Date & Time:
Jun 12, 2001 at 1300 LT
Type of aircraft:
Learjet 25
Operator:
Registration:
N333CG
Flight Phase:
Landing (descent or approach)
Flight Type:
Test
Survivors:
Yes
Schedule:
Newton - Salina
MSN:
25-262
YOM:
1978
Country:
United States of America
Region:
North America
Crew on board:
2
Crew fatalities:
0
Pax on board:
0
Pax fatalities:
0
Other fatalities:
0
Total fatalities:
0
Captain / Total hours on type:
1500
Copilot / Total hours on type:
470
Aircraft flight hours:
8419
Circumstances:
During a test flight, the airplane encountered an elevator system oscillation while in a high speed dive outside the normal operating envelope. The 17 second oscillation was recorded on the cockpit voice recorder and had an average frequency of 28 Hz. The aft elevator sector clevis (p/n 2331510-32) fractured due to reverse bending fatigue caused by vibration, resulting in a complete loss of elevator control. The flight crew reported that pitch control was established by using horizontal stabilizer pitch trim. The flightcrew stated that during final approach to runway 17 (13,337 feet by 200 feet, dry/asphalt) the aircraft's nose began to drop and that the flying pilot was unable to raise the nose using a combination of horizontal stabilizer trim and engine power. The aircraft landed short of the runway, striking an airport perimeter fence and a berm. The surface winds were from the south at 23 knots, gusting to 32 knots.
Probable cause:
The PIC's delayed remedial action during the elevator system oscillation, resulting in the failure of the aft elevator sector clevis due to reverse bending fatigue caused by vibration, and subsequent loss of elevator control. Factors contributing to the accident were high and gusting winds, the crosswind, the airport perimeter fence, and the berm.
Final Report:
N333CG.pdf130.52 KB
