20091120023149A

Accident · Substantial damage

FAA accident report · Hughes 369E · Kahuku, HI · November 20, 2009

Date
November 20, 2009 · 16:32 local
Place
Kahuku, HI
Airport
Turtle Bay Resort
Phase of flight
Takeoff
Operating rules
Air taxi and commuter (Part 135)
Operator
K2DA
Damage
Substantial damage
Aircraft
N551CR
NTSB investigation
NTSBWPR10LA060
Reported as
Hughes 369E
People aboard
5
Fatal injuries
0
Other injuries
0
Pilot’s flight hours
6,200 total2,108 in this make and model127 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

PIC had loaded 4 passengers on-board the helicopter. Engine was started and spooled up to 100 % RPM when the left aft landing gear strut collapsed. The helicopter was on a portable landing pad trailer. When left aft landing gear strut collapsed it caused the helicopter to settle backward causing the tail rotor blades to strike the ground. The part the cracked at the idler bolt hole; landing gear aft left strut p/n 369H60001-51 assembly. There was no evidence of corrosion on the damaged parts. Until metal examination is conducted the apparent damage is from material failure. The damgaed landing gear strut assembly has being sent to NTSB iic for a metal examination.

As the FAA filed it

PIC HAD LOADED 4 PASSENGERS ON-BOARD THE HELICOPTER. ENGINE WAS STARTED AND SPOOLED UP TO 100 % RPM WHEN THE LEFT AFT LANDING GEAR STRUT COLLAPSED. THE HELICOPTER WAS ON A PORTABLE LANDING PAD TRAILER. WHEN LEFT AFT LANDING GEAR STRUT COLLAPSED IT CAUSED THE HELICOPTER TO SETTLE BACKWARD CAUSING THE TAIL ROTOR BLADES TO STRIKE THE GROUND. THE PART THE CRACKED AT THE IDLER BOLT HOLE; LANDING GEAR AFT LEFT STRUT P/N 369H60001-51 ASSEMBLY. THERE WAS NO EVIDENCE OF CORROSION ON THE DAMAGED PARTS. UNTIL METAL EXAMINATION IS CONDUCTED THE APPARENT DAMAGE IS FROM MATERIAL FAILURE. THE DAMGAED LANDING GEAR STRUT ASSEMBLY HAS BEING SENT TO NTSB IIC FOR A METAL EXAMINATION.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.