# NTSB ANC96LA069: Gillespie Challenger 2, N1591G, Talkeetna, AK, May 5, 1996

- Type: NTSB accident investigation
- Classification: Accident · No injuries · Limited investigation · Final report
- Date: May 5, 1996, 09:30 local (17:30 UTC)
- Place: Talkeetna, AK
- Coordinates: 62.449153, -149.789901 (estimated)
- Nearby events: https://openairdocs.org/map.md?lat=62.4492&lon=-149.7899&mi=10
- Phase of flight: [Enroute](https://openairdocs.org/ntsb-phases/400) (OpenAirDocs' grouping)
- Highest injury: No injuries
- Injuries: 1 uninjured
- Status: Completed, report February 1, 1997
- Report: Approved by Office Director
- NTSB office: Alaska Regional Office
- NTSB case key (mKey): 2839
- NTSB case page: https://web.ntsb.gov/investigations/?ntsbnumber=ANC96LA069
- NTSB report (PDF, downloads): https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/2839/pdf
- Page: https://openairdocs.org/ntsb/ANC96LA069

## Probable cause

The pilot's failure to properly use the mixture control to enrich the fuel mixture, and the seizure of the piston in the cylinder.

## Sequence of events

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

- Loss of engine power, descent - normal
  - engine assembly,piston - seized (cause)
  - mixture - improper use of, pilot in command (cause)
- Forced landing, emergency descent/landing
- Gear collapsed, emergency landing
  - terrain condition - roadway/highway

## Analysis

The pilot was in cruise flight on a personal flight when he noted a rise in the rear cylinder head temperature of the number two (rear) cylinder. He adjusted the mixture screw and watched the temperature continue to rise. During a precautionary landing, the engine stopped producing power, and the pilot was forced to land the airplane on a road. Subsequent examination showed that the piston in the rear cylinder would not move. Examination of the mixture screws showed that the mixture screw controlling the rear cylinder was in the lean position. The direction on rotation for leaning or enriching the mixture was not marked on the mixture screws.

## Factual narrative

On May 5, 1996, at 0930 Alaska daylight time, a wheel equipped Challenger 2, experimental airplane, N1591G, registered to and operated by the pilot, experienced an engine stoppage and subsequent forced landing near Talkeetna, Alaska.  The personal flight, operating under 14 CFR Part 91, departed Talkeetna and the destination was Birchwood, Alaska.  No flight plan was filed and visual meteorological conditions prevailed.  The certificated private pilot, the sole occupant, was not injured and the airplane received substantial damage.

During a telephone conversation with the pilot on May 5, 1996, he stated that during cruise flight he noticed a rise in the rear cylinder head temperature of the two cylinder, two cycle engine.  He adjusted the individual mixture screw and watched the cylinder head temperature continue to rise.  He selected the Talkeetna Spur Road as a precautionary landing area.  As he was aligning the airplane for a landing, the engine stopped producing power and he was forced to land on the road.  During the landing roll on the roadway, a truck was approaching from the opposite direction.  The pilot stated the truck was not slowing down so he guided the airplane as far to the right side of the road as possible.  The right main landing gear rolled into soft sand and the airplane veered off the roadway into cut alder bushes.  The right main and nose landing gear separated from the airplane.

Subsequent examination of the airplane showed that each cylinder had an individual mixture screw which consisted of a long shaft mounted overhead in the cockpit.  Examination of the mixture screws showed that the number two cylinder mixture screw was turned to a lean mixture setting.  Examination of the number two cylinder showed that the piston had seized moving in the cylinder.

The mixture screw shafts were labeled according to their corresponding cylinders.  However, the direction needed to turn the mixture shaft to enrich or lean the mixture was not marked.

## Aircraft

- Registration: [N1591G](https://openairdocs.org/deregistered/N1591G-2012-08-23), registration cancelled 2012-08-23, S/N CH2-0894-1196, built 1995 (OpenAirDocs)
- Reported make and model: GILLESPIE CHALLENGER 2 (CHALLENGER)
- Registry model: [Gillespie Clare L CHALLENGER II](https://openairdocs.org/model/gillespie-clare-l-challenger-ii) (registry code 05626L7) (OpenAirDocs)
- Registry engine: [Amateur-built UNKNOWN ENG](https://openairdocs.org/engine/amateur-built-unknown-eng) (registry code 99999) (OpenAirDocs)
- Category: Airplane, amateur-built
- Serial number: 08941196
- Engines: Hirth 2706 65 horsepower reciprocating
- Damage: Substantial damage
- Flight: Personal, Part 91
- Registered owner: Claire Gillispie
- Airworthiness certificate: Special, Experimental (Special)
- Departed: TKA, AK
- Destination: BCV, BIRCHWOOD, AK

## Flight crew

As NTSB recorded them. NTSB leaves out names.

- Pilot; age 55; private; airplane ratings: single-engine land; medical: class 3, valid medical--w/ waivers/lim; seat: front; flight hours: 93 total, 26 in this make and model, 49 as pilot in command, 4 in the last 90 days, 4 in the last 30 days, 1 in the last 24 hours

## Weather

- Conditions: Visual (VMC), Day
- Wind: 320° at 6 knots
- Visibility: 50 statute miles
- Lowest ceiling: none
- Temperature: 55 °F

## 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 19960505012859A](https://openairdocs.org/incident/19960505012859A), May 5, 1996: Amtrqc CHALLENGER2, Talkeetna, AK, Substantial damage. Lost power en route. Blocked landing on road by truck, veered off into alder bushes. Cylinder mixture screw to lean

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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