19990606006419A

Accident · Destroyed

FAA accident report · Amtr SEA HAWK · Yucca Valley, CA · June 6, 1999

Date
June 6, 1999 · 14:49 local
Place
Yucca Valley, CA
Phase of flight
Normal Cruise
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N2485
NTSB investigation
NTSBLAX99LA209
Reported as
Amtr Seahawk
Reported engine
Lycoming O320E2A
People aboard
1
Fatal injuries
1
Pilot’s flight hours
500 total10 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.

Witnesses said that the acft banked to the left, spiraled in, crashed, and caught fire, the pilot/sole occupant suffered fatal injuries, the acft was destroyed, other circumstances are unknown. (From .19) on June 6, 1999, about 1446 hours pacific daylight time, a homebuilt experimental blanco sea Hawker, N2485, operated by the owner/builder/pilot, was destroyed after colliding with terrain near Yucca Valley, California. The private pilot, and sole occupant, operating under 14 CFR part 91 was fatally injured. Visual meteorological conditions prevailed for the personal cross-country flight and no flight plan was filed. The flight reportedly originated at hemet, California, at an undetermined time, and was destined for an unknown destination in Utah. According to witnesses, the aircraft was northbound when it suddenly made a sharp left turn followed by a descending spiral turn into the terrain. (.4)the owner/builder/pilot of a homebuilt experimental amphibian departed for a personal cross-country flight. About 32 minutes after departure the airplane was observed by witnesses flying north along a ridgeline in a desert area. The airplane made a sudden tight turn to the left and descended into the ground. A postaccident fire consumed the airframe and all engine accessories. One of four carbon fiber propeller blades was found separated from the propeller hub and free of impact damage. The other three blades were fire damaged. A detailed examination of the engine did not reveal any mechanical failure. A sheriff's helicopter pilot reported 'very turbulent and very rough' air above 100 feet AGL. The density altitude was about 6,180 feet MSL. (-23)LAX99LA209

As the FAA filed it

WITNESSES SAID THAT THE ACFT BANKED TO THE LEFT, SPIRALED IN, CRASHED, AND CAUGHT FIRE, THE PILOT/SOLE OCCUPANT SUFFERED FATAL INJURIES, THE ACFT WAS DESTROYED, OTHER CIRCUMSTANCES ARE UNKNOWN. (FROM .19) ON JUNE 6, 1999, ABOUT 1446 HOURS PACIFIC DAYLIGHT TIME, A HOMEBUILT EXPERIMENTAL BLANCO SEA HAWKER, N2485, OPERATED BY THE OWNER/BUILDER/PILOT, WAS DESTROYED AFTER COLLIDING WITH TERRAIN NEAR YUCCA VALLEY, CALIFORNIA. THE PRIVATE PILOT, AND SOLE OCCUPANT, OPERATING UNDER 14 CFR PART 91 WAS FATALLY INJURED. VISUAL METEOROLOGICAL CONDITIONS PREVAILED FOR THE PERSONAL CROSS-COUNTRY FLIGHT AND NO FLIGHT PLAN WAS FILED. THE FLIGHT REPORTEDLY ORIGINATED AT HEMET, CALIFORNIA, AT AN UNDETERMINED TIME, AND WAS DESTINED FOR AN UNKNOWN DESTINATION IN UTAH. ACCORDING TO WITNESSES, THE AIRCRAFT WAS NORTHBOUND WHEN IT SUDDENLY MADE A SHARP LEFT TURN FOLLOWED BY A DESCENDING SPIRAL TURN INTO THE TERRAIN. (.4)THE OWNER/BUILDER/PILOT OF A HOMEBUILT EXPERIMENTAL AMPHIBIAN DEPARTED FOR A PERSONAL CROSS-COUNTRY FLIGHT. ABOUT 32 MINUTES AFTER DEPARTURE THE AIRPLANE WAS OBSERVED BY WITNESSES FLYING NORTH ALONG A RIDGELINE IN A DESERT AREA. THE AIRPLANE MADE A SUDDEN TIGHT TURN TO THE LEFT AND DESCENDED INTO THE GROUND. A POSTACCIDENT FIRE CONSUMED THE AIRFRAME AND ALL ENGINE ACCESSORIES. ONE OF FOUR CARBON FIBER PROPELLER BLADES WAS FOUND SEPARATED FROM THE PROPELLER HUB AND FREE OF IMPACT DAMAGE. THE OTHER THREE BLADES WERE FIRE DAMAGED. A DETAILED EXAMINATION OF THE ENGINE DID NOT REVEAL ANY MECHANICAL FAILURE. A SHERIFF'S HELICOPTER PILOT REPORTED 'VERY TURBULENT AND VERY ROUGH' AIR ABOVE 100 FEET AGL. THE DENSITY ALTITUDE WAS ABOUT 6,180 FEET MSL. (-23)LAX99LA209

NTSB investigation

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