What was found
(CAN) ON ROUTINE INSPECTION FOUND THAT SECONDARY FLAP DRIVE CORE HAD BROKEN STRANDS AND BLISTERING, CORE REPLACED WITH SERVICEABLE. FUNCTION CARRIED OUT IAW MAINTENANCE MANUAL, AIRCRAFT RETURNED TO SERVICE
- Difficulty date
- June 24, 2005
- Submitted
- July 11, 2005
- Operation
- General aviation
- Make and model
- Dhav DHC8102
- Aircraft time
- 14,550 hours
- Engine
- Pwa PW120A
- Propeller
- Hamstd 14SF7
- System (JASC)
- 2750 · Trailing Edge Flap Control System
- Part
- Drive Assy
- Part number
- 5906989101
- Condition
- Broken
- Location
- Te Flaps
- Part time
- 15,588 hours, 11,057 cycles
- 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.