# Service difficulty reports: Airbus A330-243F

A list on [Airbus A330-243F](https://openairdocs.org/model/airbus-a330-243f.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 67 reports

- [SDR TAMF20260912062](https://openairdocs.org/sdr/TAMF20260912062.md): Oil Tube · chafed · Sep 11, 2026 · N330QT · Airbus A330243F · Turbine Engine Oil System
  > DURING CRUISE ON THE MIA - CWB ROUTE, THE AIRCRAFT EXPERIENCED EXCESSIVE OIL CONSUMPTION ON ENGINE 2. DUE TO THE ABNORMAL OIL CONSUMPTION, THE FLIGHT CREW DECIDED TO DIVERT AND LAND AT MDE STATION FOR FURTHER INSPECTION AND MAINTENANCE ACTION. DURING THE INSP
- [SDR TAMF20260913061](https://openairdocs.org/sdr/TAMF20260913061.md): Aoa · out of limits · Sep 10, 2026 · N334QT · Airbus A330243F · Stall Warning System
  > AIRCRAFT EXPERIENCED AN ECAM NAV AOA EXCEEDED MESSAGE ASSOCIATED WITH TURBULENCE. AIRBUS CONFIRMED LOADS EXCEEDING THE AIRCRAFT DESIGN ENVELOPE. REQUIRED INSPECTIONS WERE PERFORMED AND AIRBUS AUTHORIZED AIRCRAFT RELEASE THROUGH RDAF 81873879/017/2026 ISSUE A
- [SDR TAMF20260623056](https://openairdocs.org/sdr/TAMF20260623056.md): Actuator · cracked · Jun 22, 2026 · N336QT · Airbus A330243F · Landing Gear Actuator
  > AIRCRAFT DEPARTED MIA AND, DURING CLIMB, THE HYD G SYS LOW PRESS MESSAGE WAS DISPLAYED. AS A PRECAUTIONARY MEASURE, THE FLIGHT CREW DECIDED TO RETURN TO MIA. AFTER AIRCRAFT N336QT RETURNED TO MIA, A HYDRAULIC FLUID LEAK WAS FOUND AT THE LH MAIN LANDING GEAR D
- [SDR TAMF20250910053](https://openairdocs.org/sdr/TAMF20250910053.md): Engine · bird ingestion · Sep 8, 2025 · N330QT · Airbus A330243F · Engine (Turbine/Turboprop)
  > DURING THE PREFLIGHT WALKAROUND INSPECTION, EVIDENCE OF A BIRD STRIKE WAS IDENTIFIED ON ENGINE 1. DURING THE BORESCOPE INSPECTION OF ENGINE 1, DAMAGE WAS IDENTIFIED ON STAGE 1 OF THE INTERMEDIATE PRESSURE (IP) COMPRESSOR. THE REPLACEMENT OF ENGINE 1 IS CURREN
- [SDR TAMF20250523051](https://openairdocs.org/sdr/TAMF20250523051.md): Smoke Detector · faulted · May 20, 2025 · N336QT · Airbus A330243F · Smoke Detection
  > DURING THE CRUISE PHASE, AIRCRAFT N336QT DISPLAYED THE WARNING MESSAGE "CAB PR EXCESS CAB ALT," ACCOMPANIED BY A LOSS OF CABIN PRESSURIZATION. IN RESPONSE TO THIS SITUATION, THE CREW DECIDED TO RETURN TO THE DEPARTURE STATION, MIA. DURING THE FAULT ISOLATION P
- [SDR TAMF20250504050](https://openairdocs.org/sdr/TAMF20250504050.md): Drain · leaking · May 3, 2025 · N334QT · Airbus A330243F · Turbine Engine Oil System
  > AIRCRAFT N334QT DEPARTED FROM MDE STATION, AND DURING CLIMB, LOW OIL QUANTITY AND LOW OIL PRESSURE INDICATIONS WERE OBSERVED FOR ENGINE NUMBER 1. AS A RESULT, THE FLIGHT CREW PERFORMED AN IN-FLIGHT SHUTDOWN OF THE AFFECTED ENGINE AND RETURNED TO MDE. DURING M
- [SDR TAMF20250424049](https://openairdocs.org/sdr/TAMF20250424049.md): Acm · failed · Apr 22, 2025 · N336QT · Airbus A330243F · Cabin Cooling System
  > AFTER DEPARTING FROM MIA STATION AND DURING THE CLIMB, AIRCRAFT N336QT EXPERIENCED SMOKE ON THE LEFT SIDE OF THE COCKPIT, ACCOMPANIED BY THE 'AIR PACK 1 REGUL FAULT' INDICATION. THE CREW IMMEDIATELY DECIDED TO RETURN TO MIA STATION. DURING THE MAINTENANCE INS
- [SDR HALA20250421112](https://openairdocs.org/sdr/HALA20250421112.md): Valve · inoperative · Apr 20, 2025 · N5897K · Airbus A330243F · Pneumatic Distribution System
  > ETOPS-MULTIPLE TIMES ON DESCENT AND AFTER LANDING ECAM: AIR ENG 1 HPV NOT OPEN. REMOVED AND REPLACED ENG 1 HPV IAW 36-11-51. OPS CHECK AND LEAK CHECK GOOD.
- [SDR TAMF20250103048](https://openairdocs.org/sdr/TAMF20250103048.md): Warning Message · unknown · Feb 2, 2025 · N334QT · Airbus A330243F · Cabin Pressure Control System
  > AFTER TAKEOFF, A "VENT BLOWING FAULT" WAS DETECTED, AND THE AIRCRAFT EXPERIENCED A CABIN PRESSURIZATION ISSUE. THE CREW DECIDED TO MAINTAIN ALTITUDE, DURING WHICH THE PRESSURIZATION WAS RESTORED, THEN THE FLIGHT PROCEEDED TO MAO STATION. UPON LANDING, MAINTENA
- [SDR TAMF20241203047](https://openairdocs.org/sdr/TAMF20241203047.md): Acm · faulted · Nov 30, 2024 · N332QT · Airbus A330243F · Cabin Cooling System
  > DURING THE FLIGHT BETWEEN MIA AND MAO AIRPORTS AT CRUISE ALTITUDE, THE “AIR PACK 1 REGUL FAULT” OCCURRED, (THE PACK 2 WAS DEFERRED). PACK 1 WAS RECOVERED, BUT THE AIRCRAFT WAS DIVERTED TO THE BOG STATION BY COMPANY DECISION, AS IT IS ONE OF TAMPA CARGO'S MAIN
- [SDR TAMF202406054046](https://openairdocs.org/sdr/TAMF202406054046.md): None · none · May 31, 2024 · N331QT · Airbus A330243F · Standard Practices/Structures
  > DURING THE AIRCRAFT LOADING PROCEDURE THE MAIN DECK CARGO COMPARTMENT HAS BEEN OVERLOADED AT POSITION A BY 1106KG AND THAT 2 FLIGHTS HAVE BEEN PERFORMED SINCE THE EVENT. STRUCTURAL INSPECTIONS WERE PERFORMED IN ACCORDANCE WITH AIRBUS REPAIR AND DESIGN APPROVA
- [SDR HALA20240429119](https://openairdocs.org/sdr/HALA20240429119.md): Apu · shutdown · Apr 27, 2024 · N4649K · Airbus A330243F · APU Core Engine
  > APU IFSD-DMI# 533711 APU AUTOSHUT DOWN ( APU SYSTEM (ETOPS 120 RESTRICTED)) RECEIVED NO FLAME FUEL SUPPLY /FCU (59KFA) /FLOW DIVIDER ASSY 59KF25 WITH FAULT CODE 155 T/S 28-22-00 FOUND AIR IN FUEL LINE BLEED PER AMM 28-22-00 OPS CHECK GOOD STARTED APU 3 TIMES
- [SDR TAMF20240415045](https://openairdocs.org/sdr/TAMF20240415045.md): Pump · low pressure · Apr 13, 2024 · N331QT · Airbus A330243F · Hydraulic Pump (Electric/Engine), Main
  > REJECTED TAKE OFF BY HYD ENGINE PUMP LOW PRESSURE. THE ENGINE 2 GREEN HYD PUMP WAS REMOVED AND REPLACED IN ACCORDANCE WITH AIRBUS AMM 29-11-51-000-805-A AND AMM 29-11-51-400-805-A. HYD PUMP DATA: PN ON: 3022053-001, SN ON: G1440121 PN OFF: 3022053-001, SN O
- [SDR TAMF20240320044](https://openairdocs.org/sdr/TAMF20240320044.md): Tire · deflated · Mar 19, 2024 · N330QT · Airbus A330243F · Tire
  > THE AIRCRAFT LANDED WITH A FLAT TIRE, (THE MAIN LANDING GEAR WHEEL ASSY NO 5). THE MAIN LANDING GEAR WHEEL ASSY NO 5 AND 6 WERE REPLACED. WHEEL ASSY NO 5 PN/ OFF 3-1546, PN/ 0N 3-1546,
- [SDR TAMF2024032019043](https://openairdocs.org/sdr/TAMF2024032019043.md): Windshield · cracked · Mar 19, 2024 · N335QT · Airbus A330243F · Flight Compartment Windows
  > DURING DESCENT HAIL CONDITION WAS FOUND CAUSING DAMAGE TO THE TWO WINDSHIELD. THE INSPECTION OF THE AIRCRAFT AND THE REPLACEMENT OF THE TWO FRONT WINDOWS IS IN PROGRESS.
- [SDR TAMF20231227041](https://openairdocs.org/sdr/TAMF20231227041.md): Unknown · unknown · Dec 26, 2023 · N332QT · Airbus A330243F · Service Doors
  > AFTER LEAVING THE MIA STATION, IN THE TRANSITION BETWEEN THE CLIMB AND CRUISE PHASE, THE MESSAGE "R DOOR FWD CABIN" WAS DISPLAYED ON THE ECAM DISPLAY ACCOMPANIED BY AN INCREASE IN CABIN ALTITUDE. THE FLIGHT CREW DECIDES TO RETURN TO THE MIA STATION. THE RH FW
- [SDR TAMF20231211040](https://openairdocs.org/sdr/TAMF20231211040.md): Hose · leaking · Dec 11, 2023 · N331QT · Airbus A330243F · Hydraulic System, Main
  > DURING FINAL APPROACH THE “HYD GREEN RESERVOIR LOW LEVEL” MESSAGE WAS SHOWN. DURING MAINTENANCE INSPECTION A HYDRAULIC LEAKAGE WAS FOUND IN THE HOSE OF THE LEFT MAIN LANDING GEAR ACTUATOR.
- [SDR TAMF20231109039](https://openairdocs.org/sdr/TAMF20231109039.md): Radome · dented · Nov 9, 2023 · N330QT · Airbus A330243F · Aerodynamic Fairings
  > DURING WALK AROUND FOUND BIRD STRIKE ON RADOME. THE RADOME ASSY WAS REPLACED. RADOME ASSY PN/ OFF F53132110000, PN/ 0N F53132110000, SN/ OFF RADTA3519, SN/ ON RADTA3030.
- [SDR TAMF20230905037](https://openairdocs.org/sdr/TAMF20230905037.md): Unknown · unknown · Sep 2, 2023 · N332QT · Airbus A330243F · Fuselage Structure (General)
  > THE FORWARD LOWER CARGO COMPARTMENT WAS OVERLOAD IN 989 KG DUE TO A CARGO PALLET WAS MOVED FROM POSITION 12L TO 11 DURING FLIGHT. THE QUERY WITH THE AIRCRAFT MANUFACTURER IS IN PROGRESS TO ESTABLISH THE CAUSES, ACTIONS AND INSPECTIONS REQUIRED. (AIRBUS DOSSIE
- [SDR TAMF20230803036](https://openairdocs.org/sdr/TAMF20230803036.md): Unknown · unknown · Aug 1, 2023 · N335QT · Airbus A330243F · Fuselage Structure (General)
  > DURING THE AIRCRAFT LOADING PROCEDURE FOR FLIGHT NO. 4052 VCP BRAZIL – BOG COLOMBIA, THE AMOUNT OF WEIGHT (1452 KG) WAS EXCEEDED IN THE CARGO POSITION (CER) AND 6 FLIGHTS WERE PERFORMED AFTER THIS EVENT. THE AIRCRAFT MANUFACTURER IS PERFORMING THE ANALYSIS OF
- [SDR TAMF20230620035](https://openairdocs.org/sdr/TAMF20230620035.md): Engine · leaking · Jun 18, 2023 · N334QT · Airbus A330243F · Engine (Turbine/Turboprop)
  > ENG #2 WAS FOUND WITH A FUEL LEAK IN THE OUTSIDE AREA ON THE LEFT SIDE OF THE IP COMPRESSOR. THE ENGINE FUEL TUBE P/N FK24001 AND OIL TUBE P/N FW15740 WERE REMOVED AND REPLACED IN ACCORDANCE WITH AIRBUS AIRCRAFT MAITENENCE MANUALS AMM 75-33-51-400-801-A & 72-
- [SDR TAMF20230607034](https://openairdocs.org/sdr/TAMF20230607034.md): Unknown · unknown · Jun 3, 2023 · N335QT · Airbus A330243F · Fuselage Structure (General)
  > DURING AIRCRAFT UNLOADING PROCEDURE THE AFT CARGO DOOR CUT OUT FRAME WAS HIT WITH A LOADER EQUIPMENT, (FRAME 59A BETWEEN STRINGERS 36RH & 40RH), (FRAME 65 BETWEEN STRINGERS 35RH & 38RH). IN ACCORDANCE WITH THE JOB INSTRUCTION CARD NUMBER JIC 332-53-01367 STRUC
- [SDR TAMF20230514033](https://openairdocs.org/sdr/TAMF20230514033.md): Slat · dented · May 12, 2023 · N336QT · Airbus A330243F · Leading Edge Devices
  > DURING TRANSIT INSPECTION AT BOG STATION A DENT WAS FOUND ON RH WING SLAT NUMBER 3. PERFORMED TEMPORARY REPAIR IN ACCORDANCE WITH AIRBUS A330 SRM TASK 57-40-00-283-005.
- [SDR TAMF20230406032](https://openairdocs.org/sdr/TAMF20230406032.md): Unknown · unknown · Apr 3, 2023 · N334QT · Airbus A330243F · Fuselage Structure (General)
  > DURING THE AIRCRAFT UNLOADING PROCEDURE, A DAMAGE WAS FOUND ON AFT CARGO DOOR CUT OUT FRAME, (65 STRINGER, BTW 42-43 RH FR). IN ACCORDANCE WITH AIRBUS STRUCTURAL REPAIR MANUAL TASK 51-11-00 ITEM 2.B.(3) CATEGORY 4 TABLE 1, THE DMAGE IS IT IS WITHIN THE ALLOWA
- [SDR TAMF20230210031](https://openairdocs.org/sdr/TAMF20230210031.md): Computer · fault message · Feb 8, 2023 · N331QT · Airbus A330243F · Flight Control System
  > AFTER TAKE-OFF FROM THE AIRPORT (PTY), THE FAULT MESSAGE “F/CTL SLAT SYS 2 FAULT” WAS SHOWN IN THE ECAM DISPLAY AND BY FACILITIES OF MAINTENANCE AND PARTS STOCK IT WAS DECIDED TO DIRECT THE AIRCRAFT TO THE MAIN BASE (MDE) AND NOT (LIM) AS IT WAS SCHEDULED. TH
- [SDR TAMF20221107030](https://openairdocs.org/sdr/TAMF20221107030.md): Engine · secondary damage · Nov 6, 2022 · N336Q · Airbus A330243F · Engine (Turbine/Turboprop)
  > DURING WALKAROUND FOUND BIRD STRIKE ON ENG #2. INSPECTION AFTER ENGINE BIRD STRIKE WAS PERFORMED IN ACCORDANCE WITH AIRBUS AMM DOCUMENT 05-51-19-200-801-A
- [SDR TAMF20221104029](https://openairdocs.org/sdr/TAMF20221104029.md): None · none · Nov 1, 2022 · N334QT · Airbus A330243F · Fuselage Structure (General)
  > DURING THE AIRCRAFT UNLOADING PROCEDURE, A GOUGE WAS FOUND ON FRAME 20 RH SIDE OF THE FWD CARGO DOOR CUT OUT. IN ACCORDANCE WITH AIRBUS STRUCTURAL REPAIR MANUAL TASK MANUAL 53-21-11-283-006A TEMPORARY REPAIR WAS PERFORMED.
- [SDR TAMF20221102028](https://openairdocs.org/sdr/TAMF20221102028.md): Flap · perforated · Oct 31, 2022 · N332QT · Airbus A330243F · Trailing Edge Flaps
  > A CARGO PALLET THAT WAS ON THE RAMP (KMIA) MOVED DUE TO THE JET BLAST EFFECT OF AN AIRCRAFT THAT WAS PARKING AND HIT THE FLAP (PN/ F5757500500900, SN/ TB 11429.) OF THE N332QT AIRCRAFT THAT WAS IN LOADING PROCESS. IN ACCORDANCE WITH AIRBUS TECHNICAL DOCUMENT
- [SDR TAMF20221005027](https://openairdocs.org/sdr/TAMF20221005027.md): Windshield · cracked · Oct 2, 2022 · N331QT · Airbus A330243F · Window/Windshield System
  > DURING DESCENT PHASE A BIRD STRIKE WAS PRESENTED ON LH WINDSHIELD. THE WINDSHIELD IS IN REPLACEMENT PROCESS.
- [SDR TAMF20220914026](https://openairdocs.org/sdr/TAMF20220914026.md): None · perforated · Sep 11, 2022 · N332QT · Airbus A330243F · Fuselage Structure (General)
  > DURING CLIMB PHASE, A BIRD STRIKE IN THE NOSE RADOME WAS PRESENTED. DURING INSPECTION THE NOSE RADOME AND THE WEATHER RADAR ANTENNA WAS FOUND DAMAGED. THE NOSE RADOME AND THE WEATHER RADAR ANTENNA WERE REMOVED AND REPLACED IN ACCORDANCE WITH AIRBUS AMM 34-41-
- [SDR TAMF20220901025](https://openairdocs.org/sdr/TAMF20220901025.md): Hydraulic Line · leaking · Aug 30, 2022 · N332QT · Airbus A330243F · Hydraulic Power System
  > DURING THE APPROACH "HYD G RSVR LO LVL" DISPLAYED ON ECAM AFTER LANDING GEAR DOWN SELECTION. IN THE GROUND INSPECTION A HYDRAULIC LEAK WAS FOUND THROUGH THE FLEXIBLE LINE PN/ 29-2105216-00 OF THE LEFT MAIN GEAR. THE FLEXIBLE LINE IS IN THE ACQUISITION PROCESS.
- [SDR TAMF20220811024](https://openairdocs.org/sdr/TAMF20220811024.md): Heat Exchanger · leaking · Aug 9, 2022 · N332QT · Airbus A330243F · Engine Oil System (Airframe Furnished)
  > DURING THE FLIGHT BETWEEN MIA (MIAMI) AND MVD (MONTEVIDEO) THE CREW CONTACTS THE MCC (MAINTENANCE CONTROL CENTER) TO REPORT THAT THE RIGHT ENGINE HAS AN ABNORMAL OIL CONSUMPTION (LOW QUANTITY) AND AS A PRECAUTION IT IS DECITED TO DIVERT THE AIRCRAFT TOWARDS TH
- [SDR TAMF20220721023](https://openairdocs.org/sdr/TAMF20220721023.md): Door · cracked · Jul 20, 2022 · N336QT · Airbus A330243F · Fuselage Structure (General)
  > DURING AIRCRAFT LOADING PROCEDURE, THE AFT CARGO DOOR ANGLE PN/ F5347534721000 IN THE FUSELAGE WAS HIT. ACTION TAKEN: PERFORMED TEMPORARY REPAIR IN ACCORDANCE WITH AIRBUS SRM 53-41-29-300-001
- [SDR TAMF20220601022](https://openairdocs.org/sdr/TAMF20220601022.md): None · leaking · May 29, 2022 · N335QT · Airbus A330243F · Aircraft Fuel System
  > DURING REFUELING PROCEDURE, A FUEL LEAK WAS FOUND TRUOUGH THE CWB “CENTER WING BOX” DRAIN LINE. DURING CWB “CENTER WING BOX” INSPECTION FUEL LEAKAGE WAS NOTED ON FUEL INLET VALVES (5603QA1 PN/ B97H63-628) AND (5603QA2 PN/ B97H63-628). ACTION TAKEN: IN ACCORD
- [SDR TAMF20220426021](https://openairdocs.org/sdr/TAMF20220426021.md): None · none · Apr 23, 2022 · N330QT · Airbus A330243F · Powerplant System
  > DURING T/O THRUST SET, ENG THRUST LOSS ABNORM BLEED OR PACK APPEARED ON ECAM DISPLAY, THE PILOT DECIDED TO INTERRUPT THE TAKEOFF AND AFTER PERFORM THE CABIN PROCEDURES, THE FAILURE DISAPPEARED AND FINALLY THE TAKE OFF WAS NORMAL. AS A MAINTENANCE ACTION, AT T
- [SDR TAMF20220301020](https://openairdocs.org/sdr/TAMF20220301020.md): Wheel · deflated · Feb 28, 2022 · N335QT · Airbus A330243F · Nose/Tail Landing Gear
  > DURING TOWING OF THE N335QT AIRCRAFT THE TOW BAR CAME LOOSE AND HIT THE NOSE GEAR AND ITS RIGHT WHEEL.IN ACCORDANCE WITH AIRBUS AMM 32-21-00-220-814-A DETAILED INSPECTION OF NLG, SLIDING TUBE, EXTERNAL SURFACE WERE PERFORMED. GVI WAS PERFORMED TO NLG, NO LEAKS
- [SDR TAMF20220112019](https://openairdocs.org/sdr/TAMF20220112019.md): Slat · dented · Jan 9, 2022 · N336QT · Airbus A330243F · Leading Edge Devices
  > DURING THE “48 HOURS” AIRCRAFT SERVICE CHECK, A DENT WAS FOUND ON LH WING SLAT NUMBER 4. PERFORMED TEMPORARY REPAIR IN ACCORDANCE WITH AIRBUS RDAF REF. 81011880/020 AND AIRBUS A330 SRM TASK 57-40-00-283-005
- [SDR TAMF20211227018](https://openairdocs.org/sdr/TAMF20211227018.md): Engine · degraded · Dec 24, 2021 · N336QT · Airbus A330243F · Powerplant System
  > DURING AIRCRAFT POWER ADJUSTMENT TO START THE TAKEOFF PHASE "ENG 2 STALL FOLLOWED BY ENG FAIL" OCCURRED. THE AIRCRAFT RETURNED TO THE PARKING POSITION AND DURING THE INSPECTION OF ENGINE, DAMAGE TO THE HIGH PRESSURE COMPRESSOR (HPC) WAS FOUND. THE DAMAGE FOUND
- [SDR TAMF20211112017](https://openairdocs.org/sdr/TAMF20211112017.md): Fuel Filter · clogged · Nov 9, 2021 · N336QT · Airbus A330243F · Engine Fuel and Control
  > DURING AIRCRAFT TAXI OUT THE “ENGINE FUEL FILTER CLOG FAULT” WAS SHOWN. THE AIRCRAFT RETURNED TO THE PARKING POSITION. DURING INSPECTION NO BLOCKAGE NOR UNWANTED MATERIAL WERE FOUND. THE ENGINE 1 FUEL FILTER ELEMENT 5200EB (PN/ MFFA632-2) WAS REMOVED AND REP
- [SDR TAMF20211109016](https://openairdocs.org/sdr/TAMF20211109016.md): Starter · dislodged · Nov 9, 2021 · N335QT · Airbus A330243F · Engine Starting System
  > DURING THE TOWING OF THE N335QT AIRCRAFT AND IN THE ENGINE 1 START PROCEDURE, IT WAS NOTED THAT THE ENGINE WAS NOT TURNING. THE AIRCRAFT WAS RETURNED TO THE PARKING POSITION AND ON INSPECTION IT WAS FOUND THAT THE STARTER (PN / 3505788-8) HAD INTERNALLY DISINT
- [SDR TAMF20210927015](https://openairdocs.org/sdr/TAMF20210927015.md): None · none · Sep 26, 2021 · N330QT · Airbus A330243F · Fuselage Structure (General)
  > DURING AIRCRAFT LOADING PROCEDURE THE AFT CARGO COMPT DOOR CUT-OUT WAS FOUND WITH A SCRATCH BETWEEN STGR 42RH AND STGR 42A RH ON FR 65. //////// ACTION TAKEN: IN ACCORDANCE WITH AIRBUS A330-200F SRM TASK 53-41-11-283-006 FIGURE 002 (SHEET 1) THE DAMAGE WAS EVA
- [SDR TAMF2021082013](https://openairdocs.org/sdr/TAMF2021082013.md): Inlet · dented · Aug 20, 2021 · N331QT · Airbus A330243F · Nacelle/Pylon, Main Frame
  > DURING WALK AROUND A DENT ON RH AIR INTAKE INLET COWL WAS FOUND. THE DAMAGE WAS FOUND OUT OF ALLOWABLE LIMITS IN ACCORDANCE WITH RB211TRENT SRM 54-10-01. THE RH AIR INTAKE INLET COWL WAS REMOVED AND REPLACED IN ACCORDANCE WITH AIRBUS AMM 71-61-41 PB 401. AIR
- [SDR TAMF20210630012](https://openairdocs.org/sdr/TAMF20210630012.md): Tire · cut · Jun 29, 2021 · N334QT · Airbus A330243F · Tire
  > DURING THE TAXI OF AIRCRAFT N334QT AT THE MIA STATION THE CONDITION OF LOW PRESSURE WAS PRESENTED IN THE MAIN WHEEL NO. 8. THE AIRCRAFT RETURNED TO BLOCK AND DURING THE MAINTENANCE REVIEW THE MAIN WHEEL NO. 8 WAS FOUND DEFLATED DUE TO CUT BY FOREIGN OBJECT.
- [SDR TAMF20210327010](https://openairdocs.org/sdr/TAMF20210327010.md): Pump · leaking · Mar 26, 2021 · N332QT · Airbus A330243F · Hydraulic Pump (Electric/Engine), Main
  > AFTER TAKEOFF FROM MIA DURING THE CLIMB, THE MESSAGE "HYD G SYS LEAK" WAS SHOWN ON ECAM DISPLAY. THE CREW DECIDED TO RETURN TO THE MIA STATION AND DURING THE GROUND INSPECTION A HYDRAULIC FLUID LEAK WAS FOUND IN THE HYDRAULIC PUMP NO. 1 OF ENGINE 2. THE GREEN
- [SDR TAMF20210302009](https://openairdocs.org/sdr/TAMF20210302009.md): Radome · dented · Mar 1, 2021 · N335QT · Airbus A330243F · Aerodynamic Fairings
  > DURING TRANSIT CHECK OF AIRCRAFT N335QT AT THE BOG STATION, A "DENT" WAS FOUND ON THE RIGHT SIDE OF THE "NOSE RADOME". IN ACCORDANCE WITH AIRBUS AMM 53-15-11-200-801-A, ITEM 4.C.7, THE DAMAGE WAS FOUND OUT OF ALLOWABLE LIMITS (DENT DIMENSIONS: L=60MM; W=43MM
- [SDR TAMF20210218008](https://openairdocs.org/sdr/TAMF20210218008.md): Skin · dented · Feb 17, 2021 · N335QT · Airbus A330243F · Leading Edge Devices
  > DURING TRANSIT CHECK OF N335QT AIRCRAFT (MIA STATION), A "DENT" WAS FOUND ON SLAT NR 4 OF THE LEFT WING. IAW AIRBUS SRM TASK 57-40-00-283-001, THE DAMAGE (DENT) WAS FOUND OUT OF ALLOWABLE LIMITS AND THEREFORE IT WAS REQUIRED TO CONSULT THE MANUFACTURER AIRBUS
- [SDR TAMF20210208007](https://openairdocs.org/sdr/TAMF20210208007.md): Interface Unit · malfunctioned · Feb 7, 2021 · N331QT · Airbus A330243F · Landing Gear Retraction/Extension System
  > DURING CARGO LOADING PROCEDURE OF THE N331QT AIRCRAFT AT MIA STATION, THE FAULT MESSAGE “L/G DISAGREE” WAS SHOWN ON THE ECAM SYSTEM. THE COMPONENT (LGCIU - LANDING GEAR CONTROL INTERFACE UNIT) WAS REPLACED IN THE POSITION NO 2 AND THE FAULT MESSAGE DISAPPEARED
- [SDR TAMF20210131006](https://openairdocs.org/sdr/TAMF20210131006.md): Door Frame · scratched · Jan 28, 2021 · N330QT · Airbus A330243F · Fuselage Main, Frame
  > DURING THE TRANSIT CHECK OF THE N330QT AIRCRAFT AT UIO STATION (QUITO, ECUADOR), A SCRATCH WAS FOUND ON THE LEFT SIDE OF THE FUSELAGE, IN THE LOWER 1LT CREW DOOR FRAME. THE DAMAGE WAS EVALUATED, AND IT WAS FOUND OUT OF ALLOWABLE LIMITS AND A MANUFACTURER CONS
- [SDR TAMF20201123006](https://openairdocs.org/sdr/TAMF20201123006.md): Fmc · inoperative · Nov 22, 2020 · N332QT · Airbus A330243F · Flight Management Computing Hardware System
  > DURING TAXI OF THE N332QT AIRCRAFT, THE FAULT "AUTO FLT FM 2 FAULT" MESSAGE WAS SHOWN. THE AIRCRAFT RETURNED TO BLOCK AND THE (FMGEC) FLIGHT MANAGEMENT GUIDANCE AND ENVELOPE COMPUTER NUMBER 2 WAS DEFERRED IN ACCORDANCE WITH THE ITEM MEL 22-83-01. FINALLY THE
- [SDR TAMF20201122005](https://openairdocs.org/sdr/TAMF20201122005.md): Skin · dented · Nov 21, 2020 · N334QT · Airbus A330243F · Leading Edge Devices
  > DURING TRANSIT CHECK OF THE N334QT AIRCRAFT AT BOG STATION, A DENT WAS FOUND ON NUMBER 4 SLAT OF THE RIGHT WING. A QUERY WAS SUBMITTED TO THE AIRCRAFT MANUFACTURER. ACTION TAKEN: TEMPORARY REPAIR WAS PERFORMED ON THE WING SLAT SKIN IN ACCORDANCE WITH AIRBUS

Next page: https://openairdocs.org/model/airbus-a330-243f/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 aircraft_model_key = 'A330243F'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/airbus-a330-243f/reports

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