N161UP

Service difficulty reports · 206

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR IPXA2026092402007Valve · failedOVERBOARD 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 Sep 24, 2026 · N161UP · Airbus A300F4622R · Air Distribution SystemSDR IPXA2026062235569Gauge · obscuredL1 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.Jun 18, 2026 · N161UP · Airbus A300F4622R · Escape SlideSDR IPXA2026061935569Indicator · glazedL-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.Jun 18, 2026 · N161UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2026062294955Support Bracket · crackedLEFT SIDE UPPER HORIZONTAL APRON SUPPORT BRACKET IS CRACKED. INSTALLED SUPPORT FITTING AT LT SIDE HORIZONTAL APRON IAW SRM 51-40-21-001.Jun 16, 2026 · N161UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous StructureSDR IPXA2026062298593Support Bracket · brokenSUPPORT BRACKET ON UPPER L1 CREW DOOR IS BROKEN. INSTALLED BRACKET ON L1 CREW DOOR IAW SRM 51-40-21.Jun 16, 2026 · N161UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2026061798593Support Bracket · brokenSUPPORT BRACKET ON UPPER L-1 CREW DOOR IS BROKENJun 16, 2026 · N161UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2026061739584Strap · crackedAGING 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 SRMJun 12, 2026 · N161UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026061520701Bracket · crackedAFT 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.Jun 11, 2026 · N161UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026061520629Bracket · crackedAFT 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.Jun 11, 2026 · N161UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026061799413Support Angle · crackedINTERCOSTAL 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.Jun 10, 2026 · N161UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026063081398Skin · dentedRIGHT 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.Jun 9, 2026 · N161UP · Airbus A300F4622R · AileronsSDR IPXA2026062381318Web · crackedINTERCOSTAL 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 Jun 9, 2026 · N161UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2026062388115Carriage · crackedINTERCOSTAL 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 INTERJun 9, 2026 · N161UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2026062381140Skin · corrodedMULTIPLE 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,Jun 9, 2026 · N161UP · Airbus A300F4622R · Wing, Plate/SkinSDR IPXA2026061932235Support · crackedFAULT: 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-Jun 5, 2026 · N161UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026061832267Support · crackedNR 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.Jun 5, 2026 · N161UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026062212487Frame · crackedPYLON 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.Jun 4, 2026 · N161UP · Airbus A300F4622R · Nacelle/Pylon, Frame/Spar/RibSDR IPXA2026062212546Frame · crackedPYLON 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.Jun 4, 2026 · N161UP · Airbus A300F4622R · Nacelle/Pylon, Frame/Spar/RibSDR IPXA2026062215327Frame · crackedPYLON 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.Jun 4, 2026 · N161UP · Airbus A300F4622R · Nacelle/Pylon, Frame/Spar/RibSDR IPXA2026062215433Frame · crackedPYLON 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.Jun 4, 2026 · N161UP · Airbus A300F4622R · Nacelle/Pylon, Frame/Spar/RibSDR IPXA2026061708255Floorbeam · crackedSTA 972-FR 11 FLOORBEAM ANGLE IS BROKEN. INSTALLED NEW ANGLE ON STA 972-FR 11 FLOORBEAM IAW SRM 51-40-21.Jun 4, 2026 · N161UP · Airbus A300F4622R · Fuselage Main, Floor BeamSDR IPXA2026061694292Angle · crackedLEFT 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.Jun 3, 2026 · N161UP · Airbus A300F4622R · Wing, Attach FittingsSDR IPXA2026062395002Wire · brokenCREW 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.Jun 3, 2026 · N161UP · Airbus A300F4622R · Door System WiringSDR IPXA2026062294734Roller Guide · damagedCREW DOOR CUTOUT, LOWER FWD ROLLER GUIDE DAMAGED. INSTALLED ROLLER GUIDE ON CREW DOOR CUTOUT, LOWER FWD IAW AMM 52-10-31.Jun 3, 2026 · N161UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2026062294928Roller · damagedCREW DOOR, FWD LOWER ROLLER DAMAGED. REMOVED AND REPLACED AT CREW DOOR, FWD LOWER ROLLER IAW AMM 52-11-21/401.Jun 3, 2026 · N161UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2026062295167Roller · damagedCREW DOOR, AFT LOWER ROLLER DAMAGED. REMOVED AND REPLACED AT CREW DOOR, AFT LOWER ROLLER IAW AMM 52-11-21/401.Jun 3, 2026 · N161UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2026062295164Bracket · damagedCREW DOOR, AFT LOWER ROLLER BRACKET DAMAGED. REMOVED AND REPLACED AT CREW DOOR, AFT LOWER ROLLER BRACKET IAW AMM 52-11-21/401.Jun 3, 2026 · N161UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2026061794650Door Frame · gougedCREW 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 PRJun 3, 2026 · N161UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026061795332Handle · gougedCREW 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 AJun 3, 2026 · N161UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2026061794873Stop Fitting · damagedCREW 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.Jun 3, 2026 · N161UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2026061795268Handle · damagedCREW DOOR, EXTERNAL HANDLE PHENOLIC DAMAGED. REMOVED AND REPLACED CREW DOOR, EXTERNAL HANDLE PHENOLIC STOP I.A.W. SRM 51-49-00-001.Jun 3, 2026 · N161UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2026060494650Door Frame · gougedCREW DOOR CUTOUT, UPPER FWD CORNER HAS A GOUGE.Jun 3, 2026 · N161UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026060495332Handle · gougedCREW DOOR, EXTERNAL HANDLE HAS SEVERAL GOUGES.Jun 3, 2026 · N161UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2026060494928Roller · damagedCREW DOOR, FWD LOWER ROLLER DAMAGED.Jun 3, 2026 · N161UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2026060495167Roller · damagedCREW DOOR, AFT LOWER ROLLER DAMAGED.Jun 3, 2026 · N161UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2026060495002Wire · brokenCREW DOOR CUTOUT, HINGE BONDING WIRE BROKEN. DOT 65-39Jun 3, 2026 · N161UP · Airbus A300F4622R · Door System WiringSDR IPXA2026060495164Bracket · damagedCREW DOOR, AFT LOWER ROLLER BRACKET DAMAGED.Jun 3, 2026 · N161UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2026060495268Handle · damagedCREW DOOR, EXTERNAL HANDLE PHENOLIC DAMAGED.Jun 3, 2026 · N161UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2026061174508Fitting · crackedRIGHT 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.Jun 2, 2026 · N161UP · Airbus A300F4622R · Fuselage Main, Attach FittingsSDR IPXA2026061374527Fitting · crackedMAJOR 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-.Jun 2, 2026 · N161UP · Airbus A300F4622R · Fuselage Main, Attach FittingsSDR IPXA2026061174573Keelbeam · crackedMAJOR 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 FIGJun 2, 2026 · N161UP · Airbus A300F4622R · Fuselage Main, KeelSDR IPXA2026060875059Bulkhead · crackedNR 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.Jun 2, 2026 · N161UP · Airbus A300F4622R · Nacelle/Pylon, Bulkhead/FirewallSDR IPXA202604278989Lamp · burned outLAVATORY AUXILIARY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-00, OPS CHECKED GOOD.Apr 25, 2026 · N161UP · Airbus A300F4622R · Emergency LightingSDR IPXA2025092167557Power Supply · no testOPERATIONAL 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.Sep 21, 2025 · N161UP · Airbus A300F4622R · Emergency LightingSDR IPXA2025081845060Windshield · failedPASSING 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 Aug 13, 2025 · N161UP · Airbus A300F4622R · Flight Compartment WindowsSDR IPXA2025081300001Windshield · failedAIR 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.Aug 13, 2025 · N161UP · Airbus A300F4622R · Flight Compartment WindowsSDR IPXA2025021318055Packing · failedLND 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 Feb 12, 2025 · N161UP · Airbus A300F4622R · Landing Gear Retraction/Extension SystemSDR IPXA2025012351414Landing Gear · lack of lubeAFTER 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 32-51-00Jan 17, 2025 · N161UP · Airbus A300F4622R · Landing Gear SystemSDR IPXA2024110545086Reservoir · inoperativeGREEN 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.Nov 2, 2024 · N161UP · Airbus A300F4622R · Hydraulic Power Accumulator, MainSDR IPXA2024110445086Transmitter · malfunctioned**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 LEVENov 2, 2024 · N161UP · Airbus A300F4622R · Hydraulic System, Main
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