Zone

Crash of a Piper PA-31P Pressurized Navajo in Mosby: 1 killed

Date & Time: Jul 20, 2023 at 0935 LT
Type of aircraft:
Registration:
N200RA
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Mosby - Wichita
MSN:
31-7400198
YOM:
1974
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
Shortly after takeoff from Mosby-Midwest National Air Center Airport, the twin engine airplane collided with high tension cables and crash landed in a soybean field, bursting into flames. The airplane was destroyed by a post crash fire and the pilot, sole on board, was killed.

Crash of a Cessna 414 Chancellor in Benton: 2 killed

Date & Time: Feb 16, 2008 at 1845 LT
Type of aircraft:
Operator:
Registration:
N41LP
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Benton - Wichita
MSN:
414-0491
YOM:
1980
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
565
Captain / Total hours on type:
52.00
Aircraft flight hours:
6656
Circumstances:
According to witnesses, the airplane departed runway 35 and was observed flying in and out of the clouds. Several of the witnesses observed the airplane initiate a turn to the west. One witnesses commented that it was dark but he could still see the silhouette of the airplane. He observed the airplane descend below the trees. All of the witnesses reported flames and "fireballs." On scene evidence was consistent with the airplane impacting trees in a left turn. The airplane was destroyed. An examination of the airplane, flight controls, engines, and remaining systems revealed no anomalies. Weather observations and radar data depicted low clouds, and restricted visibility due to rain and mist, in the vicinity of the airport. Toxicological examination revealed cetirizine, an antihistamine, consistent with use within the previous 12 hours. Most studies have not found any significant impairment from the medication, though it is reported to cause substantial sedation in some individuals.
Probable cause:
The pilot's failure to maintain clearance from the trees. Contributing to the accident was the pilot's flight into known adverse weather conditions and the low clouds and visibility.
Final Report:

Crash of a Beechcraft H18 in Great Bend: 1 killed

Date & Time: Feb 9, 2007 at 0850 LT
Type of aircraft:
Registration:
N45GM
Flight Type:
Survivors:
No
Schedule:
Wichita - Great Bend
MSN:
BA-717
YOM:
1965
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
3250
Captain / Total hours on type:
125.00
Aircraft flight hours:
7702
Circumstances:
Prior to the flight, the pilot obtained a weather briefing which included an AIRMET for IFR conditions and an AIRMET for icing that was "just off to the north." According to air traffic control (ATC) information, the en route portion of the flight was uneventful. ATC cleared the pilot for an ILS approach to runway 35, and the pilot acknowledged the approach clearance. When the airplane reached the outer marker ATC approved the pilot for a frequency change to the common traffic advisory frequency. The pilot acknowledged the frequency change, and no further communications were received from the pilot by ATC. Witnesses observed the airplane approximately 200 feet above ground level (agl) on a northwesterly heading, west of runway 35. The airplane then entered a climbing left turn to the south and disappeared into the overcast cloud layer. Shortly thereafter, the witness observed the airplane in a "20 degree nose down, wings level attitude" on a southeasterly heading. The witness then lost sight of the airplane due to hangars obstructing his view. At the time of the accident, the witness stated that the ceiling was approximately 500 foot overcast with mist. The published missed approach procedure instructed the pilot to initiate a climbing left turn to a fix and hold. Examination of the accident site revealed the airplane impacted the terrain in a right wing, nose-low attitude. No ground impact marks were noted except in the immediate vicinity of the wing leading edges, engines, and propeller assemblies. The flaps and landing gear were in the extended position. The leading edge surfaces of the vertical and horizontal stabilizers revealed 1/4 to 1/2 inches of clear ice. The upper fuselage antenna displayed 1/4 to 1/2 inches of clear ice. Local authorities reported observing a "layer of ice" on the leading edges of both wings when they arrived to the accident site. Examination of the airframe and engines revealed no anomalies that would have precluded normal operations.
Probable cause:
The pilot's failure to maintain aircraft control during the missed approach which resulted in an inadvertent stall and impact with terrain. A contributing factor was the icing conditions.
Final Report:

Crash of a Beechcraft 1900C in Eagleton: 3 killed

Date & Time: Dec 9, 2002 at 1140 LT
Type of aircraft:
Operator:
Registration:
N127YV
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Wichita - Mena
MSN:
UC-127
YOM:
1990
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
10200
Aircraft flight hours:
12473
Circumstances:
The aircraft collided with mountainous terrain in a level descent during a visual approach to the destination airport. According to recorded radar data, 10 minutes after descending from 15,000 feet, the flight impacted about 200 feet below the top of the partially obscured ridgeline (elevation of 2550 feet), and 8 miles from the destination. The data indicates the flight path was similar to the global positioning satellite (GPS) approach to the airport. Six minutes before the accident, and the pilot's last transmission to air traffic control, he was informed and acknowledged that radar service was terminated. The flight was 12.4 miles from the accident site when radar contact was lost. Reduced visibility due to fog hampered search & rescue efforts, and the aircraft wreckage was located the next day. The aircraft was equipped with a GPS navigation system; however the installation was incomplete, restricting its use to visual flight rules (VFR) only. The investigation did not determine if the GPS was being used at the time. A non-enhanced Ground Proximity Warning System was also installed. The maximum elevation figure listed on the sectional aeronautical chart covering the area of the accident site and destination airport was 3000 feet mean sea level. The chart also shows an advisory for the area to use caution due to rapidly rising.
Probable cause:
In-flight collision with terrain due to the pilot's failure to maintain clearance and altitude above rapidly rising terrain while on a VFR approach. Contributing factors were the obscuration of the terrain due to clouds.
Final Report:

Crash of a Rockwell Sabreliner 75 near Florence: 2 killed

Date & Time: Jul 18, 1998 at 1622 LT
Type of aircraft:
Registration:
N547JL
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Newton - Wichita
MSN:
380-69
YOM:
1979
Location:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
10000
Copilot / Total flying hours:
478
Copilot / Total hours on type:
14
Aircraft flight hours:
5484
Circumstances:
The pilot dropped off a passenger at Newton Airport before continuing the flight. The passenger, who was a contract pilot for the company, reported there had been no indications of any problem with the airplane. The pilot conducted a low pass followed by a steep climb to 10,000 feet when he departed Newton. Seven minutes later in the flight, the cockpit voice recorder revealed the pilot stating, 'You're going to pitch up now and take it all the way around here.' The pilot said, 'Pitch up, twenty degrees up.' After the pilot called for the nose to be pitched up, he did not make any statements for about 27 seconds. Then the pilot stated, 'Oh, Jim.' Eight seconds later the airplane impacted the ground. Radar data indicated that airplane's altitude about the time the nose was pitched up was 15,900 feet msl, and it impacted the ground about 37 seconds later. All flight control surfaces were found at the impact site. No maneuver in the pilot's manual or the FAA's Commercial test guide required the nose to be pitched up 20 degrees while maintaining 250 knots. The aircraft was certified as a Transport Category aircraft and was not certified for aerobatic flight.
Probable cause:
The pilot's overconfidence in his personal ability, his improper in-flight decision to attempt aerobatics, and his loss of control of the airplane.
Final Report:

Crash of a Rockwell Aero Commander 500 in Silica: 1 killed

Date & Time: Jul 31, 1991 at 0759 LT
Operator:
Registration:
N904DF
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Wichita - Hays
MSN:
500-1057-46
YOM:
1961
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
3358
Captain / Total hours on type:
724.00
Aircraft flight hours:
11546
Circumstances:
Both aircraft departed Wichita on IFR flight plan in VFR weather conditions. They flew northwest toward their respective destinations, and cancelled IFR about 20 minutes before the accident. ATC observed the airplanes on radar, and stated they were 'dogfighting back and forth' prior to the collision. One pilot's roommate reported the two pilots, who were close friends as well as co-workers, often cancelled IFR and flew in formation if the weather was VFR. He reported the pilots often videotaped each other, and he had watched some of the tapes. He stated 'it was hard to tell from the videotape how close they were because they could use the zoom feature, etc. You could read the N numbers.' Investigation revealed brown paint transfer on the bottom of the right wing of the blue and white airplane, which had separated and was located 1.5 miles from the main wreckage. There were light colored scuff marks on the top of the left engine nacelle of the brown and white airplane. Both aircraft and both pilots were killed.
Probable cause:
The failure of both pilots to maintain adequate separation during formation flight. Related factors are overconfidence in personal ability and poor planning/decision.
Final Report:

Crash of a Rockwell Aero Commander 500 in Silica: 1 killed

Date & Time: Jul 31, 1991 at 0759 LT
Operator:
Registration:
N702CA
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Wichita - Great Bend
MSN:
500-1298-113
YOM:
1963
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
1590
Captain / Total hours on type:
322.00
Aircraft flight hours:
12747
Circumstances:
Both aircraft departed Wichita on IFR flight plan in VFR weather conditions. They flew northwest toward their respective destinations, and cancelled IFR about 20 minutes before the accident. ATC observed the airplanes on radar, and stated they were 'dogfighting back and forth' prior to the collision. One pilot's roommate reported the two pilots, who were close friends as well as co-workers, often cancelled IFR and flew in formation if the weather was VFR. He reported the pilots often videotaped each other, and he had watched some of the tapes. He stated 'it was hard to tell from the videotape how close they were because they could use the zoom feature, etc. You could read the N numbers.' Investigation revealed brown paint transfer on the bottom of the right wing of the blue and white airplane, which had separated and was located 1.5 miles from the main wreckage. There were light colored scuff marks on the top of the left engine nacelle of the brown and white airplane. Both aircraft and both pilots were killed.
Probable cause:
The failure of both pilots to maintain adequate separation during formation flight. Related factors are overconfidence in personal ability and poor planning/decision.
Final Report:

Crash of a Rockwell Aero Commander 500B in Garden City: 1 killed

Date & Time: Jan 19, 1988 at 1946 LT
Registration:
N611CA
Flight Type:
Survivors:
No
Schedule:
Garden City - Wichita
MSN:
500-0922-7
YOM:
1960
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
2125
Captain / Total hours on type:
58.00
Aircraft flight hours:
6713
Circumstances:
The aircraft departed Garden City under extremely poor weather conditions. More than half way to Dodge City, the pilot reported engine problems to Kansas City (ARTCC). Vectors were provided to the Dodge City Airport, but the pilot did not maintain assigned headings. The aircraft headed back towards Garden City to attempt an instrument approach. Radar vectors were provided for the localizer approach. Radar indicated that the aircraft did not become stabilized on the approach. There was a significant loss of ground speed as the pilot was attempting to get established on the localizer. Radar contact was lost about 2 miles from the airport at a speed approaching stall speed for this aircraft. The aircraft crashed about 2 miles short and to the right of course. The aircraft impacted in a vertical nose down attitude on heading which indicated a turn away from the airport. The left prop was found in the feather position. No mechanical problem was discovered. The right engine appeared to be producing full power at impact. The pilot, sole on board, was killed.
Probable cause:
Occurrence #1: loss of engine power (partial) - nonmechanical
Phase of operation: cruise - normal
Findings
1. 1 engine
2. (c) powerplant - undetermined
3. Propeller feathering - performed - pilot in command
4. (f) light condition - dark night
----------
Occurrence #2: loss of control - in flight
Phase of operation: approach - faf/outer marker to threshold (ifr)
Findings
5. (f) proper alignment - not maintained - pilot in command
6. (f) missed approach - not performed - pilot in command
7. (c) airspeed (vmc) - not maintained - pilot in command
8. (c) stall - inadvertent - pilot in command
----------
Occurrence #3: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Findings
9. Terrain condition - frozen
10. (f) lack of total experience in type of aircraft - pilot in command
Final Report:

Crash of a Cessna 425 Conquest in Newburgh: 1 killed

Date & Time: Dec 12, 1983 at 1856 LT
Type of aircraft:
Registration:
N6774R
Survivors:
No
Schedule:
Wichita - White Plains
MSN:
425-0045
YOM:
1981
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
8636
Captain / Total hours on type:
26.00
Aircraft flight hours:
291
Circumstances:
During arrival, there were indefinite delays at White Plains, NY, so the pilot diverted to Newburgh, NY. He was vectored for an ILS runway 09 approach. While en route, the pilot requested and was given the ILS frequency, minimums for the approach, the airport elevation (491 feet msl), the Newburgh weather and the frequency for the outer compass locator (even tho, current approach charts were on board). He was cleared for the approach, but the aircraft hit trees and crashed, 2.58 miles west of runway 09. Elevation of the crash site was about 580 feet. The minimum descent altitude (MDA) for the approach was 682 feet. An exam of the wreckage revealed no preimpact part malfunction or failure. The pilot was required to wear lenses to correct his vision. The area forecast called for icing, turbulence, low level wind shear, low ceilings, rain, drizzle, fog and a chance of light freezing rain/drizzle. Reportedly the pilot received a full weather briefing, but was not briefed on sigmets Juliett 7 and Lima 4 which called for moderate to severe turbulence and low level wind shear and occasional moderate to severe mixed/clear icing in clouds and precipitations below 8,000 feet.
Probable cause:
Occurrence #1: in flight encounter with weather
Phase of operation: approach
Findings
1. Preflight briefing service - improper - ATC personnel (FSS)
2. Flight into known adverse weather - performed - pilot in command
3. (f) approach aids - congested
4. Initiated - pilot in command
5. (f) light condition - dark night
6. (f) weather condition - icing conditions
7. (f) weather condition - turbulence
8. (f) weather condition - low ceiling
9. (f) weather condition - rain
10. (f) weather condition - fog
11. (f) weather condition - unfavorable wind
12. (f) weather condition - windshear
----------
Occurrence #2: in flight collision with terrain/water
Phase of operation: approach - faf/outer marker to threshold (IFR)
Findings
13. (c) IFR procedure - improper - pilot in command
14. (f) lack of total experience in type of aircraft - pilot in command
Final Report:

Crash of a Cessna 404 Titan in Belton: 1 killed

Date & Time: Jun 30, 1981 at 1125 LT
Type of aircraft:
Operator:
Registration:
N6810N
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Wichita - Wichita
MSN:
404-0853
YOM:
1981
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
6500
Captain / Total hours on type:
500.00
Circumstances:
The pilot, sole on board, departed Wichita on a test flight. En route, the twin engine airplane entered a steep descending turn then crashed in a field located in Belton, south of Kansas City, Missouri. The aircraft was destroyed and the pilot was killed.
Probable cause:
Uncontrolled descent and subsequent crash due to pilot incapacitation. The following contributing factors were reported:
- Moderate obese pilot,
- High blood pressure,
- Witnesses reported pilo looked tired,
- Speech slurred.
Final Report: