N291CC is a 1977 Beech C90. It is a fixed-wing multi-engine aircraft with 9 seats, powered by a P&W Canada PT6A-60A rated at 1050 horsepower. The registration is active, with the registrant based in Argyle, TX. Its standard airworthiness certificate was issued in Jun 1977. It has been registered to its current owner since Sep 2022. This page also carries 2 NTSB events.
- 49 years old
2022
1977
That's everything on file so far — TailWiki checks the FAA registry daily and adds new entries as N291CC's record changes.
On October 12, 2025, about 1334 central daylight time, a Beech C90, N291CC, was destroyed when it was involved in an accident near Fort Worth, Texas. The private pilot and pilot-rated passenger were fatally injured. The airplane was operated as a Title 14?Code of Federal Regulations Part 91 personal flight.
According to Federal Aviation Administration (FAA) Automatic Dependent Surveillance – Broadcast (ADS-B) information, the airplane took off from Perot Field/Fort Worth Alliance Airport (AFW), Fort Worth, Texas, at 1203, proceeded in a northwesterly direction and performed several approaches to the Bowie Municipal Airport (0F2), Bowie, Texas. The airplane then flew in a southerly direction, performed one 360° right turn about 13 nautical miles south-southwest of 0F2, then flew south again. The airplane continued in a southerly direction until about 1325, when it turned left to a southeasterly direction and remained on that heading until about 1333. About that time, when the flight was about 3.8 nautical miles northwest of Hicks Airfield (T67), Fort Worth, Texas, the airplane turned right and began flying in a south-southeasterly direction toward T67.
A pilot who was based at T67 and flying at the time of the accident, reported a radio transmission on the T67 common traffic advisory frequency, which was consistent with the accident airplane, on a 5-mile final approach to T67. She did not hear any further transmissions from the accident airplane, which continued the south-southeasterly heading toward T67. At 1333:34, when the flight was about 1.3 nautical miles northwest from the approach end of runway 14 at T67, the airplane turned left and began flying in a northerly direction.
A video camera located about .25 nautical mile south of the accident site recorded the airplane flying low, above powerlines while in a slight left bank with the landing gear extended. The airplane continued on the northerly direction and began descending. The left bank angle increased and exceeded 90° before the airplane went out of view behind trees/bushes. ADS-B data showed that the airplane flew over a commercial building immediately adjacent to the accident site where several videos depicted the airplane impacting the ground while inverted and in a left wing low attitude. The airplane then impacted numerous parked, unoccupied commercial vehicles with an immediate explosion and extensive postcrash fire which consumed nearly the entire airplane.
The remains of the wreckage, which included both engines and propellers, were recovered and retained for further examination.
On May 27, 2011, about 1515 eastern daylight time, a Beechcraft C90, N291CC, was substantially damaged during an encounter with severe turbulence at an altitude of 20,000 feet approximately 10 miles north of Woodward Airport (CDN), Camden, South Carolina. The airline transport pilot and four passengers were not injured. Instrument meteorological conditions prevailed, and the airplane was operating on an instrument flight rules flight plan from Charleston International Airport (CHS), Charleston, South Carolina, to Newark-Heath Airport (VTA), Newark, Ohio. The personal flight was operated under the provisions of 14 Code of Federal Regulations Part 91.
According to the pilot, he obtained weather information via the internet prior to the flight, which included advisories for convective activity and scattered thunderstorms along the intended [northwest] route of flight. The takeoff from CHS and the climb to cruise altitude were "normal," with intermittent periods of light turbulence.
The pilot also stated that about 100 miles northwest of CHS, he observed weather ahead on the airplane's on-board weather radar and requested a course deviation from the en route air traffic controller. The deviation was granted, but the pilot was instructed to turn no more than 30 degrees west of his previously established heading. After turning the 30 degrees, the pilot realized that he would require an additional 30- to 45-degree course deviation to avoid the weather ahead. The pilot stated that he attempted to contact the controller three times, and after receiving no response, elected to turn further to the west. The airplane then encountered moderate to severe turbulence lasting about 2 minutes and an approximately 300-foot deviation in altitude.
The pilot also stated that after the encounter, the airplane performed normally with no observed anomalies, so he elected to continue to the destination. His postflight visual inspection of the airplane revealed no damage, and he flew the airplane back to CHS the following day. Subsequent closer inspection of the airplane revealed wing spar damage at the fuselage attach point, as well as wrinkling of the wing skin.
A review of air traffic control voice communications (tapes and transcripts) revealed that the pilot established contact with Jacksonville Center at 1449. At that time, the pilot reported that the airplane was climbing through 7,000 feet for 8,000 feet and experiencing "light chop." The controller then cleared the airplane to climb and maintain an altitude of 15,000 feet.
At 1450, the controller asked the pilot about his routing, which he noted would take the airplane through the center of scattered areas of moderate to extreme precipitation, beginning 20 miles at 10 o'clock, scattered along the route for 100 miles. The pilot responded, "that's exactly what I'm looking at, [it] looks pretty good right now; believe we can get through it." The controller then advised the pilot to let him know if he needed to deviate.
At 1454, the pilot was cleared to climb the airplane to flight level 200.
At 1507:26, the pilot called the controller, who responded that the call was unreadable.
At 1507:37, the pilot requested a course deviation "about 45 degrees to the left" to avoid weather. The controller cleared the airplane to deviate up to 30 degrees left of the established course, and to proceed direct to VTA when able.
According to the controller, and as confirmed by radar, only 30 degrees was approved due to a commercial airliner climbing west of the accident airplane's position.
Multiple radio calls from multiple aircraft were then made, many indiscernible, regarding deviations for weather.
About 1508:40, an unidentified voice stated, "…further left for weather."
At 1510:56, the pilot attempted to contact the controller while the pilot of another airplane was reading back a clearance.
At 1511:15, a voice similar to the pilot's attempted to contact the controller while the controller was issuing instructions to another airplane.
At 1511:39, the pilot again contacted ATC, and stated that he was "getting beat up pretty good," and requested to deviate further left of course. The controller reported an opening in the weather about 11 miles from the airplane's position, and suggested a heading of 350 degrees to exit the weather. When queried about the ride conditions, the pilot reported "moderate to severe" turbulence approximately 3 minutes prior, but that the airplane was experiencing "light to moderate" turbulence at the time.
At 1514:11, the controller stated that it appeared that the airplane was exiting the extreme precipitation and the pilot concurred. When the controller asked if the airplane had sustained damage or if any passengers had been injured as a result of the turbulence encounter, the pilot replied that everything was "okay."
At 1515:55, the pilot reported that the airplane was "in the clear." The controller stated that the pilot should not hesitate to make a precautionary landing should he suspect structural damage to the airplane, then instructed the pilot to contact Atlanta Center.
The pilot held an airline transport pilot certificate with ratings for airplane single engine land and sea, and multiengine land; as well as a flight instructor certificate with ratings for airplane single- and multiengine land and instrument airplane.
The pilot reported 14,500 total hours of flight experience, of which, 2,200 hours were in the accident airplane make and model. His most recent flight review was conducted in February 2011.
According to FAA records, the airplane was manufactured in 1977, and was powered by two Pratt & Whitney PT-6 turboprop engines. The airplane's most recent continuous airworthiness program inspection was conducted on April 27, 2011, at which time the airframe had accrued a total time of 10,423 hours.
In addition to weather radar, the airplane was equipped with a multifunction display that provided Next Generation Radar (NEXRAD) weather information received from a commercial satellite weather service and a stormscope real-time lightning detection system.
According to an NTSB Weather Study, the 1515 weather observation at CDN included winds from 320 degrees at 9 knots with gusts to 39 knots, one-half mile statute visbility in rain and thunderstorms, a broken cloud layer at 300 feet above ground level (agl), overcast clouds at 3,600 feet agl, temperature 23 degrees C, dew point 20 degrees C, and an altimeter setting of 29.87 inches of mercury. The report also contained remarks for distant lightning to the east and west of the airport.
There was also an active SIGMET at the time of the accident for much of the southeastern United States, including the accident area. The SIGMET advised of severe thunderstorms moving from 220 degrees at 20 knots with cloud tops above flight level 450.
At 1210, the Storm Prediction Center issued a Severe Thunderstorm Watch covering North Carolina, central South Carolina and southern Virginia that was active at the time of the accident. It forecasted severe thunderstorms with hail aloft up to 1.5 inches in diameter with extreme turbulence and surface wind gusts up to 60 knots likely.
The Study also included a stationary base reflectivity image with radar track overlay that indicated that the airplane was headed northwest, and entered moderate precipitation by 1510. (Because the image was stationary, but the thunderstorms were moving northeast, positions as plotted may be displaced from actual positions.)
At the time of initial precipitation contact, an area from the airplane's immediate northwest to the immediate southwest exhibited reflectivity consistent with "intense" or "extreme" precipitation as defined by FAA Advisory Circular AC 00-24B, with cloud tops reaching 36,000 feet. There were also areas of lightning to the southwest and west.
At radar plot time 1511, the airplane altered track about 30 degrees to the left, and just after that, entered the intense precipitation. By 1512, the airplane was in the middle of the intense precipitation, and it then altered course to the left by about another 30 degrees. By 1513, the airplane had cleared the intense precipitation, and altered course about 45 degrees to the right, back toward its destination.
Both the radar and NEXRAD also revealed areas with less precipitation to the northeast and south when the airplane penetrated weather to west. They also showed no precipitation to the southeast, from where the airplane had come.
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