LAX96LA207

NTSB accident investigation · McDonnell Douglas MD-600 · Thermal, CA · May 28, 1996

Accident · No injuriesLimited investigationFinal report
Date
May 28, 1996, 07:11 local (14:11 UTC)
Place
Thermal, CA
Injuries
1 uninjured
Damage
Destroyed
Phase of flight
Maneuvering
Aircraft
N600RNMcDonnell Douglas MD-600
Weather
Visual (VMC) · Day
Status
Completed · report August 20, 1996
Report
Approved by Office Director
FAA report
19960528011679A
Case key
29449

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

inadequate design of the stress limits for cyclic control of the helicopter.

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.

Abrupt maneuverManeuvering
Design stress limits of aircraft - performedPilot in command
Airframe/component/system failure/malfunctionManeuvering
Misc rotorcraft,main rotor/tail boom contact
Acft/equip,inadequate designManufacturerCause
Forced landingEmergency descent/landing
Hard landingEmergency descent/landing
Terrain condition - high vegetation

Analysis

The flight was part of an engineering test flight series to complete the Part 27 certification for a new rotorcraft. The specific test point was part of a flight strain survey and involved cyclic control reversals. The pilot had set the parameters and executed the cyclic control inputs as planned. Almost simultaneous with the aft movement of the cyclic there was a loud noise and immediate vibrations in the aircraft and the controls. A pilot in the chase aircraft informed the pilot that a main rotor blade had struck and severed the tail boom. A power off autorotation was accomplished without the tail rotor system. The resultant hard landing was onto a pile of dry brush which was ignited by the hot engine exhaust. The brush fire destroyed the aircraft.

Factual narrative

On May 28, 1996, about 0711 hours Pacific daylight time a McDonnell Douglas MD-600 helicopter, N600RN, was destroyed during flight tests at Thermal, California. The pilot was not injured. The helicopter was in a flight test program for FAA certification under 14 CFR Part 27. The specific test point at the time of the mishap was part of a flight strain survey and involved cyclic control reversals.

The pilot set the parameters and executed the cyclic inputs as planned. Almost simultaneous with the aft movement of the cyclic there was a loud noise and immediate vibrations in the aircraft and controls. There was a chase aircraft for the mission and the chase pilot advised that the tail boom had been struck by a main rotor blade and had separated from the airframe. The pilot of the mishap aircraft then experimented with powered flight, but found that the right yaw was not controllable. He elected to continue the power off autorotation with a controllable left yaw. The autorotation was continued to a vacant field with some piles of brush and other desert debris. The pilot used available rotor rpm, cyclic, and collective control to execute a modified autorotation landing. The resultant landing was onto a brush pile with some skid and main rotor blade damage. The engine exhaust was adjacent to dry brush and grass which resulted in a grass fire. The ground fire destroyed the helicopter.

Aircraft

Registration
N600RN
Reported as
McDonnell Douglas MD-600
Category
Helicopter
Serial number
RN001
Airframe hours
39
Engine
Allison 250-C47, 621 horsepower, turbo shaft
Damage
Destroyed
Fire
On-Ground
Flight
Part 91
Registered owner
Mcdonnell Douglas Helicopter
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Annual · December 15, 1995 · 39 hours before
Departed
TRM · CA

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

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
48
Certificates
Commercial, Airline transport
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Helicopter, Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
10,191 total · 1,095 in this make and model · 8,000 as pilot in command · 40 in the last 90 days · 20 in the last 30 days · 4 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
320° at 7 knots
Visibility
20 statute miles
Lowest ceiling
None
Temperature
68 °F, dew point 52 °F
Altimeter
29.00 inHg
Observed at
TRM, 4 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.