California City, CA, USA
N39DF
Aero Vodochody L39
The flight crew in the accident airplane and the producer-director in a second camera ship departed for a planned aerial photography flight. During the filming operation, the director issued a series of instructions to the accident flight crew, and the flight crew maneuvered their airplane pursuant to the instructions. After filming for about 1 hour, the producer, who was in the camera ship at 5,500 feet mean sea level (msl), directed that the accident airplane's crew to perform a "sharp snap roll to the right and pull down out of frame." The crew responded by rolling into a right 135-degree bank and descending. During the attempted recovery from the near split "S" course reversal turn, the airplane impacted the underlying 3,100-foot elevation hillside. Cameras in the accident airplane and the camera ship recorded video and audio during the accident flight that was reviewed during the investigation. No abnormalities in the accident aircraft were observed. The severity of the impact and fire damage to flight controls and associated system components precluded confirmation of their preimpact integrity. Examination of available airframe and engine components revealed no evidence of preimpact mechanical malfunction.
HISTORY OF FLIGHT On February 26, 2006, about 0828 Pacific standard time, an Aero Vodochody, L39, N39DF, crashed into hilly terrain during a low altitude course reversal maneuver about 6.4 nautical miles northwest of California City, California. The experimental category turbojet was owned and operated by Mach 1 Aviation, Universal City, California. The flight was performed under the provisions of 14 Code of Federal Regulations Part 91. The airplane was fragmented upon colliding with terrain and thereafter was consumed by fire. The airline transport certificated (front seat) pilot, and the commercial certificated (rear seat) pilot were killed. Visual meteorological conditions prevailed at the time of the aerial photography flight, and no flight plan was filed. The flight originated from Van Nuys, California, about 0726. The accident occurred during a flight conducted for the purpose of filming a motion picture involving the L39 airplane. The film's producer-director was in the lead Cessna 310 airplane (camera ship) and made a video recording of a portion of the accident airplane's final maneuver. Additionally, an audio and video recording was made by a camera in the accident airplane. According to the director, at the commencement of the accident airplane's course reversal maneuver, the airplane had been cruising about 5,500 feet mean sea level. The operator indicated that the pilot who occupied the front seat was in command, and the pilot who was positioned in the rear seat was the "co-pilot." The operator also reported that the airplane could be flown from either seat. However, according to the operator, the front seat pilot was more experienced and would generally be the pilot who was handling the controls. The Safety Board investigator reviewed the voice communications between the pilots to ascertain who was issuing instructions, and who was receiving instructions. The review of the recorded communications indicates that during the majority of the flight, the rear seat pilot provided safety advisories to the front seat pilot. The following are examples of communications that occurred between the pilots a few minutes after takeoff: Front seat pilot: "Sorry, I won't pull that hard next time." Rear seat pilot: "No, it's okay. I just didn't want you to stall." Front seat pilot: "As soon as I felt a burble I broke the angle of attack." Later during the flight, the following communications occurred when the producer-director requested that the accident airplane crew reposition itself for another film shot: Front seat pilot: "Okay. Coming back. I'll give you power in just a second...." Rear seat pilot: "That's okay. I just don't want you to....I'm just here to be your little voice....Watch your power...." Several minutes prior to the accident the airplane was in a valley and positioned such that it was closing on a hillside. To avoid impacting the rapidly rising terrain directly ahead of the airplane, the crew had to abruptly climb. During this episode, the rear seat pilot stated the following to the front seat pilot: "Power. Power. Power. Let's go." About two minutes prior to the crash, the crewmembers appeared to change roles. The rear seat pilot indicated that he would fly the airplane, and the front seat pilot provided safety-related comments. During this period the following communications occurred: Rear seat pilot: "I got the plane." Front seat pilot: "You got the aircraft?" Rear seat pilot: "Yeah." Then, the producer-director, who was on the same radio frequency, issued his final directions to the accident airplane's crew (which crashed seconds later): Director: "You're doing really good. Give me a sharp snap roll to the right and pull down out of frame. Front seat pilot: "You okay [name of rear seat pilot]?" Rear seat pilot: "Yep. I got it." A Safety Board video specialist's review of the video indicates that the accident airplane then executed a 90-degree roll to the right and its nose fell below the horizon. About 1 second thereafter, the airplane abruptly rolled further right to approximately 135 degrees of bank, and the nose dropped further as the airplane directly approached hilly terrain. Two seconds later the rear seat pilot stated, "I got it, I got it, I got it." The front seat pilot stated, "ease off" and the rear seat pilot responded, "ease off." Four seconds later, the airplane began an abrupt left roll back to approximately 30 degrees of bank. Two seconds thereafter, the airplane rolled right again to about 45 degrees bank as the airplane continued to close on the side of a hill. During this time, the rear seat pilot stated, "I got it, ease off, ease off, okay." The video ended 4 seconds later with the airplane approaching terrain. The recording recovered from the accident airplane was too impact-damaged to extract additional images. The recording taken from the camera ship showed the accident airplane descending, and then the airplane went out of frame. When the video camera was directed toward the area where the accident airplane was expected to reappear, images of a developing plume of smoke and fireball were apparent on the underlying hillside in an area commensurate with the accident airplane's anticipated location. The fire spread in a longitudinal direction away from the camera ship's location, and in a direction consistent with the accident airplane's final direction of travel. PERSONNEL INFORMATION Pilot (front seat) The pilot, age 43, held an airline transport pilot certificate with the following ratings: airplane single engine land, airplane multiengine land and glider. He held FAA authorization to fly an experimental L39 airplane. According to Federal Aviation Administration (FAA) records, on the pilot's August 2005, application for a second-class aviation medical certificate, he reported 5,500 total civilian flight hours. No military flight hours were reported. The pilot's logbook was not recovered for examination. The pilot's flying experience in the model of accident airplane was not determined. Pilot (rear seat) The pilot, age 60, held a commercial pilot certificate with the following ratings: airplane single engine land, airplane multiengine land limited to center thrust, and instrument airplane. He held FAA authorization to fly an experimental L39 airplane. According to FAA records, on the pilot's December 2004, application for a second-class aviation medical certificate, he reported that his total civilian and military flight time was 2,000 and 500 hours, respectively. The pilot's logbook was not recovered for examination. The pilot's flying experience in the model of accident airplane was not determined. AIRCRAFT INFORMATION Aero Vodochody manufactured the two-seat, low-wing, turbojet, serial number 931320, in Czechoslovakia in 1979. The airplane had been manufactured as a primary military jet trainer. The owner reported that an annual inspection was completed on July 25, 2005. By the accident date the experimental category airplane's total time was about 3,000 hours. METEOROLOGICAL INFORMATION The producer-director reported that, in the vicinity of the accident site, there were few clouds at 25,000 feet. The wind was light and variable, there was no turbulence, and the visibility was about 25 miles. COMMUNICATION Within a couple of minutes before and after the accident, none of the airplanes associated with the motion picture filming operation were in communication with any FAA facility. During this time period, the accident airplane was being filmed by the camera ship, and an audio and video recording was being made in the accident airplane. This approximately 1-hour-long recording commenced with the start of the accident airplane's takeoff roll at Van Nuys Airport, and it terminated a few seconds before the crash. FLIGHT RECORDERS The airplane was not equipped with a cockpit voice or flight recorder, and no recording devices were required by the FAA. However, the accident airplane was equipped with a fixed-mounted video recorder that was located in its empennage. This recorder showed a forward-looking view of the fuselage, along the airplane's longitudinal axis, and it filmed the wing flaps, ailerons, and the aft portion of the canopy. It also captured images of the sky condition above and ahead of the airplane, and the underlying terrain. During flight, movement of the flaps and ailerons were apparent, and no anomalies were noted. The pilots' communications and traffic-related audio alert signals from within the airplane were also recorded. In addition to providing the Safety Board investigator with this recording, the operator also provided the Safety Board with a transcript of the voice communications during the hour-long accident flight and a copy of the video recording made by the camera ship. The accident airplane's recording was reviewed by the Safety Board investigator and by a specialist in the Safety Board's Vehicle Recorder Division, Washington, D.C., who prepared a Video Factual Report. WRECKAGE AND IMPACT INFORMATION From an examination of the accident site and airplane wreckage, the airplane was found to have descended into 3,100-foot mean sea level hilly terrain. The initial point of impact (IPI) was noted by the presence of an estimated 3-foot-wide by 10-foot-long ground swath in the 30-degree upsloping soft dirt hillside. Soil was loosened in the swath to an estimated 6-inch depth. Paint chips were noted in the soil in this area. Fragments from the outboard portion of the separated right wing tip were also located in the vicinity of the IPI. In total, fragmented portions of the airplane were principally found over an estimated 800-foot-long by 30-foot-wide west-southwesterly track. The track commenced at the IPI and terminated at the location of the engine and empennage. The cockpit was located in a ravine approximately midway between the IPI and the engine/empennage. The cockpit was totally fragmented and destroyed. The empennage was consumed by fire. (See the wreckage distribution diagrams and global positioning satellite coordinate list for additional details.) The severity of fire damage to flight controls and associated system components precluded confirmation of their preimpact integrity. Examination of available airframe and engine components revealed no evidence of preimpact mechanical malfunction. FIRE The video recordings indicated no evidence of smoke or fire during the airplane's flight. The video indicated that a fire occurred commensurate with ground impact. The fire consumed the airplane. MEDICAL AND PATHOLOGICAL INFORMATION On February 28, 2006, autopsies were performed on both pilots by the Kern County Sheriff-Coroner's Office, Bakersfield, California. The autopsy findings for both pilots indicated they died from multiple blunt force and thermal injuries. Forensic toxicology was performed on specimens from both pilots by the FAA's Bioaeronautical Sciences Research Laboratory, Oklahoma City, Oklahoma. The toxicology reports stated no ethanol or any screened drugs were detected. SURVIVAL ASPECTS The airplane was equipped with ejection seats. The seat's activation mechanism had been rendered inoperable according to the FAA.
The flight crew's failure to maintain terrain clearance during an intentionally performed course reversal turn at low altitude.
Source: NTSB Aviation Accident Database
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