Aircraft landing gear retraction incident during takeoff

No fatalities • Santa Fe, United States of America • Takeoff (climb)

An aircraft experienced a loss of altitude and settled back onto the ground following the retraction of its landing gear during the takeoff phase.

What happened

During the beginning of a cross-country flight, an aircraft experienced an unexpected descent immediately after leaving the runway. After the aircraft achieved liftoff, the pilot initiated the process of raising the landing gear. Following this action, the aircraft lost sufficient altitude and settled back onto the ground just beyond the runway threshold.

Prior to the impact with the ground, the pilot successfully lowered the landing gear. Investigations conducted by the pilot and an FAA inspector revealed that both engines were operating at normal power levels and the aircraft was within its prescribed weight and balance limits.

Findings

Analysis of the aircraft's configuration indicated that the elevator trim was set to 12 degrees nose up, which significantly exceeded the required setting of 3 to 6 degrees. Additionally, data from the aircraft manufacturer suggests that the movement of the landing gear doors into the airstream during the retraction cycle creates increased induced drag. This excessive nose-up trim and the drag produced during the gear cycle were key factors in the aircraft's inability to maintain flight.

Probable cause

The aircraft failed to maintain altitude due to improper elevator trim settings and increased induced drag during landing gear retraction.

Frequently asked questions

What happened in the 1999-12-16 Piper PA-31 Cheyenne accident near Santa Fe, United States of America?

An aircraft experienced a loss of altitude and settled back onto the ground following the retraction of its landing gear during the takeoff phase.

Were there any fatalities in the 1999-12-16 Piper PA-31 Cheyenne accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 1999-12-16 involved a Piper PA-31 Cheyenne, registration N919RD, operated by Robert J. Denison, at Santa Fe, United States of America.

What was the probable cause of the accident?

The aircraft failed to maintain altitude due to improper elevator trim settings and increased induced drag during landing gear retraction.

Loading the flight search…