- Registered owner
- Aircol 19
- Location
- Wilmington, DE
- Owner type
- Corporation
- Serial number
- 4167
- Year built
- 2009
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- January 20, 2010
- Certificate issued
- October 6, 2010
- Expires
- October 31, 2029
- Mode S code
- A4EA7E
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 N416AVMatched 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 N416AVMatched 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 · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR ANCF2025081323Engine · bird ingestionDURING TAKE OFF ROLL BIRD STRIKE ON ENGINE ONE VIBRATION 2,7 ON ENGINE ONE AND N1 AND LOUD NOISE (2.7 VIBRATION ON N1 ENGINE NUMBER ONE) NO MAYDAY NO PAN PAN SUST PRIORITY DURING RETURN DURING CRUISE EGT DIFFERENCE 30 ° C ON ENGINE ONE LANDING WEIGHT 63.1 TSDR ANCF20240419009Idg · abnormalIN ACCORDANCE WITH TSM TASK 24-20-00-810-900-A, STEP A, ELECTRIC CHECK WAS PERFORMED. IDG PIN A9 TO IDG CASE - NO SHORT CIRCUIT IDG PIN A9 TO A10 - 8.92 OHM IDG PIN A9 TO GCU C12 - 1,21 OHM IDG PIN A10 TO GCU C13 - 1,22 OHM GCU PIN C12, C13, AND C7, NO SHORT SDR ANCF20191217101Accumulator · malfunctionedDURING TAKE OFF, REJECTED THE TAKE OFF DUE TO HYD BLUE LOW PRESSURE. IAW TSM 29-12-00-810-804-A, AND AMM 29-12-42 PB 401, THE HY ACCU BLUE WAS REPLACED. THE OPERATIONAL TEST WAS SASTIFACTORY. DID NOT SHOW MESSAGE IN ECAM. THIS AIRCRAFT RETURN TO SERVICE.SDR ANCF2018F00138Toilet · inoperativeTHREE TOILETS ARE INOPERATIVE.SDR ANCF2015060901Turbine Blades · damagedTAKE OFF WAS DISCONTINUED DUE TO ENG FAILURE BELOW 60 KTS, ENG 2 FAIL. DURING VISUAL INSPECTION AFTER TAKEOFF WERE FOUND ALL BLADES OF LAST TURBINE STAGE DAMAGED. ITS NECESSARY REMOVAL & INSTALL A NEW ENG.SDR ANCF2015043001Engine · vibratesENG 1 VIBRATION N1 EXCEED 10.5 AFTER TAKEOFF FOR 6 MINUTES, THRUST WAS REDUCED TO 55%, TO REDUCE ENG 1 VIBRATION BELOW 6.0. BORESCOPE INSPECTIONS WERE PERFORMED AT LPT 4TH STRINGER , BOOSTER 5TH STRINGER, HPC STAGES 1, 3, & 8, COMBUSTION CHAMBER DONE AREAS NOSDR ANCF2011052900080Unknown · odorAFTER ENGINE START THERE WAS A STRONG FUEL SMELL IN CABIN.
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