# Service difficulty reports: N161UP

A list on [N161UP](https://openairdocs.org/aircraft/N161UP.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 · 206 reports

- [SDR IPXA2026092402007](https://openairdocs.org/sdr/IPXA2026092402007.md): Valve · failed · Sep 24, 2026 · N161UP · Airbus A300F4622R · Air Distribution System
  > OVERBOARD EXTRACT VALVE CAUSING EXTRACT FAN HIGH SPEED CIRCUIT BREAKER TO POP. REVERSED, REMOVED AND REPLACED EXTRACT FAN (73HR) IAW AMM 21-23-11/401, NO HELP. TROUBLESHOT IAW ASM 21-33-00 SCH 02 FOUND BAD RELAY (68HR), REMOVED AND REPLACED RELAY (68HR) IAW
- [SDR IPXA2026062235569](https://openairdocs.org/sdr/IPXA2026062235569.md): Gauge · obscured · Jun 18, 2026 · N161UP · Airbus A300F4622R · Escape Slide
  > L1 CREW DOOR ARM VIEWING WINDOW FOR DAMPNER IS UNABLE TO SEE THROUGH. REMOVED AND REPLACED VIEWING WINDOW ON L1 CREW DOOR ARM IAW M-DLPS707.
- [SDR IPXA2026061935569](https://openairdocs.org/sdr/IPXA2026061935569.md): Indicator · glazed · Jun 18, 2026 · N161UP · Airbus A300F4622R · Passenger/Crew Doors
  > L-1 CREW DOOR ARM VIEWING WINDOW FOR DAMPNER IS UNABLE TO SEE THROUGH VERIFIED AND INSPECTED REMOVED AND REPLACED VIEWING WINDOW ON L-1 CREW DOOR ARM IAW M-DLPS707.
- [SDR IPXA2026062294955](https://openairdocs.org/sdr/IPXA2026062294955.md): Support Bracket · cracked · Jun 16, 2026 · N161UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous Structure
  > LEFT SIDE UPPER HORIZONTAL APRON SUPPORT BRACKET IS CRACKED. INSTALLED SUPPORT FITTING AT LT SIDE HORIZONTAL APRON IAW SRM 51-40-21-001.
- [SDR IPXA2026062298593](https://openairdocs.org/sdr/IPXA2026062298593.md): Support Bracket · broken · Jun 16, 2026 · N161UP · Airbus A300F4622R · Passenger/Crew Doors
  > SUPPORT BRACKET ON UPPER L1 CREW DOOR IS BROKEN. INSTALLED BRACKET ON L1 CREW DOOR IAW SRM 51-40-21.
- [SDR IPXA2026061798593](https://openairdocs.org/sdr/IPXA2026061798593.md): Support Bracket · broken · Jun 16, 2026 · N161UP · Airbus A300F4622R · Passenger/Crew Doors
  > SUPPORT BRACKET ON UPPER L-1 CREW DOOR IS BROKEN
- [SDR IPXA2026061739584](https://openairdocs.org/sdr/IPXA2026061739584.md): Strap · cracked · Jun 12, 2026 · N161UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AGING FLEET INSPECTION-FAULT-COM-ZONE 300 INTERCOSTAL LOCATED IN THE AFT ACCESSORY COMPARMENT STA C85 JUST AFT OF ACCESS DOOR IS BENT AND CRACKED.AA031. INTERCOSTAL STRAP REMOVED IAW A300-600F SRM 51-40-21-001. NEW STRAP INTERCOSTAL INSTALLED IAW A300-600F SRM
- [SDR IPXA2026061520701](https://openairdocs.org/sdr/IPXA2026061520701.md): Bracket · cracked · Jun 11, 2026 · N161UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFT CARGO FWD BULKHEAD AT FR54 Y950 I/B BRACKET IS CRACKED REMOVED AND REPLACED BRACKET ON AFT CARGO FWD BULKHEAD AT FR54 Y950. BRACKET IAW SRM 51-40-21. PARG 6.
- [SDR IPXA2026061520629](https://openairdocs.org/sdr/IPXA2026061520629.md): Bracket · cracked · Jun 11, 2026 · N161UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFT CARGO FWD BULKHEAD AT FR54 Y-950 BRACKET IS CRACKED REMOVED AND REPLACE BRACKET ON AFT CARGO FWD BULKHEAD AT FR54 Y-950. BRACKET IAW SRM 51-40-21. PARG 6.
- [SDR IPXA2026061799413](https://openairdocs.org/sdr/IPXA2026061799413.md): Support Angle · cracked · Jun 10, 2026 · N161UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > INTERCOSTAL SUPPORT ANGLE LOCATED ON THE LEFT SIDE OF THE FORWARD AVIONICS COMPARMENT AT FRAME 10 IS CRACKED. INSTALLED NEW ANGLE AT FRAME 10 LT IAW SRM 51-40-21.
- [SDR IPXA2026063081398](https://openairdocs.org/sdr/IPXA2026063081398.md): Skin · dented · Jun 9, 2026 · N161UP · Airbus A300F4622R · Ailerons
  > RIGHT WING AILERON UPPER SURFACE TRAILING EDGE WEDGE HAS HAIL DAMAGE WITH NUMEROUS DENTS. NOT LISTED ON ADM OR DEFERRAL LOG. REMOVED R/H WING ALL SPEED AILERON IAW A300-600 AMM 27-11-28/401. INSTALLED RT WING ALL SPEED AILERON IAW AMM 27-11-28/401.
- [SDR IPXA2026062381318](https://openairdocs.org/sdr/IPXA2026062381318.md): Web · cracked · Jun 9, 2026 · N161UP · Airbus A300F4622R · Trailing Edge Flaps
  > INTERCOSTAL LOCATED ON RT WING TRAILING EDGE ABOVE #2 OUTBD FLAP CARRIAGE FWD LOWER CORNER IS CRACKED. AA010. REMOVED WEB AND BRACKET ON RH WING TRAILING EDGE ABOVE #2 OUTBD FLAP IAW A300 SRM 51-40-21. INSTALLED NEW WEB IN RH WING TRAILING EDGE ABOVE #2 OUTBD
- [SDR IPXA2026062388115](https://openairdocs.org/sdr/IPXA2026062388115.md): Carriage · cracked · Jun 9, 2026 · N161UP · Airbus A300F4622R · Trailing Edge Flaps
  > INTERCOSTAL LOCATED ON LEFT WING TRAILING EDGE ABOVE THE NR 2 OTBD FLAP CARRIAGE IS CRACKED AT THE LOWER FWD AND AFT CORNERS. REMOVED INTERCOSTAL AND BRACKET AT ZONE 500 LT WING TRAILING EDGE ABOVE THE NR 2 OTBD FLAP CARRIAGE IAW SRM 51-40-21. INSTALLED INTER
- [SDR IPXA2026062381140](https://openairdocs.org/sdr/IPXA2026062381140.md): Skin · corroded · Jun 9, 2026 · N161UP · Airbus A300F4622R · Wing, Plate/Skin
  > MULTIPLE AREAS OF CORROSION ON RT WING OUTBD FIXED TRAILING EDGE UPPER SURFACE IN ADDITION TO WHAT WAS ALREADY IDENTIFIED BY QC. AA008. REMOVED DAMAGED AT RT WING OUTBD FIXED TRAILING EDGE UPPER SURFACE SECTION WAS FOUND TO BE OUT OF LIMITS (75% LOSS MATERIAL,
- [SDR IPXA2026061932235](https://openairdocs.org/sdr/IPXA2026061932235.md): Support · cracked · Jun 5, 2026 · N161UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous Structure
  > FAULT: APG / Z400 / NO.1 PYLON AFT LOWER SECTION AT THE END OF DRAIN LINES SUPPORT HAS A CRACK ON LH SIDE. REMOVED MEMBER CRACKED IN NO.1 PYLON AFT LOWER SECTION I.A.W. A300-600 SRM 51-40-21. INSTALLED 1EA WEB AND 2EA SHEETMETAL FOLDED IN ASSEMBLY IAW SRM 51-
- [SDR IPXA2026061832267](https://openairdocs.org/sdr/IPXA2026061832267.md): Support · cracked · Jun 5, 2026 · N161UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous Structure
  > NR 1 PYLON AFT LOWER SECTION BEHIND OF DRAIN LINES SUPPORT HAS A CRACK ON LT SIDE INSTALLED NEW SUPPORT, P/N A5451520600000 ON NR 1 PYLON AFT LOWER SECTION IAW SRM 51-40-21-001.
- [SDR IPXA2026062212487](https://openairdocs.org/sdr/IPXA2026062212487.md): Frame · cracked · Jun 4, 2026 · N161UP · Airbus A300F4622R · Nacelle/Pylon, Frame/Spar/Rib
  > PYLON NR 2 AFT FAIRING 485AL INNER LT FWD FRAME HAS (1EA) CRACK. REMOVED FRAME WITH CRACK AT PYLON NR 2 AFT FAIRING 485AL INNER LT FWD IAW SRM 51-40-21-001. INSTALLED FRAME ON PANEL 485AL. IAW SRM 51-40-21-001.
- [SDR IPXA2026062212546](https://openairdocs.org/sdr/IPXA2026062212546.md): Frame · cracked · Jun 4, 2026 · N161UP · Airbus A300F4622R · Nacelle/Pylon, Frame/Spar/Rib
  > PYLON NR 2 AFT FAIRING 485AL INNER RT FWD FRAME HAS (1EA) CRACK. REMOVED INNER RH FWD FRAME AT PYLON NR 2 AFT FAIRING 485AL, IAW SRM 51-40-21-001. INSTALLED FRAME ON PANEL 485AL. IAW SRM 51-40-21-001.
- [SDR IPXA2026062215327](https://openairdocs.org/sdr/IPXA2026062215327.md): Frame · cracked · Jun 4, 2026 · N161UP · Airbus A300F4622R · Nacelle/Pylon, Frame/Spar/Rib
  > PYLON NR 1 FAIRING 475AL INNER RT FWD FRAME HAS (1EA) CRACK. FAIRING PYLON 475AL FRAME REMOVED IAW A300-600F SRM 51-40-21-001. INSTALLED FRAME AT THE PYLON NR 1 FAIRING 475AL INNER RT PER SRM 51-40-21.
- [SDR IPXA2026062215433](https://openairdocs.org/sdr/IPXA2026062215433.md): Frame · cracked · Jun 4, 2026 · N161UP · Airbus A300F4622R · Nacelle/Pylon, Frame/Spar/Rib
  > PYLON NR 1 FAIRING 475AL INNER LT FWD FRAME HAS (1EA) CRACK. FAIRING PYLON -475AL FRAME REMOVED IAW SRM 51-40-21-001. INSTALLED FRAME AT THE PYLON NR 1 FAIRING 475AL INNER LT IAW SRM 51-40-21.
- [SDR IPXA2026061708255](https://openairdocs.org/sdr/IPXA2026061708255.md): Floorbeam · cracked · Jun 4, 2026 · N161UP · Airbus A300F4622R · Fuselage Main, Floor Beam
  > STA 972-FR 11 FLOORBEAM ANGLE IS BROKEN. INSTALLED NEW ANGLE ON STA 972-FR 11 FLOORBEAM IAW SRM 51-40-21.
- [SDR IPXA2026061694292](https://openairdocs.org/sdr/IPXA2026061694292.md): Angle · cracked · Jun 3, 2026 · N161UP · Airbus A300F4622R · Wing, Attach Fittings
  > LEFT WING, FIXED L/E, INBD SIDE, INTERNAL STRUCTURE, JUST NEXT TO KRUEGER FLAP COMPARMENT, ANGLE WITH A CRACK 1/2 LONG. REMOVED ANGLE WITH CRACK IAW SRM 51-40-21. INSTALLED ANGLE IN LT WING, FIXED L/E, INBD SIDE, INTERNAL STRUCTURE IAW SRM 51-40-21.
- [SDR IPXA2026062395002](https://openairdocs.org/sdr/IPXA2026062395002.md): Wire · broken · Jun 3, 2026 · N161UP · Airbus A300F4622R · Door System Wiring
  > CREW DOOR CUTOUT, HINGE BONDING WIRE BROKEN. INSTALLED TERMINAL LUG AT BONDING JUMPER CREW DOOR IAW ESPM 20-56-22-03 AND INSTALLED BONDING JUMPER IAW AMM 20-28-11/001. BONDING TESTED GOOD.
- [SDR IPXA2026062294734](https://openairdocs.org/sdr/IPXA2026062294734.md): Roller Guide · damaged · Jun 3, 2026 · N161UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW DOOR CUTOUT, LOWER FWD ROLLER GUIDE DAMAGED. INSTALLED ROLLER GUIDE ON CREW DOOR CUTOUT, LOWER FWD IAW AMM 52-10-31.
- [SDR IPXA2026062294928](https://openairdocs.org/sdr/IPXA2026062294928.md): Roller · damaged · Jun 3, 2026 · N161UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW DOOR, FWD LOWER ROLLER DAMAGED. REMOVED AND REPLACED AT CREW DOOR, FWD LOWER ROLLER IAW AMM 52-11-21/401.
- [SDR IPXA2026062295167](https://openairdocs.org/sdr/IPXA2026062295167.md): Roller · damaged · Jun 3, 2026 · N161UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW DOOR, AFT LOWER ROLLER DAMAGED. REMOVED AND REPLACED AT CREW DOOR, AFT LOWER ROLLER IAW AMM 52-11-21/401.
- [SDR IPXA2026062295164](https://openairdocs.org/sdr/IPXA2026062295164.md): Bracket · damaged · Jun 3, 2026 · N161UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW DOOR, AFT LOWER ROLLER BRACKET DAMAGED. REMOVED AND REPLACED AT CREW DOOR, AFT LOWER ROLLER BRACKET IAW AMM 52-11-21/401.
- [SDR IPXA2026061794650](https://openairdocs.org/sdr/IPXA2026061794650.md): Door Frame · gouged · Jun 3, 2026 · N161UP · Airbus A300F4622R · Fuselage Main, Structure
  > CREW DOOR CUTOUT, UPPER FWD CORNER HAS A GOUGE. REMOVED MINOR GOUGE AT CREW DOOR CUTOUT, UPPER FWD CORNER IAW 51-10-10-101 AND ORIGINAL THIKNESS 0.265" MATERIAL LOST 0.003" REMAINING MATERIAL 0.262" FOUND WITH IN LIMITS IAW SRM 51-73-11-001. RESTORE SURFACE PR
- [SDR IPXA2026061795332](https://openairdocs.org/sdr/IPXA2026061795332.md): Handle · gouged · Jun 3, 2026 · N161UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW DOOR, EXTERNAL HANDLE HAS SEVERAL GOUGES. REMOVED GOUGES, EXTERNAL HANDLE AND ORIGINAL THICKNESS IS.120", MATERIAL LOSS IS.003" AND REMAINING THICKNESS IS.117" THE MAXIMUM ALLOWABLE IS.0039", FOUND TO BE WITHIN LIMITS IAW A300-600 SRM 51-73-10-201 A
- [SDR IPXA2026061794873](https://openairdocs.org/sdr/IPXA2026061794873.md): Stop Fitting · damaged · Jun 3, 2026 · N161UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW DOOR, STOPS WORN AND DAMAGED (10 EA). DOT 65-35. REMOVED AND REPLACED DOOR STOP FITTING (10EA), CREW DOOR I.A.W A-300 52-10-31/401 AND ADJUSTMENT CREW DOORS IS GOOD, I.A.W A-300 AMM 52-10-11/501.
- [SDR IPXA2026061795268](https://openairdocs.org/sdr/IPXA2026061795268.md): Handle · damaged · Jun 3, 2026 · N161UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW DOOR, EXTERNAL HANDLE PHENOLIC DAMAGED. REMOVED AND REPLACED CREW DOOR, EXTERNAL HANDLE PHENOLIC STOP I.A.W. SRM 51-49-00-001.
- [SDR IPXA2026060494650](https://openairdocs.org/sdr/IPXA2026060494650.md): Door Frame · gouged · Jun 3, 2026 · N161UP · Airbus A300F4622R · Fuselage Main, Structure
  > CREW DOOR CUTOUT, UPPER FWD CORNER HAS A GOUGE.
- [SDR IPXA2026060495332](https://openairdocs.org/sdr/IPXA2026060495332.md): Handle · gouged · Jun 3, 2026 · N161UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW DOOR, EXTERNAL HANDLE HAS SEVERAL GOUGES.
- [SDR IPXA2026060494928](https://openairdocs.org/sdr/IPXA2026060494928.md): Roller · damaged · Jun 3, 2026 · N161UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW DOOR, FWD LOWER ROLLER DAMAGED.
- [SDR IPXA2026060495167](https://openairdocs.org/sdr/IPXA2026060495167.md): Roller · damaged · Jun 3, 2026 · N161UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW DOOR, AFT LOWER ROLLER DAMAGED.
- [SDR IPXA2026060495002](https://openairdocs.org/sdr/IPXA2026060495002.md): Wire · broken · Jun 3, 2026 · N161UP · Airbus A300F4622R · Door System Wiring
  > CREW DOOR CUTOUT, HINGE BONDING WIRE BROKEN. DOT 65-39
- [SDR IPXA2026060495164](https://openairdocs.org/sdr/IPXA2026060495164.md): Bracket · damaged · Jun 3, 2026 · N161UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW DOOR, AFT LOWER ROLLER BRACKET DAMAGED.
- [SDR IPXA2026060495268](https://openairdocs.org/sdr/IPXA2026060495268.md): Handle · damaged · Jun 3, 2026 · N161UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW DOOR, EXTERNAL HANDLE PHENOLIC DAMAGED.
- [SDR IPXA2026061174508](https://openairdocs.org/sdr/IPXA2026061174508.md): Fitting · cracked · Jun 2, 2026 · N161UP · Airbus A300F4622R · Fuselage Main, Attach Fittings
  > RIGHT KEEL BEAM AT THE LEVEL OF CONNECTING FITTING BTW FR13A AND 14. (1EA) CRACK INDICATION NOTED ON LOWER AFT HOLE AT 8' O CLOCK. REMOVED ALL FASTNERS AT FR 13A FROM R/H SIDE OF THE KEEL BEAM AND DISPLACED FRAME IAW EA 300-5312-27-A5416 PRELIM 1 STEP 2 FIG 4.
- [SDR IPXA2026061374527](https://openairdocs.org/sdr/IPXA2026061374527.md): Fitting · cracked · Jun 2, 2026 · N161UP · Airbus A300F4622R · Fuselage Main, Attach Fittings
  > MAJOR REPAIR, LT KEEL BEAM AT THE LEVEL OF CONNECTING FITTING BTW FR13A AND 14. (2EA) CRACK INDICATION NOTED ON LOWER FWD HOLE AT 3 AND 9 O' CLOCK. ACCOMPLISH THE REPAIR PER EO-97755-REQ1 AND EA 300-5312-27-A4514, REV-.
- [SDR IPXA2026061174573](https://openairdocs.org/sdr/IPXA2026061174573.md): Keelbeam · cracked · Jun 2, 2026 · N161UP · Airbus A300F4622R · Fuselage Main, Keel
  > MAJOR REPAIR, LT KEEL BEAM AT THE LEVEL OF CONNECTING FITTING BTW FR13A AND 14. (2EA) CRACK INDICATION NOTED ON THE SURFACE. INSTALLED FASTENERS IN DOUBLER AND FITTING AT FR 13 A AND FR 14 ON LH SIDE OF KEEL BEAM IAW EA 300-5312-27-A4514 PRELIM 2 STEP 20 FIG
- [SDR IPXA2026060875059](https://openairdocs.org/sdr/IPXA2026060875059.md): Bulkhead · cracked · Jun 2, 2026 · N161UP · Airbus A300F4622R · Nacelle/Pylon, Bulkhead/Firewall
  > NR 1 ENG O/B NOSE COWL AFT BULKHEAD HAS A CRACK. INSTALLED NEW WEB AND SPLICE IAW SRM 51-40-21 AND SRM 54-10-00 REPAIR NO. 14.
- [SDR IPXA202604278989](https://openairdocs.org/sdr/IPXA202604278989.md): Lamp · burned out · Apr 25, 2026 · N161UP · Airbus A300F4622R · Emergency Lighting
  > LAVATORY AUXILIARY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-00, OPS CHECKED GOOD.
- [SDR IPXA2025092167557](https://openairdocs.org/sdr/IPXA2025092167557.md): Power Supply · no test · Sep 21, 2025 · N161UP · Airbus A300F4622R · Emergency Lighting
  > OPERATIONAL TEST OF THE EMERGENCY POWER-SUPPLY UNITS WITH BITE CHECK FAILS. REF STEP 15 OF PSM. T/S PER TSM 33-51-00/101. FOUND UNIT FAULT LIGHT ILLUMINATED ON ESPU. REMOVED AND REPLACED ESPU IAW MM 33-51-14/0401. ALL OPS CHECK GOOD.
- [SDR IPXA2025081845060](https://openairdocs.org/sdr/IPXA2025081845060.md): Windshield · failed · Aug 13, 2025 · N161UP · Airbus A300F4622R · Flight Compartment Windows
  > PASSING 20,000 FEET NOTICED ARCING AND BURNING IN LOWER RIGHT CORNER OF CAPT WINDSCREEN. TURNED OFF HEAT PER QRH. PASSING 24,000 WINDSCREEN SHATTERED. COMPLETED CHECK LIST IN QRH. RETURNED TO RFD. REMOVED AND REPLACED LH WINDSHIELD IN REF TO AMM 56-11-11/0401
- [SDR IPXA2025081300001](https://openairdocs.org/sdr/IPXA2025081300001.md): Windshield · failed · Aug 13, 2025 · N161UP · Airbus A300F4622R · Flight Compartment Windows
  > AIR TURNBACK, PASSING 20,000 FEET NOTICED ARCING AND BURNING IN LOWER RIGHT CORNER OF CAPT WINDSCREEN. TURNED OFF HEAT PER QRH. PASSING 24,000 WINDSCREEN SHATTERED. COMPLETED CHECK LIST IN QRH. RETURNED TO RFD.
- [SDR IPXA2025021318055](https://openairdocs.org/sdr/IPXA2025021318055.md): Packing · failed · Feb 12, 2025 · N161UP · Airbus A300F4622R · Landing Gear Retraction/Extension System
  > LND GEAR SLOW TO RAISE ON T/O ECAM: "GEAR DOWN APPEARED BUT RETRACTED BEFORE ECAM ACTION. REMOVED AND REPLACED THE PACKING AND WASHER PACKING FOR PORT A ON THE LANDING GEAR SELECTOR VALVE IAW A300 AMM 32-31-12. OPS CHECK GOOD. REVERSED DMP, VMO/MMO SWITCH
- [SDR IPXA2025012351414](https://openairdocs.org/sdr/IPXA2025012351414.md): Landing Gear · lack of lube · Jan 17, 2025 · N161UP · Airbus A300F4622R · Landing Gear System
  > AFTER TAKEOFF WE GOT LANDING GAR RETRACTION INOP AND RETURNED TO SDF LUBED BOTH BOGIE BEAMS.ACCOMPLISHED A300 TSM 32-30-00/101 FIG 109 SHEET 1 BLOCKS 1,2,3,4,5,6 AND, 13 NO FAULTS FOUND WITH NOSE GEAR STEERING REF TSM 32-51-00
- [SDR IPXA2024110545086](https://openairdocs.org/sdr/IPXA2024110545086.md): Reservoir · inoperative · Nov 2, 2024 · N161UP · Airbus A300F4622R · Hydraulic Power Accumulator, Main
  > GREEN RSVR LO LEVEL. GREEN SYSTEM SHOWED LOW INFLIGHT. REF BARCODE T3F18E005HJ2D FOR R&R OF THE GREEN SYSTEM HYDRAULIC RESERVOIR HYDRAULIC QUANTITY TRANSMITTER PER AMM 29-31-11, FUNCTION CHECK GOOD.
- [SDR IPXA2024110445086](https://openairdocs.org/sdr/IPXA2024110445086.md): Transmitter · malfunctioned · Nov 2, 2024 · N161UP · Airbus A300F4622R · Hydraulic System, Main
  > **EMERGENCY DECLARED**GREEN RSVR LO LEVEL. GREEN SYSTEM SHOWED LOW INFLIGHT. PERFORMED HYDRAULIC QUANTITY INDICATING FUNCTIONAL TEST REF AMM 29-31-00/501. FOUND TRANSMITTER NOT OPERATING NORMALLY. WORKS NORMALLY IN LOW FLUID LEVEL. WILL NOT WORK WITH HIGH LEVE

Next page: https://openairdocs.org/aircraft/N161UP/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 = 'N161UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N161UP/reports

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