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Aviation safety reports, made easier to study

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NTSB Report

October 2, 1999 · Enstrom EN-28 · N602H

Indianapolis, IN

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
October 2, 1999
Injury Outcomes
2 injuries (2 minor injuries)
Location
Indianapolis, IN
Aircraft
Enstrom EN-28
Tail Number
N602H
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
CHI00LA002

The pilot said that prior to initiating the flight he conducted a 'run-up.' He said, during the magneto check the engine ran rough and exceeded the normal magneto drop. He said he continued to run the engine at high RPM and leaned the fuel mixture for a minute. He said he then conducted another 'run-up' and the magneto drop was within specified limits. He stated that during the initial climb the engine began to 'pop' and the rotor RPM was dropping. He said he elected to attempt a turn to the heliport; however, due to the continued loss of power he elected to conduct an autorotational landing in a gravel construction area. During the autorotational landing the helicopter landed hard and received substantial damage. Subsequent to the accident an examination of the helicopter and engine was conducted. The magneto and harness were examined and no discrepancies were found. All the spark plugs were removed and examined. The bottom spark plug from the #2 cylinder was oil fouled and did not test fire. The top spark plug from the same cylinder (#2) fired with a weak and intermittent spark. All the other spark plugs test fired. No additional anomalies were found in the helicopter or engine.

NTSB Probable Cause

The pilot's attempted operation of the helicopter with known deficiencies, and his improper autorotation to landing. Factors were one fouled spark plug and another partially failed spark plug in the same cylinder, and the construction area.

Full Narrative

On October 2, 1999, at 1040 eastern standard time, an Enstrom EN-28, N602H, sustained substantial damage during an autorotational landing in a construction area, near the Downtown Indianapolis Heliport, in Indianapolis Indiana, following a partial loss of engine power. The pilot and one passenger reported minor injuries. The personal 14 CFR Part 91 flight was operating in visual meteorological conditions. No flight plan was on file. The flight was originating at the time of the accident. The pilot said that prior to initiating the flight he conducted a "run-up." He said, during the magneto check the engine ran rough and exceeded the normal magneto drop. He said he continued to run the engine at high RPM and leaned the fuel mixture for a minute. He said he then conducted another "run-up" and the magneto drop was within specified limits.. He stated that during the initial climb the engine began to "pop" and the rotor RPM was dropping. He said he elected to attempt a turn to the heliport; however, due to the continued loss of power he elected to conduct an autorotational landing in a gravel construction area. During the autorotational landing the helicopter landed hard and received substantial damage. Subsequent to the accident an examination of the helicopter and engine was conducted. The flight and engine controls were found to work correctly and have continuity. Both magnetos and harnesses were examined and no discrepancies were found. All the spark plugs were removed and examined. The bottom spark plug from the #2 cylinder was oil fouled and did not test fire. The top spark plug from the same cylinder (#2) fired with a weak and intermittent spark. All the other spark plugs test fired. No additional anomalies were found in the helicopter or engine.

Flight

Event TypeAccident
Event Time11:40 EDT
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftEnstrom EN-28
Tail NumberN602H
Aircraft CategoryHeli
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · HIO-360-E1BD · Reciprocating · 205
Seats2

People & Injuries

Injury Summary2 injuries (2 minor injuries)
Fatal0
Serious0
Minor2
Uninjured0
Total2
Crew 1Age 62 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind210° @ 10 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point64 F / 45 C
Altimeter30.00 inHg
Observation Time14:56
Weather SourceWFAC

Appendix: Source Data