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Last updated: 11 May 2021
Date:Sunday 6 June 1971
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
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
Aircraft damage: Damaged beyond repair
Location:7 km (4.4 mls) N of Duarte, CA (   United States of America)
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
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:

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."

Accident investigation:
Investigating agency: NTSB
Status: Investigation completed
Duration: 1 year and 3 months
Accident number: NTSB/AAR-72-26
Download report: Final report

Mid air collision
Loss of control

Follow-up / safety actions

NTSB issued 10 Safety Recommendations

Show all...


photo of DC-9-31-N9345
accident date: 06-06-1971
type: McDonnell Douglas DC-9-31
registration: N9345
photo of DC-9-31-N9345
accident date: 06-06-1971
type: McDonnell Douglas DC-9-31
registration: N9345
photo of DC-9-31-
Closing diagram of Airwest DC-9 and F-4 Phantom near Duarte, CA
photo of DC-9-31-
View from Airwest DC-9 flight deck prior to collision with F-4 Phantom
photo of DC-9-31-
View from F-4 Phantom flight deck prior to collision with Airwest DC-9
photo of DC-9-31-N9345
accident date: 06-06-1971
type: McDonnell Douglas DC-9-31
registration: N9345

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).
Accident location: Approximate; accuracy within a few kilometers.

This information is not presented as the Flight Safety Foundation or the Aviation Safety Network’s opinion as to the cause of the accident. It is preliminary and is based on the facts as they are known at this time.
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