- Registered owner
- Aircol 5
- Location
- Wilmington, DE
- Owner type
- Corporation
- Serial number
- 1009
- Year built
- 2009
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- April 30, 2009
- Certificate issued
- April 29, 2009
- Expires
- March 31, 2030
- Mode S code
- AD79F2
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 261
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1996 | 1 |
|---|---|
| 1999 | 1 |
| 2000 | 2 |
| 2001 | 10 |
| 2002 | 5 |
| 2003 | 9 |
| 2004 | 15 |
| 2005 | 10 |
| 2006 | 16 |
| 2007 | 22 |
| 2008 | 10 |
| 2009 | 13 |
| 2010 | 13 |
| 2011 | 17 |
| 2012 | 16 |
| 2013 | 18 |
| 2014 | 20 |
| 2015 | 13 |
| 2016 | 27 |
| 2017 | 19 |
| 2018 | 16 |
| 2019 | 21 |
| 2020 | 11 |
| 2021 | 16 |
| 2022 | 13 |
| 2023 | 14 |
| 2024 | 11 |
| 2025 | 13 |
| 2026 | 10 |
See all 382 ADs
Information bulletins that may apply · 4
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N968AVMatched 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 A330-243 aircraft
FAA incident reports
No FAA accident or incident reports matched to N968AVMatched 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 A330-243 aircraft
Service difficulty reports · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR ANCF20200306401Control Lever · faulty04.MAR.2020 @ LIM -> FLIGHT AV917A (LIM-GRU) PILOT REPORT WO 2251658:
L/G LEVER DID NOT RETRACT AFTER LIFT OFF, NO ECAM MESSAGE - LANDING WEIGHT: 169320 KG
04.MAR.2020 @ LIM -> CORRECTIVE ACTION AS FOLLOWS:
REMOVAL AND REPLACEMENT OF THE LANDING GEAR CONTSDR ANCF2019082872501Link · misinstalledLG SYSTEM DISAGREE, L/G R LENGTHENING FAULT. REMOVED AND INSTALLED CORRECTLY THE SHORTENING MECHANISM TURNBUCKLE LINK. THE FUNCTIONAL TEST OF THE NORMAL EXTENSION AND RETRACTION, OPERATIONAL TEST OF THE FREE-FALL EXTENSION AND BITE TEST OF THE NORMAL EXTENSISDR ANCF2015051901Bleed Valve · malfunctionedAFTER ENGINES START AIR ENG 2 BLEED FAULT RESET UNSUCCESSFUL. IAW AMM 36-11-51-000-804-400-A THE HP BLEED VLV WAS REPLACED. OPERATIONAL TESTED SATISFACTORY. IAW AMM 36-11-55-000-804A 400-A THE BLEED VLV CONTROL SOLENOID WAS REPLACED. OPERATIONAL TEST WAS SSDR ANCF2014011000179Idg · lowELEC IDG 1 OIL SYS FAULT & APU FAULT. ELEC IDG 1 OIL SYS FAULT MSG, HAD BEEN DEFERRED DURING TRANSIT PRIOR TO DISPATCH THE AIRCRAFT IAW MEL 24-22-02 CAT B. DURING FLIGHT THE APU FAILED. THIS ITEM ENTER ON DMI 577 LOGBOOK 0002254. ACCOMPLISHED MAINTENANCE ASDR ANCF2013012300146Wheel · vibrationREJECTED TAKEOFF RWY 10 CCS DUE TO STRANGE VIBRATION DURING TAKEOFF ROLL SPEED 90 KTS TOW 153.0 KGRS OAT 27°C. PERFORMED FAULT CONFIRMATION SUBTASK 32-20-00-710-0050A CLASS 3 NO FAULT. ON BSCU CH 1 AND 2 NO FAULT DETECTED. IN ACCORDANCE WITH AMM 32-41-12 PSDR ANCF2012100900131Actuator · malfunctionedDIVERSION TO BOG BY CREW AS ALTERNATE PROCEDURE DUE TO TRANSFER OF FUEL TO THE CENTER TRANSFER PUMPS INOPERATIVE. FOLLOWING TSM 28-21-00-810-835-A AS TROUBLESHOOTING THE FUEL INLET VALVE ACTUATOR (603QL1) WAS REPLACED BY NEW ONE ACCORDING TO AMM 28-26-53-000SDR ANCF2011052900091Epr System · malfunctionedAT CLO AIRPORT THE TAKEOFF WAS DISCONTINUED DUE TO TRANSIT ECAM INDICATION "ENG THRUST LOSS" AFTER ALL VERIFICATIONS A NORMAL TAKEOFF WAS DONE. T/S 71-00-00-810-922A INCORRECT EPR TAR GET COMPUTATION CARRIED OUT. NO PFR REPORT ACMS LABEL CALL UP WITH ENG NR SDR ANCF2010083100067Hydraulic Line · leakingPRELIMINARY REPORT: - PILOT REPORT: DURING LANDING ROLL STRONG TENDENCY TO THE LEFT AFTER BRAKES WHERE APPLIED, NO BRAKING ON RIGHT TANDEM BRAKE TEMPERATURE. 1-395 2-435 3-40 4-40 5-385 6-390 7-40 8-35. IN ACCORDANCE WITH AMM 20-23-11-350-051 ITEM B PROVISIOSDR ANCF2009123000056Proximity Sensor · intermittentMAIN DOOR R4 SHOWS UNLOCKED ON ECAM DEFERRED TO DMI NR 112 AS PER MEL 52-71-01 CAT C PILOT REPORT. ECAM MESSAGE "PACK 1,2 INOP, CABIN PRESS 1, 2 FAULT. 4R DOOR LIGHT ON RETURN TO JFK. UNABLE TO CONTINUE THE FLT. DOOR OVERRIDE PROCEDURE WAS CONFIRMED AS PER SDR ANCF2009061200047Unknown · odorON GROUND WHEN PACKS ARE WORKING EITHER WITH APU BLEED OR ENGINES BLEED, A HYD LIKE ODOR IS PERCEIVED FROM THE AIR CONDITIONING SYS IAW AMM: TASK 21-00-00- 615-804 PART B THE BLEED AIR DUCTS FROM APU WAS CHECKED FOR CONTAMINATION. NO EVIDENCE WAS FOUND, THE APSDR ANCF2009061200046Unknown · odorAT FL 410 INSIDE BAD WEATHER CONDITIONS WITH ENGINE ANTI-ICE ON STRONG BURNING ODOR. WITH NO TURBULENCE ENGINE ANTI-ICE ON. NO ODOR WAS DETECTED. IAW AMM 30-21-48 PB 601 DUCTS- ANTI ICE, ENGINE - INSPECTION CHECK WERE ACCOMPLISHED IN LT AND RT ENGINES AND WER
STCs that may be installed · 175
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.