# Service difficulty reports: N288UP

A list on [N288UP](https://openairdocs.org/aircraft/N288UP.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 6 · 300 reports

- [SDR IPXA2025081116757](https://openairdocs.org/sdr/IPXA2025081116757.md): Battery · no test · Aug 11, 2025 · N288UP · Doug MD11F · Emergency Lighting
  > PREFLIGHT DURING EMER LIGHT TEST HAD LEVEL 1 EMER LT BAT 1 LO ILLUMINATE R&RD EMERGENCY LIGHT POWER SUPPLY/ BATTERY AS REQ. OPS CK NORMAL REF. MM 33-51-01 OK FOR SVC PLACARD REMOVED DMP REVERSED
- [SDR IPXA2025080632499](https://openairdocs.org/sdr/IPXA2025080632499.md): Battery · inoperative · Aug 6, 2025 · N288UP · Doug MD11F · Emergency Lighting
  > EMERGENCY LIGHT BATTERY 1 LOW. REVERSED DMP 33-50-4 AS REQUIRED. REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY IAW A.M.M. 33-51-01-000-802/400-802. PERFORMED OPERATIONAL TEST AS PER TASK# 33-51-01-700-802 AND FOUND SATISFACTORY. THIS CLEARS DEFERRAL [T
- [SDR IPXA2025061169907](https://openairdocs.org/sdr/IPXA2025061169907.md): Power Supply · discharged · Jun 11, 2025 · N288UP · Doug MD11F · Emergency Lighting
  > EMER LT BAT 1 LO LEVEL 1 MESSAGE DURING PREFLIGHT OF EMERGENCY LIGHT SYSTEM REVERSED DMP. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY POWER SUPPLY IAW MD11 AMM 33-51-01. OPS CHECK GOOD, MESSAGE DID NOT REAPPEAR. THIS CLEARED MEL, PLACARD REMOVED.
- [SDR IPXA2025042864137](https://openairdocs.org/sdr/IPXA2025042864137.md): Splash Guard · missing · Apr 26, 2025 · N288UP · Doug MD11F · Emergency Equipment
  > CAPTAINS EVAS SLASH GUARD MISSING. INSTALLED CAPTAIN'S EVAS SPLASH GUARD PER AMM 25-69-00/601
- [SDR IPXA2025012821955](https://openairdocs.org/sdr/IPXA2025012821955.md): Battery · no test · Jan 28, 2025 · N288UP · Doug MD11F · Emergency Lighting
  > EMERGENCY LIGHTING TEST FAILED. BATTERY LOW. REPLACED EMERGENCY LIGHTING PWR SUPPLY BATTER I.A.W 33-51-01/401. CHECK SERVICEABLE PER AMM 33-51-01/501
- [SDR IPXA2024101598714](https://openairdocs.org/sdr/IPXA2024101598714.md): Skin · damaged · Oct 12, 2024 · N288UP · Doug MD11F · Leading Edge Devices
  > HOLE FOUND IN #8 RH SLAT REPLACED RH #8 SLAT REF AMM 27-80-30, RIG CHECK/ OPS CHECK GOOD.
- [SDR IPXA2024072240401](https://openairdocs.org/sdr/IPXA2024072240401.md): Pulley · damaged · Jul 22, 2024 · N288UP · Doug MD11F · Service Doors
  > R1 ENTRY DOOR, UPPER FWD TRACK DRIVE CABLE PULLEY DAMAGED. INSTALLED NEW CABLE PULLEY AND SECURED, OPERATIONAL CHECK GOOD REF MM 52-11-02.
- [SDR IPXA2025030486339](https://openairdocs.org/sdr/IPXA2025030486339.md): Beam · cracked · Jan 11, 2024 · N288UP · Doug MD11F · Fuselage Main, Structure
  > L3 DOOR UPPER HORIZONTAL BEAM AFT SIDE IS CRACKED (114-09) INSTALLED REPLACED BEAM AND REINSTALLED DOOR FRAME ASSEMBLY AT L-3 DOOR UPPER PER MD-11 SRM 51-35-01 & 51-31-01. REINSTALLED SEAL AT L-3 DOOR UPPER PER MD-11 AMM 52-00-00-400-801. APPLIED TOP COAT UPPE
- [SDR IPXA2024031694621](https://openairdocs.org/sdr/IPXA2024031694621.md): Tank · cracked · Jan 11, 2024 · N288UP · Doug MD11F · Standard Practices/Structures
  > UPPER CENTER AUX TANK HAS CRACKED FITTING LOCATED BETWEEN STA X-46 AND X-17, FRONT SPAR INTERNAL AREA. (015-111) LOCATED, DRILLED AND INSTALLED FITTING AT UPPER CTR AUX TANK BEETWEEN STA X-46 AND X-17 FRONT SPAR PER REF MD-11 SRM 51-31-01/51-33-01.
- [SDR IPXA2024022794685](https://openairdocs.org/sdr/IPXA2024022794685.md): Fuel Line · cracked · Jan 11, 2024 · N288UP · Doug MD11F · Aircraft Fuel Distribution System
  > UPPER CENTER AUX TANK. REAR SPAR AREA HAS CRACKED FUEL TUBE LOCATED BETWEEN STA X-17 AND X17. (015-112) INSTALLED ELBOW ASSY IAW UPS MD11 AMM 28-11-00-00-000-801 FFCSTAN2588. FUEL LINE INSTALLED IAW UPS MD11 AMM 28-00-00-000-801 INSTALL
- [SDR IPXA2024021686077](https://openairdocs.org/sdr/IPXA2024021686077.md): Door Frame · damaged · Jan 11, 2024 · N288UP · Doug MD11F · Fuselage Main, Structure
  > MAIN CABIN DOOR AFT FRAME IS GOUGED (114-11) MATERIAL LOSS PER NDT READING IS.003" MAX ALLOWED IS.013" AREA FOUND TO BE WITHIN LIMITS REF M11 SRM 52-00-00-2R-0 TREATED AND PRIMED REF MD11 SRM 51-21-01. TOPCOATED PAINT AREA REF MD11 SRM 51-21-02
- [SDR IPXA2024020886027](https://openairdocs.org/sdr/IPXA2024020886027.md): Door Frame · gouged · Jan 11, 2024 · N288UP · Doug MD11F · Fuselage Main, Structure
  > MAIN CABIN DOOR FWD FRAME IS GOUGED (114-10). BLENDED OUT DAMAGED AREA AT MAIN CARGO DOOR FWR FREME REF MD11 SRM 52-00-00-2R-0. MATERIAL LOSS PER NDT READING IS.006" MAX ALLOWED IS.013"AREA FAUND TO BE WITHIN LIMITSREF SRM 52-00-00-2R-0 TREATED AND PRIMER AR
- [SDR IPXA2024011294621](https://openairdocs.org/sdr/IPXA2024011294621.md): Unknown · unknown · Jan 11, 2024 · N288UP · Doug MD11F · Fuel Storage
  > *SDR FILED OPEN* STR- UPPER CENTER AUX TANK HAS CRACKED FITTING LOCATED BETWEEN STA X-46 AND X-17, FRONT SPAR INTERNAL AREA. (015-111) REQUEST NDT CHECK FOR CRACKS
- [SDR IPXA2024011294685](https://openairdocs.org/sdr/IPXA2024011294685.md): Unknown · unknown · Jan 11, 2024 · N288UP · Doug MD11F · Fuel Storage
  > *SDR FILED OPEN* FUEL- UPPER CENTER AUX TANK. REAR SPAR AREA HAS CRACKED FUEL TUBE LOCATED BETWEEN STA X-17 AND X17. (015-112)
- [SDR IPXA2024011286339](https://openairdocs.org/sdr/IPXA2024011286339.md): Unknown · unknown · Jan 11, 2024 · N288UP · Doug MD11F · Fuselage Main, Structure
  > *SDR FILED OPEN* STR - L3 DOOR UPPER HORIZONTAL BEAM AFT SIDE IS CRACKED (114-09) OK TO WORK
- [SDR IPXA2024011186027](https://openairdocs.org/sdr/IPXA2024011186027.md): Unknown · unknown · Jan 11, 2024 · N288UP · Doug MD11F · Fuselage Main, Structure
  > MAIN CABIN DOOR FWD FRAME IS GOUGED (114-10) OK TO WORK
- [SDR IPXA2024011186077](https://openairdocs.org/sdr/IPXA2024011186077.md): Unknown · unknown · Jan 11, 2024 · N288UP · Doug MD11F · Fuselage Main, Structure
  > MAIN CABIN DOOR AFT FRAME IS GOUGED (114-11) OK TO WORK
- [SDR IPXA2025030468783](https://openairdocs.org/sdr/IPXA2025030468783.md): Floor Panel · dented · Jan 10, 2024 · N288UP · Doug MD11F · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 187 GF HAS MULTIPLE DENTS IN SEVERAL AREAS..MARKED 84-38..OFF AC PART FABRICATED FLOOR PANEL PER SREO-34874-REQ001.
- [SDR IPXA2025030468698](https://openairdocs.org/sdr/IPXA2025030468698.md): Floor Panel · dented · Jan 10, 2024 · N288UP · Doug MD11F · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 187GF HAS MULTIPLE DENTS IN SEVERAL AREAS..MARKED 84-37.<BR>.OFF AC PART FABRICATED FLOOR PANEL PER SREO-34874-REQ001.
- [SDR IPXA2025030468536](https://openairdocs.org/sdr/IPXA2025030468536.md): Floor Panel · dented · Jan 10, 2024 · N288UP · Doug MD11F · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 187AF MULTIPLE DENTS AND PUNTURES..MARKED 84-36 OFF AC PART FABRICATED FLOOR PANEL PER SREO-34874-REQ001.
- [SDR IPXA2025030469862](https://openairdocs.org/sdr/IPXA2025030469862.md): Tail Cone · damaged · Jan 10, 2024 · N288UP · Doug MD11F · Aerodynamic Fairings
  > TAIL CONE R/H FWD UPPER PRODUCTION DOUBLER IS DAMAGED. FABRICATED REPAIR FILLER, AND TREATED AND PRIMED IAW SREO-66790-REQ002 REV 1 OK TO INSTALL REPAIR FILLER. WORK ACCOMPLISHED ON SREO-66790-REQ002 REV1, T3F18E003QKC3, LINE 1307.
- [SDR IPXA2024032073868](https://openairdocs.org/sdr/IPXA2024032073868.md): Frame · cracked · Jan 10, 2024 · N288UP · Doug MD11F · Nacelle/Pylon, Main Frame
  > NR 1 PYLON PRE-COOLER AERA STRUCTURE ANGLE FRAME HAS MULTIPLE CRACKED. 74-095 LOCATED DRILLED AND INSTALLED ANGLE AT #1 PYLON PRE-COOLER AREA PER REF MD-11 SRM 51-31-01-OG-0 AND 54-05-41-OG-0.
- [SDR IPXA2024021663315](https://openairdocs.org/sdr/IPXA2024021663315.md): Bulkhead · corroded · Jan 10, 2024 · N288UP · Doug MD11F · Fuselage Main, Structure
  > AFT CARGO COMP. STEP UP BULKHEAD UPPER FLANGE LOCATED AT STA 1841 HAS CORROSION AND MISSING NUTPLATES. (015-103) REMOVED NUT PLATES AND REMOVED LITE SURFACE CORROSION AT STR AFT CARGO COMP.STEP UP BULKHEAD UPPER FLANGE LOCATED AT STA 1841 REF MD11 SRM 51-35-01
- [SDR IPXA2024021663711](https://openairdocs.org/sdr/IPXA2024021663711.md): Channel · broken · Jan 10, 2024 · N288UP · Doug MD11F · Fuselage Miscellaneous Structure
  > CENTER CARGO COMP. CEILING AREA HAS BROKEN HAT CHANNEL LOCATED AT STA 1730/RBL46. (015-107) INSTALLED HAT CHANNEL SECTION ON CENTER CARGO COMP. CEILING AREA STA 1701- STA 1741 RBL 46 IN REF MD11 SRM 51-35-01. APPLIED TOP COAT PROTECTION ON HAT CHANNEL SECTION
- [SDR IPXA2024021663860](https://openairdocs.org/sdr/IPXA2024021663860.md): Channel · unknown · Jan 10, 2024 · N288UP · Doug MD11F · Fuselage Miscellaneous Structure
  > CENTER CARGO COMP. CEILING AREA HAS BROKEN HAT CHANNEL LOCATED AT STA 1701/RBL46. (015-108) CENTER CARGO COMP. CEILING AREA HAT CHANNEL LOCATED AT STA 1701 RBL 46 BEING REPLACED ON LINE # 1193, NO FURTHER ACTION REQUIRED ON THIS FAULT
- [SDR IPXA2024021663607](https://openairdocs.org/sdr/IPXA2024021663607.md): Channel · broken · Jan 10, 2024 · N288UP · Doug MD11F · Fuselage Miscellaneous Structure
  > CENTER CARGO COMP. CEILING AREA HAS BROKEN HAT CHANNEL LOCATED AT STA 1721/RBL78. (015-106) INSTALLED NEW HAT CHANNEL AT CENTER CARGO COMP. CEILING AREA AT STA 1721/RBL78 IAW DWG #AFA7991 AND SRM 51-35-01.
- [SDR IPXA2024021663527](https://openairdocs.org/sdr/IPXA2024021663527.md): Channel · deformed · Jan 10, 2024 · N288UP · Doug MD11F · Fuselage Miscellaneous Structure
  > CENTER CARGO COMP. CEILING AREA HAS DEFORMED HAT CHANNEL LOCATED AT STA 1661/RBL78. (015-105) APPLIED PRIMER, TOPCOAT, AND INSTALLED NEW HAT CHANNEL AT CENTR CARGO COMP. CEILING AREA, STA 1661/RBL78 IAW DWG # AFA7991, SRM 51-35-01, AND AMM 51-21-00
- [SDR IPXA2024021663181](https://openairdocs.org/sdr/IPXA2024021663181.md): Cargo Track · damaged · Jan 10, 2024 · N288UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO COMP. SEAT TRACK ANGLES LOCATED APPROX STA 1941/RBL20 HAS MISSING FASTENERS. (015-102) INSTALLED MISING FASTENER AT STR AFT CARGO COMP SEAT TRACK ANGLESLOCATED APPROX STA 1941RBL 20 R/H REF MD11 SRM 51-35-01
- [SDR IPXA2024011163711](https://openairdocs.org/sdr/IPXA2024011163711.md): Unknown · unknown · Jan 10, 2024 · N288UP · Doug MD11F · Fuselage Miscellaneous Structure
  > CENTER CARGO COMP. CEILING AREA HAS BROKEN HAT CHANNEL LOCATED AT STA 1730/RBL46. (015-107) OK TO WORK
- [SDR IPXA2024011168783](https://openairdocs.org/sdr/IPXA2024011168783.md): Unknown · unknown · Jan 10, 2024 · N288UP · Doug MD11F · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 187 GF HAS MULTIPLE DENTS IN SEVERAL AREAS..MARKED 84-38..OFF AC PART APPROVED
- [SDR IPXA2024011163860](https://openairdocs.org/sdr/IPXA2024011163860.md): Unknown · unknown · Jan 10, 2024 · N288UP · Doug MD11F · Fuselage Miscellaneous Structure
  > CENTER CARGO COMP. CEILING AREA HAS BROKEN HAT CHANNEL LOCATED AT STA 1701/RBL46. (015-108) OK TO WORK.
- [SDR IPXA2024011168698](https://openairdocs.org/sdr/IPXA2024011168698.md): Unknown · unknown · Jan 10, 2024 · N288UP · Doug MD11F · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 187GF HAS MULTIPLE DENTS IN SEVERAL AREAS..MARKED 84-37.<BR>.OFF AC PART APPROVED
- [SDR IPXA2024011168536](https://openairdocs.org/sdr/IPXA2024011168536.md): Unknown · unknown · Jan 10, 2024 · N288UP · Doug MD11F · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 187AF MULTIPLE DENTS AND PUNTURES..MARKED 84-36 OFF AC PART APPROVED
- [SDR IPXA2024011163527](https://openairdocs.org/sdr/IPXA2024011163527.md): Unknown · unknown · Jan 10, 2024 · N288UP · Doug MD11F · Fuselage Miscellaneous Structure
  > *SDR FILED OPEN* STR- CENTER CARGO COMP. CEILING AREA HAS DEFORMED HAT CHANNEL LOCATED AT STA 1661/RBL78. (015-105) OK TO WORK
- [SDR IPXA2024011163607](https://openairdocs.org/sdr/IPXA2024011163607.md): Unknown · unknown · Jan 10, 2024 · N288UP · Doug MD11F · Fuselage Miscellaneous Structure
  > CENTER CARGO COMP. CEILING AREA HAS BROKEN HAT CHANNEL LOCATED AT STA 1721/RBL78. (015-106) APPROVED
- [SDR IPXA2024011169862](https://openairdocs.org/sdr/IPXA2024011169862.md): Unknown · unknown · Jan 10, 2024 · N288UP · Doug MD11F · Aerodynamic Fairings
  > TAIL CONE R/H FWD UPPER PRODUCTION DOUBLER IS DAMAGED. OK TO WORK
- [SDR IPXA2024011163181](https://openairdocs.org/sdr/IPXA2024011163181.md): Seat Track · unknown · Jan 10, 2024 · N288UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO COMP. SEAT TRACK ANGLES LOCATED APPROX STA 1941/RBL20 HAS MISSING FASTENERS. (015-102) APPROVED
- [SDR IPXA2024011163315](https://openairdocs.org/sdr/IPXA2024011163315.md): Unknown · unknown · Jan 10, 2024 · N288UP · Doug MD11F · Fuselage Main, Structure
  > *SDR FILED OPEN* STR- AFT CARGO COMP. STEP UP BULKHEAD UPPER FLANGE LOCATED AT STA 1841 HAS CORROSION AND MISSING NUTPLATES. (015-103) APPROVED
- [SDR IPXA2024011173868](https://openairdocs.org/sdr/IPXA2024011173868.md): Unknown · unknown · Jan 10, 2024 · N288UP · Doug MD11F · Nacelle/Pylon Structure
  > NR 1 PYLON PRE-COOLER AERA STRUCTURE ANGLE FRAME HAS MULTIPLE CRACKED. 74-095 OK TO WORK
- [SDR IPXA2024032049912](https://openairdocs.org/sdr/IPXA2024032049912.md): Fairing · cracked · Jan 9, 2024 · N288UP · Doug MD11F · Aerodynamic Fairings
  > RH BODY FAIRING UPR AREA STA 1341 STRUCTURAL FRAME HAS CRACKED. 74-089 TREATED AND PRIMED REPAIR PARTS IAW MD11 SRM 51-21-01-OG-0 PARA 26-33. REINSTALLED RIB ON R\H BODY FAIRING UPR AERA STA 1341 IAW MD11 SRM 51-35-01-OG-0
- [SDR IPXA2024032049265](https://openairdocs.org/sdr/IPXA2024032049265.md): Fairing · cracked · Jan 9, 2024 · N288UP · Doug MD11F · Aerodynamic Fairings
  > LH BODY FAIRING AREA UPR SIDE STA 1341 FRAME STRUCTURE HAS CRACKED. 74-079 TREATED AND PRIMED REPAIR PARTS I.A.W MD-11 SRM 51-21-01-0G-0 PAR 26 AND 33. RE INSTALLED L/H BODY PNL SUPPORT RIB AT STA 1341 I.A.W MD-11 SRM 51-35-01-0G-0
- [SDR IPXA2024022753081](https://openairdocs.org/sdr/IPXA2024022753081.md): Insert · damaged · Jan 9, 2024 · N288UP · Doug MD11F · Fuselage Floor Panel
  > *** SUPPLEMENTAL SDR *** INT - MAIN CABIN FLOOR PANEL #271GF HAS A DAMAGED INSERT (114-06) REMOVED AND REPLACED (1EA) INSERT ON FLOOR PANEL 271GF AT MAIN CABIN IAW MD-11 SRM 53-00-50-2R-1 REPAIR 1.
- [SDR IPXA2024022753067](https://openairdocs.org/sdr/IPXA2024022753067.md): Insert · damaged · Jan 9, 2024 · N288UP · Doug MD11F · Fuselage Floor Panel
  > *** SUPPLEMENTAL SDR *** INT - MAIN CABIN FLOOR PANEL #263QF HAS A DAMAGED INSERT (114-05) REMOVED AND REPLACED (1EA) INSERT ON FLOOR PANEL 263QF AT MAIN CABIN IAW MD-11 SRM 53-00-50-2R-1 REPAIR 1.
- [SDR IPXA2024021649236](https://openairdocs.org/sdr/IPXA2024021649236.md): Frame · cracked · Jan 9, 2024 · N288UP · Doug MD11F · Fuselage Main, Frame
  > *** SUPPLEMENTAL SDR *** (STR) LH BODY FAIRING AREA UPR SIDE STA 1361 FRAME STRUCTURE HAS CRACKED. 74-078 LOCATED AND DRILLED REPLACEMENT ANGLE REF.MD-11 SRM 51-31-01-OG-0, AND INSTALLED AT L/H BODY FAIRING AREA UPR SIDE STA. 1361 REF.MD-11 SRM 51-35-01-OG-0
- [SDR IPXA2024020952990](https://openairdocs.org/sdr/IPXA2024020952990.md): Skin · corroded · Jan 9, 2024 · N288UP · Doug MD11F · Fuselage Main, Plate/Skin
  > MAIN CABIN CTR WING BOX R/H SIDE SURFACE HAS CORROSION AT STRINGER 15 AND 27.5 INCH FROM CL. (114-02) ORIGINAL MATERIAL THICKNESS OF CENTER WING UPPER FWD & CENTER SKIN AT BLENDED SMOOTH AREAS BETWEEN STA X=-27 & X=-31 ABOVE STRG 15 LOCATION IS 0.159" THICK I.
- [SDR IPXA2024021653083](https://openairdocs.org/sdr/IPXA2024021653083.md): Floor Panel · damaged · Jan 9, 2024 · N288UP · Doug MD11F · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL #272JF HAS COMP-DAMAGED (114-07) REMOVED DAMAGE SKIN ON MAIN CABIN FLOOR PANEL 272JF. IAW MD-11 SRM 53-00-50-2R-2. REPAIR 2. APPLIED REPAIR FILLER ON MAIN CABIN FLOOR PANEL 272J, USING POTTING COMPOUND P/N:EC3524A/B, B/N:0004177973. CURE
- [SDR IPXA2024021653031](https://openairdocs.org/sdr/IPXA2024021653031.md): Floor Panel · damaged · Jan 9, 2024 · N288UP · Doug MD11F · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL #262BF HAS A DAMAGED INSERT (114-04) REMOVED AND REPLACED (1EA) INSERT ON FLOOR PANEL 262BF AT MAIN CABIN IAW MD-11 SRM 53-00-50-2R-1 REPAIR 1
- [SDR IPXA2024021653005](https://openairdocs.org/sdr/IPXA2024021653005.md): Floor Panel · damaged · Jan 9, 2024 · N288UP · Doug MD11F · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL #262CF HAS A DAMAGED INSERT. (114-03) REMOVED AND REPLACED (1EA) INSERT ON FLOOR PANEL 262CF AT MAIN CABIN IAW MD-11 SRM 53-00-50-2R-1 REPAIR 1
- [SDR IPXA2024020952961](https://openairdocs.org/sdr/IPXA2024020952961.md): Skin · corroded · Jan 9, 2024 · N288UP · Doug MD11F · Fuselage Main, Plate/Skin
  > MAIN CABIN CTR WING BOX R/H SIDE SURFACE HAS CORROSION AT STRINGER 15 BETWEEN STA 1219-1239 (114-01) ACCOMPLISHED EA 011-5730-01-B0145 I/R AND EO-89278-REQ1 ATTACHED TO FAULT T3F18E003Q6BG
- [SDR IPXA2024011053031](https://openairdocs.org/sdr/IPXA2024011053031.md): Unknown · unknown · Jan 9, 2024 · N288UP · Doug MD11F · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL #262BF HAS A DAMAGED INSERT (114-04) APPROVED

Next page: https://openairdocs.org/aircraft/N288UP/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 = 'N288UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N288UP/reports

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