- Registered owner
- Aircol 6 Statutory Trust
- Location
- Wilmington, DE
- Owner type
- Corporation
- Serial number
- 3988
- Year built
- 2009
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- August 4, 2009
- Certificate issued
- June 14, 2024
- Expires
- June 30, 2031
- Mode S code
- A4A095
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 N398AVMatched 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 N398AVMatched 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 · 10
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR ANCF20241002018Tailpipe · fireAFTER BOTH ENGINE SHUTDOWN TAIL PIPE FIRE ON ENG 2 OBSERVED BY RAMP PERSONAL IAW TSM 72-00-00-810-A THE TRF WAS INSPECTED, THE INLET COVER PACKING AND INLET COVER SEAL WERE REMOVED AND REPLACED. NO MORE DAMAGES WERE FOUND. THE MINIMUM IDLE LEAK CHECK TEST WASDR ANCF20230713017Motor · unserviceableDURING TAKE OFF ROLL, ENG 1 COMPRESSOR VANE ON ECAM, A LOW SPEED REJECTED TAKE OFF WAS PERFORMED. ENG 1 WAS SHUTDOWN DURING TAXI-IN. (13:45 UTC) REPLACEMENT OF THE BLEED VALVE FUEL GEAR MOTOR ASSEMBLY WAS PERFORMED IAW AMM: 75-31-10-000/400-002-A REV 64 OF 0SDR ANCF20200317601Actuator · unserviceable16.MAR.2020 @ BOG -> FLIGHT AV8460 (BOG-VUP) PILOT REPORT WO 15941285:
GROUND RETURN DUE TO STRONG SMELL ON COCKPIT AND CABIN SIMILAR TO DIRTY SOCKS, REMAINS EVEN WITH USE OF APU BLEED AND BOTH ENGINES BLEED.
16.MAR.2020 @ BOG -> CORRECTIVE ACTION AS FOLLSDR ANCF2016080201Windshield · crackedDURING FLIGHT REACHING FL310, SUDDEN SEVERE TURBULENCE WAS ENCOUNTERED. RT WINDSHIELD CRACKED AND ECAM RT WINDSHEILD HEAT ILLUMINATED. TURBULENCE SPEED WAS SELECTED PRIOR ENCOUNTER. MACH 0,76. IAW AMM 56-11-11-000-001-A01, REMOVED THE RIGHT WINDSHIELD, ANDSDR ANCF2015060201Computer · malfunctionedRETURNED DUE TO PRESSURIZATION PROBLEM, AVNCS VENT SYS FAULT. IAW AMM 21-26-34 PB 401 CONF 00 & AMM 21-26-00-040 440-003-A THE AVIONICS EQUIP VENTILATION COMPUTER & CONDITIONED AIR INLET V7V WERE REPLACED. TESTED SATISFACTORY.SDR ANCF2015040201Control Valve · malfunctionedZONE TEMPERATURE INDICATORS SHOWS 32°C & THE 3 SECTIONS OF THE ACFT & IT WAS IMPOSSIBLE TO CONTROL TEMPERATURE. IAW AMM TASK 21-52-21-000 400-002A THE COMPRESSOR INLET GASKET OF PACK, RT & LT, WAS REPLACED & DID NOT HELP. IAW AMM 21-51-51-000 400 001-A THE PSDR ANCF2015010601Warning System · false activationDURING TAKEOFF RUN RETARD ANNUNCIATION WAS PRESENTED BETWEEN 90 & 100 KNOTS. IAW AMM 34-42-00-740-002 BITE TEST OF RADIO ALTIMETER PERFORMED SATISFACTORY & AMM 22-96-00-710-001 OPERATIONAL TEST OF THE AFS PERFORMED SATISFACTORY. IAW TSM TASK 05-50-00810-825-SDR ANCF2014F00102Landing Gear · malfunctionedAFTER TAKEOFF WHEN LANDING GEAR WAS SELECTED UP, APPEARED LANDING GEAR NOT UPLOCKED, MLG SHOCK ABSORBER FAULT. ACFT DIVERTED, WITH ACFT ON GROUND, JACKED AND THE FAULT WAS CONFIRMED, MAINTENANCE REPLACED 24GA AND 25GA SENSORS, AS WELL AS LGCIU NR 2, BUT THOSESDR ANCF2012062300124Engine · bird ingestionDURING TAKEOFF BIRD STRIKE AT ENGINE NUMBER 2 POWER LOSS WAS FELT. BOROSCOPE INSPECTION OF THE BOASTER STAGE 5 HPC STAGES 1, 3 AND 8 COMBUSTION CHAMBER DOME AREA, WAS ACCOMPLISHED IAW AMM TASK 72-00-00-280-057-A ITEM B, (2) FOD ASSOCIATED WITH ABNORMAL ENGINSDR ANCF2012011800109Slide · failedLEFT FORWARD SLIDE, DURING OPENING DOOR ARMED. (THE SLIDE WAS DEPLOYED AUTOMATICALLY BUT THE BOTTLE DID NOT ACTIVATE). IAW 25-62-44PB 401 THE ESCAPE-SLIDE PACK ASSY DOOR 1L WAS R & R.
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