20031019029349A

Accident · Destroyed

FAA accident report · Beech 35-C33 · Mesquite, NV · October 19, 2003

Date
October 19, 2003 · 16:25 local
Place
Mesquite, NV
Airport
Mesquite Airport
Phase of flight
Approach
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N9438S
NTSB investigation
NTSBLAX04FA019
Reported as
Beech 35C33
Reported engine
Continental IO470N
People aboard
2
Fatal injuries
2
Pilot’s flight hours
288 total2 in this make and model0 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.

(-23) On October 19, 2003, about 1625 pacific daylight time, a sherrif's deputy said he saw smoke coming from the direction of the Mesquite Airport, he immediately went to investigate and found the wreckage of an aircraft burning. Two off duty firemen were fighting the fire with no success. It was determined that the aircraft was a Beech debonair, 35-C33, s/n CD-1004, N9438S which had impacted the ground about 100 yrds from the airport property on the approach end of runway 190. The aircraft was owned by vtb fliers LLC. The aircraft was destroyed by post impact fire, leaving the left wing and tail section intact, the initial impact with the ground the aircraft was at a heading of 200 degrees and came to rest 25 feet from initial impact at a heading of 240 degrees as the aircraft had very little forward momentum. Further investigation revealed that the pilot privacy data omitted was taking instruction from the co-pilot privacy data omitted. Prior to them departing from henderson airport, privacy data omitted had flown with another individual for approximately one hour and twenty minutes in the same aircraft. The aircraft was not refueled prior to the instructional flight to Mesquite. The aircraft departed from henderson at 1500 and collided with terrain at about 1625. In talking with the owners of the aircraft it was standard for them to keep 30 gallons in each main and 6 gallons in the tip tanks for weight and balance purposes. The pilot and co-pilot sustained fatal injuries in the post impact fire. Weather was not a factor. The NTSB conducted an engine teardown and no deficiencies were found. This ends this investigation.

As the FAA filed it

(-23) ON OCTOBER 19, 2003, ABOUT 1625 PACIFIC DAYLIGHT TIME, A SHERRIF'S DEPUTY SAID HE SAW SMOKE COMING FROM THE DIRECTION OF THE MESQUITE AIRPORT, HE IMMEDIATELY WENT TO INVESTIGATE AND FOUND THE WRECKAGE OF AN AIRCRAFT BURNING. TWO OFF DUTY FIREMEN WERE FIGHTING THE FIRE WITH NO SUCCESS. IT WAS DETERMINED THAT THE AIRCRAFT WAS A BEECH DEBONAIR, 35-C33, S/N CD-1004, N9438S WHICH HAD IMPACTED THE GROUND ABOUT 100 YRDS FROM THE AIRPORT PROPERTY ON THE APPROACH END OF RUNWAY 190. THE AIRCRAFT WAS OWNED BY VTB FLIERS LLC. THE AIRCRAFT WAS DESTROYED BY POST IMPACT FIRE, LEAVING THE LEFT WING AND TAIL SECTION INTACT, THE INITIAL IMPACT WITH THE GROUND THE AIRCRAFT WAS AT A HEADING OF 200 DEGREES AND CAME TO REST 25 FEET FROM INITIAL IMPACT AT A HEADING OF 240 DEGREES AS THE AIRCRAFT HAD VERY LITTLE FORWARD MOMENTUM. FURTHER INVESTIGATION REVEALED THAT THE PILOT ^PRIVACY DATA OMITTED^ WAS TAKING INSTRUCTION FROM THE CO-PILOT ^PRIVACY DATA OMITTED^. PRIOR TO THEM DEPARTING FROM HENDERSON AIRPORT, ^PRIVACY DATA OMITTED^ HAD FLOWN WITH ANOTHER INDIVIDUAL FOR APPROXIMATELY ONE HOUR AND TWENTY MINUTES IN THE SAME AIRCRAFT. THE AIRCRAFT WAS NOT REFUELED PRIOR TO THE INSTRUCTIONAL FLIGHT TO MESQUITE. THE AIRCRAFT DEPARTED FROM HENDERSON AT 1500 AND COLLIDED WITH TERRAIN AT ABOUT 1625. IN TALKING WITH THE OWNERS OF THE AIRCRAFT IT WAS STANDARD FOR THEM TO KEEP 30 GALLONS IN EACH MAIN AND 6 GALLONS IN THE TIP TANKS FOR WEIGHT AND BALANCE PURPOSES. THE PILOT AND CO-PILOT SUSTAINED FATAL INJURIES IN THE POST IMPACT FIRE. WEATHER WAS NOT A FACTOR. THE NTSB CONDUCTED AN ENGINE TEARDOWN AND NO DEFICIENCIES WERE FOUND. THIS ENDS THIS INVESTIGATION.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.

Other reports on N9438S · 1

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