What was found
(CAN) DURING INSPECTION, THE RIGHT FLAP ROD ENDS WERE FOUND WORN. DURING REPLACEMENT, THE TREADS ON THE ROD SNAPPED. FURTHER INVESTIGATION REVEALED THEY WERE PARTIALLY CRACKED BEFORE REMOVAL OF THE ROD END.
- Difficulty date
- August 3, 1999
- Submitted
- March 26, 2000
- Operation
- General aviation
- Make and model
- Dhav DHC2MK1
- Engine
- Pwa R985AN14B
- System (JASC)
- 2752 · Trailing Edge Flap Actuator
- Part
- Rod
- Part number
- C2CF341A
- Condition
- Cracked
- Location
- Te Flap
- 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.