CHI99LA057

NTSB accident investigation · Mooney M20E · Tryon, NE · December 31, 1998

Accident · No injuriesLimited investigationFinal report
Date
December 31, 1998, 10:50 local (16:50 UTC)
Place
Tryon, NE
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N333WSMooney M20E
Weather
Visual (VMC) · Day
Status
Completed · report February 16, 2001
Report
Approved by Office Director
FAA report
19981231044249A
Case key
45572

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

other maintenance personnel's not correcting a loose cylinder assembly. Factors were loose engine cylinder assembly, fractured cylinder mounting hardware, the roadway, and road sign.

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.

Airframe/component/system failure/malfunctionCruise
Engine assembly,cylinder - looseFactor
Maintenance,annual inspection - not correctedOther maintenance personnelCause
Engine installation,mounting bolt - fracturedFactor
Forced landingDescent - emergency
On ground/water collision with objectLanding - roll
Terrain condition - roadway/highwayFactor
Object - signFactor

Analysis

While in cruise flight the engine began to lose power. The pilot elected to conduct a forced landing on a roadway due to rough and hilly terrain. The landing was successful; however, during the rollout the right wing impacted a sign, and rotated into a ditch. Subsequent to the accident an examination of the airplane engine revealed #3 cylinder was loose and six cylinder base studs were fractured. The engine had accumulated a total time of 1,100 hours time in service and 31 hours since the last inspection.

Factual narrative

On December 31, 1998, at 1050 central standard time, a Mooney M20E, N333WS, operated by a private pilot, sustained substantial damage during a forced landing following a loss of engine power. The airplane landed on a roadway 35 miles northwest of North Platte, Nebraska, near Tryon, Nebraska. The pilot told authorities that he noted a rise in the exhaust gas temperature just prior to the loss of engine power. The pilot reported no injuries. The personal 14 CFR Part 91 flight was operating in visual meteorological conditions. No flight plan was on file. The flight departed North Platte, Nebraska, with an intended destination of Rapid City, South Dakota, at 1035.

The pilot sad that after initiating a forced landing he elected to land on a roadway due to rough and hilly terrain. He said that the landing was successful; however, during rollout the right wing contacted a sign, and the airplane rotated into a ditch.

An examination of the airplane after the accident revealed that the #3 cylinder was loose from the crankcase and that six studs were broken. The intake pipe for the same cylinder was found broken. The most recent inspection of the airplane and engine occurred on September 25, 1998. The engine had accumulated 31 hours since the inspection and the total time in service of 1,100 hours.

Aircraft

Registration
N333WS
Reported as
Mooney M20E
Category
Airplane
Serial number
323
Airframe hours
4,632
Engine
Lycoming IO-360-A1A, 200 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Roger D. Smith
Airworthiness certificate
Standard, Normal
Last inspection
Annual · September 25, 1998 · 31 hours before
Departed
LBF · North Platte, NE
Destination
RAP · Rapid City, SD

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
54
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
1,435 total · 1,020 in this make and model · 1,387 as pilot in command · 26 in the last 90 days · 12 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
190° at 10 knots
Visibility
10 statute miles
Lowest ceiling
8,000 ft broken
Altimeter
30.00 inHg
Observed at
LBF, 35 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.