Registered owner
Aircol 7 Trust
Owner type
Corporation
Serial number
3992
Year built
2009
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
August 11, 2009
Certificate issued
June 4, 2024
Expires
June 30, 2031
Mode S code
ADDA25

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 N992AVMatched 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 N992AVMatched 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 · 12

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

SDR ANCF20250421008Sensor · false indicationECAM ENG 1 FIRE DURING INITIAL CLIMB PASSING 300-400FT  ECAM ENG 1 FIRE APPEARED ON ECAM NACELLE TEMP SENSOR WAS PULSING IAW AMM 36-11-53-04 CONF 00 REV 71 DATE 01 FEB 2025 OVERPRESSURE VALVE WAS REPLACED. I.A.W AMM 36-11-52-4 CONF 06 REV 71 DATE 01 FEB 2025 PApr 21, 2025 · N992AV · Airbus A320214 · Fire DetectionSDR ANCF20231230040Sensor · abnormalAFTER TAKE OFF & MLG WAS SELECTED UP ECAM INDICATION MLG NOT UPLOCKED IAW INSTRUCTIONS GIVEN ON THE JIC-32S-31-00069 REV. 03 THE PERSONAL COMPUTER MEMORY CARD (PCMCIA) DATA DOWNLOADING WAS PERFORMED IAW AMM 32-31-73-000-005-A/400-005-A THE NLG PROXIMITY-SENSODec 30, 2023 · N992AV · Airbus A320214 · Landing Gear Position and WarningSDR ANCF20232505015Solenoid · faultedFLI AV9823, DURING CLIMB - AIR ENGINE2 BLEED FAULT - ON ECAM - ENG BLEED RESET SUCCESFUL - CAB PR EXCEESS - CAB ALT. IN ACCORDANCE WITH AMM 36-11-43-100-001 AND 05-53-00-780-002 THE TERMOSTAT CONTROL SOLENID WAS REMOVED AND REPLACED AND PRESURIZATION TEST May 19, 2023 · N992AV · Airbus A320214 · Engine Bleed Air SystemSDR ANCF20220124001Hydraulic Line · chafedREPORT: JANUARY 20TH 2022, ON FLIGHT AV257 CUN-BOG, THE AIRCRAFT N992AV HAD THE NEXT REPORT "DURING CRUISE THE YELLOW HYDRAULIC PUMP PRESENTED FAILURE OF HYD Y RSVR LO LVL", IT DEVIATION TO ADZ ALTERNATE AIRPORT. CORRECTIVE ACTION: IN ACCORDANCE WITH AMM SJan 20, 2022 · N992AV · Airbus A320214 · Hydraulic System, AuxiliarySDR ANCF2021115005None · noneREPORT PILOT: 02.NOV.2021=> DURING DESCENT AT 20000 FT CAB HI ALT DOOR R AFT CABIN CAB PR LO DIFF PR CAB PR SAFETY VALVE OPEN ACTION CORRECTIVE: 05.NOV.2021=> IN ACCORDANCE WITH AIRBUS CONSULT #80985779 THESE MM (FAULTS) WERE PRESENTED BY ERROR CONFIGURANov 2, 2021 · N992AV · Airbus A320214 · Cabin Pressure Control SystemSDR ANCF20201230003Windshield · brokenON DECEMBER 27/2020, DURING FLIGHT AV9258 FROM MEDELLIN (MDE)-SANTA MARTA (SMR), AIRCRAFT N992AV DURING CLIMB THERE WAS DAMAGE TO WINDSHIELD LT. AIRCRAFT RETURNED FROM FLIGHT. PILOT REPORT (16185731) LT WINDSHIELD BROKEN. DURING CLIMB 12.000 FTS ALL THE WINDec 27, 2020 · N992AV · Airbus A320214 · Flight Compartment WindowsSDR ANCF2015022002Oven · odorINTENSE SHORT CIRCUIT ODOR IN THE CABIN. FLIGHT ATTENDANT REPORTED A GALLEY MAY BE FWD OVEN, STRONG NOISE AT THE SAME TIME. IAW AMM 25-35-19-PB 401 THE OVEN OF GALLEY FWD WAS R & R. OPERATIONAL TEST WAS PERFORMED WITH SUCCESSFUL RESULT & ADDITIONAL TSM AMM Feb 20, 2015 · N992AV · Airbus A320214 · Buffet/GalleysSDR ANCF2015010401Control Unit · malfunctionedAFTER LANDING AT APPROX. 70 KNOTS WHEEL NW STEER FAULT. THE BSCU WAS RESET UNSUCCESSFULLY. IAW TASK AMM 32-42-34-000 400-001-A REMOVAL & INSTALLATION OF THE BRAKING & STEERING CONTROL UNIT BSCU WAS DONE THE BITE TEST OF THE BSCU IS OK. PN E2132700 SN OFF 34Jan 4, 2015 · N992AV · Airbus A320214 · Landing Gear Steering SystemSDR ANCF2015010301Controller · failedAFTER TAKEOFF WHEEL NW STEERING FAULT. IAW TSM 32-51-00-810-811-A FAILURE OF THE NOSE WHEEL STEERING WAS ACCOMPLISHED & AMM 32-51-51-000-400- 001-A THE NOSE WHEEL STEERING SERVO CONTROL WAS R & R. AMM 32-51-00-710-004-A & 32-51-00-720-A FUNCTIONAL TEST OF THJan 3, 2015 · N992AV · Airbus A320214 · Steering UnitSDR ANCF201412271Bleed Valve · faultedENG 1 CTL VLV FAULT, TBV VLV, J11, ECU ENG 1A. PERFORMANCE TSM 75-26-00810-809-A & IAW AMM 75-26-10-000-001 400-001-A REPLACED THE TRANSIENT BLEED VLV. IAW AMM 71-00-00-710-006 MINIMUM IDLE CHECK WAS PERFORMED.Dec 27, 2014 · N992AV · Airbus A320214 · Compressor Bleed ValveSDR ANCF2014FA0000374Shaft · brokenDURING TAKEOFF ROLL, AT APPROXIMATELY 80 KNOTS, A STRONG HIT WAS FELT AND HEARD, LIKE A TIRE BURST, ACFT YAWED TO THE LEFT WHILE CAPTAIN TRIED TO KEEP IT ON THE CENTER LINE. A REJECTED TAKEOFF WAS PERFORMED. PERFORMED INSPECTION IAW AMM 72-00-00200-008-A, FJun 6, 2014 · N992AV · Airbus A320214 · Compressor Bleed ValveSDR ANCF2012033100117Sensor · failedECAM LT WINDSHIELD HEAT INOPERATIVE. IN ACCORDANCE WITH TSM TASK 30-42-00-810-801-A-LOSS OF THE LEFT WINDSHIELD TEMPERATURE SENSOR WAS PERFORMED TEST OK ON MCDU.Mar 31, 2012 · N992AV · Airbus A320214 · Windshield/Door Rain/Ice Removal

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