# Service difficulty reports: N286UP

A list on [N286UP](https://openairdocs.org/aircraft/N286UP.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 · 350 reports

- [SDR IPXA2025101389916](https://openairdocs.org/sdr/IPXA2025101389916.md): Hydraulic Line · broken · Oct 10, 2025 · N286UP · Doug MD11F · Hydraulic System, Main
  > ATB, SHORTLY AFTER TO UPON RAISING THE LANDING GEAR GOT HYD 3 FAILED? LEVEL 2, COMPLETED CHECKLIST & COMPLETED AIR TURN BACK TO SDF. HYD SYS SHOWS 0. REPAIRED BROKEN HYDRAULIC LINE PER MM 20-10-01. SERVICED NR 3 HYDRAULIC SYSTEM PER MM 12-13-02. MOTORED NR 3 E
- [SDR IPXA2025101089916](https://openairdocs.org/sdr/IPXA2025101089916.md): Hydraulic Line · broken · Oct 10, 2025 · N286UP · Doug MD11F · Hydraulic System, Main
  > AIR TURNBACK. SHORTLY AFTER TO UPON RAISING THE LANDING GEAR GOT €ŒHYD 3 FAIL€? LEV 2 COMPLETED CHECKLIST & COMPLETED AIR TURN BACK TO SDF. HYD SYS SHOWS 0. FOLLOWED FIM FAULT TREE 29-10-08 FIG 108. CONFIRMED HYD 3 SYSTEM SHOWING 0 ON SYNOPTIC SCREEN. DURIN
- [SDR IPXA202510063023](https://openairdocs.org/sdr/IPXA202510063023.md): Pin · installed · Oct 5, 2025 · N286UP · Doug MD11F · Standard Practices/Structures
  > L1 DOOR SLIDE/RAFT SAFETY PIN INSTALLED PER AMM 25-61-00.
- [SDR IPXA2025070104685](https://openairdocs.org/sdr/IPXA2025070104685.md): Light · inoperative · Jul 1, 2025 · N286UP · Doug MD11F · Emergency Lighting
  > DURING EMER LT TEST GOT LVL 1 €ŒEMER LT BAT 1 LO€? MSG REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY PER AMM 33-51-01. OPS CHECKED GOOD.
- [SDR IPXA2025040306085](https://openairdocs.org/sdr/IPXA2025040306085.md): Cover · broken · Apr 2, 2025 · N286UP · Doug MD11F · Escape Slide
  > L1 DOOR SLIDE ARMING COVER BROKEN. REMOVED AND REPLACED DAMAGED DOOR HANDLE GUARD ASSY.
- [SDR IPXA2024122013001](https://openairdocs.org/sdr/IPXA2024122013001.md): Fire Detector · false activation · Dec 20, 2024 · N286UP · Doug MD11F · Fire Detection
  > INTERMITTENT LVL 1 FIRE DET 2 FAULT ALERT DURING CLIMB AND CRUISE. DISCONNECTED #2 ENGINE FDCU AND ALL 6 FIRE DETECTORS. CHECKED WIRING FOR SHORTS TO GND AND OTHER CONDUCTORS, NONE FOUND. AT PYLON DETECTOR FOUND ONE RING TERMINAL LOOSE ON WIRE. RETERMINATED
- [SDR IPXA2024120544935](https://openairdocs.org/sdr/IPXA2024120544935.md): Fire Detector · faulted · Dec 5, 2024 · N286UP · Doug MD11F · Fire Detection
  > ON TAXI OUT LVL1 €Œ FIRE DET 2 FAULT€? MSG ACCOMPLISHED OPS CHECK PER AMM 71-50-01 STEP E. (4) OPS CHECK GOOD. NO FAULTS. THIS CLEARS DEFERRAL, PLACARD REMOVED.
- [SDR IPXA2024112695842](https://openairdocs.org/sdr/IPXA2024112695842.md): Battery · discharged · Nov 26, 2024 · N286UP · Doug MD11F · Emergency Lighting
  > EMERGENCY LT BAT LO. REMOVED AND REPLACED EMERGENCY LIGHTS POWER SUPPLY BATTERY PER AMM 33-51-01 OPS NORMAL
- [SDR IPXA2024092135681](https://openairdocs.org/sdr/IPXA2024092135681.md): Cover · out of position · Sep 21, 2024 · N286UP · Doug MD11F · Passenger/Crew Doors
  > L1 ENTRY DOOR SLIDE COVER LATCHES ON DOOR COVER WHEN OPENING THE L1 ENTRY DOOR. SECURED L1 ENTRY DOOR SLIDE COVER IAW AMM 25-23-07-400. OPS NORMAL
- [SDR IPXA2024072783467](https://openairdocs.org/sdr/IPXA2024072783467.md): Stiffener · cracked · Jul 5, 2024 · N286UP · Doug MD11F · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT. STEP UP BULKHEAD LOCATED AT STA 1841 AND STR49R HAS CRACKED STIFFENER. (015-36) ATA53. OPEN
- [SDR IPXA2024072783294](https://openairdocs.org/sdr/IPXA2024072783294.md): Stiffener · cracked · Jul 5, 2024 · N286UP · Doug MD11F · Fuselage Main, Bulkhead
  > AFT CARGO COMPARTMENT. STEP UP BULKHEAD LOCATED AT STA 1841 AND STR49L HAS CRACKED STIFFENER. (015-35) ATA53.REMOVED 1EA. STIFFENER AT AFT CARGO COMPARTMENT STEP UP BULKHEAD AT STA 1841 AND STR 49L IAW MD-11 SRM 51-33-01-0G-0.LOCATETD DRILLED AND INSTALLED STI
- [SDR IPXA2024072753567](https://openairdocs.org/sdr/IPXA2024072753567.md): Rib · cracked · Jul 3, 2024 · N286UP · Doug MD11F · Wing, Rib/Bulkhead
  > [STR] R/H WING. FIXED L/E COMPARTMENT HAS CRACKED RIB ANGLE LOCATED APPROX STA XORS 480. (015-10) ATA57.REMOVED RIB ANGLE DAMAGE AT R/H WING FIXED L/E COMP APPROX STA XORS 480 IN REF MD11 SRM 51-33-01.INSTALLED PROTECCION EWIS ON R/H WING FIXED L/E COMPARTMENT
- [SDR IPXA2024072453579](https://openairdocs.org/sdr/IPXA2024072453579.md): Doubler · cracked · Jul 3, 2024 · N286UP · Doug MD11F · Wing Miscellaneous Structure
  > R/H WING. FIXED L/E COMPARTMENT HAS CRACKED BEADED DOUBLER LOCATED APPROX STA XOS 680. (015-11) ATA57.REMOVED 12 EA WIRE CLAMPS FOR ACCESS TO REMOVE BEADED DOUBLER SECTION R/H WING FIXED L/E COMPARTMENT APPROX STA 572 PER REF MD-11 SRM 51-31-01-0G-0.INSTALLED
- [SDR IPXA2024072422361](https://openairdocs.org/sdr/IPXA2024072422361.md): Structure · corroded · Jul 2, 2024 · N286UP · Doug MD11F · Fuselage Miscellaneous Structure
  > MAIN CABIN UPPER WING BOX HAS CORROSION AT STA 1231 FWD OF STRINGER 15 LBL 17.00 REMOVED FASTENERS TO GAIN ACCESS TO CORROSION AT MAIN CABIN UPPER WING BOX STA 1231 FWD OF STR 15 LBL 17 PER REF MD-11 SRM 57-10-01-1A-1 AD1. PERFORMED HFEC SURFACE/OPEN HOLE INSP
- [SDR IPXA2024050274133](https://openairdocs.org/sdr/IPXA2024050274133.md): Cable · broken · May 2, 2024 · N286UP · Doug MD11F · Passenger/Crew Doors
  > L1 DOOR SLIDING PANEL CABLE BROKEN AND PANEL DAMAGE R&R L1 DOOR SLIDING CEILING PANEL IAW AMM 25-23-23 & AMM 33-27-05. OPS CHECK GOOD.
- [SDR IPXA2024050136945](https://openairdocs.org/sdr/IPXA2024050136945.md): Sliding Window · leaking · Apr 30, 2024 · N286UP · Doug MD11F · Flight Compartment Windows
  > CAPT SLIDING WINDOW LEAKING EXCESSIVELY AT BOTTOM OF GLASS AT VERY AFT PORTION REPLACED THE CAPTS SLIDING WINDOW REF AMM 56-12-01.
- [SDR IPXA2024043036945](https://openairdocs.org/sdr/IPXA2024043036945.md): Sliding Window · leaking · Apr 30, 2024 · N286UP · Doug MD11F · Flight Compartment Windows
  > CAPT SLIDING WINDOW LEAKING EXCESSIVELY AT BOTTOM OF GLASS AT VERY AFT PORTION REMOVED WINDOW TRIM AND DISCONNECTED TERMINAL BLOCK PER AMM 56-12-01-000-801
- [SDR IPXA2024031203181](https://openairdocs.org/sdr/IPXA2024031203181.md): Battery · discharged · Mar 12, 2024 · N286UP · Doug MD11F · Emergency Lighting
  > ON PDC FOUND EMERGENCY BATT LOW RNR'D EMERGENCY POWER SUPPLY AMM 33-51-01/401 OPS CK GOOD PLACARD REMOVED
- [SDR IPXA2024031315825](https://openairdocs.org/sdr/IPXA2024031315825.md): Unknown · unknown · Mar 6, 2024 · N286UP · Doug MD11F · Electrical Power System
  > POWER ON€? WHEN ON SHORT FINAL. ELECTRICAL SYSTEM IN AUTO. SYSTEM TEST NORMAL PER MM 24-24-00/501.
- [SDR IPXA2024030615825](https://openairdocs.org/sdr/IPXA2024030615825.md): Unknown · unknown · Mar 6, 2024 · N286UP · Doug MD11F · Electrical Power System
  > *SDR FILED OPEN* €ŒEM POWER ON€? WHEN ON SHORT FINAL. ELECTRICAL SYSTEM IN AUTO. SYSTEM TEST NORMAL PER MM 24-24-00/501.
- [SDR IPXA2024020632939](https://openairdocs.org/sdr/IPXA2024020632939.md): Tire · failed · Feb 6, 2024 · N286UP · Doug MD11F · Tire
  > LEVEL 2 TIRE FAILURE ALERT WITH AUDIBLE ALERT ON TAKE OFF ROLL, TAKE OFF CONTINUED, LEFT GEAR DOWN. NO TIRE FAILED INDICATIONS ON CONFIG PAGE. REVERSED DMP. R&R BRAKE TEMP/TIRE PRESS COMPUTER PER AMM 32-46-02, OPS-CHECK GOOD. TIRE PRESSURE INDICATION REMAINED
- [SDR IPXA2024013098516](https://openairdocs.org/sdr/IPXA2024013098516.md): Light · intermittent · Jan 30, 2024 · N286UP · Doug MD11F · Emergency Lighting
  > FOUND EMERGENCY LIGHTING SYSTEM TEST FUNCTION INTERMITTENTLY WORKING WHEN PRESS TO TEST. EMERGENCY LIGHTING SYSTEM TEST FUNCTION DEFERRED PER MEL 33-50-2. DMP C/W. PLACARD INSTALLED. FOUND EMERGENCY LIGHTING SYSTEM TEST FUNCTION INTERMITTENTLY WORKING WHEN PR
- [SDR IPXA2024012400101](https://openairdocs.org/sdr/IPXA2024012400101.md): Handle · not seated · Jan 23, 2024 · N286UP · Doug MD11F · Service Doors
  > R1 CONTROL DOOR HANDLE IS NOT SEATED CORRECTLY R1 DOOR EMERGENCY HANDLE (RED) IS CONFIGURED IN THE RIGHT NEUTRAL POSITION CORRECTLY IAW UPS MD11 52 CREW ENTRY DOORS TECH TIP. PLACARD REMOVED.
- [SDR IPXA2024011794605](https://openairdocs.org/sdr/IPXA2024011794605.md): Bottle · low pressure · Jan 17, 2024 · N286UP · Doug MD11F · Emergency Equipment
  > R1 DOOR ASSIST BOTTLE PRESSURE IS LOW SERVICED R1 DOOR ASSIST BOTTLE REF AMM 12-25-04-600-801. OK FOR SERVICE AT THIS TIME. PLACARD REMOVED.
- [SDR IPXA2023100656723](https://openairdocs.org/sdr/IPXA2023100656723.md): Light · damaged · Oct 6, 2023 · N286UP · Doug MD11F · Emergency Lighting
  > L1 DOOR FEW EMERGENCY LIGHT LENS DAMAGED REMOVED AND REPLACED L1 FWD EMERGENCY LIGHT ASSY. DOCUMENT REFERENCE: AM 33 52 01
- [SDR IPXA2023100309125](https://openairdocs.org/sdr/IPXA2023100309125.md): Not Reported · not reported · Sep 30, 2023 · N286UP · Doug MD11F · Nacelle/Pylon Structure
  > #3 ENG OUTBOARD FAN COWL CRACKED INSTALLED SERVICEABLE #3 ENGINE R/H FAN COWLING IAW MD11 AMM 71-12-01
- [SDR IPXA2023090394078](https://openairdocs.org/sdr/IPXA2023090394078.md): Floor Panel · gouged · Sep 3, 2023 · N286UP · Doug MD11F · Fuselage Floor Panel
  > INSPECTION TYPE:N/AMAIN DECK FLOOR PANEL GOUGED AT STA 879FABBED NEW FLOOR PANEL IAW EO MD11-5320- 27386-C
- [SDR IPXA2023032992379](https://openairdocs.org/sdr/IPXA2023032992379.md): Vent · odor · Mar 28, 2023 · N286UP · Doug MD11F · Air Distribution System
  > INSPECTION TYPE:N/AIN FLIGHT WE GOT AN ACRID SMELL FOLLOWED BY HAZY SMOKE IN THE COCKPIT. DISSIPATED AFTER SEVERAL MINUTESREPLACED CB DIMMER IAW MM 33-11-03
- [SDR IPXA2022072084371](https://openairdocs.org/sdr/IPXA2022072084371.md): Fan · inoperative · Jul 20, 2022 · N286UP · Doug MD11F · Air Distribution System
  > INSPECTION TYPE:NAON DECENT BETWEEN FL260- FL190, DISTINCT SPINNING ROTATIONAL SOUND FROM BELOW FLIGHT DECK FOLLOWED BY DISTINCT NON-CAUSTIC SMELL. AS SOON AS SOUND STOPPED SMELL DISAIPPATED QUICKLY. NO SMOKE/NO ALERTS/ NO CREW ACTION OTHER THAN EXPEDITED LFOU
- [SDR IPXA2022062783545](https://openairdocs.org/sdr/IPXA2022062783545.md): Rudder · corroded · Jun 10, 2022 · N286UP · Doug MD11F · Rudder Structure
  > INSPECTION TYPE:3CUPPER FWD. RUDDER L/E RIB AT STA. XFR= 450.173 CANT IS CORRODED.REMOVED, FABRICATED AND REPLACED RIB/TEE IAW DWG. AMC7292 AND SRM 51-33-01. (MINOR)
- [SDR IPXA2022062483458](https://openairdocs.org/sdr/IPXA2022062483458.md): Support Angle · cracked · Jun 9, 2022 · N286UP · Doug MD11F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:3C LWR FUSELAGE IN SIDE FWD AVIONICS COMP. HAS A SUPPORT ANGLE THAT IS CRACKED AT APPOX FS383 RBL12.REMOVED, FABRICATED AND REPLACED SUPPORT ANGLE IAW SRM 51-33-01. (MINOR)
- [SDR IPXA2022062483457](https://openairdocs.org/sdr/IPXA2022062483457.md): Support Angle · cracked · Jun 9, 2022 · N286UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:3CL/H AFT LOWER FUSELAGE UPPER SUPPORT ANGLE IS CRACKED AT APPX STA 1581.REMOVED, FABRICATED AND REPLACED SUPPORT ANGLE IAW SRM 51-31-01. (MINOR)
- [SDR IPXA2022062483454](https://openairdocs.org/sdr/IPXA2022062483454.md): Intercostal · cracked · Jun 9, 2022 · N286UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:3CR/H A/C BAY INTERCOSTAL IS CRACKED AT AFT UPPER CORNER LOCATED AT APPROX FS 553 RL31.REMOVED,FABRICATED AND REPLACED THE CRACKED INTERCOSTAL IAW SRM 51-33-01 (MINOR)
- [SDR IPXA2022062283357](https://openairdocs.org/sdr/IPXA2022062283357.md): Angle · cracked · Jun 8, 2022 · N286UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:3CAFT CARGO AT STA. 1841 AND LBL 25, VERTICAL STIFFNER IS CRACKED.REMOVED, FABRICATED AND REPLACED STIFFNER IAW DWG. 7170 AND SRM 51-33-01. (MINOR)
- [SDR IPXA2022062283356](https://openairdocs.org/sdr/IPXA2022062283356.md): Floor Support · cracked · Jun 8, 2022 · N286UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:3CAFT CARGO AT STA. 1841 AND RBL 25, VERTICAL STIFFNER IS CRACKED.REMOVED, FABRICATED AND REPLACED STIFFNER IAW DWG. AGA7170 AND SRM 51-33-01. (MINOR)
- [SDR IPXA2022062283355](https://openairdocs.org/sdr/IPXA2022062283355.md): Stiffener · cracked · Jun 8, 2022 · N286UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:3CAFT CARGO AT STA. 1841 RBL 36, VERTICAL STIFFNER IS CRACKED.REMOVED, FABRICATED AND REPLACED STIFFNER IAW DWG. AGA7170 AND SRM 51-33-01. (MINOR)
- [SDR IPXA2022062183323](https://openairdocs.org/sdr/IPXA2022062183323.md): Stiffener · cracked · Jun 8, 2022 · N286UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:3CAFT CARGO COMPARTMENT LH VERTICAL STIFFENER CRACK AT STA. 1841 LBL 36".REMOVED,FABRICATED AND REPLACED CRACKED STIFFENER IAW SRM 51-35-01 AND 51-33-01 (MINOR).
- [SDR IPXA2022062183329](https://openairdocs.org/sdr/IPXA2022062183329.md): Support Angle · cracked · Jun 8, 2022 · N286UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:3CFWD CARGO COMPARTMENT SLOPE PANEL SUPPORT ANGLE CRACK AT STA.6-80.REMOVED,FABRICATED AND REPLACED CRACKED SUPPORT ANGLE IAW SRM 51-31-01 AND 51-35-01 (MINOR).
- [SDR IPXA2022062183328](https://openairdocs.org/sdr/IPXA2022062183328.md): Support Angle · cracked · Jun 8, 2022 · N286UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:3CFWD CARGO COMPARTMENT SLOPE PANEL SUPPORT ANGLE CRACK AT STA. 979.REMOVED,FABRICATED AND REPLACED CRACKED SUPPORT ANGLE IAW SRM 51-31-01 AND 51-35-01 (MINOR).
- [SDR IPXA2022062183327](https://openairdocs.org/sdr/IPXA2022062183327.md): Support Angle · cracked · Jun 8, 2022 · N286UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:3CFWD CARGO COMPARTMENT SLOPE PANEL SUPPORT ANGLE CRACK AT STA.919.REMOVED,FABRICATED AND REPLACED CRACKED SUPPORT ANGLE IAW SRM 51-31-01 AND 51-35-01 (MINOR).
- [SDR IPXA2022062183326](https://openairdocs.org/sdr/IPXA2022062183326.md): Angle · cracked · Jun 8, 2022 · N286UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:3CFWD CARGO COMPARTMENT SLOPE PANEL SUPPORT ANGLE CRACK AT STA.839.REMOVED,FABRICATED AND REPLACED CRACKED SUPPORT ANGLE IAW SRM 51-31-01 AND 51-35-01 (MINOR).
- [SDR IPXA2022061783197](https://openairdocs.org/sdr/IPXA2022061783197.md): Angle · cracked · Jun 8, 2022 · N286UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:3CFWD. CARGO PANEL SUPPORT ANGLE IS CRACKED AT STA. 6-10 R/H SIDE.REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG. ADA0130 AND SRM 51-33-01. (MINOR)
- [SDR IPXA2022061783196](https://openairdocs.org/sdr/IPXA2022061783196.md): Angle · cracked · Jun 8, 2022 · N286UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:3CFWD. CARGO PANEL SUPPORT ANGLE IS CRACKED AT STA. 939 L/H SIDE.REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG. ADA0130 AND SRM 51-33-01. (MINOR)
- [SDR IPXA2022061783195](https://openairdocs.org/sdr/IPXA2022061783195.md): Angle · cracked · Jun 8, 2022 · N286UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:3CCENTER CARGO PANEL SUPPORT ANGLE IS CRACKED AT STA. 1681 L/H SIDE.REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG. ADA0130 AND SRM 51-33-01. (MINOR)
- [SDR IPXA2022061783194](https://openairdocs.org/sdr/IPXA2022061783194.md): Angle · cracked · Jun 8, 2022 · N286UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:3CFWD. CARGO COMP. PANEL SUPPORT ANGLE IS CRACKED AT STA. 1099 L/H SIDE.REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG. ADA0130 AND SRM 51-33-01. (MINOR)
- [SDR IPXA2022061783193](https://openairdocs.org/sdr/IPXA2022061783193.md): Angle · cracked · Jun 8, 2022 · N286UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:3CFWD. CARGO COMP. PANEL SUPPORT ANGLE IS CRACKED AT STA. 1119 R/H SIDE.REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG. ADA0130 AND SRM 51-33-001. (MINOR)
- [SDR IPXA2022061783192](https://openairdocs.org/sdr/IPXA2022061783192.md): Angle · cracked · Jun 8, 2022 · N286UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:3CFWD. CARGO PANEL SUPPORT ANGLE IS CRACKED AT STA. 859 L/H SIDE.REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG. ADA0130 AND SRM 51-33-01. (MINOR)
- [SDR IPXA2022070183678](https://openairdocs.org/sdr/IPXA2022070183678.md): Hinge · broken · Jun 7, 2022 · N286UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3CL/H WING LWR REAR SPAR FLAP HINGE SUPPORT TENSION STRAP FOUND CRACKED.REMOVED, FABRICTED AND REPLACED HINGE SUPPORT IAW VT-SAA EA 011-5753-01-A9613 REV I/R AND UPS EO MD11-5720-84043-A FAA FORM 8100-9 SIGNED BY S.KANG (AR-605677) DATED 06/28/
- [SDR IPXA2022062883591](https://openairdocs.org/sdr/IPXA2022062883591.md): Cap · corroded · Jun 7, 2022 · N286UP · Doug MD11F · Wing Main, Frame Structure
  > INSPECTION TYPE:3CR/H WING UPPER AFT CAP HAS CORROSION BETWEEN STA. XORS= 503 TO 519 AND XORS 571 TO 584.REPAIRED CORRODED R/H WING UPPER AFT CAP IAW VT-SAA EA 011-5710-01-A9617 REV. I/R AND UPS EO MD11-5710-84041-A. (MINOR)
- [SDR IPXA2022062883590](https://openairdocs.org/sdr/IPXA2022062883590.md): None · damaged · Jun 7, 2022 · N286UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3CR/H I/B FLAP LOWER SKIN IS DENTED AT STA. YIFH= 41 AND BETWEEN XIFH= 255.59 AND XIFH= 261.69.REPAIRED DAMAGED R/H IB FLAP LOWER SKIN AT STA. YIFH= 41 AND BETWEEN XIFH= 255.59 AND XIFH= 261.69 IAW VT-SAA EA 011-5753-01-A9611 REV. I/R AND UPS E

Next page: https://openairdocs.org/aircraft/N286UP/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 = 'N286UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N286UP/reports

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