FTW98LA404

NTSB accident investigation · Piper PA-28RT-201T · Duck Creek, UT · September 18, 1998

Accident · No injuriesLimited investigationFinal report
Date
September 18, 1998, 14:00 local (20:00 UTC)
Place
Duck Creek, UT
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N8252SPiper PA-28RT-201T
Weather
Visual (VMC) · Day
Status
Completed · report December 1, 1999
Report
Approved by Office Director
FAA report
19980918025549A
Case key
43974

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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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.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of engine power(partial) - mech failure/malfCruise - normal
Engine assembly,rocker arm/tappet - loose part/bolt/nut/clamp/etcCause
Fluid,oil - leakFactor
Engine assembly,valve,intake - low compressionFactor
Forced landingDescent - emergency
Terrain condition - roadway/highwayFactor
Object - poleFactor
On ground/water collision with objectLanding - roll

Analysis

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.

Factual 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.

Aircraft

Registration
N8252S
Reported as
Piper PA-28RT-201T (PA-28RT-20)
Category
Airplane
Serial number
28R8031170
Airframe hours
4,792
Engine
Continental TSIO-360-F, 200 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Wings Of Denver Flying Club
Registered owner
B-Y Enterprises, Inc.
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · July 24, 1998 · 43 hours before
Departed
CNY · Moab, UT
Destination
VGT · Las Vegas, NV
Flight plan
VFR

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
51
Certificate
Commercial
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
2,185 total · 140 in this make and model · 1,839 as pilot in command · 5 in the last 90 days · 4 in the last 30 days · 4 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
220° at 23 knots, gusting 30
Visibility
10 statute miles
Lowest ceiling
None
Temperature
81 °F, dew point 37 °F
Altimeter
30.00 inHg
Observed at
CDC, 41 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.

Other investigations on N8252S · 1

Matched to the same aircraft by N-number and date.