- Date
- November 21, 1992, 09:35 local (17:35 UTC)
- Place
- Snoqualmie Pass, WA
- Injuries
- 6 fatal
- Damage
- Destroyed
- Phase of flight
- Enroute
- Aircraft
- N100EKBeech A60
- Weather
- Instrument (IMC) · Day
- Status
- Completed · report July 11, 1994
- Report
- Approved by Office Director
- Safety recommendations
- Yes
- FAA report
- 19921121047529A
- Case key
- 41694
From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.
On this page
Probable cause
The NTSB’s determination of the probable cause, and any contributing factors.
Failure of the pilot to maintain control of the aircraft, his failure to prevent the aircraft from exceeding the never exceed speed (vne), and subsequent exceeding of the design stress limits of the aircraft. Factors related to the accident were: weather conditions (including icing conditions), improper airspeed, and loss of engine power for undetermined reason(s).
Analysis
While climbing in mod icing conds after takeoff, plt was cleared to 17,000'. Radar data showed acft climbed at an indcd airspeed (IAS) of 82 to 123 KTS. A Beech safety info booklet stated that a min airspeed of 140 KTS must be maintained in icing conds. Climbing at reduced airspeed would have increased angle of attack & allowed ice to accumulate under the wings & aft of the de-icing boots. Acft climbed to 13,500', descended momentarily to 13,300', then continued climbing as airspeed decreased abruptly. After slowing to 60 KTS IAS at 13,700', the acft entered a steep descending turn & accelerated to high speed (above vne). An emergency was declared, stating the aircraft 'lost an engine.' Soon there- after, radar contact was lost & the acft crashed. Pieces of empennage surfaces separated in flight & were found at remote location from the main wreckage. Both counterweights separated from the elevators. Post-crash tests disclosed no mechanical evidence of engine malfunction. Low ceiling, fog, light rain, snow & icing conditions were rprtd in area.
Factual narrative
The factual narrative1,338 words
History of flight
On November 21, 1992, at approximately 0935 Pacific standard time (PST), a Beech A 60, N100EK, impacted the terrain about two miles west of Snoqualmie Pass, Washington. The FAA certificated commercial pilot and his five passengers received fatal injuries, and the aircraft was destroyed. The pleasure flight, which departed Boeing Field/King County International Airport at 0917 PST, was in instrument meteorological conditions at the time of the accident. The aircraft, which was on an instrument flight plan to Pullman, Washington, was located as the result of the activation of the ELT.
According to information retrieved from a recording of the pilot's weather briefing, the purpose of the flight was to attended a college football game in Pullman, Washington. The pilot indicated to the briefer that it was his intention to fly to Pullman for the game, remain overnight in the Pullman area, and then to return to the Seattle area the following day.
At about 0650 PST, on the day of the flight, the pilot telephoned Seattle Flight Service and requested a briefing for an IFR flight from Boeing Field to Pullman, Washington. He received a standard briefing from Flight Service, and then filed his IFR flight plan.
At 0909 PST, the pilot of 100EK received his IFR clearance from Boeing Tower, followed one minute later by his taxi clearance. At 0916 the flight was cleared for takeoff, and then after departure was given a frequency change to Seattle Departure at about 0919. Seattle Departure issued the pilot an initial climb clearance to 4,000 feet, directed the pilot to turn left to a heading of 100 degrees to join Victor Airway #120, and then issued a further clearance to climb to 15,000 feet. At 0929 the flight was handed off to Seattle Center.
On initial contact with Center, 100EK was cleared to climb to 17,000 feet, after which the pilot requested a clearance for PULLMAN direct when Center was able to give it to him. At 0930:05, Seattle Center advised the pilot of 100EK to expect BIDDY direct in about eight miles, and requested his current altitude. The pilot responded that he was passing through 10,700 feet at that time. For the next four minutes there was no radio communication with 100EK. Then, at 0934:26 Seattle Center cleared 100EK direct BIDDY direct PULLMAN. The pilot did not make a radio response to this clearance, and no transmissions were received from 100EK for a period of 14 seconds after the clearance was transmitted by Center. Then, at 0934:40, a noisy radio transmission, with a considerable amount of background cockpit noise, was received by Seattle Center. A later review of the audio tape revealed that the person making the transmission had declared, "...this is zero echo declaring an emergency, lost an engine." The center controller immediately asked the aircraft that had declared an emergency to identify itself, and then tried numerous times, both directly and through other aircraft, to contact 100EK, but there was no response. Soon thereafter 100EK disappeared from Center's radar screen.
Meteorological information
When the pilot called for his weather briefing, he was advised that the first significant winter storm of the year was moving into the area. He was advised of airmets for obscuration of mountainous terrain, moderate rime icing in the clouds, moderate turbulence, and low level wind shear on the west side of the Cascade Mountains.
The current weather at Boeing Field at the time of the briefing was a measured ceiling of 3,500 feet overcast, visibility six miles with light rain and fog, temperature 42 degrees, dew point 40 degrees, calm winds, and an altimeter of 29.72 inches.
The forecast for western Washington was for 2,000 to 3,000 overcast, layered through 25,000 feet; changing by 1000 PST to 1,500 to 2,000 feet scattered to broken, with overcast of 3,000 to 3,500 feet, visibility three to five miles in light rain and fog or moderate rain, occasionally with snow above 3,000 feet. The forecast also called for an area of high surface winds to be moving in from the coast by 0900 PST. These winds were forecast to be 30 to 40 knots, with gusts into the fifties.
The forecast for the Columbia Basin was 3,000 to 4,000 scattered to broken, 7,000 broken, with widely scattered areas of light rain through 1300 PST. The forecast for the remainder of eastern Washington was for 8,000 scattered, 12,000 overcast, cloud tops to 20,000 through 1100 PST, and areas of rain or mixed rain and snow by 1200 PST.
Because there is no terminal forecast issued for Pullman, the pilot was given the terminal forecast for Lewiston, Idaho. This forecast showed 1,200 scattered, 4,500 overcast, winds 120 degrees at 13 knots gusting to 25 knots, with a chance of ceilings 1,200 overcast, visibility down to two miles in light rain and fog.
The Surface Weather Observation for Boeing Field taken at 0945, approximately 30 minutes after the departure of 100EK, was reporting an estimated ceiling of 3,000 overcast, five miles visibility, light rain and fog, a temperature of 43 degrees and a dewpoint of 41 degrees, wind of 130 degrees at four knots, and an altimeter setting of 29.91.
The Automatic Meteorological Observation (AMO) taken at Stampede Pass (3,800 feet MSL), about 9 miles southeast of the accident site, at 0849 PST, reported an indefinite ceiling 100 feet, sky obscured, visibility one eighth mile, snow and fog, temperature 26 degrees, dewpoint 25 degrees, wind 090 degrees at 14 knots, altimeter 29.65 inches. The AMO taken at the same location at 1009 PST, showed indefinite ceiling 100 feet, sky obscured, visibility one eighth mile, snow and fog, temperature 26 degrees, dew point 25 degrees, wind 100 degrees at 17 knots, altimeter 29.62 inches.
Pilots who flew near the area of the accident that morning, either prior to or after the mishap, reported that their aircraft picked up moderate mixed ice while in the clouds. Two of the pilots, both of which fly this portion of Victor 120 on a regular basis, said that the ice was accumulating faster and building up thicker than they were used to experiencing in this area. All agreed that the clouds were layered from about 3,000 feet above ground level (AGL) to as high as 21,000 feet. The pilot of an aircraft which departed Boeing Field for the same destination about five minutes after 100EK, reported very strong updrafts and moderate turbulence through 4,000 feet, and moderate mixed icing in the clouds to about 17,000 feet. A pilot of a turbojet aircraft, who also made an easterly departure from Boeing Field that morning, said that "It was pretty tough going in the ice and turbulence," until he got on top of the cloud layers at about 20,000 feet.
Wreckage and impact information
The aircraft impacted the terrain at approximately the 3,800 foot level of the southeasterly slope of Granite Mountain. According to the rescue personnel who responded to the scene, the aircraft impacted two or three large trees, and came to rest buried in about four feet of snow, with an additional two feet of fresh snow on top of the wings. A line drawn through the primary impact scar and the remains of the main wreckage, in the direction of the aircraft nose, measured 10 degrees magnetic. The instrument panel, main cabin, nose cargo compartment, and the inboard portion of the left wing were destroyed by fire. The inboard portion of the right wing also received considerable fire damage. The empennage, nose wheel well area, outboard four feet of the left wing, and the right wing, from the inboard end of the aileron to the wing tip, did not have significant fire damage.
The outboard section of the right wing showed rearward crushing and wing skin accordioning in the area forward of the aileron. The front wing spar had separated at a point that was forward of the midpoint of the aileron, and the rear wing spar had separated about even with the inboard aileron hinge. The rearward crushi
Sequence of events
NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.
Aircraft
- Registration
- N100EK
- Reported as
- Beech A60
- Category
- Airplane
- Serial number
- P-209
- Engine
- Lycoming TIO-541-E1C4, 380 horsepower, reciprocating
- Damage
- Destroyed
- Fire
- On-Ground
- Flight
- Personal · Part 91
- Operator
- Huber, James D.
- Registered owner
- Huber, James D.
- Airworthiness certificate
- Standard, Normal
- Last inspection
- Annual · August 17, 1992
- Departed
- BFI · Seattle, WA
- Destination
- PUW · Pullman, WA
- Flight plan
- IFR
Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.
Flight crew
As NTSB recorded them. NTSB leaves out names.
- Role
- Pilot
- Age
- 48
- Certificate
- Commercial
- Airplane ratings
- Multi-engine land, Single-engine land, Single-engine sea
- Instrument ratings
- Airplane
- Medical
- Class 3, Valid Medical--w/ waivers/lim
- Toxicology
- Performed
- Flight hours
- 3,250 total · 7 in the last 90 days · 3 in the last 30 days
Weather
- Conditions
- Instrument (IMC) · Day
- Wind
- 100° at 17 knots
- Visibility
- 0.13 statute miles
- Lowest ceiling
- 100 ft
- Temperature
- 27 °F, dew point 25 °F
- Altimeter
- 29.00 inHg
- Observed at
- SMP, 9 nm away
FAA reports on this event · 1
The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.