Casualties unknown

2022-03-02: F-16CG (89-2035) — U.S. Air Forces in Europe (USAFE) — AVIANO AB, ITALY, IT

AVIANO AB, ITALY, IT

On March 2, 2022, a F-16CG (registration 89-2035) operated by U.S. Air Forces in Europe (USAFE) was involved in an aviation accident near AVIANO AB, ITALY, IT. Investigators recorded the probable cause as: Failure of the left outboard main landing gear wheel bearing. This summary draws on records from the U.S. Air Force Accident Investigation Board (AIB); 3 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. Air Force Accident Investigation Board (AIB)Primary reportUpdated 1781081675Data APIEditorial standards

On 2 March 2022, a USAF F-16CG (T/N 89-2035) lost its left main landing gear wheel during takeoff at Aviano AB, Italy. The pilot executed a gear-up landing; no injuries occurred. Estimated repair cost: $6.1 million.

Accident Overview

On 2 March 2022, at 11:24:56 local time, a United States Air Force F-16CG Fighting Falcon, tail number 89-2035, call sign VIPER 21, assigned to the 555th Fighter Squadron, 31st Fighter Wing at Aviano Air Base, Italy, experienced separation of the left main landing gear wheel during takeoff from runway 05. The mishap pilot (MP) was leading a two-ship formation on an air tasking order mission.

During the takeoff roll, the anti-skid caution light illuminated, prompting the MP to abort the planned departure. The mishap wingman conducted an aerial inspection and, along with air traffic control, initially reported a blown tire. Security forces later found the separated wheel on the airfield, confirming the loss of the entire left main landing gear wheel.

Gear-Up Landing

After consultation with supervisory personnel and a flight safety engineer, the MP decided to land with the landing gear retracted. At 13:40:59 local time, the aircraft touched down on runway 05 and skidded to a stop at 13:41:26. The pilot was uninjured and egressed safely as emergency vehicles responded. The aircraft sustained significant damage to its ventral fins and electronic countermeasures pod due to sliding on the runway. Repair costs were estimated at $6.1 million.

Cause Determination

The Abbreviated Accident Investigation Board found, by a preponderance of the evidence, that the mishap was caused by failure of the left outboard main landing gear wheel bearing. Excessive heat and friction from the failed bearing caused softening and deformation of the bearing cone. Rotational forces led to undesired rotation of the cone around the axle, friction-welding it to the stationary spacer. Shear forces then fractured the spacer's anti-rotational tab, allowing the spacer to rotate counter-clockwise. Friction between the rotating spacer and wheel nut sheared the locking tab, loosening the nut during takeoff. Once the wheel separated, the only safe recovery option was a gear-up landing.

Probable cause

Failure of the left outboard main landing gear wheel bearing.