Cirrus NTSB Database
N254SR 20071230
Home
N254SR 20071230
N414CD 20071128
N482SR 20071125
N108GD 20071121
N901SR 20070202
N457S 20061218
N665CD 20061130
N969ES 20061027
N121LD 20061025
N929CD 20061011
N787SL 20060915
N91MB 20060828
N8163Q 20060711
N667WP 20060204
N526CD 20060109
N799TM 20051229
N621PH 20051211
N286CD 20050206
N6057M 20050120
N889JB 20050115
N1159C 20041204
N1223S 20040910
N8157J 20040419
N100BR 20031012
N9523P 20030118
N566T 20021103
N901CD 20020528
N837CD 20020424
N893MK 20020123
N116CD 20010410

On December 30, 2007, about 1140 Pacific standard time, a Cirrus SR22, N254SR, departed controlled flight and collided into the slope of a hill near Paso Robles, California. Cirrus Design Corporation was operating the airplane under the provisions of 14 CFR Part 91. The certificated flight instructor, the sole occupant, sustained fatal injuries. The airplane was substantially damaged. The personal flight departed San Carlos Airport, San Carlos, California, about 1030, with a planned destination of Paso Robles Municipal Airport. Visual meteorological conditions prevailed, and no flight plan had been filed.

The National Transportation Safety Board investigator-in-charge (IIC) interviewed a close friend of the pilot during the investigation, including immediately following the accident. He stated that the pilot was planning to visit him for the weekend, flying from his base airport to Paso Robles, as he had done many times prior. The pilot called him on a cellular telephone while in the airplane approaching the proximity of the friend's residence informing him that he was about to pass by. The pilot had done this on many occasions to let the friend know that he was about to land, as a way of notifying him that he should leave to pick him up from the airport, which was an approximate 15-minute drive.

The pilot's friend further stated that he proceeded outside to watch the airplane while speaking with the pilot on the telephone. He observed the airplane drop rapidly about 1,000 feet as it was flying toward his house. As the airplane was approaching his house in a nose-high configuration with full power, he heard the telephone drop and the pilot make a few inaudible comments. He noted that with the orientation of the airplane to the terrain he was nervous of an impending crash. The airplane than made a rapid ascent in a near vertical nose-high maneuver climbing to about 1,000 feet above ground level (agl). It subsequently made a 90-degree right turn and then continued to turn into a barrel roll, disappearing behind the tree line ahead. He noted that he heard the engine producing full power during the maneuver.

Numerous witnesses were interviewed by the IIC following the accident. One witness, who lived adjacent to the pilot's friend, stated that she was trimming olive trees that surround her property when she noticed an airplane fly over her house. The airplane continued slightly left [east] and was maneuvering at a "very, very, very low" altitude. Another witness recalled observing the airplane flying from the east and over his house at an altitude of about 200 feet. He noted that the airplane was flying very fast and descended to about the tree-top level. The airplane then began a rapid ascent, almost vertical. After gaining altitude it rolled to the right and then began a loop below the tree line, where he lost visual contact.

An additional witness, whose property is oriented on a small hill about 100 feet above the valley floor stated that from his vantage point he observed the airplane looking downward as it passed by, which he approximated was maneuvering at 75 feet agl. The airplane was flying rapidly through the valley and began a rapid accent as it reached the end of the west property lines of the neighbors. The witness further recalled that he has seen a low flying airplane in the neighborhood previous to the accident. He specifically recalled that about 2 months prior, an airplane flew about 50 feet above his house. Many of his neighbors and him have discussed an airplane that maneuvers very low in the area.

Records established that the airplane was fueled with the addition of 44.2 gallons of aviation fuel on the day of the accident.

The closest official weather observation station was in Paso Robles Airport, located about 10.5 nautical miles (nm) northwest of the accident site at an elevation of 836 feet mean sea level (msl). An aviation routine weather report (METAR) for the airport was issued at 1153. It stated: winds from 310 degrees at 5 knots; visibility 10 statue miles; scattered clouds at 1,700 feet; temperature 13 degrees Celsius; dew point 7 degrees Celsius; altimeter 30.26 inches of mercury.

The wreckage was located on the hills of an estate, stretching over 1,200 feet from the first impact marking to the farthest debris found (right main landing wheel); the main wreckage was located close to the middle. In character, the rolling hills were comprised of dirt and dry grass and populated by scattered oak trees typical of the central California region. The main wreckage was located at an estimated 35 degrees 32.525 minutes north latitude and 120 degrees 31.369 minutes west longitude, at an elevation of about 1,115 feet mean sea level (msl).

The main wreckage came to rest on a northeast facing slope and had been subjected to severe thermal damage. The main wreckage consisted of the left wing and tail section as well as the ashen remains of the fuselage. The cabin was completely consumed by fire. The left wing was inverted though remained on the correct side of the fuselage with the leading edge facing downslope and nearly perpendicular to the debris path. The empennage was aft of the wing spar and attached by sections of partially consumed fiberglass and steel cables; the rudder was askew from the empennage, positioned on the right side of the wreckage. All control surfaces were accounted for at the accident site with the exception of the left aileron. The left aileron's aluminum control surface had sections attached at the respective hinges hinges, but the middle section was absent consistent with it being consumed by fire. The firewall was imbedded under the main wreckage and the engine mounts were broken.

The first identified point of contact consisted of disrupted dirt on a small berm making up the far northern end of the debris field. The markings started as two parallel indentations in the vegetation and dirt. The right crater began about 1 foot before the left; they were about 8 feet apart, consistent in size and orientation to that of the main landing gear. The craters were continuous for about 8 feet and gradually matured into a sole crater measuring about 20 feet wide.

Enter content here

Enter content here

Enter content here

Critical Decision Making Seminars