FTW96LA291

NTSB accident investigation · Enstrom 280C · Castle Rock, CO · July 3, 1996

Accident · No injuriesLimited investigationFinal report
Date
July 3, 1996, 11:55 local (17:55 UTC)
Place
Castle Rock, CO
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N51763Enstrom 280C
Weather
Visual (VMC) · Day
Status
Completed · report February 18, 1997
Report
Approved by Office Director
FAA report
19960703016019A
Case key
19896

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

Total failure of the magneto. A factor was the pilot operating the helicopter with a known deficiency.

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 powerClimb
Ignition system,magneto - failure,totalCause
Operation with known deficiencies in equipment - intentionalPilot in commandFactor
Forced landingDescent - emergency
Gear collapsedLanding - roll

Analysis

The engine lost power and an autorotation was made. The helicopter was substantially damaged during the run-on landing on a rough field. Postaccident testing disclosed that when the magneto was rotated, none of the 12 leads produced a spark. When the distributor cap was removed, it was noted that none of the points opened when the magneto was rotated. An FAA inspector heard the engine missing on the day prior to the accident. He suggested to the pilot that the engine be checked before further flight. The pilot told the inspector that the condition was 'common on Enstrom helicopters when the engine is hot.'

Factual narrative

On July 3, 1996, approximately 1155 mountain daylight time, N51763, an Enstrom 280C, was substantially damaged during a forced landing 8 miles south of Castle Rock, Colorado. The flight instructor and the private pilot receiving instruction were not injured. Visual meteorological conditions prevailed, and no flight plan was filed. The instructional flight was being conducted under Title 14 CFR Part 91. The flight originated at Englewood, Colorado, on July 3, 1996, approximately 1150.

According to the pilots, they were in a slow climb from 500 feet to 750 feet agl (above ground level). The engine began to sputter, then lost power. They made an autorotation and run-on landing on a rough field. During the landing roll, the left front skid and crossover tube collapsed, causing the helicopter to veer 90 degrees to the left and the main rotor blades to sever the tail boom.

An FAA airworthiness inspector examined the helicopter on November 20, 1996. According to his report, the magneto (Bendix m/n D4LN-2200, s/n 35413) had failed. When the magneto was rotated, none of the 12 leads produced a spark. When the distributor cap was removed, it was noted that none of the points opened when the magneto was rotated.

In a telephone interview, the inspector also said that on the day prior to the accident, he observed the helicopter landing at Centennial Airport, Englewood, Colorado. He said the engine was missing noticeably. He suggested that the pilots (the same ones involved in the accident) have the engine checked before further flight. According to the inspector, the instructor replied that the condition was "common on Enstrom helicopters when the engine is hot."

Aircraft

Registration
N51763
Reported as
Enstrom 280C
Category
Helicopter
Serial number
1153
Airframe hours
1,500
Engine
Lycoming HIO-360-E1AD, 205 horsepower, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Operator
Denver Helicopters, Inc.
Registered owner
Darcor Holding
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · June 25, 1996 · 15 hours before
Departed
CO93 · Larkspur, CO
Destination
APA · Englewood, CO

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
27
Certificate
Commercial
Airplane ratings
Single-engine land
Instrument ratings
Helicopter, Airplane
Medical
Class 1, Valid Medical--no waivers/lim.
Seat
Right
Flight hours
1,500 total · 321 in this make and model · 1,000 as pilot in command · 158 in the last 90 days · 54 in the last 30 days · 5 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
20° at 7 knots
Visibility
50 statute miles
Lowest ceiling
None
Temperature
91 °F, dew point 36 °F
Altimeter
30.00 inHg
Observed at
APA, 12 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 N51763 · 1

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