# Service difficulty reports: N287UP

A list on [N287UP](https://openairdocs.org/aircraft/N287UP.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 · 343 reports

- [SDR IPXA2025121765208](https://openairdocs.org/sdr/IPXA2025121765208.md): Slide · no discrepancy · Dec 16, 2025 · N287UP · Doug MD11F · Escape Slide
  > R1 SLIDE LOCK PIN INSTALLED INSTALLED LOCK PIN INTO REGULATOR/VALVE ASSY @ R1 SLIDE IRW MD11 AMM 25-61-15-000-801 STEP C (1) FOM SLIDE DEACTIVATION REF SUBTASK 10-10-07-550-008.
- [SDR IPXA2025121600179](https://openairdocs.org/sdr/IPXA2025121600179.md): Slide · no discrepancy · Dec 16, 2025 · N287UP · Doug MD11F · Escape Slide
  > L1 SLIDE LOCK PIN INSTALLED INSTALLED LOCK PIN INTO REGULATOR/VALVE ASSY @ L1 SLIDE IRW MD11 AMM 25-61-15-000-801 STEP C (1) FOM SLIDE DEACTIVATION REF SUBTASK 10-10-07-550-008. (T3F18E007XVZA STEP 10)
- [SDR IPXA2025090267453](https://openairdocs.org/sdr/IPXA2025090267453.md): Battery Pack · inoperative · Sep 2, 2025 · N287UP · Doug MD11F · Emergency Lighting
  > EMER LT BAT 1 LO ON STATUS PAGE. R & R EMER SUPPLY BATTERY IAW AMM 33-51-01-401.
- [SDR IPXA2025061301745](https://openairdocs.org/sdr/IPXA2025061301745.md): Slide · misoverhauled · Jun 13, 2025 · N287UP · Doug MD11F · Escape Slide
  > FOUND R1 DOOR SLIDE HANGING DOWN AND INCORRECTLY PACKED IN DOOR HOUSING. DOOR SLIDE IS REMOVED. INSTALLED THE R1 EVACUATION SLIDE/RAFT AND CONTAINER IAW AMM 25-61-01-400-801.
- [SDR IPXA2024112225630](https://openairdocs.org/sdr/IPXA2024112225630.md): Panel · cracked · Nov 1, 2024 · N287UP · Doug MD11F · Passenger/Crew Doors
  > L1 DOOR LWR PANEL P/N AWE7758-11 IS CRACK, 52-10. INSTALLED L1 DOOR LOWER ACCESS PANEL P/N AWE7758-11 IN REF TO MD-11 SRM 51-31-01. REVIEWED.
- [SDR IPXA2024110425630](https://openairdocs.org/sdr/IPXA2024110425630.md): Panel · cracked · Nov 1, 2024 · N287UP · Doug MD11F · Passenger/Crew Doors
  > L1 DOOR LWR PANEL P/N AWE7758-11 IS CRACK, 52-10 VERIFIED STEP 3 IS C/W
- [SDR IPXA2024111667686](https://openairdocs.org/sdr/IPXA2024111667686.md): Roller Tray · corroded · Oct 25, 2024 · N287UP · Doug MD11F · Fuselage Main, Structure
  > FWD CARGO LOADING SYSTEM TRAY ASSY HAS CORROSION AT STA 1099 (114-12) ATA 53-10. ACCOMPLISHED EO-92095-REQ1 & VT-SAA EA 011-2555-01-B0305 I/R. VERIFIED REPAIR IS ACCOMPLISHED PER REQUIREMENTS IAW EA# 011-2555-02-B0305 REV P2 STEP 13.
- [SDR IPXA2024111467702](https://openairdocs.org/sdr/IPXA2024111467702.md): Floor Panel · damaged · Oct 25, 2024 · N287UP · Doug MD11F · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL 127CH AND 127AH (PANELS P/N WSP1126-507 2EA) CORNER DAMAGED. (114-13) FABRICATED FWD CARGO FLR PANEL 127CH IAW SREO-27386-REQ001/ DWG/SAMPLE, ON TRAVELER 70030451920001.
- [SDR IPXA2024110620506](https://openairdocs.org/sdr/IPXA2024110620506.md): Skin · dented · Oct 24, 2024 · N287UP · Doug MD11F · Fuselage Main, Plate/Skin
  > NOSE LOWER FUSEIAGE SKIN HAS A DENT NOT IN THE ADM MAPPING AT STA 380 BETWEEN LONGERON 51R AND 52. MARK MM001. ACCOMPLISHED REPAIR PER MD11 53-00-01-2R-1 REPAIR #1 FIGURE 201 REV 71.
- [SDR IPXA2024112258138](https://openairdocs.org/sdr/IPXA2024112258138.md): Panel · broken · Oct 21, 2024 · N287UP · Doug MD11F · Fuselage Miscellaneous Structure
  > L-1 ENTRY DOOR SLIDING CEILING PANEL EXIT' SIGN ESCUTCHEON IS BROKEN, HELD ON WITH CARGO PIT TAPE. MKD AS DBT-100. APG SKILL. ATA 52-10. REMOVED AND REPLACED GROMMET ON EXIT SIGN AND INSTALLED EXIT SIGN ON L-1 ENTRY DOOR SLIDING CEILING PANEL IN REF TO BOEING
- [SDR IPXA2024102258138](https://openairdocs.org/sdr/IPXA2024102258138.md): Structure · broken · Oct 21, 2024 · N287UP · Doug MD11F · Passenger Compartment Equipment
  > **SDR FILED OPEN**L-1 ENTRY DOOR SLIDING CEILING PANEL EXIT' SIGN ESCUTCHEON IS BROKEN, HELD ON WITH CARGO PIT TAPE. MKD AS DBT-100. APG SKILL. ATA 52-10.
- [SDR IPXA2024080579730](https://openairdocs.org/sdr/IPXA2024080579730.md): Window · delaminated · Aug 3, 2024 · N287UP · Doug MD11F · Flight Compartment Windows
  > L1 WINDOW DELAMINATED AND CRACKED R/R L1 WINDOW PER AMM 56-11-01-401 CONFIG 1. OPS CK NORMAL. ACCOMPLISHED RII STEPS AS REQUIRED PER GMM 04.02.01.15 CHAPTER 56 & MM 56-11-01-401 CONFIG 1, SYS OPS CHK€™S NORMAL.
- [SDR IPXA2024070284184](https://openairdocs.org/sdr/IPXA2024070284184.md): Skin · dented · Jun 16, 2024 · N287UP · Doug MD11F · Fuselage Main, Plate/Skin
  > DENT ON AFT UPPER FUSELAGE VERIFIED ALL REPAIR STEPS COMPLETED REF EO-90533-REQ3 [T3F18E004RSS0].
- [SDR IPXA2024061684184](https://openairdocs.org/sdr/IPXA2024061684184.md): Skin · dented · Jun 16, 2024 · N287UP · Doug MD11F · Fuselage Main, Plate/Skin
  > DENT ON AFT UPPER FUSELAGE.
- [SDR IPXA2023030191439](https://openairdocs.org/sdr/IPXA2023030191439.md): Restraint · dislodged · Feb 28, 2023 · N287UP · Doug MD11F · Emergency Equipment
  > INSPECTION TYPE:N/APBE RESTRAINT SYSTEM ON LEFT BULKHEAD NEEDS REPAIR. PBE DISLODGED DURING TAKEOFF ROLLRESECURED PBE RESTRAINT SYSTEM ON L BULKHEAD AS REQ'D IAW AMM 25-60-00
- [SDR IPXA2022111988232](https://openairdocs.org/sdr/IPXA2022111988232.md): Limit Switch · inoperative · Nov 18, 2022 · N287UP · Doug MD11F · Service Doors
  > R1 ENTRY DOOR INOP. R/R UP LIMIT SWITCH ON R1 DOOR & OPS CHECK GOOD IAW AMM 52-16-01.
- [SDR IPXA2022102487437](https://openairdocs.org/sdr/IPXA2022102487437.md): Floor Support · broken · Oct 18, 2022 · N287UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:3C, SLOPE PANEL ATTACH FLOOR SUPPORT AT BS 1721 FOUND BROKEN AT LT FLOOR LEVEL.REMOVED, REPLACED FLOOR SUPPORT IAW SRM 51-31-01, 51-35-01 (MINOR)
- [SDR IPXA2022102787567](https://openairdocs.org/sdr/IPXA2022102787567.md): Hinge · corroded · Oct 4, 2022 · N287UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3CL/H I/B FLAP O/B FWD HINGE LWR LUG I/B FACE HAS CORROSION.REPAIRED L/H I/B FLAP O/B FWD HINGE LWR LUG I/B FACE IAW VT-SAA EA 011-5740-01-A9735-REV I/R AND UPS EO MD11-5740-85051-A DATED 10/26/2022 AND FAA FORM 8100-9 SIGNED BY J.TOM (AR-60556
- [SDR IPXA2022102787563](https://openairdocs.org/sdr/IPXA2022102787563.md): Hinge · corroded · Oct 4, 2022 · N287UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3CL/H I/B FLAP O/B FWD HINGE LWR LUG O/B FACE HAS CORROSION.REPAIRED L/H I/B FLAP O/B FWD HINGE LWR LUG IAW VT-SAA EA 011-5740-01-A9735 I/R AND UPS EO MD11-5740-85051-A DATED 10/26/2022 FAA FORM SIGNED BY J.TOM (AR-605565) DATED 10/26/2022 (MIN
- [SDR IPXA2022102687533](https://openairdocs.org/sdr/IPXA2022102687533.md): Hinge Fitting · corroded · Oct 4, 2022 · N287UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3C, R/H I/B FLAP O/B FWD HINGE LWR LUG O/B FACE HAS CORROSION.REPAIRED R/H I/B FLAP O/B FWD HINGE LWR LUG O/B FACE IAW VT-SAA EA 011-5740-01-A9736 REV I/R AND UPS EO MD11-5740-85053-A DATED 10/25/2022 AND FAA FORM SIGNED BY J.TOM (AR-605565) DA
- [SDR IPXA2022102687532](https://openairdocs.org/sdr/IPXA2022102687532.md): Hinge Fitting · corroded · Oct 4, 2022 · N287UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3CR/H I/B FLAP O/B FWD HINGE LWR I/B FACE HAS CORROSION.REPAIRED R/H I/B FLAP O/B FWD HINGE I/B FACE IAW EA 011-5740-01-A9736 REV I/R AND EO MD11-5740-85083-A DATED 10/25/2022 AND FAA FORM 8100-9.
- [SDR IPXA2022102687531](https://openairdocs.org/sdr/IPXA2022102687531.md): Hinge Fitting · corroded · Oct 4, 2022 · N287UP · Doug MD11F · Trailing Edge Flap Control System
  > INSPECTION TYPE:3C, R/H AFT I/B FLAP O/B LWR BORE HOLE HAS CORROSION.REPAIRED R/H AFT I/B FLAP HINGE O/B LWR BORE IAW EA 011-5750-01-A9734 REV I/R AND EO MD11-5750-85054-A DATED 10/25/2022 AND FAA FORM.
- [SDR IPXA2022102687535](https://openairdocs.org/sdr/IPXA2022102687535.md): Hinge Fitting · worn · Oct 4, 2022 · N287UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3C, L/H I/B AFT FLAP O/B HINGE I/B LWR BORE HOLE IS WORN.REPAIRED L/H I/B AFT FLAP O/B HINGE I/B LWR BORE IAW EA 011-5750-01-A9733 REV I/R AND UPS MD11-5750-85052-A AND FAA FORM 8100-9.
- [SDR IPXA2022102687530](https://openairdocs.org/sdr/IPXA2022102687530.md): Hinge Fitting · corroded · Oct 4, 2022 · N287UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3CL/H O/B FLAP I/B AFT HINGE LWR I/B LUG BORE HOLE HAS CORROSION.REPAIRED L/H O/B FLAP I/B AFT HINGE LWR I/B LUG BORE IAW VT-SAA EA 011-5740-01-A9737 REV I/R AND UPS EO MD11-5750-85055-A DATED 10/25/2022 (MINOR)
- [SDR IPXA2022102587509](https://openairdocs.org/sdr/IPXA2022102587509.md): Stringer · cracked · Oct 4, 2022 · N287UP · Doug MD11F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:3CCENTER UPPER AUXILIARY TANK STR 47 EXISTING REPAIR BETWEEN STA X-17 AND X=17 IS CRACKED.REPAIRED CRACKED STRINGER 47 AT STA XCW=-32.00,XCW=32.00 IAW VT-SAA EA 011-5710-01-A9728 REV I/R AND UPS EO MD11-5710-84995-A AND FAA FORM 8100-9 SIGNED B
- [SDR IPXA2022101987278](https://openairdocs.org/sdr/IPXA2022101987278.md): Window Frame · corroded · Oct 4, 2022 · N287UP · Doug MD11F · Flight Compartment Windows
  > INSPECTION TYPE:3CWINDOW REPLACEMENT FOUND CORROSION ON LOWER VERTICAL WINDOW FRAME BETWEEN STA Y=275 - Y=295.REPAIRED VERTICAL WINDOW FRAME IAW VT-SAA EA 011-5310-01-A9731 REV I/R DATED 10/14/22 AND UPS EO MD11-5310-85019-A DATED 10/17/22. (MINOR)
- [SDR IPXA2022101287082](https://openairdocs.org/sdr/IPXA2022101287082.md): Spar · cracked · Oct 4, 2022 · N287UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:3CCENTER UPPER AUXILIARY TANK FRONT SPAR CLIP BETWEEN STA X17 AND X46 IS CRACKED.REPLACED CRACKED CLIP IN CTR UPPER AUXILIARY TANK IAW SRM 51-33-01 (MINOR)
- [SDR IPXA2022102787560](https://openairdocs.org/sdr/IPXA2022102787560.md): Skin · damaged · Oct 3, 2022 · N287UP · Doug MD11F · Rudder, Plate/Skin
  > INSPECTION TYPE:3CNO REPAIR DOUBER HISTORY ON RUDDER ASS AFT UPPER SKIN STA ZV = 487.312 R/H AFT SIDE.REMOVED, REPAIRED EXISTING REPAIR DOUBLER ON AFT UPPER RUDDER AT STA ZV = 487.312 IAW VT-SAA EA 011-5540-01-A9730 REV I/R AND UPS EO C-5540-85056-A AND FAA FO
- [SDR IPXA2022102687534](https://openairdocs.org/sdr/IPXA2022102687534.md): Angle · cracked · Oct 1, 2022 · N287UP · Doug MD11F · Elevator Structure
  > INSPECTION TYPE:3C, LT I/B ELEVATOR ANGLE BRAKET AT STA STA XE=125.8 O/B SIDE IS CRACKED.REPAIRED CRACKED ANGLE AT STA XE=125.8 ON THE L/H I/B ELEVATOR IAW EA 011-5520-01-A9729 REV I/R DATED 10/22/2022 AND UPS EO MD11-5520-85050-A. MAJOR
- [SDR IPXA2022102587499](https://openairdocs.org/sdr/IPXA2022102587499.md): Longeron Splice · corroded · Sep 29, 2022 · N287UP · Doug MD11F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:3CAFT CARGO BILGE AREA LONGERON 51L HAS A CLIP SPLICE WITH CORROSION AT STA 1941-1954.REMOVED, FABRICATIED, REPLACED THE CLIP SPLICE AT STA 1941-1954 IAW SRM 51-31-01 (MINOR)
- [SDR IPXA2022102087315](https://openairdocs.org/sdr/IPXA2022102087315.md): Web · corroded · Sep 29, 2022 · N287UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:3CCENTER CARGO BLIGE AREA HAS A CLIP, VERTICAL INTERCOSTAL-WEB AT STA 1730 RBL5 WITH CORROSION.REPLACED THE CLIP, INTERCOSTAL-WEB IAW SRM 51-31-01. (MINOR)
- [SDR IPXA2022102087314](https://openairdocs.org/sdr/IPXA2022102087314.md): Tee Fitting · corroded · Sep 29, 2022 · N287UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:3CCENTER CARGO BLIGE AT STA 1745 RBL5 HAS A TEE-CLIP WITH CORROSION.REPLACED TEE-CLIP AT STA 1745 RBL5 IAW SRM-51-31-01. (MINOR)
- [SDR IPXA2022101587151](https://openairdocs.org/sdr/IPXA2022101587151.md): Support Bracket · cracked · Sep 29, 2022 · N287UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:3CCAC COMPARTMENT R/H LRU RACK R/H LWR SUPPORT BRACKET IS CRACKED.REPLACED SUPPORT BRACKET IN THE CAC COMPARTMENT ON THE R/H LRU RACK IAW SRM 51-31-01 (MINOR)
- [SDR IPXA2022101287076](https://openairdocs.org/sdr/IPXA2022101287076.md): Support · damaged · Sep 28, 2022 · N287UP · Doug MD11F · Ailerons
  > INSPECTION TYPE:3CDAMAGED PANEL SUPPORT SIDE BRACE AT L/H O/B AILERON AT APPOX XORS 948.REPLACED DAMAGED SUPPORT IAW SRM 51-33-01 (MINOR)
- [SDR IPXA2022102087317](https://openairdocs.org/sdr/IPXA2022102087317.md): Skin · damaged · Sep 27, 2022 · N287UP · Doug MD11F · Wing, Plate/Skin
  > INSPECTION TYPE:3CL/H WING FIX L/E SKIN O/B OF #8 SLAT IS DAMAGED.REPAIRED FIX L/E SKIN IAW SRM 57-40-01 REPAIR 16. (MINOR)
- [SDR IPXA2022102787568](https://openairdocs.org/sdr/IPXA2022102787568.md): Door Frame · gouged · Sep 26, 2022 · N287UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:3C, CLG WHEEL WELL R/H FWD DOOR FRAME HAS A DEEP GOUGE. REPLACED FWD SIDE DOOR FRAME IAW SRM 51-35-01, 51-33-01. (MINOR)
- [SDR IPXA2022090285842](https://openairdocs.org/sdr/IPXA2022090285842.md): Floor Skin · inoperative · Sep 1, 2022 · N287UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION TYPE:N/A**SDR FILED OPEN**L1 DOOR ELECTRICAL ACTUATION INOP. ITEM TRANSFERRED TO DEFERRAL IAW MEL 52-10-3-1-2-12. PLACARD INSTALLED MUST USE R-1 DOOR 'NO DMP'.
- [SDR IPXA2021111175873](https://openairdocs.org/sdr/IPXA2021111175873.md): None · none · Nov 11, 2021 · N287UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION TYPE:N/A**SUPPLEMENTAL SDR ** L1 DOOR SLIDE PRESSURE GUAGE CANNOT BE READ THROUGH INSPECTION WINDOW. DEFERRED L1 SLIDE IAW MEL 52-10-3-1-2-1 REF M762615. PLACARD INSTALLEDBEGAN REMOVING SLIDE. REINSTALLED SLIDE REF AMM 25-61-15. VERIFIED BOTTLE PRES
- [SDR IPXA2021100674649](https://openairdocs.org/sdr/IPXA2021100674649.md): None · none · Oct 5, 2021 · N287UP · Doug MD11F · Emergency Lighting
  > INSPECTION TYPE:N/A**SUPPLEMENTAL SDR** EMERG LIGHT BAT 3 LO LEVEL ONE ALERT CAME ON DURING EMERGENCY LIGHT TEST DURING PRE FLIGHT. DEFERRED PER MEL 33-50-2 AND DMP 33-50-2REMOVED AND INSTALLED NEW MSC UNIT IAW AMM 31-42-01. THIS CLEARS M758798
- [SDR IPXA2021092974403](https://openairdocs.org/sdr/IPXA2021092974403.md): Door · broken · Sep 29, 2021 · N287UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION TYPE:N/ALEFT FORWARD CREW ENTRY DOOR SNAPPED ITS CABLES DUING ELECTRICAL SWITCH OPENNINGR&R'D FWD AND AFT LEFT CABLES ON L1 DOOR PER AMM 52-11-03-000-801 AND 52-11-03-400-801 ADJ OF DOOR ACT MOCK PER AMM 52-11-02-830-801 L1 DOOR OPS NORMAL
- [SDR IPXA2021092074046](https://openairdocs.org/sdr/IPXA2021092074046.md): Light · no test · Sep 19, 2021 · N287UP · Doug MD11F · Emergency Lighting
  > EMER LT BAT 3 LOW. DEFERRED EMERG LT SYS TEST FUNCTION UNDER MEL 33-50-2. ACCOMPLISHED DMP 33-50-2-. VERIFIED EMERG LTS ILLUMINATE. PLACARDED AFFECTED SWITCH. CTROL #M757062 ASSIGNEDR/R EMERGENCY POWER SUPPLY BATTERY PER AMM 33-51-01-401. OPS CK GOOD. THIS CLE
- [SDR IPXA2021050469001](https://openairdocs.org/sdr/IPXA2021050469001.md): Battery Pack · faulted · May 3, 2021 · N287UP · Doug MD11F · Emergency Lighting
  > INSPECTION TYPE:NAEMERG LT BATT 1 FAULT.DEFERRED PER MEL33-50-4 M-743320 ASSIGNED DMP C/W PLACARD INSTALLED.R& R'D EMERGENCY POWER SUPPLY BATTRERY OPS CHECK GOOD IAW AMM 33 51 01 DMP 33 50 4 HAS BEEN REVERSED IPC 33 51 01 05 015.
- [SDR IPXA2020111562399](https://openairdocs.org/sdr/IPXA2020111562399.md): Stiffener · cracked · Nov 12, 2020 · N287UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: 2C INTERCOSTAL CRACKED NEAR RT MLG WHEEL WELL HYD RESV ASSEMBLY. REMOVED, FABRICATED, AND REPLACED STIFFENER, IAW DWG AEA7035 AND SRM 51-33-01. (MINOR)
- [SDR IPXA2020111562397](https://openairdocs.org/sdr/IPXA2020111562397.md): Angle · corroded · Nov 9, 2020 · N287UP · Doug MD11F · Wing Miscellaneous Structure
  > INSPECTION TYPE: 2C LT WING OUTBOARD LOWER TRAILING EDGE ANGLE CORRODED. REMOVED AND REPLACED CORRODED ANGLE AT LT WING OUTBOARD LOWER TRAILING EDGE, IAW SRM 51-31-01 PG 1 AND DWG ARC7640. (MINOR)
- [SDR IPXA2020111562390](https://openairdocs.org/sdr/IPXA2020111562390.md): Angle · cracked · Nov 6, 2020 · N287UP · Doug MD11F · Wing Miscellaneous Structure
  > INSPECTION TYPE: 2C LT WING TRAILING EDGE SUPPORT PANEL CRACK AT AFT EDGE. REPAIRED CRACKED SUPPORT ANGLE AT LT WING TRAILING EDGE, IAW DWG ARC0679 AND SRM 51-31-01. (MINOR)
- [SDR IPXA2020111562389](https://openairdocs.org/sdr/IPXA2020111562389.md): Web · cracked · Nov 4, 2020 · N287UP · Doug MD11F · Nacelle/Pylon Miscellaneous Structure
  > INSPECTION TYPE: 2C NR 3 PYLON STRUCTURE WEB CRACK AT UPPER END YUS STA 240.5. REPAIRED NR 3 PYLON UPPER CRACKED WEB AT YUS STA 240.5, IAW SRM 54-00-00 REPAIR GEN FIG 204. (MINOR)
- [SDR IPXA2020111262309](https://openairdocs.org/sdr/IPXA2020111262309.md): Rib · cracked · Nov 1, 2020 · N287UP · Doug MD11F · Wing, Rib/Bulkhead
  > INSPECTION TYPE: 2C RT INBOARD AILERON LEADING EDGE RIB CRACK. REMOVED AND REPLACED RT INBOARD AILERON LEADING EDGE CRACKED RIB, IAW SRM 51-31-01 AND SRM 51-35-01. (MINOR)
- [SDR IPXA2020111162267](https://openairdocs.org/sdr/IPXA2020111162267.md): Intercostal · cracked · Nov 1, 2020 · N287UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: 2C TAILCONE PATIO DECK RT LOWER INTERCOSTAL CRACK AT FWD END. REMOVED AND REPLACED TAILCONE PATIO DECK INTERCOSTAL AT FWD END, IAW SRM 51-35-01 AND 51-33-01. (MINOR)
- [SDR IPXA2020110662091](https://openairdocs.org/sdr/IPXA2020110662091.md): Doubler · cracked · Oct 29, 2020 · N287UP · Doug MD11F · Wing, Plate/Skin
  > INSPECTION TYPE: 2C RT WING FIXED LEADING EDGE BEADED DOUBLER IS CRACKED BETWEEN STA XOS 653 TO 657.7. REPAIRED CRACKED RT WING FIXED LEADING EDGE BEADED DOUBLER BETWEEN STA XOS 653 TO 657.7, IAW SRM 57-40-02 REPAIR 15 FIG 205. (MAJOR)
- [SDR IPXA2020110662090](https://openairdocs.org/sdr/IPXA2020110662090.md): Doubler · cracked · Oct 29, 2020 · N287UP · Doug MD11F · Wing, Plate/Skin
  > INSPECTION TYPE: 2C RT WING FIXED LEADING EDGE BEADED DOUBLER IS CRACKED BETWEEN STA XOS 551 TO 555. REPAIRED CRACKED RT WING FIXED LEADING EDGE BEADED DOUBLER BETWEEN STA XOS 551 TO 555, IAW SRM 57-40-02 REPAIR 15 FIG 205. (MAJOR)

Next page: https://openairdocs.org/aircraft/N287UP/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 = 'N287UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N287UP/reports

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