Owner type Corporation
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 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 Registration Potential ADs 391 Information bulletins 8 NTSB investigations 0 FAA incident reports 0 Difficulty reports 9 Potential STCs 301 Related links 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.
1990 In force Superseded2026 ADs by the year they took effect: 558 ADs 1990 5 1991 1 1992 6 1993 10 1994 10 1995 4 1996 5 1997 10 1998 22 1999 14 2000 15 2001 9 2002 15 2003 3 2004 23 2005 20 2006 13 2007 16 2008 10 2009 13 2010 8 2011 12 2012 12 2013 17 2014 18 2015 23 2016 25 2017 24 2018 31 2019 24 2020 29 2021 17 2022 22 2023 19 2024 15 2025 21 2026 17
See all 558 ADs Information bulletins that may apply · 8 Advisory, not mandatory.
All 8 Airframe 6 Engine 2
Historical bulletins · 1
NTSB investigations No NTSB investigations matched to N686TA Matched 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 N686TA Matched 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 RJEF20263108001 Fan · faulted CABIN 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 Fan SDR RJEF20260106001 Unknown · vibration NR 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. TSM Jan 6, 2026 · N686TA · Airbus A320214 · Engine (Turbine/Turboprop) SDR 2023FA0000676 Unknown · unknown DURING 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 WA Oct 20, 2023 · N686TA · Airbus A320214 · Fuselage Structure (General) SDR RJEF20230814001 Valve · inoperative VENT 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 XCHANGER Aug 11, 2023 · N686TA · Airbus A320214 · Air Conditioning System SDR RJEF20210322001 Slat · damaged BIRD 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 WERE Mar 21, 2021 · N686TA · Airbus A320214 · Leading Edge Devices SDR RJEF20201204001 Controller · malfunctioned AIRCRAFT 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 System SDR RJEF20180326001 Engine · abnormal PRIOR 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 71-00-00-810-8 Mar 23, 2018 · N686TA · Airbus A320214 · Engine (Turbine/Turboprop) SDR RJEF20161215001 Check Valve · faulty UPON 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 System SDR RJEF20131212012 Ignition Sys · faulted DURING 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 TH Dec 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.
Airframe · Airbus A320-214 See all 301 STCs