Crash of a Rockwell Turbo Commander 681B in Calhan: 1 killed

Date & Time: Mar 28, 1985 at 1930 LT
Registration:
N772CB
Flight Phase:
Survivors:
Yes
Site:
Schedule:
Van Nuys - Denver
MSN:
681-6050
YOM:
1970
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
411
Captain / Total hours on type:
376.00
Aircraft flight hours:
4500
Circumstances:
During a cross country flight from WI to CA and return, the non instrument, low experienced private pilot, flew into IMC conditions. The aircraft impacted flat snow-covered ground, destroying the aircraft and fatally injuring his passenger. Examination of wreckage revealed no evidence of pre-accident malfunction of the aircraft or its powerplants. A passenger was killed while three other occupants were injured.
Probable cause:
Occurrence #1: in flight encounter with weather
Phase of operation: descent - normal
Findings
1. (f) light condition - night
2. (c) in-flight planning/decision - improper - pilot in command
3. (c) inadequate transition/upgrade training - pilot in command
4. (f) weather condition - turbulence
5. (c) flight into known adverse weather - initiated - pilot in command
6. (c) lack of familiarity with aircraft - pilot in command
7. (f) weather condition - night
8. (c) vfr flight into imc - continued - pilot in command
9. (c) became lost/disoriented - inadvertent - pilot in command
----------
Occurrence #2: loss of control - in flight
Phase of operation: descent - normal
Findings
10. (c) airspeed - uncontrolled - pilot in command
11. (c) altitude - uncontrolled - pilot in command
----------
Occurrence #3: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Findings
12. (f) terrain condition - open field
13. (f) terrain condition - snow covered
Final Report:

Crash of a Piper PA-31-310 Navajo in Eagle Lake

Date & Time: Mar 25, 1985
Type of aircraft:
Operator:
Registration:
N23L
Flight Type:
Survivors:
Yes
MSN:
31-76
YOM:
1968
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On or about 3/25/85, the aircraft was landed on a short private strip. During the landing, it overran the strip, then collided with a dirt bank and a tree. The pilot abandoned the aircraft. Neither he nor the new owner could be found. There was evidence that the aircraft had been set afire after the accident. The aircraft bore a registration of N23LX, but the aircraft data plate and FAA records showed that a registration of N23L should have been displayed. During a seemingly unrelated arrest, police found the records of N23L in another aircraft that was loaded with 1,500 lbs of marijuana. The pilot was presumed to have had no injuries.
Probable cause:
Occurrence #1: overrun
Phase of operation: landing - roll
Findings
1. Stolen aircraft/unauthorized use - performed - pilot in command
2. (c) distance - misjudged - pilot in command
3. (c) airspeed - misjudged - pilot in command
----------
Occurrence #2: on ground/water encounter with terrain/water
Phase of operation: landing - roll
Findings
4. (f) terrain condition - dirt bank/rising embankment
----------
Occurrence #3: on ground/water collision with object
Phase of operation: landing - roll
Findings
5. (f) object - tree(s)
Final Report:

Crash of a Cessna 401A in Dorset: 1 killed

Date & Time: Mar 17, 1985 at 2015 LT
Type of aircraft:
Registration:
N12CQ
Flight Phase:
Survivors:
No
Site:
Schedule:
Caldwell - Rutland
MSN:
401A-0116
YOM:
1969
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
4946
Captain / Total hours on type:
3149.00
Aircraft flight hours:
3062
Circumstances:
The pilot was about 30 miles from Rutland when he radioed the airport for weather info. He was informed that clouds were 1,500 feet broken and 2,700 feet overcast with snow, light fog and 5 miles visibility. The pilot responded that he would call again when he got closer to the airport. There was no further transmission received from the pilot. The aircraft collided with Dorset mount, located about 18 miles south of the airport. The aircraft was in a level attitude and at a elevation of 3,300 feet. Dorset mount is 3,515 feet high. Examination of the aircraft did not disclose evidence of malfunction. No flight plan was filed. The pilot, sole on board, was killed.
Probable cause:
Occurrence #1: in flight encounter with weather
Phase of operation: cruise
Findings
1. (f) preflight briefing service - not obtained - pilot in command
2. (f) weather condition - low ceiling
3. (c) vfr flight into imc - initiated - pilot in command
4. (f) weather condition - snow
5. (f) weather condition - fog
6. (f) judgment - poor - pilot in command
----------
Occurrence #2: in flight collision with terrain/water
Phase of operation: cruise
Findings
7. (f) terrain condition - mountainous/hilly
8. (c) visual lookout - not possible - pilot in command
9. (c) clearance - not maintained - pilot in command
Final Report:

Crash of a Douglas A-26B Invader in Lawton

Date & Time: Mar 17, 1985 at 1635 LT
Type of aircraft:
Registration:
N142ER
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Ada - Frederick
MSN:
6928
YOM:
1941
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
5395
Captain / Total hours on type:
158.00
Circumstances:
An intermittent fire in the left engine accessory section led to loss of fuel to the engine. The right engine ingested water and quit. The landing gear had been left pinned in the down position because of a malfunction reported on the previous flight. Neither propeller was feathered, but the resulting high rate of descent led to a forced landing before the left tank blew up and the wing burned off. The aircraft was destroyed by fire after all three occupants escaped without serious injury. The aircraft was being ferried to another facility for restoration.
Probable cause:
Occurrence #1: miscellaneous/other
Phase of operation: standing - pre-flight
Findings
1. (c) maintenance, inspection - inadequate - company maintenance personnel
2. (f) preflight planning/preparation - inadequate - pilot in command
3. (f) operation with known deficiencies in equipment - intentional - pilot in command
----------
Occurrence #2: fire
Phase of operation: cruise - normal
Findings
4. (c) accessory drive assy - fire
----------
Occurrence #3: loss of engine power (total) - nonmechanical
Phase of operation: descent - emergency
Findings
5. (c) fluid,fuel - water
----------
Occurrence #4: forced landing
Phase of operation: descent - emergency
----------
Occurrence #5: forced landing
Phase of operation: landing
Findings
6. Engine assembly - fire
7. Nacelle/pylon - fire
8. Wing - fire
9. Horizontal stabilizer surface - fire
10. Landing gear - overload
Final Report:

Crash of a De Havilland DHC-6 Twin Otter 300 in Kaktovik

Date & Time: Mar 12, 1985 at 0015 LT
Operator:
Registration:
N540N
Survivors:
Yes
Schedule:
Prudhoe Bay – Kaktovik
MSN:
401
YOM:
1973
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
5311
Captain / Total hours on type:
2098.00
Aircraft flight hours:
13652
Circumstances:
Aircraft crashed during missed approach to temporary winter landing strip. Aircraft hit in steep nose down attitude. Marginal weather conditions prevailed, with icing reported. All four occupants were injured, both pilots seriously.
Probable cause:
Occurrence #1: in flight collision with terrain/water
Phase of operation: go-around (vfr)
Findings
1. (f) terrain condition - snow covered
2. (c) flight manuals - not followed - pilot in command
3. (f) overconfidence in aircraft's ability - pilot in command
4. (f) inadequate surveillance of operation - company/operator mgmt
5. (f) weather condition - fog
6. (f) weather evaluation - inaccurate - pilot in command
7. (f) company-induced pressure - company/operator management
8. (f) inadequate surveillance of operation - faa (organization)
9. (f) light condition - dark night
10. (f) in-flight planning/decision - poor - pilot in command
11. (f) expectancy - other person
12. (f) insuff standards/requirements, operation/operator - company/operator mgmt
13. (f) light condition - dark night
14. (f) weather evaluation - inaccurate - pilot in command
15. (f) fatigue (flight and ground schedule) - pilot in command
16. (c) weather condition - icing conditions
17. (f) flight into known adverse weather - intentional - pilot in command
18. Fatigue (flight and ground schedule) - copilot/second pilot
19. (f) wing - ice
20. (f) anti-ice/deice system - not used - pilot in command
21. (c) altitude - inadequate - pilot in command
Final Report:

Crash of a Lockheed C-130E Hercules in Fort Hood: 8 killed

Date & Time: Mar 12, 1985
Type of aircraft:
Operator:
Registration:
64-0549
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Dyess AFB - Gray AAF
MSN:
4044
YOM:
1965
Location:
Crew on board:
8
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
8
Circumstances:
The four engine aircraft was completing a training mission from Dyess AFB (Abilene) to the Gray AAF near Killeen, carrying eight crew members. En route, while flying at low height and dropping sand bags, the airplane went out of control and crashed near Fort Hood. All eight crew members were killed.

Crash of a Piper PA-61 Aerostar (Ted Smith 601P) in Van Nuys: 1 killed

Date & Time: Mar 6, 1985 at 1858 LT
Operator:
Registration:
N777PL
Survivors:
No
Site:
Schedule:
Santa Ana – Van Nuys
MSN:
61-0334-111
YOM:
1976
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
1820
Aircraft flight hours:
1490
Circumstances:
The aircraft crashed into a residence 2 miles short of the runway after loss of power on the left engine. This engine was feathered, the gear was extended, but the flaps remained up as the aircraft continued the landing approach. Post accident investigation revealed no irregularities in the functioning of the aircraft. The pilot had radioed the report of power loss but had stated that he would not need the emergency equipment. The aircraft crashed in Sepulveda and was destroyed. The pilot, sole on board, was killed.
Probable cause:
Occurrence #1: loss of engine power
Phase of operation: approach - vfr pattern - downwind
Findings
1. (f) engine assembly - undetermined
----------
Occurrence #2: undershoot
Phase of operation: approach - vfr pattern - base leg/base to final
Findings
2. (c) planning/decision - poor - pilot in command
----------
Occurrence #3: in flight collision with object
Phase of operation: approach - vfr pattern - base leg/base to final
Findings
3. (f) object - residence
Final Report:

Crash of a Cessna 207 Skywagon in Dillingham

Date & Time: Mar 2, 1985 at 0925 LT
Registration:
N1715U
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Dillingham - Manokotak
MSN:
207-0315
YOM:
1976
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4400
Captain / Total hours on type:
3500.00
Circumstances:
The pilot was attempting a 180° turn to reverse direction away from lowering clouds and snow showers when the right wing dug into the snow covered terrain. The pilot stated a virtual 'white out' condition existed at the time. The pilot was uninjured and the aircraft was damaged beyond repair.
Probable cause:
Occurrence #1: in flight collision with terrain/water
Phase of operation: maneuvering - turn to reverse direction
Findings
1. (f) weather condition - snow
2. (f) weather condition - whiteout
3. (c) vfr flight into imc - inadvertent - pilot in command
4. (c) proper altitude - not maintained - pilot in command
Final Report:

Crash of a Rockwell Grand Commander 680 off Key West: 2 killed

Date & Time: Mar 1, 1985 at 0015 LT
Operator:
Registration:
N709G
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Belize City - Key West
MSN:
680-865-82
YOM:
1960
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
A Coast Guard Falcon aircraft was on scene when the aircraft ditched in the Atlantic ocean due to fuel exhaustion. A life raft and marker were dropped by the Coast Guard aircraft. A search was conducted all day on 3/1/85 and was called off at sunset on on 3/2/85. The occupants were presumed to have been fatally injured or drowned. The aircraft was presumed to have been destroyed.
Probable cause:
Occurrence #1: loss of engine power (total) - nonmechanical
Phase of operation: cruise
Findings
1. (c) planning/decision - improper - pilot in command
2. (c) fluid, fuel - exhaustion
3. (c) fuel supply - inadequate - pilot in command
----------
Occurrence #2: forced landing
Phase of operation: descent - emergency
----------
Occurrence #3: ditching
Phase of operation: landing - flare/touchdown
Findings
4. (f) light condition - dark night
Final Report:

Crash of a Piper PA-31P Pressurized Navajo in Saint Louis: 3 killed

Date & Time: Feb 25, 1985 at 1935 LT
Type of aircraft:
Operator:
Registration:
N404RS
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Saint Louis - Saint Louis
MSN:
31P-018
YOM:
1970
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
1420
Captain / Total hours on type:
3.00
Copilot / Total hours on type:
110
Aircraft flight hours:
493
Circumstances:
The aircraft was on a night instructional flight with 2 multi-engine instructor pilots at the controls and a rated pilot occupying a rear passenger seat. The right front seat occupant was an experienced multi-engine pilot with 110 hours in this make and model; however, his 2nd class medical certificate was issued in January 1983. The left front seat occupant had just received his multi-engine instructor rating and had only 3 hours in this make and model. He had a current medical certificate and was presumed to be the pilot-in-command. The aircrew made 2 passes over runway 18, then maneuvered onto a downwind leg of the pattern. According to witnesses, the aircraft was northeast of the airport at approximately 300 to 400 feet agl and maneuvering back toward the runway when it entered a steep descent, crashed and burned. The aircraft crashed northeast of the airport in a wooded area. Impact occurred on a southerly heading in about an 18° dive. No preimpact part failure/malfunction was found; however, the aircraft was extensively damaged during impact. Toxicological checks of the passenger and right front seat occupants showed each had an alcohol level of 1,17‰. No alcohol found in the left front seat occupant's blood. All three occupants were killed.
Probable cause:
Occurrence #1: in flight collision with terrain/water
Phase of operation: approach - vfr pattern - base turn
Findings
1. (f) judgment - poor - pilot in command
2. (c) judgment - poor - other crewmember
3. (c) impairment (alcohol) - other crewmember
4. (f) qualification - other crewmember
5. (f) light condition - dark night
6. (c) aircraft handling - not maintained - pilot in command
7. (f) lack of total experience in type of aircraft - pilot in command
8. (c) remedial action - inadequate - other crewmember
----------
Occurrence #2: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Final Report: