N9970P

Substantial
None

Piper PA-36-285 S/N: 36-7560082

Accident Details

Date
Thursday, June 20, 1996
NTSB Number
SEA96LA132
Location
HAZLETON, ID
Event ID
20001208X06124
Coordinates
42.580963, -114.069480
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

partial loss of engine power for undetermined reason(s). Factors relating to the accident were: high density altitude; the pilot's delay in dumping the entire chemical load, when he first perceived a power loss; and rough/uneven terrain in the emergency landing area.

Aircraft Information

Registration
N9970P
Make
PIPER
Serial Number
36-7560082
Engine Type
Reciprocating
Year Built
1975
Model / ICAO
PA-36-285 PA36
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
JOHNSTON AIRCRAFT SERVICE INC
Address
PO BOX 1457
Status
Deregistered
City
TULARE
State / Zip Code
CA 93275-1457
Country
United States

Analysis

On June 20, 1996, approximately 0958 mountain daylight time, a Piper PA-36-285, N9970P, registered to and being flown by a commercial pilot, was substantially damaged during an inflight collision with terrain shortly after takeoff, at the Hazelton airport, Hazelton, Idaho. The pilot was uninjured. Visual meteorological conditions existed and no flight plan had been filed. The flight, which was to have been an aerial application, was to have been operated under 14CFR137.

The pilot reported that on takeoff from the 3,000 foot gravel runway 24 he perceived an approximate 15% reduction of power but decided to continue the takeoff as he had reached 60 miles per hour at his "Go/No Go" point. He turned south, crossing Interstate 84 during which the engine surged briefly and he began dumping a portion of his chemical load. He reported that he was unable to achieve a positive climb rate and initiated dumping the remaining chemical load during which the aircraft's main landing gear contacted a plowed field approximately 30 degrees to the orientation of the furrows (refer to attached photos). The main landing gear separated from the aircraft and the aircraft came to rest. The pilot reported departing Hazelton with 200 gallons of chemical and 32 gallons of fuel. Density altitude was approximately 5,400 feet.

A compression check of all eight cylinders was accomplished on July 8, 1996, by personnel from Snake River Aircraft Maintenance in Twin Falls, and revealed no mechanical discontinuity within the engine (compression findings noted below). Additionally, the exhaust stacks were examined and no excessive buildup of sooting or carbon was noted, and approximately seven gallons of fuel was drained from one fuel tank (the opposite tank was observed to have been breached).

Cylinder: Performance: #1 72/80 #2 40/80 leaking by rings #3 40/80 leaking by exhaust #4 71/80 #5 42/80 leaking by rings #6 60/80 #7 68/80 #8 66/80

The pilot failed to respond to two requests for the completion of NTSB Form 6120.1/2.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA96LA132