19971116032979A

Accident · Destroyed

FAA accident report · Amtr SONERAI2LS · White Hills, AZ · November 16, 1997

Date
November 16, 1997 · 11:30 local
Place
White Hills, AZ
Airport
Triangle Airpark Airport
Phase of flight
To Init Climb(1st Pwr Reduct)
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N27KF
NTSB investigation
NTSBLAX98LA038
Reported as
Amtr SONERAI2LS
Reported engine
Continental A758F
People aboard
1
Fatal injuries
1
Pilot’s flight hours
2,180 total75 in this make and model21 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.

Climbed 400FT. Stalled. Indicates fatal. Minimal info.(previous remark from .19) (remark to follow from .4) the aircraft was part of a flight of three which flew into the airport earlier in the day. After visiting with friends in the nearby trailer park, the three aircraft were departing for the return to las vegas. The accident aircraft was the middle one of the three in the takeoff sequence. The pilot of the last aircraft reported that accident aircraft was in the takeoff initial climb when it appeared to loose power and enter a descent toward the desert. The aircraft touched down and then nosed over in the dirt. The accident site, which is located about 1 mile northwest of the airport, is predominantly level, although several small washes traverse the area in a direction perpendicular to the aircraft's direction of travel. The main landing gear was found to have contacted the northern lip of a wash and nosed over. The airframe and engine were examined following receovery of the wreckage. Control system continuity was established. The fuel selector valve was found in the off position. An estimated 12 gallons of automotive fuel was in the single fuselage fuel tank. No preimpact mechanical malfunctions or failures were identified during a complete disassembly of the engine, magnetos, and carburetor, or in the fuel system examination.

As the FAA filed it

CLIMBED 400FT. STALLED. INDICATES FATAL. MINIMAL INFO.(PREVIOUS REMARK FROM .19) (REMARK TO FOLLOW FROM .4) THE AIRCRAFT WAS PART OF A FLIGHT OF THREE WHICH FLEW INTO THE AIRPORT EARLIER IN THE DAY. AFTER VISITING WITH FRIENDS IN THE NEARBY TRAILER PARK, THE THREE AIRCRAFT WERE DEPARTING FOR THE RETURN TO LAS VEGAS. THE ACCIDENT AIRCRAFT WAS THE MIDDLE ONE OF THE THREE IN THE TAKEOFF SEQUENCE. THE PILOT OF THE LAST AIRCRAFT REPORTED THAT ACCIDENT AIRCRAFT WAS IN THE TAKEOFF INITIAL CLIMB WHEN IT APPEARED TO LOOSE POWER AND ENTER A DESCENT TOWARD THE DESERT. THE AIRCRAFT TOUCHED DOWN AND THEN NOSED OVER IN THE DIRT. THE ACCIDENT SITE, WHICH IS LOCATED ABOUT 1 MILE NORTHWEST OF THE AIRPORT, IS PREDOMINANTLY LEVEL, ALTHOUGH SEVERAL SMALL WASHES TRAVERSE THE AREA IN A DIRECTION PERPENDICULAR TO THE AIRCRAFT'S DIRECTION OF TRAVEL. THE MAIN LANDING GEAR WAS FOUND TO HAVE CONTACTED THE NORTHERN LIP OF A WASH AND NOSED OVER. THE AIRFRAME AND ENGINE WERE EXAMINED FOLLOWING RECEOVERY OF THE WRECKAGE. CONTROL SYSTEM CONTINUITY WAS ESTABLISHED. THE FUEL SELECTOR VALVE WAS FOUND IN THE OFF POSITION. AN ESTIMATED 12 GALLONS OF AUTOMOTIVE FUEL WAS IN THE SINGLE FUSELAGE FUEL TANK. NO PREIMPACT MECHANICAL MALFUNCTIONS OR FAILURES WERE IDENTIFIED DURING A COMPLETE DISASSEMBLY OF THE ENGINE, MAGNETOS, AND CARBURETOR, OR IN THE FUEL SYSTEM EXAMINATION.

NTSB investigation

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