20151123020809I

Incident · No damage

FAA incident report · Beech B-99 · Eugene, OR · November 23, 2015

Date
November 23, 2015 · 20:30 local
Place
Eugene, OR
Airport
Eugene
Phase of flight
Cruise/Level Flight
Operating rules
Air taxi and commuter (Part 135)
Operator
JIKA
Damage
No damage
Aircraft
N4299A
Reported as
Beech B-99
Reported engine
U/A Canada PT6A-27-28
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Airline transport, flight instructor
Pilot’s flight hours
3,510 total238 in this make and model193 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

During an IFR flight (night, IMC conditions) the #1 inverter failed.

The pilot switched to the #2 inverter, but it failed to power the aircraft systems.

The result was loss of many of the engine instruments, some primary flight indicators and navigational capability.

The pilot declared an emergency and received vectors and a descent out of the weather to VMC. The pilot elected to divert, VMC, to an appropriate nearby airfield (eug), descended and landed without further incident.

Post incident maintenance revealed the #1 inverter had failed. Upon replacement, the aircraft systems worked normally, including the #2 inverter and switching between inverters.

It is company policy to use the inverter on alternate days (#1 on odd days of the month, and #2 on even days of the month). There was no report of previous problems with either inverter.

It is unknown why, when the pilot switched to the #2 inverter inflight, that it did not provide power to the aircraft.

As the FAA filed it

DURING AN IFR FLIGHT (NIGHT, IMC CONDITIONS) THE #1 INVERTER FAILED.

THE PILOT SWITCHED TO THE #2 INVERTER, BUT IT FAILED TO POWER THE AIRCRAFT SYSTEMS.

THE RESULT WAS LOSS OF MANY OF THE ENGINE INSTRUMENTS, SOME PRIMARY FLIGHT INDICATORS AND NAVIGATIONAL CAPABILITY.

THE PILOT DECLARED AN EMERGENCY AND RECEIVED VECTORS AND A DESCENT OUT OF THE WEATHER TO VMC. THE PILOT ELECTED TO DIVERT, VMC, TO AN APPROPRIATE NEARBY AIRFIELD (EUG), DESCENDED AND LANDED WITHOUT FURTHER INCIDENT.

POST INCIDENT MAINTENANCE REVEALED THE #1 INVERTER HAD FAILED. UPON REPLACEMENT, THE AIRCRAFT SYSTEMS WORKED NORMALLY, INCLUDING THE #2 INVERTER AND SWITCHING BETWEEN INVERTERS.

IT IS COMPANY POLICY TO USE THE INVERTER ON ALTERNATE DAYS (#1 ON ODD DAYS OF THE MONTH, AND #2 ON EVEN DAYS OF THE MONTH). THERE WAS NO REPORT OF PREVIOUS PROBLEMS WITH EITHER INVERTER.

IT IS UNKNOWN WHY, WHEN THE PILOT SWITCHED TO THE #2 INVERTER INFLIGHT, THAT IT DID NOT PROVIDE POWER TO THE AIRCRAFT.

Other reports on N4299A · 5

Matched to the same aircraft by N-number and date.