Owner type
Corporation
Serial number
53592
Year built
2004
Type
Rotorcraft
Engine
Turbo-shaft
Airworthiness
Standard, normal
Airworthiness date
July 2, 2004
Certificate issued
October 7, 2008
Expires
July 31, 2028
Mode S code
A4C7CF

From the FAA registry file of October 24, 2026.

On this page

Airworthiness directives that may apply · 49

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1982In forceSuperseded2026
ADs by the year they took effect: 69 ADs
19821
19961
19971
19984
19994
20006
20014
20025
20034
20041
20053
20062
20071
20081
20094
20112
20123
20135
20141
20152
20181
20192
20212
20234
20242
20251
20262
See all 72 ADs

Information bulletins that may apply · 7

Advisory, not mandatory.

Historical bulletins · 2

NTSB investigations

No NTSB investigations matched to N407NAMatched 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 Bell 407 aircraft

FAA incident reports

No FAA accident or incident reports matched to N407NAMatched 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 Bell 407 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 HDNA2024120200936Display · burned outPRIMARY FLIGHT DISPLAY HAD INTERNAL FAILURE RESULTING IN SMOKE COMING FROM SD CARD SLOTS. AIRCRAFT LANDED WITH NO OTHER FAULTS.Dec 2, 2024 · N407NA · Bell 407 · Central DisplaySDR QMLA2020052920023Belt · out of adjustDURING TAKEOFF, CREW COMPLAINED OF BURNT RUBBER OR PLASTIC SMELL IN THE CABIN. AIR CONDITIONER WAS TURNED ON AND UPON THE SMELL OF THE RUBBER THE A/C WAS TURNED OFF AND SMELL EVENTUALLY WENT AWAY AFTER THE CREW ABORTED THE FLIGHT, AND OPENED WINDOWS TO VENT AMay 28, 2020 · N407NA · Bell 407 · Cabin Cooling SystemSDR QMLA2020051820019Cooling Fan · seizedWHILE RETURNING TO THE BASE, THE PILOT REPORTED AN ELECTRICAL SMELL IN THE COCKPIT AND SAW A SLIGHT AMOUNT OF SMOKE FWD OF INSTRUMENT PANEL. ONCE ON THE GROUND, THE MECHANIC ARRIVED TO TROUBLESHOOT THE CAUSE OF THIS SMELL AND FOUND THE AVIONICS COOLING FAN ON May 16, 2020 · N407NA · Bell 407 · Air Distribution FanSDR QMLA2019110749082Vhf Comm · malfunctionedPILOTS REPORT: AT TAKE OFF, THE NUMBER 2 VHF RADIO/GPS SHUT OFF. I WAS UNABLE TO GET IT TO COME BACK ON. BEING FAMILIAR WITH THE MEL (2312-01) I KNEW THAT I ONLY HAD TO HAVE ONE VHF RADIO OPERATIONAL TO CONTINUE MY FLIGHT. AFTER A SHORT DISCUSSION WITH THE CRENov 4, 2019 · N407NA · Bell 407 · Communications SystemSDR QMLA2016092816111Blade · crackedFOUND SMALL CRACK IN TAIL ROTOR BLADE ON FLAT SURFACE JUST INBOARD OF CURVED SECTION OF ROOT AREA. THIS IS THE THIRD CRACK IN THE SAME LOCATION. BLADE HAD BEEN REPAIRED.Sep 28, 2016 · N407NA · Bell 407 · Tail Rotor BladesSDR 2016FA0000459Blade · crackedFOUND SMALL CRACK IN TAIL ROTOR BLADE ON FLAT SURFACE JUST INBOARD OF CURVED SECTION OF ROOT AREA. BLADE HAD BEEN REPAIRED.Sep 28, 2016 · N407NA · Bell 407 · Tail Rotor BladesSDR QMLA2013063013086Hydraulic System · malfunctionedAFTER DECENT AND LEVELING AT 2500 FEET THE HYD PRESS AND CYCLIC CENTER LIGHTS ILLUMINATED ALONG WITH THE LOSS OF NORMAL CONTROL FORCES AND THE ACFT BECAME VERY SLOPPY AND HEAVY. ALL INDICATIONS ARE THAT THE HYD FAILED, DECLARED AN EMERGENCY AND DIVERTED. TURJun 30, 2013 · N407NA · Bell 407 · Hydraulic System, MainSDR QMLA2013021613025Engine · making metalPILOT REPORTED ENGINE CHIP LIGHT ILLUMIINATED JUST AFTER LANDING AND RETURNING TROTTLE TO IDLE. MX WAS CALLED AND A LARGE AMOUNT OF FLAKES WERE FOUND ON BOTH THE UPPER AND LOWER ENGINE CHIP DETECTORS. SOME FLAKES EXCEEDED THE MAXIMUM ALLOWABLE IAW MM 72, PARA Feb 16, 2013 · N407NA · Bell 407 · Engine (Turbine/Turboprop)SDR QMLA2012111512183Engine · malfunctionedPILOT REPORTED A FADEC FAIL, FADEC RESTART FAULT AND FADEC DEGRADE LIGHT IN CRUISE FLIGHT. FADEC CONTROLS REVERTED TO REVERSIONARY GOVERNOR AND PILOT HAD NO RESPONSE FROM COLLECT THROTTLE CONTROL. ENGINE SPEED REMAINED CONSTANT AT 100 PERCENT. MADE A PRECUATIONov 15, 2012 · N407NA · Bell 407 · Engine (Turbine/Turboprop)
Reports on N407NA not matched to an aircraft · 1

They name N407NA, 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 · 327

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 327 STCs