Crash of a Beechcraft TC-45J Expeditor in Kansas City: 1 killed

Date & Time: Dec 5, 1983 at 1710 LT
Type of aircraft:
Operator:
Registration:
N704M
Flight Type:
Survivors:
No
Schedule:
Quincy – Kansas City
MSN:
5495
YOM:
1942
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
3200
Aircraft flight hours:
20776
Circumstances:
The aircraft was a Beech TC-45J that had been modified into a Hamilton Turboliner under STC SA-1821-WE. During arrival, the pilot reported that he encountered moderate icing at 4,000 feet. He made a localizer-only approach to runway 35. An ATC specialist stated that they saw the aircraft break out of the clouds over the approach end of the runway. At about that time, the pilot transmitted that he was going to enter a left base turn for runway 35 and that he had the runway in sight. He started a turn, and shortly thereafter, the aircraft enter a steep nose down attitude. The aircraft impacted in a railroad yard in a relatively level attitude with the landing gear extended and the wing flaps retracted. However, during impact, it was still descending at a steep angle (estimated approximately 30°). It was destroyed by impact and ground fire. No preimpact, mechanical failure or malfunction was found. The minimum ceiling and visibility for a straight-in approach were 500 feet and one mile, and for a circling approach, the minimums were 700 feet and one mile. The pilot, sole on board, was killed.
Probable cause:
Occurrence #1: in flight encounter with weather
Phase of operation: approach
Findings
1. (f) flight into known adverse weather - continued - pilot in command
2. (f) weather condition - low ceiling
3. (f) weather condition - rain
4. (f) weather condition - icing conditions
5. (f) weather condition - fog
6. (f) weather condition - below approach/landing minimums
7. (f) not performed - pilot in command
----------
Occurrence #2: loss of control - in flight
Phase of operation: circling (IFR)
Findings
8. Go-around - initiated - pilot in command
9. Maneuver - initiated - pilot in command
10. (c) airspeed - inadequate - pilot in command
11. (c) stall - inadvertent - pilot in command
----------
Occurrence #3: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Final Report:

Crash of a Beechcraft 60 Duke in Wichita

Date & Time: Sep 29, 1983 at 1720 LT
Type of aircraft:
Registration:
N7277R
Survivors:
Yes
Schedule:
Wichita – Grand Rapids
MSN:
P-318
YOM:
1975
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
3600
Captain / Total hours on type:
60.00
Aircraft flight hours:
1100
Circumstances:
Shortly after takeoff, the left engine began to progressively lose power and was shut down. The aircrew notified Beech Tower of the problem and reported they would like to return and land. The aircraft was observed on final approach to runway 18 with the gear extended and the left prop stopped. Before landing, the aircraft began veering to the left. It crossed over the end of the airport at about 40 feet agl and 300 feet left (east) of the runway. The left wing and nose dropped and the aircraft impacted the ramp, left wing first. The aircraft then skidded across the ramp on a heading of 160° and collided with and damaged three other aircraft; a Beechcraft F33A registered N1833S; another Beechcraft 60 Duke registered N6747D and a Beechcraft 58 registered N5800B. An investigation revealed that the #2 exhaust valve lifter had become flat and the #2 exhaust valve had failed from fatigue. Both pilots escaped uninjured.
Probable cause:
Occurrence #1: loss of engine power (total) - mech failure/malf
Phase of operation: climb - to cruise
Findings
1. (c) engine assembly, valve,intake - other
2. (c) engine assembly, valve,intake - fatigue
3. Propeller feathering - performed - pilot in command
4. Performed - pilot in command
----------
Occurrence #2: in flight collision with terrain/water
Phase of operation: landing - flare/touchdown
Findings
5. Precautionary landing - performed - pilot in command
6. (c) airspeed (VMC) - not maintained - pilot in command
Final Report:

Crash of a Cessna 500 Citation I in Wichita

Date & Time: Apr 26, 1983 at 1454 LT
Type of aircraft:
Operator:
Registration:
N22FM
Flight Phase:
Survivors:
Yes
Schedule:
Wichita - Chicago
MSN:
500-0229
YOM:
1974
Crew on board:
2
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
6725
Captain / Total hours on type:
2300.00
Aircraft flight hours:
4112
Circumstances:
The aircraft collided with the ground during takeoff. The fuel tank in the right wing ruptured and the aircraft burned while sliding to a stop. The day before the accident the aircraft was washed and the thrust reverser doors were polished. After the service, the reverser doors circuit breakers which had been pulled were not reset. It was company policy to leave circuit breakers out that were pulled during servicing. Prior to flight, the aircraft was loaded and the engines started. The reversed unlock lights on both reverser annunciator panels illuminated. The pilot discussed the situation with the copilot and elected to go. He pushed the light assemblies which unlatched the light housing and put out the 'unlock' lights. After takeoff while the gear was retracting the aircraft yawed right and impacted the ground. All occupants evacuated and after the fire was put out a Cessna Aircraft investigator observed the two thrust reverser circuit breakers in the 'out', open position and partially covered by a flight chart. Both thrust reversers were deployed.
Probable cause:
Occurrence #1: loss of control - in flight
Phase of operation: takeoff - initial climb
Findings
1. (c) thrust reverser,door - unlocked
2. (c) maintenance - inadequate - company maintenance personnel
3. (c) thrust reverser,door - deployed inadvertently
4. (c) aircraft preflight - inadequate - pilot in command
5. (c) electrical system,circuit breaker - popped/tripped
6. (c) operation with known deficiencies in equipment - attempted - pilot in command
7. (c) annunciator panel light(s) - switched off
8. (c) checklist - not followed - pilot in command
----------
Occurrence #2: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Final Report:

Crash of a Cessna 501 Citation I in Wichita

Date & Time: Nov 12, 1982 at 1404 LT
Type of aircraft:
Operator:
Registration:
N2627U
Flight Type:
Survivors:
Yes
Schedule:
Wichita - Wichita
MSN:
501-0247
YOM:
1982
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Aircraft flight hours:
179
Circumstances:
A non-pilot mechanic employed at the manufacturer's facility took off in the aircraft. The aircraft was observed entering a very steep climb and appeared to stall. The nose was lowered and the aircraft turned left and entered a downwind leg to runway 01R. It then turned onto a low base leg and continued to a very low final. After several oscillations in roll the aircraft touched down 557 feet short of the runway and collided with approach light stanchions. The mechanic had been and was, at the time of the accident, under psychiatric care (schizophrenia).
Probable cause:
Occurrence #1: loss of control - in flight
Phase of operation: approach - VFR pattern - final approach
Findings
1. (c) aircraft handling - improper - unqualified person
2. (f) stolen aircraft/unauthorized use - intentional - unqualified person
----------
Occurrence #2: in flight collision with object
Phase of operation: landing - flare/touchdown
Findings
3. Object - approach light/navaid
Final Report:

Crash of a Cessna 402A in Kansas City: 1 killed

Date & Time: Jan 21, 1982 at 1924 LT
Type of aircraft:
Registration:
N4553Q
Flight Type:
Survivors:
No
Schedule:
Springdale - Kansas City
MSN:
402-0053
YOM:
1979
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
5993
Captain / Total hours on type:
1200.00
Aircraft flight hours:
3746
Circumstances:
The pilot received two weather briefings. Most of the first briefing was spend finding an alternate. The forecast include IMC with low ceilings, low visibilities with light snow, fog and possible freezing drizzle. The aircraft was not certificated for flight in known icing conditions. During arrival, the plane entered an overcast at 3,500 feet MSL. Two minutes later, the pilot reported and encounter with freezing precipitation. The first approach was abandoned in the vicinity of the FAF/outer marker after the pilot flew through the localizer course line and was half mile to the right. He was vectored for another ILS approach. While inbound on the approach, he was informed that approach control had received a low altitude alert. He was reminded that his altitude should be 2,600 feet until reaching the FAF; however, he reached only 2,400 feet. His airspeed was much higher than normal while descending from the FAF. The plane struck a building and burned about 1/3 mile northeast of the end of runway 18. The pilot, sole on board, was killed.
Probable cause:
In flight encounter with weather during approach - FAF/outer marker to threshold (IFR), loss of control and subsequent collision with object. The following findings were reported:
- Dark night,
- Low ceiling,
- Fog,
- Snow,
- Rain,
- Icing conditions,
- Wing ice,
- The pilot initiated operation with known deficiencies in equipment,
- Overconfidence in aircraft's ability on part of the pilot,
- The pilot continued flight into known adverse weather,
- Overconfidence in personal ability on part of the pilot,
- Non residential building.
Final Report:

Crash of a Rockwell Aero Commander 685 in Kansas City: 4 killed

Date & Time: Sep 4, 1981 at 1645 LT
Registration:
N777MM
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Kansas City - Rapid City
MSN:
685-12030
YOM:
1973
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
4640
Circumstances:
After takeoff from Kansas City Airport, while climbing, the airplane suffered an engine failure. The airplane lost height and entered a spin then crashed in a field, bursting into flames. All four occupants were killed.
Probable cause:
Stall and subsequent crash after engine structure failed. The following contributing factors were reported:
- Lack of lubrication - specifica part, not system,
- Oil starvation,
- The pilot failed to follow approved procedures,
- Improper emergency procedures,
- Inadequate preflight preparation,
- Improperly loaded aircraft,
- Complete engine failure one engine,
- N° 4, 5, 6 main engine bearings, n°1, 2, 6 rod bearings and front prop shaft bearing failed,
- Approximately 400 lbs over max gross weight.
Final Report:

Crash of a Beechcraft H18 in Olathe: 1 killed

Date & Time: Feb 15, 1980 at 1528 LT
Type of aircraft:
Registration:
N729F
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Olathe - Iola
MSN:
BA-706
YOM:
1964
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
3566
Captain / Total hours on type:
1647.00
Circumstances:
The pilot departed Iola Airport in poor weather conditions on a cargo flight to Olathe-Johnson County Airport. En route, communication systems (transmitter/receiver) failed and on approach, the pilot lost control of the airplane that stalled and crashed in a field. The aircraft was destroyed and the pilot, sole on board, was killed.
Probable cause:
Stall and subsequent crash after the pilot initiated flight in adverse weather conditions. The following contributing factors were reported:
- Airframe ice,
- Communications and navigation equipment: transmitters and/or receivers,
- Communications failure,
- Low ceiling,
- Snow,
- Icing conditions including sleet, freezing rain,
- Visibility half a mile or less,
- Lost radio transmitter,
- Destination NDB/ILS glideslope inoperative,
- Low visibility on approach,
- Ice on wings and stabilizers.
Final Report:

Crash of a Mitsubishi MU-2B-10 Marquise in Hays: 7 killed

Date & Time: Aug 3, 1979 at 2125 LT
Type of aircraft:
Registration:
N208MA
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Salina - Denver
MSN:
16
YOM:
1967
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
7
Captain / Total flying hours:
2168
Captain / Total hours on type:
140.00
Circumstances:
En route from Salina to Denver, the pilot informed ATC about an engine failure and elected to divert to the nearest airport. The airplane lost height and eventually stalled and crashed in Hays. The aircraft was destroyed and all seven occupants were killed.
Probable cause:
Engine failure during normal cruise and subsequent stall due to compressor assembly bearing failure. The following contributing factors were reported:
- Material failure,
- Improper in-flight decisions,
- Failed to maintain flying speed,
- Complete failure one engine,
- Forward main shaft bearing failed.
Final Report:

Crash of a Mitsubishi MU-2B-10 Marquise in Gardner

Date & Time: Apr 9, 1979 at 1350 LT
Type of aircraft:
Registration:
N251M
Survivors:
Yes
Schedule:
Iola - Kansas City
MSN:
013
YOM:
1967
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
1657
Captain / Total hours on type:
908.00
Circumstances:
En route from Iola to Kansas City, the crew encountered engine problems and was cleared to divert to Gardner Municipal Airport. On approach, both engines failed, forcing the crew to attempt an emergency landing. The airplane crash landed one mile west of the airfield. All three occupants escaped with minor injuries.
Probable cause:
Controlled collision with ground due to double engine failure. The following contributing factors were reported.
- Poor ground servicing,
- Water in fuel,
- Complete failure of both engines,
- Forced landing off airport on land,
- Fuel truck contaminated with water.
Final Report:

Crash of a Cessna 414 Chancellor in Arlington

Date & Time: Feb 7, 1979 at 1330 LT
Type of aircraft:
Operator:
Registration:
N141WB
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Wichita - Wichita
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
9201
Captain / Total hours on type:
31.00
Circumstances:
The pilot, sole on board, departed Wichita Airport on a local test flight, accompanied by a second aircraft. Both aircraft were visually checking each others underside when they collided in flight. Out of control, they crashed in a field located in Arlington, Kansas. Both pilots were injured, the one on board the Chancellor critically.
Probable cause:
In-flight collision during normal cruise after the pilot failed to maintain adequate separation. The following contributing factors were reported:
- Pilot of other aircraft,
- Not under radar contact,
- No control area.
Final Report: