- Registered owner
- Wilmington Trust Co Trustee
- Location
- Wilmington, DE
- Owner type
- Corporation
- Serial number
- 1428
- Year built
- 2013
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- July 3, 2013
- Certificate issued
- December 20, 2023
- Expires
- December 31, 2030
- Mode S code
- A39EAD
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 144
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1999 | 1 |
|---|---|
| 2002 | 1 |
| 2004 | 1 |
| 2007 | 1 |
| 2010 | 1 |
| 2011 | 11 |
| 2012 | 12 |
| 2013 | 14 |
| 2014 | 14 |
| 2015 | 11 |
| 2016 | 23 |
| 2017 | 16 |
| 2018 | 11 |
| 2019 | 20 |
| 2020 | 10 |
| 2021 | 11 |
| 2022 | 9 |
| 2023 | 11 |
| 2024 | 10 |
| 2025 | 12 |
| 2026 | 8 |
See all 208 ADs
Information bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N332QTMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Airbus A330-243F aircraft
FAA incident reports
No FAA accident or incident reports matched to N332QTMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Airbus A330-243F aircraft
Service difficulty reports · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR TAMF20260531055Not Reported · not reportedAIRCRAFT DEPARTED SCL OPERATING FLIGHT TPA4092 (SCL-MIA) WITH A PALLET LOADED IN POSITION 41P WITH A DECLARED WEIGHT OF 1,096 KG IN THE LOAD CONTROL SYSTEM (LCS). SUBSEQUENT VERIFICATION IDENTIFIED THAT THE ACTUAL PALLET WEIGHT WAS 2,970 KG. BASED ON THE CORRESDR TAMF20250708052Engine · failedDURING THE TAKE-OFF ROLL, A THRUST LOSS OCCURRED ON ENGINE NO. 2, ALONG WITH AN ABNORMAL INDICATION FROM THE ENGINE ANTI-ICE SYSTEM. THE ECAM DISPLAYED: "A. ICE ENG 2 VALVE OPEN". AN OPERATIONAL CHECK OF THE ENGINE AIR INTAKE ICE PROTECTION SYSTEM WAS PERFORMESDR TAMF20241203047Acm · faultedDURING 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 TAMF20231227041Unknown · unknownAFTER 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 FWSDR TAMF20230905037Unknown · unknownTHE 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 DOSSIESDR TAMF20221102028Flap · perforatedA 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 TAMF20220914026None · perforatedDURING 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 TAMF20220901025Hydraulic Line · leakingDURING 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 TAMF20220811024Heat Exchanger · leakingDURING 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 THSDR TAMF20210327010Pump · leakingAFTER 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 GREENSDR TAMF20201123006Fmc · inoperativeDURING 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 THESDR TAMF20190917001Smoke Detector · contaminatedDURING CLIMB "MD SMOKE WARNING" WAS SHOWN ON ECAM 3 TIMES. THE AIRCRAFT RETURN TO GROUND, THE TSM 26-19-00-810-801-A WAS PERFORMED AND THE SMOKE DETECTOR (117WU) LOCATED IN THE MAIN DECK CARGO COMPARTMENT WAS FOUND CONTAMINATED WITH A POWDER THAT WAS SPREADED SDR TAMF2015FA0000128Landing Gear · malfunctionedLANDING GEAR SELECTOR DID NOT SELECT UP, DUE TO THAT THE RT MLG DID NOT GET UP, REVERSE 1 AND 2 DID NOT ARM. AFTER A VISUAL INSPECTION OF THE LANDING GEAR WAS FOUND THE TARGET OF THE SENSOR WAS FOUND BENT. TO FIX IT WAS PERFORMED A DIMENSIONAL CHECK OF BOGIE
STCs that may be installed · 94
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.