Accident description
Last updated: 1 September 2014
Status:Final
Date:Sunday 6 June 1971
Time:18:11
Type:Silhouette image of generic DC93 model; specific model in this crash may look slightly different
McDonnell Douglas DC-9-31
Operator:Hughes Airwest
Registration: N9345
C/n / msn: 47441/503
First flight: 1969
Total airframe hrs:5542
Engines: 2 Pratt & Whitney JT8D-7
Crew:Fatalities: 5 / Occupants: 5
Passengers:Fatalities: 44 / Occupants: 44
Total:Fatalities: 49 / Occupants: 49
Collision casualties:Fatalities: 1
Airplane damage: Damaged beyond repair
Location:7 km (4.4 mls) N of Duarte, CA (   United States of America) show on map
Phase: En route (ENR)
Nature:Domestic Scheduled Passenger
Departure airport:Los Angeles International Airport, CA (LAX/KLAX), United States of America
Destination airport:Salt Lake City International Airport, UT (SLC/KSLC), United States of America
Flightnumber: 706
Narrative:
Airwest flight 706, a DC-9, was to fly from Los Angeles, CA (LAX) to Seattle, WA (SEA) with intermediate stops at Salt Lake City (SLC), Boise (BOI), Lewiston (LWS), Pasco (PSC) and Yakima (YKM). The aircraft departed Los Angeles at 18:02. At 18:09 the crew reported leaving FL120 and Los Angeles ARTCC cleared them direct to Daggett. At 17:16 h a US Marine Corps McDonnell F-4B Phantom 151458 departed Naval Auxiliary Air Station (NAAS) Fallon for a flight to MCAS El Toro at low altitude. The aircraft had several technical difficulties, including an inoperative transponder and a leak in the oxygen system. Due to deteriorating visibility northwest of Palmdale, the crew climbed to 15,500 feet . Shortly after level-off, aircraft was 50 miles from MCAS El Toro. The pilot executed a 360░ aileron roll at this time, which took approximately 3seconds to complete. The Radar Intercept Officer (RIO) estimated that the true airspeed in the climb and after level-off was 420 knots. The F-4B collided with the Airwest DC-9 about 1 minute and 20sec after the roll, at 15150 feet. After the collision, the F-4 began to tumble violently about the lateral axis. The RIO waited about 5 seconds, and, after seeing numerous warning lights in the cockpit, he ejected from the aircraft . The ejection was successful, and he parachuted to the ground without injury. The other F-4 crewmember did not survive the accident.

PROBABLE CAUSE: The failure of both crews to see and avoid each other but it is recognized that they had only marginal capability to detect, assess, and avoid the collision. Other causal factors include a very high closure rate, comingling of IFR and VFR traffic in an area where the limitation of the ATC system precludes effective separation of such traffic, and failure of the crew of BuNo458 to request radar advisory service, particularly considering the fact that they had an inoperable transponder."

Classification:
Mid air collision
Loss of control

Sources:

Official accident investigation report
investigating agency: National Transport Safety Bureau (NTSB) - USA
report status: Final
report number: NTSB/AAR-72-26
report released:30-AUG-1972
duration of investigation:451 days (1 year 2.9 months)
download report: Hughes Airwest DC-9, N9345, and U.S. Marine Corps F-4B, 151458, near Duarte, California, June 6, 1971. (NTSB/AAR-72-26)
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Follow-up / safety actions

NTSB issued 10 Safety Recommendations

Show all AD's and Safety Recommendations

Photos

photo of
Closing diagram of Airwest DC-9 and F-4 Phantom near Duarte, CA
photo of
View from Airwest DC-9 flight deck prior to collision with F-4 Phantom
photo of
View from F-4 Phantom flight deck prior to collision with Airwest DC-9
Add your photo of this accident or aircraft
 

Map
This map shows the airport of departure and the intended destination of the flight. The line between the airports does not display the exact flight path.
Distance from Los Angeles International Airport, CA to Salt Lake City International Airport, UT as the crow flies is 943 km (589 miles).

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