ANC01LA023

NTSB accident investigation · Cessna 180 · Chugiak, AK · December 14, 2000

Accident · No injuriesLimited investigationFinal report
Date
December 14, 2000, 14:00 local (18:00 UTC)
Place
Chugiak, AK
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N4955ACessna 180
Weather
Visual (VMC) · Day
Status
Completed · report July 17, 2001
Report
Approved by Office Director
NTSB office
Alaska Regional Office
FAA report
20001214041839A
Case key
51023

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

The failure of a mechanic to ensure the throttle linkage was secure. A factor in the accident was the pilot's failure to take remedial action during an emergency landing and overrun.

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/malfunctionTakeoff - initial climb
Throttle/power lever,linkage - loose part/bolt/nut/clamp/etcCause
Maintenance,installation - inadequateOther maintenance personnelCause
Forced landingEmergency landing after takeoff
OverrunEmergency landing after takeoff
Remedial action - not performedPilot in commandFactor
In flight collision with objectEmergency landing after takeoff
Object - fence
Object - tree(s)

Analysis

The commercial certificated pilot had just gotten the airplane from a maintenance facility after the engine had been disassembled. The engine was reinstalled by a mechanic who made several engine runs to check for leaks and proper rigging of the engine controls. The pilot said an engine run-up to 1,700 rpm before takeoff was normal. Just after lift-off, the pilot said the engine did not seem to be producing full power, and the airplane would not climb above about 300 feet. He decided to return to the airport, and when the pilot pulled the throttle control to idle, the engine power did not change. It continued to run at less than full throttle, but he could not make any power changes, up or down. The pilot said he descended to the runway, but since he could not reduce power, continued to fly down the length of the runway until reaching the end. He said he was flying at low level, and did not remember to shut-off the engine with the mixture or magnetos. Upon reaching the end of the runway, he banked the airplane to the left along a taxiway. The taxiway abruptly ended at a six feet high fence. The airplane collided with the fence, and then struck numerous trees beyond the fence. The airplane received damage to the engine, wings, and fuselage. The mechanic, and another mechanic employee observed the airplane climb to about 500 feet and then return for landing. During the landing, the airplane touched down on the runway for about 5 to 7 seconds on the main landing gear tires. The touchdown point appeared to be about mid-length of the runway. The airplane then lifted off to about 40 feet until reaching the end of the runway. It banked hard to the left, bounced the main wheels on the taxiway, and disappeared from view. After the accident, the mechanic recovered the airplane. During a postaccident examination of the engine, the nut that clamps the throttle linkage to the carburetor throttle arm, was found to be loose.

Factual narrative

On December 14, 2000, about 1400 Alaska standard time, a wheel-equipped Cessna 180 airplane, N4955A, sustained substantial damage after colliding with a fence and trees at the Birchwood Airport, Chugiak, Alaska. The airplane was being operated as a visual flight rules (VFR), local personal flight, when the accident occurred. The airplane was operated by the pilot. The commercial certificated pilot, the sole occupant, was not injured. Visual meteorological conditions prevailed.

During a telephone conversation with the National Transportation Safety Board (NTSB) investigator-in-charge (IIC), on December 15, 2000, the pilot reported he had just gotten the airplane from a maintenance facility at the Birchwood airport, and he was planning to fly to the Elmendorf Air Force Base, Anchorage, Alaska. The pilot said he performed an engine run-up to 1,700 rpm before takeoff. The run-up was normal. He then departed on runway 19R and began a left turn-out. Just after lift-off, the pilot said the engine did not seem to be producing full power. He did not recall the amount of power, but the airplane would not continue to climb above about 300 feet. He decided to return to the airport and began a landing approach to runway 19R. When the pilot pulled the throttle control to idle, the engine power did not change. It continued to run at less than full throttle, but he could not make any power changes, up or down. The pilot said he descended to the runway, but since he could not reduce power, continued to fly down the length of the runway until reaching the end. He said he was flying at low level, and did not remember to shut-off the engine with the mixture or magnetos. Upon reaching the end of the runway, he banked the airplane to the left along a taxiway. The taxiway abruptly ended at a six feet high fence. The airplane collided with the fence, and then struck numerous trees beyond the fence. The airplane received damage to the engine, wings, and fuselage.

During a telephone interview with the maintenance facility personnel and the NTSB IIC, the mechanic/owner of the facility reported that the airplane's engine was removed and disassembled due a previous propeller strike. The engine was reinstalled, and had several engine runs to check for leaks and proper rigging of the engine controls. The mechanic, and another mechanic employee, observed the pilot perform an engine run-up before departing. The airplane appeared to only climb to about 500 feet and then return for landing. During the landing, the airplane touched down on the runway for about 5 to 7 seconds on the main landing gear tires. The touchdown point appeared to be about mid-length of the runway. The airplane then lifted off to about 40 feet until reaching the end of the runway. It banked hard to the left, bounced the main wheels on the taxiway, and disappeared from view.

After the accident, the maintenance facility personnel recovered the airplane. During a postaccident examination of the engine, the nut that clamps the throttle linkage to the carburetor throttle arm, was found to be loose.

Aircraft

Registration
N4955A
Reported as
Cessna 180
Category
Airplane
Serial number
32352
Airframe hours
4,400
Engine
Continental O-470-K, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Lawrence W. Seethaler
Airworthiness certificate
Standard, Normal
Last inspection
Annual · May 4, 2000 · 17 hours before
Departed
PABV
Destination
PAED · Anchorage, AK
Airport
PABV · Birchwood, runway 19R, 4,010 × 100 ft, asphalt

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
57
Certificate
Commercial
Airplane ratings
Single-engine sea, Single-engine land
Medical
Class 3, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
703 total · 255 in this make and model · 570 as pilot in command

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
10 statute miles
Lowest ceiling
None
Temperature
64 °F, dew point 50 °F
Altimeter
30.00 inHg
Observed at
PAB

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 N4955A · 2

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