N9330M

Destroyed
Fatal

MOONEY M20ES/N: 1262

Accident Details

Date
Monday, April 1, 2013
NTSB Number
CEN13FA217
Location
Guymon, OK
Event ID
20130403X14843
Coordinates
36.730556, -101.605278
Aircraft Damage
Destroyed
Highest Injury
Fatal
Fatalities
2
Serious Injuries
0
Minor Injuries
0
Uninjured
0
Total Aboard
2

Probable Cause and Findings

The noninstrument-rated pilot's encounter with instrument meteorological conditions, which resulted in spatial disorientation and his subsequent loss of airplane control. Contributing to the accident was the pilot's decision to take off in deteriorating weather conditions.

Aircraft Information

Registration
N9330M
Make
MOONEY
Serial Number
1262
Engine Type
Reciprocating
Year Built
1966
Model / ICAO
M20EM20P
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
ASTING NEIL J
Address
19670 BLUE CLOVER LN
Status
Deregistered
City
MONUMENT
State / Zip Code
CO 80132-9448
Country
United States

Analysis

HISTORY OF FLIGHT

On April 1, 2013, about 1210 central daylight time, N9330M, a Mooney Aviation Company, Inc. M20E, single engine airplane, was destroyed after impacting terrain near Guymon, Oklahoma. The pilot and passenger were fatally injured. The airplane was registered to and operated by a private individual. Instrument meteorological conditions (IMC) prevailed at the time of departure and a flight plan had not been filed for the 14 Code of Federal Regulations part 91 personal flight. The airplane departed Guymon Municipal Airport (KGUY), Guymon, Oklahoma, at 1204, and was en route to Meadow Lake Airport (KFLY), Peyton, Colorado.

The airplane had earlier that morning departed from El Reno Regional Airport (KRQO), El Reno, Oklahoma, with a final destination of KFLY. After landing for an en route fuel stop at KGUY the pilot checked the weather and departed during deteriorating weather conditions. The airplane failed to arrive at KFLY. The burned wreckage was discovered two days later on the afternoon of April 3, 2013, in a remote area about 6 miles northwest from KGUY.

PERSONNEL INFORMATION

The pilot, age 68, held a Federal Aviation Administration (FAA) private pilot certificate with a rating for only airplane single engine land. He did not hold an instrument rating. His first FAA pilot certificate was a student pilot certificate which was issued on December 1, 2004, and his FAA private pilot certificate was initially issued on December 14, 2005.

The pilot's logbooks were not available during the course of the investigation. Based on the pilot's most recent airman medical certification application, aircraft maintenance logbooks, aviation insurance company documents completed by the pilot, and other documents, the pilot's flight experience as of March 9, 2013, was estimated as 933 hours of total flight experience with about 638 hours of pilot experience in Mooney M20 series airplanes.

No records were found which indicated that the pilot had flight experience in any aircraft other than single engine land airplanes, and there was no logbook record of the pilot's instrument flying experience.

A certified flight instructor (CFI) administered a satisfactory flight review to the pilot on October 19, 2011, and reported that the pilot knew his aircraft and was knowledgeable of the regulations and proper procedures. The CFI also reported that during the 1.4 hour long period of flight instruction the pilot flew the airplane well in visual conditions, but had some difficulty flying in simulated instrument conditions while wearing a hood. After more instruction the pilot's hood work improved and he completed three unusual attitude recoveries while under the hood.

AIRCRAFT INFORMATION

The four-seat, low-wing, retractable landing gear, single engine airplane, serial number (s/n) 1262, was manufactured in 1973. It was equipped with a 200-horsepower Lycoming model IO-360-A1A engine, s/n L-2718-51A, which drove a Hartzell, model HC-C2YR-1BF, 2-blade metal alloy propeller, s/n CH42095B.

The accident airplane was equipped with a Garmin GNS430W GPS; and an Aspen EFD 1000 system with an Aspen EWR50 XM weather receiver capable of displaying satellite weather overlays on the moving map display. The Aspen equipment had been installed in April, 2012. The airplane was also equipped with a J.P. Instruments EDM-700 engine monitoring system; an S-TEC System 30 two axis autopilot; and a model EBC-102A emergency locator transmitter (ELT).

Fuel receipts at KGUY showed the airplane had been topped-off to its 52 gallon capacity with 21.6 gallons of 100LL aviation gasoline. A postaccident fuel quality inspection of the refueling facility at KGUY was satisfactory.

A witness at KGUY reported that the pilot and passenger were seated in the two front seats, and the rear cabin was loaded with baggage and personal cargo "all the way up to the roof". The witness also reported that the pilot told him that he had "airborne XM weather radar installed on the airplane, but that it wasn't working".

METEOROLOGICAL INFORMATION

KGUY was the closest official weather station to the accident site and had an Automated Surface Observing System (ASOS5) whose reports were not supplemented by a human observer. At 1053 KGUY reported the wind was from 020 degrees at 17 knots, visibility 10 miles, ceiling overcast at 1,400 feet above ground level (agl), temperature 4 degrees Celsius (C), dew point 0 degrees C, with an altimeter setting of 30.17 inches of mercury.

At 1203 the data from KGUY revealed that the wind was from 360 degrees at 13 gusting to 23 knots, visibility 10 miles, ceiling broken at 800 feet agl, overcast clouds at 1,200 feet agl, temperature 3 degrees C, dew point 0 degrees C, with an altimeter setting of 30.20 inches of mercury. Remarks indicated that the pressure was rising rapidly.

At 1253 the data from KGUY revealed that the wind was from 020 degrees at 15 gusting to 21 knots, visibility 10 miles, overcast clouds at 800 feet agl, temperature 2 degrees C, dew point -1 degrees C, with an altimeter setting of 30.18 inches of mercury. Remarks indicated that unknown precipitation began at 15 minutes after the hour and ended at 30 minutes after the hour, and rain began at 18 minutes after the hour and ended at 28 minutes after the hour. The ceiling was variable from 600 to 1,000 feet agl. Remarks also indicated that the freezing rain sensor not operating.

A witness at KGUY reported that the cloud condition was a low ceiling when the airplane landed and the ceiling was even lower with sprinkling rain and sleet when the airplane departed.

Another witness recalled hearing hail or sleet on the hangar roof before the airplane departed.

Records showed that the pilot used a desktop computer in the FBO pilot's flight planning room to check weather using "WSI" and "Aviation Sentry Weather" before he departed from KGUY. However, neither of those resources logs access, so there was no record of what specific weather information was obtained by the pilot.

COMMUNICATIONS AND POSTACCIDENT SEARCH ACTIVITY

On April 1, 2013, about 0733, the pilot of the accident airplane telephoned the Flight Service Station (FSS) and received a pilot weather briefing to fly from KRQO to KFLY. The pilot received only a weather briefing for the expected 3-hour flight and did not file a flight plan.

There was no record of any subsequent communications from the pilot.

On April 2, 2013, family members had become concerned and notified the FAA that the airplane had failed to arrive. Within minutes several different agencies became involved in the search efforts. Local emergency responders near KFLY conducted a physical search and confirmed the accident airplane had not arrived at the airport and the pilot's vehicle was still there. The FSS issued an alert notice (ALNOT) which directed an extensive communication search for the overdue, unreported, or missing aircraft.

FAA air traffic control (ATC) coordinated with the U. S. Air Force Rescue Coordination Center (AFRCC) and with volunteers from the Civil Air Patrol (CAP). AFRCC reported there had not been any reports of ELT signals along the route of flight from KRQO to KFLY. FAA ATC and CAP forensic radar specialists identified several radar targets in the area around KRQO, but were unable to positively identify the accident airplane. A volunteer CAP cell phone forensics specialist began tracking data from the pilot's cell phone and determined the pilot's cell phone had last been in the vicinity of KGUY.

Direct coordination with the airport fixed base operator (FBO) at KGUY showed that the accident airplane had landed at KGUY at 1050 on April 1, 2015, refueled, and took off northbound from runway 36 at 1204.

The FAA ATC radar forensics specialist reported that radar coverage west and northwest of KGUY is "sparse" below 5,000 to 6,000 feet mean sea level (msl), and that no radar tracks were visible for the accident airplane. The KGUY airport is at an elevation of 3,125 feet msl, and the elevation of the accident location was estimated about 3,209 feet msl.

The FAA, FSS, and AFRCC, coordinated with volunteer CAP search teams from Texas, Oklahoma, and Colorado to immediately begin efforts for an airborne search, but the CAP units were prevented from launching because of adverse weather.

About 1600 on April 3, 2015, a local pilot at KGUY, who was aware of the missing airplane, was airborne on a local flight when he visually spotted the burned wreckage in a remote area about 6 miles northwest from KGUY. A local law enforcement officer drove to the accident scene and confirmed the location of the wreckage and the airplane's registration number. Other emergency personnel responded, the ALNOT was cancelled, the AFRCC search and rescue mission was terminated, and the multi-state CAP search mission was terminated.

WRECKAGE AND IMPACT INFORMATION

The wreckage was found impacted on dirt and rock in high desert terrain in a remote unpopulated area. The intact wreckage was upright and remained in or immediately adjacent to the impact ground scars. The fuel tanks were breached and much of the airplane was mostly consumed by a postimpact fire.

Impact scars, accordion compression buckling of the leading edges of the wings, and other evidence at the scene, was consistent with a wings level, terrain impact of about 70 degrees nose down. Witness marks showed the tail surfaces had bent straight forward during the impact, struck the empennage, and then rebounded.

All of the airplane components and flight control surfaces were accounted for and remained connected. Flight control continuity was confirmed from the control surfaces to impact separations or to the melted metal mass in the cockpit area. Areas of some flight control push-pull tubes were missing or significantly damaged by fire but there was no evidence of preimpact separation.

Fire consumed the inboard portion of the right wing, most of the left wing, and much of the instr...

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN13FA217