Crash of a Beechcraft BeechJet 400A in Bentonville

Date & Time: Feb 14, 2024 at 1410 LT
Type of aircraft:
Operator:
Registration:
N95GK
Flight Phase:
Survivors:
Yes
Schedule:
Bentonville – Concord
MSN:
RK-027
YOM:
1991
Crew on board:
2
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On February 14, 2024, about 1410 central standard time, a Beech 400A airplane, N95GK, was substantially damage when it was involved in an accident in Bentonville, Arkansas. The 2 pilots and 3 passengers were not injured and 2 passengers were seriously injured. The airplane was operated under the provisions of Title 14 Code of Federal Regulations Part 91 as a business flight. According to preliminary information, while on takeoff from the Bentonville Municipal Airport (VBT), Bentonville, Arkansas, the pilot pulled the control yoke back to rotate the airplane and the control yoke was unresponsive. He aborted the takeoff, but insufficient runway remained to stop. The airplane departed the end of runway 18 and came to rest in mud and grass. During the runway overrun, the right main landing gear collapsed, and the right wing sustained substantial damage. Inspectors from the Federal Aviation Administration responded to the accident site and visually examined the airplane. The elevator control cable was found separated in the area of the vertical stabilizer.

Crash of a Cessna 414 Chancellor in Modesto: 1 killed

Date & Time: Jan 18, 2023 at 1307 LT
Type of aircraft:
Registration:
N4765G
Flight Type:
Survivors:
No
Schedule:
Modesto – Concord
MSN:
414-0940
YOM:
1977
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
4506
Captain / Total hours on type:
9.00
Aircraft flight hours:
3574
Circumstances:
Shortly after taking off, the pilot was instructed to change from the airport tower frequency to the departure control frequency. Numerous radio transmissions followed between tower personnel and the pilot that indicated the airplane’s radio was operating normally on the tower frequency, but the pilot could not change frequencies to departure control as directed. The pilot subsequently requested and received approval to return to the departure airport. During the flight back to the airport, the pilot made radio transmissions that indicated he continued to troubleshoot the radio problems. The airplane’s flight track showed the pilot flew directly toward the runway aimpoint about 1,000 ft from, and perpendicular to, the runway during the left base turn to final and allowed the airplane to descend as low as 200 ft pressure altitude (PA). The pilot then made a right turn about .5 miles from the runway followed by a left turn towards the runway. A pilot witness near the accident location observed the airplane maneuvering and predicted the airplane was going to stall. The airplane’s airspeed decreased to about 53 knots (kts) during the left turn and video showed the airplane’s bank angle increased before the airplane aerodynamically stalled and impacted terrain. Post accident examination of the airframe, engines, and review of recorded engine monitoring data revealed no evidence of any preimpact mechanical malfunctions or failures that would have precluded normal operation. Toxicology testing showed the pilot had diphenhydramine, a sedating antihistamine, in his liver and muscle tissue. While therapeutic levels could not be determined, side effects such as diminished psychomotor performance from his use of diphenhydramine were not evident from operational evidence. Thus, the effects of the pilot’s use of diphenhydramine was not a factor in this accident. The accident is consistent with the pilot becoming distracted by the reported non-critical radio anomaly and turning base leg of the traffic pattern too early during his return to the airport. The pilot then failed to maintain adequate airspeed and proper bank angle while maneuvering from base leg to final approach, resulting in an aerodynamic stall and impact with terrain.
Probable cause:
The pilot’s exceedance of the airplane’s critical angle of attack and failure to maintain proper airspeed during a turn to final, resulting in an aerodynamic stall and subsequent impact with terrain. Contributing to the accident was the pilot’s distraction due to a non-critical radio anomaly.
Final Report:

Crash of a Mitsubishi MU-2B-40 Solitaire in Concord: 2 killed

Date & Time: Jul 9, 1992 at 0730 LT
Type of aircraft:
Registration:
N220MA
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Concord - Yucata - Trenton
MSN:
441
YOM:
1981
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
6452
Aircraft flight hours:
2706
Circumstances:
The 74 year old pilot and his wife were on a trip to attend a funeral. A witness, who heard the airplane overhead, reported that it sounded low and at least one engine was operating. He reported that when he looked up, the airplane was in a dive, spinning slowly; however, the airplane did not make a complete revolution. Radar data showed the airplane in a left descending turn at approximately 2000 feet per minute. The airplane impacted the ground about 3 miles west of the airport in a near vertical descent, and much of the forward section had penetrated the ground. There was a post-crash fire. Examination of the airplane and various actuators confirmed that the landing gear was retracted, flaps were extended 5°, elevator and aileron trim were neutral, and the rudder was positioned 3° left. Examination of the engine confirmed internal/rotational damage. Both occupants were killed.
Probable cause:
Loss of control during flight for undetermined reason(s).
Final Report:

Crash of a Cessna 402C in Keene: 2 killed

Date & Time: Feb 3, 1984 at 1713 LT
Type of aircraft:
Operator:
Registration:
N6814G
Flight Phase:
Survivors:
No
Site:
Schedule:
Concord - Morristown
MSN:
402C-0647
YOM:
1982
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
4300
Captain / Total hours on type:
3700.00
Aircraft flight hours:
368
Circumstances:
The pilot had filed an IFR flight plan; however, he took off in VFR conditions and did not activate the flight plan. Radar data showed that the latter part of the flight was flown at 6,300 feet, then at 1712:39 est, a descent was begun. One minute later, the flight was last recorded at 3,700 feet. Subsequently, the aircraft crashed near the top of a 3,165 feet mountain. The elevation of the crash site was about 3,000 feet. The terrain was rocky and covered with ice and snow when the investigators arrived at the crash site. Approximately 8 miles west-northwest at Keene, NH, the 1755 est weather was, in part, 3,200 feet broken, 5,500 feet overcast, visibility 10 miles, wind from 130° at 10 knots. The elevation of the Dillant-Hopkins Airport at Keene was 487 feet. Both occupants were killed.
Probable cause:
Occurrence #1: in flight encounter with weather
Phase of operation: cruise - normal
Findings
1. (f) weather condition - clouds
2. Descent - initiated - pilot in command
3. (f) weather condition - low ceiling
----------
Occurrence #2: in flight collision with terrain/water
Phase of operation: maneuvering
Findings
4. (f) light condition - dusk
5. (c) in-flight planning/decision - improper - pilot in command
6. (f) visual/aural detection - pilot in command
7. (f) terrain condition - high terrain
8. (c) proper altitude - not maintained - pilot in command
9. (f) terrain condition - mountainous/hilly
10. (f) terrain condition - snow covered
Final Report:

Crash of a Piper PA-31-350 Navajo Chieftain in Templeton: 3 killed

Date & Time: Jan 11, 1979 at 1110 LT
Operator:
Registration:
N33TN
Flight Phase:
Survivors:
No
Schedule:
Concord - White Plains
MSN:
31-7305050
YOM:
1973
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
12225
Captain / Total hours on type:
870.00
Circumstances:
While in cruising altitude in good weather conditions, en route from Concord to White Plains, the twin engine airplane collided with a Piper PA-60 Aerostar (Ted Smith Aerostar 600) owned by Northeast Cellulose Inc and registered N8011J. En route from Boston to Syracuse, it was carrying one passenger and one pilot. Following the collision, both aircraft entered a dive and crashed near Templeton. Both aircraft were destroyed and all five occupants were killed.
Probable cause:
In-flight collision with another aircraft after the pilot failed to see and avoid other traffic while cruising in an uncontrolled area.
Final Report:

Crash of a Rockwell Aero Commander 500 in Oakland

Date & Time: Feb 29, 1976 at 1150 LT
Registration:
N202Q
Flight Phase:
Survivors:
Yes
Site:
Schedule:
Concord - San Jose
MSN:
500-793
YOM:
1959
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
3346
Captain / Total hours on type:
684.00
Circumstances:
While cruising at low altitude in poor weather conditions, the twin engine airplane struck a hillside near Oakland. The aircraft was destroyed and all three occupants were seriously injured.
Probable cause:
The crew continued VFR flight into adverse weather conditions. The following contributing factors were reported:
- High obstructions,
- Low ceiling,
- Rain,
- Turbulences associated with clouds and thunderstorm activity,
- Fog.
Final Report:

Crash of a Cessna 402B in Greenville: 6 killed

Date & Time: May 11, 1973 at 1800 LT
Type of aircraft:
Operator:
Registration:
N2985Q
Survivors:
No
Schedule:
Concord - Greenville
MSN:
402B-0242
YOM:
1972
Crew on board:
2
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
6
Captain / Total flying hours:
4471
Captain / Total hours on type:
290.00
Circumstances:
The crew started the descent to Greenville Airport in poor weather conditions with fog and limited visibility. On final approach, the pilot-in-command passed below the glide and below the MDA fixed at 2,200 feet, probably to establish a visual contact with the ground. While descending to an altitude of 1,400 feet, the twin engine airplane struck trees and crashed in a wooded area located few miles short of runway. The aircraft was destroyed and all six occupants were killed.
Probable cause:
Improper IFR operation on part of the crew. The following factors were reported:
- High obstructions,
- Low ceiling, fog,
- Descended below MDA at 2,200 feet,
- Hit trees at 1,400 feet,
- Witnesses reported hillside was in fog about halfway up.
Final Report: