20070104000149A

Accident · Substantial damage

FAA accident report · Hughes 369D · Lyman, WA · January 4, 2007

Date
January 4, 2007 · 12:55 local
Place
Lyman, WA
Phase of flight
Hovering
Operating rules
Rotorcraft external load (Part 133)
Operator
GHZL
Damage
Substantial damage
Aircraft
N1088G
NTSB investigation
NTSBSEA07LA041
Reported as
Hughes 369D
Reported engine
Allison 250C20B
Fatal injuries
0
Pilot’s flight hours
20,650 total20,484 in this make and model200 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.

(-23) On 01/04/07, at approximately 1255 PST, a Hughes 369D helicopter, N1088G, owned and operated by the pilot privacy data omitted of hi line helicopters, experienced a loss of power as it was coming to a hover while performing external load work (slinging shake bolts) in snowing conditions. The aircraft dropped vertically approx. 130' crashing onto a stump in the clear cut area the aircraft was working. The aircraft received substantial damage, the pilot was seriously injured. After the accident the pilot stated, while maneuvering the aircraft he saw a large amount of snow and ice slide from the front of the canopy back into the air inlet area and the engine flamed out. During the on site accident investigation inspectors from this office recorded the position of the engine anti-ice lever in the off position. Phone conversation with the pilot and this office on 01/10/2007, the pilot stated he had the engine anti-ice was on, approx. 25 gals. Of fuel, and flown approx. 5 to 8 minutes on the fuel load before the accident. Aircraft flight manual limitations permits flight operations in falling and or blowing snow when the auto reignition and engine epo is installed and working. N1088G was in compliance with this limitation.

As the FAA filed it

(-23) ON 01/04/07, AT APPROXIMATELY 1255 PST, A HUGHES 369D HELICOPTER, N1088G, OWNED AND OPERATED BY THE PILOT ^PRIVACY DATA ^ OF HI LINE HELICOPTERS, EXPERIENCED A LOSS OF POWER AS IT WAS COMING TO A HOVER WHILE PERFORMING EXTERNAL LOAD WORK (SLINGING SHAKE BOLTS) IN SNOWING CONDITIONS. THE AIRCRAFT DROPPED VERTICALLY APPROX. 130' CRASHING ONTO A STUMP IN THE CLEAR CUT AREA THE AIRCRAFT WAS WORKING. THE AIRCRAFT RECEIVED SUBSTANTIAL DAMAGE, THE PILOT WAS SERIOUSLY INJURED. AFTER THE ACCIDENT THE PILOT STATED, WHILE MANEUVERING THE AIRCRAFT HE SAW A LARGE AMOUNT OF SNOW AND ICE SLIDE FROM THE FRONT OF THE CANOPY BACK INTO THE AIR INLET AREA AND THE ENGINE FLAMED OUT. DURING THE ON SITE ACCIDENT INVESTIGATION INSPECTORS FROM THIS OFFICE RECORDED THE POSITION OF THE ENGINE ANTI-ICE LEVER IN THE OFF POSITION. PHONE CONVERSATION WITH THE PILOT AND THIS OFFICE ON 01/10/2007, THE PILOT STATED HE HAD THE ENGINE ANTI-ICE WAS ON, APPROX. 25 GALS. OF FUEL, AND FLOWN APPROX. 5 TO 8 MINUTES ON THE FUEL LOAD BEFORE THE ACCIDENT. AIRCRAFT FLIGHT MANUAL LIMITATIONS PERMITS FLIGHT OPERATIONS IN FALLING AND OR BLOWING SNOW WHEN THE AUTO REIGNITION AND ENGINE EPO IS INSTALLED AND WORKING. N1088G WAS IN COMPLIANCE WITH THIS LIMITATION.

NTSB investigation

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