What was found
(CAN) INNER SURFACE LOWER CENTER AREA BETWEEN WINDOW AND LOWER FRAME. CORROSION SPOT 1CM WIDE. WHEN BLENDED MATERIAL THICKNESS WAS INSUFFICIENT. (TC NR 20060619013)
- Difficulty date
- May 30, 2006
- Submitted
- December 4, 2006
- Operation
- General aviation
- Make and model
- Beech 100BEECH
- Aircraft time
- 24,242 hours
- Engine
- Pwa PT6A28
- Propeller
- Hartzl HCD4N3A
- System (JASC)
- 5220 · Emergency Exits
- Part
- Skin
- Part number
- 115430100605
- Condition
- Corroded
- Location
- Emergency Exit
- Component
- Emergency Exit · Beech
- Component part number
- 100
- Stage of operation
- IN
- How discovered
- 9
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.