- Registered owner
- Wilmington Trust Co Trustee
- Location
- Wilmington, DE
- Owner type
- Corporation
- Serial number
- 3961
- Year built
- 2009
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- July 8, 2009
- Certificate issued
- July 8, 2009
- Expires
- December 31, 2027
- Mode S code
- AD5FF1
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every CFM International CFM56-5B4 model are included below.
On this page
Airworthiness directives that may apply · 391
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1990 | 5 |
|---|---|
| 1991 | 1 |
| 1992 | 6 |
| 1993 | 10 |
| 1994 | 10 |
| 1995 | 4 |
| 1996 | 5 |
| 1997 | 10 |
| 1998 | 22 |
| 1999 | 14 |
| 2000 | 15 |
| 2001 | 9 |
| 2002 | 15 |
| 2003 | 3 |
| 2004 | 23 |
| 2005 | 20 |
| 2006 | 13 |
| 2007 | 16 |
| 2008 | 10 |
| 2009 | 13 |
| 2010 | 8 |
| 2011 | 12 |
| 2012 | 12 |
| 2013 | 17 |
| 2014 | 18 |
| 2015 | 23 |
| 2016 | 25 |
| 2017 | 24 |
| 2018 | 31 |
| 2019 | 24 |
| 2020 | 29 |
| 2021 | 17 |
| 2022 | 22 |
| 2023 | 19 |
| 2024 | 15 |
| 2025 | 21 |
| 2026 | 17 |
See all 558 ADs
Information bulletins that may apply · 8
Advisory, not mandatory.
Airframe · Airbus A320-214
SAIB NE-19-03Escape Slide Maintenance Tasks and Intervals - JASC 2565SAIB NM-15-02Cabin Equipment/FurnishingsSAIB NM-14-21Communications: Honeywell RTA 44D VHF TransceiversSAIB NM-13-24Air Conditioning System: Air Distribution FanSAIB NM-13-03Hydraulic Power System: Power Transfer UnitSAIB NM-06-57Reports of damage to airplanes and to property on the ground caused by blue or clear ice falling from airplanes.Engine · CFM International CFM56-5B4 series
SAIB NE-08-17R3Turbine Section - Propulsion Technology LLC Unapproved RepairSAIB NE-12-29Engine Fuel Distribution CFM56-5B LPTACC Fuel ManifoldHistorical bulletins · 1
NTSB investigations
No NTSB investigations matched to N961AVMatched 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 A320-214 aircraft
FAA incident reports
No FAA accident or incident reports matched to N961AVMatched 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 A320-214 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 ANCF20260426012Sensor · out of limitsNR 1 ENGINE VIBRATION. REJECTED TAKE OFF WAS PERFORMED DUE TO HIGH ENGINE VIBRATION INDICATION BETWEEN 71KTS AND 99KTS. ENGINE 1 VIBRATION CHECK WAS PERFORMED SATISFACTORILY IAW AMM 71-00-00-710-009-B, REV 76. VIBRATION OF BEARING 1 IS MORE THAN 6 U, IAWTSSDR ANCF20250924329Hydraulic Line · leakingHYDRAULIC SYS -Y- RESERVOIR LOW LEVEL. REMOVAL & INSTALLED TUBE HYDRAULIC SYSTEM -Y- IAW 29-24-21-000-001SDR ANCF2025052700515Engine · vibrationDURING TAKE OFF ROLL AT APROX 80 KTS ENG HING VIBRATION DURING TAKE OFF ROLL AT APROX 80 KTS ENG HING VIBRATION ON ECAM N1. VIB ENG1 WAS 9.9 DURING TAKE OFF ROLL AT APROX 80 KTS ENG HING VIBRATION IAW TSM 77-00-00-810-864-A REV 72 OF 01-MAY-2025 FAN VIBRATIONSSDR ANCF20240929019Lever · damagedTHR LEVER NOT SET. RTO RWY O1 THR LEVER NOT SET TO TAKE OFF THRUST, FMA INDICATED MAN FLX, ENG 2 TOOK LONG TIME TO SPOOL UP, ENG THR LEVERS NOT SET THR LEVER NOT SET I.A.W TSM 76-11-00-810-823-A ENGINE THRUST NOT SET AT CORRECT POSITION , ADJUSTMENT OF MECHAANSDR ANCF20240519013Pilot Valve · abnormalG SYS LO PR PITOT VALVE WAS REPLACED IAW AMM TASK 32-31-17-400-001-A AND REF 32-31-17-000-001-A, PERFORMED OPERATIONAL CHECK OF THE SAFETY VALVE IAW AMM TASK:32-31-00-710-013-A REV#68 ALL TEST SATISFACTORY NO LEAKS FOUND. DUE TO PILOT PERFOSDR ANCF20230809022Fault Message · illuminatedF/CTRL EN VLO SLATS NO RETRACT + MSG DOOR L AFT EMER EXIT FWC N.1 FAULT IAW TSM 31-53-00-810-804-A REV 65 WAS REMOVED AND REPLACED FWC N.1 FIN 1WW1 AS PER AMM 31-53-34-000/400-001 REV 65 PERFORMED GROUND SCANNING AS PER AMM 31-50-00-710-001-A REV 65, PERFORMSDR ANCF2015021601Brake · overtempBRAKE TEMP OF BRAKE NR 1 EXCEEDED IN MORE THAN 215°C, AGAIN BRAKE NR 2, DURING TAKEOFF ROLL BRAKE TEMP INCREASED FROM 115°C TO 290 °C. DURING TAXI IN & OUT, HIGH THRUST WAS NECESSARY TO MAINTAIN TAXI SPEED IAW AMM 32-41-11-401. THE MAIN WHEEL ASSEMBLY NR 2 WSDR ANCF2014011000180Valve · faultedECAM MSG VENT AVNCS SYS FAULT & VENT SKIN VALVE FAULT.SDR ANCF2011040400076Computer · malfunctionedDURING T/O ROLL FMGC 1 & 2 FAILED. NO V1, VR, NO FD, NO ATHR, RTO. AS PER TSM 22-83-00-810-901 RESET FMGC 1 & 2. PERFORMED AFS TEST ALL PASSED REF AMM 22-91-00-710-001. IN ADDITION, AIRCRAFT WALK AROUND OUTSIDE INSPECTION WAS FOUND NORMAL. RII ITEMSDR 2011F00093Computer · failedDURING T/O ROLL FMGC 1 & 2 FAILED. NO V1, VR, NO FD, NO ATHR. RTO: IAW TSM 22-83-00-810-901 RESET FMGC 1 & 2. PERFORMED AFS TEST ALL L PASSED REF AMM 22-91-00-710-001. IN ADDITION, ACFT WALKAROUND OUTSIDE INSP WAS FOUND NORMAL.SDR ANCF2010061100063Line · brokenPRELIMINARY REPORT - SMOKE IN APU . PILOT REPORT: APU AUTO SHUTDOWN AFTER ENG 1 START. PRELIMINARY MAINTENANCE, THIS ITEM IS DEFERRED TO DMI 66, MEL 49-10-01 CAT C, APU SYSTEM SELF TEST VIA MCDU PERFORMED, LOW OIL LEVEL, LUBRICATION LINE WAS FOUND BROKEN, M
STCs that may be installed · 301
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 301 STCs