N91099

HISTORY OF FLIGHT

On August 13, 2011, about 1940 Alaska daylight time (ADT), a Cessna 207 airplane, N91099, impacted mountainous, brush-covered terrain, about 37 miles west of McGrath, Alaska. Of the six people aboard, the pilot and one passenger died at the scene, and four passengers received serious injuries. The airplane sustained substantial damage. The flight was operated by Inland Aviation Services, Inc., Aniak, Alaska, as a 14 CFR Part 135 visual flight rules (VFR) on-demand charter flight when the accident occurred. Visual meteorological conditions prevailed at the airplane's point of departure, and instrument meteorological conditions were reported along the airplane's flight route. The flight originated at the McGrath Airport, about 1915, and was en route to the Anvik Airport, Anvik, Alaska, before continuing on to Aniak, the airplane's home base. VFR company flight following procedures were in effect, but there is no record that a weather briefing was obtained before departure.

During a hospital room interview with the National Transportation Safety Board (NTSB) investigator-in-charge (IIC), on August 16, a passenger related that the purpose of the flight was to transport a group of school teachers to Anvik before the start of the school year. His wife and two children were also aboard the accident airplane.

The passenger stated that he was seated in the front, right seat, next to the pilot. He said that about 20 minutes after leaving McGrath, as the flight progressed into mountainous terrain, low clouds, rain and fog restricted visibility. At one point the pilot told the passenger, in part: "This is getting pretty bad." The passenger said that the pilot then descended and flew the airplane very close to the ground, then climbed the airplane, and then it descended again. Moments later the passenger said that the airplane entered "whiteout conditions." The next thing the passenger recalled was looking out the front windscreen, and just before impact, seeing the mountainside suddenly appear out of the fog. He said that all of the survivors lost consciousness during the impact, and he was the first to regain consciousness.

The passenger noted that while boarding the airplane in McGrath, he happened to notice a SPOT satellite personal tracker that was clipped to the pilot's sun visor. He said that after the accident, he was able to find the SPOT device in the wreckage, and began pushing the emergency SOS button.

According to the operator, the pilot routinely carried his own SPOT satellite personal tracker. About 2030, family members in Wasilla, Alaska, the pilot's hometown, received an emergency SOS message from the pilot's SPOT device. A family member then immediately called the operator in Aniak to alert them of the distress message.

When the airplane failed to arrive in Aniak by 2045, company personnel initiated a phone and radio search to see if the airplane had diverted to another village. Unable to locate the airplane, company personnel initiated an aerial search along the pilot's anticipated route, but poor weather and dark night conditions prohibited a search of the entire flight route.

The Federal Aviation Administration (FAA) issued an alert notice (ALNOT) at 2200 Alaska daylight time.

PERSONNEL INFORMATION

The pilot, age 66, held a commercial pilot certificate with airplane single-engine land, multiengine land, single-engine sea, and instrument airplane ratings. In addition, he held a commercial rotorcraft helicopter certificate. The most recent second-class medical certificate was issued to the pilot on December 23, 2009, which contained no limitations.

In the Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1) submitted by Inland Aviation, the pilot's total aeronautical experience was listed as 25,000 flight hours, with 10,000 flight hours in the accident airplane make and model. The report noted that in the preceding 90 and 30 days prior to the accident, the pilot accrued a total of 60 flight hours and 30 flight hours.

During an interview with the NTSB IIC on August 24, Inland Aviation Service's president said that the accident pilot was initially hired on August 10, 2009, and he continued to fly for the company on a seasonal and as needed basis. He added that the accident pilot had operated his own air taxi business, Grayling Air Service, from 1974 to 1978, operating in the same geographic areas as Inland Aviation.

A review of company training records revealed that the pilot completed his initial ground and flight training on August 9, 2009. Additionally, the pilot received ground training in the use and operation of the automatic dependent surveillance-broadcast (ADS-B) / Capstone equipment installed in the accident airplane.

The pilot's most recent FAA Part 135.293 and 135.299 check ride was on August 5, 2010. Inland Aviation's president/director of operations, the FAA approved company check airman, administered the check ride. In the remarks section of FAA form 8410-3 it states, in part: "Demonstrated Instrument Competency."

Once the pilot completed the company's training program and passed a check ride, he was officially hired, then assigned to fly Cessna 207 airplanes from the company base in Aniak.

The pilot's normally scheduled duty day was from 0800 to 2200. In the three days prior to the accident, the pilot was off duty on August 11. On August 12, his duty day started at 0800, and he flew only .3 hours. On the accident date of August 13, the company president estimated that the accident pilot flew about 2.2 hours.

AIRCRAFT INFORMATION

According to the Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1) submitted by the operator, the airplane had a total time in service of 31,617.7 flight hours. The last recorded inspection of the engine and airframe was a 100-hour inspection, on July 18, 2011, about 20 flight hours before the accident.

METEOROLOGICAL INFORMATION

The closest weather reporting facility was the Tatalina Airport, 28 miles east-southeast of the accident site. At 1955, a weather observation from the Tatalina Airport was reporting, in part: Wind, 280 degrees at 5 knots; visibility, 3 statute miles; clouds and sky condition, 1,600 broken, 2,400 broken, 3,100 feet overcast; temperature, 54 degrees F; dew point, 52 degrees F; altimeter, 29.89 inches Hg.

The next closest official weather observation station was the McGrath Airport, the accident airplane's departure point, 37 miles south-southeast of the accident site. At 1953, an Aviation Routine Weather Report (METAR) was reporting, in part: Wind, 310 degrees at 7 knots; visibility, 10 statute miles; clouds and sky condition, 2000 feet few, 3,600 feet overcast; temperature, 57 degrees F; dew point, 52 degrees F; altimeter, 29.88 inHg.

An NTSB meteorologist did a comprehensive study of the weather conditions around the accident site, revealing two strong low pressure systems stretching west-northwest from the central Yukon to northwest Alaska. The study disclosed that the forecast for the area included increasing instabilities over the region that were expected to produce rain showers, fog, and reduced visibility.

Additionally, the NTSB meteorologist reviewed archived satellite imagery, captured about the time of the accident, which revealed evidence of low clouds, light rain, drizzle, fog, and instrument meteorological conditions (IMC) in the area around the accident site.

A copy of the meteorologist's report is included in the public docket of this accident.

WRECKAGE AND IMPACT INFORMATION

On August 14, the NTSB IIC, along with two Alaska State Troopers, and a Federal Aviation Administration (FAA) aviation safety inspector from the Anchorage Flight Standards District Office (FSDO), Anchorage, examined the wreckage at the accident site, and no mechanical problems were found.

All of the airplane's major components were found at the main wreckage site. The accident site was in an area of steep, mountainous, tundra and rock-covered terrain, with sparsely populated areas of low trees/scrubs, at an elevation of about 1,720 feet msl.

The main debris path was on a 260 degree heading, and uphill (All headings/bearings noted in this report are magnetic). An area believed to be the initial impact point, about 50 feet below the main wreckage site, was marked by broken shrubs and disrupted tundra.

Scattered upslope, in a line between the initial impact point and the final resting point of the main wreckage, were portions of wreckage debris, landing gear components, broken Plexiglas, aircraft seats, and personal effects.

The airplane's wings remained attached to the fuselage attaching points, but both had extensive spanwise leading edge aft crushing. The wing's flight control surfaces remained connected to their respective attach points.

The airplane's empennage was severed just forward of the stabilizer attach point, but all of the flight control surfaces and control cables remained connected to their respective attach points.

The fuselage and cabin area was crushed inward. The airplane's belly, interior floorboards, and seat track rails, between the two front seats, extending aft to the third row seats, was torn aft, which exposed the occupants to terrain and broken trees.

The engine remained attached to the fuselage, but it was displaced about 30 degrees to the right.

The propeller and hub remained attached to the engine crankshaft. All three propeller blades were loose in the propeller hub, but remained attached to the hub assembly. All three of the propeller blades had multiple leading edge gouges, substantial torsional "S" twisting, and chordwise scratching.

Due to impact damage, the flight controls could not be moved by their respective controls, but continuity of the flight control cables was established to the cockpit area.

MEDICAL AND PATHOLOGICAL INFORMATION

A postmortem examination was conducted under the authority of the Alaska ...