Crash of a Cessna 402 in Pocatello: 1 killed

Date & Time: May 15, 1985 at 1826 LT
Type of aircraft:
Registration:
N402CS
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Pocatello - Boise
MSN:
402A-0108
YOM:
1969
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
4500
Captain / Total hours on type:
350.00
Circumstances:
Shortly after departure and level off, the pilot reported an engine malfunction and initiated a return to the airport. About 2 minutes later, he reported an engine fire and declared an emergency. Approximately one minute thereafter, the right wing separated from the aircraft and the plane crashed. An exam of the wreckage revealed extensive inflight fire damage in the area of separation. A 2.5 by 3 inches hole was found in the right inboard exhaust tube, pn 0850712-6. It was oriented toward the accessory compartment with numerous fuel and oil lines which were fire damaged and charred. Also, much of the engine support structure and wing spar were melted in that area. An exam of the exhaust tube revealed its walls were thin, brittle and discolored in the area of the rupture and several areas of cracks and small holes were found. The exhaust tube had 5,862 hours of total service and 1,762 hours since it was overhauled. Records showed that ad 75-23-08 had been complied with during the last inspection, 25 flight hours prior to the accident. The pilot, sole on board, was killed.
Probable cause:
Occurrence #1: airframe/component/system failure/malfunction
Phase of operation: unknown
Findings
1. (c) exhaust system, manifold/pipe - corroded
2. (c) maintenance, inspection - inadequate - company maintenance personnel
3. (f) procedure inadequate - manufacturer
4. (f) inadequate surveillance of operation - faa (organization)
5. (c) exhaust system, manifold/pipe - failure,total
6. (c) exhaust system, manifold/pipe - leak
----------
Occurrence #2: loss of engine power (partial) - mech failure/malf
Phase of operation: cruise - normal
Findings
7. Initiated - pilot in command
----------
Occurrence #3: fire
Phase of operation: descent
Findings
8. (c) miscellaneous - fire
9. Wing, spar - burned
----------
Occurrence #4: airframe/component/system failure/malfunction
Phase of operation: descent
Findings
10. (c) wing - failure, total
11. Wing - separation
----------
Occurrence #5: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Final Report:

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

Date & Time: Feb 15, 1983 at 1102 LT
Operator:
Registration:
N361V
Survivors:
Yes
Schedule:
Boise - Hailey
MSN:
361
YOM:
1973
Flight number:
SPA868
Crew on board:
2
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
12000
Captain / Total hours on type:
1000.00
Copilot / Total flying hours:
275
Copilot / Total hours on type:
100
Aircraft flight hours:
4767
Circumstances:
About 1100 mst, on February 15,1983, a Sierra Pacific Airlines DHC-6, operating as Transwestern Flight 868, crashed during its final approach to a landing on runway 31, 1.7 mile south of the Friedman Memorial Airport at Hailey, Idaho. Flight 868 was a regularly scheduled commuter passenger flight between Boise and Hailey, Idaho. There were two flightcrew members and six passengers on board the flight. One passenger escaped with minor injuries, but all the other occupants sustained serious injuries in the accident. There was no fire. About 800 feet above the small town of Bellevue, 2 miles south of the airport, the captain reduced power in order to configure the airplane for its final approach. Immediately afterward, the captain realized that he had lost eleva control of the airplane. The airplane nosed over and descended steeply. The captain attempted to control the pitch of the airplane by adding power; it began to recover but it crash landed on a highway in a slight nosedown attitude, with the right wing slightly down The airplane then veered off the highway, struck a 4-foot-high snowbank, and broke apart.
Probable cause:
The in-flight loss of elevator control following separation of the control rod from the torque tube at a connection where the company's maintenance department had used a non-standard, unsecured bolt, which the company's inspection department had failed to detect. Contributing to the accident was the company's failure to maintain the separation of maintenance and inspection functions required by the maintenance program approved by the Federal Aviation Administration, and the failure of the FAA to detect the company's deviation from approved maintenance procedures during surveillance inspection.
Final Report:

Crash of a Cessna T207A Skywagon in Boise

Date & Time: Aug 27, 1982 at 1339 LT
Operator:
Registration:
N7306U
Flight Phase:
Survivors:
Yes
Schedule:
Boise - Salmon
MSN:
207-0393
YOM:
1977
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
1086
Captain / Total hours on type:
417.00
Aircraft flight hours:
2811
Circumstances:
Before takeoff, the pilot filed a company flight plan for a VFR flight from Boise to Salmon, ID. He reported that during initial climb, the engine surged, then seemed to return to normal operation. He reduced the power to 33 inches of manifold pressure and set the propeller to 2,550 rpm. Shortly thereafter, the engine began losing power again, there was a second surge, then the propeller stopped. During an emergency landing, the pilot elected to cross over a road and land in an open field. He saw a power line along the road at the edge of the field and elected to cross under it to land. However, he did not see a single telephone pole on the opposite side of the road. The left wing struck the pole and the plane cartwheeled and crashed. Three occupants escaped with minor injuries and four others were uninjured. An investigation revealed that the crankshaft had failed from fatigue.
Probable cause:
Occurrence #1: loss of engine power(total) - mech failure/malf
Phase of operation: takeoff - initial climb
Findings
1. (c) engine assembly,crankshaft - fatigue
----------
Occurrence #2: forced landing
Phase of operation: approach
----------
Occurrence #3: in flight collision with object
Phase of operation: approach - vfr pattern - final approach
Findings
2. (f) terrain condition - high obstruction(s)
3. Maneuver - performed - pilot in command
4. (f) object - utility pole
----------
Occurrence #4: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Final Report:

Crash of a Rockwell Aero Commander 500B in Twin Falls

Date & Time: Apr 2, 1977 at 0355 LT
Registration:
N223LH
Flight Type:
Survivors:
Yes
Schedule:
Twin Falls – Boise – Twin Falls – Pocatello – Boise – Twin Falls
MSN:
500-1528-188
YOM:
1965
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4963
Captain / Total hours on type:
63.00
Circumstances:
While descending by night to Twin Falls, both engines stopped simultaneously. Due to loss of speed, the airplane lost height. The pilot elected to make an emergency landing when the airplane struck power cables and crashed in a snow covered field. The pilot was injured and the aircraft was damaged beyond repair.
Probable cause:
Double engine failure caused by a fuel exhaustion. The following contributing factors were reported:
- Collision with wires/poles,
- Mismanagement of fuel,
- Miscalculated fuel consumption,
- Fuel exhaustion,
- High obstructions.
Final Report:

Crash of a Douglas B-26C Invader in Boise: 1 killed

Date & Time: Aug 1, 1974 at 1935 LT
Type of aircraft:
Operator:
Registration:
N91354
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Boise - Boise
MSN:
7181
YOM:
1941
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
16549
Captain / Total hours on type:
729.00
Circumstances:
The pilot, sole on board, was preparing for a local fire fighting mission. While taxiing on the apron, the Invader collided with a private Beechcraft M24R registered N2529W with one pilot on board. Following the collision, both aircraft caught fire and were destroyed. The pilot on board the Beechcraft was killed instantly while the pilot on board the Invader was seriously injured. He died three days later from his injuries.
Probable cause:
Diverted attention from operation of aircraft. The following contributing factors were reported:
- Failed to see and avoid other aircraft,
- ATC failed to advise crew about other traffic,
- Invader taxiing east and Beechcraft taxiing north.
Final Report:

Crash of a Beechcraft 65-B80 Queen Air near Fairfield: 5 killed

Date & Time: Feb 20, 1972 at 1032 LT
Type of aircraft:
Operator:
Registration:
N1027C
Flight Phase:
Survivors:
No
Schedule:
Hailey - Boise
MSN:
LD-309
YOM:
1966
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
12179
Captain / Total hours on type:
612.00
Circumstances:
While in cruising altitude, the left engine caught fire and exploded. Shortly later, the left wing separated. Out of control, the airplane dove into the ground and crashed near Fairfield, killing all five occupants.
Probable cause:
Engine failure in normal cruise followed by an airframe failure. The following factors were reported:
- Improper maintenance by maintenance personnel,
- Powerplant failure due to cylinder assembly which was improperly installed,
- Engine fire,
- Fire in brakes, wheel assembly and wheel well,
- Separation in flight,
- Cylinder separation,
- Excessive working hours may have contributed.
Final Report:

Crash of a Hawker-Siddeley HS.125-1A in Boise: 2 killed

Date & Time: Dec 28, 1970 at 1837 LT
Type of aircraft:
Operator:
Registration:
N36MK
Survivors:
No
Site:
Schedule:
Billings - Boise
MSN:
25073
YOM:
1966
Location:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
16871
Captain / Total hours on type:
2183.00
Circumstances:
While descending to Boise International Airport by night and marginal weather conditions, the crew failed to realize his altitude was too low when the airplane struck a mountain located 10 miles northeast of the airfield. The aircraft was totally destroyed and both pilots were killed.
Probable cause:
Improper IFR operation on part of the crew who failed to follow the approved procedures. The following factors were reported:
- Instruments misread or failed to read,
- Aircraft northeast circling, ILS approach to runway 10L,
- Leveling at 10,000 feet then descended below the minimum safe altitude of 8,600 feet until striking the ground at an altitude of 5'690 feet MSL.
Final Report:

Crash of a Stinson V-77 Reliant in Boise: 2 killed

Date & Time: Oct 16, 1965 at 1745 LT
Type of aircraft:
Registration:
N60361
Flight Type:
Survivors:
No
Schedule:
Boise - Boise
MSN:
77-43
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
5000
Captain / Total hours on type:
100.00
Circumstances:
On approach to Boise Airport, the pilot initiated a go-around procedure when the aircraft struck a dirt bank and crashed, bursting into flames. Both occupants, performing a demo flight, were killed.
Probable cause:
The pilot delayed in initiating go-around procedure and seat belt was not fastened.
Final Report:

Crash of a Beechcraft Queen Air 65 in Billings: 4 killed

Date & Time: Apr 27, 1964 at 1005 LT
Type of aircraft:
Registration:
N451H
Survivors:
No
Schedule:
Boise – Billings
MSN:
LC-90
YOM:
1961
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
7041
Circumstances:
On final approach to Billings-Logan Airport, one of the engine failed. Control was lost and the airplane crashed in flames onto a house. The aircraft was destroyed and all four occupants were killed.
Probable cause:
The accident was caused by a mismanagement of fuel on part of the crew. Due to inadequate supervision of flight, a fuel starvation occurred.
Contributing factors were:
- Improper emergency procedures,
- Partial loss of power on one engine,
- Complete engine failure/flameout on one engine,
- Fire after impact.
Final Report:

Crash of a Douglas DC-3-194H in Elk Mountain: 21 killed

Date & Time: Jan 31, 1946 at 0247 LT
Type of aircraft:
Operator:
Registration:
NC25675
Flight Phase:
Survivors:
No
Site:
Schedule:
Portland – Pendleton – Boise – Denver
MSN:
2147
YOM:
1939
Flight number:
UA014
Crew on board:
3
Crew fatalities:
Pax on board:
18
Pax fatalities:
Other fatalities:
Total fatalities:
21
Captain / Total flying hours:
13003
Captain / Total hours on type:
2909.00
Copilot / Total flying hours:
2021
Copilot / Total hours on type:
21
Aircraft flight hours:
16333
Circumstances:
On the non stop leg from Boise to Denver, while flying by night and poor visibility, the aircraft hit the slope of Mt Elk located southeast of Elk Mountain, south Wyoming. The wreckage was found few hours later in a deep snow and in poor weather conditions, about 340 feet from the summit. The aircraft was destroyed by impact forces and all 21 occupants were killed. At the time of the accident, the aircraft deviated from the prescribed flight path by 4,5 miles and its altitude was 11,000 feet.
Probable cause:
On the basis of the foregoing the Board finds that the probable cause of this accident was the deviation from the prescribed route at an altitude insufficient to assure adequate clearance over Elk Mountain.
Final Report: