Crash of a Cessna 402B in Greenville: 6 killed

Date & Time:
Type of aircraft:
Operator:
Registration:
N2985Q
Survivors:
No
Schedule:
Concord - Greenville
MSN:
402B-0242
YOM:
1972
Crew on board:
2
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
6
Captain / Total flying hours:
4471
Captain / Total hours on type:
290.00
Circumstances:
The crew started the descent to Greenville Airport in poor weather conditions with fog and limited visibility. On final approach, the pilot-in-command passed below the glide and below the MDA fixed at 2,200 feet, probably to establish a visual contact with the ground. While descending to an altitude of 1,400 feet, the twin engine airplane struck trees and crashed in a wooded area located few miles short of runway. The aircraft was destroyed and all six occupants were killed.
Probable cause:
Improper IFR operation on part of the crew. The following factors were reported:
- High obstructions,
- Low ceiling, fog,
- Descended below MDA at 2,200 feet,
- Hit trees at 1,400 feet,
- Witnesses reported hillside was in fog about halfway up.
Final Report:

Crash of a Beechcraft C-45G Expeditor in Sarasota

Date & Time:
Type of aircraft:
Operator:
Registration:
N7697C
Flight Type:
Survivors:
Yes
Schedule:
Kingston - Tampa
MSN:
AF-404
YOM:
1953
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
7226
Captain / Total hours on type:
100.00
Circumstances:
While cruising along the west coast of Florida on a cargo flight from Kingston to Tampa, the pilot informed ATC about an engine fire and elected to divert to Sarasota-Bradenton Airport for an emergency landing. On approach, the pilot realized he could not make it so he landed the airplane in a prairie. The aircraft rolled for few dozen yards before coming to rest in flames. While the pilot escaped uninjured, the aircraft was destroyed by fire.
Probable cause:
Engine fire in flight and precautionary landing off airport. Fire after impact. The pilot executed a wheels down landing. The cause of fire described as whitish in colour could not be determined.
Final Report:

Crash of a Curtiss C-46A-55-CK Commando at Ellington AFB

Date & Time:
Type of aircraft:
Operator:
Registration:
N446M
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Ellington - Miami
MSN:
133
YOM:
1944
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
After takeoff from Ellington AFB, while climbing, the crew informed ATC about technical problems with the right engine and elected to return for an emergency landing. The captain realized this was not possible and attempted an emergency landing along the I-45 highway. The airplane belly landed and slid for several yards before coming to rest. While both pilots escaped uninjured, the aircraft was damaged beyond repair.
Probable cause:
The right propeller oversped, forcing the crew to attempt an emergency landing. The following factors were reported:
- Powerplant propeller and accessories,
- Foreign materials affecting normal operations,
- Inadequate maintenance and inspection,
- Failed to follow approved procedures,
- Inadequate preflight preparation,
- Improperly loaded aircraft,
- Improper emergency procedures,
- Intentional wheels-up landing,
- Suspected or known aircraft damage,
- Right propeller oversped, metal chips, feathered,
- Overweight by 1,129 pounds,
- Unlower gear normal system,
- Hit wires.
Final Report:

Crash of a Beechcraft E90 King Air in Pratt: 4 killed

Date & Time:
Type of aircraft:
Operator:
Registration:
YV-T-ADJ
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Wichita - Wichita
MSN:
LW-53
YOM:
1973
Location:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
3305
Captain / Total hours on type:
93.00
Circumstances:
The crew was completing a local training flight out from Wichita prior to deliver the aircraft in Venezuela. While cruising at low height, the pilot-in-command lost control of the airplane that stalled and crashed in an open field located near Pratt. The airplane was destroyed and all four occupants were killed.
Probable cause:
Loss of control after the pilot-in-command failed to maintain flying speed. The following factors were reported:
- Customer pilot training flight,
- Pilot-in-command non instrument rated,
- Gear down, flaps in approach position,
- Pilot-in-command in right seat.
Final Report:

Crash of a Lockheed PV-1 Ventura near Union Springs: 2 killed

Date & Time:
Type of aircraft:
Registration:
N45CK
Flight Phase:
Survivors:
No
Schedule:
Montgomery - Montgomery
MSN:
5333
YOM:
1943
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
5100
Captain / Total hours on type:
67.00
Circumstances:
The crew was engaged in a crop spraying mission in the region of Union Springs and departed Montgomery-Franklin Airport in the early morning. While flying at low height above a wooded area, the airplane struck tree tops and crashed in flames. The aircraft was destroyed and both crew members were killed.
Probable cause:
Collision with trees after the pilot-in-command misjudged speed and altitude. The following factors were reported:
- Diverted attention from operation of aircraft,
- Jettisoned load,
- Aircraft descended and hit ground in near level flight attitude.
Final Report:

Crash of a Beechcraft C18S in Cleveland

Date & Time:
Type of aircraft:
Operator:
Registration:
N6417C
Survivors:
Yes
Schedule:
Cleveland - Cleveland
MSN:
5549
YOM:
1943
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
1676
Captain / Total hours on type:
103.00
Circumstances:
Following a local skydiving mission, the pilot was returning to Cleveland Airport. On final approach, both engines failed due to fuel exhaustion. The airplane lost height and while avoiding power cables, the pilot lost control of the airplane that stalled and crashed in an open field. The airplane was destroyed and the pilot was injured.
Probable cause:
Failure of both engines due to fuel exhaustion. The following factors were reported:
- Inadequate preflight preparation,
- Mismanagement of fuel,
- Fuel exhaustion,
- Failed to maintain flying speed,
- Evasive manoeuvre to avoid collision,
- High obstructions,
- Complete engine failure on both engines,
- Pilot had to maneuver to avoid power lines on final approach.
Final Report:

Crash of a Beechcraft E18S in Davenport: 6 killed

Date & Time:
Type of aircraft:
Operator:
Registration:
N310WA
Survivors:
No
Schedule:
Muscatine - Davenport - Chicago
MSN:
BA-12
YOM:
1954
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
6
Captain / Total flying hours:
6000
Captain / Total hours on type:
2000.00
Circumstances:
On approach to Davenport Airport, the right wing detached. The twin engine airplane went out of control and crashed in an open field located few miles from the airfield. The aircraft was totally destroyed and all six occupants were killed.
Probable cause:
Structural failure of the right wing on descent due to fatigue cracks. The following factors were reported:
- Airframe, wings spars,
- Fatigue fracture,
- Inadequate inspection of aircraft on part of the maintenance personnel,
- Preexisting crack on lower spar cap WS-81 that was discernible but not detected over a 6-year period,
- Right wing folded upward.
Final Report:

Crash of a Beechcraft 65-A80 Queen Air in Brick Township: 6 killed

Date & Time:
Type of aircraft:
Operator:
Registration:
N456WM
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Monmouth - Monmouth
MSN:
LD-225
YOM:
1965
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
6
Circumstances:
While cruising at a relative low altitude, the twin engine airplane entered a series of hazardous manoeuvres when control was lost. The airplane crashed near Brick Township and was totally destroyed. All six occupants were killed.
Probable cause:
The pilot exceeded the designed stress limits of the aircraft. The following factors were reported:
- Pilot's physical impairment,
- Alcoholic impairment of efficiency and judgment,
- Separation in flight,
- Overload failure,
- Pilot alcohol level 1,05‰ tissue fluid,
- In-flight separation of wings and tail after a series of steep dives and pull-ups.
Final Report:

Crash of a Cessna 402A in Greensboro: 6 killed

Date & Time:
Type of aircraft:
Operator:
Registration:
N4599Q
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Greensboro - Greensboro
MSN:
402A-099
YOM:
1969
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
6
Captain / Total flying hours:
10500
Captain / Total hours on type:
2000.00
Circumstances:
Shortly after takeoff from Greensboro, while engaged in a local demo flight, the twin engine airplane went out of control and crashed in flames. All six occupants were killed.
Probable cause:
Uncontrolled descent following a failure of the elevator tab control system. The following factors were reported:
- Flight control system disconnected,
- Bolt connecting aft elevator bellcrank and elevator pushrod came loose,
- 100 h ours inspection completed 66 hours prior to the accident.
Final Report:

Crash of a Rockwell Sabreliner 60 in Montrose: 2 killed

Date & Time:
Type of aircraft:
Operator:
Registration:
N743R
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Los Angeles - Montrose - Denver
MSN:
306-11
YOM:
1968
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
10000
Captain / Total hours on type:
84.00
Aircraft flight hours:
2372
Circumstances:
After takeoff from Montrose Airport, while climbing to an altitude of 1,000 feet, the airplane banked left to an angle of 55° then stalled and crashed in a huge explosion. The aircraft was destroyed by impact forces and a post crash fire and both pilots were killed.
Probable cause:
Loss of control during initial climb after the left engine thrust reverser deployed. The following factors were reported:
- Improper operations of powerplant,
- The pilot-in-command failed to follow the approved procedures,
- Improper emergency procedures,
- Unwanted thrust reversal,
- Continued operations of left engine at climb power after unwanted in-flight deployment of the left engine thrust reverser.
Final Report: