What was found
SEPARATION BETWEEN TIP WEIGHT SUPPORT BLOCK AND BLADE SKIN. RECOMMEND ALL IN SERVICE BLADES BE INSPECTED FOR DEBONDING OF TIP WEIGHT CHAMBER.
- Difficulty date
- April 1, 1996
- Submitted
- March 26, 2000
- Operation
- General aviation
- Filed by
- RW1R467K
Sikorsky Aircraft Corporation - Make and model
- Skrsky S76
- System (JASC)
- 6410 · Tail Rotor Blades
- Part
- Tail Rotor Assy
- Part number
- 7610105101041
- Condition
- Separation
- Location
- Tip Weight
- Part time
- 5,408 hours
- 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.