND UPS EO MD11- - [SDR IPXA2020112362695](https://openairdocs.org/sdr/IPXA2020112362695.md): Skin · cracked · Nov 4, 2020 · N272UP · Doug MD11F · Trailing Edge Flaps > INSPECTION TYPE: 2C RT OUTBOARD FLAP HAS A CRACKED FITTING INSIDE PANEL 657HT, HINGE ATTACH FITTING. REMOVED AND REPLACED RT OUTBOARD FLAP, IAW AMM27-50-30-400-802. (MINOR) - [SDR IPXA2020112262668](https://openairdocs.org/sdr/IPXA2020112262668.md): Stiffener · cracked · Nov 4, 2020 · N272UP · Doug MD11F · Wing Miscellaneous Structure > INSPECTION TYPE: 2C RT WING UPPER LEADING EDGE PANEL 616ET 2 EA STIFFENER CRACK. REMOVED AND REPLACED CRACKED 2 EA STIFFENER AT RT WING LEADING EDGE, IAW SRM 51-31-01 AND SRM 51-35-01. (MINOR) - [SDR IPXA2020112162612](https://openairdocs.org/sdr/IPXA2020112162612.md): Spar Cap · corroded · Nov 4, 2020 · N272UP · Doug MD11F · Wing Spar > INSPECTION TYPE: 4C LT WING REAR SPAR UPPER CAP AFT FLANGE HAS CORROSION BETWEEN XORS 672.5 AND XORS 762. REPAIRED CORRODED LT WING REAR SPAR UPPER CAP AFT FLANGE BETWEEN XORS 672.5 AND XORS 762, IAW VT-SAA EA 011-5710-01-A8724 REV IR AND UPS EO MD11-5710-785 - [SDR IPXA2020111962580](https://openairdocs.org/sdr/IPXA2020111962580.md): Skin · chafed · Nov 4, 2020 · N272UP · Doug MD11F · Wing, Plate/Skin > INSPECTION TYPE: 4C RT WING DROOP LEADING EDGE INBOARD LEADING EDGE SKIN REPAIR DOUBLER IS CHAFED. REPAIRED CHAFED RT WING DROOP LEADING EDGE INBOARD LEADING EDGE SKIN REPAIR AT STA XDLE 309.934, IAW MD-11 SRM 57-40-01, REPAIR 15, FIGURE 202. (MAJOR) - [SDR IPXA2020111762512](https://openairdocs.org/sdr/IPXA2020111762512.md): Spar Cap · corroded · Nov 4, 2020 · N272UP · Doug MD11F · Wing Spar > INSPECTION TYPE: 4C LT WING REAR SPAR LOWER CAP HAS CORROSION JUST BELOW NR 3 SPOILER. REPAIRED LT WING REAR SPAR LOWER CAP/VERTICAL FLANGE AFT SURFACE/BETWEEN XORS 582 & XORS 587, IAW VT-SAA EA 011-5710-01-A8708 REV. IR AND UPS EO MD11-5710-78522-A. (MINOR) - [SDR IPXA2020111762511](https://openairdocs.org/sdr/IPXA2020111762511.md): Spar Cap · corroded · Nov 4, 2020 · N272UP · Doug MD11F · Wing Spar > INSPECTION TYPE: 4C RT WING AFT LOWER SPAR CAP HAS EXFOLIATION CORROSION INBOARD OF OUTBOARD FLAP OUTBOARD HINGE.REPAIRED CORRODED RT WING REAR SPAR LOWER CAP VERTICAL FLANGE AFT SURFACE, HORIZONTAL AFT FLANGE UPPER AND LOWER SURFACES/BETWEEN XORS 720 & XORS 7 - [SDR IPXA2020111762497](https://openairdocs.org/sdr/IPXA2020111762497.md): Skin · dented · Nov 4, 2020 · N272UP · Doug MD11F · Trailing Edge Flaps > INSPECTION TYPE: 4C LT WING INBOARD FLAP UPPER SKIN HAS 2 EA LARGE DENTS 45" FROM TRAILING EDGE AND 77' FROM INBOARD END. REPAIRED DENTED LT WING INBOARD FLAP UPPER SKIN AT STA XIFH 203 AND XIFH 39, IAW MD-11 SRM 57-00-01, REPAIR 1, FIGURE 201. (MAJOR) - [SDR IPXA2020111862543](https://openairdocs.org/sdr/IPXA2020111862543.md): Longeron · cracked · Nov 4, 2020 · N272UP · Doug MD11F · Fuselage Main, Longeron/Stringer > INSPECTION TYPE: 4C MAIN CABIN LONGERON 14R IS CRACKED AT STA 1219. REPAIRED CRACKED MAIN CABIN LONGERON 14R BETWEEN STA 1211-1226.5, IAW MD-11 SRM 53-00-05, REPAIR 1, FIGURE 201 & 202. (MAJOR) - [SDR IPXA2020111562383](https://openairdocs.org/sdr/IPXA2020111562383.md): Skin · dented · Nov 4, 2020 · N272UP · Doug MD11F · Aerodynamic Fairings > INSPECTION TYPE: 2C TAILCONE LT SKIN HAS A DENT AT 7 O'CLOCK POSITION STA 2184. REPAIRED DENT ON TAILCONE LT SKIN AT 7 O'CLOCK POSITION STA 2184, IAW SRM 53-00-00 REPAIR GENERAL FIG 204. (MINOR) - [SDR IPXA2020110862141](https://openairdocs.org/sdr/IPXA2020110862141.md): Spar Cap · corroded · Nov 4, 2020 · N272UP · Doug MD11F · Wing Spar > INSPECTION TYPE: 2C RT WING AFT LOWER SPAR CAP HAS CORROSION AT XORS STA 705. REPAIRED RT WING AFT LOWER SPAR CAP BETWEEN XORS STA 703-XORS STA 708, IAW SRM 57-00-10 FIG 101 ALLOWABLE DAMAGE 1. (MINOR). - [SDR IPXA2020112262657](https://openairdocs.org/sdr/IPXA2020112262657.md): Skin · cracked · Nov 3, 2020 · N272UP · Doug MD11F · Trailing Edge Flaps > INSPECTION TYPE: 2C LT OUTBOARD FLAP INBOARD HINGE FITTING CRACK. REMOVED AND REPLACED LT OUTBOARD FLAP ASSEMBLY, IAW AMM 27-50-30-000-802 AND AMM 27-50-30-400-802. (MINOR) - [SDR IPXA2020112162625](https://openairdocs.org/sdr/IPXA2020112162625.md): Rivet · loose · Nov 3, 2020 · N272UP · Doug MD11F · Engine Air Intake System > INSPECTION TYPE: 4C NR 2 ENGINE INLET NOSE COWL LIP HAS NUMEROUS LOOSE AND WORKING RIVETS. REPAIRED NR 2 ENGINE INLET NOSE COWL LIP LOOSE AND WORKING RIVETS, IAW VT-SAA EA 011-7110-01-A8735 REV IR AND UPS EO MD11-7110-78559-A. (MINOR) - [SDR IPXA2020112162624](https://openairdocs.org/sdr/IPXA2020112162624.md): Angle · cracked · Nov 3, 2020 · N272UP · Doug MD11F · Wing Miscellaneous Structure > INSPECTION TYPE: 4C LT WING FIXED LEADING EDGE TEE ANGLE SUPPORT FOR PANEL 515FB IS CRACKED. REMOVED AND REPLACED CRACKED LT WING FIXED LEADING EDGE TEE ANGLE SUPPORT FOR PANEL 515FB, IAW MD-11 SRM 51-35-01. (MINOR) - [SDR IPXA2020112162619](https://openairdocs.org/sdr/IPXA2020112162619.md): Stiffener · cracked · Nov 3, 2020 · N272UP · Doug MD11F · Fuselage Miscellaneous Structure > INSPECTION TYPE: 4C RT MLG WHEEL WELL AFT OUTBOARD WEB 4TH VERTICAL STIFFENER IS CRACKED. REMOVED AND REPLACED CRACKED RT MLG WHEEL WELL AFT OUTBOARD WEB 4TH VERTICAL STIFFENER, IAW MD-11 SRM 51-35-01. (MINOR) - [SDR IPXA2020111862550](https://openairdocs.org/sdr/IPXA2020111862550.md): Stiffener · cracked · Nov 3, 2020 · N272UP · Doug MD11F · Fuselage Miscellaneous Structure > INSPECTION TYPE: 4C AFT CARGO RT VERTICAL STIFFENER 38" FROM CENTER LINE AT STA 1841 IS CRACKED. REMOVED AND REPLACED CRACKED AFT CARGO RT VERTICAL STIFFENER 38" FROM CENTER LINE AT STA 1841, IAW MD-11 SRM 51-33-01. (MINOR) - [SDR IPXA2020111862547](https://openairdocs.org/sdr/IPXA2020111862547.md): Stiffener · cracked · Nov 3, 2020 · N272UP · Doug MD11F · Fuselage Miscellaneous Structure > INSPECTION TYPE: 4C AFT CARGO RT VERTICAL STIFFENER 31" FROM CENTER LINE AT STA 1841 IS CRACKED. REMOVED AND REPLACED CRACKED RT VERTICAL STIFFENER 31" FROM CENTER LINE AT STA 1841, IAW MD-11 SRM 51-33-01. (MINOR) - [SDR IPXA2020111862546](https://openairdocs.org/sdr/IPXA2020111862546.md): Stiffener · cracked · Nov 3, 2020 · N272UP · Doug MD11F · Fuselage Miscellaneous Structure > INSPECTION TYPE: 4C AFT CARGO RT VERTICAL STIFFENER 38" FROM CENTER LINE AT STA 1841 IS CRACKED. REMOVED AND REPLACED CRACKED AFT CARGO RT VERTICAL STIFFENER 38" FROM CENTER LINE AT STA 1841, IAW MD-11 SRM 51-33-01. (MINOR) - [SDR IPXA2020111962562](https://openairdocs.org/sdr/IPXA2020111962562.md): Skin · gouged · Nov 3, 2020 · N272UP · Doug MD11F · Wing, Plate/Skin > INSPECTION TYPE: 4C RT WING FIXED LEADING EDGE SKIN SHROUD OUTBOARD OF NR 8 SLAT IS GOUGED. REPAIRED GOUGED RT WING FIXED LEADING EDGE SKIN SHROUD BETWEEN XOS 1187-XOS 1191, IAW MD-11 SRM57-40-01, REPAIR 16, FIGURE 201. (MAJOR) - [SDR IPXA2020111862530](https://openairdocs.org/sdr/IPXA2020111862530.md): Floorbeam · cracked · Nov 3, 2020 · N272UP · Doug MD11F · Fuselage Main, Floor Beam > INSPECTION TYPE: 4C FWD CARGO FLOOR BEAM TEE ANGLE AT STA 6-70 ABOVE LONGERON 43R IS CRACKED. REMOVED AND REPLACED CRACKED FWD CARGO FLOOR BEAM TEE ANGLE AT STA 6-70 ABOVE LONGERON 43R, IAW MD-11 SRM 51-33-01. (MINOR) - [SDR IPXA2020111862522](https://openairdocs.org/sdr/IPXA2020111862522.md): Truss · cracked · Nov 3, 2020 · N272UP · Doug MD11F · Fuselage Main, Structure > INSPECTION TYPE: 4C CENTER ACCESSORY COMPARTMENT LONGERON 27R TRUSS FITTING BETWEEN STA 1139-1159 IS CRACKED. REMOVED AND REPLACED CRACKED CENTER ACCESSORY COMPARTMENT LONGERON 27R TRUSS FITTING BETWEEN STA 1139-1159, IAW MD-11 SRM 51-33-01. (MINOR) - [SDR IPXA2020111762505](https://openairdocs.org/sdr/IPXA2020111762505.md): Intercostal · cracked · Nov 3, 2020 · N272UP · Doug MD11F · Fuselage Miscellaneous Structure > INSPECTION TYPE: 4C RT A/C BAY INTERCOSTAL BETWEEN STA 535-555 IS CRACKED. REMOVED AND REPLACED CRACKED RT A/C BAY INTERCOSTAL BETWEEN STA 535-555, IAW MD-11 SRM 51-35-01. (MINOR) Next page: https://openairdocs.org/deregistered/N272UP-2025-07-13/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 = 'N272UP' AND deregistration_id = 'N272UP-2025-07-13' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N272UP-2025-07-13/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.