Zone

Crash of a Rockwell 690A Turbo Commander in Bullhead City

Date & Time: Mar 6, 2023 at 1945 LT
Registration:
N4PZ
Flight Type:
Survivors:
Yes
Schedule:
Plainview – Henderson
MSN:
690-11269
YOM:
1975
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
11095
Captain / Total hours on type:
3720.00
Aircraft flight hours:
6643
Circumstances:
The pilot reported that while enroute, a low fuel level annunciation occurred. The pilot subsequently prepared to divert to a nearby airport due to low fuel. Within 2 minutes the left engine shut down, followed by the right. The pilot asked air traffic control for vectors to the nearest airport. The sky conditions were clear with no moon, no horizon and no terrain feature visible. While approaching the airport at approximately 2,000 feet above the runway, the airport runway lighting turned off. The pilot was unable to turn the lights back on and subsequently used the terminal and ramp lights to maneuver the airplane to the runway. The airplane touched down and veered off the runway, which resulted in substantial damage to the fuselage. The pilot reported to a first responder that there were no pre accident mechanical failures or malfunctions with the airplane that would have precluded normal operation and that he ran out of gas.
Probable cause:
The pilot’s improper fuel planning for a cross-country flight, which resulted in fuel exhaustion, a total loss of engine power and subsequent impact with terrain.
Final Report:

Crash of a Piper PA-46-310P Malibu near Seligman: 2 killed

Date & Time: Sep 13, 2022 at 1100 LT
Registration:
N43605
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Albuquerque – Henderson
MSN:
46-8408052
YOM:
1984
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
47
Circumstances:
The student pilot was enroute at an altitude about 17,700 ft mean sea level (msl) on a crosscountry flight with a passenger in his high-performance airplane. The pilot was receiving visual flight rules flight following services from air traffic control, who advised him of an area of moderate to heavy precipitation at the airplane’s 12 o’clock position. The pilot replied that he had been able to “dodge” the areas of precipitation, but that they were getting bigger. There were no further communications from the pilot. Shortly thereafter, the airplane entered a left turn that continued through 180° before the airplane began a descent from its cruise altitude. The flight track ended in an area of moderate to extreme reflectivity as depicted on weather radar and indicated that the airplane was in a rapidly descending right turn at 13,900 ft when tracking information was lost. The wreckage was scattered across a debris field about 2 miles long. Examination of the wreckage revealed lateral crushing along the left side of the fuselage and the separation of both wings and the empennage. Wing spar signatures and empennage and wing impact marks suggested positive wing loading before the wing separation and in-flight breakup. The area of the accident site was included in a Convective SIGMET advisory for thunderstorms, hail, and wind gusts of up to 50 kts. A model atmospheric sounding near the accident site indicated clouds between about 15,000 ft and 27,000 ft, as well as the potential for light rime icing from 15,500 ft to 23,000 ft. Review of the pilot’s logbook revealed that he had about 47 total hours of flight experience, with about 4 hours of instruction in simulated instrument conditions. A previous flight instructor reported that the pilot displayed attitudes of “anti-authority” and “impulsivity.” Ethanol was detected in two postmortem tissue specimens; however, based on the distribution and amount detected, the ethanol may have been from postmortem production, and it is unlikely to have contributed to the crash. Fluoxetine, trazodone, and phentermine were also detected in the pilot’s postmortem toxicology specimens. The pilot had reported his use of fluoxetine for anger and irritability. Anger and irritability are nonspecific symptoms that may or may not be associated with mental health conditions, including depression, certain personality disorders, and bipolar disorder. These conditions may be associated with impulsive behavior, increased risk taking, lack of planning, not appreciating consequences of actions, and substance use disorders. Both trazodone and phentermine have the potential for impairing effects; however, an unimpaired pilot with the pilot’s relative inexperience would have been likely to lose aircraft control during an encounter with instrument meteorological conditions (IMC). It is therefore unlikely that the pilot’s use of trazodone and phentermine affected his handling of the airplane in a way that contributed to the crash. Based on review of the pilot’s Federal Aviation Administration (FAA) medical certification file, no specific conclusion can be drawn regarding any underlying psychiatric condition that may have contributed to his decision to attempt and continue the flight into IMC, as that decision was consistent with his previous pattern of risk-tolerant behavior. The pilot had not formally been diagnosed with a mental health disorder in his personal medical records reviewed other than substance use disorders. The psychological and psychiatric evaluations reviewed were not for diagnostic and treatment purposes, but for evaluation for FAA medical certification, and therefore did not generate diagnoses. There is evidence that the pilot had a pattern of poor decision-making, high-risk tolerance, and impulsive behavior. The circumstances of the accident are consistent with the student pilot’s decision to continue into an area of deteriorating weather conditions, his encounter with instrument meteorological conditions and convective activity, and loss of visual references, which resulted in spatial disorientation and a loss of aircraft control. During the descent, the airplane exceeded its design limitations, resulting in structural failure and an in-flight breakup.
Probable cause:
The student pilot’s continued visual flight into instrument meteorological conditions, which resulted in spatial disorientation, a loss of control, exceedance of the airplane’s design limitations, and in-flight breakup.
Final Report:

Crash of a Cessna 340 in Lytle Creek: 2 killed

Date & Time: Jan 18, 2010 at 1508 LT
Type of aircraft:
Registration:
N2217B
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Henderson – Compton
MSN:
340-0532
YOM:
1975
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
474
Aircraft flight hours:
3105
Circumstances:
The pilot was on a cross-country flight near mountainous terrain when he encountered clouds along the flight path. A comparison of recorded radar data and weather reports in the local area indicated that the pilot was maneuvering near the cloud bases in an area with low visibility and ceilings. Based on the erratic and circling flight path, it is likely that the pilot was having difficulty determining his location and desired flight track when the airplane collided with terrain. Post accident examination of the airframe and engine revealed no mechanical failures or malfunctions that would have precluded normal operation.
Probable cause:
The pilot’s loss of situational awareness while maneuvering under a cloud layer and failure to maintain sufficient clearance from mountainous terrain.
Final Report:

Crash of a Beechcraft E18S near Henderson: 4 killed

Date & Time: Jan 3, 1965 at 1445 LT
Type of aircraft:
Registration:
N208UB
Flight Phase:
Flight Type:
Survivors:
No
MSN:
BA-331
YOM:
1958
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
4341
Captain / Total hours on type:
174.00
Circumstances:
While in cruising altitude, the propeller blades on the left engine detached. Control was lost and the airplane dove into the ground and crashed in a lake located near Henderson. The aircraft was destroyed and all four occupants were killed.
Probable cause:
The left engine tearaway following the in-flight separation of the propeller blade due to fatigue fracture.
Final Report: