# Service difficulty reports: N261UP

A list on [N261UP](https://openairdocs.org/aircraft/N261UP.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 2 · 74 reports

- [SDR IPXA2023112876756](https://openairdocs.org/sdr/IPXA2023112876756.md): Unknown · unknown · Nov 28, 2023 · N261UP · Doug MD11F · Passenger/Crew Doors
  > LH ENTRY DOOR INOPERATVE-WILL NOT OPEN FOUND L1 OPEN LIMIT SWITCH S1-592 PLUNGER STUCK. CLEANED AND LUBRICATED OPEN LIMIT SWITCH PLUNGER. SEE WDM 52-11-01. PERFORMED L1 DOOR TEST PER AMM 52-11-02-2. PLACARD HAS BEEN REMOVED.
- [SDR IPXA2023080393791](https://openairdocs.org/sdr/IPXA2023080393791.md): Battery · discharged · Aug 3, 2023 · N261UP · Doug MD11F · Emergency Lighting
  > EMER LT BAT 1 LO LEVEL ONE ALERT DURING TEST. ITEM DEFERRED PER MEL 33 50 4. ASSIGNED M 811065 PLACARD INSTALLED ACCOMPLISHED DMP 33 50 4.REVERSED DMP 33-50-4 AND R&R EMERGENCY LIGHT BATT POWER SUPPLY PER AMM 33-51-01. OPERATIONAL CHK GOOD. THIS CLEARS M811065
- [SDR IPXA2023061693452](https://openairdocs.org/sdr/IPXA2023061693452.md): Battery · no test · Jun 15, 2023 · N261UP · Doug MD11F · Battery/Charger System
  > INSPECTION TYPE:NAEMER PWR TEST FAILR&R'D BOTH SHIPS BATTERIES PER AMM 24-34-62-000-802 AND 24-34-62-400-802 OPS TEST PER AMM 24-34-02-700-802 NORMAL AT THIS TIME
- [SDR IPXA2023032092052](https://openairdocs.org/sdr/IPXA2023032092052.md): Rudder · unknown · Mar 20, 2023 · N261UP · Doug MD11F · Rudder Structure
  > INSPECTION TYPE:N/A*MAJOR REPAIR* AFT UPPER RUDDER RT SKIN LIGHTNING STRIKE REPAIRREPAIRED PER EO MD11 5540-86037-B
- [SDR IPXA2022110687873](https://openairdocs.org/sdr/IPXA2022110687873.md): Door · faulted · Nov 6, 2022 · N261UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION TYPE:NAMAIN ENTRY DOOR UPON ARRIVAL WOULD NOT OPEN ELECTRONICALLYPERFORMED OPS CHECK OF L1 DOOR OPS CHECKS PASSED FOUND EXTENDED AND NEEDED TO BE STOWED FOR OPERATION REF AMM 52-10-01
- [SDR IPXA2022092886694](https://openairdocs.org/sdr/IPXA2022092886694.md): Seat · out of position · Sep 28, 2022 · N261UP · Doug MD11F · Flight Compartment Equipment
  > L1 ENTRY DOOR LIFT BAR CONTACTS COURIER SEAT WHEN CLOSING, ADJUSTED COURIER SEATS AFT. PERFORMED OPS TEST OF L1 DOOR REF AMM 52-10-01, PB 201 DOOR NO LONGER MAKES CONTACT. THIS CLEARS M792141
- [SDR 2022FA0000333](https://openairdocs.org/sdr/2022FA0000333.md): Disk · cracked · Jul 7, 2022 · N261UP · Doug MD11F · Turbine Engine Air Inlet Section
  > INDICATION IN BORE A ZONE CORNER, AMPLITUDE 2020MV. GE ENGINE SHOP MANUAL (ESM) EVALUATION/REJECTION LIMIT IS 1500MV.
- [SDR IPXA2022062883566](https://openairdocs.org/sdr/IPXA2022062883566.md): Light · inoperative · Jun 27, 2022 · N261UP · Doug MD11F · Emergency Lighting
  > INSPECTION TYPE:NAEMERG LIGHT LO BATT MSG DURING TESTREPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY IAW AMM 33-51-01. OPS TEST GOOD. IPC33-51-10-01 ITEM 005J
- [SDR IPXA2022032880588](https://openairdocs.org/sdr/IPXA2022032880588.md): Support Angle · corroded · Mar 12, 2022 · N261UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:1CAFT CARGO FLOOR BEAM SUPPORT ANGLE CORRODED AT X=3,Y=1841.REPAIRED CORRODED AFT CARGO FLOOR BEAM SUPPORT ANGLE IAW VT-SAA EA 011-5310-01-A9512 REV I/R AND UPS EO MD11-5310-83234-A BY P.LAU (AR-830967) DATED 03/25/2022 (MAJOR).
- [SDR IPXA2022032280379](https://openairdocs.org/sdr/IPXA2022032280379.md): Stiffener · cracked · Mar 12, 2022 · N261UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C1AFT CARGO COMPARTMENT STEP UP AT STA 1841 HAS A CRACKED STIFFENER AT LONGERON 48L.REMOVED,FAB, REPLACE THE CRACK STIFFENER IAW DWG AGA7170 AND SRM 51-33-01.
- [SDR IPXA2022032980636](https://openairdocs.org/sdr/IPXA2022032980636.md): Former · cracked · Mar 11, 2022 · N261UP · Doug MD11F · Leading Edge Devices
  > INSPECTION TYPE:4CL/H WING FIXED L/E FORMER IS CRACKED AT STA. XOS. 584.891.REPAIRED CRACKED L/H WING FIXED L/E FORMER AT STA. XOS. 584.891 IAW VT-SAA EA 011-5740-01-A9515 REV. I/R AND UPS EO MD11- 5710-83235-A. (MAJOR) REF FAA FORM 8100-9 BY P. LAU (AR830967)
- [SDR IPXA2022032880587](https://openairdocs.org/sdr/IPXA2022032880587.md): Former · cracked · Mar 11, 2022 · N261UP · Doug MD11F · Leading Edge Devices
  > INSPECTION TYPE:1CRT WING FIXED L/E FORMER CRACK AT STA. XOS=667.79.REPAIRED RT WING FIXED L/E CRACKED FORMER AT STA. XOS=667.79 IAW VT-SAA EA 011-5754-01-A9516 REV I/R AND UPS EO MD11-5710-83236-A BY P.LAU (AR-830967) DATED 03/25/2022 (MAJOR).
- [SDR IPXA2022032280384](https://openairdocs.org/sdr/IPXA2022032280384.md): Doubler · cracked · Mar 11, 2022 · N261UP · Doug MD11F · Wing, Attach Fittings
  > INSPECTION TYPE:1CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 692.0 TO 703.5.REPAIRED CRACKED R/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 692.0 TO 703.5 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)
- [SDR IPXA2022032280383](https://openairdocs.org/sdr/IPXA2022032280383.md): Doubler · cracked · Mar 11, 2022 · N261UP · Doug MD11F · Wing, Attach Fittings
  > INSPECTION TYPE:1CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 763.3 TO 768.2.REPAIRED CRACKED R/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 763.3 TO 768.2 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)
- [SDR IPXA2022032280381](https://openairdocs.org/sdr/IPXA2022032280381.md): Doubler · cracked · Mar 11, 2022 · N261UP · Doug MD11F · Wing, Attach Fittings
  > INSPECTION TYPE:1CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 679.8 TO 685.9.REPAIREDCRACKED R/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 679.85 TO 685.9 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)
- [SDR IPXA2022010477499](https://openairdocs.org/sdr/IPXA2022010477499.md): None · inoperative · Jan 3, 2022 · N261UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION TYPE:NA**SUPPLEMENTAL SDR**L1 DOOR WILL NOT OPEN ELECTRICALLY. DEFERRED PER MEL 52-10-3-1-2-1-2. M768556 ASSIGNED, PLACARD INSTALLEDREPLACED S2-730 LOCK REL SOL, R2-177 DOOR ACT RELAY PER AMM 52-10-06 & 20-30-00 W/ REF IPC 52-34-01-01-911. RAN ALL W
- [SDR IPXA2021122977372](https://openairdocs.org/sdr/IPXA2021122977372.md): None · none · Dec 28, 2021 · N261UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION TYPE:N/A** SUPPLEMENTAL SDR ** L1 DOOR DOES NOT WORK FROM INSIDE SWITCH. DEFERRED IAW MEL 52-10-3-1-2-1-2. L1 DOOR DOES NOT OPEN/CLOSE ELECTRICALLY.T/S PER WDM 52-11-01, FOUND GIRT BAR SWITCH S1-1090 STICKING, FREED UP SWITCH & PERFORMED OPS CK PER
- [SDR IPXA2021122877349](https://openairdocs.org/sdr/IPXA2021122877349.md): None · none · Dec 28, 2021 · N261UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION TYPE:N/AL1 DOOR DOES NOT OPERATE. DEFER L1 DOOR PER MEL 52-10-3-1-2-1, PLACARD INSTALLED, ITEM #M767960.OPERATED DOOR MULTIPLE TIMES FROM INSIDE AND OUTSIDE SWITCHES. NO FAULTS NOTED, DEFERRAL CLEARED.
- [SDR IPXA2021121877064](https://openairdocs.org/sdr/IPXA2021121877064.md): None · none · Dec 18, 2021 · N261UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION TYPE:NAL1 DOOR INOP.OPS CHECK L1 DOOR IAW AMM 52-10-00. OPS CHECK GOOD M766663 CLEARED.
- [SDR IPXA2021100374503](https://openairdocs.org/sdr/IPXA2021100374503.md): Light · none · Oct 3, 2021 · N261UP · Doug MD11F · Emergency Lighting
  > INSPECTION TYPE:N/AR1 MED FLOOR EMERGENCY LIGHT INOPR&R BULBS @ R1 MED FLOOR EMERGENCY LIGHT OPS CHECK GOOD REF AMM 33 50 00
- [SDR IPXA2021061470579](https://openairdocs.org/sdr/IPXA2021061470579.md): Evas Unit · no test · Jun 11, 2021 · N261UP · Doug MD11F · Emergency Equipment
  > INSPECTION TYPE:NAWHILE PREFORMING TC-9197 EVAS TEST BOTH LH AND RH EVAS UNITS FAIL BLOWER TEST. WILL NOT RUN. MANUAL SWITCH ON CKS OK. ACCOMP. DMP 25-68-1 REMOVED AND PROCESSED. DEFERRED UNDEER MEL 25-68-1 CONTROL NUMBER M747080. PLACRD INSTALLED.INSTALLED
- [SDR IPXA2021061170428](https://openairdocs.org/sdr/IPXA2021061170428.md): Door · inoperative · Jun 11, 2021 · N261UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION TYPE:NAL1 DOOR ELECTRIC MODE INOP. OPENED DOOR PNUMATICALLY. ELECTRONIC FUNCTION RESTORED. ITEM DEFERRED IAW MEL 52-10-3-1-2-1-1FOUND L1 DOOR BOTTLE DEPLETED. RESET & SERVICED BOTTLE AS REQ AMM 12-54-04 LEAK CHECK BOTTLE & FITTING. NO LEAKS NOTED. T
- [SDR IPXA2021050468973](https://openairdocs.org/sdr/IPXA2021050468973.md): Battery · discharged · May 4, 2021 · N261UP · Doug MD11F · Emergency Lighting
  > EMER LT BATT / LOW ON PREFLIGHT. ACCOMPLISHED M743368 ASSIGNED PLACARD INSTALLED.REPLACED EMERGENCY BATTERY REF AMM 33-51-01-000-802, OPS CK GOOD. REVERSED DMP.
- [SDR IPXA2020123063953](https://openairdocs.org/sdr/IPXA2020123063953.md): Engine · flamed out · Dec 28, 2020 · N261UP · Doug MD11F · Engine (Turbine/Turboprop)
  > INSPECTION TYPE: N/A DURING TAXI, NR 2 ENGINE FLAMED OUT, ALL ENGINE PARAMETER ROLLED BACK. NO FCC FAULTS ON ECU 2A ON 2B FAULTS, PER FON MTS NORMAL START, PER MD11 AMM 71-00-00. OPERATIONS TEST GOOD AT THIS TIME.
- [SDR IPXA2020061056337](https://openairdocs.org/sdr/IPXA2020061056337.md): Shear Tie · cracked · May 13, 2020 · N261UP · Doug MD11F · Fuselage Internal Mounting Structure
  > INSPECTION TYPE:3C AFT CARGO LT LOWER BILGE FRAME SHEAR TIE CHORD CRACKED AT STA 1841. REMOVED, FABRICATED AND INSTALLED SHEARTIE IN LT LOWER BILGE STA 1841 IAW SRM 51-35-01. (MINOR)
- [SDR IPXA2020062256771](https://openairdocs.org/sdr/IPXA2020062256771.md): Skin · gouged · May 2, 2020 · N261UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3C WHILE INSTALLING THE LEFT MAIN LANDING GEAR FIXED BRACE ASSEMBLY, GEAR STAND DOOR OPENED AND CONTACTED THE LEFT I/B FLAP LOWER SKIN. REPAIRED GOUGED LT I/B FLAP LOWER SKIN BETWEEN XIFH 190 AND XIFH 213.05 IAW EA 011-5750-01-A8184 AND EO MD1
- [SDR IPXA2020052635668](https://openairdocs.org/sdr/IPXA2020052635668.md): Frame · cracked · Apr 24, 2020 · N261UP · Doug MD11F · Fuselage Main, Frame
  > INSPECTION TYPE:C3AFT AVI COMP BILGE AREA L/H CANTED FRAME IS CRACKED AT STA 469.173.ACCOMPLISHED PERMANENT REPAIR ON CRACKED CANTED FRAME IN AFT AVIONICS COMPARTMENT AT STA 469.173 IAW MD11 SRM 53-10-07 REPAIR 1 FIGURE 201 REV. 66. (MAJOR)
- [SDR IPXA2020051855411](https://openairdocs.org/sdr/IPXA2020051855411.md): Frame · cracked · Apr 24, 2020 · N261UP · Doug MD11F · Fuselage Main, Frame
  > INSPECTION TYPE:3CFUSELAGE FRAME AT STA. 469.173 CANT AND X=60 IS CRACKED.REPAIRED CRACKED FUSELAGE FRAME AT STA. 469.173 CANT AND X=60 IAW SRM 53-10-07 REPAIR 1 FIG. 201. (MAJOR)
- [SDR IPXA2020062977053](https://openairdocs.org/sdr/IPXA2020062977053.md): Seat Track · corroded · Apr 23, 2020 · N261UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:3CMAIN CABIN FLOOR SEAT TRACK STA 1381 -1521 X=8.50 HAS CORROSION.REPAIRED CORRODED SEAT TRACK IN MAIN CARGO BETWEEN STA 1371 AND 1531 X=8.50 IAW SRM 53-00-52 REPAIR 1 FIG 201 AND EA 011-5310-01-A8188, EO MD11-5310-76615A. (MAJOR)
- [SDR IPXA2020062977049](https://openairdocs.org/sdr/IPXA2020062977049.md): Seat Track · corroded · Apr 23, 2020 · N261UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:3C, MAIN CARGO RT FLOOR AREA SEAT TRACK HAS CORROSION BETWEEN STA 1401 TO STA 1501 X= -75.25REPAIRED CORRODED SEAT TRACK IN MAIN CARGO BETWEEN STA 1391 AND 1531 X= -75.25 IAW SRM 53-00-52 REPAIR 1 FIG 201, EA 011-5310-01-A8188 AND EO MD11-5310
- [SDR IPXA2020061056406](https://openairdocs.org/sdr/IPXA2020061056406.md): Seat Track · corroded · Apr 23, 2020 · N261UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:3C SEAT TRACK IS CORRODED BETWEEN STA 1401-1521 AT X=8.50. REMOVED AND REPLACED SEAT TRACK IAW EA 011-5310-01-A8188 REV IR AND EO MD-11-5310-76615-A. (MINOR)
- [SDR IPXA2020060155979](https://openairdocs.org/sdr/IPXA2020060155979.md): Floor Support · corroded · Apr 23, 2020 · N261UP · Doug MD11F · Fuselage Miscellaneous Structure
  > 3C MAIN CABIN RT FLOOR AREA AT STA 1481 FLOOR PANEL LANDING SUPPORT HAS SURFACE CORROSION. REMOVED CRACKED SUPPORT. FABRICATED AND INSTALLED IN MAIN CABIN RT FLOOR AREA AT STA 1481 IAW SRM 51-33-01.
- [SDR IPXA2020060155980](https://openairdocs.org/sdr/IPXA2020060155980.md): Intercostal · cracked · Apr 23, 2020 · N261UP · Doug MD11F · Fuselage Miscellaneous Structure
  > 3C FWD CARGO COMPARTMENT. LT SIDE BILGE INTERCOSTAL, BETWEEN STATION 6 - 10 AND 6 - 30, UNDERNEATH Z-FRAME HAS A CRACK. REMOVED CRACKED INTERCOSTAL. FABRICATED AND INSTALLED BETWEEN STATION 6 - 10 AND 6 - 30, UNDERNEATH Z-FRAME IAW SRM 51-31-01.
- [SDR IPXA2020052635671](https://openairdocs.org/sdr/IPXA2020052635671.md): Skin · corroded · Apr 23, 2020 · N261UP · Doug MD11F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:3CRT AFT FUSELAGE EXTERIOR SKIN HAS CORROSION BETWEEN STA 2140 - 2163.ACCOMPLISH PERMANENT REPAIR ON CORRODED RT AFT FUSELAGE SKIN BETWEEN STA 2140 - 2163 IAW MD-11 SRM 53-70-01 REPAIR 3 FIG 201. (MAJOR)
- [SDR IPXA2020060856294](https://openairdocs.org/sdr/IPXA2020060856294.md): Support · cracked · Apr 22, 2020 · N261UP · Doug MD11F · Fuselage Main, Frame
  > INSPECTION TYPE:3C AFT CARGO BILGE AREA LOWER FRAME SUPPORT HAS A CRACK AT STA 1841 ABOVE LONGERON 43. REMOVED CRACKED FRAME SUPPORT, FABRICATED AND INSTALLED IN AFT CARGO AT STA 1841 ABOVE LONGERON 43 IAW SRM 51-35-01 AND DWG AGA7098. (MINOR)
- [SDR IPXA202005265731](https://openairdocs.org/sdr/IPXA202005265731.md): Bracket · cracked · Apr 22, 2020 · N261UP · Doug MD11F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:3CCAC COMPARTMENT STA 1159 TRUSS BRACKET AT LONGERON 27 RH IS CRACKED IN 2 PLACES.REMOVED CRACKED TRUSS BRACKET, FABRICATED AND INSTALLED BETWEEN STA 1139 AND 1159 AT LONGERON 27 RH IN CAC COMP. IAW MD11 SRM 51-30-01 AND DRAWING AFA7605. (MINOR
- [SDR IPXA2020052645694](https://openairdocs.org/sdr/IPXA2020052645694.md): Intercostal · cracked · Apr 22, 2020 · N261UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:3CCENTER CARGO COMP L/H SIDE INTERCOSTAL UNDER Z-FRAME BETWEEN STA 1761 AND 1781 HAS A CRACK.REMOVED, FABRICATED CRACKED INTERCOSTAL AND INSTALLED IN CETER CARGO LH SIDE UNDER Z-FRAME BETWEEN STA 1761 AND 1781 IAW DRAWING ACA7046 AND AMM 20-50-
- [SDR IPXA2020051855407](https://openairdocs.org/sdr/IPXA2020051855407.md): Intercostal · cracked · Apr 22, 2020 · N261UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:3CCENTER CARGO COMP MRH INTERCOSTAL UNDER Z-FRAME BETWEEN STA 5-11 AND 5-32 HAS A CRACK AT FWD SIDE.REMOVED, FABRICATED AND INSTALLED INTERCOSTAL IN CENTER CARGO COMP BETWEEN STA 5-11 - 5-32. IAW SRM 51-33-01. (MINOR)
- [SDR IPXA2020051855406](https://openairdocs.org/sdr/IPXA2020051855406.md): Angle · corroded · Apr 22, 2020 · N261UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:3CAFT CARGO DOOR JAMB LWR AFT ANGLE SUPPORT IS CORRODED.REMOVED, FABRICATED AND INSTALLED ZEE ANGLES ON AFT CARGO DOOR JAMB IAW SRM 51-31-01. (MINOR)
- [SDR IPXA2020051155174](https://openairdocs.org/sdr/IPXA2020051155174.md): Intercostal · cracked · Apr 22, 2020 · N261UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:3CCENTER CARGO COMP R/H INTERCOSTAL UNDER Z FRAME BETWEEN STA 5-11 AND 5-32 HAS A CRACK AT FWD SIDE.REMOVED, FABRICATED AND INSTALLED CENTER CARGO COMP R/H INTERCOSTAL BETWEEN STA 5-11 AND STA 5-32 IAW SRM 51-33-01. (MINOR)
- [SDR IPXA2020061056405](https://openairdocs.org/sdr/IPXA2020061056405.md): Skin · gouged · Apr 21, 2020 · N261UP · Doug MD11F · Horizontal Stabilizer, Plate/Skin
  > INSPECTION TYPE:3C LT HORZONTAL STAB L/E SKIN IS GOUGED ON O/B SECTION BETWEEN XFS 351.215 AND XFS 357.032. REPAIRED GOUGED LT HORIZONTAL STAB L/E SKIN BETWEEN XFS 351.215 AND XFS 357.032 IAW EA 011-5510-01-A8186 AND EO MD11-5510-76731-A (MAJOR).
- [SDR IPXA2020061056404](https://openairdocs.org/sdr/IPXA2020061056404.md): Skin · gouged · Apr 21, 2020 · N261UP · Doug MD11F · Horizontal Stabilizer, Plate/Skin
  > INSPECTION TYPE:3C LT HORIZONTAL STAB L/E SKIN IS GOUGED ON O/B SECTION BETWEEN XFS 351.215 AND XFS 357.032. REPAIRED GOUGED LT HORIZONTAL STAB L/E SKIN BETWEEN XFS 391.933 AND XFS 397.749 IAW EA 011-5510-01-A8186 AND EO MD11-5510-76731-A (MAJOR).
- [SDR IPXA2020060155981](https://openairdocs.org/sdr/IPXA2020060155981.md): Floorbeam · cracked · Apr 21, 2020 · N261UP · Doug MD11F · Fuselage Main, Floor Beam
  > 3C SUB FLOORBEAM AT APPROX STATION 6 - 73, LONGERON 43, LT CORNER IS CRACKED AT ITS ANGLE CHANGE. REMOVED CRACKED SUB FLOORBEAM, FABRICATED AND INSTALLED AT STATION 6 - 73, LONGERON 43 LT IAW SRM 51-31-01.
- [SDR IPXA2020051155166](https://openairdocs.org/sdr/IPXA2020051155166.md): Intercostal · cracked · Apr 21, 2020 · N261UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:3CFWD CARGO RT SIDE BILGE INTERCOSTAL BETWEEN STA 6-30 AND 6-50 CRACKED AT AFT UPPER SIDE.REMOVED, FABRICATED AND INSTALLED INTERCOSTAL AT FWD CARGO BETWEEN STA 6-30 AND 6-50 IAW SRM 51-33-01 AND DRAWING ACA7049. ( MINOR)
- [SDR IPXA2020052645696](https://openairdocs.org/sdr/IPXA2020052645696.md): Support Frame · cracked · Apr 20, 2020 · N261UP · Doug MD11F · Aerodynamic Fairings
  > INSPECTION TYPE:3CR/H WING TO BODY AT STRINGER 31 RH HAS VERTICAL ATTACHMENT SUPPORT FRAME CRACKED.REMOVED, FABRICATED CRACKED SUPPORT FRAME AND INSTALLED AT RH WING TO BODY AT STRINGER 31 IAW DRAWING ANB7143 AND SRM 51-35-01. (MINOR)
- [SDR IPXA2020052255603](https://openairdocs.org/sdr/IPXA2020052255603.md): Panel · cracked · Apr 20, 2020 · N261UP · Doug MD11F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:3CL/H UNDERWING BARREL CANTED PANEL CRACKED AT STA X=1236.8 Z=100.ACCOMPLISHED PERMANENT REPAIR OF CRACKED LH UNDERWING BARREL CANTED PANEL AT STA 1236.8 IAW EO.MD11-5310-76331-A REV 05/18/2020. (MAJOR)
- [SDR IPXA2020051855409](https://openairdocs.org/sdr/IPXA2020051855409.md): Longeron · corroded · Apr 20, 2020 · N261UP · Doug MD11F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:3CRH UPPER WING TO BODY AREA UNDER R3 DOOR AT LONGERON 28 RH HAS CORROSION.REPAIRED LONGERON 28 RH AT STA 1300 IAW EA 011-5300-01-A8170 I/R AND UPS EO MD11-5300-76521-A ( MINOR)
- [SDR IPXA2020051155173](https://openairdocs.org/sdr/IPXA2020051155173.md): Angle · cracked · Apr 20, 2020 · N261UP · Doug MD11F · Aerodynamic Fairings
  > INSPECTION TYPE:3CL/H UPPER WING TO BODY FAIRING ATTACH FRAME HAS BOTTOM L-ANGLE CRACKED AT STA 1401.REMOVED FABRICATED AND INSTALLED L-ANGLE AT L/H WING TO BODY FRAME AT STA 1401 IAW SRM 51-35-01 AND SRM 51-33-01. (MINOR)
- [SDR IPXA2020062256768](https://openairdocs.org/sdr/IPXA2020062256768.md): Bulkhead · damaged · Apr 19, 2020 · N261UP · Doug MD11F · Nacelle/Pylon, Bulkhead/Firewall
  > INSPECTION TYPE:3C NR 1 PYLON INTERNAL BULKHEAD INSIDE ACCESS PANELS 438CR/DR HAS ELONGATED HOLE. REPAIRED ELONGATED HOLE ON NR 1 PYLON BULKHEAD WEB AT YWN 315.500 INSIDE ACCESS PANEL 438CR/DR IAW EA 011-5410-01-A8220 AND EO MD11-5410-76813-A. (MAJOR)
- [SDR IPXA2020061056338](https://openairdocs.org/sdr/IPXA2020061056338.md): Beltframe · dented · Apr 19, 2020 · N261UP · Doug MD11F · Fuselage Main, Frame
  > INSPECTION TYPE:3C MAIN CABIN BELT FRAME DENTED AT STA 715 LONGERON 13R. CUTOUT DAMAGE AND ACCOMPLISHED PERMANENT REPAIR ON BELT FRAME IN MAIN CABIN AT STA 715 LONGERON 13R IAW EA 011-5310-01-A8168 REV I/R AND EO MD11-5310-76728-A. (MAJOR)

Next page: https://openairdocs.org/aircraft/N261UP/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 = 'N261UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N261UP/reports

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