Owner type
Corporation
Serial number
3980
Year built
2009
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
July 28, 2009
Certificate issued
July 27, 2009
Expires
December 31, 2027
Mode S code
ADAB38

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
ADs by the year they took effect: 558 ADs
19905
19911
19926
199310
199410
19954
19965
199710
199822
199914
200015
20019
200215
20033
200423
200520
200613
200716
200810
200913
20108
201112
201212
201317
201418
201523
201625
201724
201831
201924
202029
202117
202222
202319
202415
202521
202617
See all 558 ADs

Information bulletins that may apply · 8

Advisory, not mandatory.

Historical bulletins · 1

NTSB investigations

No NTSB investigations matched to N980AVMatched 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 N980AVMatched 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 ANCF20260810016Fwc · abnormalSLATS DOES NOT RETRACT TO 0° POSITION.REMOVED AND REPLACED FLIGHT WARNIG COMPUTER (1) IAW AMM 31-53-34-400-001-A, FLIGHT CONTROLS TEST OK, GOOD FOR SVC PERFORMED TSM 31-53-00-810-878-A LOSS OF THE RH SLTAug 10, 2026 · N980AV · Airbus A320214 · Leading Edge Slat Control SystemSDR ANCF20231225038Windshield · crackedAIRCRAFT RETURN TO KMIA DUE TO WINDOW CRACKED FO SIDE, NO OVERWEIGHT LANDING THE F/O SIDE WINDSHIELD WAS REMOVED AS PER AMM 56-11-11-000-001A, AND  REPLACED AS PER AMM 56-11-11-400-001A FROM STEP TO STEP 4 G.3, TOOL USED QD2R200 S/N 0681402946 DUE DATE MAY Dec 25, 2023 · N980AV · Airbus A320214 · Flight Compartment WindowsSDR ANCF20232403007Pump · unserviceablePILOT REPORT 11-MAR-23 WO 17'202'358 => ELEC HYD BLUE PUMP OVERHEAT ACTIONS TAKEN 11-MAR-23 WO 17'202'358 => PERFORM TSM 29-12-00-810-806-A. 12-MAR-23 WO 17'202'358 => DUE TO ELEC HYD BLUE PUMP OVERHEAT IAW TSM 29-12-00-810-806-A REV 63 WAS REMOVED ANMar 11, 2023 · N980AV · Airbus A320214 · Hydraulic Pump (Electric/Engine), MainSDR ANCF20230501007Vbv · unknownPILOT REPORT 31.DIC.2022 WO 12'667'812 => MANDATORY: PERFORM EOD- EOD-32S-75-0001-R06 COMPONENT (ENGINEERING ORDER DETAIL) REV. 06 PARTNO : CFM56-5B4/3 / SERIALNO : 643277 ENGINE A320 POS: ENGLH ENGINE-RE-GREASING OF THE VBV SYSTEM 31.DIC.Dec 31, 2022 · N980AV · Airbus A320214 · Engine Bleed Air SystemSDR ANCF20221010029Engine · bird ingestionPILOT REPORT 06.OCT.2022 WO 1'860'682 => BIRD STRIKE ON ENG 1 ENG 1 STALL ACTIONS TAKEN NOT DEFINED YET, ACTIONS TAKEN IN PROCESSOct 6, 2022 · N980AV · Airbus A320214 · Engine (Turbine/Turboprop)SDR ANCF20220725028Valve · not reportedPILOT REPORT 23.JUL.2022 WO 54'337'534 => DURING INITIAL CLIMB AFTER T/O AFTER DURING INITIAL CLIMB AFTER T/O AFTER PACKS WHERE ON VENT AVNCS SYS FAULT PRESENTED ON ECAM INMEDIATLY AFTER CAB PR EXCESS CAB ALT ON ECAM. ACTIONS TAKEN 23.JUL.2022 WO 54'337Jul 23, 2022 · N980AV · Airbus A320214 · Air Conditioning SystemSDR ANCF201911080080Apu · unknownDURING PREFLIGHT PROCEDURES APU AUTOSHUTDOWN WAS SHOWN ON ECAM PAGES F/O & MAINTENANCE PERSONNEL FELT AND EXPLOSION ON THE OUTSIDE APU SECTION.Nov 8, 2018 · N980AV · Airbus A320214 · Airborne Auxiliary Power Unit (APU) SystemSDR ANCF2019F00093Mechanism · malfunctionedINFORMATION ABOUT COCKPIT DOOR MECHANISM NO LOCKING.Oct 23, 2018 · N980AV · Airbus A320214 · Fixed Inner DoorsSDR ANCF2016080901Tachometer · failedDURING TAKE OFF ROLL AT 50 KT, BRAKES RELEASE ILLUMINATED ON ECAM. REJECTED TAKE OFF. IN THE STATUS PAGE AUTOBRAKE WAS INOPERATIVE. IN ACCORDANCE WITH TSM 32-42-00-810-815-A THE BSCU TEST SHOW TACHOMETER 4 (22GG). IN ACCORDANCE WITH AMM 32-42-57 PB 401 CONFAug 9, 2016 · N980AV · Airbus A320214 · Landing Gear SystemSDR ANCF2015030807Connector · looseAFTER ENG 1 START, EGT REMAINED AT 60 & EGT OF ENG 2 WAS 490. IAW TSM 77-20-00-810-803-A LOSS OF THE EGT THERMOCOUPLE SIGNAL TO THE ECU ON ENG 1 WAS PERFORMED. IAW AMM 77-21-10-200-002-A INSPECTION CHECK OF THE T 495 THERMOCOUPLE LE WIRING HARNESS WAS PERFORMar 9, 2015 · N980AV · Airbus A320214 · Engine Indicating System WiringSDR ANCF20150224001Support Rib · crackedDETAILED INSPECTION OF HORIZONTAL STABILIZER HINGE FITTINGS & SUPPORT RIBS. ON C CHECK OF THE ACFT, MSN-3980, DURING ACCOMPLISHMENT OF MPD TASK 551020-01 IN RT HORIZONTAL STABILIZER, FOUND CRACKS ON SUPPORT RIBS NR 5 & 6. CRACK LENGTH 41MM, SUPPORT RIBS 6, Feb 24, 2015 · N980AV · Airbus A320214 · Horizontal Stabilizer, Spar/RibSDR ANCF2012120100139Hydraulic Line · brokenDURING APPROACH AFTER LANDING DOWN SELECTION GREEN HYD RSVR LOW PRESSURE ON ECAM1. THE FLEXIBLE HOSE ASSEMBLY OF MLG DOOR ACTUATOR WAS REPLACED THE OPERATIONAL TEST OF LANDING GEAR DOOR (WITHOUT FALSE TARGETS), CHECK V/V 3083 GM WAS REPLACED. RESULTS SATISFADec 1, 2012 · N980AV · Airbus A320214 · Hydraulic System, MainSDR ANCF2011121800103Slide · partial deployDURING WALK AROUND LT AFT SERVICE DOOR SLIDE WAS ACTIVATED BY FLIGHT ATTENDANT. IN ACCORDANCE WITH AMM 25-62-44-000-007A /400-007A THE LT AFT OF THE ESCAPE SLIDE ROFT PACK ASSEMBLY WAS REMOVED AND REPLACED AND AMM 52-10-00-610-001A THE DIAPHRAGM IN THE PERCUSDec 18, 2011 · N980AV · Airbus A320214 · Escape Slide

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