- Registered owner
- Aircol 22
- Location
- Wilmington, DE
- Owner type
- Corporation
- Serial number
- 4821
- Year built
- 2011
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- October 1, 2011
- Certificate issued
- September 30, 2011
- Expires
- September 30, 2027
- Mode S code
- AB34A6
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 N821AVMatched 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 N821AVMatched 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 ANCF20220202008Engine · bird ingestionPILOT REPORT
29.JAN.2022 WO 54'349'122=> BIRD STRIKE ENG 1 RETURN TO BOG.
29.JAN.2022 WO 54'349'123=> OVERWEIGHT LANDING AT SKBO 67500 (NO HARD LANDING ).
CORRECTIVE ACTIONS
30.JAN.2022 WO 54'349'122 => IN ACCORDANCE WITH AMM 05-51-19-200-001-A THE PNEUMSDR ANCF2020030301Static Inverter · malfunctioned03.MAR.2020 @ CTG -> FLIGHT AV8548 (BOG-CTG) PILOT REPORT WO 16056958:
AFTER PARKING IN CTG THE CABIN WAS FULL OF SMOKE AND FUMES WAS FELT
03.MAR.2020 @ CTG -> DEFERRED MAINTENANCE ITEM AS FOLLOWS:
IN ACCORDANCE WITH TSM 05-50-00-810-831-A IDENTIFICATION SDR ANCF2019040833119Proximity Sensor · out of adjustAFTER TAKE OFF DOOR FWD CARGO DOOR ECAM ALERT POP OUT ON ECAM. IN ACCORDANCE WITH AMM 52-31-00-710-001 OPERATIONAL TEST OF THE FWD CARGO COMPARTMENT DOOR WAS ACCOMPLISHED, AMBER INDICATION WAS SHOWN. PFR FWD CARGO DR SAFETY MECHANISM PROX SNSR (30WV) TGT POSSDR ANCF2017102500001Electrical Box · failedDURING CLIMB, THE NR 1 ENGINE EGT INDICATION DISPLAYED, AMBER CROSSES WITH NO ECAM ALERT TRIGGERED. IAW TSM 77-20-00-810-826-A FOUND RESISTANCE VALUES OUT LIMITS IN THE MAIN JUCTION BOX IAW AMM 77-21-10-000/400-025-A. THE MAIN JUCTION BOX WAS REPLACED.SDR ANCF2017041701Engine · malfunctionedIN T/O ROLL RT ENGINE EGT OVERLIMIT APPEARS ON ECAM. TSM 72-00-00-200-008-A WAS ACCOMPLISHED; DAMAGE IS LOCATED ON AREA C. THE DECISION TO REPLACE THE ENGINE.SDR ANCF2015032401Pressure Switch · faultyAFTER ENG 1 START ELAC 1 PITCH FAULT WAS PRESENTED ON ECAM. IAW AMM 27-92-17 PB 401
PRESS SWITCH HYD FLIGHT CONTROL, 10CE1, WAS REPLACED, TESTED SATISFACTORY. IAW AMM 27-94-34 PB 401 THE SECOND ONE WAS REPLACED, TESTED OK.SDR ANCF2015032001Warning System · false activationBEFORE TAKEOFF ELAC 1 PITCH CONTROL FAULT MSG APPEARS. IAW AMM TASK 27-93-00-810-947 FALSE ELAC WARNING WAS PERFORMED & NO HELP. TRANSFER TO DMI 257 MEL 27-93-01 CAT B. IAW AMM 27-93-00-040-001A TEST WAS PERFORMED SATISFACTORY & IAW MEL 27-93-01.L THE PROC
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