Crash of a Cessna 650 Citation III in Caico Seco: 3 killed

Date & Time: Feb 18, 2008 at 1815 LT
Type of aircraft:
Operator:
Registration:
N385EM
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Valencia – Puerto Ordaz
MSN:
650-0145
YOM:
1987
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
The aircraft departed Valencia-Arturo Michelana Airport on a private flight to Puerto Ordaz, carrying one passenger and two pilots. While cruising at an altitude of 30,000 feet, the aircraft entered an uncontrolled descent and crashed in a near vertical attitude. The aircraft disintegrated on impact and all three occupants were killed.
Probable cause:
The copilot probably gave his place on board to a passenger without any qualification to operate the aircraft, moments after takeoff. During the en-route flight phase, a failure of the primary pitch trim system was simulated by the activation of the secondary system, which would have resulted in an abnormal operation of the system, followed by violent loss of altitude and over speed condition.

Crash of a Cessna 650 Citation III in Atlantic City

Date & Time: Oct 27, 2007 at 1110 LT
Type of aircraft:
Operator:
Registration:
N697MC
Flight Type:
Survivors:
Yes
Schedule:
Farmingdale – Atlantic City
MSN:
650-0097
YOM:
1985
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
9472
Captain / Total hours on type:
199.00
Copilot / Total flying hours:
2535
Copilot / Total hours on type:
120
Aircraft flight hours:
7052
Circumstances:
The first officer was flying the Area Navigation, Global Positioning System, approach to runway 22. During the approach, the airplane was initially fast as the first officer had increased engine power to compensate for wind conditions. Descending below the minimum descent altitude (MDA), the first officer momentarily deployed the speed brakes, but stowed them about 200 feet above ground level (agl), and reduced the engine power to flight idle. The airplane became low and slow, and developed an excessive sink rate. The airplane subsequently landed hard on runway 22, which drove the right main landing gear into the right wing, resulting in substantial damage to the right wing spar. The first officer reported intermittent airspeed fluctuations between his airspeed indicator and the captain's airspeed indicator; however, a subsequent check of the pitot-static system did not reveal any anomalies that would have precluded normal operation of the airspeed indicators. About the time of the accident, the recorded wind was from 190 degrees at 11 knots, gusting to 24 knots; and the captain believed that the airplane had encountered windshear near the MDA, with the flaps fully extended. Review of air traffic control data revealed that no windshear advisories were contained in the automated terminal information system broadcasts. Although the local controller provided windshear advisories to prior landing aircraft, he did not provide one to the accident aircraft. Review of the airplane flight manual (AFM) revealed that deploying the speed brakes below 500 feet agl, with the flaps in any position other than the retracted position, was prohibited.
Probable cause:
The first officer's failure to maintain airspeed during approach, and the captain's inadequate remedial action. Contributing to the accident was the first officer's failure to comply with procedures, windshear, and the lack of windshear warning from air traffic control.
Final Report: