# Service difficulty reports: N273UP

A list on [N273UP](https://openairdocs.org/aircraft/N273UP.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 · 305 reports

- [SDR IPXA2025081217326](https://openairdocs.org/sdr/IPXA2025081217326.md): Battery · inoperative · Aug 12, 2025 · N273UP · Doug MD11F · Emergency Lighting
  > EMERGENCY LIGHT TEST SHOWING BAT LO ON EAD. EMERGENCY LIGHTING BATTERY POWER SUPPLY R&R IAW AMM 33-51-01/401. LIGHTS CHECKS SERVICEABLE.
- [SDR IPXA2025060641156](https://openairdocs.org/sdr/IPXA2025060641156.md): Skin · corroded · May 17, 2025 · N273UP · Doug MD11F · Fuselage Main, Plate/Skin
  > FOUND CORROSION AT M. CABIN R/H TUNNEL AFT OF STA 1361. ACCOMPLISH REPAIR PER EO-93960-REQ1 AND VT-SAA EA 011-5730-01-B0493, REV. I/R, PRIOR TO FURTHER FLIGHT.
- [SDR IPXA2025060501984](https://openairdocs.org/sdr/IPXA2025060501984.md): Longeron · corroded · May 15, 2025 · N273UP · Doug MD11F · Fuselage Main, Longeron/Stringer
  > EXFOLIATED CORROSION AT FWD CARGO SUMP AREA STA 979-989 BL"0"/LONGERON 52.040-43, ATA 53-10. INSTALLED 2 EA LONGERON SECTION, 3 EA LONGERON SPLICE AND 1 EA DRAIN AT FWD CARGO SUMP AREA STA 969.6 TO STA 1009.5 IAW E.A.# 011-5310-01-B0490 P3 STEP 12. ACCOMPLISH
- [SDR IPXA2025052303083](https://openairdocs.org/sdr/IPXA2025052303083.md): Support · damaged · May 15, 2025 · N273UP · Doug MD11F · Fuselage Miscellaneous Structure
  > FWD CARGO/CEILING PANEL SUPPORT IS DAMAGED AT STA 987/RBL107.MARKED 040-39, ATA 51-00.INSTALLED REPAIR ANGLE, INSTALLED FASTENERS IN NET TO CLEARENCE FIT HOLES, FILL REAMED HOLE WITH PR1422 SEALANT, AND INSTALLED CLIP NUT AT FWD CARGO/CEILING PANEL SUPPORT STA
- [SDR IPXA2025060884755](https://openairdocs.org/sdr/IPXA2025060884755.md): Rib · cracked · May 14, 2025 · N273UP · Doug MD11F · Wing, Rib/Bulkhead
  > RH FIXED LE HAS A CRACK AT #3 RIB O/B OF #12 SLAT TRACK. INSTALLED 1EA RIB AT O/B OF #12 SLAT TRACK IN RH WING FIXED L/E COMPARTMENT AT STA XOS=794 REF. MD-11 SRM 51-33-01-0G-0 AND SRM 51-35-01-0G-0.
- [SDR IPXA2025060864761](https://openairdocs.org/sdr/IPXA2025060864761.md): Frame · corroded · May 13, 2025 · N273UP · Doug MD11F · Fuselage Main, Frame
  > CORROSION ON FRAME INSIDE FWD AVI BAY BETWEEN STA Y440 TO Y449 IN BILGE AREA ATA53-10. NSTALLED ALL REPAIR PARTS -1 FRAME SECTION, 2EA -2 SPLICE ANGLES, 2EA -3 SPLICE ANGLES, 2EA INTERCOSTALS, 2EA STRAPS, 2EA INTERCOSTAL CLIPS AND 2EA INTERCOSTAL ANGLES REF. E
- [SDR IPXA2024111830459](https://openairdocs.org/sdr/IPXA2024111830459.md): Lens · detached · Nov 16, 2024 · N273UP · Doug MD11F · Emergency Lighting
  > L1 DOOR EMERGENCY FLOOD LIGHT LENS WILL NOT HOLD TO ASSEMBLY REMOVED AND REPLACED L1 DOOR EMERGENCY LIGHT ASSY PER AMM 33-52-02. OPS CHECK GOOD
- [SDR IPXA2024110111230](https://openairdocs.org/sdr/IPXA2024110111230.md): Access Panel · damaged · Nov 1, 2024 · N273UP · Doug MD11F · Wing Structure
  > **SDR FILED OPEN**LIFT WING LOWER SURFACE, TRAILING EDGE PANEL 541KB APPEARS TO HAVE CIRCULAR REPAIR TOP COVERING MISSING. REINSTALLED PANEL 541KB REFER T3F18E00GZ3Q
- [SDR IPXA2024100191073](https://openairdocs.org/sdr/IPXA2024100191073.md): Door · faulted · Oct 1, 2024 · N273UP · Doug MD11F · Passenger/Crew Doors
  > LEFT FORWARD PASSENGER DOOR WILL NOT OPEN OR CLOSE. RESET BREAKERS. PERFORMED OPS CHECK OF THE L1 DOOR IAW AMM 52-10-01-700-801.OPS CHECK GOOD.
- [SDR IPXA2024100169712](https://openairdocs.org/sdr/IPXA2024100169712.md): Computer · faulted · Sep 29, 2024 · N273UP · Doug MD11F · Fuel Indicating System
  > WITH FSCIN IN AUTO MODE, THE SYS CREATED A 1500LBS IMBALANCE BETWEEN TANKS 1 AND 3. ALSO NOT BURNING FUEL EVENLY FROM EA MAIN TANK. TANK 2 HAD 5K LESS THAN TANK 1 AND 3K LESS THAN TANK 3 REMOVED & REPLACED FSC PER MD11 AMM 28-08-01-000 & 400. PERFORM RTS OF FS
- [SDR IPXA2024050715606](https://openairdocs.org/sdr/IPXA2024050715606.md): Skin · damaged · May 4, 2024 · N273UP · Doug MD11F · Passenger/Crew Doors
  > L1 DOOR TOP FORWARD EDGE SKIN DAMAGED. REPAIRED DAMAGE REF EO-90308-REQ1. THIS REPAIR IS PERMANENT.
- [SDR IPXA2024050615606](https://openairdocs.org/sdr/IPXA2024050615606.md): Skin · damaged · May 4, 2024 · N273UP · Doug MD11F · Passenger/Crew Doors
  > **SDR FILED OPEN** L1 DOOR TOP FORWARD EDGE SKIN DAMAGED REPAIRED DAMAGE REF EO-90308-REQ1. THIS REPAIR IS PERMANENT.
- [SDR IPXA2024012453082](https://openairdocs.org/sdr/IPXA2024012453082.md): Switch · inoperative · Jan 20, 2024 · N273UP · Doug MD11F · Emergency Lighting
  > EMERGENCY LIGHTING SYSTEM WILL NOT TEST R/R PUSH TO TEST SWITCH S1-402 PER WDM 33-51-01-4 PG 4 OPS CHECKS GOOD
- [SDR IPXA2024012253082](https://openairdocs.org/sdr/IPXA2024012253082.md): Switch · no test · Jan 20, 2024 · N273UP · Doug MD11F · Emergency Lighting
  > **SDR FILED OPEN**EMERGENCY LIGHTING SYSTEM WILL NOT TEST R/R PUSH TO TEST SWITCH S1-402 PER WDM 33-51-01-4 PG 4 OPS CHECKS GOOD
- [SDR IPXA2023122187687](https://openairdocs.org/sdr/IPXA2023122187687.md): Unknown · unknown · Dec 21, 2023 · N273UP · Doug MD11F · Emergency Lighting
  > ON F/O PREFLIGHT EMERGENCY LIGHTING SYSTEM TEST FUNCTION INOP. ACCOMPLISHED FIM 33-51-02-00, NO FAULTS NOTED.
- [SDR IPXA00300](https://openairdocs.org/sdr/IPXA00300.md): Unknown · unknown · Nov 15, 2023 · N273UP · Doug MD11F · Passenger/Crew Doors
  > R1 DOOR WOULD NOT ARM - HANDLE WOULD NOT STOW UP (ARMED) POSITION ARMING LEVER INSIDE WOULD NOT STOW ALL THE WAY, ARMING LEVER OUTSIDE WAS ALSO STICKING OUT BUT INDICATIONS SHOWED DOOR ARMED. FOUND €˜ARMED€™ FLAG WINDOW PLATE LOWER SIDE ON DOOR GETTING CAUGH
- [SDR IPXA2023081093861](https://openairdocs.org/sdr/IPXA2023081093861.md): Seat Track · unknown · Aug 9, 2023 · N273UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:NA*MAJOR REPAIR* SEAT TRACK DAMAGE SAT 1158 RBL 75.25REPAIRED PER E.O.MD11-5310-87827-A
- [SDR IPXA2023080893839](https://openairdocs.org/sdr/IPXA2023080893839.md): Floor Panel · damaged · Aug 7, 2023 · N273UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:N/AFLOOR PANEL AEA 7435-14 DAMAGED.FABRICATED NEW PANEL PER SREO MD11-5320-27386.
- [SDR IPXA2023080893838](https://openairdocs.org/sdr/IPXA2023080893838.md): Floor Panel · damaged · Aug 7, 2023 · N273UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:N/AFLOOR PANEL AEA7435-18 DAMAGEDFABRICATED NEW PANEL PER EO MD11-5320-27386.
- [SDR IPXA2023080393792](https://openairdocs.org/sdr/IPXA2023080393792.md): Battery · discharged · Aug 3, 2023 · N273UP · Doug MD11F · Emergency Lighting
  > EMER LT BAT 1 LO1. DEFERRED PER MEL 33-50-4 WITH M811071. DMP C/W PLACARD INSTALLED.REVERSED DMP & REVERSED DMP FOUND BATT LOW. REPLACED EMER LIGHTING POWER SUPPLY IAW MD11 AMM 33-51-01. OPS CHECK GOOD. THIS CLARS M811071, PLACARD REMOVED.
- [SDR IPXA2023080293779](https://openairdocs.org/sdr/IPXA2023080293779.md): Battery · inoperative · Aug 2, 2023 · N273UP · Doug MD11F · Emergency Lighting
  > EMER LT BAT I LO. PLACED ON MEL 33 50 4 C/N M 811000 DI LGO UPDATED PLACARD INSTALLED DMP.PERFORMED OPS CK OF EMERGENCY LIGHTS, DMP REVERSED TC0050 THIS CLEARS M811000, PLACARD REMOVED AMM 33-52-01-700-805.
- [SDR IPXA2023071393657](https://openairdocs.org/sdr/IPXA2023071393657.md): Handle · inoperative · Jul 13, 2023 · N273UP · Doug MD11F · Emergency Equipment
  > INSPECTION TYPE:NAF.O. OVERHEAD HADLE INOP SCREW STRIPPEDRESERVED HANDLE ON FO'S OVERBD REF AMM 20 00 00/001 STARTED ILLEG OPS CHECK GOOD
- [SDR IPXA2023070793616](https://openairdocs.org/sdr/IPXA2023070793616.md): Bracket · gouged · Jun 29, 2023 · N273UP · Doug MD11F · Fuselage, Landing Gear Attach Fittings
  > INSPECTION TYPE:3CNLG COMPARTMENT RETRACT ACTUATOR BRACKET ANTI-ROTATION FITTING IS GOUGED AT STA Y=596.REPAIRED BRACKET ASSY. AT THE NLG COMPARTMENT RETRACT ACTUATOR BRACKET AT STA Y=596 IAW VTSAA EA 011-5310-01-B0022 I/R AND UPS EO MD11-5310-87538-A DATED 07
- [SDR IPXA2023070793615](https://openairdocs.org/sdr/IPXA2023070793615.md): Bracket · gouged · Jun 29, 2023 · N273UP · Doug MD11F · Landing Gear Doors
  > INSPECTION TYPE:3CNLG COMPARTMENT RETRACT ACTUATOR BRACKET ANTI-ROTATION FITTING HAS IS GOUGED AT STA Y=596.REPAIRED BRACKET ASSY. AT THE NLG COMPARTMENT RETRACT ACTUATOR BRACKET AT STA Y=596 IAW VTSAA EA 011-5310-01-B0022 I/R AND UPS EO MD11-5310-87538-A DATE
- [SDR IPXA2023070693604](https://openairdocs.org/sdr/IPXA2023070693604.md): Support Fitting · corroded · Jun 10, 2023 · N273UP · Doug MD11F · Fuselage, Landing Gear Attach Fittings
  > INSPECTION TYPE:3CFOUND NOSE GEAR L/H TRUNNION WITH CORROSION AT STA Y=587.REPAIRED CORRODED L/H TRUNNION AT THE NOSE GEAR SUPPORT FITTING AT STA Y=587 IAW VTSAA EA 011-5310-01-A9996 I/R AND UPS EO MD11-5310-87549-A DATED 07/05/23. (MINOR)
- [SDR IPXA2023070793607](https://openairdocs.org/sdr/IPXA2023070793607.md): Support Fitting · corroded · Jun 10, 2023 · N273UP · Doug MD11F · Fuselage, Landing Gear Attach Fittings
  > INSPECTION TYPE:3CFOUND NOSE GEAR R/H TRUNNION WITH CORROSION AT STA Y=587.REPAIRED CORRODED SUPPORT FITTING AT THE R/H NOSE GEAR TRUNNION AT STA Y=587 IAW VTSAA 011-5310-01-B0009 I/R AND UPS EO MD11-5310-87550-A DATED 07/05/23 (MINOR)
- [SDR IPXA2023070893624](https://openairdocs.org/sdr/IPXA2023070893624.md): Hinge · worn · Jun 9, 2023 · N273UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3CR/H I/B FLAP O/B HINGE LOWER O/B LUG HOLE #6 IS OUT OF LIMITS AT STA XW=-254.REPAIRED HINGE ASSY AT THE R/H I/B FLAP O/B HINGE AT STA XW=-254 IAW VTSAA EA 011-5740-01-A9988 I/R, UPS EO MD11-5750-87385-A DATED 07/07/23 AND FAA FORM 8100-9 SIGN
- [SDR IPXA2023070893623](https://openairdocs.org/sdr/IPXA2023070893623.md): Hinge · worn · Jun 9, 2023 · N273UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3CR/H I/B FLAP O/B HINGE LOWER I/B LUG HOLE #7 IS OUT OF LIMITS AT STA XW=-254.REPAIRED HINGE ASSY. AT THE R/H I/B FLAP O/B HINGE AT STA XW=-254 IAW VTSAA EA 011-5740-01-A9988 I/R, UPS EO MD11-5750-87385-A DATED 07/07/23 AND FAA FORM 8100-9 SIG
- [SDR IPXA2023070193578](https://openairdocs.org/sdr/IPXA2023070193578.md): Elevator · broken · Jun 8, 2023 · N273UP · Doug MD11F · Elevator Structure
  > INSPECTION TYPE:3CL/H I/B ELEVATOR TOP I/B SIDE HAS A BROKEN OFF UPPER FLANGE AT STA XE=125.8.REPAIRED ELEVATOR UPPER FLANGE AT THE L/H I/B SIDE AT STA XE=125.8 IAW VTSAA EA 011-5520-01-A9979 I/R AND UPS EO MD11-5520-87368-A DATED 06/27/23 AND FAA FORM SIGNED
- [SDR IPXA2023070893618](https://openairdocs.org/sdr/IPXA2023070893618.md): Bracket · corroded · Jun 7, 2023 · N273UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3CL/H WING A/C SIDE I/B FLAP O/B HINGE #3 LUG I/B FLAP I/B FACE HAS CORROSION AT STA XW=254.000.REPAIRED CORRODED HINGE BRACKET ASSY. AT THE L/H WING A/C SIDE I/B FLAP O/B HINGE AT STA XW=254.000 IAW VTSAA EA 011-5740-01-B0002 I/R, UPS EO MD11-
- [SDR IPXA2023070793612](https://openairdocs.org/sdr/IPXA2023070793612.md): Stringer · cracked · Jun 7, 2023 · N273UP · Doug MD11F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:3C*** MAJOR REPAIR *** UPPER CENTER AUXILIARY TANK STRINGER 52 IS CRACKED BETWEEN STA XCW=81 AND XCW=17.REPAIRED CRACKED STRINGER 52 AT THE UPPER CENTER AUXILIARY TANK BETWEEN STA XCW=81 AND XCW=17 IAW VTSAA EA 011-5710-01-A9993 I/R, UPS EO MD1
- [SDR IPXA2023070893622](https://openairdocs.org/sdr/IPXA2023070893622.md): Hinge · corroded · Jun 7, 2023 · N273UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3CL/H WING FLAP SIDE I/B FLAP O/B HINGE #7 LUG BORE HAS CORROSION AT STA XW=-254.REPAIRED CORRODED HINGE ASSY AT THE L/H WING FLAP SIDE I/B FLAP O/B HINGE AT STA XW=-254 IAW VTSAA EA 011-5740-01-B0017 I/R, UPS EO MD11-5750-87572-A DATED 07/07/2
- [SDR IPXA2023070893621](https://openairdocs.org/sdr/IPXA2023070893621.md): Hinge · corroded · Jun 7, 2023 · N273UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3CL/H WING FLAP SIDE I/B FLAP O/B HINGE #6 LUG BORE HAS CORROSION AT STA XW=254.REPAIRED CORRODED HINGE ASSY. AT THE L/H WING FLAP SIDE I/B FLAP O/B HINGE AT STA XW=254 IAW VTSAA EA 011-5740-01-B0017 I/R AND EO MD11-5750-87572-A DATED 07/07/23
- [SDR IPXA2023070893619](https://openairdocs.org/sdr/IPXA2023070893619.md): Bracket · corroded · Jun 7, 2023 · N273UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3CL/H WING A/C SIDE I/B FLAP O/B HINGE #3 LUG O/B FACE HAS CORROSION AT STA XW=254.000.REPAIRED CORRODED HINGE BRACKET ASSY. AT THE L/H WING A/C SIDE I/B FLAP O/B HINGE AT STA XW=254.000 IAW VTSAA EA 011-5740-01-B0002 I/R, UPS EO MD11-5740-8756
- [SDR IPXA2023070793611](https://openairdocs.org/sdr/IPXA2023070793611.md): Bracket · corroded · Jun 7, 2023 · N273UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3CR/H WING A/C SIDE I/B FLAP O/B HINGE #3 LUG I/B FACE HAS CORROSION AT STA XW=-254.REPAIRED CORRODED HINGE AT THE R/H WING A/C SIDE I/B FLAP O/B HINGE IAW VTSAA EA 011-5740-01-B0006 I/R AND UPS EO MD11-5740-87565-A DATED 07/05/23 AND FAA FORM
- [SDR IPXA2023070793608](https://openairdocs.org/sdr/IPXA2023070793608.md): Bracket · corroded · Jun 7, 2023 · N273UP · Doug MD11F · Leading Edge Devices
  > INSPECTION TYPE:3CR/H WING A/C SIDE I/B FLAP O/B HINGE #3 LUG O/B FACE HAS CORROSION AT STA XW=-254.000.REPAIRED CORRODED HINGE AT THE R/H WING A/C SIDE I/B FLAP O/B HINGE AT STA XW=-254.000 IAW VTSAA EA 011-5740-01-B0006 I/R, UPS EO MD11-5740-87565-A DATED 0
- [SDR IPXA2023070693603](https://openairdocs.org/sdr/IPXA2023070693603.md): Stringer · cracked · Jun 7, 2023 · N273UP · Doug MD11F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:3CUPPER CENTER AUXILIARY TANK HAS CRACK BETWEEN STA XCW=-46 AND XCW=-81 ON LOWER STRINGER 45.REPAIRED CRACKED LOWER STRINGER 45 AT THE UPPER CENTER AUXILIARY TANK BETWEEN STA XCW=-46 AND XCW=-81 IAW SRM 57-10-03 REPAIR 1 FIG 201. (MAJOR)
- [SDR IPXA2023070693602](https://openairdocs.org/sdr/IPXA2023070693602.md): Stringer · cracked · Jun 7, 2023 · N273UP · Doug MD11F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:3CUPPER CENTER AUXILIARY TANK HAS A CRACK BETWEEN STA XCW=81 AND XCW=17 ON LOWER STRINGER 49.REPAIRED CRACKED LOWER STRINGER 49 AT THE UPPER CENTER AUXILIARY TANK BETWEEN STA XCW=81 AND XCW=17 IAW 57-10-03 REPAIR 1 FIG 201. (MAJOR)
- [SDR IPXA2023070693601](https://openairdocs.org/sdr/IPXA2023070693601.md): Stringer · cracked · Jun 7, 2023 · N273UP · Doug MD11F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:3CUPPER CENTER AUXILIARY TANK HAS CRACKS LOCATED BETWEEN STA XCW=17.0 AND XCW=46.5 ON LOWER STRINGER 47.REPAIRED CRACKED LOWER STRINGER 47 AT THE UPPER CENTER AUXILIARY TANK AT STA XCW=17.0 AND XCW=46.5 IAW SRM 57-10-03 REPAIR 1 FIG 201. (MAJOR
- [SDR IPXA2023070693600](https://openairdocs.org/sdr/IPXA2023070693600.md): Bracket · corroded · Jun 7, 2023 · N273UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3CL/H WING A/C SIDE O/B FLAP O/B HINGE #3 LUG I/B FACE HAS CORROSION.REPLACED HINGE ASSY. AT THE L/H WING A/C SIDE O/B FLAP O/B HINGE IAW AMM 57-53-01-400-801. (MINOR)
- [SDR IPXA2023070693599](https://openairdocs.org/sdr/IPXA2023070693599.md): Bracket · corroded · Jun 7, 2023 · N273UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3CR/H WING A/C SIDE O/B FLAP O/B HINGE #1 LUG BORE HAS CORROSION.REPLACED HINGE ASSY. AT THE R/H WING A/C SIDE O/B FLAP O/B HINGE IAW AMM 57-53-01-400-801. (MINOR)
- [SDR IPXA2023070693598](https://openairdocs.org/sdr/IPXA2023070693598.md): Bracket · corroded · Jun 7, 2023 · N273UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3CR/H WING A/C SIDE O/B FLAP I/B HINGE #1 LUG BORE HAS CORROSION.REPLACED HINGE ASSY. AT THE R/H WING A/C SIDE O/B FLAP I/B HINGE IAW AMM 57-53-01-400-801. (MINOR)
- [SDR IPXA2023070193574](https://openairdocs.org/sdr/IPXA2023070193574.md): Lever · worn · Jun 7, 2023 · N273UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3CL/H WING A/C SIDE I/B FLAP I/B ACTUATOR MOUNT BOTH BUSHING ARE MIGRATED AT STA XIFH=116.850.REPAIRED BOTH LUG BORE AT THE L/H WING A/C SIDE I/B FLAP I/B ACTUATOR MOUNT AT STA XIFH=116.850 IAW VTSAA EA 011-5700-01-A9982 I/R AND UPS EO MD11-574
- [SDR IPXA2023070693597](https://openairdocs.org/sdr/IPXA2023070693597.md): Bracket · corroded · Jun 5, 2023 · N273UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3CL/H WING O/B FLAP I/B HINGE HAS CORROSION AT THE LOWER I/B ATTACH POINT.REPLACED CORRODED HINGE ASSY. AT THE L/H WING O/B FLAP I/B HINGE IAW AMM 57-53-01-400-801. (MINOR)
- [SDR IPXA2023070193577](https://openairdocs.org/sdr/IPXA2023070193577.md): Skin · corroded · Jun 3, 2023 · N273UP · Doug MD11F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:3CMAIN CABIN AT CTR WING TANK UPPER SURFACE L/H SIDE HAS CORROSION AT STA XCW=46.5 BETWEEN STRINGER 14 - 15.REPAIRED CORRODED SKIN AT THE MAIN CABIN CTR WING TANK UPPER SURFACE L/H SIDE HAS CORROSION AT STA XCW=46.5 BETWEEN STRINGER 14 - 15 IA
- [SDR IPXA2023070193576](https://openairdocs.org/sdr/IPXA2023070193576.md): Skin · corroded · Jun 2, 2023 · N273UP · Doug MD11F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:3CMAIN CABIN AT CENTER WING TANK UPPER SURFACE BETWEEN STRINGER 14 - 15 HAS CORROSION AT STA XCW=-17.00.REPAIRED CORRODED SURFACE AT THE MAIN CABIN CTR WING TANK UPPER SKIN BETWEEN STRINGER 14 -15 AT STA XCW=-17.00 IAW VTSAA EA 011-5730-01-A997
- [SDR IPXA2023041692892](https://openairdocs.org/sdr/IPXA2023041692892.md): Door · inoperative · Apr 15, 2023 · N273UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION TYPE:NAL/H L1 DOOR EMERGENCY RED HANDLE IS TURNED DOOR IS IN DOWN POSITION C/B FOR DOOR IS PULLEDPUT L1 DOOR BACK IN NORMAL CONDITION PER MD11 AMM 52-10 OK FOR SERVICE SEE LP# 528149 ITEM #2 FOR SERVICING PAX DOOR PNEUMATIC STORAGE RESERVOIR
- [SDR IPXA2023041792903](https://openairdocs.org/sdr/IPXA2023041792903.md): Reservoir · discharged · Apr 15, 2023 · N273UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION TYPE:NAL1 DOOR PNEUMATIC STORAGE RESERVOIR DEPLETED.SERVICED L1 DOOR PNEUMATIC STORAGE RESERVOIR PER MD11 AMM 12-25-04 PRESSURE WITHIN LIMITS.
- [SDR IPXA2022112288336](https://openairdocs.org/sdr/IPXA2022112288336.md): Battery · no test · Nov 21, 2022 · N273UP · Doug MD11F · Emergency Lighting
  > INSPECTION TYPE:NAON PDC EMERG. LIGHT TEST FAILING. EMER BATT LO MSG. REMOVED AND REPLACED EMERG. LIGHT BATTERY IAW AMM 33-51-01 OPS CHECK GOOD
- [SDR IPXA2022103187685](https://openairdocs.org/sdr/IPXA2022103187685.md): Aileron Sys · malfunctioned · Oct 31, 2022 · N273UP · Doug MD11F · Aileron Control System
  > ATB, T/O PLUS 1.5HR - LVL 2 AIL DEFLECT DISAG - REQUIRED DIVERT TO CGN. DEFLECTED AILERON SYSTEM DEFERRED IAW MEL 27-13-2-0-1 REV 37A. DMP PERFORMED. PLACARD INSTALLED AND DMI M794302 OPENED.R/R R/IB AILERON DEFLECTION ACTIVATOR PER AMM 27-16-01. OPS CKS GOOD

Next page: https://openairdocs.org/aircraft/N273UP/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 = 'N273UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N273UP/reports

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