N272EF

Destroyed
Fatal

CESSNA T210KS/N: 21059302

Accident Details

Date
Monday, January 2, 2017
NTSB Number
WPR17FA045
Location
Payson, AZ
Event ID
20170103X14851
Coordinates
34.429721, -111.277778
Aircraft Damage
Destroyed
Highest Injury
Fatal
Fatalities
4
Serious Injuries
0
Minor Injuries
0
Uninjured
0
Total Aboard
4

Probable Cause and Findings

The non-instrument-rated pilot's improper decisions to begin and to continue a flight under visual flight rules into instrument meteorological conditions, which resulted in controlled flight into terrain.

Aircraft Information

Registration
N272EF
Make
CESSNA
Serial Number
21059302
Engine Type
Reciprocating
Year Built
1970
Model / ICAO
T210KC210
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
N9402M AVIATION LLC
Address
20860 N TATUM BLVD STE 240
Status
Deregistered
City
PHOENIX
State / Zip Code
AZ 85050-4280
Country
United States

Analysis

HISTORY OF FLIGHTOn January 2, 2017, about 0937 mountain standard time, a Cessna T210K, N272EF, was destroyed when it collided with mountainous terrain near Payson, Arizona. The private pilot and three passengers were fatally injured. The airplane was registered to N9402M Aviation, LLC, of Phoenix, Arizona. The personal flight was operated by the pilot under the provisions of 14 Code of Federal Regulations Part 91. Instrument meteorological conditions (IMC) prevailed, and no flight plan was filed for the visual flight rules (VFR) cross-country flight that departed Scottsdale Airport (SDL), Scottsdale, Arizona, at 0912 and was destined for Telluride, Colorado.

According to the co-owner of the airplane, the pilot planned to fly from SDL, where the airplane was based, to Colorado with his family for their annual vacation.

The Federal Aviation Administration (FAA) provided a radar track for an airplane with a 1200 transponder code that corresponded with the airplane's departure time and route. The radar data indicated that the airplane departed SDL at 0912 and proceeded north. The final radar target was at 0937:39, at a Mode C altitude of 6,700 ft mean sea level (msl), and about 0.07 nautical miles (nm) east of the accident site. According to the FAA, the pilot did not receive VFR flight following services or contact any of the low altitude sectors along his route of flight.

An Electronics International MVP-50P electronic display device was recovered from the wreckage and forwarded to the National Transportation Safety Board (NTSB) Vehicle Recorders Laboratory for data recovery. The small battery used to power the unit's internal clock had become dislodged, and the unit reverted to an unset time setting. As a result, the flight and engine data time stamps in this report differ by about 20-minutes from the actual time derived from the FAA radar data.

Engine data retrieved from the MVP-50P indicated that the fuel flow, manifold pressure, and rpm increased at 09:33:05, consistent with departure performance. GPS and flight data retrieved from the unit showed the airplane's groundspeed rise from 0 knots and its altitude increase from 1,437 ft, which is about SDL's field elevation, consistent with a departure. The airplane then climbed to the northeast before turning left to a north heading for the remainder of the flight. The engine parameters did not indicate any anomalies during the flight. At 0943:59, the airplane reached a peak altitude of 8,029 ft and subsequently descended to about 7,850 ft. The airplane maintained this altitude within 30 ft for about 2 minutes and then climbed to 7,936 ft briefly before entering a descent and reaching about 6,651 ft at 0947:44. In the next minute, the airplane climbed to about 6,900 ft and then, at 0950:28, descended to and maintained about 6,200 ft, within 100 ft, for about 2 minutes 30 seconds. The last recorded data occurred while the airplane was in a 10-second climb at 0953:06, a GPS altitude of 6,767 ft, and about 0.22 nm from the accident site. In the airplane's final 12 seconds of flight, fuel flow decreased from about 20 to 17.4 gallons per hour, manifold pressure decreased from about 31 to 28 inches of mercury, and rpm remained unchanged.

Track data from the GPS showed that the airplane maintained a straight course after its departure all the way to the accident site located at the mountain rim, which had a published peak elevation that varied between 6,750 feet msl and 8,077 feet msl.

Family members became concerned on the afternoon of January 2 as they had not heard from the flight and were unable to reach the occupants on their cell phones. Around 2100, they notified local law enforcement who traced the flight's location using the pilot's and his wife's cell phones. An alert notice, or ALNOT, was issued at 2252 by Denver Center, and the wreckage was subsequently discovered the following morning at 0427 in a wooded area on the rising face of the Mogollon Rim, a cliff that extends across northern Arizona. PERSONNEL INFORMATIONThe pilot held a private pilot certificate with an airplane single-engine land rating. He did not hold an instrument rating. The pilot's most recent third-class medical certificate was issued on April 10, 2015, with no limitations. At the time of the exam, the pilot reported that he had accumulated 295 total flight hours of which 14 hours were in the previous 6 months.

The last recorded flight in the pilot's logbook was dated August 28 with the remark "Flight Review," but the logbook did not indicate the year the flight took place. An entry in the back of the logbook showed that the pilot's most recent flight review was conducted on May 11, 2016. His previous flight review was dated August 27, 2014.

According to FAA records, the pilot purchased the airplane in 2011. In February 2014, the pilot sold 50% of the ownership to an individual who responded to an advertisement that he posted on an internet website. This individual stated that he developed a friendship with the pilot through their co-ownership of the airplane. He stated that the accident pilot sometimes flew with him as a safety pilot when he practiced instrument approaches, but he did not believe that the accident pilot had aspired to become instrument rated. According to the co-owner, the accident pilot made less than five total cross-country flights each year, and his local flying normally took place ahead of his cross-country flights and was for the purpose of maintaining his currency to carry passengers.

The pilot's business partner flew with the pilot on three occasions and observed him watching a moving map on an iPad during one of the flights. AIRCRAFT INFORMATIONAccording to FAA records, the airplane was manufactured in 1970 and registered to N9402M Aviation, LLC on July 22, 2011. The airplane was powered by a turbocharged, direct-drive, air-cooled, 310-horsepower Continental TSIO-520R engine. A review of the airplane's logbooks revealed that the airplane's most recent annual inspection was completed on October 21, 2016, at a tachometer time and total time of 4,307 hours. The engine logbook indicated that a 100-hour inspection was completed on October 21, 2016, at which time the engine had accrued 311 flight hours since major overhaul. At the time of the accident, the tachometer time was 4,323 hours.

A fuel receipt obtained from Signature Flight Support at SDL showed that the pilot purchased 42 gallons of 100 LL aviation grade gasoline at 0845 on the day of the accident. The co-owner reported that he was the last person to fly the airplane before the accident flight. He returned the airplane with about 44 gallons of fuel onboard about 4 days before the accident.

The owners installed a Garmin 750 GPS that was equipped with a Terrain Awareness Warning System (TAWS) and an engine analyzer in April 2016. The co-owner routinely updated the GPS databases and tested the TAWS system.

An estimate of the airplane's weight and balance was computed using the occupants' weights reported by the medical examiner. The baggage weight was determined by adding the weight of the baggage recovered by the medical examiner to the weight of the baggage that remained with the wreckage. The center row left seat had been removed from the airplane, and two weight and balance scenarios were computed. The first scenario (labeled "Graph no. 1" in the "Weight & Balance Computation" document in the NTSB public docket) assumed that the 218 pounds of baggage was split between the center and aft rows, and the second scenario (labeled "Graph no. 2" in the in the "Weight & Balance Computation" document in the NTSB public docket) split the same baggage weight between the center row and the baggage compartment. Computations showed the airplane's center of gravity within the moment envelope for both scenarios. METEOROLOGICAL INFORMATIONWeather Conditions at Time of Accident

At 0935, the weather conditions recorded at Payson Airport (PAN), Payson, Arizona, elevation 5,157 feet, located about 11 nm south of the accident site, included wind variable at 4 knots with gusts to 10 knots, visibility 10 statute miles, overcast ceiling at 300 ft above ground level (agl), temperature 2°C, dew point 1°C, and an altimeter setting of 30.11 inches of mercury.

Visible satellite imagery showed extensive cloud cover over the accident site with the clouds moving from west to east. Sounding data and infrared satellite imagery were used to determine the likely cloud cover that the airplane encountered along the route of flight. Figure 1, which depicts the cloud cover and the airplane's flight track, shows that the airplane departed in visual meteorological conditions (VMC) and entered a combination of IMC/VMC when it climbed above 7,000 ft. The airplane then entered IMC when it crossed over the Mazatzal Mountains, about 20 nm south of the accident site, and remained in IMC for the rest of the flight.

Figure 1 – Cloud Cover with height (Color Fill) and Accident Flight Track (Line)

A pilot weather report made near the time of the accident reported cloud tops at 11,000 ft about 40 nm west of the accident site. Another report made about 1 hour after the accident reported cloud bases between 5,900 ft and 6,400 ft and cloud tops about 8,000 ft about 50 nm northwest of the accident site. Pilot reports of light rime icing were made about 90 minutes after the accident took place and 45 nm northwest of the accident site.

Weather Forecasts

Airmen's meteorological information (AIRMET) advisories SIERRA and TANGO were issued at 0745 and were valid for the accident site at the time of the accident. AIRMET SIERRA forecasted IMC and mountain obscuration conditions due to clouds, precipitation, and mist, and AIRMET TANGO forecasted moderate turbulence below FL180.

An area forecast issued at 0445 and valid at the time of the accident called for a broken to overcast ceiling at 9,000 ft with cloud tops at 10,000 ft and a south wind gu...

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR17FA045