Crash of a Dassault Falcon 20D-5 in Lorain

Date & Time: Sep 1, 2005 at 1950 LT
Type of aircraft:
Operator:
Registration:
N821AA
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Lorain - Saint Louis
MSN:
203
YOM:
1970
Flight number:
JUS821
Location:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4444
Captain / Total hours on type:
639.00
Copilot / Total flying hours:
2172
Copilot / Total hours on type:
193
Aircraft flight hours:
16970
Circumstances:
The small, twin-engine business jet was about 15 feet above the runway on takeoff, when a flock of birds from both sides of the runway flew up in front of the airplane. The number two engine "surged," and "loud reports" were heard before the copilot noted a complete loss of power on the number two engine instruments. The airplane climbed for about 10 seconds, before the copilot observed the gas producer (N1) gauge on the number one engine decay through 50 percent. The stall warning horn sounded, and the pilot adjusted the flight controls for landing. The airplane contacted the runway with the landing gear retracted, overran the runway, struck a fence, crossed a road, and came to rest in a cornfield about 1,000 feet beyond the initial point of ground contact. Post accident examination of both engines revealed evidence and damage consistent with multiple bird ingestion.
Probable cause:
The ingestion of multiple birds in each engine at takeoff, which resulted in a complete loss of engine power.
Final Report:

Crash of a Dassault Falcon 20C in Moscow

Date & Time: May 20, 2005
Type of aircraft:
Operator:
Registration:
RA-09007
Survivors:
Yes
MSN:
136
YOM:
1968
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Aircraft lost power on both engines while on approach to Moscow-Vnukovo airport. The crew decided to divert to Sheremetievo Airport when the undercarriage collapsed on landing. The aircraft veered off runway and slid in a grassy area before coming to rest. Nobody was injured but the aircraft was damaged beyond repair.
Probable cause:
It is believed that the engine lost power on approach because of the poor fuel quality.

Crash of a Dassault Falcon 20C in Oranjestad

Date & Time: Feb 13, 2005
Type of aircraft:
Operator:
Registration:
PR-SUL
Flight Type:
Survivors:
Yes
Schedule:
Porlamar - Oranjestad
MSN:
129
YOM:
1968
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Following an uneventful positioning flight from Porlamar, the aircraft landed at Oranjestad-Reina Beatrix Airport with its undercarriage retracted. The aircraft slid on ity belly for few dozen metres before coming to rest. Both pilots escaped uninjured while the aircraft was damaged beyond repair.

Crash of a Dassault Falcon 20C in Pueblo

Date & Time: Jan 21, 2004 at 0040 LT
Type of aircraft:
Operator:
Registration:
N200JE
Flight Type:
Survivors:
Yes
Schedule:
Saint Louis – Pueblo
MSN:
133
YOM:
1968
Location:
Crew on board:
2
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
3750
Captain / Total hours on type:
1900.00
Copilot / Total flying hours:
2850
Copilot / Total hours on type:
110
Aircraft flight hours:
8378
Circumstances:
The captain reported that he obtained weather briefings prior to and during the flight. The briefings did not include any NOTAMS indicating a contaminated runway at their destination airport. The captain obtained a report from the local fixed base operator that a Learjet had landed earlier and reported the runway as being okay. The tower was closed on their arrival, so they made a low pass over the airport to inspect the runways. Based on the runway and wind conditions, they decided their best choice for landing was on runway 08L. The captain said the landing was normal and the airplane initially decelerated with normal braking. As they encountered snow and ice patches, the captain said he elected to deploy the thrust reversers. The captain said that as the thrust reversers deployed, the airplane began to yaw to the left and differential braking failed to realign the airplane with the runway. The captain said the airplane departed the left side of the runway and rotated counter clockwise before coming to rest on a southwesterly heading. A witness on the airport said, "I watched them touch down. I heard the [thrust] reversers go on and then off, and then on again. As they came back on for the second time, that's when the plane started making full circles on the runway. This happened two, maybe three times before going off the side of the runway." The airplane's right main landing gear collapsed on departing the runway, causing substantial damage to the right wing, right main landing gear and aft pressure bulkhead. At the accident site, the right engine thrust reverser was partially deployed. The left engine thrust reverser was fully deployed with the blocker doors extended. An examination of the airplane revealed a stuck solenoid on the right engine thrust reverser. No other system anomalies were found. Approximately 33 minutes prior to the accident, the pilot requested from Denver Air Route Traffic Control Center, the weather for the airport. Denver Center reported the conditions as "winds calm, visibility 6 miles with light mist, 3,000 overcast, temperature zero degrees Centigrade (C) dew point -1 degree C, altimeter three zero 30.20, and there was at least a half inch of slush on all surfaces." The pilot acknowledged the information. The NOTAM log for the airport showed that at 2115, the airport issued a NOTAM stating there was "1/2 inch wet snow all surfaces." The airport operations manager reported that at the time of the accident the runway surface was covered with 3/4 inch of wet snow. The airport conducts a 24 hour, 7 days a week operation; however, operations support digresses to fire coverage only after 2300.
Probable cause:
The pilot's improper in-flight planning/decision to land on the contaminated runway, the stuck thrust reverser solenoid resulting in partial deployment of the right engine thrust reverser, and the pilot's inability to maintain directional control of the airplane due to the asymmetric thrust combined with a contaminated runway. Factors contributing to the accident were the wet, snow-covered runway, the airport's failure to remove the snow from the runway, and the pilot's failure to recognize the reported hazardous runway conditions by air traffic control.
Final Report: