- Registered owner
- Aircol 12
- Location
- Wilmington, DE
- Owner type
- Corporation
- Serial number
- 4051
- Year built
- 2009
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- October 16, 2009
- Certificate issued
- October 15, 2009
- Expires
- August 31, 2028
- Mode S code
- A575E7
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 N451AVMatched 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 N451AVMatched 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 · 14
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR ANCF2024090400688Lgciu · faultedLG LGCIU 1+2 FAULT, REPLACED ELECTRICAL CONNECTORS 26 GA-A AND 28 GA-A IAW ESPM ABS0121-40 REV 50, ESPM 20-48-21-01 REV 50, ASM 32-31-03 SCH 03 P 0001 (SHEET 1/2) AND ASM 32-31-04 SCH 04 P 0001 (SHEET 1/2) . -WERE REPLACED PROX SENS 26GA AND 28GA IAW AMM 32-SDR 2024F00192Controller · malfunctionedCAB PRESSURE. ADV CABIN ALTITUDE 8’800 AP 4.4 V/S 0 ACTION RECOMMENDED WERE PERFORMED AP CONTINUE INCREASING AN V/S “0 IAW TROUBLESHOOTING TASK 21-31-00-810-868-A THE PROCEDURE WAS PERFORMED & OPS TEST´S STEP 4.F WAS PERFORMED SATISFACTORYLY, & STEP 4A ITEM 1SDR ANCF20240310005Pump · low pressureDURING TAKE OFF THE MESSAGE: HYD B ELEC PUMP LO PR CAME ON E/WD THE THE TAKE OFF WAS ABORTED. HYD B ELEC PUMP LO PR IAW TSM 29-12-00-810-804-A REV 67 WAS REPLACED PUMP - ELECTRIC, BLUE SYSTEM AS PER AMM 29-12-51-000/400-001-A REV 67. WAS INSTALLED THE UNION SDR ANCF20210407009Controller · malfunctionedF/CTL FLAP LOCKED - WING TIP BRK ON APPEAR DURING INITIAL CLIMB. FLAPS LOCKET AT AIRCRAFT POWER-UP IN ACCORDANCE WITH TSM 27-51-00-810-849-A. WAS PERFORMED TO STEP 4.A.1. AND I.A.W. AMM 27-50-00-869-006-A. RESET OF THE WINGTIP BRAKE (WTB) OF FLAP SYSTEM ON TSDR ANCF2019021701Engine · malfunctionedFEB 17. DURING TAKE OFF ENG NR 2 EGT OVERLIMIT REACHED 981°C DIENG 4-8 SECONDS. CORRECTIVE ACTIONS: FEB 22. IN ACCORDANCE WITH AMM TASK 72-00-00-200-008-A AND AMM TASK 71-00-00-000-042-A/AMM TASK 71-00-00-400-042-A THE ENG NR 2 WAS REPLACED TEST SATISFACTORY. SDR ANCF2015061501Strut · out of adjustDURING APPROACH, WHEN FLAPS WAS SELECTED, FLIGHT CONTROL FLAPS LOCKED APPEAR ON ECAM. IAW AMM 27-54-00-200-001 A VISUAL INSPECTION OF THE TRANSMISSION ASSEMBLY, AMM 27-51-44-820-001-A ADJUSTMENT OF THE INTERCONNECTING STRUT LT FLAPS WAS ACCOMPLISHED. OPERATSDR ANCF2015030806Warning System · activatedAFTER ENG START ELAC 1 FAULT WAS PRESENTED, RESET WAS UNSUCCESSFUL. IAW AMM 27-93-00-710-001-A, OPERATIONAL TEST OF ELAC 1 WAS PERFORMED WITH SATISFACTORY RESULTS.SDR ANCF2015030808Brake · disintegratedDURING PUSH BACK BLACK SMOKE CAME ON WHEEL, NR 3 BRAKE WAS FOUND DISINTEGRATED. IAW AMM 32-42-27-000 400-0001A & AMM 32-41-11-000 400-006A THE MAIN BRAKE & WHEEL NHR 3 WERE R & R. MAIN WHEEL PRESS 215 PSI PN 2-1684, SN OFF 8788, SN ON 8284, PN 3-153, SN OFF SDR ANCF2015020201Control Valve · leakingFUEL LEAK ON ENG 2 WAS FOUND DURING 360° BY MAINTENANCE AFTER BOTH ENGS STARTED. LEAK IS CONSTANT & THERE IS A LOT OF FUEL ON THE FLOOR IN THE PARKING GATE. IAW TASK 75-21-10-000 400-002A THE HIGH PRESSURE TURBINE ACTIVE CLEARANCE CONTROL VLV WAS REPLACED, TSDR ANCF2013030200149Engine · bird ingestionBIRD STRIKE ENGINE 2 AT TAKEOFF IN BGA HIGH VIBRATION DURING CLIMB N1 6.0. IN ACCORDANCE WITH AMM TASK 72-00-00-200 006-A AND SUBTASKS 72-00-00-220-172-A (B1) 72-00-00-280-057-A BOROSCOPE INSPECTION OF THE STAGE 4 LP TURBINE BLADES, HPC STAGES 1, 3 AND 8 CONBSDR ANCF2012071900126Sdac · inoperativeAFTER NR 1 ENGINE START, AMBER XX APPEAR ENG 1 PSI, WAS CONSULTED AND C/B 121 NV N-40 WAS RESET PSI APPEARS AND INDICATION WAS BETWEEN 16-18 PSI AN ADVISORY APPEARS ON THE RATING TAKE OFF CONSEQUENTLY REPLACED T/O WAS DONE AT 75K APROX PSO DROPS TO 12, ENGINE SDR ANCF2011112500104Slide · partial deployDURING ACCOMPLISHMENT OF T-256241-50-1-AV / AFT LT, THE SLIDE DIDN'T EXTEND FULLY, AND THE DOOR DIDN'T OPEN COMPLETELY. CURRENTLY THIS EVEN IS UNDER INVESTIGATION BY AIRCUISERS AND AIRBUS. THE SLIDE WAS SENT TO SHOP AND WAS REPAIRED.SDR ANCF2011110700093Interface Unit · malfunctionedPILOT REPORT: ECAM WARNING L/G LGCIU 1 FAULT. CORRECTIVE ACTION: IAW TSM 32-31-00-810-819 BITE TEST THE LGCIU1 AND 2 WERE ACCOMPLISHED TEST SATISFCTORY MCDU. BUT SHOWS STATUS FAULT AND ECAM WARNING LGCIU1) IAW AMM 32-31-71-000-001 AND AMM 32-31-71-400-001 SDR ANCF2011052900081Blade · damagedBIRD STRIKE, DURING TAKEOFF (V1) ON ENG NR2, HIGH VIBRATION FELT AND STRONG NOISE WITH HIGH THRUST SETTING FG VIB N1 ENG NR2 REACHED 7 UNITS. R & R FAN ROTOR BLADES POS 9, 10, 11, 27, 28 AND 29 IAW AMM TASK 72-21-00-000-007, AMM 72-21-00-300- 028. REPLACEMEN
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