SEA98FA040

NTSB accident investigation · Freije Lancair IV · Garwood, ID · February 26, 1998

Accident · FatalField investigationFinal report
Date
February 26, 1998, 07:50 local (15:50 UTC)
Place
Garwood, ID
Injuries
2 fatal
Damage
Destroyed
Phase of flight
Maneuvering
Aircraft
N109GFFreije Lancair IV
Weather
Instrument (IMC) · Day
Status
Completed · report January 10, 2000
Report
Approved by Office Director
FAA report
19980226001869A
Case key
42705

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

The NTSB’s determination of the probable cause, and any contributing factors.

The pilot's failure to maintain aircraft control after entering known adverse weather. Related factors were, the pilot's failure to follow the published IFR departure procedures, low ceilings and snow, and the pilot's lack of recent instrument experience.

Analysis

The pilot of the experimental aircraft, who had been on an IFR departure in instrument meteorological conditions (IMC), began maneuvering around the vicinity of Alpine Lake. After a period of between three to five minutes, the pilot lost control of the aircraft, descended out of the low ceiling, and impacted an unoccupied personal residence. At the time of the accident, it was snowing heavily in areas around Alpine Lake, and the visibility was estimated to be one-half mile or less. After the accident, a review of the pilot's log showed that he had recorded only one and nine-tenths hour of instrument time in the last year, and only one hour in the last six months. His log did not show any hours of actual or simulated instrument time in the model aircraft he was flying at the time of the accident. There was no evidence of any pre-impact engine anomaly or vacuum system malfunction.

Factual narrative

The factual narrative1,333 words

History of flight

On February 26, 1998, approximately 0750 Pacific standard time, an experimental Freije Lancair IV, N109GF, impacted a personal residence about three miles southeast of Garwood, Idaho. The commercial pilot and his passenger, who possessed a private pilot's license, received fatal injuries. The aircraft, which was built, owned, and operated by the commercial pilot, was destroyed. The 14 CFR Part 91 personal pleasure flight, which departed Coeur D' Alene Air Terminal about five minutes prior to the crash, had been on an IFR departure in instrument meteorological conditions (IMC). His IFR flight plan was from Coeur D'Alene to Billings, Montana. There was no report of an ELT transmission.

According to friends and family members, the pilot was planning to fly to Billings on the morning of the accident, in order to attend a pilots' convention. He contacted Seattle Automated Flight Service Station at 2142 Pacific standard time the night before the flight, and received a briefing for an intended IFR flight to Billings. During that briefing, he indicated he would be departing about 0600 the next day. At 0608 the next morning, he again contacted Seattle Flight Service and asked for a briefing for an IFR flight to Billings, with a stop en route at Coeur D'Alene, Idaho. After receiving the briefing, the pilot filed an IFR flight plan from Felts Field, Spokane, Washington, to Coeur D'Alene, and a second IFR flight plan from Coeur D'Alene to Billings. At that time, he estimated he would be departing Coeur D'Alene about 0730. The time he departed Felts Field and flew VFR to Coeur D'Alene was not determined, but he reportedly arrived in Coeur D'Alene around 0715. After landing, he added 56.05 gallons of 100LL aviation fuel to the aircraft fuel system.

At 0744, while still on the ground at Coeur D'Alene, the pilot contacted Spokane Approach and advised them that he was ready to depart Coeur D'Alene "...IFR to Billings." Spokane Approach then cleared the pilot to Billings Airport "as filed" and instructed him to maintain 11,000 feet after departure, to contact Departure on frequency 132.1, and to squawk code 3511. The pilot correctly read back the clearance, and then Approach asked him how soon he would be ready and what runway he would be using. The pilot responded that he was "...ready to go now" and that he would be using runway 01. Soon thereafter the aircraft was seen taking off on runway 01 and climbing into the overcast. The next apparent transmission from the pilot was two minutes and 40 seconds later, but its content was unintelligible. Approach responded to the transmission by advising the pilot that the transmission was "...breaking up and hard to read." The pilot of the accident aircraft immediately responded with his call sign, and was advised by approach that the transmission was a little better and to verify his altitude. His response to that request was to transmit "I'm not sure, we're in a turn right now, and uh." The controller then advised the pilot that approach had radar contact with the aircraft "... three north of Coeur D'Alene Airport...," and to maintain one one thousand. About six seconds after the controller's transmission, there was another unintelligible transmission from an aircraft that could not be positively identified. There was no further radio contact with the accident aircraft, and coded radar contact was lost approximately 45 seconds after it had first been established.

Approximately the same time as radio and radar contact with the aircraft was lost, individuals in the vicinity of Alpine Lake, located about three and one-half miles north-northeast of Coeur D'Alene Airport, became aware of an aircraft maneuvering in the low clouds overhead. Of the seven local residents interviewed, three were outside their homes at the time the aircraft was first heard in the area. Two of these witnesses estimated they heard the aircraft maneuvering around the area for about five minutes before the crash, and the other felt that he had been aware of the aircraft for about three minutes. All three said that the aircraft's engine seemed to be running smoothly, without any missing or sputtering, as the aircraft continued to fly around the area. One thought the engine may have sputtered during the last two to three seconds prior to impact, but the other two said that it ran strong and smooth until it hit the house. Four other individuals, all of whom were inside homes near the point of impact, and who said they heard the aircraft less than five seconds before it hit, reported that the engine was running smoothly, but at a very high power setting. Two of the outdoor witnesses said that the pilot seemed to be making occasional changes in the power setting during the period they listened to him maneuver, but the other was of the opinion that the tonal changes he heard were caused by the normal effect created when the aircraft flew in different directions. All three outside witnesses said they saw the aircraft come out of the clouds in a steep angle of descent. Two said that the aircraft was near 90 degrees of bank, and the third said that visibility through the fog and heavy snow made it impossible to distinguish the wings from the fuselage or to tell what the aircraft's attitude might have been. All three of these witnesses said that the aircraft impacted the house near the northwest shore of Alpine Lake within two to three seconds after it came out of the clouds.

Individuals in the nearby houses reported hearing or feeling the impact, and all said there was no immediate explosion. According to local authorities, the aircraft severed a natural gas line as it passed through the structure of the house, and as a result, about ten to fifteen seconds after the impact, all but a portion of one wall of the house was destroyed by a powerful explosion. The aircraft wreckage and the remains of the house continued to burn for approximately three hours after the impact.

Meteorological information

During the briefing the pilot received on the morning of the flight, he was advised that in the area through which he planned to fly, there were Airmets for IFR conditions, icing, and mountain obscuration. The briefer advised him that the icing Airmet called for "... occasional moderate rime or mixed, from the surface on up through one six thousand..." He was also advised that at the time of the briefing, the automated weather from Coeur D'Alene indicated a calm wind, a temperature/dewpoint spread of one degree, and a 900 foot broken ceiling. In addition, the briefer told the pilot that, although the Coeur D'Alene forecast was for 2,000 overcast and six miles visibility, temporary conditions could drop to four miles visibility, with light snow and mist/fog and an 800 foot ceiling. Near the end of the briefing the pilot questioned the briefer about whether it would be possible to get to Coeur D'Alene VFR. The briefer responded that "... it doesn't appear so..." because the ceiling at Coeur D'Alene was still at 900, and the visibility had dropped to five miles. He also advised the pilot that the ceiling at Spokane at that time was down to 600 feet.

The Coeur D'Alene automated surface observation (METAR) taken at 0714, which was approximately the same time as the pilot's VFR arrival, indicated calm winds, a visibility of four miles, a 600 foot overcast, and a two degree temperature/dewpoint spread. The METAR taken at 0734, about ten minutes prior to the aircraft's departure, reported calm winds, one and one-half mile visibility, a 600 foot overcast, and a one degree temperature dewpoint spread. The METAR data for 0754, about 10 minutes after the departure, indicated calm winds, one and one-quarter mile visibility, 600 feet overcast, and a one degree spread between temperature and dewpoint. The investigation also confirmed that the Automated Weather Observation System (AWOS) was operating during the time the pilot was at the Coeur

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.

Loss of control - in flightManeuvering
Flight into known adverse weather - intentionalPilot in commandFactor
Ifr procedure - not followedPilot in commandFactor
Aircraft control - not maintainedPilot in commandCause
Lack of recent instrument timePilot in commandFactor
Weather condition - low ceilingFactor
Weather condition - snowFactor
In flight collision with objectDescent - uncontrolled
Object - residence

Aircraft

Registration
N109GF
Reported as
Freije Lancair IV
Category
Airplane, amateur-built
Serial number
LIV-109
Engine
Lycoming IO-540-K1F5, 290 horsepower, reciprocating
Damage
Destroyed
Fire
On-Ground
Flight
Personal · Part 91
Registered owner
George Freije
Airworthiness certificate
Special, Experimental (Special)
Departed
COE · Coeur D' Alene, ID
Destination
BIL · Billings, MT
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
73
Certificate
Commercial
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Toxicology
Performed
Flight hours
5,044 total · 70 in this make and model · 5 in the last 30 days

Weather

Conditions
Instrument (IMC) · Day
Wind
Calm
Visibility
1.2 statute miles
Lowest ceiling
600 ft overcast
Temperature
28 °F, dew point 27 °F
Altimeter
30.00 inHg
Observed at
KCO, 4 nm away

Docket · 9

The files NTSB released with the investigation on March 4, 1999, on NTSB’s docket system: statements, records, photos and specialists’ reports. 1.5 MB in all.

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.