Crash of a Cessna 404 Titan in Aspen: 1 killed

Date & Time: Dec 27, 1982 at 0743 LT
Type of aircraft:
Registration:
N5301J
Flight Phase:
Survivors:
Yes
Schedule:
Aspen - Salt Lake City
MSN:
404-0643
YOM:
1980
Crew on board:
1
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
10000
Captain / Total hours on type:
18.00
Aircraft flight hours:
373
Circumstances:
The right front seat passenger, who is a private pilot, stated that the pilot did not use takeoff flaps. The aircraft lifted off at about 85 knots and immediately started buffeting. The aircraft then impacted a highway in a nose high, left wing low attitude and collided with a rock face mountain. According to the aircraft operating manual the rate-of-climb/maximum climb chart indicates that (with wing flaps up at a density alt of 6,000 feet) the aircraft required a climb speed of 103 knots. Flaps up lift off speed is 95 knots. All six passengers were injured while the pilot was killed.
Probable cause:
Occurrence #1: loss of control - in flight
Phase of operation: takeoff - initial climb
Findings
1. (c) airspeed (vlof) - not attained - pilot in command
2. (c) lift-off - premature - pilot in command
3. Stall - inadvertent - pilot in command
4. (f) weather condition - high density altitude
----------
Occurrence #2: in flight collision with terrain/water
Phase of operation: takeoff - initial climb
Findings
5. Terrain condition - mountainous/hilly
Final Report:

Crash of a Swearingen SA227AC Metro III near Pueblo: 2 killed

Date & Time: Dec 7, 1982 at 1907 LT
Type of aircraft:
Operator:
Registration:
N30093
Flight Type:
Survivors:
No
Schedule:
Santa Fe - Pueblo
MSN:
AC-449
YOM:
1981
Location:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
8534
Captain / Total hours on type:
945.00
Aircraft flight hours:
2269
Circumstances:
At 1906 the flight was cleared to descend and maintain 7,500 feet, turn right to a heading 040 for an ASR approach to Pueblo Memorial Airport, and that the MDA is 5,200 feet. The flight read back "left to one forty five two zero zero." Approach control advised the flight that the heading was 040 and the flight acknowledged. There were no further communications with the flight. The aircraft was travelling in excess of an estimated 200 mph when it struck tundra in level flight on a heading of about 040. The copilot's autopsy revealed that the trachae, bronchi, and lungs contained aspirated gastric contents, including skeletal muscle fibers. Another company pilot reported that the copilot had vomited during a flight on November 14, 1982.
Probable cause:
Occurrence #1: in flight collision with terrain/water
Phase of operation: descent
Findings
1. (f) light condition - dark night
2. (c) altitude - inattentive - pilot in command
3. (f) diverted attention - pilot in command
4. (f) physical impairment - copilot/second pilot
Final Report:

Crash of a Piper PA-61 Aerostar (Ted Smith 601P) in Fountain: 2 killed

Date & Time: Nov 12, 1982 at 2303 LT
Registration:
N3641T
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Pueblo – Englewood
MSN:
61P-0818-8063427
YOM:
1980
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
7200
Aircraft flight hours:
948
Circumstances:
After taking off at approximately 2250, the aircraft was identified on radar and observed to climb on course to an altitude of 10,700 feet. The aircraft then descended thru 10,500 feet and the crew reported they would maintain that altitude. At about 2301 the aircraft was about 5 miles southeast of Colorado Springs and at 10,300 feet when radar contact was lost. The aircraft crashed in that area in a near vertical descent. The outboard 8 feet of the right wing had separated in flight and impacted about 1/4 mile from the main wreckage. The right aileron had sheared in 3 pieces also and was found near the failed wing. There was evidence that the the wing had yielded to a down and up loading (1 cycle) when it separated upward and rearward. All fracture surfaces had evidence of overload failures except the aileron control linkage which was further damaged on impact and could not be evaluated. Both pilots were using medication that was contraindicated for use by airmen and both pilots had little sleep during the previous 48 hours. Before the flight the pilot seemed agitated and the copilot had an odor of beer. Both occupants were killed.
Probable cause:
Occurrence #1: loss of control - in flight
Phase of operation: cruise - normal
Findings
1. (c) reason for occurrence undetermined
----------
Occurrence #2: airframe/component/system failure/malfunction
Phase of operation: descent - uncontrolled
Findings
2. (f) light condition - night
3. (c) design stress limits of aircraft - exceeded
4. (f) fatigue - pilot in command
5. (f) fatigue - copilot/second pilot
6. Other psychological condition - pilot in command
7. Impairment(alcohol) - copilot/second pilot
8. Impairment(drugs) - pilot in command
9. Impairment(drugs) - copilot/second pilot
10. Flight control,aileron - overload
11. Flight control,aileron - separation
12. Wing,spar - overload
13. Wing,spar - separation
----------
Occurrence #3: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Final Report:

Crash of a Mitsubishi MU-2B-25 Marquise in Hayden: 6 killed

Date & Time: Sep 12, 1982 at 1328 LT
Type of aircraft:
Registration:
N66U
Flight Phase:
Survivors:
No
Schedule:
Hayden - Fort Collins
MSN:
309
YOM:
1974
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
6
Captain / Total flying hours:
10451
Captain / Total hours on type:
833.00
Aircraft flight hours:
1493
Circumstances:
A maintenance supervisor and two pilots noted that the left engine did not respond normally while being started. Aft starting, the pilot taxied to runway 10 for an IFR departure. Since the taxiway did not extend to the end of the runway, the pilot of another aircraft waited on the taxiway, just short of the runway, approximately 2,967 feet from the end. He observed smoke coming from the left engine of the MU-2 and reported this info on the unicom frequency. He reported that the MU-2 continued and rotated for takeoff approximately 200 to 250 yards east of his position. Reportedly, the aircraft climbed to approximately 300-400 feet afl, then turned left toward higher terrain. After turning, it enter what two witnesses described as a VMC roll, then crashed and burned. An examination of the airframe revealed no preimpact mechanical failures. A teardown of the left engine revealed that a turbine bearing, pn 3101092-1, had been misaligned and subsequently began to fail, damaging the 2nd and 3rd stages of the turbine section. The airport elev was 6,597 feet. The computed takeoff roll was 1,620 feet and the computed accelerate stop distance was 3,100 feet. The landing gear and selector found in down position. The aircraft was destroyed and all six occupants were killed.
Probable cause:
Occurrence #1: loss of engine power(partial) - mechanical failure/malfunction
Phase of operation: takeoff - roll/run
Findings
1. (c) turbine assembly,shaft bearing - failure,partial
2. (c) maintenance,installation - improper - other maintenance personnel
----------
Occurrence #2: loss of control - in flight
Phase of operation: maneuvering - turn to landing area (emergency)
Findings
3. (f) weather condition - high density altitude
4. (f) aborted takeoff - not performed - pilot in command
5. (c) gear retraction - not performed - pilot in command
6. (c) airspeed (VMC) - not maintained - pilot in command
----------
Occurrence #3: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Findings
7. Terrain condition - mountainous/hilly
Final Report:

Crash of a Convair CV-440 Metropolitan near Wolf Creek Pass

Date & Time: Aug 25, 1982 at 1330 LT
Operator:
Registration:
N477KW
Flight Phase:
Flight Type:
Survivors:
Yes
Site:
Schedule:
Pueblo - Carlsbad
MSN:
210
YOM:
1954
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Aircraft flight hours:
37102
Circumstances:
The crew was completing a positioning flight from Pueblo to Carlsbad on behalf of Air Resort Airlines. While cruising at an altitude of 11,700 feet over a mountainous area under VFR mode, weather conditions deteriorated. Shortly later, the airplane struck trees and crashed. Both pilots were seriously injured and the aircraft was destroyed.
Probable cause:
Occurrence #1: in flight encounter with weather
Phase of operation: cruise - normal
Findings
1. (f) weather condition - clouds
2. (c) VFR flight into IMC - continued - pilot in command
----------
Occurrence #2: in flight collision with terrain/water
Phase of operation: climb
Findings
3. (f) terrain condition - mountainous/hilly
Final Report:

Crash of a Mitsubishi MU-2B-40 Marquise in Hayden

Date & Time: Feb 3, 1982 at 1715 LT
Type of aircraft:
Registration:
N149JA
Survivors:
Yes
Schedule:
Kearny - Hayden
MSN:
402
YOM:
1979
Crew on board:
2
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
9700
Captain / Total hours on type:
1700.00
Aircraft flight hours:
1203
Circumstances:
The aircraft was 20 feet agl during landing when the crew heard a propeller go into beta mode and the aircraft yawed to the right. The pilot lost control of the aircraft and it collided with a snow bank which separated the wings from the fuselage. Impact damage made it impossible to tell why the propeller went into beta mode.
Probable cause:
Occurrence #1: airframe/component/system failure/malfunction
Phase of operation: landing - flare/touchdown
Findings
1. (f) propeller system/accessories,pitch change mech - undetermined
2. (f) propeller system/accessories,reversing system - undetermined
3. (f) propeller system/accessories,prop control unit - undetermined
----------
Occurrence #2: loss of control - on ground/water
Phase of operation: landing - flare/touchdown
Findings
4. (c) directional control - not maintained - pilot in command
5. (c) remedial action - not used - pilot in command
6. (c) ground loop/swerve - uncontrolled - pilot in command
----------
Occurrence #3: in flight collision with terrain/water
Phase of operation: landing - roll
Findings
7. (f) terrain condition - snowbank
Final Report:

Crash of a Cessna 340A in Pueblo

Date & Time: Dec 31, 1981 at 2137 LT
Type of aircraft:
Registration:
N6272N
Survivors:
Yes
Schedule:
Denver – Pueblo
MSN:
340A-0457
YOM:
1978
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
5299
Captain / Total hours on type:
165.00
Circumstances:
On a night approach to Pueblo Memorial Airport while on a taxi flight from Denver, the pilot encountered technical problems with the power levers. The left engine was shut down then the airplane lost height, stalled and crashed on final. All four occupants were injured and the aircraft was destroyed.
Probable cause:
Stall on final approach due to engine control problems. The following contributing factors were reported:
- Throttle-power lever assemblies jammed,
- The pilot failed to maintain flying speed,
- Partial loss of power on left engine,
- Shut down left engine after the left throttle cable jammed at approximately 30 inches of manifold pressure.
Final Report:

Crash of a Piper PA-31-350 Navajo Chieftain in Durango: 4 killed

Date & Time: Dec 31, 1981 at 2000 LT
Operator:
Registration:
N41070
Survivors:
Yes
Schedule:
Albuquerque - Durango
MSN:
31-8253005
YOM:
1982
Flight number:
SNW070
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
4900
Captain / Total hours on type:
1381.00
Circumstances:
While on a night approach to Durango-La Plata County Airport, the pilot decided to initiate a go-around. For unknown reasons, the twin engine airplane failed to gain sufficient height, struck trees and crashed in a wooded area located few miles from the airport. Two passengers were seriously injured while four other occupants were killed.
Probable cause:
Controlled collision with ground during a missed approach for undetermined reasons. The following contributing factors were reported:
- Low ceiling,
- Fog,
- Snow,
- Visibility one mile or less,
- The pilot failed to execute successfully a missed approach procedure for undetermined reasons.
Final Report:

Crash of a Mitsubishi MU-2B-35 Marquise in Wolcott: 7 killed

Date & Time: Nov 18, 1981 at 1820 LT
Type of aircraft:
Registration:
N444AR
Survivors:
No
Site:
Schedule:
Shreveport - Eagle
MSN:
555
YOM:
1972
Crew on board:
2
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
7
Captain / Total flying hours:
5339
Captain / Total hours on type:
45.00
Circumstances:
Following an uneventful flight from Shreveport, the crew started the descent to Eagle County Airport, Colorado. By a dark night and overcast ceiling, the crew failed to realize his altitude was too low when the airplane struck the slope of a mountain and crashed near Wolcott, about 13 miles northeast of Eagle County Airport. The airplane was destroyed upon impact and all seven occupants were killed.
Probable cause:
Controlled flight into terrain due to improper IFR operation.
Final Report:

Crash of a Boeing B-52D-55-BO Stratofortress near Las Animas: 8 killed

Date & Time: Oct 30, 1981
Type of aircraft:
Operator:
Registration:
55-0078
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
March - March
MSN:
17194
YOM:
1955
Crew on board:
8
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
8
Circumstances:
The crew departed March AFB, California, on a night training flight. In the evening, while cruising at low altitude to simulate an aerial attack, the airplane struck a sand dune then crashed in a huge explosion in a prairie located few miles west of Las Animas. All eight crew members were killed.
Crew:
Cpt James L. MacGregor, pilot,
Cpt Gani Aydoner, copilot,
Cpt Clifford R. Duane,
1st/Lt Kendall E. Wallace,
Cpt Stanley H. Eddleman,
S/A Timothy E. McFarland,
A1c Bruce E. Schaefer,
A1c David W. Smith.