# Service difficulty reports: N159UP

A list on [N159UP](https://openairdocs.org/aircraft/N159UP.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 5 · 202 reports

- [SDR IPXA2026082163543](https://openairdocs.org/sdr/IPXA2026082163543.md): Bulb · burned out · Aug 21, 2026 · N159UP · Airbus A300F4622R · Passenger Compartment Lighting
  > LAV AUX LIGHT INOPERATIVE. REPLACED LAV AUX LIGHT BULB IAW AMM 33-51-21, OPS CHECKED GOOD.
- [SDR IPXA2026071688814](https://openairdocs.org/sdr/IPXA2026071688814.md): Lock · stuck · Jul 16, 2026 · N159UP · Airbus A300F4622R · Passenger/Crew Doors
  > MAIN CABIN DOOR LOCK RELEASE PUSH BUTTON STUCK IN DOWN POSITION. DOOR WILL NOT STAY OPEN LOCKED POSITION. PUSHED STUCK DOOR LOCK RELEASE BUTTON. BUTTON RELEASED PROPERLY AS ADVERTISED. PERFORMED PROPER DOOR OPERATION PER AMM 52-00-00/001. DOOR STAYS OPEN AND L
- [SDR IPXA2026042766665](https://openairdocs.org/sdr/IPXA2026042766665.md): Light · inoperative · Apr 24, 2026 · N159UP · Airbus A300F4622R · Emergency Lighting
  > LAVATORY EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LAVATORY AUX EMERGENCY LIGHT ASSY IAW AMM 33-51-21/401. OPS CHECK GOOD.
- [SDR IPXA2026031113413](https://openairdocs.org/sdr/IPXA2026031113413.md): Windshield Wiper · malfunctioned · Mar 10, 2026 · N159UP · Airbus A300F4622R · Windshield/Door Rain/Ice Removal
  > AIR TURN BACK, UNCOMMANDED WINDSHIELD WIPE OPERATION WITH SWITCH OFF ON CLIMB OUT EXCEEDED 230KT LIMITATION. MAX SPEED REACHED. 250 KTS. WIPER OPERATED ON DRY WINDSHIELD FOR APPROX 15 MINUTES. THIS RESULTED IN R/R 25DB PER TSM 30-45-00/101 AND ESPM 20-46-50. O
- [SDR IPXA2025120229938](https://openairdocs.org/sdr/IPXA2025120229938.md): Slide · obstructed · Dec 2, 2025 · N159UP · Airbus A300F4622R · Escape Slide
  > ON GROUND WHILE SECURING FOR FLIGHT, MAIN ENTRY DOOR SLIDE WOULD NOT ARM - LEVER WOULD NOT MOVE TO THE ARMED POSITION. UPON TROUBLESHOOTING INSPECTED L1 & MCD SEALS. NO FAULTS FOUND AT THIS TIME. FOUND L1 DOOR SLIDE EJECTOR BAG RELEASE CABLE/ QUICK DISCONNECT
- [SDR IPXA2025072139249](https://openairdocs.org/sdr/IPXA2025072139249.md): Bottle · discharged · Jul 21, 2025 · N159UP · Airbus A300F4622R · Passenger/Crew Doors
  > L-1 DOOR EMERGENCY OPERATING CYLINDER INADVERTENTLY DISCHARGED REPLACED DIAPHRAGM, SEALS, SHEAR PIN, AND SERVICED DOOR DAMPER CYLINDER - OPS CHECKS GOOD AT THIS TIME. SAFETY PIN REMOVED IAW MM 52-10-14/301
- [SDR IPXA2025052809506](https://openairdocs.org/sdr/IPXA2025052809506.md): Slide · malfunctioned · May 28, 2025 · N159UP · Airbus A300F4622R · Escape Slide
  > DOOR SLIDE ONLY DISARMS WITH EXTREME FORCE LUBRICATED GIRT BAR AND SEVERAL OTHER MECHANISMS IN THE SYSTEM REF AMM 52-10-30/601 OPS CHECKS GOOD
- [SDR IPXA2025031447289](https://openairdocs.org/sdr/IPXA2025031447289.md): Unknown · noise · Mar 14, 2025 · N159UP · Airbus A300F4622R · Cargo/Baggage Doors
  > VERY HIGH PITCH NOISE FROM MAIN CABIN DECK CARGO DOOR OR CREW ENTRY DOOR AREA. CABIN PRESSURE AND CABIN ALTITUDE WERE ALL NORMAL (DIFF 8.0 V/S 0, CABIN ALTITUDE 5 AT FL 320). ALL ECAM DOOR INDICATIONS PRESSURIZED A/C PER AMM 05-51-00/001. NO NOISE FROM CREW EN
- [SDR IPXA2025020608461](https://openairdocs.org/sdr/IPXA2025020608461.md): Switch · worn · Feb 6, 2025 · N159UP · Airbus A300F4622R · Door Warning System
  > IMMEDIATELY AFTER TAKEOFF "FORWARD CARGO DOOR NOT CLOSED" AND "CHECK 0001 TIMES" WHICH LED US TO COMPLETE AN AIR TURN BACK AS AIRCRAFT DIDNT SEEM TO BE PRESSURIZING. REMOVED & REPLACED DOOR WARNING SWITCH 14WS PER AMM 52-71-00/401. OPS CHECK GOOD. ADJUSTMENT
- [SDR IPXA2024090969718](https://openairdocs.org/sdr/IPXA2024090969718.md): Handle · binding · Sep 7, 2024 · N159UP · Airbus A300F4622R · Passenger/Crew Doors
  > AFTER BLOCK IN, CREW WAS UNABLE TO DISARM THE ESCAPE SLIDE. DISARM HANDLE MOVES 3/4 WAY, BUT WILL BOT FULLY DISARM. INSPECTED PASSENGER CREW ENTRY DOOR JAWS SLIDERS AND GIRT BAR TOLERANCES IAW AMM 52-10-30/601. ALL ARE WITHIN TOLERENCES. CLEANED ALL MECHANICAL
- [SDR IPXA2024072956769](https://openairdocs.org/sdr/IPXA2024072956769.md): Girt Bar · fod · Jul 29, 2024 · N159UP · Airbus A300F4622R · Emergency Equipment
  > DIFFICULTY DISARMING SLIDE. LEVER WAS CATCHING ON SOMETHING. REMOVED DEBRIS FROM GIRT BAR FITTINGS AND CLEANED AS REQUIRED. SLIDE ARMING LEVER OPS CHECKS GOOD. REF AMM 52-10-11
- [SDR IPXA202407096961](https://openairdocs.org/sdr/IPXA202407096961.md): Latch · out of adjust · Jun 28, 2024 · N159UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW ENTRY DOOR AFT LATCH INDICATION HALF RED HALF GREEN. MADE ADUSTMENT AND PERFORMED FUNCTIONAL TEST OF FWD PASSENGER/CREW DOOR IAW AMM 52-10-11. OPS CHECK GOOD
- [SDR IPXA2024070106961](https://openairdocs.org/sdr/IPXA2024070106961.md): Latch · out of position · Jun 28, 2024 · N159UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW ENTRY DOOR AFT LATCH INDICATION HALF RED HALF GREEN. OPEN
- [SDR IPXA2024062384287](https://openairdocs.org/sdr/IPXA2024062384287.md): Skin · cracked · May 28, 2024 · N159UP · Airbus A300F4622R · Wing, Plate/Skin
  > RT WING, UPPER SURFACE, APPROX RIB 18, HAVE A CRACK ON SKIN. DOT 103-199 INSTALLED REPAIR AS REQUIRED IAW SRM 57-51-12 PARA G FIG 207 RIVETS INSTALLED.
- [SDR IPXA2024062623455](https://openairdocs.org/sdr/IPXA2024062623455.md): Frame · damaged · May 11, 2024 · N159UP · Airbus A300F4622R · Fuselage Main, Frame
  > LEFT FR47 HOLE IS REAMED TO A SIZE OF.610" WITH NO DAMAGE INDICATIONS. ACCOMPLISH THE REPAIR PER EO-90513-REQ1 AND EA 300-5710-27-A3600 REV. -.
- [SDR IPXA2024062601474](https://openairdocs.org/sdr/IPXA2024062601474.md): Panel · damaged · May 3, 2024 · N159UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > PANEL 131GE HAS DAMAGED EDGE SEAL. REPAIRED DAMAGE EDGE SEAL IN PANEL 131GE, I.A.W. EO NO.: A300-5320-42722-F. PANEL #131GE, WAS REPAIRED IAW EO A300-5320-42722-F. NO FURTHER ACTON REQUIRED.
- [SDR IPXA2024062404353](https://openairdocs.org/sdr/IPXA2024062404353.md): Panel · torn · May 3, 2024 · N159UP · Airbus A300F4622R · Fuselage Structure (General)
  > PANEL 132SG HAS TORN FIBERGLASS AND EDGE DAMAGE. REPAIRED FIBERGLASS BREAKS AND EDGE DAMAGE IAW EO NO: A300-5320-42722-F.
- [SDR IPXA2024062404288](https://openairdocs.org/sdr/IPXA2024062404288.md): Panel · torn · May 3, 2024 · N159UP · Airbus A300F4622R · Fuselage Structure (General)
  > PANEL 152QF HAS TORN FIBERGLASS AND DELAMINATED. REPAIRED TORN FIBERGLASS AND DELAMINATION OF PANEL 152QF, I.A.W. EO. A300-5320-42722-F.
- [SDR IPXA2024062404413](https://openairdocs.org/sdr/IPXA2024062404413.md): Floor Panel · damaged · May 3, 2024 · N159UP · Airbus A300F4622R · Fuselage Floor Panel
  > **SUPPLEMENTAL SDR** FAULT: PANEL 132G HAS FIBERGLASS DAMAGE AND EDGE DAMAGE. DOT 109/080. REPAIRED FIBERGLASS TORN AND EDGE DAMAGE IN PANEL 132 QG, IAW (SREO) EO NO: A300-5320-42722-F. REVIEWED
- [SDR IPXA2024062104353](https://openairdocs.org/sdr/IPXA2024062104353.md): Panel · damaged · May 3, 2024 · N159UP · Airbus A300F4622R · Fuselage Structure (General)
  > PANEL 132SG HAS TORN FIBERGLASS AND EDGE DAMAGE. DOT 109/078. REPAIRED FIBERGLASS BREAKS AND EDGE DAMAGE IAW EO NO: A300-5320-42722-F. MAJOR REPAIR
- [SDR IPXA2024062104288](https://openairdocs.org/sdr/IPXA2024062104288.md): Panel · damaged · May 3, 2024 · N159UP · Airbus A300F4622R · Fuselage Structure (General)
  > PANEL 152QF HAS TORN FIBERGLASS AND DELAMINATED. DOT 109/075. REPAIRED TORN FIBERGLASS AND DELAMINATION OF PANEL 152QF, I.A.W. EO. A300-5320-42722-F. MAJOR REPAIR
- [SDR IPXA2024062104413](https://openairdocs.org/sdr/IPXA2024062104413.md): Panel · damaged · May 3, 2024 · N159UP · Airbus A300F4622R · Fuselage Structure (General)
  > PANEL 132G HAS FIBERGLASS DAMAGE AND EDGE DAMAGE. DOT 109/080. REPAIRED FIBERGLASS TORN AND EDGE DAMAGE IN PANEL 132 QG, IAW (SREO) EO NO: A300-5320-42722-F. MAJOR REPAIR
- [SDR IPXA2024061489771](https://openairdocs.org/sdr/IPXA2024061489771.md): Floor Panel · delaminated · May 2, 2024 · N159UP · Airbus A300F4622R · Fuselage Floor Panel
  > FLOOR PANEL 143DF SOAKED AND DELAMINATE. FABRICATED FWD CARGO FLOOR PANEL 143DF IAW A300-5320-40552. JOB COMPLETE. REVIEWED
- [SDR IPXA2024052092058](https://openairdocs.org/sdr/IPXA2024052092058.md): Skin · cracked · Apr 26, 2024 · N159UP · Airbus A300F4622R · Trailing Edge Flaps
  > THE L/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 26, AFT SIDE. AREA MARKED IN RED. ACCOMPLISH CATEGORY A PERMANENT REPAIR PER EO-90269-REQ1 AND EA 300-5750-27-A3581 REV.
- [SDR IPXA2024052092103](https://openairdocs.org/sdr/IPXA2024052092103.md): Skin · cracked · Apr 26, 2024 · N159UP · Airbus A300F4622R · Trailing Edge Flaps
  > THE L/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 27, AFT SIDE. AREA MARKED IN RED. ACCOMPLISH CATEGORY A PERMANENT REPAIR PER EO-90269-REQ1 AND EA 300-5750-27-A3581 REV.
- [SDR IPXA2024052075373](https://openairdocs.org/sdr/IPXA2024052075373.md): Skin · cracked · Apr 25, 2024 · N159UP · Airbus A300F4622R · Trailing Edge Flaps
  > THE R/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 18 AFT SIDE. AREA MARKED IN RED. ACCOMPLISH CATEGORY A PERMANENT REPAIR PER EO-90290-REQ1 AND EA 300-5750-27-A3580 REV -.
- [SDR IPXA2024052075328](https://openairdocs.org/sdr/IPXA2024052075328.md): Skin · cracked · Apr 25, 2024 · N159UP · Airbus A300F4622R · Trailing Edge Flaps
  > THE R/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 13 AFT SIDE. AREA MARKED IN RED. ACCOMPLISH CATEGORY A PERMANENT REPAIR PER EO-90290-REQ1 AND EA 300-5750-27-A3580 REV -. MAJOR REPAIR.
- [SDR IPXA2024052075065](https://openairdocs.org/sdr/IPXA2024052075065.md): Skin · cracked · Apr 25, 2024 · N159UP · Airbus A300F4622R · Trailing Edge Flaps
  > THE R/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 12 AFT SIDE. AREA MARKED IN RED. ACCOMPLISH CATEGORY A PERMANENT REPAIR PER EO-90290-REQ1 AND EA 300-5750-27-A3580 REV.
- [SDR IPXA2024052075380](https://openairdocs.org/sdr/IPXA2024052075380.md): Skin · cracked · Apr 25, 2024 · N159UP · Airbus A300F4622R · Trailing Edge Flaps
  > THE R/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 19 AFT SIDE. AREA MARKED IN RED. ACCOMPLISH CATEGORY A PERMANENT REPAIR PER EO-90290-REQ1 AND EA 300-5750-27-A3580 REV.
- [SDR IPXA2024052075365](https://openairdocs.org/sdr/IPXA2024052075365.md): Skin · cracked · Apr 25, 2024 · N159UP · Airbus A300F4622R · Trailing Edge Flaps
  > THE R/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 17 AFT SIDE. AREA MARKED IN RED. ACCOMPLISH CATEGORY A PERMANENT REPAIR PER EO-90290-REQ1 AND EA 300-5750-27-A3580 REV.
- [SDR IPXA2024052075478](https://openairdocs.org/sdr/IPXA2024052075478.md): Doubler · cracked · Apr 25, 2024 · N159UP · Airbus A300F4622R · Trailing Edge Flaps
  > MAJOR REPAIR, THE R/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 11 AFT SIDE. AREA MARKED IN RED. INSTALLED NEW REPAIR FLANGE AND REINFORCEMENT REPAIR ANGLE I.A.W. A300-600 S.R.M. 51-40-21.
- [SDR IPXA2024052075469](https://openairdocs.org/sdr/IPXA2024052075469.md): Skin · cracked · Apr 25, 2024 · N159UP · Airbus A300F4622R · Trailing Edge Flaps
  > THE R/H CENTER FLAP ASSY HAS MULTIPLE CRACKS (2EA) AT RIB LOCATION 26 AFT & FWD SIDES. AREA MARKED IN RED. ACCOMPLISH CATEGORY A PERMANENT REPAIR PER EO-90290-REQ1 AND EA 300-5750-27-A3580 REV-.
- [SDR IPXA2024052075428](https://openairdocs.org/sdr/IPXA2024052075428.md): Skin · cracked · Apr 25, 2024 · N159UP · Airbus A300F4622R · Trailing Edge Flaps
  > THE RT CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 25 AFT SIDE. ACCOMPLISH CATEGORY A PERMANENT REPAIR PER EO-90290-REQ1 AND EA 300-5750-27-A3580 REV -.
- [SDR IPXA2024062546410](https://openairdocs.org/sdr/IPXA2024062546410.md): Inlet · cracked · Apr 24, 2024 · N159UP · Airbus A300F4622R · Engine Air Intake System
  > NR 2 ENGINE INLET COWL ANTI-ICE DUCT FLANGE IS CRACKED AT INLET COWL AFT BULKHEAD. INSTALLED INLET COWL ANTI-ICE DUCT IAW AMM 30-21-00-401.- PERFORMED LEAK TEST IAW AMM 71-00-00/501 NO LEAKS FOUND. DYE PENETRANT INSPECTION FOR THE NR 2 ENGINE INLET COWL WAS P
- [SDR IPXA2024061846640](https://openairdocs.org/sdr/IPXA2024061846640.md): Bulkhead Web · damaged · Apr 24, 2024 · N159UP · Airbus A300F4622R · Turbine Engine Accessory Drive
  > FAULT: #2 ENGINE INLET COWL AFT BULKHEAD IS DAMAGED AROUND I/B P-2 LINE. DOT 142-53. INSTALLED NEW WEB AND SPLICE. IAW A300-600 SRM 51-40-21. REVIEWED
- [SDR IPXA2024051859424](https://openairdocs.org/sdr/IPXA2024051859424.md): Floor Panel · broken · Apr 24, 2024 · N159UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 232WG IS BROKEN FABRICATE PNL FROM 5024N400001SS-G BACH #4055277 IAW SREO-40552-REQ001 C/W
- [SDR IPXA2024051859256](https://openairdocs.org/sdr/IPXA2024051859256.md): Floor Panel · broken · Apr 24, 2024 · N159UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 221CG IS BROKEN FABRICATED PNL 221CG FROM 5024N400001SS-G BACH # 4055277 IAW SREO-40552-REQ001 (APPX B) C/W.
- [SDR IPXA2024051759338](https://openairdocs.org/sdr/IPXA2024051759338.md): Floor Panel · broken · Apr 24, 2024 · N159UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 232LF IS BROKEN FABRICATED PANEL FROM 5024N400001SS-G, BATCH #4055277 IAW S.R.E.O A300-5320-40552-B C/W.
- [SDR IPXA2024053028466](https://openairdocs.org/sdr/IPXA2024053028466.md): Cover · damaged · Apr 23, 2024 · N159UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW DOOR, EXTERNAL SKIN HEX COVERS DAMAGED; DOT 117-020. REMOVED AND REPLACED CREW DOOR HIST POINT COVERS IAW AMM 11-00-11/001.
- [SDR IPXA2024051738316](https://openairdocs.org/sdr/IPXA2024051738316.md): Floor Panel · broken · Apr 23, 2024 · N159UP · Airbus A300F4622R · Fuselage Floor Panel
  > RH FLOOR PANEL 252 KM BROKEN DOT 44-007 FABRICATED PANEL 252KM FROM 5024N400001SS-G, BATCH# 4055277 PER SREO A300-5320-40552--B C/W.
- [SDR IPXA2024042328466](https://openairdocs.org/sdr/IPXA2024042328466.md): Skin · damaged · Apr 23, 2024 · N159UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW DOOR, EXTERNAL SKIN HEX COVERS DAMAGED;
- [SDR IPXA2024062015716](https://openairdocs.org/sdr/IPXA2024062015716.md): Hinge · damaged · Apr 22, 2024 · N159UP · Airbus A300F4622R · Fuselage, Door Hinge
  > DAMAGE FOUND IN AFT HINGE OF PIANO HINGE FITTINGS (ALUMINIUM LAYER 19F, 20F, 21F, 22F, 24F, 25F, 26F) (STEEL LAYER 20D). INSTALLED NEW HINGE AT MDC DOOR AFT SECTION, IAW A300-600 SRM 51-40-21, AND SRM 51-49-00. (T89019). VERIFIED HINGE WAS INSTALLED USING EX
- [SDR IPXA2024061815861](https://openairdocs.org/sdr/IPXA2024061815861.md): Support Bracket · cracked · Apr 22, 2024 · N159UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > E.E COMARTMENT, FR 10 UNDER RH FLOOR OF COCKPIT (BL 7097) BRACKET SUPPORT IS CRACKED. DOT 103-33 INSTALLED WEB AND ANGLE IAW-A300-600 SRM-51-40-21.
- [SDR IPXA2024061116226](https://openairdocs.org/sdr/IPXA2024061116226.md): Crossbeam · mechanic error · Apr 22, 2024 · N159UP · Airbus A300F4622R · Fuselage Main, Structure
  > E/E COMPARTMENT, FR16A, UNDER PANEL 121RF, DOUBLE DRILLED SCREW HOLE, BRACKET SUPPORT IS DAMAGE. INSTALLED NEW CROSSBEAM IAW SRM 51-40-21.
- [SDR IPXA2024062596080](https://openairdocs.org/sdr/IPXA2024062596080.md): Seat Track · corroded · Apr 20, 2024 · N159UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK BETWEEN FR79 AND FR80 HAS CORROSION AT Y0. INSTALLED NEW SEAT TRACK, U-SECCTION SPLICE (02 E/A) AND REPAIR ANGLE (01 E/A) IAW SRM 53-10-16 AND S.R.M. 51-40-21. ACCOMPLISH CATEGORY A REPAIR PER SRM REV 40 CHAPTER 53-10-16-201 PARAGRAPH 4 FIGURE 201
- [SDR IPXA2024061296583](https://openairdocs.org/sdr/IPXA2024061296583.md): Bracket · cracked · Apr 20, 2024 · N159UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > CRACKED BRACKETS AT FWD CARGO BULKHEAD FR38.2 INNER SIDE OF AFR CARGO WALL. VERIFIED INSTALLATION OF 5 EA BRACKETS ON FWD CARGO BULKHEAD FR38.2 IAW-A300-600 SRM-51-40-21.
- [SDR IPXA2024061296571](https://openairdocs.org/sdr/IPXA2024061296571.md): Bracket · broken · Apr 20, 2024 · N159UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > BROKEN BRACKETS SUPPORT AT FWD CARGO BULKHEAD FR 38.2 L/H WALL (2 EA). APPLIED PROTECTIVE SURFACE TREATMENT IAW SRM 51-21-10 AND EO M-5100-2780-L REQUEST TO INSTALL. INSTALLED BRACKETS (2EA) IAW SRM A300-600 51-40-21.
- [SDR IPXA2024061285949](https://openairdocs.org/sdr/IPXA2024061285949.md): Skirt · cracked · Apr 19, 2024 · N159UP · Airbus A300F4622R · Engine Thrust Reverser
  > NR 1 ENGINE OBD T/R CENTER UPPER EDGE PYLON SIDE FWD FINGER ( SKIRT) CRACKED. INSTALLED NEW PART EXTRUSION EDGING ON NR 1 ENGINE OBD T/R CENTER UPPER EDGE PYLON SIDE FWD. FINGER IAW SRM 51-40-21.
- [SDR IPXA2024010285037](https://openairdocs.org/sdr/IPXA2024010285037.md): Unknown · unknown · Dec 28, 2023 · N159UP · Airbus A300F4622R · Landing Gear Retraction/Extension System
  > ATB. GEAR DID NOT RETRACT, PUT HANDLE DOWN GOT 3 GREEN T/S PER TSM 32-61-00/101, REPLACED PROXIMITY DETECTOR PROCESSING UNIT, 54GB, PER AMM 32-31-71/401; OPS CHKS GOOD, OK FOR SVC
- [SDR IPXA2023072493714](https://openairdocs.org/sdr/IPXA2023072493714.md): Control Lever · inoperative · Jul 20, 2023 · N159UP · Airbus A300F4622R · Landing Gear Selector
  > AFTER TO IN IAH PLACED THE GEAR LEVER IN THE "UP" POSITION. GEAR REMAINED DOWN, "L/G RETRACTION INOP" ON ECAM. MOVED GEAR LEVER TO "DOWN" POSITION CYCLED BACK TO "UP" AND GEAR EXTENDED NORMALLY IN AUS. LANDING GEAR RETRACT SYS DEFERRED PER MEL 32-30-01. DMP 32

Next page: https://openairdocs.org/aircraft/N159UP/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 = 'N159UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N159UP/reports

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