Zone

Crash of a Cessna 421B Golden Eagle II in Kelso: 5 killed

Date & Time: Oct 29, 2003 at 1222 LT
Registration:
N444AM
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Bullhead City – Van Nuys
MSN:
421B-0367
YOM:
1973
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
11371
Captain / Total hours on type:
1237.00
Aircraft flight hours:
3114
Circumstances:
The aircraft broke up in-flight during a high speed descent after encountering clouds and reduced visibilities aloft. The weather conditions included multiple cloud layers at 9,000, 12,000 and 16,000 feet, and reduced visibility aloft from smoke and haze from wilderness wild fires that were occurring over large portions of Southern California. The aircraft departed the airport toward a VORTAC to the west, approximately 30 nautical miles (nm) away. The first radar contact was at 1159, and the aircraft's Mode C transponder reported an altitude of 3,500 feet mean sea level (msl). By the time the aircraft reached the VORTAC, the altitude had increased to 4,900 feet msl. The aircraft continued to climb, passing through the VFR flight plan filed altitude of 8,500 feet msl, until it reached an altitude of 12,900 feet msl. The last 6 minutes of radar data reported the aircraft at various altitudes, starting at 11,000 feet msl and climbing to a maximum altitude of 12,700 feet msl. During the last 3 minutes of flight, radar data showed the aircraft made numerous left and right climbing and descending turns, eventually reversing course. The next to last radar return at 1221:24 indicated an altitude of 11,900 feet msl. Nineteen seconds later, the last radar return reported an altitude of 7,700 feet msl. The computed vertical speed between the last two radar returns was 13,263 feet per minute. The wreckage was distributed over a 0.2-nm distance, with the main wreckage approximately 0.5 miles northwest of the last radar return. The northern end of the debris path began with pieces of the left elevator, followed by sections of the right stabilizer and elevator, and more sections from both horizontal empennage surfaces. Pieces of the vertical stabilizer, rudder, and both ailerons were also found along the debris path. The southern 100 feet of the debris path contained the fuselage and both sets of wings, engines, and propellers. The aircraft impacted the ground inverted. The wings separated just outboard of the nacelles at the initial point of impact. Examination of the wreckage showed that all structural failures were the result of overload.
Probable cause:
The pilot's continued VFR flight into instrument conditions between cloud layers and with reduced visibility due to smoke that resulted in an in-flight loss of control from spatial disorientation, and the structural overload of the airframe during the subsequent high speed descent.
Final Report:

Crash of a Rockwell Shrike Commander 500S near Kelso: 2 killed

Date & Time: Mar 8, 1975 at 1325 LT
Operator:
Registration:
N711LZ
Flight Phase:
Survivors:
No
Site:
Schedule:
Apple Valley - Amarillo - Oklahoma City
MSN:
500-1846-35
YOM:
1968
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
9000
Captain / Total hours on type:
150.00
Circumstances:
While in cruising altitude between Apple Valley and Amarillo, the pilot encountered poor weather conditions and limited visibility. He failed to realize his altitude was too low when the airplane struck the slope of a mountain located in the region of Kelso. The wreckage was found four days later and both occupants were killed.
Probable cause:
Controlled flight into terrain after the pilot continued VFR flight into adverse weather conditions. The following contributing factors were reported:
- Improper in-flight decisions,
- Inadequate preflight preparation,
- Low ceiling,
- Rain,
- High obstructions,
- Advised VFR flight not recommended.
Final Report: