Crash of a Beechcraft C90 King Air near Jackson: 1 killed

Date & Time: Jun 16, 1986 at 1500 LT
Type of aircraft:
Registration:
N114CM
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Olathe - Jackson
MSN:
LJ-709
YOM:
1977
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
6700
Captain / Total hours on type:
500.00
Aircraft flight hours:
3002
Circumstances:
The pilot departed Olathe, KS, en route to Jackson, WY. The pilot radioed the Denver EFAS and reported his position as 56 miles northwest of Casper, WY. There was no further radio communication with N114CM. The pilot's wife stated after the accident that the pilot had a habit of taking a 'cat nap' when he flew. The pilot, sole on board, was killed.
Probable cause:
Occurrence #1: in flight collision with terrain/water
Phase of operation: descent
Findings
1. (c) aircraft handling - improper - pilot in command
2. (c) proper altitude - not maintained - pilot in command
3. (f) inattentive - pilot in command
4. (c) fatigue (lack of sleep) - pilot in command
5. Terrain condition - mountainous/hilly
Final Report:

Crash of a Beechcraft C99 Airliner in Laramie

Date & Time: May 16, 1986 at 1042 LT
Type of aircraft:
Operator:
Registration:
N6728J
Survivors:
Yes
Schedule:
Denver – Laramie
MSN:
U-217
YOM:
1983
Crew on board:
2
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
2530
Captain / Total hours on type:
1809.00
Aircraft flight hours:
5008
Circumstances:
This part 135 IFR flight was inbound for landing at Laramie, Wyoming. During the en route and approach for landing portions of the flight the aircraft picked up a moderate to heavy load of ice. During the landing flare the aircraft stalled, hit the runway, bounced, veered off the runway, and struck a VASI lighting system. The left landing gear collapsed and the aircraft skidded to a stop. All nine occupants escaped uninjured while the aircraft was damaged beyond repair.
Probable cause:
Occurrence #1: in flight encounter with weather
Phase of operation: climb - to cruise
Findings
1. (c) weather condition - icing conditions
2. (f) weather condition - snow
----------
Occurrence #2: loss of control - in flight
Phase of operation: landing - flare/touchdown
Findings
3. (c) airspeed - uncontrolled - pilot in command
4. (c) stall - inadvertent - pilot in command
----------
Occurrence #3: on ground/water collision with object
Phase of operation: landing - roll
Findings
5. Object - approach light/navaid
----------
Occurrence #4: main gear collapsed
Phase of operation: landing - roll
Findings
6. Landing gear, main gear - overload
Final Report:

Crash of a Cessna 414 Chancellor in Cheyenne

Date & Time: Oct 20, 1984 at 1338 LT
Type of aircraft:
Registration:
N1597T
Flight Phase:
Survivors:
Yes
Schedule:
Cheyenne - Salt Lake City
MSN:
414-0377
YOM:
1973
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
13200
Aircraft flight hours:
18035
Circumstances:
The aircraft departed the airport in IFR conditions (snowing) and was observed staggering into the air. Shortly after takeoff the aircraft struck power lines and crashed into homes in a residential area. Investigation revealed that the aircraft had accumulated ice and in addition was over certified max gross weight. There was no evidence of airframe, flight control or engine failure/malfunction prior to impact with the power lines.
Probable cause:
Occurrence #1: in flight encounter with weather
Phase of operation: takeoff - roll/run
Findings
1. (f) weather condition - fog
2. (f) weather condition - snow
3. (c) flight into known adverse weather - performed - pilot in command
4. (f) overconfidence in personal ability - pilot in command
----------
Occurrence #2: in flight collision with object
Phase of operation: takeoff - initial climb
Findings
5. (f) object - wire, static
6. (c) proper climb rate - not maintained - pilot in command
7. (f) aircraft weight and balance - exceeded - pilot in command
----------
Occurrence #3: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Final Report:

Crash of a Rockwell Grand Commander 690 in Little America: 4 killed

Date & Time: Aug 25, 1984 at 1030 LT
Registration:
N9150N
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Ogden - Aurora
MSN:
690-11063
YOM:
1973
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
3410
Circumstances:
About 10 minutes after takeoff at 1005 mdt, the pilot was cleared to climb to FL190. This was ATC's last communication with the aircraft. At 1030:39, the controller attempted to contact the pilot to advise that he had lost radar contact and to recycle the transponder and squawk 6062. There was no response. Two witnesses reported seeing the aircraft just before it impacted the ground. According to them, they saw fire and/or an explosion before impact and one witness reported the aircraft broke up after it came below an estimated 1,000 to 1,200 feet ceiling. However, the wreckage was scattered over a 2 miles area. An exam revealed evidence of a catastrophic in-flight breakup from overload which included positive overload of both wings. Radar data showed that just before radar contact was lost, the aircraft's speed varied between 221 and 272 knots, heading varied from 072° to 014° and vertical velocity varied from +300 to -2,400 feet/min. Thunderstorms, turbulences, rain and cloud tops to 25,000 feet were reported. Probable light to moderate icing in clouds above the freezing level of 14,000 feet. Aircraft had weather radar aboard. All four occupants were killed.
Probable cause:
Occurrence #1: in flight encounter with weather
Phase of operation: cruise
Findings
1. (f) weather condition - clouds
2. (f) weather condition - thunderstorm
3. (f) weather condition - turbulence in clouds
4. (f) weather condition - rain
5. (f) weather condition - low ceiling
6. (f) weather condition - icing conditions
7. (c) flight into known adverse weather - continued - pilot in command
----------
Occurrence #2: loss of control - in flight
Phase of operation: cruise
Findings
8. Aircraft handling - not maintained
----------
Occurrence #3: airframe/component/system failure/malfunction
Phase of operation: descent - uncontrolled
Findings
9. Design stress limits of aircraft - exceeded
10. Wing - overload
11. Fuel system, tank - overload
----------
Occurrence #4: fire
Phase of operation: descent - uncontrolled
----------
Occurrence #5: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Final Report:

Crash of a Cessna 340 in Rock Springs: 3 killed

Date & Time: Apr 26, 1983 at 1103 LT
Type of aircraft:
Registration:
N5415M
Flight Type:
Survivors:
No
Schedule:
Rock Springs - Rock Springs
MSN:
340-0028
YOM:
1972
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
4281
Captain / Total hours on type:
31.00
Aircraft flight hours:
2022
Circumstances:
The aircrew of a Cessna 340, N5415M, were scheduled for an air taxi check ride with an inspector at Jackson, WY, later in the afternoon. They had planned to takeoff from Rock Springs, WY, practice at few instrument approaches at Rock Springs, then proceed to Jackson. After taking off, they made an NDB approach, made a missed approach, then began an ILS approach. A Beech Bonanza, N1825F, was on a flight from Scottsbluff, NE to Rock Springs. During arrival to Rock Springs, the Bonanza pilot was monitoring the position of a King Air that was ahead of him and also on an approach to the same airport. All three aircraft were using the same frequency and all three were providing reports of their respective positions. At approximately 1103 mdt, witnesses heard N5415M and N1825F collide, then saw the aircraft and pieces of wreckage falling. An investigation revealed the Cessna was inbound toward the outermarker (270° course) and the Bonanza was in level flight, heading approximately 219°. Both aircraft were operating VFR. All six occupants in both aircraft were killed.
Probable cause:
Occurrence #1: midair collision
Phase of operation: approach - iaf to faf/outer marker (IFR)
Findings
1. Radar traffic information service - not used - pilot in command
2. (c) visual lookout - inadequate - copilot/second pilot
3. (c) visual lookout - inadequate - pilot of other aircraft
----------
Occurrence #2: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Final Report:

Crash of a Piper PA-60 Aerostar (Ted Smith 602P) in Almy: 1 killed

Date & Time: Jan 5, 1983 at 1730 LT
Registration:
N6893L
Flight Type:
Survivors:
No
Schedule:
Casper – Almy
MSN:
62P-0893-8165025
YOM:
1981
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
1642
Captain / Total hours on type:
341.00
Aircraft flight hours:
372
Circumstances:
Before departing, the pilot obtained a weather briefing and was advised of a sigmet which forecasted severe turbulence below 18,000 feet, strong up/downdrafts, strong surface winds and wind shear near mountains and in passes. He took off with full fuel tanks and approximately 400 lbs of cargo on board. ARTCC reported that the en route portion of the flight was handled routinely. During arrival, the pilot contacted the airport unicom for a landing advisory. A King Air pilot was arriving at about the same time and asked the Aerostar pilot if he was making a full stop. The Aerostar pilot replied that he was. The King Air pilot lost sight of the Aerostar and began a 360° turn. He asked the Aerostar pilot to advise of his position, and shortly thereafter, the Aerostar pilot transmitted three mayday calls. Reportedly, the aircraft nosed up and went into a steep right bank just before impact. No preimpact mechanical failure/malfunction was found. There was evidence that most of the cargo was in the baggage compartment (limited to 240 lbs) and could have moved the CofG well beyond the aft limit. Elevator trim found full nose down. The pilot, sole on board, was killed.
Probable cause:
Occurrence #1: loss of control - in flight
Phase of operation: approach - VFR pattern - base leg/base to final
Findings
1. (c) preflight planning/preparation - inadequate - pilot in command
2. (c) aircraft weight and balance - exceeded - pilot in command
3. Light condition - dusk
4. Visual lookout - reduced - pilot in command
5. (f) diverted attention - pilot in command
6. Aircraft handling - not maintained - pilot in command
7. Stall - uncontrolled - pilot in command
----------
Occurrence #2: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Final Report:

Crash of a Mitsubishi MU-2B-60 Marquise in Saratoga: 2 killed

Date & Time: Nov 5, 1981 at 1730 LT
Type of aircraft:
Registration:
N53AD
Flight Phase:
Survivors:
No
Schedule:
Saratoga - Albuquerque
MSN:
776
YOM:
1980
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
16600
Captain / Total hours on type:
5000.00
Circumstances:
After takeoff from Saratoga-Shively Field, while in initial climb, the twin engine airplane crashed in a right descending turn, bursting into flames. Both occupants were killed.
Probable cause:
Uncontrolled collision with ground for unknown reasons. Density altitude 6,900 feet. No pre-accident malfunction or failure found.
Final Report:

Crash of a Mitsubishi MU-2B-15 Marquise in Riverton: 5 killed

Date & Time: Sep 6, 1981 at 0900 LT
Type of aircraft:
Registration:
N3ED
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Lander - North Platte
MSN:
101
YOM:
1968
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
1500
Captain / Total hours on type:
15.00
Circumstances:
While in cruising altitude on a flight from Lander to North Platte, Nebraska, the pilot encountered icing conditions. The airplane entered an uncontrolled descent then crashed in a field, bursting into flames. All five occupants were killed.
Probable cause:
Uncontrolled descent and subsequent uncontrolled collision with ground after the pilot attempted operation with known deficiencies in equipment. The following contributing factors were reported:
- Airframe ice,
- Icing conditions including sleet, freezing rain,
- Pilot aware of four deferred maintenance discrepancies involving the anti-ice system,
- Moderate icing forecast.
Final Report:

Crash of a Cessna T207 Skywagon in Casper: 1 killed

Date & Time: Aug 21, 1981 at 1930 LT
Registration:
N17464
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Casper - Erie
MSN:
207-0346
YOM:
1976
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
6939
Captain / Total hours on type:
4673.00
Circumstances:
Shortly after takeoff from Casper-Natrona County Airport, while climbing, the single engine airplane struck trees and crash landed in a field. The pilot, sole on board, was killed.
Probable cause:
Engine failure during initial climb due to fuel starvation. The following contributing factors were reported:
- Poor/inadequate design,
- Powerplant, fuel system,
- Inadequate preflight preparation,
- Improperly loaded aircraft,
- Cargo shifted,
- Forced landing off airport on land,
- Vapor lock,
- Approximately 310 lbs over MTOW,
- Cargo shifted at impact, crushing the pilot.
Final Report:

Crash of a Cessna 340 in Riverton

Date & Time: Jul 30, 1978 at 1000 LT
Type of aircraft:
Operator:
Registration:
N1381G
Flight Phase:
Survivors:
Yes
Schedule:
Riverton - Evanston
MSN:
340-0080
YOM:
1972
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
2997
Captain / Total hours on type:
345.00
Circumstances:
At liftoff, both engines lost power. The pilot elected to return but eventually decided to make an emergency landing. He was forced to make an evasive maneuver to avoid collision and completed a belly landing in an open field. The aircraft was destroyed and all three occupants were seriously injured.
Probable cause:
Powerplant failure for undetermined reasons. The following contributing factors were reported:
- Improper maintenance, servicing, inspection,
- Fuel injection system,
- Excessive pressure,
- Intentional wheels-up landing,
- High density altitude,
- Reversed course immediately after takeoff.
Final Report: