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September 18, 1998 · Piper PA-28RT-201T PA-28RT-20 · N8252S

Duck Creek, UT

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
September 18, 1998
Injury Outcomes
No injuries (1 uninjured)
Location
Duck Creek, UT
Aircraft
Piper PA-28RT-201T PA-28RT-20
Tail Number
N8252S
Operator
Wings of Denver Flying Club
Injuries
None
Aircraft Damage
Substantial
NTSB Number
FTW98LA404

The airplane was in cruise flight at 12,500 feet when the pilot noticed the manifold pressure had dropped from 51.8 inches to 25 inches. 'The engine had poor response to throttle movement, and the engine sounded bad when I moved the throttle.' He made the decision not to proceed further due to the remote terrain. As he checked his maps for the nearest airport, the airplane lost altitude. 'The engine did not seem to have much power, and I was about 3,000 feet AGL by this time.' The pilot made a forced landing on a dirt road. During rollout the aircraft struck poles alongside of a cattle guard. According to the salvage company and the FAA inspector who examined the engine, two of the four screws securing the rocker cover on the number 3 cylinder were missing, and oil was leaking out. The rocker cover had a round indention on the outside, and a wear mark on the inside. The exhaust rocker arm studs were also loose. The rear stud was only finger tight. Aluminum was found imbedded in its threads. The front stud was loose, but its nut locking mechanism was still in place.

NTSB Probable Cause

Loose intake valve rocker arm studs that allowed a loss of compression and a loss of oil. A factor was unsuitable terrain on which to make a forced landing and poles next to a cattle guard.

Full Narrative

On September 18, 1998, approximately 1400 mountain daylight time, a Piper PA-28RT-201T, N8252S, was substantially damaged when it collided with poles during a forced landing near Duck Creek, Utah. The commercial pilot, the sole occupant aboard, was not injured. Visual meteorological conditions prevailed, and a VFR flight plan had been filed for the personal cross-country flight conducted under Title 14 CFR Part 91. The flight originated at Canyonlands Field, Moab, Utah, approximately 1300. In his accident report, the pilot said he was in cruise flight at 12,500 feet, en route to Las Vegas, Nevada, when he noticed the manifold pressure had dropped from 51.8 inches to 25 inches. "The engine had poor response to throttle movement, and the engine sounded bad when I moved the throttle." The pilot made the decision not to proceed further due to the remote terrain. As he checked his maps for the nearest airport, the airplane lost altitude. The pilot said the "engine did not seem to have much power, and I was about 3,000 feet AGL by this time." The pilot made a forced landing on a dirt road. During the landing roll, the aircraft struck poles next to a cattle guard, causing substantial damage. According to the salvage company and the FAA inspector who examined the engine, two of the four screws securing the rocker cover on the number 3 cylinder were missing, and oil was leaking out. The rocker cover had a round indention on the outside, and a wear mark on the inside. The exhaust rocker arm studs were also loose. The rear stud was only finger tight. Aluminum was found imbedded in its threads. The front stud was loose, but its nut locking mechanism was still in place.

Flight

Event TypeAccident
Event Time14:00 MDT
Nearest Airport0nm
Runway0
Flight Plan FiledVFR
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftPiper PA-28RT-201T PA-28RT-20
Tail NumberN8252S
Aircraft CategoryAir
DamageSubstantial
OperatorWings of Denver Flying Club
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsContinental · TSIO-360-F · Reciprocating · 200
Seats4

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 51 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind220° @ 23 kt, gusting 30 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point37 C
Altimeter30.00 inHg
Observation Time20:53
Weather SourceWFAC

Appendix: Source Data