N345RB

Destroyed
Serious

CESSNA 172A S/N: 47512

Accident Details

Date
Tuesday, August 1, 1995
NTSB Number
ANC95LA124
Location
CHICKALOON, AK
Event ID
20001207X04121
Coordinates
61.739555, -148.219116
Aircraft Damage
Destroyed
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
1
Uninjured
0
Total Aboard
2

Probable Cause and Findings

THE PILOT'S INADVERTENT ENCOUNTER WITH ADVERSE WEATHER CONDITIONS AND FAILURE TO MAINTAIN SUFFICIENT ALTITUDE/CLEARANCE FROM THE TERRAIN TO COMPENSATE FOR SUCH CONDITIONS. FACTORS RELATED TO THE ACCIDENT WERE: DOWNDRAFTS, THE PROXIMITY OF MOUNTAINOUS TERRAIN, AND THE PILOT'S INADEQUATE WEATHER EVALUATION.

Aircraft Information

Registration
N345RB
Make
CESSNA
Serial Number
47512
Engine Type
Reciprocating
Year Built
1960
Model / ICAO
172A C172
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SALE REPORTED
Address
UNKNOWN
Status
Deregistered
City
BIG LAKE
State / Zip Code
AK 99687
Country
United States

Analysis

On August 1, 1995, about 1145 Alaska daylight time, a float equipped Cessna 172A, N345RB, collided with terrain while maneuvering in a remote area, about 30 miles east of Chickaloon, Alaska. The airplane was being operated as a visual flight rules (VFR) local area personal flight when the accident occurred. The airplane, operated by the pilot, was destroyed. The certificated private pilot received serious injuries. The sole passenger received minor injuries. Visual meteorological conditions prevailed. A VFR flight plan was filed. The flight originated at the Wasilla Lake Seaplane base, Wasilla, Alaska, at 1042.

The pilot reported that he was flying in the area of Sheep Mountain and Caribou Creek about 5,500 feet mean sea level (MSL). He indicated that the airplane encountered a strong downdraft and began losing altitude and airspeed at full power. The pilot began a turn away from rising terrain but the airplane stalled about 40 feet above the ground. The left wingtip struck a small rise and the airplane cartwheeled downslope. The engine was torn from the airplane and the fuselage was broken in-half. The airplane came to rest about 4,800 feet msl. The airplane was reported overdue to the Federal Aviation Administration (FAA) and an alert notice (ALNOT) was issued at 1603. Search aircraft located the accident site by tracking the airplane's emergency locator transmitter (ELT) about 1900.

The pilot reported that the airplane was 128 pounds below gross weight. A review of climb data from the airplane owners manual revealed that at gross weight, 5,000 feet and 41 degrees F, the airplane should have been capable of a 350 foot per minute climb. The pilot also indicated that scattered rain showers were present in the area.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC95LA124