20080216010289A

Accident · Destroyed

FAA accident report · Amtr RV-6A · Stanwood, WA · February 16, 2008

Date
February 16, 2008 · 12:50 local
Place
Stanwood, WA
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N154RM
NTSB investigation
NTSBLAX08LA059
Reported as
Amtr RV6A
Reported engine
Lycoming O320D1A
People aboard
2
Fatal injuries
2
Pilot’s flight hours
0 total0 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) Aircraft crashed in field at 45 degree angle with no ground marks. Witness stated radio contact was made before crash, and pilot was having engine problems. Conducted teardown inspection of aircraft. Reviewed condition of engine, carburetor, magnetos, engine fuel pump, spark plugs, airframe fuel system, airframe engine controls, engine electrical system, and verified flight control continuity. No condition was noted in aircraft to cause loss of engine power. Could not verify operation of carburetor heat system due to crash damage. Local weather at time of accident: temp: 46 degrees, dew point: 37 degrees, relative humidity: 71%, wind: calm, visibility: 10 miles.

As the FAA filed it

(-23) AIRCRAFT CRASHED IN FIELD AT 45 DEGREE ANGLE WITH NO GROUND MARKS. WITNESS STATED RADIO CONTACT WAS MADE BEFORE CRASH, AND PILOT WAS HAVING ENGINE PROBLEMS. CONDUCTED TEARDOWN INSPECTION OF AIRCRAFT. REVIEWED CONDITION OF ENGINE, CARBURETOR, MAGNETOS, ENGINE FUEL PUMP, SPARK PLUGS, AIRFRAME FUEL SYSTEM, AIRFRAME ENGINE CONTROLS, ENGINE ELECTRICAL SYSTEM, AND VERIFIED FLIGHT CONTROL CONTINUITY. NO CONDITION WAS NOTED IN AIRCRAFT TO CAUSE LOSS OF ENGINE POWER. COULD NOT VERIFY OPERATION OF CARBURETOR HEAT SYSTEM DUE TO CRASH DAMAGE. LOCAL WEATHER AT TIME OF ACCIDENT: TEMP: 46 DEGREES, DEW POINT: 37 DEGREES, RELATIVE HUMIDITY: 71%, WIND: CALM, VISIBILITY: 10 MILES.

NTSB investigation

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