Hughes 269C N9692F

Summary

On 14 June 2000 at about 16:15 local time, a Hughes 269C registered N9692F, operated by MAX & Ene's Aeroplanes Co, Inc, was involved in an accident near Santa Clarita, California, United States. 2 people were on board and nobody was injured. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.

Date

14 June 2000 at 16:15

Classification

Accident

Location

Santa Clarita, California, United States

Coordinates

Not recorded

Aircraft

Hughes 269C

Registration

N9692F

Category

Helicopter

Engines

1

Operator

MAX & Ene's Aeroplanes Co, Inc

Operating rule

Part 91: General Aviation

Purpose of flight

Instructional

Phase of flight

Not recorded

Aircraft damage

Substantial

Weather

VMC

Light

Day

NTSB number

LAX00LA226

Nobody was injured.

Settling with power precipitated by a wind direction change during the approach to land sequence and the check pilot's delayed remedial action to correct the event. Factors in the accident were crew resource management coordination concerning flight control authority and unsuitable terrain for landing.

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

Read the full NTSB narrative

The helicopter touched down on the downside portion of a hill, struck a tree, and became inverted. The purpose of the flight was to conduct a new hire checkout. The purpose of the landing was to retrieve a door that had come off in flight the day prior to the accident. During the approach for landing the new hire pilot performed a high and low reconnaissance of the area. This was to check for wind direction and verify the landing area was clear of obstructions. About 100 feet from the intended touchdown point, the wind changed direction and became a tailwind. He attempted to compensate for the loss of altitude by increasing power, but the engine did not have enough power. The helicopter was still controllable with full left rudder. The helicopter started to settle and the engine and rotor rpm were decaying. When the new hire attempted to fly down hill to regain rpm, he felt resistance on the controls, but did not recall the check pilot indicating that he was going to take the controls. The check pilot instructed the other pilot to verify his rpm and verbalized that he was taking the flight controls. He attempted to perform a low rpm recovery. He reduced the collective and rolled on the throttle. However, he noted that the throttle was already in the full on position. He attempted to recover rpm by moving the collective up and down to clear the ridgeline. The helicopter continued to settle and landed hard. No discrepancies were noted with engine power.

Quoted verbatim from the NTSB record.