# Service difficulty reports: N260UP

A list on [N260UP](https://openairdocs.org/aircraft/N260UP.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 · 329 reports

- [SDR IPXA2025050129299](https://openairdocs.org/sdr/IPXA2025050129299.md): Fitting · corroded · Apr 18, 2025 · N260UP · Doug MD11F · Fuselage Main, Structure
  > UPON REMOVAL OF LONGERON FITTING P/N AAA7088 AT L51R STA 6-70 TO 6-90 FOUND TO BE CRACK AND CORRODED ATA-53-00 REMOVED & REPLACED LONGERON 51R (P/N: AAA7088-1 PER MD11-SRM CHAPTER 51 USING DAC DWG AAA7088-1 AND PARTS AS SAMPLE IAW UPS GMM 09-08.
- [SDR IPXA2025050643072](https://openairdocs.org/sdr/IPXA2025050643072.md): Skin · corroded · Apr 16, 2025 · N260UP · Doug MD11F · Fuselage Main, Plate/Skin
  > CORROSION FOUND APPROX 18 INCHES FWD OF CENTER WING BOX AND APPROX AT RBL 88. 49-036 ATA 53-00 CENTER WING TANK UPPER FWD SKIN BETWEEN STA XCW=-74 TO XSW=-111 AND BETWEEN S-16 AND S-21 LOCATION CORROSION REWORK ACCOMPLISHED PER VT SAA E.A.#011-5730-01-B0472 R
- [SDR IPXA2025050245994](https://openairdocs.org/sdr/IPXA2025050245994.md): Longeron · corroded · Apr 16, 2025 · N260UP · Doug MD11F · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND IN CAC STA 6-70 TO 6-90 / LONGERON R51. PM040-80. ATA-51-00 LONGERON SPLICE REPAIR ACCOMPLISHED @ FWD EXTENDED FUSELAGE SECTION LONGERON 51R (P/N: A6A7027-1) BETWEEN STA Y=6-62 AND Y=6-81 LOCATION PER MD11-SRM 53-00-05-2R REPAIR 1 REV 71.
- [SDR IPXA2025050928077](https://openairdocs.org/sdr/IPXA2025050928077.md): Stiffener · cracked · Apr 15, 2025 · N260UP · Doug MD11F · Fuselage Miscellaneous Structure
  > (STR) AFT CGO COMP FLOOR BEAM AREA STA 1841 RBL 30" STIFFENER HAS CRAKED. 74-033 ATA CODE 53 INSTALLED NEW STIFFENER AT AFT CARGO COMPARTMENT FLOOR BEAM AREA, STA 1841 RBL 30" IAW MD11 SRM 51-35-01-OG-0
- [SDR IPXA2025050692110](https://openairdocs.org/sdr/IPXA2025050692110.md): Doubler · cracked · Apr 13, 2025 · N260UP · Doug MD11F · Wing, Plate/Skin
  > CRACKED BEADED DOUBLER AT RH LE APPROX 15 INCHES I/B OF #9 SLAT TRACK. 49-005 ATA 57-00 INSTALLED BEADED DOUBLER AND REMOVED EWIS PROTECTION AT R/H L/E I/B OF SLAT TRACK #9 IAW MD-11 SRM 57-40-02-2R-15 REPAIR 15 AND MD-11 SRM 51-00-12.
- [SDR IPXA2025031446915](https://openairdocs.org/sdr/IPXA2025031446915.md): Structure · damaged · Mar 14, 2025 · N260UP · Doug MD11F · Fuselage Miscellaneous Structure
  > LWR FWR CARGO CEILING-STRUCTURE FWD OF AFT FLOOD LAMP -DAMAGED- NUTPLATE RIPPED OUT -HOLE SIZE IS.375 AND JAGGED EDGES.ACCOMPLISHED STEPS 1-7 OF EO-93152-REQ1
- [SDR IPXA2025031447024](https://openairdocs.org/sdr/IPXA2025031447024.md): Structure · damaged · Mar 14, 2025 · N260UP · Doug MD11F · Fuselage Miscellaneous Structure
  > LWR FWD CARGO COMPT-CEILING-STRUCTURE AT INBD SIDE OF AFT FLOOD LAMP DAMAGED -BENT DOWN-MISSING NUTPLATE REF. ACCOMPLISHED STEPS 1-6 OF EO-93150-REQ1
- [SDR IPXA2025030445471](https://openairdocs.org/sdr/IPXA2025030445471.md): Bottle · low pressure · Mar 4, 2025 · N260UP · Doug MD11F · Passenger/Crew Doors
  > R1 DOOR ASSIST BOTTLE PRESSURE BELOW GREEN BAND. SERVICED R1 DOOR ASSIST BOTTLE WITH REF TO AMM 12-25-04-600-801. NO LEAKS NOTED DURING LEAK CHECK. THIS CLEARS MEL 52-10-3-1-2-1-1. PLACARD REMOVED.
- [SDR IPXA2025012825896](https://openairdocs.org/sdr/IPXA2025012825896.md): Bottle · low pressure · Jan 28, 2025 · N260UP · Doug MD11F · Passenger/Crew Doors
  > ON PRE-FLIGHT R1 DOOR PNEUMATIC PRESSURE BELOW LIMITS (OUT OF GREEN BAND). SERVICED THE R1 DOOR PNEUMATIC STORAGE SYSTEM IAW MD11 AMM 12-25-04. THIS CLEARS MEL. PLACARD REMOVED. OSD: 1/28/2025
- [SDR IPXA2024092134968](https://openairdocs.org/sdr/IPXA2024092134968.md): Chain · broken · Sep 21, 2024 · N260UP · Doug MD11F · Passenger/Crew Doors
  > L1 ENTRY DOOR EMERGENCY PNEUMATIC DRIVE MOTOR DRIVE CHAIN MISSING. FOUND BROKEN CHAIN LOCATED ON CEILING PANEL. INSTALLED NEW CHAIN ASSY REF MM 52-11-09. DOOR OPERATIONAL CHECK GOOD.
- [SDR IPXA2024061915026](https://openairdocs.org/sdr/IPXA2024061915026.md): Wire · damaged · Jun 18, 2024 · N260UP · Doug MD11F · Flight Control System Wiring
  > ATB, ON DEPARTURE, WHILE STILL CONFIGURED, GOT A LEVEL 1 AIL DEFLECT INOP. AFTER FLAP RETRACT, GOT A LEVEL 2 AIL DEFLECT DISAG. WE ENGAGED A/P 2 AND THE AIRCRAFT ROLLED RIGHT AND THE A/P DISCONNECTED. WET. REPAIRED DAMAGED WIRE N316-27-18RD AND REPLACED DAMAG
- [SDR IPXA2024011811319](https://openairdocs.org/sdr/IPXA2024011811319.md): Unknown · unknown · Jan 18, 2024 · N260UP · Doug MD11F · Emergency Equipment
  > R1 DOOR ASSIST BOTTLE PRESSURE LOW SVC'D R1 DOOR ASSIST BOTTLE AS REQ'D REF AMM 12-24-04
- [SDR IPXA2023090694099](https://openairdocs.org/sdr/IPXA2023090694099.md): Battery · discharged · Sep 5, 2023 · N260UP · Doug MD11F · Emergency Lighting
  > EMERGENCY LIGHT BAT 1 LO STATUS MESSAGE. R & R EMERGENCY BATTERY POWER IAW AMM 33-51-01-400. OPS CHKS GOOD.
- [SDR IPXA2023071393653](https://openairdocs.org/sdr/IPXA2023071393653.md): Door · inoperative · Jul 12, 2023 · N260UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION TYPE:NACREW DOOR LOUVRE PANEL DETACHED FROM DOORRESECURED AND INSTALLED FLIGHT COMPARTMENT CREW DOOR LOUVRE PANEL IAW AMM 52-54-02-400-801. NO DEFECTS NOTED
- [SDR IPXA2023062593511](https://openairdocs.org/sdr/IPXA2023062593511.md): Light · inoperative · Jun 24, 2023 · N260UP · Doug MD11F · Emergency Lighting
  > L1 DOOR EMERGENCY LIGHT EXIT SIGN HALF OUT. RELAMPED NO HELP. R/R L1 DOOR EXIT SIGN REF AMM 33-27-05 PB 401. OPS CHECKS GOOD.
- [SDR IPXA2023052293296](https://openairdocs.org/sdr/IPXA2023052293296.md): Door · inoperative · May 22, 2023 · N260UP · Doug MD11F · Passenger/Crew Doors
  > BEFORE BLOCK OUT I HAD DIFFICULTY ARMING THE FWD CABIN DOOR UPON LANDING I WAS OT ABLE TO DIS ARM THE DOORFOUND DEBRIS IN R1 DOOR ARMING HANDLE AND GIRT BAR DISLODGED FROM GIRT. REMOVED DEBRIS FROM ARMING AN REINSTALLED GIRT BAR TO GIRT PER AMM 25-61-01-400-80
- [SDR IPXA2023051993270](https://openairdocs.org/sdr/IPXA2023051993270.md): Seat Track · corroded · May 9, 2023 · N260UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C3*MAJOR REPAIR* MAIN CABIN L/H SIDE SEAT TRACK HAS CORROSION AT STA Y=5-73 - Y=1568 AND X=8.50.REPAIRED CORRODED SEAT TRACK AT THE MAIN CABIN L/H SIDE BETWEEN STA Y=5-73 - Y=1568 AND X=8.50 IAW SRM 53-00-52 REPAIR 1 FIG 201. (MAJOR)
- [SDR IPXA2023051993269](https://openairdocs.org/sdr/IPXA2023051993269.md): Seat Track · corroded · May 9, 2023 · N260UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:3C*MAJOR REPAIR* MAIN CABIN L/H SIDE SEAT TRACK HAS CORROSION BETWEEN STA Y=1581-1601 AND X=8.5.REPAIRED CORRODED SEAT TRACK AT THE MAIN CABIN L/H SIDE BETWEEN STA Y=1581-1601 AND X=8.5 IAW SRM 53-00-52 REPAIR 1 FIG 201. (MAJOR)
- [SDR IPXA2023051193193](https://openairdocs.org/sdr/IPXA2023051193193.md): Floor Panel · corroded · May 8, 2023 · N260UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:N/ACOURIER AREA R/H FLOOR PANEL JUST I/B OF LAV. HAS CORROSION AT STA Y=392 - Y=421.578 X=0 - X=-17REPLACED FOR PANEL PER DWG SP11530074,ABA8225 AND MD-11 SRM51-31-01,SRM51-33-01. USING PART AS SAMPLE PER UPS GMM 09-10.MINOR
- [SDR IPXA2023051993272](https://openairdocs.org/sdr/IPXA2023051993272.md): Skin · punctured · May 7, 2023 · N260UP · Doug MD11F · Wing, Plate/Skin
  > INSPECTION TYPE:3C*** MAJOR REPAIR *** R/W FIXED L/E SKIN HAS TWO PUNCTURES THROUGH SKIN O/B OF SLAT TRACK BETWEEN STA XIS=250 - XIS=263.REPAIRED SKIN AT THE R/H FIXED L/E O/B OF SLAT TRACK BETWEEN STA XIS=250 - XIS=263 IAW VTSAA EA 011-5730-01-A9957 I/R, UPS
- [SDR IPXA2023051193192](https://openairdocs.org/sdr/IPXA2023051193192.md): Floor Panel · corroded · May 5, 2023 · N260UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:N/ACORROSION FOUND ON MAIN CABIN FLOOR PANEL AT STA Y=386 - Y=421.578 AND BETWEEN X= 27.5 TO X=42REPLACED MAIN CABIN FLOOR PANEL AT STA Y=386 TO Y=421.578, X=27.5 TO X=42 IAW DWG ABA8304 AND SRM 51-31-01,SRM 51-33-01 AND USING ORIGINAL PART A
- [SDR IPXA2023050293095](https://openairdocs.org/sdr/IPXA2023050293095.md): Stringer · cracked · May 2, 2023 · N260UP · Doug MD11F · Wing, Plate/Skin
  > INSPECTION TYPE:C3*MAJOR REPAIR* R/H FIXED LE LOWER STRINGER IS CRACKED AT PANEL LANDING 11 IN O/B OFSLAT TRACK 12, STA XOS=787REPAIRED R/H WING FIXED LE LOWER STRINGER AT STA XOS =787 IAW MD-11 SRM 57-40-03-2R-1 REPAIR 1, REV 69.01. MAJOR
- [SDR IPXA2023051693250](https://openairdocs.org/sdr/IPXA2023051693250.md): Seat Track · corroded · Apr 25, 2023 · N260UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:3CCOURIER AREA R/H SEAT TRACK HAS CORROSION AT STA STA 421.578 X=-27.500 FROM CL.REPAIRED CORRODED SEAT TRACK AT THE COURIER AREA R/H SIDE STA 421.578 X=-27.500 FROM CL IAW VTSAA EA 011-5310-01-A9949 I/R, UPS EO MD11-5310-86791-A DATED 05/12/23
- [SDR IPXA2023051293203](https://openairdocs.org/sdr/IPXA2023051293203.md): Seat Track · corroded · Apr 25, 2023 · N260UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:3CCOURIER AREA HAS A SEAT TRACK AT STA X=0.00 WITH CORROSION BETWEEN Y=420.77 AND Y=515.93.REMOVED, FABRICATED AND REPLACED CORRODED SEAT TRACK AT THE COURIER AREA AT STA X=0.00 BETWEEN Y=420.77 - Y=515.93 IAW SRM 51-31-01 (MINOR)
- [SDR IPXA2023050693139](https://openairdocs.org/sdr/IPXA2023050693139.md): Floor Panel · corroded · Apr 25, 2023 · N260UP · Doug MD11F · Fuselage Floor Panel
  > INSPECTION TYPE:3CCOURIER AREA R/H SIDE HAS A FLOOR PANEL WITH CORROSION 68 INCH FROM CL AT STA 421.578.REPLACED CORRODED FLOOR PANEL AT THE COURIER AREA R/H SIDE 68 INCH FROM CL AT STA 421.578 IAW SRM 51-31-01. (MINOR)
- [SDR IPXA2023051993271](https://openairdocs.org/sdr/IPXA2023051993271.md): Skin · corroded · Apr 23, 2023 · N260UP · Doug MD11F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:3C*** MAJOR REPAIR *** AFT FUSELAGE R/H SIDE BODY FAIRING AREA STA Y=2140-Y=2160 AND LONGERON 33R-35R LWR EXTERNAL SURFACE HAS CORROSION.REPAIRED CORRODED SURFACE SKIN AT THE AFT FUSELAGE R/H SIDE BODY FAIRING BETWEEN STA Y=2140-Y=2160 AND LON
- [SDR IPXA2023051893262](https://openairdocs.org/sdr/IPXA2023051893262.md): Splice · cracked · Apr 22, 2023 · N260UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:3CMAIN CABIN L/H WALL AT STA Y=5-123, LONGERON 14L HAS A PRODUCTION SPLICE WITH A CRACKED.REMOVED, FABRICATED AND REPLACED CRACKED SPLICE AT THE MAIN CABIN L/H WALL AT STA Y=5-123 LONGERON 14L IAW SRM 51-33-01. (MINOR)
- [SDR IPXA2023051893261](https://openairdocs.org/sdr/IPXA2023051893261.md): Splice · cracked · Apr 22, 2023 · N260UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:3CMAIN CABIN R/H WALL AT STA Y=5-123, LONGERON 8R HAS A PRODUCTION SPLICE WITH A CRACKED.REMOVED, FABRICATED AND REPLACED CRACKED SPLICE AT THE MAIN CABIN R/H WALL AT STA Y=5-123, LONGERON 8R IAW SRM 51-33-01. (MINOR)
- [SDR IPXA2023051893260](https://openairdocs.org/sdr/IPXA2023051893260.md): Splice · cracked · Apr 22, 2023 · N260UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:3CMAIN CABIN R/H WALL AT STA Y=5-123, LONGERON 6R HAS PRODUCTION SPLICE WITH A CRACKED.REMOVED, FABRICTED AND REPLACED CRACKED SPLICE AT THE MAIN CABIN R/H WALL AT STA Y=5-123, LONGERON 6R IAW SRM 51-33-01. (MINOR)
- [SDR IPXA2023051993268](https://openairdocs.org/sdr/IPXA2023051993268.md): Stringer · cracked · Apr 21, 2023 · N260UP · Doug MD11F · Wing, Longeron/Stringer
  > INSPECTION TYPE:3C*MAJOR REPAIR* UPPER CENTER AUXILIARY TANK HAS CRACKED EXISTING REPAIR BETWEEN STA XCW =-46 AND XCW =-17 ON STRINGER 47.REPAIRED CRACKED STRINGER 47 AT THE UPPER CENTER AUXILIARY TANK BETWEEN STA XCW=-46 AND XCW=-17 IAW VTSAA EA 011-5710-01-
- [SDR IPXA2023052293273](https://openairdocs.org/sdr/IPXA2023052293273.md): Spar Cap · corroded · Apr 20, 2023 · N260UP · Doug MD11F · Wing Spar
  > INSPECTION TYPE:3C*** MAJOR REPAIR *** L/H WING REAR SPAR LOWER CAP LOCATED ABOVE OF O/B FLAP HINGE FITTING STA XORS=737.550 HAS CORROSION.REPAIRED CORRODED REAR SPAR LOWER CAP AT THE L/H WING ABOVE O/B FLAP HINGE FITTING AT STA XORS=737.550 IAW VTSAA EA 011-5
- [SDR IPXA2023050993163](https://openairdocs.org/sdr/IPXA2023050993163.md): Skin · corroded · Apr 20, 2023 · N260UP · Doug MD11F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:3CMAIN CABIN R/H CTR WING BOX UPPER SURFACE FWD EDGE HAS CORROSION BETWEEN STA XCW=-96.5 AND XCW=-81.REPAIRED CORRODED SURFACE SKIN AT THE MAIN CABIN R/H CTR WING BOX UPPER FWD EDGE BETWEEN STA XCW=-96.5 AND XCW=-81 IAW VTSAA EA 011-5710-01-A99
- [SDR IPXA2023050993160](https://openairdocs.org/sdr/IPXA2023050993160.md): Seat Track · corroded · Apr 20, 2023 · N260UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:3C*MAJOR REPAIR* MAIN CABIN R/H SEAT TRACK HAS CORROSION AT STA Y=5-11 AND 28 INCH FROM CL.REPAIRED CORRODED SEAT TRACK AT THE MAIN CABIN R/H SIDE STA Y=5-11 AND 28 INCH FROM CL IAW SRM 53-00-52-2R-1 FIG 201 REPAIR 1. (MAJOR)
- [SDR IPXA2023050993159](https://openairdocs.org/sdr/IPXA2023050993159.md): Seat Track · corroded · Apr 20, 2023 · N260UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:3C*MAJOR REPAIR* MAIN CABIN R/H SEAT TRACK HAS CORROSION AT STA Y=5-11 AND 8.5 INCH FROM CL.REPAIRED CORRODED SEAT TRACK AT THE MAIN CABIN AT STA Y=5-11 AND 8.5 INCH FROM CL IAW SRM 53-00-52 FIG 201 REPAIR 1 (MAJOR)
- [SDR IPXA2023050993158](https://openairdocs.org/sdr/IPXA2023050993158.md): Seat Track · corroded · Apr 20, 2023 · N260UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:3C*MAJOR REPAIR* MAIN CABIN R/H SEAT TRACK HAS CORROSION BETWEEN STA Y=1521/5-11 AND X=75.5.REPAIRED CORRODED SEAT TRACK AT THE MAIN CABIN R/H SIDE BETWEEN STA Y=1521/5-11 AND X=75.5 IAW SRM 53-00-52-2R-1 FIG 201 REPAIR 1 (MAJOR)
- [SDR IPXA2023050993167](https://openairdocs.org/sdr/IPXA2023050993167.md): Skin · corroded · Apr 20, 2023 · N260UP · Doug MD11F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:3CMAIN CABIN R/H CTR WING BOX TUNNEL HAS 3EA AREA OF CORROSION BETWEEN STA Y=1256-1305 AND 105 - 108 INCH FROM CL.REPARIED CORRODED SKIN AT THE MAIN CABIN R/H CTR WING BOX TUNNEL BETWEEN STA Y=1256-1305 AND 105-108 INCH FROM CL IAW VTSAA EA 011
- [SDR IPXA2023050993166](https://openairdocs.org/sdr/IPXA2023050993166.md): Skin · corroded · Apr 20, 2023 · N260UP · Doug MD11F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:3CMAIN CABIN L/H CTR WING BOX SKIN AT STRINGER 15 HAS CORROSION 98 INCH FROM CL.REPAIRED CORRODED SKIN AT THE MAIN CABIN L/H CTR WING BOX AREA AT STA XCW=94 - XCW=98 IAW VTSAA EA 011-5730-01-A9947 I/R UPS MD11-5730-86789-A DATED 05/05/23 (MINOR
- [SDR IPXA2023050593129](https://openairdocs.org/sdr/IPXA2023050593129.md): Bracket · cracked · Apr 20, 2023 · N260UP · Doug MD11F · Wing, Plate/Skin
  > INSPECTION TYPE:3CL/H WING O/B FLAP I/B HINGE FWD TIP STRUCTURE HAS A CRAKCED CLIP.REMOVED, FABRICATED AND REPLACED CLIP AT THE L/H WING O/B FLAP I/B HINGE FWD SIDE IAW SRM 51-33-01 DWR ARC0744 (MINOR)
- [SDR IPXA2023050593127](https://openairdocs.org/sdr/IPXA2023050593127.md): Bracket · cracked · Apr 20, 2023 · N260UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3CR/H O/B FLAP I/B FAIRING FWD O/B BRACKET CLIP IS CRACKED.REMOVED, FABRICATED AND REPLACED CLIP AT THE R/H O/B FLAP FWD SIDE IAW SRM 51-31-01 (MINOR)
- [SDR IPXA2023051293204](https://openairdocs.org/sdr/IPXA2023051293204.md): Slat · damaged · Apr 19, 2023 · N260UP · Doug MD11F · Leading Edge Devices
  > INSPECTION TYPE:3CL/H WING #5 SLAT I/B UPPER CORNER HAS KNIFE EDGE DAMAGED.REMOVED, FABRICATED AND REPLACED TRAILING EDGE AT THE L/H WING #5 SLAT IAW VTSAA EA 011-5740-01-A9954 I/R, UPS EO MD11-5750-86857-A DATED 05/12/23 (MINOR)
- [SDR IPXA2023050993157](https://openairdocs.org/sdr/IPXA2023050993157.md): Floor Panel · corroded · Apr 19, 2023 · N260UP · Doug MD11F · Fuselage Floor Panel
  > INSPECTION TYPE:3CUNDER RCB WALL FLOOR PANEL WSP0791-501 HAS CORROSION AFT OF 1ST FLOOR FITTING.REPLACED CORRODED FLOOR PANEL UNDER RCB WALL AFT OF 1ST FLOOR FITTING IAW SRM 51-31-01 (MINOR)
- [SDR IPXA2023051293202](https://openairdocs.org/sdr/IPXA2023051293202.md): Floor Panel · corroded · Apr 18, 2023 · N260UP · Doug MD11F · Passenger Compartment Equipment
  > INSPECTION TYPE:3C COURIER FLOOR AREA UNDER MOON MAT HAS BULGING SURFACE BETWEEN STA Y=392 - Y=440.REPLACED CORRODED FLOOR PANEL AT THE COURIER FLOOR AREA AT STA Y=392 - Y=440 IAW SRM 51-33-01 (MINOR)
- [SDR IPXA2023050993161](https://openairdocs.org/sdr/IPXA2023050993161.md): Angle · bent · Apr 18, 2023 · N260UP · Doug MD11F · Fuselage Structure (General)
  > INSPECTION TYPE:3CL/H MLG W/W AREA O/B LWR AFT SIDE WALL ANGLE FRAME HAS A BENT.REPLACED BENT ANGEL AT THE L/H MLG W/W AREA O/B LWR AFT SIDE WALL IAW SRM 51-31-01 (MINOR)
- [SDR IPXA2023020390568](https://openairdocs.org/sdr/IPXA2023020390568.md): Door · not reported · Feb 3, 2023 · N260UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION TYPE:NA*** SUPPLEMENTAL SDR *** DOOR L1 INTERMITTENT CLOSING. DEFERRED L1 CREW ENTRY DOOR IAW MEL 52-10-3-1-2 1 M801890 OPEN.ADJUSTED TIE ROD END ON L1 DOOR MOTOR REF MD11 AMM 52-10-06 OPS CHK GOOD THIS CLEARS M 801890
- [SDR IPXA2023012490219](https://openairdocs.org/sdr/IPXA2023012490219.md): Control Unit · faulted · Jan 23, 2023 · N260UP · Doug MD11F · Passenger/Crew Doors
  > L1 DOOR ELECTRIC CONTROL INOP. CW OPS CHECK PER AMM 52-11-02 AFTER CYCLING CB.
- [SDR IPXA2023010389495](https://openairdocs.org/sdr/IPXA2023010389495.md): Chain · broken · Jan 2, 2023 · N260UP · Doug MD11F · Passenger/Crew Doors
  > L1 DOOR EMERGENCY OPERATION INOP. L1 EMER DOOR CHAIN BROKEN. R & R THE SPROCKET FOR THE FWD L1 DOOR POWER DRIVE SUPPORT ASSY IAW CMM 52-11-09, REPLACED ROLLER CHAIN IAW CMM 52-11-09 7793949. PERFORMED PNEUMATIC OPS CHECK IAW AMM 52-11-04. SERVICED RESEVOIR
- [SDR IPXA2023010289481](https://openairdocs.org/sdr/IPXA2023010289481.md): Line · stripped · Jan 2, 2023 · N260UP · Doug MD11F · Service Doors
  > DURING INSPECTION OF R1 DOOR BOTTLE LINES, FOUND UNION ON MOTOR DAMAGED. R & R UNION FITTING ON THE MOTOR IAW AMM 52-11-05.
- [SDR IPXA2022122189205](https://openairdocs.org/sdr/IPXA2022122189205.md): Anti-Skid Sys · inoperative · Dec 20, 2022 · N260UP · Doug MD11F · Brake Anti-Skid Section
  > INSPECTION TYPE:NA ON LANDING A/C DECELERATED NORMALLY W/ AUTO BRAKES WHEN BRAKES WERE DISARMED A/C CONT BRAKING 50% N1 REQUIRD TO EXIT RUNWAY ATTEMPTED SHORT TAXI, HIGH POWER REQUIRD. A/C PULLED SLIGHTLY TO RIGHT ON TAXI SHUT DOWN SHORT OF RAMP REQUESTED MAIN
- [SDR IPXA2021081172616](https://openairdocs.org/sdr/IPXA2021081172616.md): Door · inoperative · Aug 6, 2021 · N260UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION TYPE:N/ATRIED CLOSING THE CABIN DOOR FORWARD LEFT AND WOULD NOT OPERATECYCLED CB DOOR POWER, DOOR OPS CHK NML REF AMM 52-10-01
- [SDR IPXA2021062570951](https://openairdocs.org/sdr/IPXA2021062570951.md): Start Valve · faulted · Jun 24, 2021 · N260UP · Doug MD11F · Engine Start Valves/Controls
  > ATB ** LANDED WITHOUT INCIDENT ** PASSING FL220 START VALVE LIGHT ILLUMINATED. CREW WAS DIVERTED DUE TO ICING CONDITIONS. CREW WILL WORK WITH DISPATCH ON THAT. ITEM REMAINS ON DEFERRAL. M747866.RAN WIRING WDM 80-11-02. FRN-RD SHRTD TO SHIELD BTWN P1 8235 PIN "

Next page: https://openairdocs.org/aircraft/N260UP/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 = 'N260UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N260UP/reports

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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.