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N939AV

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2011 Airbus A320-214 · CFM International CFM56-5B4 series

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Registered owner
Aircol 24
Location
Wilmington, DE
Owner type
Corporation
Serial number
4939
Year built
2011
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
December 20, 2011
Certificate issued
December 19, 2011
Expires
December 31, 2027
Mode S code
AD072C
Airbus A320-214Airframe model · 182 seats · 2 engines · 160 registeredTCDS A28NMAirframe · Airbus A320-214Engine modelCFM International CFM56-5B4 series

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.

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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.

1990In forceSuperseded2026
See all 558 ADs

Information bulletins that may apply · 8

Advisory, not mandatory.

Historical bulletins · 1
SAIB NE-08-17R2Turbine Section - Propulsion Technology LLC Unapproved RepairIssued Mar 7, 2011

NTSB investigations

No NTSB investigations matched to N939AVMatched 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 N939AVMatched 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 · 5

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR ANCF20240322008Compressor · slowENG 2 COMPRESSOR VANE ENG2 SLOW RESPONSE WO 54'702'467 - REPLACE THE ECU PERFORMED RII INSPECTION AFTER REPLACEMEN ECU IAW AMM 73-21-60-000-001-B AND AMM 73-21-60-400-001-B REV 67, THEM PERFORMED FUNCTIONAL TEST IAW AMM 73-21-60-720-040-B REV 67 TEST IS OK ANMar 22, 2024 · N939AV · Airbus A320214 · Turbine Engine Compressor SectionSDR ANCF20220601021None · nonePILOT REPORT 29.MAY.2022 WO 54'424'191=> (AFT T.O. ECAM) AFT T.O. ECAM ALERT L/G SHOCK ABSORBER FAULT ACTIONS TAKEN IN PROCESSMay 29, 2022 · N939AV · Airbus A320214 · Landing Gear SystemSDR ANCF20220316003Vane · nonePROBLEM 11.MAR.2022 WO 54'386'879=> IN ACCORDANCE TSM 75-30-00-810-837-A FAILURE OF THE CONTROL OF THE VBV ACTUATOR ON ENGINE 1-CHANEL B-FAULT CONFIRMATION WAS PERFORMED IN ACCORDANCE AMM 73-29-00-710-040 OPERATIONAL TEST OF FADEC 1B ON THE GROUND (WITH ENGMar 11, 2022 · N939AV · Airbus A320214 · Compressor Bleed ControlSDR ANCF20210830015Outflow Valve · faultedDURING CLIMB PASS ING 26000 FEET SAFETY VALVE ECAM COME OUT FALLOW V/S INCREASED BY 2.500 FT/M AT 7.4 PSI. IAW AMM 21-31-52 PB 401 CONF 00 THE SAFETY VALVES 6HL AND 7HL WERE REPLACED BY MCC SUGGESTION. IAW AMM TASK 21-31-00-710-006-A OPERTAIONAL TEST SATISFAug 29, 2021 · N939AV · Airbus A320214 · Pressure Regulator/Outflow ValveSDR ANCF2019102892201Engine · failedATB. SEP 22. ATB: DURING LIFT OFF ENG 2 FAIL + ENG 2 SHUT DOWN // CORRECTIVE ACTIONS: OCT 9. IN ACCORDANCE WITH JIC -32S-71-000245 RV 00 AND AMM 71-00-00-000-042-A/400-042-A THE ENGINE 2 WAS REMOVED AND REPLACED, THE OPERATIONAL TESTS WERE PERFORMED WITH SATISSep 22, 2019 · N939AV · Airbus A320214 · Engine (Turbine/Turboprop)

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