LAX00TA006

NTSB accident investigation · McDonnell Douglas 369E · Moreno Valley, CA · October 8, 1999

Accident · No injuriesFinal report
Date
October 7, 1999, 20:05 local (Oct 8, 1999, 03:05 UTC)
Place
Moreno Valley, CA
Injuries
3 uninjured
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N991SDMcDonnell Douglas 369E
Weather
Visual (VMC) · Night/dark
Status
Completed · report April 25, 2001
Report
Approved by Office Director
FAA report
19991007028609A
Case key
47553

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 failure of the pilot to maintain sufficient forward airspeed to preclude an inadvertent encounter with loss of tail rotor effectiveness, which resulted in a loss of yaw control. The pilot's failure to initiate timely remedial action is a factor.

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 flightManeuvering
Weather condition - unfavorable wind
Airspeed - inadequatePilot in commandCause
Translational lift - not maintainedPilot in commandCause
Loss of tail rotor effectiveness - encountered
Remedial action - delayedPilot in commandFactor
In flight collision with terrain/waterDescent - uncontrolled
Terrain condition - open field

Analysis

The Sheriff's Department helicopter was orbiting over ground based law enforcement activity. It was a dark night and the winds aloft were 20 to 25 knots at 500 feet agl. The pilot said he was attempting to shine the helicopter's spotlight on a vehicle; however, the wind kept blowing the helicopter past the location on each of the first two orbits. On the third orbit, the pilot inadvertently allowed the helicopter to slow below translational lift speed and the helicopter yawed 180 degrees to the right uncontrollably. The pilot momentarily recovered directional control of the helicopter but then the right yaw resumed. He made several more attempts to recover directional control of the helicopter but when he saw the altitude becoming low, he flew to a pre-selected landing zone where the helicopter landed hard while in a right yawing spin. During the landing the main rotor blades severed the tail boom and the helicopter came to rest on its right side.

Factual narrative

On October 7, 1999, at 2005 hours Pacific daylight time, a McDonnell Douglas 369E helicopter, N991SD, was substantially damaged during a forced landing at Moreno Valley, California, following an in-flight loss of directional control. The commercial pilot and two observer crewmembers were not injured. The helicopter was operated by the Riverside County Sheriff's Department under the provisions of 14 CFR Part 91 as a public-use aircraft. Visual meteorological conditions prevailed and no flight plan was filed for the local area patrol flight, which originated from Hemet, California, at 1950.

According to the Sheriff's Department report, it was a dark night and the winds aloft were northerly at 20 to 25 knots, at 500 feet agl, as the pilot orbited over ground based law enforcement activity. In accordance with department operating procedures, the pilot had identified a school athletic field as a suitable emergency landing site. He was attempting to shine the helicopter's spotlight on a vehicle; however, the northerly wind kept blowing the aircraft well south of the location on each of the first two orbits. On the third orbit, he inadvertently allowed the helicopter to slow below translational lift speed and the helicopter yawed 180 degrees to the right uncontrollably. The pilot momentarily recovered directional control of the helicopter but then the right yaw resumed. He made several more attempts to recover directional control of the helicopter but when he saw the altitude becoming low, he flew to the pre-selected landing zone where the helicopter landed hard while in a right yawing spin. During the landing the main rotor blades severed the tail boom and the helicopter came to rest on its right side.

Aircraft

Registration
N991SD
Reported as
McDonnell Douglas 369E
Category
Helicopter
Serial number
500E
Airframe hours
5,474
Engine
Allison 250C20B, 420 horsepower, turbo shaft
Damage
Substantial damage
Flight
Public aircraft · Part 91
Registered owner
Riverside Co. Sheriff'S Dept
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · September 1, 1999 · 30 hours before
Departed
HMT · Hemet, CA

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
41
Certificate
Commercial
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane, Helicopter
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
2,737 total · 94 in this make and model · 2,153 as pilot in command · 174 in the last 90 days · 51 in the last 30 days · 6 in the last 24 hours

Weather

Conditions
Visual (VMC) · Night/dark
Wind
340° at 9 knots
Visibility
35 statute miles
Lowest ceiling
None
Temperature
77 °F, dew point 28 °F
Altimeter
29.00 inHg
Observed at
RIV, 1 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.