- Registered owner
- Aircol 14 Trust
- Location
- Wilmington, DE
- Owner type
- Corporation
- Serial number
- 4281
- Year built
- 2010
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- May 6, 2010
- Certificate issued
- June 7, 2024
- Expires
- June 30, 2031
- Mode S code
- A2D1C6
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 N281AVMatched 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 N281AVMatched 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 · 15
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2026FA0000307Isis · faultedISIS FAULT DURING TAXISDR 2026FA0000232Indication Sys · faultedDURING TAXI AOUT FUEL IN LEFT OUTER TANK INCREASED TO 590KG AND FUEL IN LEFT INNER TANK DECREASED TO 1340 KG FUEL IS LOADING OUT OF LIMITS FOR T/OFFSDR 2023F00329Control Unit · inoperativeAFTER TAKE OFF, LGCIU 2 FAULT INDICATION WAS SHOWN. ATB PROCUEDURE TO BOGOTA STATION DUE TO BY MEL MANUAL, BOTH REVERSIBLES SHOULD BE OPERATIVE TO APROACH IN SANTA MARTA STATION// AS PER TSM 32-31-00-810-819-A FAULT INSOLATION LGCIU 2 WAS REMOVED AND REPLACEDSDR ANCF20230911033Lgciu · warning messageLGCIU 2 FAULT AFTER TAKE OFF AS PER TSM 32-31-00-810-819-A FAULT INSOLATION LGCIU 2 WAS REMOVED AND REPLACED TEST OK. DUE TO LGCIU 2 REPLACED AND SOFTWARE CONFIGURATION, THE LGCIU1 WAS REPLACED TEST OKSDR ANCF2019102892401Engine · stalledSEP 24. DURING TAKE OFF JUSTON INITIAL CLIMB E FELT 3 STALLS FROM ENGINE N-2 THE EGT REACHES 944 C° WE RETURN TO BOGOTA AS PER COMPANY POLICE PLEASE DOWNLOAD THE CVR AND THE FDR // CORRECTIVE ACTIONS: SEP 25. IN ACCORDANCE WITH TSM 73-00-00-810-866-A.THE BOROSSDR ANCF2019082873101Pump · low pressureJUL 31. DURING CLIMB HYD Y RSVR LO LVL FOLLOWER BY Y ENG 2 PUMP LO PR COME ON ECAM. SUPPORT REMOVED AND REPLACED IAW AMM 20-23-11 PB 201 CONF 00. THE HYD TUBING SYS YELLOW WAS INSTALLED AND AMM 29-00-00-210-003-A DETAILED VISUAL INSPECTION FOR CORRECT INSTALLSDR ANCF2019053143001Idg · leakingABR. 30. DURING TAKE OFF RUN ELEC IDG 1 OIL LO PR (APPROX 60 KG) ON ELEC SD IDG 1 AMBAR // CORRECTIVE ACTIONS: MAY 1. IN ACCORDANCE WITH TSM 24-20-00-810-904-A STEP 1 IDG WAS REPLACED // IAW AMM 24-00-720-041-A THE OPERATIONAL TEST OF THE IDG DISCONNECT AND RESDR ANCF2016031201Pump · malfunctionedLANDING GEAR DOORS NOT CLOSED DURING TAKEOFF. THEN HYD G RSVR LO LVL ECAM WAS COMPLETELY UNSATISFACTORY. EMER WAS DECLARED. IAW AMM 29-11-51-041-A & THE AMM 29-1-51-400-041 GREEN EDP WAS REPLACED, TESTED OK. IAW AMM 32-11-22-000-001 & AMM 32-11-22-400-001 SDR ANCF2015050201Transducer · faultyAFTER ENG START HYD PTU FAULT. IAW AMM 29-32-11-000 400-003 HYD PRESS TRANSDUCER WAS REPLACED. OPERATIONAL TEST OF THE SYS PRESS SW WAS DONE, ALL TESTED SUCCESSFUL.SDR ANCF201412051Engine · vibrationDURING CRUISE ENG 1 FAIL & STRONG VIBRATION WAS FELT. IAW PRELIMINARY INVESTIGATION, PROBABLE CAUSE OF INCIDENT WAS A FLAW OF OIL SYS. IN PROCESS TO REMOVE & INTALL NEW ENG. REMOVED ENG WILL BE SENT IN ORDER TO ACCOMPLISH AN INVESTIGATION.SDR ANCF2014082101Cradle · damagedDURING CRUISE BURNING SMELL WAS FELT FROM ROWS 24 TO 26 AT THE PAX CABIN. SMOKE WAS NOT PRESENTED, INFLIGHT ENTERTAINMENT SYS WAS TURNED OFF. IAW AMM 23-32-00-210-801 CABLE INSPECTION WAS PERFORMED, THE CRADLE WERE FOUND IN BAD CONDITION IAW SIL 5O22613-HW 8SDR ANCF2014070602Controller · malfunctionedDURING CLIMB AFTER TAKEOFF AIR PACK TWO REGULATOR FAULT WAS DISPLAYED, ALSO HOT AIR FAULT, TRIM AIR SYS FAULT, AFT & FWD CABIN TRIM VLV FAULT. IAW TSM 21-61-00-810-900 PERFORMED SWAP BETWEEN ACSC 1 & ACSC 2 IAW AMM 21-61-34-000-002-A & 21-61-34-400-002-A. OPSDR ANCF2013030200150Fuel Filter · cloggedDURING TAKEOFF ROLL ENGINE 2 FUEL FILTER CLOG CAME ON THE ECAM - IN ACCORDANCE WITH AMM 73-11-10-400-004A IN THE ENGINE 2 FUEL FILTER ELEMENT WAS REMOVED AND REPLACED. RUN UP TEST IN ACCORDANCE WITH 71-00-00-710-003B, RUN UP OF ENG AUTOMATIC START WAS SATISFASDR ANCF2011052900089Valve · faultyAFTER T/O VENT AVNCS SYS FAULT ON ECAM (BLOWER AND EXTRACT VALVE FAULT). IN ACCORDANCE WITH AMM 21-26-53 PB 401 THE SKIN AIR OULET VALVE (22HQ) WAS REPLACED BY NEW ONE, OPERATIONAL TEST OF AEV SYSTEM WAS SUCCESSFULLY CARRIED OUT.SDR ANCF2011052900087Unknown · smokeAT LAST MINUTE ELECTRICAL SMOKE WAS FELT BY FLIGHT ATTENDANT OVER WINGS AREA. IN ACCORDANCE WITH TSM 24-00-00-810-123 VISUAL INSPECTION WAS PERFORMED AND NO DISCREPANCIES WERE FOUND.
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