China Lake Airport
Aircraft Accident/Incident Report

China Lake, California 93555
Friday, May 5, 2000 10:15 PDT

NTSB Narrative Summary Released at Completion of Accident

The twin-engine airplane experienced a loss of control after becoming entangled with a deploying parachute during cruise flight at 20,000 feet and 180 knots. The test flight was conducted to test an experimental parachute with a 331-pound anthropomorphic dummy that was rigged to the parachute. Two crewmembers in the airplane's cabin were to push the dummy out of the door and the parachute would deploy by pulling on a static line that was secured to a floor seat track. The static line for this flight had been reduced in length from 14 feet to 9 feet because of a previous test flight where a pin on the end of the static line became entangled with the elevator hinge and caused control problems. With the shortened static line, it was in tension when the dummy was positioned in the doorway. During the accident flight, once the dummy cleared the doorway, the static line deployed the pilot chute which in turn deployed the drogue chute. The drogue chute cleared the top of the left horizontal stabilizer while the dummy fell below. The dummy began oscillating and impacted the empennage and lower side of the horizontal stabilizer, eventually resulting in the partial separation and bending down of the stabilizer about midspan. As the dummy became entangled on the left horizontal stabilizer, the airplane made an uncommanded nose over into a negative G arc, which threw one crewmember about the cabin while the second crewmember was able to restrain himself by holding onto the static line. As the main parachute deployed, the drogue chute lines separated and the dummy and canopies fell away from the airplane. As the dummy fell away, the airplane pitched up and began an uncommanded roll to the right, stopping in a fully inverted attitude. The airplane initially nosed forward and then began a slow roll to the left, eventually stabilizing in wings level attitude. The pilots then returned the airplane to the airport and landed without further incident. Review of the parachute test program's Test Hazard Analysis revealed that the plan's cause/effect assessment and hazard mitigation actions inadequately addressed all potential "out of aircraft" hazard possibilities, including the effect of the parachute lines and/or dummy becoming entangled on the horizontal stabilizer. Additionally, no revision to the Test Hazard Analysis was noted after the previous static line entanglement incident and subsequent shortening of the static line.

NTSB Probable Cause Narrative

the inadvertent early deployment of the test parachute lines and dummy and it's entanglement with the horizontal stabilizer, which resulted from the operator's inadequate test plan substantiation process for shortening the parachute's static line. .

Event Information

Type of Event Accident
Event Date 5/5/2000
Event Day of the Week Friday
Time of Event 1015
Event Time Zone Pacific Daylight Time
Event City China Lake
Event State CALIFORNIA
Event Country --
Zipcode of the event site 93555
Event Date Year 2000
Event Date Month 5
MidAir Collision Indicator No
On Ground Collision occurred ? No
Event Location Latitude 354000N
Event Location Longitude 1174000W
Event Location Airport China Lake
Event Location Nearest Airport ID NID
Indicates whether the acc/inc occurred off or on an airport Off Airport/Airstrip
Distance from airport in statute miles --
Degrees magnetic from airport --
Airport Elevation --
Weather Briefing Completeness Unknown
Investigator's weather source Weather Observation Facility
Time of the weather observation 956 Pacific Daylight Time
Direction of event from weather observation facility (degrees) --
Weather Observation Facility ID NID
Elevation of weather observation facility 2283
Distance of event from weather observation facility (units?) --
Time Zone of the weather observation PDT
Lighting Conditions Day
Lowest Ceiling Height 20000
Lowest Non-Ceiling Height 8000
Sky/Lowest/Cloud Conditions Scattered
Sky Condition for Lowest Ceiling Broken
Visibility Runway Visual Range (Feet) --
Visibility Runway Visual Value (Statute Miles) --
Visibility (Statute Miles) 35
Air Temperature at event time (in degrees celsius) 28
Dew Point at event time (in degress fahrenheit) 9
Wind Direction (degrees magnetic) 190
Variable Wind Indicator Wind direction could be determined
Wind Speed (knots) 14
Wind Velocity Indicator --
Wind Gust Indicator Not Gusting
Wind Gust (knots) --
Altimeter Setting at event time (in. Hg) 29
Density Altitude (feet) --
Intensity of Precipitation --
METAR weather report --
Event Highest Injury Serious
On Ground, Fatal Injuries 0
On Ground, Minor Injuries 0
On Ground, Serious Injuries 0
Injury Total Fatal --
Injury Total Minor --
Injury Total None 3
Injury Total Serious 1
Injury Total All 1
Investigating Agency NTSB
NTSB Docket Number (internal use) 14292
NTSB Notification Source FAA
NTSB Notification Date May 5 2000 12:00AM
NTSB Notification Time 0
Fiche Number and/or location -used to find docket information DMS
Date of most recent change to record Nov 25 2003 11:36AM
User who most recently changed record NTSB\MONR
Basic weather conditions Visual Meteorological Cond
FAA District Office --

Aircraft Involved

Aircraft #1

Aircraft Registration Number N32229
NTSB Number LAX00GA185
Missing Aircraft Indicator N
Federal Aviation Reg. Part Part 91: General Aviation
Type of Flight Plan filed Military VFR
Flight plan Was Activated? No
Damage Substantial
Aircraft Fire None
Aircraft Explosion None
Aircraft Manufacturer's Full Name Beech
Aircraft Model 65-90
Aircraft Series Identifier 65-90
Aircraft Serial Number LJ-49
Certified Max Gross Weight 9300
Aircraft Category Airplane
Aircraft Registration Class U.S. Registered/U.S. Soil
Aircraft is a homebuilt? No
Flight Crew Seats --
Cabin Crew Seats --
Passenger Seats --
Total number of seats on the aircraft 2
Number of Engines 2
Fixed gear or retractable gear Retractable
Aircraft, Type of Last Inspection Continuous Airworthiness
Date of Last Inspection Feb 15 2000 12:00AM
Airframe hours since last inspection 22.3
Airframe Hours 11749.4
ELT Installed Yes
ELT Activated No
ELT Aided Location of Event Site No
ELT Type --
Aircraft Owner Name Joe Crottwell
Aircraft Owner Street Address --
Aircraft Owner City Apple Valley
Aircraft Owner State CA
Aircraft Owner Country USA
Aircraft Owner Zipcode 92307
Operator is an individual? No
Operator Name Aerospace Equipment Research Organization
Operator Same as Owner? No
Operator Is Doing Business As --
Operator Address Same as Owner? No
Operator Street Address 3 Mill Road, Suite 206
Operator City Willmington
Operator State A
Operator Country USA
Operator Zip code 19806
Operator Code --
Owner has at least one certificate None
Other Operator of large aircraft? --
Certified for Part 133 or 137 Operation --
Operator Certificate Number --
Indicates whether an air carrier operation was scheduled or not --
Indicates Domestic or International Flight --
Operator carrying Pax/Cargo/Mail --
Type of Flying (Per_Bus / Primary) Public Use
Second Pilot on Board Yes
Departure Point Same as Event Yes
Departure Airport Code NID
Departure City China Lake
Departure State CA
Departure Country USA
Departure Time 945
Departure Time Zone PDT
Destination Same as Local Flt dest & departure same, accident can occur anywhere
Destination Airport Code NID
Destination City China Lake
Destination State A
Destination Country USA
Specific Phase of Flight Cruise
Report sent to ICAO? --
Evacuation occurred No
Date of most recent change to record Sep 15 2003 1:24PM
User who most recently changed record COOS
Since inspection or accident Time of Accident
Event Location Runway Number and Location 32
Runway Length 9011
Runway Width 200
Sight Seeing flight No
Air Medical Flight No
Medical Flight --