- Registered owner
- Aircol 10
- Location
- Wilmington, DE
- Owner type
- Corporation
- Serial number
- 4026
- Year built
- 2009
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- September 23, 2009
- Certificate issued
- September 22, 2009
- Expires
- April 30, 2028
- Mode S code
- A511FD
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 N426AVMatched 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 N426AVMatched 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 · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR ANCF2025102733Actuator · faultedAFTER TAKE OFF ENG 1 AND 2 BLEED FAULT ON THE OVERHEAD PANEL. RESET UNSUCCESFULLY. AFTER 5 MINUTES RESET SUCCESFULL BUT ON THE SD PAGE PRESS OUTFLOW VALVE DOES NOT REGULATE PRESS. THE VALVE ALWAYS WAS OPEN.SDR ANCF20250501011Unknown · vibrationAT TAKE OFF ROL HIGH VIB ENG 2- BIRD STRIKE - PERFORMED BORESCOPE INSPECTION OF BOOSTER ASSEMBLY IAW AMM TASK 72-21-00-290-003-A AND LOW PRESSURE TURBINE IAW TASK AMM 72-54-00-290-005-A AND AMM TASK 72-54-00-290-006-A REV. 72 REV. NO DAMAGE FOUND.SDR ANCF20231230039Lgciu · warning messageL/G LGCIU 1 FAULT REFERENT TSM 32-31-00-810-819-A-R66 WAS REMOVED AND REPLACED LGCIU IAW AMM 32-31-71-000/400-001-A AND PROX SW 26AG IAW AMM 32-31-73-000/400-001-A REV 66AND PERFORMED TEST OK IAW AMM 32-64-00-740-001 REV 66SDR ANCF2015051101Proximity Sensor · faultedBEFORE TAKEOFF, LG LGCIU 1 FAULT MSG ON ECAM. COMPUTER RESET WAS PERFORMED & WAS NOT SATISFACTORY. IAW AMM 32-31-00-810-819-A RT LG DOOR CLOSED PROXIMITY SENSOR FAULT STEP 3A - 4A3 WAS PERFORMED. IAW AMM 32-31-73-000-001-A 400-001-A. THE PROXIMITY SENSOR WSDR ANCF2012032300116Sliding Window · openDURING INITIAL TAKEOFF ROLL THE LEFT SLIDING WINDOW SUDDENLY OPENED TAKEOFF WAS ABORTED. IAW AMM SLIDING WINDOWS LEFT INSPECTION AND CHECK VISUAL FOR CRACKS, CHIPS BUBBLE WAS PERFORMED NORMAL CONDITION.SDR MU1Z2011020200006Skin · dentedDURING SERVICE OF 20 MONTHS FOUND TWO DENTS BETWEEN FRAME 16 AND 18 DOWN OF LT STRINGER 5. DENT 2 IS OUT OF LIMITS BECAUSE IS AT 13.5 MM FROM THE STR 5 LT DENT 1 IS ON LIMITS, PERFORMED INTERNAL AND EXTERNAL HIGH FREQUENCY EDDY CURRENT INSPECTIONS PER CRACKS
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