What was found
(CAN) ALL THREE FLYING WIRES ATTACHED TO CLEVIS AT THE FUSELAGE WERE FOUND CRACKED DURING INSPECTION. CAUSE OF CRACKS TO BE DETERMINED.
- Difficulty date
- May 11, 1998
- Submitted
- March 26, 2000
- Operation
- General aviation
- Make and model
- Dhav DHC2MK1
- Engine
- Pwa R985AN14B
- System (JASC)
- 2720 · Rudder Control System
- Part
- Clevis
- Part number
- 6AO2059
- Condition
- Cracked
- Location
- Rudder
- Part time
- 360 hours
- Component
- Wiplineinc · 6100
- 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.