SEA05CA149

NTSB accident investigation · Hughes 269A · Laurel, MT · July 21, 2005

Accident · Minor injuriesData collectionFinal report
Date
July 21, 2005, 11:00 local (17:00 UTC)
Place
Laurel, MT
Injuries
1 minor, 1 uninjured
Damage
Substantial damage
Phase of flight
Approach
Aircraft
N801CPHughes 269A
Weather
Visual (VMC) · Day
Status
Completed · report October 27, 2005
Report
Approved by Office Director
FAA report
20050721016349A
Case key
62038

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

the pilot's failure to maintain rotor rpm while executing a pinnacle approach, which resulted in a loss of control and collision with terrain.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of control - in flightApproach - vfr pattern - final approach
Rotor rpm - not maintainedPilot in commandCause
Aircraft control - not maintainedPilot in commandCause
In flight collision with terrain/waterDescent - uncontrolled
Terrain condition - pinnacle

Analysis

The commercial pilot was taking his initial flight instructor check ride in the helicopter with an FAA inspector acting as the check pilot. According to the pilot, during performance of a pinnacle approach, on final approach, about 300 to 400 yards from the pinnacle, he "got a bit shallow." He informed the check pilot that he "was going to level-off to regain a steep approach angle." After correcting the approach angle, he then continued the descent. Toward the end of the approach, the pilot began increasing lift to terminate the approach at a hover. He "had to do this somewhat early as we were still a bit high and a bit too far from the pinnacle." As he started to glance at the instruments, the check pilot called for a go-around. The pilot began the go-around (increasing collective and adding forward cyclic) and "then noticed our RPMs were low." According to the check pilot, "the approach to the pinnacle was a little shallow, but for the wind conditions was acceptable. At approximately 50 feet above the pinnacle, and with about 40 knots airspeed, the approach began to get steeper. I called for a go around. [The pilot] responded by lowering collective and moving aft on the cyclic." The check pilot "noticed the airspeed slow to around 20 knots" and "observed a reduction in rotor RPM and a large increase of manifold pressure." The helicopter began to yaw to the right rotating approximately 280 to 300 degrees clockwise prior to impacting the ground on its right side.

Factual narrative

On July 21, 2005, approximately 1100 mountain daylight time, a Hughes 269A helicopter, N801CP, sustained substantial damage when it collided with terrain following a loss of control during a pinnacle approach near Laurel, Montana. The commercial pilot, who was taking a check ride for his initial flight instructor rating, was not injured, and the check pilot, who was an FAA inspector, sustained minor injuries. The helicopter was registered to and operated by Northern Skies Aviation, Inc., of Laurel. Visual meteorological conditions prevailed, and no flight plan was filed for the 14 CFR Part 91 local flight that departed from the Laurel Municipal Airport about 1050.

According to the commercial pilot, during the final approach, about 300 to 400 yards from the pinnacle, he "got a bit shallow." He informed the check pilot that he "was going to level-off to regain a steep approach angle." After correcting the approach angle, he then continued the descent. Toward the end of the approach, the pilot began increasing lift to terminate the approach at a hover. He "had to do this somewhat early as we were still a bit high and a bit too far from the pinnacle." As he started to glance at the instruments, the check pilot called for a go-around. The pilot began the go-around (increasing collective and adding forward cyclic) and "then noticed our RPMs were low." The pilot stated that "the next thing I remember is our being out of control and then hitting the surface with the right side of the cabin striking the ground."

According to the check pilot, "the approach to the pinnacle was a little shallow, but for the wind conditions was acceptable. At approximately 50 feet above the pinnacle, and with about 40 knots airspeed, the approach began to get steeper. I called for a go around. [The pilot] responded by lowering collective and moving aft on the cyclic." The check pilot "noticed the airspeed slow to around 20 knots" and "observed a reduction in rotor RPM and a large increase of manifold pressure." The helicopter began to yaw to the right "rotating approximately 280 to 300 degrees clockwise prior to impact." Following the loss of control, he took the flight controls and attempted to level the helicopter and cushion the impact.

According to the operator, there was damage to the main and tail rotors, drive shafts, gearboxes, tail boom, horizontal stabilizer, cabin section, and cabin glass.

Aircraft

Registration
N801CP
Reported as
Hughes 269A
Category
Helicopter
Serial number
980965
Engine
Lycoming HIO-360-A1A, reciprocating
Damage
Substantial damage
Flight
Flight test · Part 91
Registered owner
Northern Skies Aviation, Inc.
Airworthiness certificate
Standard, Normal
Departed
6S8 · Laurel, MT

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew · 2

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
33
Certificate
Commercial
Instrument ratings
Helicopter
Medical
Class 2
Flight hours
187 total · 121 in this make and model · 31 in the last 90 days · 16 in the last 30 days
Role
Check pilot
Age
38
Certificates
Flight instructor, Airline transport
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Helicopter, Airplane
Medical
Class 2

Weather

Conditions
Visual (VMC) · Day

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.