What was found
(CAN) THE FLAP CONTROL ROD ATTACHMENT BRACKET HORN WAS CRACKED IN THE RADIUS OF EACH OF THE BENDS FOR TAB ATTACHMENTS RIVETED TO THE FLAP STRUCTURE. PART REPLACED.
- Difficulty date
- February 15, 2000
- Submitted
- April 14, 2000
- Operation
- Air carrier
- Make and model
- Slinds 100180
- Aircraft time
- 1,528 hours
- Engine
- Lyc O360A2F
- Propeller
- Mcauly 1A170CFA
- System (JASC)
- 5753 · Trailing Edge Flaps
- Part
- Bracket
- Part number
- 32190
- Condition
- Cracked
- Location
- Te Flap
- Component
- Wing Flap · Rkwell · 320042
- 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.