N6249L

Substantial
Fatal

Grumman AA5B S/N: AA1B-0049

Accident Details

Date
Tuesday, June 25, 1996
NTSB Number
CHI96LA220
Location
FRYBURG, ND
Event ID
20001208X05940
Coordinates
46.879116, -103.190055
Aircraft Damage
Substantial
Highest Injury
Fatal
Fatalities
1
Serious Injuries
0
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

the pilot's VFR flight into instrument meteorological conditions. Factors were the fog, low ceiling, and rising terrain.

Aircraft Information

Registration
N6249L
Make
GRUMMAN
Serial Number
AA1B-0049
Engine Type
Reciprocating
Year Built
1972
Model / ICAO
AA5B AA5
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SALE REPORTED
Address
NONE
Status
Deregistered
City
XXX
State / Zip Code
OK 73125
Country
United States

Analysis

On June 25, 1996, about 1000 mountain daylight time (mdt), a Grumman AA5B, N6249L, sustained substantial damage when it impacted terrain near Fryburg, North Dakota. The solo private pilot sustained fatal injuries. The personal, 14 CFR Part 91 flight originated in West Fargo, North Dakota about 0830 central daylight time with a planned destination of Beach, North Dakota. Instrument meteorological conditions prevailed in the vicinity of the accident site about the time of the accident. No flight plan was filed.

Witnesses reported "low fog" in the vicinity of the accident site. One witness reported that he observed the accident airplane "circling" over Medora, North Dakota about 1000 mdt. Another witness, who was two miles west of the accident site, reported that she observed the airplane flying westbound "low enough to see into the cockpit."

The Federal Aviation Administration (FAA) Inspector who examined the accident site reported that the accident site was located on the upward slope of a 60 degree incline. The wreckage path was on a heading of 050 degrees.

Examination of the wreckage revealed the throttle was in the full forward position and the yolk was trapped in the full aft position. No evidence of flight control malfunction was reported and all flight control surfaces were located at the accident site.

The attitude indicator was trapped in a position corresponding to 30 degrees of right bank and the turn needle was trapped on the right side of the case. The vertical velocity indicator was trapped at 200 feet per minute. The alternator circuit breaker was in the off position and the left fuel gauge was trapped in the 1/4 position.

The engine rotated freely and exhibited no evidence of preimpact mechanical malfunction. The left magneto sparked when rotated by hand. Examination of the spark plugs, vaccuum pump, and fuel pumps revealed no anomalies.

The autopsy of the pilot was conducted at St. Joseph's Hospital, 30 West Seventh Street, Dickinson, North Dakota 58601. FAA toxicological testing was negative for all tests conducted.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI96LA220