What was found
(CAN) COMPLETED INSPECTION AS PER SB 2/28 AND AD CF-84-01R1, FOUND CRACK IN WELD. 128 HOURS SINCE LAST INSPECTION.SUBMITTER FEELS LACK OF MAINTENANCE MAY BE RESPONSIBLE FOR THIS CRACK BEING NOTED EARLY.
- Difficulty date
- January 24, 2001
- Submitted
- February 23, 2001
- Operation
- General aviation
- Make and model
- Dhav DHC2MK1
- Aircraft time
- 15,151 hours
- Engine
- Pwa R985AN14B
- System (JASC)
- 2701 · Control Column Section
- Part
- Control Column
- Part number
- C2CF834A
- Condition
- Cracked
- Location
- At Weld
- Part time
- 15,576 hours
- Component
- Fuselage · Dhav
- Stage of operation
- IN
- How discovered
- V
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.