LAX06FA005

Seconds after takeoff during an instructional flight, the airplane stalled and impacted into an open field about 0.2 miles from the runway's departure end. The purpose of the flight was for the certified flight instructor (CFI) to provide the private certificated pilot instruction in unusual attitude maneuvers including in-flight loss of control and engine failure after takeoff with a return to runway landing. Ground witnesses observed the airplane in its initial takeoff climb at a 45-degree nose up attitude reach about 650 feet above ground level (agl), whereupon it stalled, banked sharply left, and then "fell out of the sky." Thereafter, it descended in a nose down attitude to ground impact while reversing direction. The accident site and wreckage examination revealed the airplane impacted the ground in a near level flight attitude. Insufficient altitude existed for the CFI to fully recover from the incipient spin/stall. A post impact ground fire destroyed the airplane. The airframe and engine were examined, and no evidence of any mechanical malfunction or control system disconnect was found.

History of flight

On October 10, 2005, about 1435 Pacific daylight time, an American Champion Aircraft Corporation (ACAC) 8KCAB, N943D, impacted terrain seconds after taking off from the Oroville Municipal Airport, Oroville, California. The airplane crashed into an open field about 0.2 miles east of the departure end of runway 12. The airplane was destroyed during the impact sequence and by post impact ground fire. The certified flight instructor (CFI), who held an airline transport pilot certificate, and the second pilot, who held a private pilot certificate, were fatally injured. The CFI was providing dual flight instruction to the second pilot. Alpine Aviation, Inc., Grass Valley, California, operated the airplane. Visual meteorological conditions prevailed at the time of the local area instructional flight, and no flight plan had been filed. The flight was performed under the provisions of 14 CFR Part 91, and it originated from Grass Valley about 1400.

An eyewitness to the accident, who was located about 1.2 miles northwest of the accident site, reported observing the airplane on a close-in left base leg to runway 12. The airplane made a "sharp" left turn and landed on the runway. Seconds thereafter, the airplane took off and climbed to an estimated maximum altitude of 650 feet above the ground. Suddenly, the airplane banked "sharply" left and "fell out of the sky."

Another eyewitness, who was located between 0.25- and 0.5-mile southwest of the airport, reported observing the airplane on its takeoff roll from runway 12. After the airplane became airborne, it climbed at an estimated 45-degree nose up pitch attitude. The witness stated that the airplane climbed between 300 and 400 feet above the ground, whereupon it appeared to stall. Thereafter, it made a steep left bank and looked as though it was out of control. As the airplane descended in a nose down attitude it completely reversed its direction. The airplane burst into flames seconds after crashing into the ground.

The owner of Alpine Aviation indicated to the National Transportation Safety Board investigator that the CFI had flown with the student earlier in the day for 1.5 hours, as recorded in company records. The student was undertaking flying lessons in a curriculum that provided training involving stall-spin recovery, unusual attitude recovery, and critical in-flight situations. The records indicated, in part, that during their morning flight the CFI had likely continued instructing the student in unusual attitude maneuvers. The records specifically indicated that they had reviewed the following maneuvers: slips, rolls, unusual attitude recoveries and low altitude 180-degree approaches to landing. Additionally, the records indicated that the CFI had provided his student with practice regarding control loss in flight.

Alpine's owner reported that the CFI had outlined the day's lesson plan on the flight school classroom's whiteboard. Near the center of the whiteboard, and partially underlined, the following words were written by the CFI: "180 degree Pwr Off Lndg [and] Eng Fail after T/O & RTN."

Alpine's owner opined to the Safety Board investigator that this lesson plan indicated the CFI anticipated teaching the student a specific emergency procedure. The procedure involved simulating an engine failure after takeoff following which the airplane's course would be reversed with the intent of returning to the airport for a landing.

Personnel information

Pilot-in-Command (CFI).

The CFI held an airline transport pilot certificate, with an airplane multiengine land rating. He had commercial pilot privileges for airplane single engine land and sea. Additionally, he held a DC-9 type rating. The pilot also held a certified flight instructor certificate for airplane single engine, with an expiration date of January 2006.

On a pilot experience form dated July 20, 2005, the pilot informed his employer, Alpine Aviation, that he had 3,300 total logged civilian pilot flying hours. Also, he had 3,300 logged military flying hours. The pilot's total single engine fixed gear flying experience was 300 hours. The pilot's employer reported that the pilot's total flying experience in the accident model of airplane was about 200 hours.

Second Pilot.

The second pilot held a private pilot certificate with an airplane single engine land and an instrument rating. According to the owner of Alpine Aviation, the renter-pilot's total flying experience was about 924 hours. The pilot's total flying experience in the accident model of airplane was 10 hours.

Aircraft information

The accident airplane, commonly referred to as a "Super Decathlon," was issued a Federal Aviation Administration (FAA) Standard airworthiness certificate in the normal and acrobatic category. The airplane was capable of inverted flight maneuvers.

The airplane's maximum certificated gross weight in the normal and acrobatic categories was 1,800 and 1950 pounds, respectively. Based on calculations provided by Alpine Aviation, at the time of the accident the airplane was being operated within the prescribed weight and balance limits. The estimated gross weight of the airplane was approximately 1,837 pounds, and the center of gravity was about 16.7 inches aft of datum. The aft limit was 18.5 inches aft of datum. (See Alpine's calculations in the docket for this report.)

The airplane was maintained on an annual and 100-hour inspection basis. The last annual inspection was performed on December 1, 2004, at a total airplane time of 142.4 hours. The last 100-hour inspection was performed on September 20, 2005, at a total airplane time of 301.3 hours. By the accident date, the airplane's total time was about 325 hours.

Meteorological information

The closest aviation weather observation station to the accident site was located at the Oroville Airport. In pertinent part, at 1453, the following weather conditions were reported by the airport's automated surface observing system (ASOS): sky clear; visibility 10 miles; wind from 160 degrees at 9 knots; and temperature/dew point 27 and 4 degrees, Celsius, respectively.

Communication

The FAA reported that no communications or services were provided to the accident pilot/airplane during the accident flight.

Airport and ground facilities

The Oroville Municipal Airport, elevation 192 feet mean sea level (msl), has runway 01-19, which is 6,020 feet long by 100 feet wide, and runway 12-30, which is 3,540 feet long by 100 feet wide. No obstructions are listed beyond the departure end of runway 12.

Wreckage and impact information

Under the Safety Board investigator's direction, the FAA coordinator responded to the accident site and performed the on-scene wreckage examination. The FAA coordinator reported that the airplane impacted an open, near level dirt field, about 140 feet msl. The accident site was located about 0.2 miles east of the departure end of runway 12. The approximate coordinates of the location are 39 degrees 29.17 minutes north latitude by 121 degrees 36.42 minutes west longitude.

The initial point of ground impact (IPI) was identified by the presence of a ground swath, consistent with the width of the airplane's fuselage. The swath was cut into the native grass vegetation and was oriented along a northeasterly course nearly perpendicular to the runway. The ground swath led toward the main wreckage, which was an estimated 125 feet northeast of the IPI. The propeller assembly was found in the ground swath, about 1/3 the distance between the IPI and the main wreckage. In the same general area, oil was observed in the grass. The airplane came to rest in an upright attitude.

The airplane was consumed by fire except for the outboard portion of the left wing, the left horizontal stabilizer, and the left elevator assembly, which remained mostly intact. Both wing tips remai