# NTSB CHI00LA002: Enstrom EN-28, N602H, Indianapolis, IN, October 2, 1999

- Type: NTSB accident investigation
- Classification: Accident · Minor injuries · Limited investigation · Final report
- Date: October 2, 1999, 10:40 local (15:40 UTC)
- Place: Indianapolis, IN
- Location: 39.7684° N, 86.1580° W: Placed by OpenAirDocs: center of Indianapolis, IN, within about 11 miles (OpenAirDocs)
- Nearby events: https://openairdocs.org/map.md?lat=39.7684&lon=-86.1580&mi=10
- Phase of flight: [Initial climb](https://openairdocs.org/ntsb-phases/350) (OpenAirDocs' grouping)
- Highest injury: Minor injuries
- Injuries: 2 minor
- Status: Completed, report January 18, 2001
- Report: Approved by Office Director
- NTSB case key (mKey): 47543
- NTSB case page: https://web.ntsb.gov/investigations/?ntsbnumber=CHI00LA002
- NTSB report (PDF, downloads): https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/47543/pdf
- Page: https://openairdocs.org/ntsb/CHI00LA002

## 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.

## Sequence of events

In NTSB's coding before 2008 (https://www.ntsb.gov/GILS/Documents/codman.pdf).

- Loss of engine power, takeoff - initial climb
  - ignition system,spark plug - fouled (contributing factor)
  - operation with known deficiencies in equipment - attempted, pilot in command (cause)
  - ignition system,spark plug - failure,partial (contributing factor)
- Forced landing, emergency descent/landing
- Hard landing, emergency landing
  - terrain condition - construction area (contributing factor)
  - autorotation - improper, pilot in command (cause)

## Analysis

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.

## Factual 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.

## Aircraft

- Registration: [N602H](https://openairdocs.org/aircraft/N602H), registered now, S/N 1077, built 1977 (OpenAirDocs)
- Reported make and model: Enstrom EN-28
- Registry model: [Enstrom Helicopter 280C](https://openairdocs.org/model/enstrom-helicopter-280c) (registry code 3300505) (OpenAirDocs)
- Registry engine: [Lycoming HI0-360 series](https://openairdocs.org/engine/lycoming-hi0-360-series) (registry code 41553, turbo-shaft) (OpenAirDocs)
- Category: Helicopter
- Serial number: 1077
- Airframe hours: 3272
- Engines: Lycoming HIO-360-E1BD 205 horsepower reciprocating
- Damage: Substantial damage
- Flight: Personal, Part 91
- Registered owner: Hawk, Robert H.
- Airworthiness certificate: Standard, Normal
- Last inspection: Annual, March 29, 1999, 59 hours before
- Departed: IN03, IN

## Flight crew

As NTSB recorded them. NTSB leaves out names.

- Pilot; age 62; commercial; airplane ratings: single-engine land, multi-engine land; instrument ratings: airplane; medical: class 2, valid medical--w/ waivers/lim; seat: right; flight hours: 4,758 total, 147 in this make and model, 4,758 as pilot in command, 87 in the last 90 days, 23 in the last 30 days

## Weather

- Conditions: Visual (VMC), Day
- Wind: 210° at 10 knots
- Visibility: 10 statute miles
- Lowest ceiling: none
- Temperature: 64 °F, dew point 45 °F
- Altimeter: 30.00 inHg
- Observed at: IND, 7 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 (OpenAirDocs).

- [Accident 19991002032089A](https://openairdocs.org/incident/19991002032089A), Oct 2, 1999: Enstrm 280C, Indianapolis, IN, Substantial damage. (.19) On October 2, 1999, at 1040 eastern standard time, an Enstrom EN-28, N602H, sustained substantial damage during an autorotational landing in a field,…

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

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