- Registered owner
- Aircol 23
- Location
- Wilmington, DE
- Owner type
- Corporation
- Serial number
- 4862
- Year built
- 2011
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- October 18, 2011
- Certificate issued
- October 17, 2011
- Expires
- October 31, 2027
- Mode S code
- ABD659
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 N862AVMatched 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 N862AVMatched 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 · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR V2JA202606250541Pressure Switch · faultedDURING FLIGHT HYD GREEN RESERVOIR LOW LEVEL. PERFORMED AMM 29-11-49-210-002-A REV.77 REV-. VISUAL INSPECTION OF THE HYD HOSES AND TUBES OF ENG NR 1 FOUND HYD LOW-PRESSURE SWITCH TUBE WITH SEVERAL HYD LEAK. REPLACED THE HYD LOW PRESSURE SWITCH TUBE IAW AMMSDR ANCF20250330005Sense Line · leakingENGINE 2 BLEED FAULT IN FLIGHT DUE TO PNEUMATIC AIR LEAK WAS REMOVED AND REPLACED THE SENSE LINE BTW THE PRV AND THE PYLON INTERFACE ON ENGINE #2 I.A.W AMM 36-11-49-000/400-026-A REV 71 REV DATE 01-FEB-2025 AND PERFORMED LEAK CHECK I.W.A AMM 36-11-52-790-001-ASDR ANCF20220917038Blade · bird ingestionPILOT REPORT
15.SEP.2022 WO 16'702'588=> DURING TAKE OFF ROLL REJECTED TAKE OFF DUE TO MULTIPLE BIRD STRIKES. HIGH SPEED REJECTED TAKE OFF, NO CHANGES ON ENGINES PARAMETERS.
ACTION TAKEN
15.SEP.2022 WO 16'702'588=> INSPECTION OF THE AIRCRAFT AFTER A BIRD SDR 2021F00327None · nonePILOT REPORT – WO 15663695: 01-DEC-2021=> AUTO FLT RUD TRV LIM 1 FAULT CAME ON ECAM.
CORRECTIVE ACTION: 02-DEC-2021=> IN ACCORDANCE WITH TSM 22-61-00-810-803-A PREV LEG REP, CORRELATED FAILURE AND POST RLT REPORTS SHOW FAC1/RTL ACTR (4CC) = REPLACE THE ELECSDR 2021F00326None · nonePILOT REPORT – WO 15663695: 01-DEC-2021=> AUTO FLT RUD TRV LIM 1 FAULT CAME ON ECAM.
CORRECTIVE ACTION: 02-DEC-2021=> IN ACCORDANCE WITH TSM 22-61-00-810-803-A PREV LEG REP, CORRELATED FAILURE AND POST RLT REPORTS SHOW FAC1/RTL ACTR (4CC) = REPLACE THE ELECSDR ANCF20200311001Brake Assy · hot10.MAR.2020 @ BOG -> FLIGHT AV9716 (BOG-BAQ) PILOT REPORT WO 16176367:
DURING TAKE OFF ROLL, BRAKES HOT APPEAR ON ECAM BRAKE #4 WAS AT 310°C AND OTHERS WERE AT 150°C OR BELOW
10.MAR.2020 @ BOG -> CORRECTIVE ACTION AS FOLLOWS:
IN ACCORDANCE WITH AMM 32-SDR ANCF2017102500002Stop · warning messageDURING TAKE OFF ROLL, ENGINE COMPRESSOR VANE 80KTS. STOP MECHANISM WAS REPLACED IAW AMM 75-31-20 PB401.SDR ANCF2017030201Unknown · malfunctionedDURING APPROACH AFTER SELECTING LG DOWN A/P DISCONNECTED AUTOMATICALLY AND A/C BECOME ON DIRECT LAW WITH NO FAILURE INDICATION WHEN G/AROUND AND WITH LG RETRACTED. A/C BECOME ON NORMAL LOW AGAIN (RA+2) WORKED PROPERLY. DUE FAILURE MSG IN PFR AFS ELAC 2. TROUBLSDR ANCF2016041102Warning System · unknownREJECTED TAKEOFF APPROX AT 80 KTS DUE TO NAV ADR 2 FAULT & AOA SENSOR 2. IAW TSM 34-11-00-810-830-A LOSS OF THE ANGLE OF ATTACK SENSOR 2 & TASK AMM 34-13-00-740-002-A WAS PERFORMED INTERFACE TEST OF THE ADRIS, TESTED SATISFACTORY NO FOUND FAULT PRESENTED.SDR ANCF2016041101Warning System · unknownREJECTED TAKEOFF APPROX AT 80 KTS DUE TO NAV ADR 2 FAULT & AOA SENSOR. IAW TSM 34-11-00-810-830-A LOSS OF THE ANGLE OF ATTACK SENSOR 2 & TASK AMM 34-13-00-740-002-A WAS PERFORMED INTERFACE TEST OF THE ADRIS, TESTED SATISFACTORY NO FOUND FAULT PRESENTED.SDR ANCF2015030809Light · inoperativeDURING TAXI, TAXI & TAKEOFF LIGHT INOPERATIVE & RT LANDING LIGHT INOPERATIVE. IAW AMM 33-46-11-960 001-A & AMM 33-46-12-960-001-A THE TAXI & TAKEOFF LIGHT WERE REPLACED. OPERATIONAL TESTED SATISFACTORY. IAW AMM 33-42-11 PB 401 THE RT LANDING LIGHT UNIT WAS SDR ANCF2013131000173Actuator · failedMASTER CAUTION, ENGINE 1 COMPRESSOR VALVE DURING TAKEOFF, APROXIMATE AT 80 KNTS, IAW AMM 75-31-50-000-002A AND AMM 75-31-50-400-002A THE BLEED VALVE AND MASTER BALL SCREW ACTUATOR ASSY IN LT ENGINE WAS R & R, PERFORMED OPS TEST ON GROUND MINIMUM IDLE SATISFACSDR ANCF2012062700125Valve · malfunctionedDURING APPROACH I PEI AFTER FLAPS 3 SELECTION BRAKES ALTN L RELEASED NO AUTO BRAKE WAS USED FOR LANDING NORMAL BRAKES OPERATED NORMALLY AND WERE APPLIED AT APPROX 60 KTS. IN ACCORDANCE WITH MM TASK 32-43-35-400-001 REMOVED OF THE ALTERNATE BRAKE DIRECT DRIV
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