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Crash of a Cessna 340A in Tatum: 1 killed

Date & Time: Apr 19, 2021 at 1346 LT
Type of aircraft:
Registration:
N801EC
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Longview - Tatum
MSN:
340A-0312
YOM:
1977
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
28665
Captain / Total hours on type:
120.00
Aircraft flight hours:
6500
Circumstances:
The pilot was planning to perform a functional test of the airplane’s newly upgraded autopilot system. Automatic dependent surveillance-broadcast data showed that, after takeoff, the airplane turned east and climbed to 2,750 ft. Air traffic control information indicated that the controller cleared the pilot to operate under visual flight rules to the east of the airport. Communications between ground control, tower control, and the pilot were normal during the ground taxi, takeoff, and climb. Radio and radar communications were lost 6 minutes after takeoff, and no radio distress calls were received from the pilot. The airplane impacted wooded terrain about 3/4 mile to the east of the last recorded radar data point. Groundspeeds and headings were consistent throughout the flight with no abrupt deviations. The airplane impacted the wooded terrain in a nose-down, near-vertical flight attitude. Most of the airplane, including the fuselage, wings, and empennage, were consumed by a postimpact fire. Both engines and propellers separated from the airplane at impact with the ground. Examination of the engines revealed no preaccident failures or malfunctions that would have precluded normal operations. Both propellers showed signs of normal operation. Flight control continuity was confirmed. The elevator trim cables stop blocks were secured to the cables and undamaged. They were found against the forward stop meaning the trim tab was at full down travel (elevator leading edge full down) which indicated that the airplane was trimmed full nose up at impact. The airplane’s cabin sustained fragmentation from impact and was consumed by fire; as a result, the autopilot system could not be examined. The investigation was unable to determine why the pilot lost control of the airplane.
Probable cause:
The pilot’s loss of airplane control for undetermined reasons.
Final Report:

Crash of a Gulfstream GII in Little Rock: 7 killed

Date & Time: Jan 19, 1990 at 1710 LT
Type of aircraft:
Operator:
Registration:
N46TE
Survivors:
No
Schedule:
Longview - Little Rock
MSN:
243
YOM:
1979
Crew on board:
2
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
7
Captain / Total flying hours:
20000
Captain / Total hours on type:
160.00
Copilot / Total flying hours:
20000
Copilot / Total hours on type:
160
Aircraft flight hours:
5812
Circumstances:
During arrival, heavy rain showers were reported west of airport. At the airport, the weather was about 200 feet obscured with fog and drizzle, wnd was easterly at 5 to 7 knots. The pilots intended to land on runway 22, but after being told the wind was gusting to 27 knots, they elected to land on runway 04. The actual wind was not gusty. The erroneous gust indication was from a malfunction of the LLWAS. On final approach for an ILS runway 04 approach, the flight was advised the wind was from 030° at 5 knots and the RVR was 1,800 feet. Minimum RVR for the approach was 2,400 feet. The crew acknowledged; 22 seconds later, the ELT activated as the aircraft touched down 1,600 feet short of runway 04 and hit approach lighting system, railroad tracks and a fence. Investigations revealed the aircraft descended thru windshear. While maneuvering onto final approach; ground speed varied between 320 and 190 knots as aircraft was maneuvered thru tailwind to headwind near faf. CVR data verified a delay in descent from 4,000 feet to 1,900 feet before reaching faf and that the gear warning horn sounded before extension of gear and speed brakes. There was evidence of low engine rpm during impact, but no preimpact mechanical problem was found. Each pilot had over 10,000 hours of flight time, but only about 160 hours each in jet aircraft. All seven occupants were killed.
Probable cause:
Failure of the pilot-in-command to follow IFR procedures (maintain an ILS glide path or initiate a missed approach) during an ifr arrival to the airport. Factors related to the accident were:
- Unfavorable weather conditions,
- An erroneous wind indication from the low level windshear alert system (LLWAS), which resulted in an inaccurate weather (wind) observation, and
- Failure of the pilots to take adequate remedial action.
Final Report:

Crash of a Rockwell Grand Commander 690A in Nacogdoches: 2 killed

Date & Time: Sep 18, 1983 at 1955 LT
Operator:
Registration:
N111QL
Flight Type:
Survivors:
No
Schedule:
Oklahoma City – Longview – Nacogdoches
MSN:
690-11312
YOM:
1976
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
3310
Captain / Total hours on type:
135.00
Aircraft flight hours:
3077
Circumstances:
After transporting passengers from Longview, TX to Oklahoma City, OK and return to Longview, the aircraft was refueled for a flight back to Nacogdoches, TX, where the aircraft was based. About 12 min after takeoff, the pilot was cleared for an NDB approach to Nacogdoches and instructed to contact the Lufkin FSS for weather and current altimeter setting. During the NDB approach, the aircraft collided with trees, crashed and burned. An investigation revealed no evidence of either an engine or airframe failure or malfunction. Initial impact occurred with trees about 700 yards east of the NDB site. Initially, trees were cut in an upsloping manner where the terrain sloped upwards. Elevation of the crash site was 530 feet msl. The minimum descent altitude (MDA) was 900 feet msl. About 28 miles north, the 1955 cdt weather at Lufkin was, in part: 3,500 feet broken, visibility 5 miles. However, witnesses at Nacogdoches reported considerably lower ceilings, reduced visibility and some hilltops obscured by clouds. A pilot witness reported light rain, fog in the treetops. Reportedly, the airport was below minimums. Both occupants were killed.
Probable cause:
Occurrence #1: in flight encounter with weather
Phase of operation: approach - FAF/outer marker to threshold (IFR)
Findings
1. (f) preflight planning/preparation - inadequate - pilot in command
2. (f) light condition - dusk
3. (f) weather condition - low ceiling
4. (f) weather condition - fog
5. (f) weather condition - rain
6. (f) weather condition - below approach/landing minimums
----------
Occurrence #2: in flight collision with object
Phase of operation: approach - FAF/outer marker to threshold (IFR)
Findings
7. (c) IFR procedure - improper - pilot in command
8. (f) overconfidence in personal ability - pilot in command
9. (c) minimum descent altitude - not maintained - pilot in command
10. (f) object - tree(s)
----------
Occurrence #3: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Findings
11. Terrain condition - mountainous/hilly
Final Report:

Crash of a Beechcraft E18S in Longview: 1 killed

Date & Time: May 31, 1973 at 0200 LT
Type of aircraft:
Operator:
Registration:
N73JB
Flight Type:
Survivors:
No
Schedule:
Dallas - Longview
MSN:
BA-218
YOM:
1956
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
5600
Captain / Total hours on type:
2600.00
Circumstances:
On final approach to Longview Airport by night, the pilot encountered marginal weather conditions with limited visibility. On final, the twin engine airplane struck trees and crashed in flames 1,75 mile short of runway threshold. The aircraft was destroyed and the pilot was killed.
Probable cause:
Collision with trees on final approach after the pilot misjudged distance and altitude. The following factors were reported:
- High obstructions,
- Pilot fatigue,
- Hit trees 32 feet agl 1,75 mile from airport,
- Pilot had landing lights on and gear down.
Final Report: