N326AFDiamond Aircraft Ind DA 40

The flight instructor reported that, during an instructional flight with the student pilot at the flight controls, just prior to touchdown, the airplane started drifting left of center. The instructor told his student to go around, but the airplane had already reached the edge of the runway. When the instructor took control, the airplane had already exited the runway and came to rest on the adjacent dirt terrain, which resulted in substantial damage to the left wing. The flight instructor reported that there were no preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation.

On December 8, 2010, about 1310 Mountain Standard Time, a single-engine Diamond Aircraft DA 40, N326AF, sustained minor damage during a hard landing at the United States Air Force Academy Airfield (AFF), Colorado Spring, Colorado. Neither the student pilot nor instructor pilot were injured. The airplane was registered to and operated by Doss Aircraft Inc., of Colorado Springs, Colorado, under an exclusive contract with the United States Air Force (USAF). Visual meteorological conditions prevailed and a military flight plan was filed for the 14 Code of Federal Regulations Part 91 instructional flight. The local flight originated from AFF about 1250.

According to the instructor pilot, on the fourth touch-and-go maneuver of the day the student pilot bounced the airplane on landing. The instructor assessed that the bounce was not severe and allowed the student to remain on the controls for a second touchdown. As the airplane contacted the runway for the second time, the instructor observed the nose landing wheel depart the airplane. The airplane skidded down the runway for about 120-feet before coming to rest in an upright position.

An examination of the nose landing gear revealed that the nose fork had completely fractured on the left and right sides allowing the wheel to depart the airplane. The nose fork was sent to the Air Force Research Laboratory (AFRL) at Wright Patterson Air Force Base, Ohio, for examination.

The nose wheel pieces were examined on January 18, 2011. The examination determined that the failure was due to multiple crack initiation and propagation at the outboard side, inner diameter surface of both upper and lower webs in the forward machined pocket of both left and right forks until the remaining ligament could not sustain the applied operation loads, whereby final ductile overload failure ensued.

The AFRL Report and the nose wheel pieces were sent to the National Transportation Safety Board Materials Laboratory for verification. The Materials laboratory confirmed the Air Force’s findings.

The USAF Academy Chief of Flight Safety reported that the airplane had an airframe time of 559.9 hours at the incident. The nose wheel assembly had 2,674 cycles and was previously inspected on November 19, 2010. The airframe time from the inspection to the incident was 61.8 hours.

The National Transportation Safety Board had investigated several similar incidents involving failed nose gear forks on Diamond DA-20 airplanes. The designs of the two airplane models forks were very similar.

As a result of this National Transportation Safety Board investigation, the Air Force conducted a one-time inspection of its fielded fleet to identify any other nose forks that might have fatigue cracks. They implemented a method to nondestructively inspect all their airplanes’ nose wheel forks for fatigue cracks on a periodic basis. They evaluated and implemented ways to decrease low cycle, high intensity stress brought on by nose wheel shimmy during takeoffs and landings, and they published guidance outlining specific steps to take in the event of hard landings, bounces, nose wheel strikes, and excessive nose wheel shimmy or vibration.