# Service difficulty reports: N264UP

A list on [N264UP](https://openairdocs.org/aircraft/N264UP.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 3 · 101 reports

- [SDR IPXA2025101577220](https://openairdocs.org/sdr/IPXA2025101577220.md): Fuel Sys · warning message · Oct 15, 2025 · N264UP · Doug MD11F · Fuel Indicating System
  > DIVERTED DURING TAXI OUT WE RECEIVED LEVEL 2 LAT FUEL INBALANCE THAT CORRECTED ITSELF PRIOR TO TAKEOFF. AFTER TAKEOFF RECEIVED A LEVEL 2 FUEL QTY AND MISSING 2400 LBS. DIVERTED IN TO OAK DUE TO INTERMITTENT FUEL IN 1 TANK. NR1 FUEL QTY READS LOW. DEFERRED NR1
- [SDR IPXA2025101081235](https://openairdocs.org/sdr/IPXA2025101081235.md): Door · malfunctioned · Oct 9, 2025 · N264UP · Doug MD11F · Passenger/Crew Doors
  > L1 DOOR DOES NOT OPEN ELECTRICALLY. REPOSITIONED REAR FACING COURIER SEATS TO RETRACTED POSITION, OPERATED L1 DOOR ELECTRICALLY SEVERAL TIMES. NO FAULTS NOTED.
- [SDR IPXA2025082327433](https://openairdocs.org/sdr/IPXA2025082327433.md): Manifold · broken · Aug 23, 2025 · N264UP · Doug MD11F · Hydraulic System, Auxiliary
  > EMERGENCY DECLARED, DIVERSION, LVL 2 HYD 3 FAIL. STARTED HYD 3 ELEV OFF THEN HYD 3 OFF. REMOVED & REPLACED #3 ENGINE UPPER (LEFT) EDP PER AMM TASK 29-11-20-400-802 UP TO STEP (H). BLEED, LEAK & OPS CHECK REQUIRED. SERVICED #3 HYD SYSTEM IAW AMM 12-13-02/301.PE
- [SDR IPXA2025071643387](https://openairdocs.org/sdr/IPXA2025071643387.md): Connector · loose · Jul 15, 2025 · N264UP · Doug MD11F · Door System Wiring
  > L1 DOOR UNABLE TO ARM. FOUND CONNECTOR ON SOLENOID NEAR AFT BAR RECEIVER LOOSE. TIGHTENED AS REQUIRED. DOOR OPERATES AND ARMS NORMALLY. REF AMM TASK 52-10-01-700-801.
- [SDR IPXA2025032295372](https://openairdocs.org/sdr/IPXA2025032295372.md): Frame · cracked · Mar 6, 2025 · N264UP · Doug MD11F · Fuselage Main, Frame
  > AFT AVI COMP R/H SIDE FRAME STA 475 AT LIGHTING HOLE HAS A CRACKED. INSTALLED THE REPLACEMENT FRAME SPLICE, -3 REPAIR ANGLE, -5 REPAIR STRAP AND ROUND DOUBLER IN CANTED FRAME STA 469.173 RH SIDE AT FWD AVIONICS COMPARTMENT. REF. EA# 011-5310-01-B0421 REV P1
- [SDR IPXA2025032861369](https://openairdocs.org/sdr/IPXA2025032861369.md): Stiffener · cracked · Mar 4, 2025 · N264UP · Doug MD11F · Fuselage Miscellaneous Structure
  > AFT CGO COMP STA 1841 FLOOR PANEL FRAME RBL 26" STIFFENER HAS CRACKED. 74-059 ATA CODE 53. INSTALLED STIFFNER AT AFT CARGO COMP STA 1841 RBL26" REF MD11 SRM 51-33-01. ACCOMPLISHED REPAIR PER VT-SAA EA 011-5310-01-B0428, REV. IR.
- [SDR IPXA2025032961156](https://openairdocs.org/sdr/IPXA2025032961156.md): Frame · cracked · Mar 4, 2025 · N264UP · Doug MD11F · Fuselage Main, Frame
  > AFT CGO COMP WASTE TANK BILGE AREA STA 1986-2007 LONGERON 45L HAS CRACKED. 74-058 ATA CODE 53. INSTALLED 1EA LONGERON REPLACEMENT 45LH, 1 EA LONGERON SPLICE, 4 EA BRACKET, 3 EA FRAME SPLICE, 2EA FRAME,1EA FRAME SUPPORT 1EA STANCHION, 1EA FRAME SPLICE, 3EA I
- [SDR IPXA2025032261156](https://openairdocs.org/sdr/IPXA2025032261156.md): Longeron · cracked · Mar 4, 2025 · N264UP · Doug MD11F · Fuselage Main, Longeron/Stringer
  > AFT CGO COMP WASTE TANK BILGE AREA STA 1986-2007 LONGERON 45L HAS CRACKED. 74-058 ATA CODE 53 INSTALLED 1EA LONGERON REPL 45LH, 1 EA LONGERON SPLICE, 4 EA BRACKET, 3 EA FRAME SPLICE, 2EA FRAME, 1EA FRAME SUPPORT, 1EA STANCHION, 1EA FRAME SPLICE, 3EA INTERCOST
- [SDR IPXA2025011519891](https://openairdocs.org/sdr/IPXA2025011519891.md): Door · inoperative · Jan 15, 2025 · N264UP · Doug MD11F · Passenger/Crew Doors
  > L1 DOOR INOP. REMOVED AND REPLACED SOLENOID S2-730 REFERENCE AMM<BR>52-10-06-401. RAN DOOR MULTIPLE TIMES WITH NO FAULTS.<BR>THIS CLEARS 2834297. PLACARD REMOVED. OSD: 1/16/2025
- [SDR IPXA2024102979210](https://openairdocs.org/sdr/IPXA2024102979210.md): Skin · damaged · Oct 26, 2024 · N264UP · Doug MD11F · Wing, Plate/Skin
  > BIRDSTRIKE ON BASE-TO-FINAL TURN FOR PHL RWY 27R. POST-FLIGHT REVEALED EXTENSIVE DAMAGE TO RH WING LEADING EDGE INBOARD OF #3 ENGINE. INSTALLED R/H WING #2 SLAT PER AMM 27-80-20-400-802, PERFORMED ADJUSTMENT PER AMM 27-80-20-820-802 NO ISSUES NOTED AT THIS TI
- [SDR IPXA2024102879210](https://openairdocs.org/sdr/IPXA2024102879210.md): Skin · damaged · Oct 26, 2024 · N264UP · Doug MD11F · Wing, Plate/Skin
  > *SDR FILED OPEN* BIRDSTRIKE ON BASE-TO-FINAL TURN FOR PHL RWY 27R. POST-FLIGHT REVEALED EXTENSIVE DAMAGE TO RH WING LEADING EDGE INBOARD OF #3 ENGINE. REMOVED #2 INBOARD R/H SLAT PER AMM 27-80-20-000-802.
- [SDR IPXA2024072392472](https://openairdocs.org/sdr/IPXA2024072392472.md): Structure · damaged · Jul 19, 2024 · N264UP · Doug MD11F · Nacelle/Pylon Structure
  > *SUPPLEMENTAL SDR* #1 ENGINE PYLON DAMAGED. REMOVED AND REPLACED #1 ENG WING PYLON AFT LOWER FAIRING PER AMM 54-81-01 AND SRM 51-31-01.
- [SDR IPXA2024071992472](https://openairdocs.org/sdr/IPXA2024071992472.md): Fairing · damaged · Jul 19, 2024 · N264UP · Doug MD11F · Nacelle/Pylon, Main Frame
  > NR 1 ENGINE PYLON DAMAGED. UPDATE: PYLON DAMAGE IS REFERRING TO #1 ENG WING PYLON AFT LOWER FAIRING.
- [SDR IPXA2023121123218](https://openairdocs.org/sdr/IPXA2023121123218.md): Unknown · unknown · Dec 11, 2023 · N264UP · Doug MD11F · Passenger/Crew Doors
  > LEFT ENTRY DOOR OPEN CLOSE OPERATION INOP. FOUND DEBRIS LODGED BEHIND DRAWER ASSEMBLY UNDER COURIER SEATS. REMOVED MATERIAL LOCKED SEATS IN FORWARD POSITION DOOR OPERATES NORMALLY IAW AMM 52-11-02, SAFETY SENSOR WORKS NORMALLY IAW AMM 25-11-15-400-801. PLACAR
- [SDR IPXA2023120502061](https://openairdocs.org/sdr/IPXA2023120502061.md): Unknown · unknown · Dec 5, 2023 · N264UP · Doug MD11F · Passenger/Crew Doors
  > L1 ENTRY DOOR INOP FOUND COURIER SEAT NOT PROPERLY STOWED PAST GREEN STOW LINE MARKED ON FLOOR PER INSTRUCTIONS POSTED ABOVE L1 DOOR SWITCH. STOWED COURIER SEAT AND OPERATED L1 DOOR REF. AMM 52-11-02 OPS CHECK IS GOOD AT THIS TIME. THIS CLEARS DEFERRAL, PLACAR
- [SDR IPXA2023112188188](https://openairdocs.org/sdr/IPXA2023112188188.md): Unknown · unknown · Nov 21, 2023 · N264UP · Doug MD11F · Passenger/Crew Doors
  > L1 DOOR POWER SWITCH DOES NOT WORK AFTER LANDING. BOTH INSIDE & OUTSIDE SWITCH INOP. **OII 2** FOUND DEBRIS LODGED BEHIND COURIER SEATS PREVENTING FULL TRAVEL INTO STOW POSITION AND CONTACT WITH SAFETY SENSOR. REMOVED DEBRIS AND OPS CHECKED FORWARD PASSENGER D
- [SDR IPXA2023082894036](https://openairdocs.org/sdr/IPXA2023082894036.md): Adi · inoperative · Aug 27, 2023 · N264UP · Doug MD11F · Pitot/Static System
  > INSPECTION TYPE:NA*ATB* ALT FLAG CAPT'S ADI CLIMBOUT THRU 2500' WSHEAR DET FAIL CLIMB THRU 5000' ALT FLAG FO ADI CLIMBING 10,000' IAS FLAG CAPT ADI BTWN 14-15,000' CMP ALT WINDOW BLANK UNABLE TO SELECT 18,000 - CONTINUED FROM ITEM 1- IAS FLAG FO ADI @ 18,000RE
- [SDR IPXA2023042092928](https://openairdocs.org/sdr/IPXA2023042092928.md): Battery · discharged · Apr 20, 2023 · N264UP · Doug MD11F · Emergency Lighting
  > INSPECTION TYPE:NA*SDR FILED OPEN* ON PREFLIGHT EMERG LIGHT BAT 1 LOW (LEVEL 1) ALERT. DEFERRED EMERGENCY LIGHTING SYS PER MEL 33 50 4. DMP 33 50 4. C/W PLACARD INSTALLED M 807289 ASSIGNED. REVERSED DMP 30-50-04. T/S PER FIM 33-51-00-810-801. R&R EMERGENCY LT
- [SDR IPXA2023041192795](https://openairdocs.org/sdr/IPXA2023041192795.md): Stiffener · cracked · Apr 10, 2023 · N264UP · Doug MD11F · Standard Practices/Structures
  > INSPECTION TYPE:C1AFT CARGO COMPARTMENT STEP UP BULKHEAD HAS CRACKED STIFFNER AT STA Y1841 / STR 49RREMOVED, FABBED, AND INSTALLED STIFFNER AT STA. Y1841 AND STR 49 IAW SRM 51-31-01,SAA TRAVLER 70027364700001 AND DRAWING AGA7170
- [SDR IPXA2022102187316](https://openairdocs.org/sdr/IPXA2022102187316.md): Door · intermittent · Oct 19, 2022 · N264UP · Doug MD11F · Passenger/Crew Doors
  > L1 DOOR WORKING INTERMITTENTLY WITH INTERNAL & EXTERNAL CONTROL PANELS. DEFERRED L1 DOOR PER MEL 52-10-3-1-2-1-2 PLACARD INSTALLED. LINKED TO EO MD11-2520-85062.
- [SDR IPXA2022102087316](https://openairdocs.org/sdr/IPXA2022102087316.md): Control Panel · intermittent · Oct 19, 2022 · N264UP · Doug MD11F · Passenger/Crew Doors
  > L1 DOOR WORKING INTERMITTENTLY WITH INTERNAL & EXTERNAL CONTROL PANELS. LINKED TO EO MD11-2520-85062. INSTALLED 4 SCREWS AT MAIN CARGO DOOR CONTROL ACCESS PANEL DOOR IAW AMM 20-50-02.
- [SDR IPXA2022062483427](https://openairdocs.org/sdr/IPXA2022062483427.md): Door · inoperative · Jun 23, 2022 · N264UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION TYPE:NAR1 (ONE) DOOR INOPREPLACED R1 DOOR LOCK PIN (ILLEG) PER MM 52-10-06-401 AND R1 DOOR CONTROL RELAY PER RPM 20-10-00 DOOR OPS CHECK GOOD PER 52-10-01-201 ESR IPC 52-11-05-01
- [SDR IPXA2022021679058](https://openairdocs.org/sdr/IPXA2022021679058.md): Light · inoperative · Feb 15, 2022 · N264UP · Doug MD11F · Emergency Lighting
  > INSPECTION TYPE:N/A**SUPPLEMENTAL SDR** EMERGENCY LIGHTS INOP. DEFER EMERGENCY LIGHTS IAW MEL 33-50-4. DMP C/W INSTALLED PLACARD ASSIGNED M772946 TRIED REPLACING POWER SUPPLY, NO HELP. REF MM 33-50-00-700-802. ORIGINAL IS INSTALLEDREVERSED DMP T/S PER WDM 33-5
- [SDR IPXA2021090773666](https://openairdocs.org/sdr/IPXA2021090773666.md): Indicator · inoperative · Sep 3, 2021 · N264UP · Doug MD11F · Escape Slide
  > INSPECTION TYPE:N/AL-1 DOOR EVAC SLIDE REMOTE PRESSURE PRESS TO TEST IND INOP. DEFERRED PER MEL 25-61-2 M 755635 ASSIGNED C/W DMP VERIFIED SLIDE PRESSURE GOOD L-1 DOOR PLACARD INSTALLED.REPLACED L1 EVAC SLIDE SW IAW AMM 25-61-00. OPS CK GOOD. AMM 25-61-06. THI
- [SDR IPXA2021033067543](https://openairdocs.org/sdr/IPXA2021033067543.md): Floor Support · corroded · Mar 23, 2021 · N264UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: 3C FLOOR SUPPORT ANGLE IS CORRODED AT STA. 1387. REMOVED, FABRICATED AND REPLACED SUPPORT ANGLE IAW DWG. AEA0397 AND SRM 51-35-01. (MINOR)
- [SDR IPXA2021032967438](https://openairdocs.org/sdr/IPXA2021032967438.md): Seat Track · corroded · Mar 22, 2021 · N264UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:3CMAIN CABIN SEAT TRACK HAS CORROSION BETWEEN STA. 1501 TO 1521 AT X= -107.25.REPAIRED CORRODED SEAT TRACK BETWEEN STA. 1501 TO 1521 AT X= -107.25 IAW SRM 53-00-52 REPAIR 1 FIG. 201. (MAJOR)
- [SDR IPXA2021033067531](https://openairdocs.org/sdr/IPXA2021033067531.md): Skin · cracked · Mar 7, 2021 · N264UP · Doug MD11F · Wing, Plate/Skin
  > INSPECTION TYPE:3CL/H WING LOWER SKIN FUEL ACCESS PANEL BETWEEN STA. XORS. 683.4 TO XORS. 713.6 HAS 2 EA. SCREW HOLES WITH CRACKS.REPAIRED L/H LOWER SKIN IAW SRM 57-20-02 REPAIR 5 FIG. 201. (MINOR)
- [SDR IPXA2021032867387](https://openairdocs.org/sdr/IPXA2021032867387.md): Seat Track · corroded · Mar 4, 2021 · N264UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:3CMAIN CABIN SEAT TRACK IS CORRODED BETWEEN STA. 745 TO 800 AT X= 8.50.REPAIRED CORRODED SEAT TRACK BETWEEN STA. 745 TO 800 AT X= 8.50 IAW SRM 53-00-52 REPAIR 1 FIG. 201. (MAJOR)
- [SDR IPXA2021032867384](https://openairdocs.org/sdr/IPXA2021032867384.md): Intercostal · cracked · Mar 4, 2021 · N264UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:3CFWD. CARGO INTERCOSTAL IS CRACKED AT STA. 6-40 AND LOING. 42L.REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG. ACA7049 AND SRM 51-33-01. (MINOR)
- [SDR IPXA2021032867382](https://openairdocs.org/sdr/IPXA2021032867382.md): Support Fitting · cracked · Mar 4, 2021 · N264UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:3CCENTER TANK SUPPORT FITTING IS CRACKED AT STA. 1156 AND X= 01.REMOVED, FABRICATED AND REPLACED FITTING IAW DWG. APB7350 AND SRM 51-33-01. (MINOR)
- [SDR IPXA2021032867389](https://openairdocs.org/sdr/IPXA2021032867389.md): Seat Track · corroded · Mar 3, 2021 · N264UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:3CMAIN CABIN SEAT TRACK IS CORRODED AT STA. 1110 AND X= 8.50.REPAIRED CORRODED SEAT TRACK BETWEEN STA. 1099 TO 1119 AT X= 8.50 IAW SRM 53-00-52 REPAIR 5 FIG. 201. (MAJOR)
- [SDR IPXA2021032867388](https://openairdocs.org/sdr/IPXA2021032867388.md): Seat Track · corroded · Mar 3, 2021 · N264UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:3CMAIN CABIN SEAT TRACK IS CORRODED AT STA. 1119 AND X= -8.50.REPAIRED CORRODED SEAT TRACK AT STA. 1119 AND X= -8.50 IAW SRM 53-00-52 REPAIR 5 FIG. 201. (MAJOR)
- [SDR IPXA2021032867386](https://openairdocs.org/sdr/IPXA2021032867386.md): Cargo Track · corroded · Mar 3, 2021 · N264UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:3CAFT CARGO SEAT TRACK IS CORRODED BETWEEN STA. 1841-1967 AT X= -20.REMOVED, FABRICATED AND REPLACED SEAT TRACK BETWEEN STA. 1841-1967 AT X= -20 IAW DWG. AGA3855 AND SRM 51-31-01. (MINOR)
- [SDR IPXA2021032867385](https://openairdocs.org/sdr/IPXA2021032867385.md): Retainer · cracked · Mar 3, 2021 · N264UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:3CCENTER CARGOFLOOR PANEL RETAINER IS CRACKED AT STA. 1521 AND RBL 26.REMOVED, FABRICATED AND REPLACED RETAINER IAW DWG. AEA0341 AND SRM 51-31-01. (MINOR)
- [SDR IPXA2021032867383](https://openairdocs.org/sdr/IPXA2021032867383.md): Attach Angle · cracked · Mar 3, 2021 · N264UP · Doug MD11F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:3CCENTER CARO SLOPE PANEL ATTACH ANGLE IS CRACKED AT STA. 1661 L/H SIDE.REMOVED, FABRICATED AND REPLACED SLOPE PANEL ATTACH ANGLE IAW VT-SAA EA 011-5320-01-A8960 REV. I/R AND UPS EO MD11-5300-79690-A. (MINOR)
- [SDR IPXA2021032867381](https://openairdocs.org/sdr/IPXA2021032867381.md): Stiffener · cracked · Mar 3, 2021 · N264UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:3CAFT CARGO VERTICAL STIFFNER IS CRACKED AT STA. 1841 AND LBL 25.REMOVED, FABRICATED AND REPLACED STIFFNER IAW DWG. AGA7170 AND SRM 51-31-01. (MINOR)
- [SDR IPXA2021032867380](https://openairdocs.org/sdr/IPXA2021032867380.md): Floor Support · corroded · Mar 3, 2021 · N264UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:3CAFT CARGO FLOOR SUPPORT IS CORRODED AT STA. 1964 L/H SIDEUNDER PANEL 187DF.REMOVED, FABRICATED AND REPLACED SUPPORT IAW DWG. AGA7195 AND SRM 51-31-01. (MINOR)
- [SDR IPXA2021032867377](https://openairdocs.org/sdr/IPXA2021032867377.md): Stiffener · cracked · Mar 3, 2021 · N264UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:3CAFT CARGO VERTICAL STIFFNER IS CRACKED AT STA. 1841 AND LBL 19.REMOVED, FABRICATED AND REPLACED STIFFNER IAW DWG. AGA7170 AND SRM 51-33-01. (MINOR)
- [SDR IPXA2021032867376](https://openairdocs.org/sdr/IPXA2021032867376.md): Support · cracked · Mar 3, 2021 · N264UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:3CCENTER CARGO FLOOR BEAM SUPPORT IS CRACKED AT STA. 5-53, RBL=18.REMOVED, FABRICATED AND REPLACED FLOOR BEAM SUPPORT IAW DWG ADA0033 AND SRM 51-31-01. (MINOR)
- [SDR IPXA2021032867375](https://openairdocs.org/sdr/IPXA2021032867375.md): Support · cracked · Mar 3, 2021 · N264UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:3CCENTER CARGO FLOOR BEAM SUPPORT IS CRACKED AT STA. 5-32, RBL=18.REMOVED, FABRICATED AND REPLACED FLOOR BEAM SUPPORT IAW DWG. AFA3168 AND SRM 51-33-01. (MINOR)
- [SDR IPXA2021032767357](https://openairdocs.org/sdr/IPXA2021032767357.md): Truss Fitting · cracked · Mar 3, 2021 · N264UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:3CCAC COMPARTMENT LONGERON 27R TRUSS FITTING AT STA 1159 IS CRACKED.REMOVED AND REPLACED CRACKED CAC COMPARTMENT LONGERON 27R TRUSS FITTING AT STA 1159 IAW SRM 51-33-01 & 51-35-01. (MINOR)
- [SDR IPXA2021032767356](https://openairdocs.org/sdr/IPXA2021032767356.md): Stiffener · chafed · Mar 3, 2021 · N264UP · Doug MD11F · Aerodynamic Fairings
  > INSPECTION TYPE:3CFWD TAIL CONE R/H PATIO DOOR UPPER FWD STIFFENER IS CHAFED.REMOVED AND REPLACED CHAFED FWD TAIL CONE R/H PATIO DOOR UPPER FWD STIFFENER IAW SRM 51-35-01. (MINOR)
- [SDR IPXA2021032767354](https://openairdocs.org/sdr/IPXA2021032767354.md): Beam · bent · Mar 3, 2021 · N264UP · Doug MD11F · Aerodynamic Fairings
  > INSPECTION TYPE:3CFWD TAIL CONE FWD UPPER INTERCOSTAL (BEAM) AND WEB ARE BENT AT TAIL CONE SAFETY LATCH.REMOVED AND REPLACED BENT FWD TAIL CONE FWD UPPER INTERCOSTAL (BEAM) AND WEB AT TAIL CONE SAFETY LATCH IAW SRM 51-33-01 & 51-35-01. (MINOR)
- [SDR IPXA2021032767353](https://openairdocs.org/sdr/IPXA2021032767353.md): Frame · cracked · Mar 3, 2021 · N264UP · Doug MD11F · Aerodynamic Fairings
  > INSPECTION TYPE:3CFWD TAIL CONE R/H AFT FRAME IS CRACKED AT UPPER LATCH KEEPER.REPAIRED CRACKED FWD TAIL CONE R/H AFT FRAME AT UPPER LATCH KEEPER IAW SRM 53-80-07 REPAIR 4 FIGURE 202. (MINOR)
- [SDR IPXA2021032767352](https://openairdocs.org/sdr/IPXA2021032767352.md): Stringer Clip · cracked · Mar 3, 2021 · N264UP · Doug MD11F · Wing, Attach Fittings
  > INSPECTION TYPE:3C#1 MAIN FUEL TANK STRINGER 38 CLIP IS CRACKED AT STA XORS 506.REMOVED AND REPLACED CRACKED #1 MAIN FUEL TANK STRINGER CLIP AT STA XORS 506 IAW SRM 51-33-01. (MINOR)
- [SDR IPXA2021040967981](https://openairdocs.org/sdr/IPXA2021040967981.md): Tee Fitting · cracked · Mar 2, 2021 · N264UP · Doug MD11F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:3CMAIN CABIN LONGERON 15R TEE ANGLE BRACKET IS CRACKED AT STA 1341.REMOVED AND REPLACED CRACKED MAIN CABIN LONGERON 15R TEE ANGLE BRACKET AT STA 1341 IAW SRM 51-33-01. (MINOR)
- [SDR IPXA2021040967980](https://openairdocs.org/sdr/IPXA2021040967980.md): Tee Fitting · cracked · Mar 2, 2021 · N264UP · Doug MD11F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:3CMAIN CABIN LONGERON 15L TEE ANGLE IS CRACKED BETWEEN STA 1219 AND STA 1239.REMOVED AND REPLACED CRACKED MAIN CABIN LONGERON 15L TEE ANGLE BETWEEN STA 1219 AND STA 1239 IAW SRM 51-33-01. (MINOR)
- [SDR IPXA2021040567778](https://openairdocs.org/sdr/IPXA2021040567778.md): Frame · dented · Mar 2, 2021 · N264UP · Doug MD11F · Fuselage Main, Frame
  > INSPECTION TYPE:3CMAIN CABIN FRAME IS DENTED AT STA. 695 BETWEEN LONG. 12R TO 13R.REPAIRED DENTED FRAME AT STA. 695 BETWEEN LONG. 12R TO 13R IAW VT-SAA EA 011-5310-001-A8951 REV. I/R AND UPS EO MD11-5310-79803-A. (MAJOR)
- [SDR IPXA2021032867392](https://openairdocs.org/sdr/IPXA2021032867392.md): Floorbeam · cracked · Mar 2, 2021 · N264UP · Doug MD11F · Fuselage Main, Floor Beam
  > INSPECTION TYPE:3CLOWER FWD. CARGO FLOOR BEAM IS CRACKED AT STA. 6-70, X= 57.5 AND Z= -98.REPAIRED CRACKED FLOOR BEAM AT STA. 6-70, X= 57.5 AND Z= -98 IAW SRM 53-40-51 REPAIR 1 FIG. 201. (MAJOR)
- [SDR IPXA2021032867391](https://openairdocs.org/sdr/IPXA2021032867391.md): Floorbeam · cracked · Mar 2, 2021 · N264UP · Doug MD11F · Fuselage Main, Floor Beam
  > INSPECTION TYPE:3CFWD. LOWER CARGO FLOOR BEAM IS CRACKED AT STA. 6-70, X= -57.5 AND Z= -98.REPAIRED CRACKED FLOOR BEAM AT STA. 6-70, X= -57.5 AND Z= -98 IAW SRM 53-40-51 REPAIR 1 FIG. 202. (MAJOR)

Next page: https://openairdocs.org/aircraft/N264UP/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 = 'N264UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N264UP/reports

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