What was found
(CAN) AFTER COMPLETING AD CF-80-03 & SB6/390 THE TRIM ROD WAS BEING ADJUSTED AT INSTALLATION WHEN IT WAS FOUND THAT THE FORWARD SWAG WAS ALLOWING THE ROD END FITTING TO ROTATE. THE ROD WAS REPLACED.
- Difficulty date
- April 11, 2002
- Submitted
- April 26, 2002
- Operation
- General aviation
- Make and model
- Dhav DHC6300
- Aircraft time
- 15,228 hours
- Engine
- Pwa PT6A27
- System (JASC)
- 2750 · Trailing Edge Flap Control System
- Part
- Rod
- Part number
- C6CT10461
- Condition
- Loose
- Location
- Te Flap Control
- 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.