Crash of a Beechcraft 99A Airliner in Spokane: 7 killed

Date & Time: Jan 20, 1981 at 1127 LT
Type of aircraft:
Operator:
Registration:
N390CA
Survivors:
Yes
Schedule:
Seattle - Moses Lake - Spokane
MSN:
U-101
YOM:
1969
Flight number:
CZ201
Crew on board:
2
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
7
Captain / Total flying hours:
11680
Captain / Total hours on type:
7000.00
Copilot / Total flying hours:
8242
Copilot / Total hours on type:
3102
Aircraft flight hours:
23322
Circumstances:
The aircraft crashed during an instrument approach in IMC at Spokane-Intl Airport. The aircraft hit a hill about 4.5 miles from the runway threshold at an elevation of 2,546 feet. The minimum descent altitude for the instrument approach procedure was 2,760 feet. Of the nine persons aboard flight 201, seven were killed and two were injured seriously. The instrument approach procedure the fiightcrew used required that a altitude of 3,500 feet be maintained until the aircraft passed the final approach fix, located 4,5 miles from the runway threshold. The aircraft impacted the ground near the location of the final approach fix, which was about 1,800 feet southeast of the Spokane VORTAC.
Probable cause:
A premature descent to minimum descent altitude (MDA) based on the flight crew's use of an incorrect distance measuring equipment (DME) frequency and the flight crew's subsequent failure to remain at or above MDA. Contributing to the cause of the accident was the design of the DME mode selector which does not depict the frequency selected and the failure of the flight crew to identify the localizer DME facility.
Final Report:

Crash of a Lockheed P-3A-55-LO Orion at Whidbey Island NAS

Date & Time: Jan 18, 1981
Type of aircraft:
Operator:
Registration:
152161
Flight Type:
Survivors:
Yes
Schedule:
Whidbey Island - Whidbey Island
MSN:
185-5131
YOM:
1965
Crew on board:
7
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
While conducting a Naval Air Training and Operating Procedures Standardization check the pilot at controls was allowed to perform his first attempt at shooting an obstacle approach at Whidbey Island NAS. This maneuver was inadequately briefed by the pilot in command during the mission brief. The pilot in command, having great confidence in the pilot at controls, allowed him to conduct this maneuver without prior demonstration. After pushing over for the approach an excessive sink rate developed. Upon determination that the approach was getting dangerous, power was applied and the nose pulled up. Due to the combination of slow approach speed, late and in inadequate power application, the excessive sink rate was not arrested, resulting in a hard landing followed by failure of the starboard wing.
Probable cause:
The accident was the consequence of the following factors:
- The pilot-in-command failed to recognize a dangerous situation and take appropriate corrective action,
- The pilot at controls failed to properly compensate for excessive sink rate during landing transition,
- The pilot at controls began transition to landing attitude too late to arrest a high rate of descent for the power applied,
- Poor crew coordination.

Crash of a Rockwell Aero Commander 700 in Everett: 5 killed

Date & Time: Feb 15, 1980 at 1615 LT
Registration:
N9908S
Flight Phase:
Survivors:
Yes
Schedule:
Everett - Portland
MSN:
700-08
YOM:
1978
Crew on board:
1
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
2567
Captain / Total hours on type:
66.00
Circumstances:
Shortly after takeoff from Everett-Paine Field Airport, the twin engine airplane encountered difficulties to climb, stalled and crashed. Two passengers were seriously injured while five other occupants were killed.
Probable cause:
Stall during initial climb due to inadequate preflight preparation on part of the pilot. The following contributing factors were reported:
- Airframe ice,
- Improperly loaded aircraft,
- 1,000 lbs over max gross weight,
- CofG 1,59 inch behind aft limit,
- Ice and snow on wings and tail prior to takeoff.
Final Report:

Crash of a SCAN-30 near Skykomish: 4 killed

Date & Time: May 27, 1979
Type of aircraft:
Registration:
N4451
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Wenatchee - Stevens Lake
MSN:
33
YOM:
1949
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
712
Captain / Total hours on type:
49.00
Circumstances:
The seaplane was completing a flight from Wenatchee to Lake Stevens, carrying three passengers and one pilot. While cruising under VFR mode into adverse weather conditions, the airplane struck the slope of a mountain and crashed in the region of Skykomish. SAR operations were initiated but eventually abandoned after few days as no trace of the aircraft nor the four occupants was found. The wreckage was discovered by walkers in an isolated area on July 20, 1979.
Probable cause:
Controlled flight into terrain after the pilot continued VFR flight into adverse weather conditions. The following contributing factors were reported:
- High obstructions,
- low ceiling,
- Rain,
- Thunderstorm activity,
- Visibility less than a quarter of a mile.
Final Report:

Crash of a Cessna 207 Skywagon in Olga

Date & Time: Jul 11, 1978 at 0815 LT
Operator:
Registration:
N91041
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Anacortes - Eastsound
MSN:
207-0028
YOM:
1969
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
1094
Captain / Total hours on type:
93.00
Circumstances:
En route from Anacortes to Eastsound Airport (Orcas Island), weather conditions deteriorated. Flying at an insufficient height in low ceiling and fog, the single engine airplane struck trees and crashed. The pilot was injured and the airplane was destroyed.
Probable cause:
Controlled collision with trees in normal cruise due to improper in-flight decisions on part of the pilot who continued VFR flight into adverse weather conditions. The following contributing factors were reported:
- Low ceiling,
- Fog,
- High obstructions.
Final Report:

Crash of a Beechcraft 99 Airliner in Richland: 17 killed

Date & Time: Feb 10, 1978 at 1650 LT
Type of aircraft:
Operator:
Registration:
N199EA
Flight Phase:
Survivors:
No
Schedule:
Richland - Seattle
MSN:
U-037
YOM:
1968
Flight number:
EV023
Crew on board:
2
Crew fatalities:
Pax on board:
15
Pax fatalities:
Other fatalities:
Total fatalities:
17
Captain / Total flying hours:
3250
Captain / Total hours on type:
300.00
Copilot / Total flying hours:
1061
Copilot / Total hours on type:
199
Aircraft flight hours:
13701
Circumstances:
Columbia Pacific Airlines Flight 23, a Beech 99 (N199EA), was operated under the provisions of 14 CFR 135 as a regularly scheduled passenger flight from Richland to Seattle, Washington. The crew arrived at Richland at 1525 P.s.t. on Flight 18 from Seattle. When they arrived, N199EA was being inspected to fulfill the requirements of an Airworthiness Directive. The aircraft was not available to the crew for preflight inspection until 1630; Flight 23 was scheduled to depart at 1640. At 1628, the captain was briefed on weather by the Walla Walla, Washington, Flight Service Station (FSS), and he filed a dispatch release which contained aircraft weight and balance, route of flight, and weather information. About 1630, the aircraft was fueled and 600 lbs of baggage was loaded. About 1635, the first officer left the terminal building and connected the auxiliary power unit to the aircraft. He then inspected the aircraft and boarded; the captain boarded shortly thereafter. When the passenger boarding call was made, the captain left the aircraft to obtain magazines for the passengers. He was seen getting into his seat when the first passenger boarded. At 1646, the first officer contacted the Pasco Airport Traffic Control Tower, using Flight No. 29, and advised that they were taxiing and would request an instrument flight rules clearance to Seattle via Yakima, Washington, when airborne. The Pasco Control Tower received no further calls from Flight 23. The first officer informed operations on company frequency that they would be departing shortly and would relay their estimated time of arrival in Seattle when airborne. There were no further radio communications with the crew. The aircraft daily flight log for February 10 showed that the aircraft left the ramp at 1645 and took off at 1648. In general, witnesses described the aircraft's attitude at liftoff as normal and estimated the point of liftoff between 1,173 and 1,486 ft; however, immediately thereafter the aircraft began a steep climb at an angle of 20' to 45" to an altitude of 300 to 400 ft above the runway and then appeared to decelerate. The wings rocked or wobbled at the top of the climb, and the aircraft turned or yawed to the left.
The nose dropped and the aircraft descended to the ground at a flightpath angle estimated to have been 45°. Fuel from ruptured fuel tanks caught fire after the aircraft hit the ground. Fire consumed the aircraft within 7 minutes. All 17 occupants were killed.
Probable cause:
The National Transportation Safety Board determines that the probable cause of the accident was the failure or inability of the flightcrew to prevent a rapid pitchup and stall by exerting sufficient push force on the control wheel. The pitchup was induced by the combination of a mistrimmed horizontal stabilizer and a center of gravity near the aircraft's aft limit. The mistrimed condition resulted from discrepancies in the aircraft's trim system and the flightcrew's probable preoccupation with making a timely departure. Additionally, a malfunctioning stabilizer trim actuator detracted from the flightcrew's efforts to prevent the stall. Contributing to the accident were inadequate flightcrew training, inadequate trim warning system check procedures, inadequate maintenance procedures, and ineffective FAA surveillance.
Final Report:

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

Date & Time: Oct 8, 1977 at 0825 LT
Type of aircraft:
Registration:
N117HC
Flight Phase:
Survivors:
No
Schedule:
Vancouver - Penticton
MSN:
31P-54
YOM:
1971
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
7200
Captain / Total hours on type:
700.00
Circumstances:
Shortly after takeoff from Vancouver Airport, south Washington, the airplane encountered difficulties to gain height when it stall and crashed in flames. All three occupants were killed.
Probable cause:
Stall after engine failure during initial climb. The following contributing factors were reported:
- Powerplant - ignition system: spark plug,
- Failed to maintain flying speed,
- Improper maintenance,
- Powerplant - propeller and accessories: other,
- Directional control problem,
- Prop slow to feather,
- No aircharge,
- Pilot unable to maintain directional control.
Final Report:

Crash of a De Havilland DHC-2 Beaver near Stevens Pass: 7 killed

Date & Time: Oct 1, 1977 at 1400 LT
Type of aircraft:
Operator:
Registration:
N64391
Flight Phase:
Survivors:
No
Site:
Schedule:
Kenmore – Lake Hatheume – Penticton
MSN:
1145
YOM:
1958
Crew on board:
1
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
7
Captain / Total flying hours:
4122
Captain / Total hours on type:
799.00
Circumstances:
While flying at low altitude over mountainous terrain, the pilot entered a canyon and was approaching a mountain pass when he elected to gain height. Unable to outclimb the rising terrain, the single engine airplane struck trees and crashed in a wooded area located near Stevens Pass, in the Cascade Mountain Range. The wreckage was found few hours later and all seven occupants were killed.
Probable cause:
Collision with trees due to improper in-flight decisions on part of the pilot. The following contributing factors were reported:
- Unwarranted low flying,
- Misjudged distance, speed and altitude,
- Inadequate preflight preparation,
- Improperly loaded aircraft, weight and CofG.,
- High obstructions,
- Exceeded gross weight and aft CofG.
Final Report:

Crash of a Rockwell Grand Commander 680FP in Fall City: 1 killed

Date & Time: Aug 27, 1976 at 1550 LT
Registration:
N680FP
Flight Phase:
Survivors:
No
Schedule:
Wenatchee - Seattle
MSN:
680-1322-135
YOM:
1963
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
950
Circumstances:
The pilot started the descent to Seattle-Boeing Field Airport when the left engine failed. The airplane entered a dive, went through the clouds and crashed in flames in Fall City. The pilot, sole on board, was killed.
Probable cause:
Uncontrolled descent following an in-flight powerplant failure for undetermined reasons. The following contributing factors were reported:
- Failed to maintain flying speed,
- Improper operation of flight controls,
- Cause of feathered propeller could not be found,
- Observed spinning out of clouds.
Final Report:

Crash of a Cessna 207 Skywagon in Friday Harbor: 7 killed

Date & Time: Apr 8, 1976 at 0725 LT
Registration:
N1645U
Survivors:
No
Schedule:
Burlington - Friday Harbor
MSN:
207-0245
YOM:
1974
Crew on board:
1
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
7
Captain / Total flying hours:
1685
Captain / Total hours on type:
883.00
Circumstances:
While approaching Friday harbor, weather conditions worsened with a limited visibility to half of mile due to fog and low ceiling. Unable to locate the runway, the pilot decided to initiate a go-around when he lost control of the airplane that crashed in flames. The aircraft was totally destroyed and all seven occupants have been killed.
Probable cause:
Stall during a go-around procedure due to inadequate supervision of flight crew. The following contributing factors were reported:
- Continued VFR flight into adverse weather conditions,
- Spatial disorientation,
- Failed to maintain flying speed,
- Premature flap retraction,
- Low ceiling,
- Fog,
- Limited visibility to half a mile,
- Weather conditions below minimums,
- Aircraft loaded near max gross weight and CofG near aft limit.
Final Report: