1 fatality

Tail Stand Discovery Precedes Fatal Stall and Crash of Beechcraft TC-45J (N9231)

Memphis, United States of AmericaTakeoff (climb)

On October 9, 1987, a Volpar Turboliner 18 (registration N9231) operated by Connie Kalitta Services was involved in an aviation accident near Memphis, United States of America during takeoff. One person was killed. Investigators recorded the probable cause as: Occurrence #1: loss of control - in flight. Phase of operation: maneuvering - turn to reverse direction. Findings: 1. (f) aircraft preflight - inadequate - pilot in command; 2. (f) aircraft weight and balance - not performed - pilot in command; 3. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 3 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 2026-06-11Data APIEditorial standards

A Beechcraft TC-45J crashed after the pilot was informed the tail stand was still attached. The aircraft stalled during a return maneuver, was 379 lbs over max takeoff weight, and had a forward CG. The pilot had low experience and no load manifest was found.

Accident Details

Shortly after takeoff, the pilot was informed by the tower that the tail stand, used to prevent the aircraft from tipping on its tail when loaded, was still attached. The pilot requested a teardrop turn to return to the departure runway. While maneuvering back to runway 36R, the aircraft stalled. Recovery was attempted, but the aircraft impacted the ground before completing the level off. The approach controller reported observing a Mode C indication of 700 feet; the airport elevation is 332 feet. The accident occurred during bright night conditions.

Aircraft Information

The aircraft was a modified Beechcraft TC-45J, initially built in 1943 and rebuilt by Hamilton in 1971. It was found to be 379 pounds over the maximum takeoff weight, and its center of gravity (CG) was at least 3 inches forward of the forward limit. No record of a load manifest was found.

Pilot Information

The pilot, who was the sole occupant and was killed, had low pilot-in-command (PIC) experience. He received 2.7 documented flight hours with the operator's instructor pilot, including a 135 competency check ride of 1.1 hours. The operator's initial training certification for the pilot showed 5 hours of flight training.

Probable Cause (Official Findings)

Occurrence #1: loss of control - in flight. Phase of operation: maneuvering - turn to reverse direction. Findings: 1. (f) aircraft preflight - inadequate - pilot in command; 2. (f) aircraft weight and balance - not performed - pilot in command; 3. (f) lack of total experience in type of aircraft - pilot in command; 4. Light condition - bright night; 5. (f) inadequate initial training - company/operator management; 6. (f) diverted attention - pilot in command; 7. (c) airspeed (vs) - not maintained - pilot in command; 8. (c) stall - inadvertent - pilot in command. Occurrence #2: in flight collision with terrain/water. Phase of operation: descent - uncontrolled.