Beechcraft F33A N8000J

Summary

On 27 March 1992 at about 20:12 local time, a Beechcraft F33A registered N8000J, operated by Steering Committee Corp., was involved in an accident near Payson, Arizona, United States. 2 people were on board and 2 died. The aircraft was destroyed. The NTSB has published a probable cause for this accident; it is quoted in full below.

Date

27 March 1992 at 20:12

Classification

Accident

Location

Payson, Arizona, United States

Coordinates

34.1895, -111.1697

Aircraft

Beechcraft F33A

Registration

N8000J

Category

Airplane

Engines

1

Operator

Steering Committee Corp.

Operating rule

Part 91: General Aviation

Purpose of flight

Personal

Phase of flight

Not recorded

Route

Durango → Phoenix

Aircraft damage

Destroyed

Weather

IMC

Light

Day

NTSB number

LAX92LA153

2 people died.

THE PILOT'S POOR PREFLIGHT PLANNING/PREPARATION BY INTENTIONALLY FLYING INTO KNOWN ADVERSE WEATHER AND HIS POOR IN-FLIGHT DECISION BY NOT FLYING TO AN ALTERNATE AIRPORT WHEN THE AIRPLANE BEGAN TO ENCOUNTER ICING. CONTRIBUTING TO THIS ACCIDENT WAS THE ICING CONDITION.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

THE PILOT RECEIVED A WEATHER BRIEFING FROM THE FLIGHT SERVICE STATION BEFORE DEPARTING ON THE ACCIDENT FLIGHT. THE WEATHER BRIEFER ADVISED THE PILOT OF FORECASTED ICING CONDITIONS ALONG THE INTENDED ROUTE OF FLIGHT. THE AIRPLANE WAS NOT EQUIPPED WITH ANY ANTI OR DEICING SYSTEMS. ABOUT 15 MINUTES AFTER DEPARTING WHILE AT 14,000 FT MSL ICE BEGAN TO FORM ON THE AIRPLANE AND THE PILOT ASKED FOR A LOWER ALTITUDE AND A GROUND SPEED CHECK. THE AIRPLANE'S GROUND SPEED WAS 170 KTS. 20 MINUTES LATER THE PILOT AGAIN REQUESTED A LOWER ALTITUDE BUT THE CONTROLLER WAS UNABLE DUE TO THE MEA. ABOUT 18 MINUTES LATER THE PILOT ASKED FOR A GROUND SPEED CHECK AND THE CONTROLLER RESPONDED, 150 KNOTS AND 11 MINUTES LATER CLEARED THE FLIGHT TO 12,000 FT. ABOUT 19 MINUTES LATER THE PILOT REPORTED THAT THE AIRPLANE WAS PICKING UP RIME ICE AND AGAIN REQUESTED A LOWER ALTITUDE. ABOUT 7 MINUTES LATER THE CONTROLLER REPORTED THE AIRPLANE'S GROUND SPEED WAS 120 KNOTS. ABOUT 14 MINUTES LATER THE PILOT REPORTED HAVING PROBLEMS MAINTAINING AIRSPEED AND ALTITUDE. SIX MINUTES LATER THE PILOT REPORTED THAT HE WAS UNABLE TO MAINTAIN THE ALTITUDE AND RADAR CONTACT WAS LOST 2 MINUTES LATER. THE AIRPLANE COLLIDED WITH UPSLOPING TERRAIN IN A WINGS LEVEL, NOSE DOWN ATTITUDE.

Quoted verbatim from the NTSB record.