Owner type
Corporation
Serial number
3835
Year built
2009
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
October 27, 2021
Certificate issued
October 22, 2021
Expires
October 31, 2028
Mode S code
AD474E

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every CFM International CFM56-5B4/3 model are included below.

On this page

Airworthiness directives that may apply · 381

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
ADs by the year they took effect: 545 ADs
19905
19911
19926
199310
199410
19954
19965
19979
199820
199914
200013
20018
200212
20033
200423
200520
200613
200716
20089
200913
20107
201112
201212
201317
201418
201523
201625
201724
201831
201923
202029
202116
202222
202319
202415
202521
202617
See all 545 ADs

Information bulletins that may apply · 8

Advisory, not mandatory.

Historical bulletins · 1

NTSB investigations

No NTSB investigations matched to N955AVMatched 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 N955AVMatched 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 2026FA0000880Hydraulic Line · looseHYD G RSVR LO LVL DURING CLIMB. IAW AMM 29-11-49-400-049-A REV 78, THE GREEN HCE PIPE#6 NUT WAS TORQUED AND ADJUSTED PROPERLY SATISFACTORY. THE OPERATIONAL TEST OF THE GREEN HYD SYS WAS PERFORMED SATISFACTORY IAW AMM 12-12-24-611-002-A THE GREEN RSVR WAS SERVOct 18, 2026 · N955AV · Airbus A320214 · Hydraulic System, MainSDR 2026FA0000585Warning Message · false activationBRAKES SYS 2 FAULT ON ECAM AFTER LANDING  GEAR RETRACTION. BITE TEST OF THE BSCU WAS PERFORMED SATISFACTORY IAW AMM 32-46-00-740-001-AJul 13, 2026 · N955AV · Airbus A320214 · Landing Gear Brake SystemSDR ANCF20233003009Unknown · unknownAFTER TAKE OFF WHEN SELECTING LANDING GEAR TO THE UP POSITION , L/G NOT UPLOCKED ECAM CAUTION APPEARED . L/G LEVER WAS RECYCLED UP TO TREE TIMES WITH UNSASTIFCTORY RESULTS. IN ACCORDANCE WITH TSM 32-31-00-810836-A L/G UPLOCK ORDOWMLOCK FAULT, THE NLG GROUND Mar 25, 2023 · N955AV · Airbus A320214 · Landing Gear Retraction/Extension SystemSDR ANCF2023011001001Ecu · malfunctionedIAW TSM 73-00-00-810-866-A REV.62 REV-, THE FAULT ISOLATION PARAGRAPH 4 STEP A ITEM 2, A TO F  WAS PERFORMED & SATISFACTORY . BOROSCOPE INSPECTION WAS ACCOMPLISHED  NO RELEVANT DISCREPANCIES FOUND, NORMAL DETERIORATION, IAW TSM 73-10-00-810-836 AT THE STEP AJan 4, 2023 · N955AV · Airbus A320214 · Fuel Controlling SystemSDR ANCF20221228006Idg · faultedELEC IDG 1 OIL LO PR DURING TAKE OFF APPROX 100KTS, ELEC IDG 1 OIL LO PR MESSAGE APPEARED ABORTED TAKE OFF WAS EXECUTED. INSPECTION OF THE AIRCRAFT AFTER BRAKE EMERGENCY APPLICATION WAS PERFORMED IAW AMM 05-51-16-200-001-A NO WERE FOUND DISCREPANDec 25, 2022 · N955AV · Airbus A320214 · AC Generator-Alternator

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