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October 17, 2007 · Cessna 210 · N215MD

Canon City, CO

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
October 17, 2007
Injury Outcomes
No injuries (2 uninjured)
Location
Canon City, CO
Aircraft
Cessna 210
Tail Number
N215MD
Injuries
None
Aircraft Damage
Substantial
NTSB Number
DEN08LA014

On final approach during the fourth landing the instructor noticed they had descended below the glideslope. When the student advanced the throttle to climb back onto the glideslope there was no response from the engine. The student pumped the throttle and turned on the electric fuel pump without result. The airplane landed in a dirt field, approximately 200 feet short of the runway. The nose landing gear collapsed and the airframe sustained substantial damage. Examination of the airplane revealed the throttle cable was broken, and several areas of the cable showed signs of wear. A broken throttle cable may prevent application of power when commanded. An examination of the remaining airplane systems revealed no anomalies.

NTSB Probable Cause

The failure of the engine throttle cable resulting in a lack of engine power when commanded.

Full Narrative

On October 17, 2007, approximately 1515 mountain daylight time, a Cessna 210, N215MD, was substantially damaged when it impacted terrain following a loss of engine power while on final approach to Fremont County Airport (1V6), Canon City, Colorado. Visual meteorological conditions prevailed at the time of the accident. The instructional flight was being conducted under the provisions of Title 14 Code of Federal Regulations Part 91 without a flight plan. The flight instructor and private pilot receiving instruction were not injured. The local flight originated at 1400. According to the flight instructor's statement, he and the student had completed their maneuvers and returned to the airport for a series of touch-and-go landings, in partial completion of a flight review. While on final approach for the fourth landing, the instructor noticed they had descended below the glideslope on the Visual Approach Slope Indicator (VASI). The student advanced the throttle to climb back onto the glideslope and there was no response from the engine. The student pumped the throttle and turned on the electric fuel pump without result. The airplane landed in a dirt field approximately 200 feet short of the runway. Examination of the airplane revealed the nose gear collapsed and the frame cross beam on the right side was cracked. An examination of the airplane engine by the Safety Board Investigator-in-charge and a representative from Teledyne Continental Motors revealed that the engine throttle cable rod had broken. Further examination of the throttle cable assembly, conducted by Cessna Aircraft Company under the auspices of the Federal Aviation Administration, revealed the throttle cable outer sleeve was cracked and had separated from the steel fitting. The end of the steel fitting was worn and deformed, and the swivel ball fitting at the end of the plunger was worn. The throttle cable was not a Cessna provided part. A placard on the throttle cable identified it as originating from Aircraft Components Inc. (ACI) of Benton Harbor, Michigan. ACI was a mail-order aircraft parts supplier, and ceased operations in 1990. Cessna recommends that all engine control cables be replaced at engine overhaul. A review of the maintenance records revealed the last engine overhaul was completed on November 2, 1989. The last annual inspection was competed on October 2, 2007. There was no entry in the maintenance records reflecting when the engine control cables were last replaced.

Flight

Event TypeAccident
Event Time15:15 MDT
Nearest AirportFremont County Airport (0nm)
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftCessna 210
Tail NumberN215MD
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsContinental · IO470E · Reciprocating · 260
Seats4

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 48 · Second Class · None
Crew 2Age 75 · Third Class · None

Conditions

ConditionsVMC
LightDaylight
WindCalm
Visibility10 sm
CeilingNone
Temperature / Dew Point59 / 23 C
Altimeter29.46 inHg
Observation Time21:55
Weather SourceWFAC

Appendix: Source Data