- Registered owner
- Aircol 21
- Location
- Wilmington, DE
- Owner type
- Corporation
- Serial number
- 4381
- Year built
- 2010
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- August 31, 2010
- Certificate issued
- August 30, 2010
- Expires
- March 31, 2028
- Mode S code
- A5EC64
From the FAA registry file of October 22, 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 N481AVMatched 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 N481AVMatched 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 2026FA0000659Engine · bird ingestionAFTER TAKEOFF DURING INITIAL CLIMB BIRD STRIKE TO ENG 2 WITH ENG FAILURE. PERFORM JIC-32S-71-01022 COMPONENT (JOB INSTRUCTION CARD) R MANDATORY: PERFORM JIC-32S-71-01022 COMPONENT (JOB INSTRUCTION CARD) REV. 00. POWER PLANT REMOVAL AND INSTALLATION.SDR ANCF2025052213Gps · malfunctionedBOTH GPS LOST DURING TAKE-OFF NAV ADS-B RPTG (1)(2) FAULT WAS PRESENTED ON ECAM, GPS MONITOR WAS CHECKED AND THE SAT IN BOTH GPS WERE DASHES, REQUESTED VECTORS TO ATC AND WE HAD GPWS ALERTS (FALSE) ABOUT 16000 FEET THE FLIGHT PLAN SUDDENLY DISSEPPEARED AND CABSDR ANCF20241216028Valve · faultedAFTER TAKE OFF ENG 1 BLEED FAULT AND ENG 2 BLEED WAS DEFERED - AS PER AMM 36-11-52-04 AND AMM 36-11-49-04 ENG 2 PRV WAS REPLACED AND SENSE LINES OF PRV WERE REPLACED AT BOTH ENGINES. LEAK TEST OF THE PRV WITH ENGINE IN OPERATION PERFORMED SATISFACTORY AT BOTH SDR ANCF20220506018None · nonePILOT REPORT
05.MAY.2022 WO 54'436'967=> (EGT OVERLIMIT) - EGT OVERLIMIT ON ENG 1 APPEARS ON ECAM DURING TO.
ACTIONS TAKEN
05.MAY.2022 WO 54'436'967=> (EGT OVERLIMIT) - IN ACCORDANCE WITH TSM 77-00-00-810-849-A EGT OVERLIMIT ON ENG 1 AND AMM SUBTASK 72-00SDR ANCF2020020713101Fault Message · false activation31.JAN.2020 -> AV4901 (BAQ-BOG) PILOT REPORTED (WO 16047158):
DURING TAKEOFF AND AFTER TAKE OFF NAV IAS DISCREPANCY FAULT ON ECAM DIFFERENCE BETWEEN CAP AND F/O AIRSPEED MORE THAT 60KTS.
31.JAN.2020 -> CORRECTIVE ACTION WAS PERORMED AS FOLLOWS:
TEST OF SDR ANCF2017111001Bleed Valve · failedNR 2 ENGINE BLEED ILLUMINATED IN FLIGHT, AIR ENG 2 BLEED FAULT ON ECAM. FOUND OXYGEN MASK IN ALL STATIONS DEPLOYED. IAW TSM TASK 36-11-00-810-B39-. A FAILURE OF REGULATION OF THE BLEED-PRESSURE REGULATING VALVE DURING TAKE-OFF ON ENGINE 2 WAS ACCOMPLISHED ANSDR ANCF2015042101Warning System · false activationFLAPS OVER SPEED WARNING OCCURRED DURING DESCENT WHILE SELECTING FLAPS 2 & DURING TURBULENCE SPEED REACHED 205KS APPROX DURING LESS THAN ONE SECOND. IAW AMM 05-51-13-200-001-A INSPECTION AFTER FLAP & SLAT EXTENSION AT MORE THAN THE FLAP & SLAT LIMITING SPEED SDR ANCF2014F00104Warning Message · false activationRTO THRUST LEVER FAULT ON ECAM, AT ABOUT 80 KNOTS. INTERNAL POSSIBLES CAUSES OF FAILURES ON ECU IAW AMM 76-11-00-810-811A. ENGINES 1 AND 2 WERE DONE AND NO MAINTENANCE ACTIONS WERE REQUIRED BECAUSE WAS NOT CONFIRMED. REF: SUBTASK 76-11-00-710-078-A.SDR ANCF2013061600161Door · out of rigDURING CLIMB, MAX PRESENTED DOOR RT AFT EMERGENCY EXIT ON ECAM. THE SLIDE EXIT DOOR COVER WAS ADJUSTMENT AND RIGGING, TEST IS OK ON ECAM AND FAP IAW AMM 52-21-11-400-001ASDR ANCF2011052900085Door · damagedLT AFT PASSENGER AT FR68 HAS A SCRATCH ON UPPER SIDE AND THE SKIN IS DOUBLE IN THE LOWER RIGHT SIDE CORNER, BESIDE THE CHANNEL SEAL IS CRACKED.SDR ANCF2011010500073Computer · malfunctionedAIR TURNBACK. PILOT REPORT: AFTER TAKEOFF AIL SERVO FAULT FCTL ALT LAW PROTECTION LOST. IAW AMM TASK 27-93-34-000-001 / 27-93-34-400-001 ELAC N° 2 WAS REMOVED AND REPLACED. OPERATIONAL TEST OF ELAC WAS PERFORMED AMM TASK 27-93-00-710-001.
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