N165UP

Service difficulty reports · 173

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 = 'N165UP' 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 IPXA2026082163037Door · out of rigAIR TURN BACK, EMERGENCY DECLARED, BETWEEN 10-13K IN CLIMB, CONSTANT AURAL WARNING FROM CABIN DOOR SLIDE. ATB TO SDF. ACCOMPLISHED L1 DOOR LOCKING MECHANISM ADJUSTMENT (ROD 9). OPS CHECKS GOOD. NO RIG PINS REQUIRED. IAW AMM 52-10-20/501.Aug 21, 2026 · N165UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2026061652024Fitting · gougedFR47 LH FOWARD FITTING ULTRASONIC INSP HOLE "A" HAS GOUGE AT 11 O'CLOCK(FWD LOOKING AFT). INSTALL THE FASTENER (NSA5351V8-28(1EA)(OR ALTERNATE PER SRM51-40-30), BATCH# 0004023434) NUT# ASNA2531-8(1EA), BATCH# 0004403833 AT HOLE"A" LOCATION PER SRM51-40-21-001Jun 13, 2026 · N165UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026021260798Handle · brokenENTRY DOOR OUTR HANDLE SHUTTER BROKEN REMOVED AND REPLACED L1 DOOR SHUTTER HANDLE IAW AIRBUS CMM 52-11-11. OPS CHECK GOOD.Feb 11, 2026 · N165UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2025080583394Selector Valve · inoperativeDURING CRUISE, NOTICED SLOW DEPLETION OF GREEN SYSTEM HYDRAULIC RESERVOIR. SHORTLY THEREAFTER, RECIEVED €ŒGREEN RSVR LO LEVEL€? ECAM MESSAGE. RAN ECAM ITEMS AND QRH / AOM ASSOCIATED CHECKLISTS. ENGAGED. FOUND LANDING GEAR SELECTOR VALVE 3GA LEAKING BEYOND Aug 4, 2025 · N165UP · Airbus A300F4622R · Landing Gear Retraction/Extension SystemSDR IPXA2025041495052Light · no discrepancyEMERGENCY EXIT LIGHTS WILL NOT DISARM OPERATED AND TESTED SUPERNUMERARY AREA EMERGENCY LIGHTS REF AMM 33-51-00/501 LIGHTS GO ON/OFF AS COMMANDEDApr 13, 2025 · N165UP · Airbus A300F4622R · Emergency LightingSDR IPXA2025012460562Trim Panel · unsecureTOP TRIM PANEL ON CREW ACCESS DOOR IS NOT SECURE AND NEEDS TIGHTENING TIGHTED AND INSTALLED TOP TRIM PANEL MOUNTING HARDWARE IAW AMM 25-23-41. OPS CHECK GOOD.Jan 24, 2025 · N165UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2024122097598Circuit Breaker · faultedEMERGENCY EXIT LIGHT SWITCH WOULD NOT DISARM LIGHTS AFTER LANDING RECYCLED EMER LIGHT CHARGER C/B, CKS OK IAW MM 33-51-00-715-001 NO HISTORY LAST 10 DAYS, SYS OK FOR SERVICE.Dec 19, 2024 · N165UP · Airbus A300F4622R · Emergency LightingSDR IPXA2024121385564Bottle · low pressureMAIN CABIN DOOR ASSIST BOTTLE PRESSURE READS 900. SERVICED ASSIST BOTTLE IAW AMM 52-10-14.Dec 13, 2024 · N165UP · Airbus A300F4622R · Emergency EquipmentSDR IPXA2024101104287Rib · crackedPANEL 423AL HAS A CRACK (BETWEEN 3" TO 4" LONG) DOT 129-001 (GE-129) INSTALLED RIB AT PYLON #2 WITH EXISTING FASTENERS IAW A300-600 SRM 51-40-21.Oct 1, 2024 · N165UP · Airbus A300F4622R · Nacelle/Pylon, Frame/Spar/RibSDR IPXA2024102334491Stringer · crackedSTR R/H I/B AILERON P/N A57661001179 HAS A GOUGE WITH A CRACK IN IT ON FITTING. COMPLIED WITH EO-91570-REQ1 AND VTMAE FINAL EA 300-5761-27-A3701 REV -. REVIEWEDSep 27, 2024 · N165UP · Airbus A300F4622R · AileronsSDR IPXA2024100908610Arm · deterioratedCREW ENTRY DOOR, DOOR ARM W/CIC DETERIORATED; NO DOT. JR-117. APPLIED CIC IAW EO-2780-REQ001. PN 04-002-0153 BATCH 0004291043. REVIEWEDSep 26, 2024 · N165UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2024092608610Door · deteriorated*SDR FILED OPEN* FAULT: APG-Z800 CREW ENTRY DOOR, DOOR ARM W/CIC DETERIORATED; NO DOT. JR-117. APPROVEDSep 26, 2024 · N165UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2024100965843Support · crackedR/H MCD FOOR DAWG BONE SUPPORT BETWEEN FR 38.1-38.2 AT -Y2462 IS CRACKED. 33-026. INSTALLED DAWG BONE AT MDC BETWEEN FR38.1 AND FR38.2 -Y2462 USING FASTENERS P/N HL10VF6-8, BATCH 0004288775 AND P/N HL70-6, BATCH 0004305623, IAW A300-600 SRM 51-40-21.Sep 24, 2024 · N165UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2024100171033Seat Track · brokenMAIN DECK. SEAT TRACK AT FR37 BTW Y2462/Y1959 BROKEN. INSTALLED ADAPTER AT MAIN DECK SEAT TRACK AT FR 37 IAW 51-41-21 PN B5377413620490 BN 0004312613.Sep 24, 2024 · N165UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2024100168160Web · brokenBTW FR 79 AND 80, L/H NEXT TO SEAT TRACK Y2462, WEB BROKEN. DOT 73-038 (MOYA-73). INSTALLED NEW WEB AT FR79 TO FR 80 IAW A300 SRM 51-40-21 PN#5398111320051 BATCH#0003652288.Sep 24, 2024 · N165UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2024100168231Web · brokenBTW FR 79 AND 80, R/H NEXT TO SEAT TRACK Y-2462, WEB BROKEN. DOT 73-039 (MOYA-73). INSTALLED NEW WEB AT FR79 TO FR80 IAW 300 SRM 51-40-21 PN 4263193 BN#02-013-8 PN#4319064 BN#PG-W2K4Q PAINT CUP 02-012-176.Sep 24, 2024 · N165UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2024100165567Track · brokenR/H MCD FLOORPANEL 242KF C-TRACK AT FR 34 IS BROKEN. 33-022. INSTALLED ADAPTER IAW A300-600 SRM 51-40-21.Sep 24, 2024 · N165UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2024100168243Web · damagedMCC, BTW FR 76 AND 77, R/H NEXT TO SEAT TRACK Y-2462, WEB BROKEN. DOT 73-040 (MOYA-73). INSTALLED NEW WEB WITH EXISTING FASTENERS AND RIVETS P/N MS20426AD5-8, BATCH 0004289284 AND MS20426AD6-15, BATCH 0004225945 IAW A300-600 SRM 51-40-21.Sep 24, 2024 · N165UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2024100168184Seat Track · damagedBTW FR 38.1, AND 38.2, L/H AFTER SEAT TRACK 2462, BONE SUPPORT BROKEN. DOT 73-036 (MOYA-73). INSTALLED NEW BONE SUPPORT AT FR38.1 TO FR38.2 IAW A300 SRM 51-40-21 PN 5378103821400 BN 0004062096.Sep 24, 2024 · N165UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2024101422996Skin · dentedRIGHT WING CENTER FLAP, LEADING EDGE. DENTED FOWARD OF CENTER UPPER SKIN SLING ATTACH POINT. INSTALLED 02 EA BUTTSTRAPS AND DOUBLER TO RH CENTER FLAP LEADING EDGE SKIN. WITH RIVETS P/N: MS20426DD4-5. BATCH: 4196486. P/N: NAS1739E4-3. BATCH: 4302252 AND SEALANTSep 20, 2024 · N165UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2024101122648Rib · crackedPYLON #1 UPPER AREA PRESSURE RELIEF DOOR AFT BOLT SIDE HAS 2 POINTS WITH CRACKS 34-023. INSTALLED RIB AT PYLON #1 IAW A300-600 SRM 51-40-21 USING EXSISTING FASTENERS.Sep 20, 2024 · N165UP · Airbus A300F4622R · Nacelle/Pylon, Frame/Spar/RibSDR IPXA2024100100692Floorbeam · bentMAIN DECK-FR 48 CROSSBEAM BENT -Y450 TO -Y953-DOT 109-097-VWV. REMOVED AND REPLACED ON MAIN CABIN DECK FR 48 CROSSBEAM IAW A 300-600 SRM 51-40-21.NO FURTHER ACTION REQUIRED.Sep 19, 2024 · N165UP · Airbus A300F4622R · Fuselage Main, Floor BeamSDR IPXA2024100100764Inlet · crackedENG# 1 INLET COWL T/E AREA AT POSITION 9 O'CLOCK HAS SURFACE CRACKED. DOT 34-003. INSTALLED NEW WEB REPAIR AND SPLICE IAW PRATT & WHITNEY SRM 54-10-00. PN: CR3213-6-06, BN: 0004304591, PN: CR3213-6-04, BN: 0004282032. INSTALLED LINE AND COVER IAW A300 AMM 73-2Sep 19, 2024 · N165UP · Airbus A300F4622R · Nacelle/Pylon, Main FrameSDR IPXA2024100291945Floor Panel · crackedPANEL 147CZ HAS (1EA) CRACK TO EDGE AT ATTACH HOLE-DOT 109-076-VWV. REPLACED 147CZ WITH NEW PANEL P/N A2551030700600 BATCH 0004327949 IAW A300-600 AMM 25-72-41/401. NO FURTHER ACTION REQUIRED.Sep 19, 2024 · N165UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2024100150355Floor Support · crackedAFT CARGO FWD BULKHEAT FR 54 L/H MID FOUND TWO CRACKED FLOOR SUPPORT BARCKETS. DOT 60-008 AND 60-009. INSTALLED NEW SUPPORT IAW A300 SRM 51-40-21 PN EN6001D6-10 BN :0004085927.Sep 17, 2024 · N165UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2024100141579Support Bracket · crackedAFT CARGO-FR54 L/H B/H PANEL SUPPORT (A5341076522200) AT Y1959 CRACKED-DOT 109-010-VWV. INSTALLED NEW SUPPORT IAW A300 SRM 51-40-21 PN EN6001D6-10 BN 00040855927.Sep 17, 2024 · N165UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2024100141519Support Bracket · crackedAFT CARGO-FR54 CTR B/H PANEL SUPPORT (A5341076521700) AT Y0 CRACKED-DOT 109-009-VWV. INSTALLED NEW SUPPORT BRACKET AT AFT CARGO COMPARTMENT IAW A300 SRM 51-40-21 PN EN6001D6-10 BN 0004085927.Sep 17, 2024 · N165UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2024100131294Bracket · deterioratedFUSELAGE LOWER, AFTER ADAPTER SAFETY STAY HAS BRACKET DETERIORATED DOT 108-08. INSTALLED 02 EA ANGLES WITH 04 EA RIVETS P/N: HL12VF6-4. BATCH: 4115479 WITH 04 EA COLLARS P/N:HL70-6, BATCH: 4305623. AND SEALANT P/N: PR1422 B2. BATCH: 4305492. IAW A300-600 SRM 5Sep 16, 2024 · N165UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2024091373656Light · inoperativeEMERGENCY EXIT LIGHTS IN DISARM POSITION NOT WORKING. EMERGENCY LIGHTS IN SUPERNUMERARY AREA ON. PERFORMED OPS CHECK OF EMERGENCY EXIT LIGHT SWITCH IAW AMM 33-51-00. OPS CHECK GOOD.Sep 13, 2024 · N165UP · Airbus A300F4622R · Emergency LightingSDR IPXA2024050600755Relay · faultedOPERATIONAL CHECK OF INTERIOR EMERGENCY LIGHTS FAILED THE AUTOMATIC ACTIVATION IN EVENT OF DC POWER FAILURE CHECK T/S PER A300 AWM 33-51-03 SUSPECT 490VU MAINTENANCE PANEL 233LT RLY DIM. R&R RELAY IAW ESPM 20-46-50-01. PERFORMED OPS TEST OF EMERGENCY LIGHTING May 3, 2024 · N165UP · Airbus A300F4622R · Emergency LightingSDR IPXA2024050300755Light · no testOPEN, OPERATIONAL CHECK OF INTERIOR EMERGENCY LIGHTS FAILED THE AUTOMATIC ACTIVATION IN EVENT OF DC POWER FAILURE CHECKMay 3, 2024 · N165UP · Airbus A300F4622R · Emergency LightingSDR IPXA2024012403951Contact · brokenCREW ENTERANCE DOOR SLIDE LIGHT OUT OF MOUNTING BRACKET FOUND WIRE 5273-1099 BROKEN AT CONTACT 2 OF THE SLIDE LIGHT ASSEMBLY 7WN. REPINNED, REF ESPM 20-48-21 AND AWM 52-73-05. OP CHECKS GOOD, REF AMM 52-73-11. DEFERRAL CLEARED. PLACARD REMOVED.Jan 24, 2024 · N165UP · Airbus A300F4622R · Door System WiringSDR IPXA2023122881716Unknown · unknownDOOR SLIDE ARMING LEVER RED LIGHT INOPERATIVE RESEATED CONNECTOR ON THE AUTONOMOUS PWR SUPPLY UNIT 70WN REF AMM 52-73-18 & OPS CHECKED OK IAW AMM 52-73-00. WARNING LIGHT 7WN TESTS OK.Dec 28, 2023 · N165UP · Airbus A300F4622R · Door Warning SystemSDR IPXA2023120506560Unknown · unknownDOOR ACTUATOR PRESSURE IS LOW SERVICED DOOR DAMPER WITH HIGH PRESSURE DRY NITROGEN PER AMM 52-10-14. OPS CHECK GOOD.Dec 5, 2023 · N165UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2023112057964Unknown · unknownDURING PREFLIGHT FOUND WHAT APPEARS TO BE A CRACK RUNNING ACROSS THE CENTER OF F/O WINDSCREEN. REMOVED F/O WINDSHIELD UP TO STEPS 1.C.(6) PER AM 56-11-11. COMPLETED INSTALL OF F/O WINDSHIELD IAW AMM 56-11-11Nov 18, 2023 · N165UP · Airbus A300F4622R · Flight Compartment WindowsSDR IPXA05769Unknown · unknownLOWER VERTICAL STAB LEADING EDGE PANEL HAS SUSPECTED EROSION DAMAGE ON BOTTOM TWO THIRDS OF PANEL AS VIEWED FROM GROUND LEVEL. REMOVED AND REPLACED LOWER VERTICAL STAB LEADING EDGE PANEL 322AL IAW A300 AMM 55-32-11-401Oct 22, 2023 · N165UP · Airbus A300F4622R · Vertical Stabilizer, Plate/SkinSDR IPXA2023041992920Damper · inoperativeINSPECTION TYPE:NACREW ENTRY DOOR DAMPER / EMERGENCY OPERATION CYLINDER PRESSURE LOW.CYLINDER SERVICED WITH NITROGEN REF: A300 AMM 52-10-14-0301. NO LEAKS/DEFECTS.Apr 18, 2023 · N165UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2023010189457Control Switch · faultedATB, CONTINUOUS GEAR OVERSPEED WARNING DUE TO DOWN ARROW ON GEAR AIR TURNED BACK TO RFD, FLSE GEAR DWN INDICTION AT ALT VRIFID THRU ATS RPLCD L/G CTOL MICROSWTCH UNIT (2GA) A300MM 32-31-11-401 OPS CK NRML RPLCD FAULTY FWC2 IPC 32-31-12-10. MM 31-51-00 ECAM SYDec 31, 2022 · N165UP · Airbus A300F4622R · Landing Gear Retraction/Extension SystemSDR IPXA2022080885030Light · inoperativeINSPECTION TYPE:N/AEMER EXIT LT ON OVHD NOT ILLUMINATED WHEN DISARMED LGIHT DOES NOT TESTEMER EXIT LT ON OVHD OPS CHECK GOOD IAW AMM 33 14 00Aug 6, 2022 · N165UP · Airbus A300F4622R · Emergency LightingSDR IPXA2022032180336Power Supply · unserviceableINSPECTION TYPE:SEGDOES NOT ILLUMINATE RESIDUAL PRESSURE WARNING LIGHTREMOVED AND REPLACED ASPSU IAW AMM 52-73-18-401Mar 20, 2022 · N165UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2022032080290Stiffener · crackedINSPECTION TYPE:SEGCRACK IN APU TAIL COMPARTMENT AT FRAM 101 APP. 3 O'CLOCK POSITION LOOKING FORWARD.ACCOMPLISHED REPAIR PER FINAL EA 300-5319-27-A2874 AND FINAL UPS EO A300-5320-83201-AMar 19, 2022 · N165UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2022032080279Shear Plate · crackedINSPECTION TYPE:CLH SIDE STR 44 AT FR65 WEB IS CRACKED AT UPPER AFT CORNERFAB REMOVED AND REPLACED WE (SHEAR PLATE) IAW SRM 53-17-8 AND SRM 51-40-21Mar 19, 2022 · N165UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2022032080278Angle · brokenINSPECTION TYPE:CRH WING KRUEGER FLAP ZONE LH SIDE PANEL SUPPERT IS BROKENFAB REMOVED AND REPLACED ANGLE IAW SRM 57-41-11 AND SRM 51-40-21Mar 19, 2022 · N165UP · Airbus A300F4622R · Leading Edge DevicesSDR IPXA2022031880260Angle · crackedINSPECTION TYPE:A300RH WING KREUGER FLAP MIDDLE ZONE WEB IS CRACKEDREMOVED AND REPLACED ANGLE IAW SRM 51-40-21Mar 18, 2022 · N165UP · Airbus A300F4622R · Leading Edge DevicesSDR IPXA2022031880259Angle · crackedINSPECTION TYPE:A300RH WING KRUEGER FLAP ZONE SUPPORT BRACKET (ANGLE) IS CRACKEDFABRICATED,REMOVED AND REPLACED ANGLE IAW SRM 57-41-11 AND SRM 51-31-00 TABLE 4Mar 18, 2022 · N165UP · Airbus A300F4622R · Leading Edge DevicesSDR IPXA2022031880258Angle · crackedINSPECTION TYPE:A300LH WING KREUGER FLAP MIDDLE ZONE WEB IS CRACKEDREMOVED AND REPLACED ANGLE IAW SRM 51-40-21Mar 18, 2022 · N165UP · Airbus A300F4622R · Leading Edge DevicesSDR IPXA2022031780233Fitting · brokenINSPECTION TYPE:SEGLH WING KRUEGER FLAP MIDDLE ZONE HAS METAL PLATE BROKENFABRICATED AND REPLACED PLATE PER SRM 57-41-12 FIG 3 SECTION B-BMar 17, 2022 · N165UP · Airbus A300F4622R · Wing Main, Frame StructureSDR IPXA2022031580147None · brokenINSPECTION TYPE:SEGE/E COMP FLOOR PANEL 121YF BROKENREPAIR IAW SREO A300-5320-42722FMar 15, 2022 · N165UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR IPXA2021091974035Skin · damagedDAMAGE TO THE UPPER SKIN OF THE FLAP REQUIRES REPAIR. ACCOMPLISH REPAIR IN ACCORDANCE WITH EO A300-5750-81573-BSep 19, 2021 · N165UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2021083173362Slide · inoperativeSLIDE ARMING LEVER WILL NOT MOVE CANNOT ARM EMERG ESCAPE SLIDE. DEF PER MEL 52-11-01-2-3. SLIDE ARMING LEVER WILL NOT MOVE CANNOT ARM EMERG ESCAPE SLIDE. DEF PER MEL 52-11-01-2-3DMP REVERSED REMOVED GIRT BAR FROM FLAP. REORIENTED GIRT BAR IAW AMM 25-61-21.Aug 30, 2021 · N165UP · Airbus A300F4622R · Escape Slide
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