Crash of a Cessna 208B Super Cargomaster in Steamboat Springs: 1 killed

Date & Time: May 5, 2001 at 0858 LT
Type of aircraft:
Operator:
Registration:
N948FE
Flight Type:
Survivors:
No
Schedule:
Casper – Steamboat Springs
MSN:
208B-0052
YOM:
1987
Flight number:
FDX8810
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
2916
Captain / Total hours on type:
43.00
Aircraft flight hours:
8690
Circumstances:
The pilot obtained a weather briefing, filed an IFR flight plan, and departed on a nonscheduled domestic cargo flight, carrying 270 pounds of freight. The flight proceeded uneventfully until it was established on the VOR/DME-C approach. Radar data indicates that after turning inbound towards the VORTAC from the DME arc, the airplane began its descent from 10,600 feet to the VOR crossing altitude of 9,200 feet. Enlargement of the radar track showed the airplane correcting slightly to the left as it proceeded inbound to the VORTAC at 9,400 feet. Shortly thereafter, aircraft track and altitude deviated 0.75 miles northwest and 9,700 feet, 0.5 miles southeast and 9,600 feet, and 0.5 miles northwest and 9,400 feet before disappearing from radar. Witnesses said the weather at the time of the accident was 600 foot overcast, 1.5 miles visibility in "misting" rain that became "almost slushy on the ground," and a temperature of 36 degrees Fahrenheit. One weather study indicated "an icing potential greater than 50% and visible moisture" in the accident area. Another report said "icing conditions were likely present in the area of the accident." The airplane was equipped and certified for flight into known icing conditions. The wreckage was found in a closely area. There was no evidence of pre-impact airframe, engine, or propeller malfunction/failure. The pilot was properly certificated, but his flight time in aircraft make/model was only 38 hours. He had previously recorded 16 icing encounters, totaling 11.2 hours in actual meteorological conditions. He recorded no ice encounters and only 1.0 hour of simulated (hooded) instrument time in the Cessna 208. Microscopic examination of annunciator light bulbs revealed the GENERATOR OFF light was illuminated. This condition indicates a generator disconnection due to a line surge, tripped circuit breaker, or inadvertent switch operation. The operator's chief pilot agreed, noting that one of the items on the Before Landing Checklist requires the IGNITION SWITCH be placed in the ON position. The START SWITCH is located next to the IGNITION SWITCH. Inadvertently moving the START SWITCH to the ON position would cause the generator to disconnect and the GENERATOR OFF annunciator light to illuminate. He said this would be distracting to the pilot.
Probable cause:
An inadvertent stall during an instrument approach, which resulted in a loss of control. Contributing factors were the pilot's attention being diverted by an abnormal indication, conditions conducive to airframe icing, and the pilot's lack of total experience in the type of operation (icing conditions) in aircraft make/model.
Final Report:

Crash of a Gulfstream GIII in Aspen: 18 killed

Date & Time: Mar 29, 2001 at 1901 LT
Type of aircraft:
Operator:
Registration:
N303GA
Survivors:
No
Schedule:
Burbank – Los Angeles – Aspen
MSN:
303
YOM:
1980
Crew on board:
3
Crew fatalities:
Pax on board:
15
Pax fatalities:
Other fatalities:
Total fatalities:
18
Captain / Total flying hours:
9900
Captain / Total hours on type:
1475.00
Copilot / Total flying hours:
5500
Copilot / Total hours on type:
913
Aircraft flight hours:
7266
Aircraft flight cycles:
3507
Circumstances:
On March 29, 2001, about 1901:57 mountain standard time, a Gulfstream III, N303GA, owned by Airbourne Charter, Inc., and operated by Avjet Corporation of Burbank, California, crashed while on final approach to runway 15 at Aspen-Pitkin County Airport (ASE), Aspen, Colorado. The charter flight had departed Los Angeles International Airport (LAX) about 1711 with 2 pilots, 1 flight attendant, and 15 passengers. The airplane crashed into sloping terrain about 2,400 feet short of the runway threshold. All of the passengers and crew members were killed, and the airplane was destroyed. The flight was being operated on an instrument flight rules (IFR) flight plan under 14 Code of Federal Regulations (CFR) Part 135.
Probable cause:
The flight crew's operation of the airplane below the minimum descent altitude without an appropriate visual reference for the runway. Contributing to the cause of the accident were the Federal Aviation Administration's (FAA) unclear wording of the March 27, 2001, Notice to Airmen regarding the nighttime restriction for the VOR/DME-C approach to the airport and the FAA's failure to communicate this restriction to the Aspen tower; the inability of the flight crew to adequately see the mountainous terrain because of the darkness and the weather conditions; and the pressure on the captain to land from the charter customer and because of the airplane's delayed departure and the airport's nighttime landing restriction.
Final Report:

Crash of a Socata TBM-700 in Denver: 1 killed

Date & Time: Mar 26, 2001 at 0719 LT
Type of aircraft:
Registration:
N300WC
Flight Phase:
Survivors:
No
Schedule:
Denver – Santa Monica
MSN:
82
YOM:
1993
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
1024
Captain / Total hours on type:
136.00
Aircraft flight hours:
5139
Circumstances:
The airplane was fueled to capacity and placed in a heated hangar about one hour before departure. The instrument rated pilot obtained a weather briefing, filed an IFR flight plan, and obtained an IFR clearance. Low ceiling, reduced visibility, and ice fog prevented control tower personnel from observing the takeoff. Radar (NTAP) and on-board GPS data indicated the airplane began drifting to the left of runway centerline almost immediately after takeoff. The airplane made a climbing left turn, achieving a maximum altitude of 7,072 feet and completing 217 degrees of turn, before beginning a descending left turn. The airplane impacted terrain on airport property. Autopsy/toxicology protocols were unremarkable. There was no evidence of preimpact failure/malfunction of the airframe, powerplant, propeller, or flight controls. The autopilot and servos, pitot-static system, and flight instruments were tested and all functioned satisfactorily. The pilot's shoulder harness was found attached to the seatbelt, but the male end of the seatbelt buckle was broken.
Probable cause:
The pilot's spatial disorientation, which led to his failure to maintain aircraft control. A contributing factor was the pilot's decision to intentionally fly into known adverse weather that consisted of low ceilings, obscuration, and ice fog.
Final Report:

Crash of a Beechcraft 200 Super King Air in Byers: 10 killed

Date & Time: Jan 27, 2001 at 1737 LT
Operator:
Registration:
N81PF
Flight Phase:
Survivors:
No
Schedule:
Jefferson - Stillwater
MSN:
BB-158
YOM:
1976
Location:
Crew on board:
2
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
10
Captain / Total flying hours:
5117
Captain / Total hours on type:
767.00
Copilot / Total flying hours:
1828
Copilot / Total hours on type:
1218
Aircraft flight hours:
8737
Circumstances:
On January 27, 2001, about 1737 mountain standard time, a Raytheon (Beechcraft) Super King Air 200, N81PF, owned by North Bay Charter, LLC, and operated by Jet Express Services, crashed into rolling terrain near Strasburg, Colorado. The flight was operating on an instrument flight rules (IFR) flight plan under 14 Code of Federal Regulations (CFR) Part 91. The flight departed about 1718 from Jefferson County Airport (BJC), Broomfield, Colorado, with two pilots and eight passengers aboard. The pilot who occupied the left seat in the cockpit was solely responsible for the flight. The pilot who occupied the right seat in the cockpit, referred to in this report as the "second pilot," was not a required flight crewmember. N81PF was one of three airplanes transporting members of the Oklahoma State University (OSU) basketball team and associated team personnel to Stillwater Regional Airport (SWO), Stillwater, Oklahoma, after a game at the University of Colorado at Boulder that afternoon. All 10 occupants aboard N81PF were killed, and the airplane was destroyed by impact forces and a post crash fire. Instrument meteorological conditions (IMC) prevailed at the time of the accident.
Probable cause:
The pilot’s spatial disorientation resulting from his failure to maintain positive manual control of the airplane with the available flight instrumentation. Contributing to the cause of the accident was the loss of a.c. electrical power during instrument meteorological conditions.
Final Report:

Crash of a Piper PA-31-350 Navajo Chieftain in Kiowa: 2 killed

Date & Time: Jun 5, 2000 at 1031 LT
Operator:
Registration:
N67BJ
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Denver - Denver
MSN:
31-7952250
YOM:
1979
Location:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
3900
Aircraft flight hours:
11279
Circumstances:
The purpose of the flight was for the instructor pilot to administer second-in-command (SIC) flight training to the commercial pilot in the twin-engine aircraft. According to the training manual, SIC training encompassed 4 hours of normal and emergency flight maneuvers to include stalls in the landing and takeoff configuration and while turning at a 15-30 degree bank. A witness heard the airplane's engines and observed the airplane from her driveway. The witness stated that as "the [engine] noise was getting louder and louder, I spotted it spiraling downward." The witness thought that the airplane was performing aerobatics; however, the airplane was getting too close to the ground. The witness heard a loud thud, and approximately 3 seconds later, she heard a loud boom and saw black smoke billow up. Another witness stated that she observed the airplane "going nose first straight down and spinning...counterclockwise." She thought the airplane was performing aerobatic maneuvers; however, the airplane did not stop descending. The airplane disappeared behind trees and the witness heard a loud explosion and saw smoke. She added that she did not observe what the airplane was doing prior to seeing it in a "downward spiral." Radar data depicted the airplane at 8,400 feet msl for the last 2 minutes and 26 seconds of the flight. The recorded aircraft ground speed during that time period fluctuated between 75 and 59 knots. The final radar returns depicted the airplane as making a 180 degree turn before radar contact was lost. No mayday calls were received from the airplane. The airplane impacted the ground in a near wings level attitude and was consumed by a post-crash fire. No anomalies were noted with the airplane or its engines during a post-accident examination. It is unknown which of the pilots was flying the airplane at the time of the accident.
Probable cause:
The flight instructor's failure to maintain aircraft control while practicing stall maneuvers, which resulted in an inadvertent spin.
Final Report:

Crash of a Piper PA-61 Aerostar (Ted Smith 601) in Estes Park: 2 killed

Date & Time: Apr 30, 2000 at 1211 LT
Registration:
N7421S
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Page - Fort Collins
MSN:
61-0006
YOM:
1968
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
4400
Circumstances:
While on a cross-country flight, according to radar data and weather information, the pilot descended below terrain clearance altitude and entered IMC conditions. The aircraft impacted a mountain peak approximately 100 feet below the summit. No flight plan had been filed and the pilot was not instrument rated.
Probable cause:
A descent below the surrounding terrain, by the pilot, in IMC conditions. Factors were high mountainous terrain, clouds, inaccurate weather evaluation by the pilot, and the pilot's flight into IMC conditions.
Final Report:

Crash of a Cessna 421B Golden Eagle II near Telluride: 1 killed

Date & Time: Jan 2, 2000 at 0950 LT
Operator:
Registration:
N421CF
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Montrose - Las Cruces
MSN:
421B-0513
YOM:
1973
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
3700
Captain / Total hours on type:
200.00
Aircraft flight hours:
3154
Circumstances:
The non-instrument rated private pilot departed Montrose, Colorado, southbound in a Cessna 421B. According to radar data, the airplane climbed from 14,300 to 16,600 feet msl at a rate of 1,792 fpm. The data shows that 19 seconds later, the airplane lost 4,000 feet of altitude, or descended at a rate of 12,631 fpm. The airplane then climbed back to 13,300 feet msl at a rate of 1,448 fpm, and then disappeared from radar. The airplane crashed in snow covered mountainous terrain. Snowmobilers, who were in the vicinity of the impact site at the time of the accident, said that snow showers made visibility less than 1/2 sm. A pilot departing Telluride Regional Airport (located 33 nm at 045 degrees from the crash site), on a heading of 300 degrees, at approximately 1015 said that it was clear right over Telluride. He said that as he climbed out, he got into weather at 12,000 feet msl, and didn't break out until 22,000 feet msl. He also said that he experienced no icing or turbulence during his climb out.
Probable cause:
The non-instrument rated pilot's intentional flight into IMC, and his subsequent spatial disorientation that resulted in an inadvertent stall. A factor was the snow showers weather condition.
Final Report: