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January 17, 2009, Farmington, N.M., Beech A36 Bonanza

At 1858 local time the airplane was substantially damaged after departing the side of the runway. The solo private pilot was not injured although the airplane was substantially damaged. Visual conditions prevailed. The pilot later stated he positioned the gear handle in the "down" position, but the three position lights did not activate, so the pilot radioed the control tower and requested an visual inspection of the landing gear. After performing a low approach, tower personnel responded the landing gear appeared to be down. After touchdown, the gear collapsed, the pilot lost control of the airplane and it exited the runway.

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Key Takeaways:

  • An airplane sustained substantial damage after its landing gear collapsed upon touchdown, causing it to depart the runway, though the solo pilot was uninjured.
  • Prior to landing, the pilot observed the landing gear position lights did not activate and, after a low approach, received visual confirmation from the control tower that the gear appeared to be down.
  • Investigation revealed the gear collapse was caused by an incorrectly installed left main landing gear retract rod and a damaged/inoperative limit switch, both stemming from recent maintenance performed in December.
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At 1858 local time the airplane was substantially damaged after departing the side of the runway. The solo private pilot was not injured although the airplane was substantially damaged. Visual conditions prevailed.

The pilot later stated he positioned the gear handle in the “down” position, but the three position lights did not activate, so the pilot radioed the control tower and requested an visual inspection of the landing gear. After performing a low approach, tower personnel responded the landing gear appeared to be down. After touchdown, the gear collapsed, the pilot lost control of the airplane and it exited the runway.

Subsequent investigation revealed various work was performed on the landing gear in December. An examination of the work determined the left main landing gear retract rod was installed incorrectly and failed on the accident flight. The landing gear transmission/motor limit switch was damaged and rendered inoperative.

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