What was found
IAW AD 77-07-05(S) AND HILLER SB 36-1 REV 3, PARA 2(G). FOUND CRACK AT CONTROL BLADE CUFF INBOARD BOLT HOLE DURING 100-HOUR REPETATIVE DYE-PENETRANT INSPECTION. NOTE: 6,860 HOUR LIFE-LIMIT.
- Difficulty date
- March 26, 1997
- Submitted
- March 26, 2000
- Operation
- General aviation
- Aircraft
- N62392
- Make and model
- Hiller UH12E
- Aircraft serial
- 1591
- System (JASC)
- 6410 · Tail Rotor Blades
- Part
- Cuff
- Part number
- 36124
- Condition
- Cracked
- Location
- Control Blade
- Part time
- 4,402 hours
- Component
- 3612319
- 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.