Aviation Crash Map

Pohlman/Pohlman ROTORWAY EXEC 90 N94CJ

21 September 1997 · Westminster, Maryland, United States · Minor injuries

Summary

On 21 September 1997 at about 18:45 local time, a Pohlman/Pohlman ROTORWAY EXEC 90 registered N94CJ was involved in an accident near Westminster, Maryland, United States. One person was on board and one had minor injuries. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.

The record

Date
at 18:45
Classification
Accident
Location
Westminster, Maryland, United States
Nearest airport
Carroll County Regional (W54)
Coordinates
39.6496, -77.0401
Aircraft
Pohlman/Pohlman ROTORWAY EXEC 90
Registration
N94CJ
Category
Helicopter
Engines
1
Operator
Not recorded
Operating rule
Part 91: General Aviation
Purpose of flight
Personal
Phase of flight
Not recorded
Aircraft damage
Substantial
Weather
VMC
Light
Day
NTSB number
IAD97LA121

People

1 person had minor injuries.

On board Died Serious Minor Uninjured
1 0 0 1 0

Probable cause

The loss of power due to carburetor icing. A factor to this accident was the carburetor heat was not accessible from within the cockpit.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

The pilot remained in the traffic pattern for 40 minutes in his homebuilt helicopter, performing takeoffs and landings. At 200 feet on final approach with 19 inches of manifold pressure set, the engine stopped running. During the forced landing, the pilot maneuvered to avoid an embankment and impacted the ground damaging the tail boom and rotor blades. Examination of the engine revealed no mechanical malfunctions. The temperature/dew point was: 57 degrees Fahrenheit and 38 degrees Fahrenheit, respectively. Utilizing the 'Icing Probability Curves' charts, these temperatures combined with a glide power setting, placed the carburetor within the serious icing range. Examination of the helicopter revealed that the carburetor heat was preset prior to the flight and not accessible from inside the cockpit. After the accident, the FAA recommended to the manufacturer that a switch be placed in the cockpit. The manufacturer completed a modification allowing control of the carburetor heat from inside the cabin.

Quoted verbatim from the NTSB record.

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