# Service difficulty reports: N166UP

A list on [N166UP](https://openairdocs.org/aircraft/N166UP.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 · 159 reports

- [SDR IPXA2026100128643](https://openairdocs.org/sdr/IPXA2026100128643.md): Arming Lever · out of adjust · Oct 1, 2026 · N166UP · Airbus A300F4622R · Passenger/Crew Doors
  > AFTER BLOCK IN, USABLE TO DISARM SLIDE. SLIDE ARM/DISARM LEVER UNABLE TO MOVE TO FULL DISARM POSITION. MAIN ENTRY CREW DOOR. ADJUSTED DISARM HANDLE AND OPERATION CHECKS GOOD AT THIS TIME IAW AMM 52-10-30/501.
- [SDR IPXA2026100126338](https://openairdocs.org/sdr/IPXA2026100126338.md): Track · fod · Oct 1, 2026 · N166UP · Airbus A300F4622R · Emergency Equipment
  > CREW ENTRY SLIDE WILL NOT ARM. SLIDE ARMING HANDLE DOES NOT MOVE OUT OF DISARM POSITION. CLEARED DEBRIS FROM TRACK. OPS CHECKED NORMAL PER AMM 25-61-21/401.
- [SDR IPXA2026092372312](https://openairdocs.org/sdr/IPXA2026092372312.md): Screw · loose · Sep 22, 2026 · N166UP · Airbus A300F4622R · Emergency Lighting
  > EXIT SIGN ABOVE THE MAIN CABIN DOOR, NOT SECURE, HANGING DOWN ON THE RIGHT SIDE. FOUND MAIN CABIN DOOR EXIT SIGN FORWARD MOUNTING SCREW VERY LOOSE. SECURED MOUNTING SCREW PER AMM 33-51-13-401. EMERGENCY LIGHT TEST OK PER AMM 33-51-13-401. OK FOR SERVICE
- [SDR IPXA2026073160624](https://openairdocs.org/sdr/IPXA2026073160624.md): Apu · shutdown · Jul 31, 2026 · N166UP · Airbus A300F4622R · APU Core Engine
  > APU EMERGENCY SHUTDOWN DURING NR 1 ENGINE START. REPLACED LUBE/GENERATOR SCAVENGE OIL FILTER AND DRAINED AND FILLED ENGINE OIL PER AMM 49-91-12. OPS CHECK GOOD.
- [SDR IPXA2026062495344](https://openairdocs.org/sdr/IPXA2026062495344.md): Skin Panel · gouged · Jun 16, 2026 · N166UP · Airbus A300F4622R · Wing, Plate/Skin
  > MAJOR REPAIR, LT WING, SLAT NR 1 OUTER EDGE INNER SURFACE CLOSE TO PYLON HAS A SCRATCH BY A FASTERNER UNLOCK OF THE PANEL 512AT. ACCOMPLISHED REPAIR IAW EO-97805-REQ1 AND VT-MAE EA 300-5742-27-A4521, REV. -.
- [SDR IPXA2026031355705](https://openairdocs.org/sdr/IPXA2026031355705.md): Handle · failed · Mar 13, 2026 · N166UP · Airbus A300F4622R · Passenger/Crew Doors
  > L1 DOOR HARD TO CLOSE. BOTH INTERIOR AND EXTERIOR HANDLE STIFF TO OPERATE. BELL CRANK LUG ON COMPENSATION LINK REPLACEMENT. THIS CLEARS MEL 52-11-01-2-4
- [SDR IPXA2026020310141](https://openairdocs.org/sdr/IPXA2026020310141.md): Bottle · empty · Feb 3, 2026 · N166UP · Airbus A300F4622R · Passenger/Crew Doors
  > DURING PRE-FLIGHT MAIN DOOR ENTRY ASSIST GAUGE READING 0. SERVICED DOOR ASSIST BOTTLE AS REQUIRED IAW AMM 52-10-14/301.
- [SDR IPXA2026012802866](https://openairdocs.org/sdr/IPXA2026012802866.md): Processing Unit · faulted · Jan 28, 2026 · N166UP · Airbus A300F4622R · Door Warning System
  > DIVERTED, ON GEAR RETRACTION, ECAM MLG DOORS NOT CLOSED. ? (LEFT MAIN DOOR). TROUBLESHOT IAW TSM 32-61-00/101. FOUND PROXIMITY DETECTOR PROCESSING UNIT FAILING (54GB). REMOVED AND REPLACED PROXIMITY DETECTOR PROCESSING UNIT IAW AMM 32-31-71-401. SYSTEM OP CHE
- [SDR IPXA2025070351374](https://openairdocs.org/sdr/IPXA2025070351374.md): Landing Gear · faulted · Jul 3, 2025 · N166UP · Airbus A300F4622R · Landing Gear Retraction/Extension System
  > ATB, EMERGENCY DECLARED, LANDING GEAR FAILED TO RETRACT AFTER TO RAN ECAM PROCEDURE AND QRH PROC FOR L/G RETRACTIONFAULT. DECLARED EMERGENCY AND RETURNED TO PHL VERIFIED NORMAL EXTENSION AND RETRACTION TEST REF AMM 32-31-00 P BLOCK 501 AND GMM 04-02.
- [SDR IPXA2025032404261](https://openairdocs.org/sdr/IPXA2025032404261.md): Fuel Sys · leaking · Mar 20, 2025 · N166UP · Airbus A300F4622R · Fuel Storage
  > FUEL LEAKING FROM NACA INTAKE LEFT WING OUTBD SURGE TANK. SUSPECT LEAKING IN FLIGHT FOUND ON ARRIVAL. FUELED TANK TO FULL, NO LEAKS AND OPS CHECK NORMAL OF FLOAT.
- [SDR IPXA2024103181448](https://openairdocs.org/sdr/IPXA2024103181448.md): Hydraulic System · faulted · Oct 31, 2024 · N166UP · Airbus A300F4622R · Hydraulic System, Main
  > *EMERGENCY DECLARED* ON DESCENT LOSS OF GREEN HYD SYSTEM ON QUANTITY GAUGE AND ECAM. PERFORMED LOSS OF GREEN HYD PROCEDURE. SYSTEM RESTORED WITH ELECTRIC GREEN PUMPS RESET LANDING GEAR FREE FALL SYSTEM REF AMM 32-33-00/201 NOSE GEAR STEERING AND GEAR DOORS CHE
- [SDR IPXA2025073138042](https://openairdocs.org/sdr/IPXA2025073138042.md): Skin · damaged · Oct 15, 2024 · N166UP · Airbus A300F4622R · Fuselage Main, Plate/Skin
  > MAJOR REPAIR, BEFORE INSTALLATION OF TAIL STAND NOTED AREA AFT OF TAIL STAND BALL IS DAMAGED WITH 2 SCRATCHES AND CREASE. VERIFIED ALL STEPS OF EO-91694- REQ 4 PERMANANT REPAIR COMPLIED WITH.
- [SDR IPXA2024101175609](https://openairdocs.org/sdr/IPXA2024101175609.md): Seal · broken · Oct 11, 2024 · N166UP · Airbus A300F4622R · Leading Edge Devices
  > SLAT JACK SHUTTER SEAL RIB #27 ON RIGHT WING BROKEN REMOVED DAMAGED SHUTTER SEAL. DRILLED AND INSTALLED NEW SHUTTER SEAL IAW SRM 51-40-21.
- [SDR IPXA2024101175550](https://openairdocs.org/sdr/IPXA2024101175550.md): Seal · broken · Oct 11, 2024 · N166UP · Airbus A300F4622R · Leading Edge Devices
  > SLAT JACK SHUTTER SEAL, RIB #10 ON RIGHT WING BROKEN REMOVED AND REPLACED SHUTTER SEAL IAW A300 SRM 51-40-21.
- [SDR IPXA2024072468148](https://openairdocs.org/sdr/IPXA2024072468148.md): Angle · cracked · Jul 23, 2024 · N166UP · Airbus A300F4622R · Wing Miscellaneous Structure
  > FAULT: LH WING, I/B SHROUD BOX LWR T/E, I/B SUPPORT BRACKET IS CRACKED. INSTALLED ANGLE AT LH WING T/E LOWER SKIN WITH MATERIAL P/N: MS20470AD5-11. BTCH: 4222164. IAW A300-600 SRM 51-40-21. AUDIT COMPLETE.
- [SDR IPXA2024073144072](https://openairdocs.org/sdr/IPXA2024073144072.md): Shroud · damaged · Jul 22, 2024 · N166UP · Airbus A300F4622R · Fuselage Structure (General)
  > LH INBD SHROUD BOX LOWER T/E IS DAMAGED.REMOVED BOOM STRAP PANEL SKIN FROM LH WING TRAILING EDGE LOWER SKIN. IAW A300-600 SRM 51-40-21.INSTALLED NEW SKIN I.A.W. A300-600 SRM 51.40.21.
- [SDR IPXA2024080117695](https://openairdocs.org/sdr/IPXA2024080117695.md): Roller · damaged · Jun 25, 2024 · N166UP · Airbus A300F4622R · Passenger/Crew Doors
  > FWD CREW DOOR LIFTING SHAFT ROLLER RH HAS RUBBING MARK DOT 108-105.EVALUATED RUBBING MARK AND FOUND TO BE TYPICAL WEAR. NO MATERIAL LOSS NOTED PER AMM 52-10-00.
- [SDR IPXA2024070217710](https://openairdocs.org/sdr/IPXA2024070217710.md): Structure · worn · Jun 25, 2024 · N166UP · Airbus A300F4622R · Passenger/Crew Doors
  > FWD CREW DOOR INNER TOP SIDE LH HAS RUBBING MARK DOT 108-106. CHECKED LIMITS AFTER REWORK AREA. FOUND IN LIMITS IAW A300-600 SRM 52-11-00-101, POINT 6 DAMAGE CRITERIA AND TABLE 102 ALLOWABLE DAMAGE. MATERIAL REMOVED: 0.001". LESS THAN 10% OF THE MATERIAL TICKN
- [SDR IPXA2024062617695](https://openairdocs.org/sdr/IPXA2024062617695.md): Roller · chafed · Jun 25, 2024 · N166UP · Airbus A300F4622R · Passenger/Crew Doors
  > FWD CREW DOOR LIFTING SHAFT ROLLER RH HAS RUBBING MARK. OPEN
- [SDR IPXA2024062617710](https://openairdocs.org/sdr/IPXA2024062617710.md): Structure · chafed · Jun 25, 2024 · N166UP · Airbus A300F4622R · Passenger/Crew Doors
  > FWD CREW DOOR INNER TOP SIDE LH HAS RUBBING MARK DOT 108-106. OPEN
- [SDR IPXA2024070896004](https://openairdocs.org/sdr/IPXA2024070896004.md): Shield · bent · Jun 21, 2024 · N166UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous Structure
  > PYLON NR 2 RIB 12 SHIELD PANEL EDGE BENT. FABRICATED, LOCATED AND DRILLED NEW #2 PYLON RIB 2 SHIELD PANEL ON TRAVELER# T24/1764214. TREATED AND PRIMED NEW SHIELD PANEL IAW SRM 51-21-10 VERIFIED JOB IN STEP #6. JOB COMPLETE REVIEWED
- [SDR IPXA2024071693907](https://openairdocs.org/sdr/IPXA2024071693907.md): Stringer Splice · cracked · Jun 17, 2024 · N166UP · Airbus A300F4622R · Fuselage Main, Longeron/Stringer
  > FAULT - MAIN DECK, STRINGER SPLICE FITTING AT FR47 AND S-18L CRACKED. INSTALLED SPLICER ON STRG 18, FR 47 IAW A300-600 SRM 51-40-21. KIT P/N 536157A01R00, SEALANT P/N 04-001-0109, BATCH # 0004281040. TREATED AND PRIMED AREA IAW A300-600 SRM 51-21010. PRIMER P/
- [SDR IPXA2024062083075](https://openairdocs.org/sdr/IPXA2024062083075.md): Crossbeam · bent · Jun 16, 2024 · N166UP · Airbus A300F4622R · Fuselage Main, Structure
  > BENT MAIN CARGO DECK FLOOR CROSS BEAM UNDER PANEL 242ZJ AT FR48. DOT 140-009. INSTALLED CROSS BEAM P/N: A5381337800000 BTCH: 4292958 AT FR 48, I.A.W. A300-600 AMM 20.21.12. APPLIED CIC I.A.W. EO-2780-REQ001, P/N: 04-002-0153, BATCH: 4275498.
- [SDR IPXA2024062083071](https://openairdocs.org/sdr/IPXA2024062083071.md): Crossbeam · cracked · Jun 16, 2024 · N166UP · Airbus A300F4622R · Fuselage Main, Structure
  > CRACKED MAIN CARGO DECK FLOOR CROSS BEAM UNDER PANEL 242ZJ AT FR51. INSTALLED OF CROSS BEAM AT FR. 51 I.A.W. A300-600 AMM 20.21.12. APLLIED CIC I.A.W. EO-2780-REQ001.
- [SDR IPXA2024062083086](https://openairdocs.org/sdr/IPXA2024062083086.md): Crossbeam · bent · Jun 16, 2024 · N166UP · Airbus A300F4622R · Fuselage Main, Structure
  > BENT MAIN CARGO DECK FLOOR CROSS BEAM UNDER PANEL 242ZJ AT FR49. DOT 140-010. INSTALLED OF CROSS BEAM P/N: A5381337800000 BTCH: 4293002, I.A.W. A300-600 AMM 20.21.12. APPLIED CIC I.A.W. EO-2780-REQ001, P/N:04-002-0153, BATCH: 4275498.
- [SDR IPXA2024062083088](https://openairdocs.org/sdr/IPXA2024062083088.md): Floorbeam · bent · Jun 16, 2024 · N166UP · Airbus A300F4622R · Fuselage Main, Floor Beam
  > BENT MAIN CARGO DECK FLOOR CROSS BEAM UNDER PANEL 242ZJ AT FR50. DOT 140-011.REMOVED CROSS BEAM UNDER PANEL 242ZJ AT FR50 I.A.W. A300-600 AMM 20.21.12.INSTALLED CROSS BEAM P/N A5381337800000 BTCH 4293011 IAW A300-600 AMM 20-21-12.
- [SDR IPXA2024071973345](https://openairdocs.org/sdr/IPXA2024071973345.md): Frame · corroded · Jun 15, 2024 · N166UP · Airbus A300F4622R · Fuselage Main, Frame
  > CORROSION FOUND IN THE E&E BAY LH FR 11A AT FLOOR LEVEL ACCOMPLISHED REPAIR PER EO-90796-REQ1 AND EA 300-5312-27-A3632 REV.
- [SDR IPXA2024062471773](https://openairdocs.org/sdr/IPXA2024062471773.md): Floor Panel · cracked · Jun 15, 2024 · N166UP · Airbus A300F4622R · Fuselage Floor Panel
  > FLOOR PANEL 131RG IS DAMAGED. FABRICATED FLOOR PANEL 131RG IAW SREO 16407-REQ002.
- [SDR IPXA2024070871766](https://openairdocs.org/sdr/IPXA2024070871766.md): Floor Panel · cracked · Jun 15, 2024 · N166UP · Airbus A300F4622R · Fuselage Floor Panel
  > FLOOR PANEL 132PG IS DAMAGED FABRICATED FLOOR PANEL 132PG IAW SREO 16407-REQ002. INSPECTED FABRICATED FLOOR PANEL 132PG PER S.R.E.O. JOB COMPLETED.
- [SDR IPXA2024062471721](https://openairdocs.org/sdr/IPXA2024062471721.md): Floor Panel · cracked · Jun 15, 2024 · N166UP · Airbus A300F4622R · Fuselage Floor Panel
  > FLOOR PANEL 152TF IS DAMAGED FABRICATED FLOOR PANEL 152TF IAW SREO 16407-REQ002. INSPECTED FABRICATED FLOOR PANEL 152TF PER SREO JOB COMPLETED. REVIEWED
- [SDR IPXA2024070871746](https://openairdocs.org/sdr/IPXA2024070871746.md): Floor Panel · cracked · Jun 15, 2024 · N166UP · Airbus A300F4622R · Fuselage Floor Panel
  > FLOOR PANEL 132AH IS DAMAGED FABRICATED FLOOR PANEL 132AH IAW SREO 16407-REQ002. INSPECTED FABRICATED FLOOR PANEL 13AH PER S.REO JOB COMPLETED. REVIEWED
- [SDR IPXA2024070300970](https://openairdocs.org/sdr/IPXA2024070300970.md): Fitting · cracked · Jun 11, 2024 · N166UP · Airbus A300F4622R · Wing Main, Frame Structure
  > CRACK FOUND IN FIRST LAYER OF L/W FR40 LOWER RADIUS HOLE. INSTALLED FILLER AND COVER PLATE AT FR40 LH LOWER RADIUS HOLE. WITH BOLT P/N: EN6115V8-24. BTCH: 4297160. NUT P/N: NAS1726-8E. BTCH: 4249205. BOLT P/N: EN6115V5-24, BTCH: 4274797. NUT P/N: NAS1726-5E. B
- [SDR IPXA2024070164066](https://openairdocs.org/sdr/IPXA2024070164066.md): Slat Track · damaged · Jun 8, 2024 · N166UP · Airbus A300F4622R · Leading Edge Devices
  > RH WING LE SLAT PANEL LOWER TRACK 10 HAS MISSING MATERIAL DOT 108-23. INSTALLED PACKER OF RH WING TRACK 10, I.A.W. A300-600 SRM 51.40.21. APPLIIED FINISH PAINT TO FASTENERS P/N: ECL-G-101, BATCH: 4266626, CUP: 02-012-176 I.A.W. A300-600 SRM. 51.23.10.
- [SDR IPXA2024061461891](https://openairdocs.org/sdr/IPXA2024061461891.md): Support Angle · cracked · Jun 8, 2024 · N166UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > FWD CARGO COMPT. DOOR CUTOUT, FR20A LOWER AREA WITH PROFILE ANGLE DAMAGED & LITTLE SPLICE PLATE CRACKED. INSTALLED NEW PROFILE ANGLE IAW SRM 51-40-21.
- [SDR IPXA2024062245622](https://openairdocs.org/sdr/IPXA2024062245622.md): Adapter · broken · Jun 7, 2024 · N166UP · Airbus A300F4622R · Fuselage Main, Attach Fittings
  > MAIN DECK CLS ADAPTER AT FR 33 BETWEEN SEAT TRACK Y2462 AND Y1959 IS BROKEN DOT 06999-08. INSTALLED ADAPTER IAW A300 SRM 51-40-21 PARAGRAPH 7.
- [SDR IPXA2024062245618](https://openairdocs.org/sdr/IPXA2024062245618.md): Adapter · broken · Jun 7, 2024 · N166UP · Airbus A300F4622R · Fuselage Main, Attach Fittings
  > MAIN DECK CLS ADAPTER AT FR 34 BETWEEN SEAT TRACK Y2462 AND Y1959 IS BROKEN DOT 06999-09. INSTALLED ADAPTER IAW SRM 51-40-21 PARAGRAPH 7.
- [SDR IPXA2024072331717](https://openairdocs.org/sdr/IPXA2024072331717.md): Frame · cracked · Jun 6, 2024 · N166UP · Airbus A300F4622R · Fuselage Main, Frame
  > CRACKS FOUND IN ALL 3 HOLES ON FR40 RH UPPER TENSION BOLTS. COMPLIED WITH FINAL EO-90798-REQ1 AND VTMAE FINAL EA A300-5710-27-A3627 REV-. REVIEWED
- [SDR IPXA2024072633742](https://openairdocs.org/sdr/IPXA2024072633742.md): Seat Track · corroded · Jun 6, 2024 · N166UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK SEAT TRACK AT Y0 AT FR 80 HAS CORROSION DOT 06999-04 INSTALLED NEW SEAT TRACK SECTION 02 EA ANGLES AND 02 EA SPLICES ON MAIN DECK "Y0" FR 80 IAW A300-600 SRM 53-10-16
- [SDR IPXA2024072633763](https://openairdocs.org/sdr/IPXA2024072633763.md): Seat Track · corroded · Jun 6, 2024 · N166UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK SEAT TRACK R/H -Y450 AT FR 80 HAS CORROSION. INSTALLED NEW TRACK AND 2EA SPLICES IAW A300 SRM 51-40-21 AND 53-10-16 FIG 201B.
- [SDR IPXA2024070833150](https://openairdocs.org/sdr/IPXA2024070833150.md): Tension Tie · cracked · Jun 6, 2024 · N166UP · Airbus A300F4622R · Fuselage Main, Frame
  > CRACK FOUND IN TOP HOLE ON FR40 LH UPPER TENSION. INSTALLED NEW BUSHINGS (3EA) IN TOP HOLE ON FR40 L/H UPPER TENSION IAW A300-600 SRM 51-40-49-0001.
- [SDR IPXA2024061533705](https://openairdocs.org/sdr/IPXA2024061533705.md): Seat Track · corroded · Jun 6, 2024 · N166UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK SEAT TRACK L/H Y450 AT FR 80 HAS CORROSION. NSTALLED NEW SEAT TRACK SECTION, 02 EA ANGLES AND 02 EA SPLICES OF MAIN DECK L/H Y450 AT FR80 IAW SRM 53-10-16. ACCOMPLISH PERMANENT REPAIR PER SRM REV 40, 53-10-16-201, PARAGRAPH 4, FIGURE 201B.
- [SDR IPXA2024061533763](https://openairdocs.org/sdr/IPXA2024061533763.md): Seat Track · corroded · Jun 6, 2024 · N166UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK SEAT TRACK R/H -Y450 AT FR 80 HAS CORROSION DOT 06999-05 REJECTED, SUBTASKS INCOMPLETE. OPEN
- [SDR IPXA2024072614664](https://openairdocs.org/sdr/IPXA2024072614664.md): Frame Splice · cracked · Jun 5, 2024 · N166UP · Airbus A300F4622R · Fuselage Main, Frame
  > DAMAGE FOUND IN HOLES (B, E, F, L, M, & N) TWO CRACKS FOUND IN HOLE (L) ON FR47 RH SPLICE FITTINGS. AREAS MARKED IN RED. COMPLIED WITH EO-90784-REQ1 AND VTMAE FINAL EA 300-5315-27-A3624 REV. REVIEWED
- [SDR IPXA2024072613801](https://openairdocs.org/sdr/IPXA2024072613801.md): Static Wick · corroded · Jun 5, 2024 · N166UP · Airbus A300F4622R · Pitot/Static System
  > *SUPPLEMENTAL SDR* FAULT STR Z500 LEFT WING OUTBOARD FLAP STATIC WICK BASE IS CORRODED DOT 72-009 ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-90896-REQ1 AND VT-MAE EA 300-5750-27-A3638, REV. -.
- [SDR IPXA2024071913801](https://openairdocs.org/sdr/IPXA2024071913801.md): Static Wick · corroded · Jun 5, 2024 · N166UP · Airbus A300F4622R · Pitot/Static System
  > LEFT WING OUTBOARD FLAP STATIC WICK BASE IS CORRODED DOT 72-009 VERIFIED STEP # 72 C/W. OPEN
- [SDR CNF52024031500225](https://openairdocs.org/sdr/CNF52024031500225.md): None · none · Mar 15, 2024 · N166UP · Airbus A300F4622R · Standard Practices/Structures
  > MAINTENANCE AND REPAIR PROBLEM: AFTER A DOUBLE CHECK CONTROL ONE AXLE PART CADMMIUM PROCESS REPAIR, THE POST-PLATE BAKE OVEN TIME AFTER ELECROLYTIC PLATING OPERATION RECORDED A TIME OF 14 HOURS INSTEAD OF 23 HOURS.
- [SDR IPXA2024030610729](https://openairdocs.org/sdr/IPXA2024030610729.md): Rvdt · faulted · Mar 5, 2024 · N166UP · Airbus A300F4622R · Engine Thrust Reverser
  > PASSING THROUGH FL340 RVR UNLOCK #2 LIGHT CAME ON. IT WAS FAIRLY DIM. WE DID A LIGHT TEST AND ECAM DISPLAYED THAT THE #2 REVERSER WAS UNLOCKED, WE TESTED THE LIGHT SEVERAL TIMES AND EACH TIME THE. REMOVED AND REPLACED #2 ENG RVDT AND STOW/DEPLOY SWITCH ASSEMBL
- [SDR IPXA2024013025213](https://openairdocs.org/sdr/IPXA2024013025213.md): Landing Gear · malfunctioned · Jan 25, 2024 · N166UP · Airbus A300F4622R · Landing Gear Retraction/Extension System
  > ON TAKEOFF GEAR FAILED TO RETRACT. SWITCHED TO SYS 2 ON POSITION DETECTION SYSTEM AND GEAR RETRACTED NORMALLY. VERIFIED GEAR SWING IAW MM-32-31-00 PAGE BLOCK 501,SYS OPS NORMAL.
- [SDR IPXA2023011769955](https://openairdocs.org/sdr/IPXA2023011769955.md): Skin · dented · Jan 16, 2023 · N166UP · Airbus A300F4622R · Trailing Edge Flaps
  > MAJOR REPAIR, LEFT WING INBOARD FLAP LOWER SURFACE SKIN DENTED AT TRAILING EDGE REPAIRED IAW E.O. A300-5750-84804-B.
- [SDR IPXA2022102487435](https://openairdocs.org/sdr/IPXA2022102487435.md): Connector · dirty · Oct 21, 2022 · N166UP · Airbus A300F4622R · Emergency Equipment
  > PUSH TO TEST BUTTON FOR ESCAPE SLIDE STICKS IN THE DOWN POSITION TEMPORARILY WHEN PRESSEDCLEANED ELECTRICAL CONNECTION OF TEST BUTTON IAW ESPM 20-55-00 OPS CHECK GOOD

Next page: https://openairdocs.org/aircraft/N166UP/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 = 'N166UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N166UP/reports

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