Zone

Crash of a De Havilland DHC-2 Beaver near Pelican: 2 killed

Date & Time: Apr 19, 1989 at 1315 LT
Type of aircraft:
Registration:
N62873
Flight Phase:
Survivors:
No
Site:
Schedule:
Juneau - Pelican
MSN:
323
YOM:
1952
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
4800
Captain / Total hours on type:
460.00
Aircraft flight hours:
18800
Circumstances:
During a flight from Juneau to Pelican, AK, the aircraft collided with terrain approximately 12 miles east of Pelican while crossing over Chichagof Island. Impact occurred on a vertical rock wall at an elevation of about 1,950 feet. No preimpact part failure or malfunction of the aircraft was evident. Another pilot, who had planned to fly the same route about 1 hr and 45 min earlier, decided to fly around the island due to low clouds, rain and fog in the area. He reported that he flew over icy straits rather than take a more direct route and that ceilings were about 2,000 feet broken with lower stratus in the valleys. A helicopter pilot said he was unable to work in mountain passes in the vicinity of the accident due to low clouds, rain and fog; he also said the passes were 'socked in.' Both occupants were killed.
Probable cause:
Improper in-flight decision by the pilot, and his inadvertent flight into instrument meteorological conditions (IMC). The terrain and weather conditions were considered to be factors.
Final Report:

Crash of a De Havilland DHC-2 Beaver in Pelican

Date & Time: Jul 3, 1978 at 1930 LT
Type of aircraft:
Registration:
N8690
Flight Phase:
Survivors:
Yes
Schedule:
Elfin Cove - Herbert Graves Island
MSN:
811
YOM:
1955
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
5150
Captain / Total hours on type:
125.00
Circumstances:
While cruising under VFR mode in adverse weather conditions, the pilot entered a narrow channel at an altitude of 100 feet when he lost control of the aircraft that spiraled to the ground. The wreckage was found in the region of Pelican. All three occupants were injured and the aircraft was destroyed.
Probable cause:
Stall during normal cruise due to improper in-flight decisions. The following contributing factors were reported:
- Continued VFR flight into adverse weather conditions,
- Failed to maintain flying speed,
- Low ceiling,
- Fog,
- High obstructions,
- Flew to blind canyon,
- Float equipped,
- Entered narrow channel at 100 feet AGL.
Final Report:

Crash of a Grumman G-44 Widgeon near Pelican: 1 killed

Date & Time: Nov 4, 1954 at 1310 LT
Type of aircraft:
Operator:
Registration:
N67794
Flight Phase:
Survivors:
Yes
Schedule:
Sitka – Pelican – Hoonah – Juneau
MSN:
1321
YOM:
1943
Flight number:
ACA060
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
14000
Captain / Total hours on type:
600.00
Aircraft flight hours:
2763
Circumstances:
Flight 60 originated at Sitka, Alaska, with stops scheduled at Pelican City, Hoonah, and Juneau, the destination. Before departure from Sitka, the dispatcher in Juneau issued clearance for the flight to proceed DVFR (Defense Visual Flight Rules) to Hoonah and wait, if necessary, at that station for weather to improve in the Juneau area. The flight plan indicated estimated time from Sitka to Juneau, including stops, would be two hours and fifty minutes. Fuel consumption was estimated at 60 gallons, with 20 gallons re-serve upon arrival at Juneau. Gross weight of all disposable load at takeoff was 1,401 pounds, 30 less than the maximum allowable. The flight departed Sitka at 1153 with Captain James C. Rinehart (pilot), four passengers, cargo, mail, and baggage. The route between Sitka and Pelican City follows the North Pacific shore. The flight landed at Pelican City at 1235. Two passengers deplaned and 88 pounds of baggage, mail, and cargo were taken off; 159 pounds of cargo were added. The aircraft was not refueled. The pilot reported by radio that the flight departed Pelican City at 1305 en route to Hoonah. This was the last radio contact. When the flight became overdue at Hoonah, search operations were instituted. The Coast Guard was notified at 1655 and began search. At approximately 0800 the following morning, the pilot of a private aircraft located the wreckage in a mountain pass several miles southeast of Pelican City. A Coast Guard and civilian ground rescue party arrived the afternoon of November 5, rendered first aid to the two passengers, and stayed until the survivors and the body of the pilot were evacuated by helicopter on November 6.
Probable cause:
The Board determines that the probable cause of this accident was loss of control of the aircraft during a steep turn in severe turbulence while the pilot was attempting to conduct visual flight at less than the required altitude and weather minimums. The following findings were reported:
- Weather conditions within the pass were: Rain, fog, severe turbulence, and low ceiling, with the base of the clouds extending about halfway down the 3,000-foot mountain slopes,
- Flight 60 crashed one-fourth mile due south of the summit of the pass about 1.500 feet above mean sea level, the pilot having negotiated about three miles of its 10-mile length,
- The aircraft struck the ground on a west heading at a sharp bend in the narrow pass, having encountered strong turbulence in a steep left bank at low altitude,
- The pilot had reversed course when the accident occurred,
- The two passengers survived but the pilot was fatally injured,
- Alaska Coastal Airlines flights in this type aircraft are restricted to Defense Visual Flight Rules operations,
- The Alaska Coastal Airlines operations manual specified that the pass must be flown at 3,000 feet altitude,
- The pilot was attempting to negotiate the pass at less than the altitude specified in the operations manual and in weather conditions which were lower than DVFR requirements.
Final Report: