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Crash of a BAe 125-700A near Beaumont: 3 killed

Date & Time: Sep 20, 2003 at 1854 LT
Type of aircraft:
Operator:
Registration:
N45BP
Flight Type:
Survivors:
No
Schedule:
Houston - Beaumont
MSN:
257026
YOM:
1978
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
5230
Captain / Total hours on type:
3521.00
Copilot / Total flying hours:
3817
Copilot / Total hours on type:
2684
Aircraft flight hours:
9781
Aircraft flight cycles:
7098
Circumstances:
The purpose of the flight was for the instructor-pilot to prepare the first and second pilots for their FAA Part 135 competency and proficiency checks scheduled to be conducted in the accident airplane the following week, with operator proving tests to follow shortly thereafter. The first pilot obtained a computer science corporation (CSC) direct user access terminal service (DUATS) weather briefing and filed an instrument flight rules (IFR) flight plan. The instructor-pilot was listed as the pilot-in-command. The airplane took off and proceeded to its designated practice area. According to the cockpit voice recorder (CVR), the pilots practiced various maneuvers under the direction of the instructor-pilot, including steep turns and approaches to stalls. Then the first pilot was asked the to demonstrate an approach-to-landing stall. The first pilot asked the instructor-pilot if he had "ever done stalls in the airplane?" The instructor-pilot replied, "It's been awhile." The first pilot remarked, "This is the first time I've probably done stalls in a jet. Nah, I take that back, I've done them in a (Lear)." The instructor pilot said he had stalled "the JetStar on a [FAR] one thirty five ride." Flaps were extended and the landing gear was lowered. Digital electronic engine control (DEEC) recorded a power reduction that remained at idle. According to national track analysis program (NTAP) data, the stall was initiated from an altitude of 5,000 feet. The stick shaker sounded and shortly thereafter, the recording ended. The consensus of 25 witness' observations was that the airplane was flying at low altitude and doing "erratic maneuvers." One witness said it "seemed to stop in midair," then pitched nose down. Some witnesses said that the airplane was spinning. Other witnesses said it was in a flat spin. Still another witness said the airplane fell "like a falling leaf." The airplane impacted marshy terrain in a nose-down, wings-level attitude. Wreckage examination revealed the landing gear was down and the flaps were set to 25 degrees. Both engines' compressor/turbine section blades were gouged and bent in the opposite direction of rotation, and there were rotational scoring marks on both cases. No discrepancies were noted.
Probable cause:
The first pilot's failure to maintain aircraft control and adequate airspeed. Contributing factors included performing intentional stalls at too low an altitude to afford a safe recovery, the pilot's failure to add power in an attempt to recover, and the flight instructor's inadequate supervision of the flight.
Final Report:

Crash of an Embraer ERJ-145 in Beaumont

Date & Time: Feb 11, 1998 at 1216 LT
Type of aircraft:
Operator:
Registration:
N14931
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Beaumont - Beaumont
MSN:
145-013
YOM:
1997
Flight number:
CO910
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
10800
Captain / Total hours on type:
800.00
Copilot / Total flying hours:
1932
Copilot / Total hours on type:
15
Aircraft flight hours:
1844
Aircraft flight cycles:
1472
Circumstances:
The pilot-in-command (PIC) was administering a proficiency check flight to the first officer (FO) in a regional jet. One of the required check items was the loss of an engine at "V1" speed. While on takeoff roll with the FO at the controls, the PIC retarded the left engine throttle to idle when "V1" speed was attained. The FO called, "check max thrust," and then called, "positive rate gear up." As the PIC reached for the gear lever, he noticed the airplane roll to the left at a rate which he felt was "excessive and dangerous." He then reached for the flight controls and felt the left rudder "go all the way to the floor." As the PIC took control of the airplane, he applied full right rudder and right aileron. The airplane began recovering from the bank and impacted the ground. Flight recorder data revealed that the time interval between the throttle retarded to idle and ground impact was about 8 seconds. The data showed that the airplane became airborne about 2 seconds after the throttle was retarded, and that the airplane had rolled to a 71 degree left bank within 6 seconds from the throttle reduction. Ground scars and wreckage distribution revealed that the left wing had contacted the ground first and then the right wing prior to the airplane coming to rest. The FO had a total of 15 hours in the type aircraft in the last 90 days. Examinations of the airframe, engines, and flight control system did not reveal any anomalies that could have contributed to the accident. Company flight training policy stated that all check airmen should be ready to take control of the airplane while practicing these types of training maneuvers.
Probable cause:
The first officer's improper use of the rudder when given a simulated engine failure on takeoff and the pilot-in-command's delayed remedial action which resulted in a loss of control. A factor was the first officer's lack of experience in the regional jet airplane.
Final Report:

Crash of a Beechcraft Queen Air 65 in Beaumont: 7 killed

Date & Time: Apr 28, 1968 at 0015 LT
Type of aircraft:
Operator:
Registration:
N968Q
Flight Type:
Survivors:
No
MSN:
LC-120
YOM:
1962
Crew on board:
1
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
7
Captain / Total flying hours:
4900
Captain / Total hours on type:
40.00
Circumstances:
While on a night approach to Beaumont-Jack Brooks Airport, the twin engine aircraft struck the ground and crashed few miles short of runway. The aircraft was totally destroyed and all seven occupants were killed.
Probable cause:
Investigations were unable to determine the cause of the accident.
Final Report: