N5793P

Substantial
Fatal

AEROSPATIALE AS350BAS/N: 1476

Accident Details

Date
Saturday, November 14, 2009
NTSB Number
WPR10FA055
Location
Doyle, CA
Event ID
20091114X82100
Coordinates
39.851387, -120.349998
Aircraft Damage
Substantial
Highest Injury
Fatal
Fatalities
3
Serious Injuries
0
Minor Injuries
0
Uninjured
0
Total Aboard
3

Probable Cause and Findings

The pilot became spatially disoriented while maneuvering on a dark night, which resulted in a loss of helicopter control.

Aircraft Information

Registration
N5793P
Make
AEROSPATIALE
Serial Number
1476
Engine Type
Turbo-shaft
Year Built
1982
Model / ICAO
AS350BAAS50
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
MOUNTAIN LIFEFLIGHT
Address
471-920 JOHNSTONVILLE RD
HANGAR 4 SUSANVILLE AIRPORT
Status
Deregistered
City
SUSANVILLE
State / Zip Code
CA 96130
Country
United States

Analysis

HISTORY OF FLIGHT

On November 14, 2009, about 0201 Pacific standard time, an Aerospatiale AS350BA, N5793P, collided with terrain near Doyle, California. Mountain Lifeflight was operating the helicopter under the provisions of 14 Code of Federal Regulations (CFR) Part 91. The commercial pilot and two passengers sustained fatal injuries; the helicopter was substantially damaged by impact forces and post-crash fire. The cross-country positioning flight departed Reno, Nevada, about 0143 with a planned destination of Susanville, California. Visual meteorological conditions prevailed, and a company flight plan had been filed.

The helicopter departed its home base at Susanville Airport at 0016, and picked up a patient at Banner Hospital in Susanville. It departed Susanville at 0038, and arrived at Renown Hospital in Reno at 0111. It departed Renown Hospital at 0143, and the medical crew made position reports every 10 minutes to its dispatch center in Susanville. At 0153, they reported Hallelujah Junction; Susanville was 43 miles at 311 degrees, and the accident site was 5 miles at 341 degrees. At 0201, dispatch received a transmission that the helicopter was going down.

Law enforcement personnel interviewed a witness who was in a car on nearby Highway 395. The witness observed the helicopter flying straight and level; it then descended vertically at a rapid rate. The witness lost sight of it behind terrain, and then observed a fireball. The witness drove on a dirt road, and found the wreckage, which was approximately 1/4 mile west of Highway 395.

The company reported that the pilot departed at 1955 on the same round trip (base to Banner Hospital to Reno and return), but with a different medical crew on board. Both crewmen stated that the pilots typically flew about 8,500 feet msl, which was above the mountain tops along their route of flight. The pilots typically followed Highway 395 in order to maintain the best visual contact with the ground.

The National Transportation Safety Board (NTSB) investigator-in-charge (IIC) reviewed recorded radar data. The helicopter was using a discreet code of 0465. A plot of the radar track is part of the public docket. The first target appeared at 0144:16, at a Mode C reported altitude of 4,700 feet mean sea level (msl); it was at the approximate coordinates for Renown Hospital, which was at an estimated elevation of 4,500 feet. It climbed on a northwesterly course for about 5 miles, and then turned about 15° left for 4 miles until the target was lost at 0150:08. At this point, it was about halfway between Highway 395 and Reno Stead Airport, and indicating a Mode C altitude of 7,100 feet.

The target was reacquired at 0200:19, at a Mode C altitude of 9,200 feet in the vicinity of the accident site. The target tracked to the northeast for about 0.6 mile, and climbed to 9,700 feet by 0200:43. The next target, which occurred 10 seconds later, was back to the southwest at an altitude of 9,800 feet. At 0201:06, the target was west of the previous location at a Mode C altitude of 10,100 feet; a target 5 seconds later was essentially in the same location at 10,200 feet. The next target was less than 5 seconds later and northeast of the previous two targets. About 10 seconds later, the next target continued to the northeast. The last two targets occurred 4.5 seconds apart; they were at 10,200 feet, and collocated about 90° east of the previous target. This location was within the immediate vicinity of the accident site.

PERSONNEL INFORMATION

The operator reported that the 39-year-old pilot held a commercial pilot certificate with ratings for rotorcraft-helicopter and instrument helicopter. The pilot held a certified flight instructor (CFI) certificate with a rating for rotorcraft-helicopter.

The pilot held a second-class medical certificate issued on May 20, 2009. It had no limitations or waivers.

The operator reported that the pilot had a total flight time of 6,055 hours. He logged 49 hours in the last 90 days, and 10 in the last 30 days. He had 4,815 hours in this make and model. He completed a flight review on August 3, 2009. The pilot accumulated 53 hours with this company and 46 hours of this mission type. He had a total of 248 hours of flight experience in night conditions with 15 hours of night time logged in the 8 months prior to the accident.

The pilot indicated on his resume that he worked as a tour pilot in Hawaii the previous 6 years. He had flown as a tour, charter, external load, and EMS pilot in Alaska the 6 months prior to Hawaii. The pilot information/experience form that the pilot filled out for Mountain Lifeflight indicated that as of July 24, 2009, he had a total time of 6,003 hours with 233 hours at night. His resume indicated that he had 53 hours of instrument time. His date of assignment as a pilot with Mountain Lifeflight was August 3, 2009. He lived in Hawaii, and would live at the base when on shift. He arrived at the base a couple of days before the accident flight to begin a week of night shifts from 1900-0700. The accident occurred on the second night of his shift.

The pilot reported for duty at 1900, and flew the same mission as the accident fight with two different crew members. That flight began at 1955. Both crew members reported that the pilot was in good spirits, and appeared to be rested.

AIRCRAFT INFORMATION

The helicopter was originally manufactured by Aerospatiale in 1982 as an AS350D, serial number 1476. The helicopter’s logbooks revealed that it was converted to AS350BA. On July 18, 2008, the operator replaced the type-certificated Turbomeca Arriel 1B engine with a Honeywell LTS-101-600A-3A engine under a Soloy LLC Supplemental Type Certificate (STC) # SR00805SE. The helicopter had accrued a total airframe time of 5,827 hours at the last 250-hour inspection on October 8, 2009. The logbooks contained an entry for an annual inspection dated January 29, 2009, at an airframe total time of 5,432 hours.

The engine was a Honeywell LTS101-600A-3A, serial number LE-46096CE. Total time recorded on the engine was 7,020 hours, and time since major overhaul was 751 hours.

Operator personnel stated that the helicopter stands by with a 60% fuel load, and that was how it was configured for the accident flight.

Two crew members flew on a flight earlier in the evening with the accident pilot. Both stated that the flight was uneventful from startup to shut down with no strange sounds or vibrations noted during the flight. The entire crew had commented on how good the helicopter was operating.

METEOROLOGICAL INFORMATION

An NTSB meteorologist provided a weather brief.

The closest official weather observation station was Reno (KRNO), which was 25 nautical miles (nm) at 150° from the accident site at an elevation of 4,415 feet mean sea level (msl). An aviation routine weather report (METAR) was issued at 0155 PST. It stated: wind from 340° at 6 knots; visibility 10 miles; skies 5,500 feet broken; temperature 4/39° Celsius(C)/Fahrenheit(F); dew point -3/25°C/F; altimeter 29.96 inches of mercury.

Doppler weather radar gave no indication of precipitation in the area. No PIREPs were available near the time of accident.

METARs from KRNO and Truckee, California (KTRK), (33 NM south at an elevation of 5,900 feet) indicated the presence of clouds in the area. KRNO and KTRK reported cloud bases as broken at 5,500 feet above ground level (agl or approximately 9,900 feet msl) and 3,200 feet agl (approximately 9,100 feet msl), respectively. Visibility was at or greater than 10 statute miles.

GOES11 and MODIS infrared imagery confirmed clouds in the area at the time of the accident. Brightness temperatures in the MODIS infrared imagery for clouds in the area were -12°C, which corresponded to cloud tops reaching about 13,000 feet msl.

A rawinsonde launch from KRNO at 1200 universal coordinated time, as well as meteorological model data, indicated light clear icing at the upset altitude, with potential for moderate clear icing in/near clouds.

For the California forecasting region, there was no active AIRMET SIERRA, TANGO or ZULU for the accident location/time. However, there was an active AIRMET ZULU for ice between 4,000 feet and 12,000 feet msl near the accident site.

For the Nevada forecasting region, there was an active AIRMET TANGO for moderate turbulence at flight levels 180-390. This forecast extended into California, but there were no other active AIRMETS for the accident time and location.

Two crew members flew on a flight earlier in the evening with the accident pilot. One stated that he didn’t observe clouds on their flight; if there were any, he said that they were above them and very few. He was able to distinguish the mountains along the route. The other noted that there was very little moon, and it was a very dark night.

WRECKAGE AND IMPACT INFORMATION

Investigators examined the wreckage at the accident scene. Detailed on site notes are in the public docket. The first identified point of contact (FIPC) consisted of three parallel ground scars. The center scar contained the recognition light fixture. All references in the following paragraphs reflect left and right of the debris path centerline and distance from the FIPC.

The debris path was 305 feet along a magnetic heading of 230 degrees; the first half of the path was on a 20-degree downslope of uneven terrain.

The vertical stabilizers separated as a unit, and were at 29 feet. Landing gear pieces were about 15 feet to the right of them.

The tailboom with tail rotor attached separated aft of the cabin, and came to rest on its right side at 58 feet. The left side of the tailboom was crushed in and aft with wrinkles; it sustained more damage than the right side. Scrape marks from the front to the rear on the left side were parallel to the longitudinal axis, and were visible within the folds of the wrinkles. The right horizontal stabilizer sustained less damage than the left horizontal sta...

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR10FA055