SEA06GA158

NTSB accident investigation · Eurocopter AS-350-B3 · Yellow Pine, ID · August 13, 2006

Accident · FatalFinal report
Date
August 13, 2006, 17:10 local (23:10 UTC)
Place
Yellow Pine, ID
Injuries
4 fatal
Damage
Destroyed
Phase of flight
Maneuvering
Aircraft
N355EVEurocopter AS-350-B3
Weather
Visual (VMC) · Day
Status
Completed · report May 29, 2007
Report
Approved by Office Director
Parties
U.S. Forest Service, American Eurocopter, Turbomeca, National Transportation Safety Board, Evergreen Helicopters, FAA, AAI-100
FAA report
20060813015989A
Case key
64316

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

On this page

Probable cause

The NTSB’s determination of the probable cause, and any contributing factors.

The pilot's intentional low altitude flight and his failure to maintain an adequate altitude to clear the trees.

Analysis

The helicopter collided with a tree as it flew over a mountain ridgeline. The helicopter was under contract to the U.S. Forest Service and was assigned to Krassel Helibase (24K), Idaho. The pilot was requested to fly a relief Fire Lookout to a lookout tower on Williams Peak, which was 4 nautical miles (nm) and a 2,844 feet elevation gain away. There were several forest fires in the area and visibility in the lower valley was approximately 1 nm. The relief Fire Lookout, who was dropped off, said that as the helicopter flew up the ridge, visibility got much better. He said that there were two forest service personnel on board, to assist in off-loading and on-loading equipment, supplies, and refuse from the two open-top external cargo baskets that were secured to the helicopter's skid gear. Cargo was secured in the cargo baskets by multiple bungee cords. The return flight would have been flown directly into the late afternoon sun. There were no witnesses to the accident. Thirteen cubitainers (5 gallon plastic containers for potable water), two large plastic refuse bags, yellow crepe paper and several chips of green helicopter paint were found near a freshly downed and up rooted snag (a dead, defoliated conifer) located on the ridgetop. The snag was estimated to have been 90 feet tall. Further down the mountain side was a tail rotor paddle which had separated at its cuff. The burned out wreckage of the helicopter was found on a forest service road, approximately 2,000 feet down the mountain and 1,230 foot elevation loss from the initial downed snag. Postaccident examination of the engine revealed that the power turbine's blades were sheared from their disc, which indicated an over speed event. This would occur with a main rotor blade strike/sudden-stoppage event, and the subsequent compromised engine to main rotor power train. Additionally, 11 of the containers that had been in one cargo basket had 3 to 9 inch slashes in them from the tail rotor. Interviews were conducted by U.S. Forest Service personnel with four Helitack crew members who were assigned to the helicopter. They said the pilot did like to do "showy" flying at times, but would always ask the passengers if they were comfortable. He would "buzz" a ridge every now and then, and perform a maneuver he called the "sleigh ride." One of the Helitack crew members said that a "sleigh ride was where you top a ridge then drop the collective, drop the nose a bit....it was a common maneuver for him." No preimpact engine or airframe anomalies, which might have affected the helicopter’s performance, were identified.

Factual narrative

The factual narrative1,284 words

History of flight

On August 13, 2006, at approximately 1710 mountain daylight time, a Eurocopter AS-350-B3 helicopter, N355EV, was destroyed by fire following impact with the East Fork Road (US Forest Road 48) about 18 miles west of Yellow Pine, Idaho. The commercial pilot and his three passengers were fatally injured. The helicopter was being operated under contract to the United States Forest Service by Evergreen Helicopters, Inc. of McMinnville, Oregon, as a public use flight. Visual meteorological conditions prevailed for the cross-country flight that had originated approximately 5 minutes before the accident. A company flight plan had been filed. The helicopter was en route from Williams Peak (elevation 6,826 feet) lookout tower to Krassel Helibase (24K; elevation 3,982 feet) when the accident occurred.

At 1656, the flight-tracking log for the helicopter indicated that it departed Krassel Helibase to transport a relief Fire Lookout to Williams Peak lookout tower and return. The relief Fire Lookout reported that the flight (approximately 4 nautical miles [nm] and 2,844 feet elevation gain) was "very normal and smooth." He said that forest fire smoke limited the visibility in the lower valley to approximately 1 mile, but as the helicopter flew up the ridge, visibility got much better. The relief Fire Lookout said that the pilot flew up the mountain by following the terrain with 100 to 200 feet of clearance. He said that there were two forest service personnel on board, to assist in off-loading and on-loading equipment, supplies, and refuse from the external cargo baskets, to minimize the aircraft's time at Williams Peak. He said the helicopter departed between 1705 and 1710, with the Fire Lookout person who was going off duty and the two other employees.

There were no witnesses to the accident. A U.S. Forest Service employee discovered the accident at approximately 1730. The aircraft was consumed by postimpact fire.

Personnel information

The pilot's most recent Federal Aviation Administration flight medical exam (second class) was taken on July 1, 2006. The pilot's flight logbook, as of December 2005, and his employer's payroll records indicated that he had 4,386 hours of flight time. The pilot's employer stated that he had completed his last flight review on February 13, 2006. The mission log-sheets, at Krassel Airfield, documented that the pilot had been off duty on August 8 thru 10. On August 11 and 12, he flew 6.6 hours, and on the day of the accident he had flown 3.1 hours. The pilot was in his second year of flying under the Krassel Rappel contract.

During interviews conducted by U.S. Forest Service personnel, four Helitack crew members, who were assigned to the helicopter, said the pilot was very skillful. One crew member described the pilot as "a perfectionist--in everything about his flying--all had to be perfect." They said he did like "showy" flying at times, but would always ask the passengers if they were comfortable. He would "buzz" a ridge every now and then, and perform a maneuver he called the "sleigh ride." One of the Helitack crew members said that a "sleigh ride was where you top a ridge then drop the collective, drop the nose a bit....it was a common maneuver for him."

Aircraft information

The helicopter was a single engine, six seat aircraft, which was manufactured by Eurocopter in May 2002. It was powered by a Turbomeca Arriel 2B turboshaft engine, which was rated at 825 horsepower at sea level. Maintenance logbooks indicated that the airframe had 1,384 hours, and the engine had 1,260 hours. The helicopter was equipped with two open-top external cargo baskets whose framework was tubular steel which was covered with expanded steel mesh. They were 52 inches long, 12 inches wide, and 7 inches high, and were secured to the helicopter's skid gear. Cargo was secured inside these baskets by multiple bungee cords.

Meteorological information

At 1650, the weather conditions at McCall Municipal Airport (elevation 5,021 feet), McCall, Idaho, located 225 degrees magnetic and 18 nautical miles from the accident site, were: wind variable at 5 knots; visibility 10 statue miles; clear of clouds; temperature 73 degrees Fahrenheit; dew point 36 degrees Fahrenheit; altimeter setting 30.10 inches Hg.

At 1710, the sun was at 250.7 degrees magnetic, and 38 degrees above the horizon. Several forest service personnel at Krassel Helibase said that the pilot would commonly navigate by following the mountain ridges. The ridge line from Williams Peak lookout tower to the accident site was a westerly heading (250 degrees) with a left dogleg turn (220 degrees) at the half way point.

Wreckage and impact information

The main wreckage was found on Forest Service Road 48 (N45:00:32; W115:42:45; elevation 3,719 feet), also known as East Fork Road. This was in the Payette National Forest, approximately 2,100 feet east of the confluence of the East Fork of the South Fork of the Salmon River and the South Fork of the Salmon River. The surrounding terrain was comprised of steep, rugged mountains, with narrow valleys and sharp ridges. The mountain sides were predominately granite detritus with scattered rocky outcrops. The vegetation consisted of dispersed conifers and native grasses. A ground scar on a 180 degree magnetic orientation terminated at the main wreckage. Additional wreckage was distributed up the mountain side for approximately 2,000 feet (with a 1,230 foot elevation gain) on a north, by north-east heading from the accident site. All of the helicopter's significant components were accounted for.

At the highest point on the mountain, where the initial debris was found (hence, initial-debris-point, or IDP), there was an uprooted, downed snag (a dead, defoliated conifer). An accompanying forester estimated that it had been 90 feet tall. It was broken into several segments, and was oriented approximately 220 degrees magnetic. Several bits/scraps of paper, some with writing/notes on them, were found within 30 feet of the downed snag. Next down the mountain, from approximately 100 to 600 feet below the IDP, were found thirteen cubitainers (5 gallon plastic containers for potable water), and several cubitainer caps and handles. There were two large plastic refuse bags, yellow crepe paper, and a plastic bread sack. The two large plastic bags were torn, and eleven of the cubitainers had 3 to 9 inch slashes in them. One cubitainer had a chip of blue paint in it, which was consistent with the tail rotor paddle paint. Several green and white paint chips, consisting of aircraft primer overlaid with paint, were found in the same general area.

Approximately 550 feet down from the IDP was another large snag with its top broken off in a 220 degree orientation. Down hill from this was a live conifer with a fresh broken limb. West, for approximately 200 feet and down slope for approximately 200 feet, from these two damaged trees, was found a tail rotor paddle which had separated at its cuff. Further down slope, approximately 1,450 feet down from the IDP and aligned with the two damaged trees, was found the tail rotor gearbox cover which exhibited evidence of tail rotor drive shaft flailing. Approximately 80 to 90 feet further down the mountain was the upper WSPS (wire strike protection system) guide, and approximately 60 feet below that was the tail-cone with its vertical and dorsal fins. Approximately 400 feet (200 foot elevation loss) further down the mountain was the main wreckage on the road. On the edge of the road was a tree, approximately 4 inches in diameter, whose top had been severed.

The first piece of debris on the road was an external-load viewing mirror, which had been mounted under the pilot's feet on the right side of the helicopter. Approximately 25 feet further, were the two cargo baskets side-by-side. One basket had burned refuse in it;

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

In flight collision with objectManeuvering
Terrain condition - mountainous/hilly
Object - tree(s)
Low altitude flight/maneuver - intentionalPilot in commandCause
Altitude/clearance - not maintainedPilot in commandCause
Terrain condition - roadway/highway
In flight collision with terrain/waterDescent - uncontrolled

Aircraft

Registration
N355EV
Reported as
Eurocopter AS-350-B3
Category
Helicopter
Serial number
3550
Airframe hours
1,387
Engine
Turbomeca Arriel 2B, 825 horsepower, turbo shaft
Damage
Destroyed
Fire
On-Ground
Flight
Public aircraft · Public use
Operator
Evergreen Helicopters
Registered owner
Ventures Acquisition Company LLC
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · July 1, 2006
Departed
NONE · Williams Peak, ID
Destination
24K · Krassel USFS, ID
Flight plan
Company VFR

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
42
Injuries
Fatal
Certificates
Flight instructor, Commercial, Private
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Without waivers/limitations
Last flight review
February 1, 2006
Seat
Right
Toxicology
Performed
Flight hours
4,386 total · 1,640 in this make and model · 2,824 as pilot in command · 88 in the last 30 days · 3 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
Variable at 5 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
73 °F, dew point 36 °F
Altimeter
30.10 inHg
Observed at
MYL, 18 nm away

Docket · 54

The files NTSB released with the investigation on March 28, 2007, on NTSB’s docket system: statements, records, photos and specialists’ reports. 37.9 MB in all.

Pilot/Operator Aircraft Accident Report, NTSB Form 6120.1Item 1 · .PDF · 478 KBAdditional StatementsItem 2 · .PDF · 308 KBMaps and Wreckage DistributionItem 3 · .PDF · 1.8 MBEngine DrawingsItem 4 · .PDF · 374 KBReports from Parties to the InvestigationItem 5 · .PDF · 224 KBOther Pertinent FormsItem 6 · .PDF · 412 KBToxicological ReportItem 7 · .PDF · 60 KBStatement of Party Representatives to NTSB InvestigationItem 8 · .PDF · 172 KBRelease of Aircraft Wreckage, NTSB Form 6120.15Item 9 · .PDF · 42 KBImage 1. Fallen snag uprooted.Item 10 · .PDF · 1.1 MBImage 2. Main trunk of fallen snag.Item 11 · .PDF · 1.1 MBImage 3. Top of fallen snag.Item 12 · .PDF · 879 KBImage 4. Debris found on the mountain side.Item 13 · .PDF · 1.6 MBImage 5. Debris found on the mountain side.Item 14 · .PDF · 1.6 MBImage 6. Debris, cubies, and tailrotor paddle.Item 15 · .PDF · 1.8 MBImage 7. Paint chip from tailrotor in a cubie.Item 16 · .PDF · 1.3 MBImage 8. Separated tail rotor on the mountain.Item 17 · .PDF · 319 KBImage 9. Tailrotor paddle with two cubies.Item 18 · .PDF · 292 KBImage 10. Aerial view of two damaged trees to accident site.Item 19 · .PDF · 1 photo · 101 KBImage 11. Tailrotor gear box found on mountain side.Item 20 · .PDF · 317 KBImage 12. Wire strike protection system guide found on the mountain side.Item 21 · .PDF · 271 KBImage 13. Tailcone found on the side of the mountain.Item 22 · .PDF · 315 KBImage 14. Tailcone found on the side of the mountain.Item 23 · .PDF · 315 KBImage 15. Overview of main accident site.Item 24 · .PDF · 2.3 MBImage 16. Severed tree top next to the road.Item 25 · .PDF · 3.2 MBImage 17. Skid tube impact damage.Item 26 · .PDF · 413 KBImage 18. Accident scene looking east.Item 27 · .PDF · 295 KBImage 19. Left side basket with burned cargo.Item 28 · .PDF · 277 KBImage 20. Crushed right side basket, fuselage is to the right.Item 29 · .PDF · 1.2 MBImage 21. Aft end of right side basket.Item 30 · .PDF · 1.2 MBImage 22. Accident scene looking west, northwest.Item 31 · .PDF · 1.1 MBImage 23. Looking from main fuselage to transmission.Item 32 · .PDF · 318 KBImage 24. Main transmission with rotorhead.Item 33 · .PDF · 318 KBImage 25. Starflex rotor hub with the engine behind it.Item 34 · .PDF · 311 KBImage 26. Engine upright, oriented about 220 degrees.Item 35 · .PDF · 155 KBImage 27. Engine with transmission.Item 36 · .PDF · 297 KBImage 28. Left side of engine, note departure hole in exhaust duct.Item 37 · .PDF · 159 KBImage 29. Right side of engine.Item 38 · .PDF · 161 KBImage 30. Right side of tail boom inverted, note the engine.Item 39 · .PDF · 310 KBImage 31. Tail boom, note damaged right stabilizer.Item 40 · .PDF · 1.1 MBImage 32. Tail boom with gear box and tail rotor paddle in background.Item 41 · .PDF · 3.5 MBImage 33. Tail rotor gear box with one tail rotor paddle I.Item 42 · .PDF · 320 KBImage 34. Vertical speed indicator.Item 43 · .PDF · 1.1 MBImage 35. Transmission shaft in situ.Item 44 · .PDF · 94 KBImage 36. Transmission shaft, aft.Item 45 · .PDF · 700 KBImage 37. Transmission shaft, front.Item 46 · .PDF · 771 KBImage 38. Engine just before teardown at Grand Prairie.Item 47 · .PDF · 461 KBImage 39. The engine just before teardown.Item 48 · .PDF · 393 KBImage 40. Centrifugal turbine shroud.Item 49 · .PDF · 423 KBImage 41. Free turbine nozzle guide.Item 50 · .PDF · 429 KBImage 42. Power turbine, note all the blades have separated.Item 51 · .PDF · 407 KBImage 43. Power turbine.Item 52 · .PDF · 190 KBImage 44. Power turbine casing.Item 53 · .PDF · 397 KBImage 45. Power turbine casing.Item 54 · .PDF · 413 KB

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.