20030407005609A

Accident · Substantial damage

FAA accident report · Hughes 369D · Queets, WA · April 7, 2003

Date
April 7, 2003 · 09:05 local
Place
Queets, WA
Phase of flight
Low Level Operations
Operating rules
Rotorcraft external load (Part 133)
Damage
Substantial damage
Aircraft
N5225C
NTSB investigation
NTSBSEA03LA058
Reported as
Hughes 369D
Fatal injuries
0

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.

(-23) MD 396D helicopter sustained substantial damage during a hard landing following a loss of engine power while engaged in cedar block lift work in accordance with title 14 code of federal regulations part 133 operations. The pilot reported that initially, he experienced a power surge and then about five minutes later a total loss of power. He released the external load and transitioned into an autorotational descent. During the descent, the main rotor blades contacted trees and the helicopter landed hard collapsing the left skid. The pilot reported approximately 120 pounds of fuel on board at the time of the accident. (See attached sheet).

As the FAA filed it

(-23) MD 396D HELICOPTER SUSTAINED SUBSTANTIAL DAMAGE DURING A HARD LANDING FOLLOWING A LOSS OF ENGINE POWER WHILE ENGAGED IN CEDAR BLOCK LIFT WORK IN ACCORDANCE WITH TITLE 14 CODE OF FEDERAL REGULATIONS PART 133 OPERATIONS. THE PILOT REPORTED THAT INITIALLY, HE EXPERIENCED A POWER SURGE AND THEN ABOUT FIVE MINUTES LATER A TOTAL LOSS OF POWER. HE RELEASED THE EXTERNAL LOAD AND TRANSITIONED INTO AN AUTOROTATIONAL DESCENT. DURING THE DESCENT, THE MAIN ROTOR BLADES CONTACTED TREES AND THE HELICOPTER LANDED HARD COLLAPSING THE LEFT SKID. THE PILOT REPORTED APPROXIMATELY 120 POUNDS OF FUEL ON BOARD AT THE TIME OF THE ACCIDENT. (SEE ATTACHED SHEET).

NTSB investigation

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

Other reports on N5225C · 2

Matched to the same aircraft by N-number and date.