Crash of a Beechcraft C-45G Expeditor in Kasilof

Date & Time: Aug 5, 1977 at 2200 LT
Type of aircraft:
Operator:
Registration:
N2853G
Survivors:
Yes
Schedule:
Tyonek - Kasilof
MSN:
AF-188
YOM:
1952
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
2907
Captain / Total hours on type:
250.00
Circumstances:
During an adverse bounced landing at Kasilof Airstrip, the cargo shifted and the airplane went out of control. It crashed and came to rest in flames. Both occupants were seriously injured and the aircraft was destroyed.
Probable cause:
Uncontrolled collision with ground after the 2,000 pounds cargo shifted upon landing. The following contributing factors were reported:
- Inadequate preflight preparation,
- Cargo not tied down.
Final Report:

Crash of a De Havilland DHC-3 Otter in Alatna River: 1 killed

Date & Time: Aug 4, 1977 at 1905 LT
Type of aircraft:
Operator:
Registration:
N48064
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Alatna River - Bettles
MSN:
278
YOM:
1958
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
5000
Captain / Total hours on type:
1500.00
Circumstances:
The pilot took off from a gravel bar adjacent to the Alatna River, bound for Bettles. After departure, the single engine airplane encountered difficulties to gain height, struck trees and crashed in flames. The aircraft was destroyed by a post crash fire and the pilot, sole on board, was killed.
Probable cause:
Stall during initial climb due to misuse of flaps. The following contributing factors were reported:
- Failed to obtain flying speed,
- Misjudged distance, speed and altitude,
- Failed to abort takeoff,
- Loose gravel,
- High obstructions,
- Downdrafts, updrafts,
- Obstructions to vision,
- Evasive maneuver to avoid collision,
- Takeoff from rvr gravel bar toward bend in river,
- Trees, steep rvr bank at bend.
Final Report:

Crash of a Beechcraft E90 King Air in Sitka: 5 killed

Date & Time: Jul 31, 1977 at 0130 LT
Type of aircraft:
Registration:
N4207S
Flight Type:
Survivors:
No
Site:
Schedule:
King Salmon - Sitka
MSN:
LW-207
YOM:
1977
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
2800
Captain / Total hours on type:
20.00
Circumstances:
While descending to Sitka in limited visibility, the twin engine airplane struck a mountain and crashed few miles from the destination. The aircraft was destroyed upon impact and all five occupants were killed.
Probable cause:
Controlled flight into terrain on final approach. The following contributing factors were reported:
- Improper IFR operation,
- Lack of familiarity with aircraft,
- Mountains adjacent to Sitka obscured.
Final Report:

Crash of a Britten-Norman BN-2A-6 Islander in Ruby: 1 killed

Date & Time: Jul 21, 1977 at 1845 LT
Type of aircraft:
Registration:
N22JA
Flight Phase:
Survivors:
Yes
Schedule:
Ruby - Colorado Creek
MSN:
264
YOM:
1971
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
3675
Captain / Total hours on type:
400.00
Circumstances:
At takeoff from an unsuitable terrain, the twin engine airplane went out of control and crashed. A passenger was killed while three other occupants were injured.
Probable cause:
The pilot selected unsuitable terrain and misjudged speed and clearance.
Final Report:

Crash of a Rockwell Grand Commander 680FL in Savoonga

Date & Time: Feb 19, 1977 at 1050 LT
Operator:
Registration:
N112NA
Survivors:
Yes
Schedule:
Nome - Savoonga
MSN:
680-1750-145
YOM:
1968
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
19076
Captain / Total hours on type:
321.00
Circumstances:
While descending to Savoonga, the pilot encountered poor weather conditions when the airplane struck the ground few miles from the airstrip. All three occupants were injured and the aircraft was destroyed. The accident occurred in whiteout conditions (IMC conditions) with a 500 feet ceiling.
Probable cause:
Controlled flight into terrain in traffic pattern-circling after the pilot continued VFR flight into adverse weather conditions. The following contributing factors were reported:
- Ice propeller,
- Airframe ice,
- Whiteout conditions,
- Icing conditions including sleet and freezing rain,
- Low ceiling,
- Visibility below minimums.
Final Report:

Crash of a Beechcraft U-21A Ute in the Cook Inlet: 7 killed

Date & Time: Feb 10, 1977
Type of aircraft:
Operator:
Registration:
67-18081
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Elmendorf - King Salmon
MSN:
LM-81
YOM:
1967
Crew on board:
2
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
7
Circumstances:
Few minutes after takeoff from Elmendorf AFB, while cruising in IMC conditions, the crew contacted ATC and requested the permission to obtain a higher level of flight. Shortly later, the airplane went out of control and crashed in the Cook Inlet. Intensive SAR operations were conducted but no trace of the airplane nor the seven occupants was ever found.
Crew:
Cpt Donald W. Deeter, pilot,
CW3 Ralph G. Battle, pilot,
Passengers:
SP4 Paul E. Jones,
Ltc William I. Barrett Jr.,
Ltc John S. Edge,
Maj James W. Nelson,
Maj Melvin J. Swiney.

Crash of a Chase YC-122C Avitruc in Anchorage: 1 killed

Date & Time: Jan 31, 1977 at 1416 LT
Type of aircraft:
Operator:
Registration:
N5904V
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Anchorage - Nome
MSN:
CY-886
YOM:
1954
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
5226
Captain / Total hours on type:
5.00
Circumstances:
Shortly after takeoff from Anchorage-Intl Airport, while climbing, the airplane stalled and crashed. A crew member was killed while two others were seriously injured.
Probable cause:
Stall during initial climb after the pilot-in-command failed to maintain flying speed. The following contributing factors were reported:
- Inadequate preflight preparation,
- Airframe ice,
- Frost found on wings after impact.
Final Report:

Crash of a Douglas DC-8-62AF in Anchorage: 5 killed

Date & Time: Jan 13, 1977 at 0635 LT
Type of aircraft:
Operator:
Registration:
JA8054
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Moses Lake - Anchorage - Tokyo
MSN:
46148/553
YOM:
1971
Flight number:
JL8054
Crew on board:
5
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
23252
Captain / Total hours on type:
4040.00
Copilot / Total flying hours:
1603
Copilot / Total hours on type:
1207
Aircraft flight hours:
19744
Circumstances:
On January 13, 1977, a Japan Air Line (JAL) McDonnell-Douglas DC-8-62F, JA 8054, operated as an international charter cargo flight from Moses Lake, Washington, U.S.A., to Tokyo, Japan. An en route stop and crew change were scheduled at Anchorage, Alaska. The aircraft arrived at Anchorage at 0503. The incoming flightcrew reported that the only weather they encountered en route was a layer of fog on the final approach at 800 feet, and that they did not encounter any precipitation or icing. The aircraft was serviced and a walk-around inspection was performed by JAL maintenance personnel and contract mechanics. The two contract mechanics stated that there was ice on the inlet guide vanes, the engine cowlings, and the engine bullet noses, but no ice was reported on the airfoil surfaces. The JAL personnel stated that they did not see any ice on the aircraft. One contract mechanic advised the JAL representative that the engine anti-icing system should be used by the next crew to clear the ice in the engine inlets. No maintenance was performed on the aircraft. The outbound flightcrew was wakened about 0330, left the hotel by taxi about 0430, and arrived at the JAL dispatch office about 0 0500. The taxicab driver who brought the outbound crew to the airport stated that he became concerned by the captain's actions in the taxi and called his dispatcher to report his impressions. He stated that the captain's movements were uncoordinated; that his face was flushed and his eyes were glazed; that his conversation was garbled and incoherent; that his movements were jerky and unstable; and that he had trouble getting out of the cab and had to steady himself on the car door. About 0450 the taxi dispatcher called the operations agent for the contract maintenance company and reported that one of her drivers had taken an "intoxicated" JAL captain to the airport. The operations agent stated that "...it seemed logical that JAL would detect anything unusual and act accordingly." He further stated that a 0620, he notified his line manager of the conversation with the taxi dispatcher and that "I felt that if the captain was intoxicated JAL OPS...or his first officer would have stopped the flight immediately." The JAL dispatch personnel and the inbound JAL crew stated that they noted nothing unusual about the outbound crew. The dispatch briefing proceeded smoothly and no significant questions were asked by the outbound crew. The outbound crew consisted of an American captain and a Japanese first officer and flight engineer. They went to the aircraft about 0515 and boarded the aircraft with the two cattle handlers. The driver of the crew car, a friend of the captain, stated that "...he was in good condition as far as way's I've seen him sometimes and I made that statement before I ever heard any rumors that he was supposedly drunk or had been partying or whatever." A review of the cockpit voice recorder (CVR) indicated that about 0603 the captain and first officer were checking the inputs to the inertial navigation system. They also checked the Automatic Terminal Information Service (ATIS) for local visibility, received their clearance, and began their prestart checklists about 0609. The weather on the ATIS report was in part: "...sky partially obscured, visibility one-quarter mile, fog...". The checklists were completed and the takeoff data reviewed. About 0615 the engines were started and the stickshaker (stall warning system) was tested. The after-start checklist was completed and the aircraft was cleared to taxi to runway 24L. During the taxi, the flight engineer requested and received permission from the captain to turn the engine anti-ice system on because of the ice on the inlet guide vanes. The flight controls and spoilers were checked while taxiing and the flaps were extended to 23°. The taxi checklist was completed and the takeoff data, the flap settings, and the trim settings were again reviewed. The captain, in response to the challenge "anti-ice, de-ice, and rain removal," said, "Ok, we will use engine anti-ice." The de-ice system was reported "off'' by the flight engineer. The captain briefed the crew on the takeoff and abort procedures he would use. He commented that the runway was slippery and he didn't think they would abort. The captain taxied the aircraft southeast on the ramp, past the terminal toward runway 24L. He stopped on the ramp after being instructed to hold short of runway 24R. After several communications with the controller, the aircraft taxied onto runway 24R, and reported ''...ready for takeoff." The tower advised the captain that he was on runway 24R which the captain contradicted. The controller then issued taxi instructions to get the aircraft to runway 24L. The captain made a 180° turn on runway 24R before he finally taxied to the taxiway which leads to the approach end of runway 24L. The crew again reported that they were ready for takeoff at 0633:37. Takeoff was initiated and at 0634:32 the captain called "maximum power". At 0634:50 the captain announced, "I have" and at 0634:52, "80" (knots) was called by the copilot. At 0635:10, "Vee one" was called by the copilot and at 0635:16 rotation was called and acknowledged by the captain. At 0635:19.5 the captain called "Ten degrees" and at 0635:21.4 the first officer called V2. At 0635:26.2 a sound similar to aircraft buffet was recorded. This sound became more frequent and continued until the sounds of impact. At 0635:32 the first officer called "Gear up" and at 0635:33 the flight engineer said "Too much speed (steep)".' At 0635: 38 the engineer called "stall" simultaneously the stickshaker sounded and continued until 0635:39.3, when impact was recorded. A witness near the departure end of the runway saw the aircraft climb to an estimated altitude of about 100 feet above the ground, veer to the left, and then slide '... out of the air." The aircraft was totally destroyed upon impact and all five occupants were killed as well as the 56 cows.
Probable cause:
The probable cause of the accident was a stall that resulted from the pilot's control inputs aggravated by airframe icing while the pilot was under the influence of alcohol. Contributing to the cause of this accident was the failure of the other flightcrew members to prevent the captain from attempting the flight.
Final Report:

Crash of a Beechcraft E90 King Air in Tok: 2 killed

Date & Time: Nov 29, 1976 at 1855 LT
Type of aircraft:
Operator:
Registration:
N6843S
Flight Phase:
Survivors:
No
Schedule:
Tok - Anchorage
MSN:
LW-137
YOM:
1975
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
6291
Captain / Total hours on type:
311.00
Circumstances:
Shortly after takeoff from Tok Airport in poor weather conditions, the pilot lost control of the airplane that descended to the ground and crashed near the airport. The aircraft was destroyed and both occupants were killed.
Probable cause:
Uncontrolled descent during initial climb after the pilot suffered a spatial disorientation. The following contributing factors were reported:
- Low ceiling,
- Turbulences associated with clouds and thunderstorms,
- Rain,
- Fog,
- Ceiling at 400 feet,
- Wind gusting to 40 knots.
Final Report:

Crash of a Volpar Turboliner II (G18S) in Dutch Harbor: 5 killed

Date & Time: Jul 22, 1976 at 0905 LT
Type of aircraft:
Registration:
N600WA
Flight Type:
Survivors:
No
Schedule:
Cold Bay - Dutch Harbor
MSN:
BA-463
YOM:
1959
Location:
Crew on board:
2
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
15868
Captain / Total hours on type:
3605.00
Circumstances:
On approach to Dutch Harbor, the crew encountered poor weather conditions. On final, the twin engine airplane was too low and struck the ground few miles short of runway and crashed. The aircraft was destroyed and all five occupants were killed.
Probable cause:
Controlled flight into terrain on final approach following improper IFR operation. The following contributing factors were reported:
- Low ceiling,
- Rain,
- Fog,
- CLGS below 1,000 feet,
- Areas of visibility below 3 miles in drizzle and fog.
Final Report: