7 fatalities

Left Wing Failure Leads to Crash at Dallas Elementary School (N3831C)

Dallas-Love Field, United States of AmericaLanding (descent or approach)

On September 27, 1967, a Rockwell Aero Commander 560 (registration N3831C) operated by Ling-Temco-Vought (LTV Aerospace) was involved in an aviation accident near Dallas-Love Field, United States of America during landing or approach. 7 people were killed. Investigators recorded the probable cause as: Uncontrolled descent following the structural failure of the left wing due to fatigue fracture. Two overlapping rivet holes found in aft leg of the spar cap. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 2 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 2026-06-12Data APIEditorial standards

An aircraft on approach to Dallas Love Field lost its left wing due to fatigue fracture, crashed into Bradfield Elementary School, killing all seven aboard; no ground injuries were reported.

Accident Overview

While approaching Dallas-Love Field Airport, an aircraft operated on behalf of LTV Electrosystems experienced a catastrophic structural failure. The left wing separated from the airframe, resulting in a complete loss of control. The airplane entered a dive and subsequently crashed into Bradfield Elementary School, a structure on the ground.

Occupants and Ground Impact

All seven individuals aboard the aircraft were killed in the crash. Despite the impact, no injuries were sustained by any persons on the ground. The school building sustained extensive damage, with parts of the structure destroyed. Additionally, several vehicles in the vicinity were damaged or destroyed.

Investigation Findings

The official investigation determined that the accident was caused by an uncontrolled descent following the structural failure of the left wing. The failure was attributed to a fatigue fracture. Specifically, investigators identified two overlapping rivet holes in the aft leg of the spar cap, which led to the weakening of the wing structure.

The examination did not specify the aircraft type, registration, or other operational details beyond the operator and location.

Probable cause

Uncontrolled descent following the structural failure of the left wing due to fatigue fracture. Two overlapping rivet holes found in aft leg of the spar cap.