2 fatalities

Loss of Control After Left Engine Thrust Reverser Deployment During Initial Climb (N743R)

Montrose, United States of AmericaTakeoff (climb)

On April 13, 1973, a Rockwell Sabreliner 60 (registration N743R) operated by Continental Airlines was involved in an aviation accident near Montrose, United States of America during takeoff. 2 people were killed. Investigators recorded the probable cause as: Loss of control during initial climb after the left engine thrust reverser deployed. Factors: improper operations of powerplant, pilot-in-command failed to follow approved procedures, improper emergency procedures, unwanted thrust reversal, continued… This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary report: the U.S. National Transportation Safety Board (NTSB) historical archive (1962-1981)Updated 2026-07-04Data APIEditorial standards

After takeoff from Montrose Airport, the aircraft banked left to 55° and stalled, crashing in a huge explosion. Both pilots were killed. The probable cause was loss of control after the left engine thrust reverser deployed, with contributing factors including improper powerplant operations and failure to follow procedures.

Accident Overview

On an unspecified date, a multi-engine aircraft departed from Montrose Airport. During the initial climb, as the aircraft reached an altitude of approximately 1,000 feet, it executed an uncommanded left bank to an angle of 55°. Subsequently, the airplane stalled and descended uncontrollably, impacting the ground with a huge explosion. The force of the impact and the resulting post-crash fire destroyed the aircraft. Both pilots onboard were killed.

Probable Cause

The official investigation determined the probable cause of the accident was a loss of control during the initial climb after the left engine thrust reverser deployed. The following factors were reported in the investigation:

  • Improper operations of the powerplant,
  • The pilot-in-command failed to follow approved procedures,
  • Improper emergency procedures,
  • Unwanted thrust reversal,
  • Continued operation of the left engine at climb power after the unwanted in-flight deployment of the left engine thrust reverser.

Sequence of Events

After takeoff, while climbing through 1,000 feet, the aircraft experienced an unwanted deployment of the left engine thrust reverser. The flight crew continued to operate the left engine at climb power despite the deployment. This led to an asymmetric thrust condition, causing the airplane to bank sharply to the left. The bank angle reached 55°, at which point the aircraft stalled. The crew was unable to recover from the stall before the aircraft crashed.

Damage and Injuries

The aircraft was destroyed by the impact and subsequent fire. Both pilots sustained fatal injuries.

Conclusions

The investigation concluded that the loss of control resulted from the deployment of the left engine thrust reverser, compounded by the pilots' failure to follow proper emergency procedures and their continued operation of the affected engine at climb power.

Frequently asked questions

What happened in the 13 Apr 1973 Rockwell Sabreliner 60 accident near Montrose, United States of America?

After takeoff from Montrose Airport, the aircraft banked left to 55° and stalled, crashing in a huge explosion. Both pilots were killed. The probable cause was loss of control after the left engine thrust reverser deployed, with contributing factors including improper powerplant operations and failure to follow…

Were there any fatalities in the 13 Apr 1973 Rockwell Sabreliner 60 accident?

The accident was fatal, resulting in 2 fatalities.

What aircraft was involved and where did it happen?

The accident on 13 Apr 1973 involved a Rockwell Sabreliner 60, registration N743R, operated by Continental Airlines, at Montrose, United States of America.

What was the probable cause of the accident?

Loss of control during initial climb after the left engine thrust reverser deployed. Factors: improper operations of powerplant, pilot-in-command failed to follow approved procedures, improper emergency procedures, unwanted thrust reversal, continued operations of left engine at climb power after unwanted in-flight…