# Service difficulty reports: N165UP

A list on [N165UP](https://openairdocs.org/aircraft/N165UP.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 4 · 173 reports

- [SDR IPXA2026082163037](https://openairdocs.org/sdr/IPXA2026082163037.md): Door · out of rig · Aug 21, 2026 · N165UP · Airbus A300F4622R · Passenger/Crew Doors
  > AIR 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.
- [SDR IPXA2026061652024](https://openairdocs.org/sdr/IPXA2026061652024.md): Fitting · gouged · Jun 13, 2026 · N165UP · Airbus A300F4622R · Fuselage Main, Structure
  > FR47 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 SRM51-40-21-001
- [SDR IPXA2026021260798](https://openairdocs.org/sdr/IPXA2026021260798.md): Handle · broken · Feb 11, 2026 · N165UP · Airbus A300F4622R · Passenger/Crew Doors
  > ENTRY DOOR OUTR HANDLE SHUTTER BROKEN REMOVED AND REPLACED L1 DOOR SHUTTER HANDLE IAW AIRBUS CMM 52-11-11. OPS CHECK GOOD.
- [SDR IPXA2025080583394](https://openairdocs.org/sdr/IPXA2025080583394.md): Selector Valve · inoperative · Aug 4, 2025 · N165UP · Airbus A300F4622R · Landing Gear Retraction/Extension System
  > DURING 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
- [SDR IPXA2025041495052](https://openairdocs.org/sdr/IPXA2025041495052.md): Light · no discrepancy · Apr 13, 2025 · N165UP · Airbus A300F4622R · Emergency Lighting
  > EMERGENCY EXIT LIGHTS WILL NOT DISARM OPERATED AND TESTED SUPERNUMERARY AREA EMERGENCY LIGHTS REF AMM 33-51-00/501 LIGHTS GO ON/OFF AS COMMANDED
- [SDR IPXA2025012460562](https://openairdocs.org/sdr/IPXA2025012460562.md): Trim Panel · unsecure · Jan 24, 2025 · N165UP · Airbus A300F4622R · Passenger/Crew Doors
  > TOP 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.
- [SDR IPXA2024122097598](https://openairdocs.org/sdr/IPXA2024122097598.md): Circuit Breaker · faulted · Dec 19, 2024 · N165UP · Airbus A300F4622R · Emergency Lighting
  > EMERGENCY 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.
- [SDR IPXA2024121385564](https://openairdocs.org/sdr/IPXA2024121385564.md): Bottle · low pressure · Dec 13, 2024 · N165UP · Airbus A300F4622R · Emergency Equipment
  > MAIN CABIN DOOR ASSIST BOTTLE PRESSURE READS 900. SERVICED ASSIST BOTTLE IAW AMM 52-10-14.
- [SDR IPXA2024101104287](https://openairdocs.org/sdr/IPXA2024101104287.md): Rib · cracked · Oct 1, 2024 · N165UP · Airbus A300F4622R · Nacelle/Pylon, Frame/Spar/Rib
  > PANEL 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.
- [SDR IPXA2024102334491](https://openairdocs.org/sdr/IPXA2024102334491.md): Stringer · cracked · Sep 27, 2024 · N165UP · Airbus A300F4622R · Ailerons
  > STR 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 -. REVIEWED
- [SDR IPXA2024100908610](https://openairdocs.org/sdr/IPXA2024100908610.md): Arm · deteriorated · Sep 26, 2024 · N165UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW ENTRY DOOR, DOOR ARM W/CIC DETERIORATED; NO DOT. JR-117. APPLIED CIC IAW EO-2780-REQ001. PN 04-002-0153 BATCH 0004291043. REVIEWED
- [SDR IPXA2024092608610](https://openairdocs.org/sdr/IPXA2024092608610.md): Door · deteriorated · Sep 26, 2024 · N165UP · Airbus A300F4622R · Passenger/Crew Doors
  > *SDR FILED OPEN* FAULT: APG-Z800 CREW ENTRY DOOR, DOOR ARM W/CIC DETERIORATED; NO DOT. JR-117. APPROVED
- [SDR IPXA2024100965843](https://openairdocs.org/sdr/IPXA2024100965843.md): Support · cracked · Sep 24, 2024 · N165UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > R/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.
- [SDR IPXA2024100171033](https://openairdocs.org/sdr/IPXA2024100171033.md): Seat Track · broken · Sep 24, 2024 · N165UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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.
- [SDR IPXA2024100168160](https://openairdocs.org/sdr/IPXA2024100168160.md): Web · broken · Sep 24, 2024 · N165UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > BTW 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.
- [SDR IPXA2024100168231](https://openairdocs.org/sdr/IPXA2024100168231.md): Web · broken · Sep 24, 2024 · N165UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > BTW 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.
- [SDR IPXA2024100165567](https://openairdocs.org/sdr/IPXA2024100165567.md): Track · broken · Sep 24, 2024 · N165UP · Airbus A300F4622R · Fuselage Main, Structure
  > R/H MCD FLOORPANEL 242KF C-TRACK AT FR 34 IS BROKEN. 33-022. INSTALLED ADAPTER IAW A300-600 SRM 51-40-21.
- [SDR IPXA2024100168243](https://openairdocs.org/sdr/IPXA2024100168243.md): Web · damaged · Sep 24, 2024 · N165UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MCC, 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.
- [SDR IPXA2024100168184](https://openairdocs.org/sdr/IPXA2024100168184.md): Seat Track · damaged · Sep 24, 2024 · N165UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > BTW 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.
- [SDR IPXA2024101422996](https://openairdocs.org/sdr/IPXA2024101422996.md): Skin · dented · Sep 20, 2024 · N165UP · Airbus A300F4622R · Trailing Edge Flaps
  > RIGHT 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 SEALANT
- [SDR IPXA2024101122648](https://openairdocs.org/sdr/IPXA2024101122648.md): Rib · cracked · Sep 20, 2024 · N165UP · Airbus A300F4622R · Nacelle/Pylon, Frame/Spar/Rib
  > PYLON #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.
- [SDR IPXA2024100100692](https://openairdocs.org/sdr/IPXA2024100100692.md): Floorbeam · bent · Sep 19, 2024 · N165UP · Airbus A300F4622R · Fuselage Main, Floor Beam
  > MAIN 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.
- [SDR IPXA2024100100764](https://openairdocs.org/sdr/IPXA2024100100764.md): Inlet · cracked · Sep 19, 2024 · N165UP · Airbus A300F4622R · Nacelle/Pylon, Main Frame
  > ENG# 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 73-2
- [SDR IPXA2024100291945](https://openairdocs.org/sdr/IPXA2024100291945.md): Floor Panel · cracked · Sep 19, 2024 · N165UP · Airbus A300F4622R · Fuselage Floor Panel
  > PANEL 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.
- [SDR IPXA2024100150355](https://openairdocs.org/sdr/IPXA2024100150355.md): Floor Support · cracked · Sep 17, 2024 · N165UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFT 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.
- [SDR IPXA2024100141579](https://openairdocs.org/sdr/IPXA2024100141579.md): Support Bracket · cracked · Sep 17, 2024 · N165UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFT 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.
- [SDR IPXA2024100141519](https://openairdocs.org/sdr/IPXA2024100141519.md): Support Bracket · cracked · Sep 17, 2024 · N165UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFT 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.
- [SDR IPXA2024100131294](https://openairdocs.org/sdr/IPXA2024100131294.md): Bracket · deteriorated · Sep 16, 2024 · N165UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > FUSELAGE 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 5
- [SDR IPXA2024091373656](https://openairdocs.org/sdr/IPXA2024091373656.md): Light · inoperative · Sep 13, 2024 · N165UP · Airbus A300F4622R · Emergency Lighting
  > EMERGENCY 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.
- [SDR IPXA2024050600755](https://openairdocs.org/sdr/IPXA2024050600755.md): Relay · faulted · May 3, 2024 · N165UP · Airbus A300F4622R · Emergency Lighting
  > OPERATIONAL 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
- [SDR IPXA2024050300755](https://openairdocs.org/sdr/IPXA2024050300755.md): Light · no test · May 3, 2024 · N165UP · Airbus A300F4622R · Emergency Lighting
  > OPEN, OPERATIONAL CHECK OF INTERIOR EMERGENCY LIGHTS FAILED THE AUTOMATIC ACTIVATION IN EVENT OF DC POWER FAILURE CHECK
- [SDR IPXA2024012403951](https://openairdocs.org/sdr/IPXA2024012403951.md): Contact · broken · Jan 24, 2024 · N165UP · Airbus A300F4622R · Door System Wiring
  > CREW 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.
- [SDR IPXA2023122881716](https://openairdocs.org/sdr/IPXA2023122881716.md): Unknown · unknown · Dec 28, 2023 · N165UP · Airbus A300F4622R · Door Warning System
  > DOOR 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.
- [SDR IPXA2023120506560](https://openairdocs.org/sdr/IPXA2023120506560.md): Unknown · unknown · Dec 5, 2023 · N165UP · Airbus A300F4622R · Passenger/Crew Doors
  > DOOR ACTUATOR PRESSURE IS LOW SERVICED DOOR DAMPER WITH HIGH PRESSURE DRY NITROGEN PER AMM 52-10-14. OPS CHECK GOOD.
- [SDR IPXA2023112057964](https://openairdocs.org/sdr/IPXA2023112057964.md): Unknown · unknown · Nov 18, 2023 · N165UP · Airbus A300F4622R · Flight Compartment Windows
  > DURING 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 56-11-11
- [SDR IPXA05769](https://openairdocs.org/sdr/IPXA05769.md): Unknown · unknown · Oct 22, 2023 · N165UP · Airbus A300F4622R · Vertical Stabilizer, Plate/Skin
  > LOWER 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 55-32-11-401
- [SDR IPXA2023041992920](https://openairdocs.org/sdr/IPXA2023041992920.md): Damper · inoperative · Apr 18, 2023 · N165UP · Airbus A300F4622R · Passenger/Crew Doors
  > INSPECTION TYPE:NACREW ENTRY DOOR DAMPER / EMERGENCY OPERATION CYLINDER PRESSURE LOW.CYLINDER SERVICED WITH NITROGEN REF: A300 AMM 52-10-14-0301. NO LEAKS/DEFECTS.
- [SDR IPXA2023010189457](https://openairdocs.org/sdr/IPXA2023010189457.md): Control Switch · faulted · Dec 31, 2022 · N165UP · Airbus A300F4622R · Landing Gear Retraction/Extension System
  > ATB, 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 SY
- [SDR IPXA2022080885030](https://openairdocs.org/sdr/IPXA2022080885030.md): Light · inoperative · Aug 6, 2022 · N165UP · Airbus A300F4622R · Emergency Lighting
  > INSPECTION 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 00
- [SDR IPXA2022032180336](https://openairdocs.org/sdr/IPXA2022032180336.md): Power Supply · unserviceable · Mar 20, 2022 · N165UP · Airbus A300F4622R · Passenger/Crew Doors
  > INSPECTION TYPE:SEGDOES NOT ILLUMINATE RESIDUAL PRESSURE WARNING LIGHTREMOVED AND REPLACED ASPSU IAW AMM 52-73-18-401
- [SDR IPXA2022032080290](https://openairdocs.org/sdr/IPXA2022032080290.md): Stiffener · cracked · Mar 19, 2022 · N165UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > INSPECTION 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-A
- [SDR IPXA2022032080279](https://openairdocs.org/sdr/IPXA2022032080279.md): Shear Plate · cracked · Mar 19, 2022 · N165UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > INSPECTION 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 51-40-21
- [SDR IPXA2022032080278](https://openairdocs.org/sdr/IPXA2022032080278.md): Angle · broken · Mar 19, 2022 · N165UP · Airbus A300F4622R · Leading Edge Devices
  > INSPECTION TYPE:CRH WING KRUEGER FLAP ZONE LH SIDE PANEL SUPPERT IS BROKENFAB REMOVED AND REPLACED ANGLE IAW SRM 57-41-11 AND SRM 51-40-21
- [SDR IPXA2022031880260](https://openairdocs.org/sdr/IPXA2022031880260.md): Angle · cracked · Mar 18, 2022 · N165UP · Airbus A300F4622R · Leading Edge Devices
  > INSPECTION TYPE:A300RH WING KREUGER FLAP MIDDLE ZONE WEB IS CRACKEDREMOVED AND REPLACED ANGLE IAW SRM 51-40-21
- [SDR IPXA2022031880259](https://openairdocs.org/sdr/IPXA2022031880259.md): Angle · cracked · Mar 18, 2022 · N165UP · Airbus A300F4622R · Leading Edge Devices
  > INSPECTION 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 4
- [SDR IPXA2022031880258](https://openairdocs.org/sdr/IPXA2022031880258.md): Angle · cracked · Mar 18, 2022 · N165UP · Airbus A300F4622R · Leading Edge Devices
  > INSPECTION TYPE:A300LH WING KREUGER FLAP MIDDLE ZONE WEB IS CRACKEDREMOVED AND REPLACED ANGLE IAW SRM 51-40-21
- [SDR IPXA2022031780233](https://openairdocs.org/sdr/IPXA2022031780233.md): Fitting · broken · Mar 17, 2022 · N165UP · Airbus A300F4622R · Wing Main, Frame Structure
  > INSPECTION TYPE:SEGLH WING KRUEGER FLAP MIDDLE ZONE HAS METAL PLATE BROKENFABRICATED AND REPLACED PLATE PER SRM 57-41-12 FIG 3 SECTION B-B
- [SDR IPXA2022031580147](https://openairdocs.org/sdr/IPXA2022031580147.md): None · broken · Mar 15, 2022 · N165UP · Airbus A300F4622R · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:SEGE/E COMP FLOOR PANEL 121YF BROKENREPAIR IAW SREO A300-5320-42722F
- [SDR IPXA2021091974035](https://openairdocs.org/sdr/IPXA2021091974035.md): Skin · damaged · Sep 19, 2021 · N165UP · Airbus A300F4622R · Trailing Edge Flaps
  > DAMAGE TO THE UPPER SKIN OF THE FLAP REQUIRES REPAIR. ACCOMPLISH REPAIR IN ACCORDANCE WITH EO A300-5750-81573-B
- [SDR IPXA2021083173362](https://openairdocs.org/sdr/IPXA2021083173362.md): Slide · inoperative · Aug 30, 2021 · N165UP · Airbus A300F4622R · Escape Slide
  > SLIDE 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.

Next page: https://openairdocs.org/aircraft/N165UP/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 = 'N165UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N165UP/reports

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