Registered owner
Umb Bank Na Trustee
Owner type
Corporation
Serial number
5238
Year built
2012
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
August 9, 2012
Certificate issued
February 23, 2023
Expires
February 28, 2030
Mode S code
A91B2B

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.

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 N686TAMatched 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 N686TAMatched 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 · 9

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

SDR RJEF20263108001Fan · faultedCABIN PRESSURE EXCESS CAB ALTITUDE DISPLAYED ON ECAM PROCEDURE WAS MADE ACCORDING TO OEB 61. PERFORMED GENERAL VISUAL INSPECTION ON AVIONICS VENTILATION DUCTS AND WERE FOUND 3 DUCTS WITH CRACK BTW LATERAL AVIONICS COMPARTMENT RH AND AFT AVIONICS COMPARTMENT. Aug 31, 2026 · N686TA · Airbus A320214 · Air Distribution FanSDR RJEF20260106001Unknown · vibrationNR 1 ENG HIGH VIBRATION DURING TAKE OFF ROLL OUT 95 KTS APROXIMATE, IAW AMM 72-21-00-210-804-A DETAILED INSPECTION AND RELUBRICATION OF THE FAN BLADES, DOVETAILS, MIDSPAN SHROUDS, SPACERS, PLATFORMS AND FAN DISK DOVETAILS SLOTS WERE PERFORMED SATISFACTORY. TSMJan 6, 2026 · N686TA · Airbus A320214 · Engine (Turbine/Turboprop)SDR 2023FA0000676Unknown · unknownDURING WALK AROUND AS PART OF THE PRELIMINARY INSPECTION OF THE AIRCRAFT FOR MAINTENANCE SERVICE, WERE FOUND 2 BROKEN FASTENERS ON RH WASTE SERVICE PANEL AND CORROSION AT LOWER AFT CORNER OF WASTE SERVICE PANEL CUT OUT. ADDITIONAL, CLAMP-SHELLS HOLDING THE WAOct 20, 2023 · N686TA · Airbus A320214 · Fuselage Structure (General)SDR RJEF20230814001Valve · inoperativeVENT AVNCS SYS FAULT AFTER TAKEOFF PHASE AND NO OVERWEIGHT LANDING. DEFERRED SKINK AIR OUTLET VLV IAW MEL 21-26-04 CAT C REV 35 25 APR 22 MAIN FLAP´PLACED IN FULL CLOSED POS AND INTERNAL FLAP IN OPEN POS AT LWR ECAM DU THE VLV STAYS AT 45° SKIN HEAT XCHANGERAug 11, 2023 · N686TA · Airbus A320214 · Air Conditioning SystemSDR RJEF20210322001Slat · damagedBIRD STRIKE ON LEFT WING DURING APPROACH. ACTION TAKEN: AS PER TSM TASK 05-50-00-810-803-A AND AMM TASK 05-51-14-200-803-A, PERFORMED INSPECTION OF THE AIRCRAFT AFTER BIRD STRIKE, AND ONLY L/H WING, SLAT #1 WAS FOUND DAMAGED, NO MORE DAMAGES FOUND. DENTS WEREMar 21, 2021 · N686TA · Airbus A320214 · Leading Edge DevicesSDR RJEF20201204001Controller · malfunctionedAIRCRAFT HAD F/CTL SYS 2 FAULT DEFERRED ON DEC-04, THEN ON THE SAME DAY ON FLIGHT AV310 SAL-MIA SYSTEM 1 FAILS AND AIRCRAFT EMIT THE F/CTL FLAPS FAULT ECAM WARNING, WHICH LEADS THE CREW TO DECLARE EMERGENCY FOR LANDING. ONCE THE AIRCRAFT WAS ON GROUND TSM 27-Dec 4, 2020 · N686TA · Airbus A320214 · Leading Edge Slat Control SystemSDR RJEF20180326001Engine · abnormalPRIOR TO TAKE OFF, THE PILOT REPORTED THAT DURING APPLICATION OF TAKEOFF POWER, THE NR 1 ENGINE DID NOT SPOOL UP AS EXPECTED. LAGGED MORE THAN THE NR 2 ENGINE. THE AIRCRAFT RETURNED TO THE GATE, MAINTENANCE PERFORMED A FAULT ANALYSIS IAW TSM 71-00-00-810-8Mar 23, 2018 · N686TA · Airbus A320214 · Engine (Turbine/Turboprop)SDR RJEF20161215001Check Valve · faultyUPON ARRIVAL, THE PILOT REPORTED: "WHEN LANDING GEAR DOWN, ECAM MESSAGE BRAKES ALTN L RELEASED" MAINTENANCE PERSONNEL PERFORMED FAULT ANALYSIS AS PER TSM 32-43-00-810-824-A, PERFORMED THE OPERATIONAL CHECK TO START THE FUNCTIONAL TEST OF THE ALTERNATE BRAKING Dec 11, 2016 · N686TA · Airbus A320214 · Pneumatic Distribution SystemSDR RJEF20131212012Ignition Sys · faultedDURING THE DISPATCH OF FLIGHT TA311 FROM MIA TO SAL, THE PILOT REPORTED THAT THE ACFT HAD FAILURE OF ENG 2 IGNITION A FAULT, THE ACFT RETURNED TO THE GATE FOR MAINTENANCE. IT WAS VERIFIED THAT SUCH FAILURE IS DEFERRABLE IAW MEL 74-31-01 CAT C PROVIDED THAT THDec 9, 2013 · N686TA · Airbus A320214 · Ignition System
Reports on N686TA not matched to an aircraft · 4

They name N686TA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

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