What was found
(CAN) WHILE INSPECTING CONTROL COLUMN ON A REGULAR INSPECTION, AN EXCESSIVE WEAR WAS NOTED, A SLIGHT VERTICAL FORCE APPLIED ON THE CONTROL WHEEL, BROKE THE COLUMN IN TWO PARTS.
- Difficulty date
- July 28, 1997
- Submitted
- March 26, 2000
- Operation
- General aviation
- Make and model
- Bnorm BN2B26
- System (JASC)
- 2701 · Control Column Section
- Part
- Column
- Part number
- NB45D859
- Condition
- Cracked
- Location
- Cockpit
- Part time
- 8,850 hours
- Stage of operation
- IN
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.