- Registered owner
- Avsa Leasing 3
- Location
- Wilmington, DE
- Owner type
- Corporation
- Serial number
- 3664
- Year built
- 2008
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- November 1, 2008
- Certificate issued
- October 31, 2008
- Expires
- August 31, 2028
- Mode S code
- A8C329
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 N664AVMatched 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 N664AVMatched 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 ANCF202509010027Lgciu · faultedLGCIU 1 FAULT WAS PRESENTED ON CRUISE. FOLLOWING TSM 32-31-00-810-807-A REV 73, REV DATE: 01-AUG-2025, WAS REMOVED AND REPLACED SELECTOR VALVE 41GA IAW AMM 32-31-34-000/400-001-A REV 73, REV DATE: 01-AUG-2025, TORQUE APPLIED THE SCREWS (1): 80 LB-IN, AND WAS SDR ANCF20250224002Steering Sys · abnormal41543SG AFT L/G DOWN WASSELECTED ON GROUND SYS RESET WAS MADE WITH UNSATISFACTORY BY RESULT IN ACCORDANCE WITH TSM 32-51-00-810-826-A AND AMM 32-51-51-000-001/400-001 SERVO CTL N/W STEERING (6GC) WAS REPLACED WITH TEST SATISFACTORYSDR ANCF20220921041Chip Detector · fodPILOT REPORT
17.SEP.2022 WO 16'689'419 => DURING FLIGHT ENG 1 STALL WITH HIGH VIBRATION OF 9.9 UNITS
ACTIONS TAKEN
18.SEP.2022 WO 16'689'419 => IN ACCORDANCE A.M.M. REV. 61 A.M.M. 79-21-10-000-007-A / 400-007-A CHECK THE SCAVENGE SCREEN OF ENGINE 1 FOUNSDR ANCF20210723001Pressure Switch · defectivePILOT REPORT, 22.JUL.2021 -> (WO 16438431) TAKEOFF WAS ABORTED AT 60KT DUE TO ECAM ANNUNCIATION HYD B PUMP LO PR AND HYD B SYS LO PR. CORRECTIVE ACTION, 23.JUL.2021 -> IN ACCORDANCE WITH AMM 29-12-07-000-001-A AND AND AMM 29-12-17-400-001-A THE ELECTRIC PUMP SDR ANCF201812270901Control Valve · malfunctionedDURING INITIAL CLIMB, PACK 2 REGULATOR FAULT WAS PRESENTED ON ECAM // CORRECTIVE ACTION: DEC 10. IN ACCORDANCE WITH AMM 21-51-51-000-001-A THE FLOW CONTROL VALVE WAS REMOVED // IN ACCORDANCE WITH AMM 21-51-51-400-001-ATHE FLOW CONTROL VALVE PACK WAS INSTALED, SDR ANCF2016010401Control Unit · malfunctionedAFTER POS 4 BACK, THE PARKING BRAKE DIDN'T WORK. AFTER CB'S RESET, ECAM MSG BRAKES ALTN BRK FAULT APPEARED. IAW AMM 32-43-34-000-+001400-001A THE ALTERNATE CONTROL UNIT, ABSU, WAS R & R. OPERATIONAL TEST WAS SATISFACTORY. PN E21328002, SN OFF S01420 & SN OSDR ANCF2015031102Brake · smokeDURING PUSH BACK BLACK SMOKE WAS EVIDENT OUT FROM MAIN BRAKE ASSEMBLY N°2. MAIN BRAKE ASSEMBLY N°2 & MAIN WHEEL N°2 WAS REPLACED IAW AMM 32-42-27 PB 401. TIRE PRESS WAS 210 PSI, PN 2-1684, SN OFF 8223, SN ON 8721, PN 3-1530, SN OFF A1645 & SN ON 9227.SDR ANCF2015012901Sense Line · faultyAFTER TAKEOFF ENG 1 BLEED FAULT CAME ON, APPROX 30 SECONDS AFTER THAT ENG 2 FAULT BLEED CAME ON ECAM. PERFORMED & SUCCESSFULLY IAW AMM 36-11-52-400-042-A BPRV & SENSE LINE WERE REPLACED. LEAK TEST WAS PERFORMED IAW AMM 36-11-52-790-001, NO LEAKS WERE FOUND. SDR ANCF2014FA0000375Control Unit · brokenDURING APPROACH, FLAPS LEVER BROKEN AT POSITION 2 LANDING SPEED, 149KT. THE CONTROL LEVER FLAP WAS R & R IAW MM 27-51-17, PB401 ND COMMAND SENSOR UNIT WAS REMOVED AND INSTALLED IAW AMM 27-54-00-710-002-A OPS TEST OF THE FLAP AND SLAT WAS SATISFACTORY.SDR ANCF2012090700129Engine · bird ingestionAFTER T/O IN CLO PASSING 6000FT, BIRD STRIKES RIGHT ENGINE IMMEDIATE RETURN, ENG VIBRATION WENT UP TO 9.2 N1, MODERATE VIBRATION OTHER PARAMETERS WERE NORMAL. IN ACCORDANCE WITH AMM 05-51-19 PB 601 TASK 72-00-00-200-006-A ITEM 4-A(8) AND B (2)(A)(B) BOROSCOPSDR ANCF2011022700074Light · failedPILOT REPORT: UPDATING C/E MCDU DURING THE PREFLIGHT, A STRONG BEAN OF LIGHT ACCOMPANIED BY A SHORT CIRCUIT EXPLOSION WAS FELT ON KERAKER PANEL 122VU THE EXPLOSION WAS FELT WITH SOME LIGHT VOLTS, IMMEDIATELY EVACUATED. IN ACCORDANCE WITH AMM 24-00-00-810-823SDR ANCF2010033000060Iru · faultyPILOT REPORT: NAV IR 1 FAULT ECAM ILLUM. GROUND RETURN. THE ADIRU NR 1 WAS REPLACED IAW AMM 34-12-34-400-001, OPERATIONAL TEST ON GROUND.SDR ANCF09123000056AController · malfunctionedAIR TURN BACK. LT AND RT AILERON FAULT WAS PRESENTED AFTER TAKE OFF. IAW TSM 27-95-00-810-802 FAILURE OF THE FCDC 2 WAS PERFORMED AND TEST OK AND AMM 27-96-00-740-0021 THE BITE TEST OF THE EFCS GROUND SCANING WAS PERFORMED AND SATISFACTORY.
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