Accident · substantial damage
Nov 29, 1986 · Capac, MITEN MINUTES AFTER TAKEOFF AND JUST PRIOR TO LETDOWN FROM 350 FEET AGL A MAIN ROTOR BLADE DRAG STRUT FAILED DUE TO PROGRESSIVE FATIGUE THROUGH A THREADED PORTION OF THE STRUT. ONLY PARTIAL CONTROL OF THE HELICOPTER WAS POSSIBLE AFTER THE FAILURE. THE PILOT LOST CONTROL OF THE AIRCRAFT AT ONE POINT, BUT REGAINED CONTROL IN TIME TO PERFORM A HARD, SLIDING LANDING IN A FIELD. SUBSTANTIAL DAMAGE…
- Damage
- Substantial
- Injuries
- None
- Report
- CHI87LA045
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CHI87LA045)