Country
Crash of a Raytheon 390 Premier I in North Las Vegas
Date & Time:
May 27, 2004 at 1557 LT
Operator:
Registration:
N5010X
Survivors:
Yes
Schedule:
Palm Springs - North Las Vegas
MSN:
RB-10
YOM:
2002
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total hours on type:
62.00
Circumstances:
The airplane overran the runway after landing on runway 7. The passenger stated that he felt that the approach was "fast" and that the pilot was "behind the power curve" because of high
minimum en route altitudes in the area and that they had to "hustle down" during the descent. The passenger indicated that the flight crossed the runway threshold "maybe a bit more" that 10 knots above Vref and touched down about 10 knots above Vref. He said it was not a stabilized approach. Landing distance calculations and other evidence suggest that the lift dump panels did not extend after landing; however, the investigation did not determine the reason(s) for the lack of lift dump. No evidence was found of any failures affecting the lift dump or braking systems. Evidence and interview statements reveal that the pilot flew an unstabilized approach to the runway and landed well above target speed. The high landing speed was result of the pilot's excessive airspeed on the approach and a tailwind component of about 8 knots. Although the pilot landed the airplane within the touchdown area, the airplane's speed upon touchdown was about 17 knots above the prescribed speed. The flight's unstabilized approach and excessive speed should have prompted the pilot to initiate a missed approach.
minimum en route altitudes in the area and that they had to "hustle down" during the descent. The passenger indicated that the flight crossed the runway threshold "maybe a bit more" that 10 knots above Vref and touched down about 10 knots above Vref. He said it was not a stabilized approach. Landing distance calculations and other evidence suggest that the lift dump panels did not extend after landing; however, the investigation did not determine the reason(s) for the lack of lift dump. No evidence was found of any failures affecting the lift dump or braking systems. Evidence and interview statements reveal that the pilot flew an unstabilized approach to the runway and landed well above target speed. The high landing speed was result of the pilot's excessive airspeed on the approach and a tailwind component of about 8 knots. Although the pilot landed the airplane within the touchdown area, the airplane's speed upon touchdown was about 17 knots above the prescribed speed. The flight's unstabilized approach and excessive speed should have prompted the pilot to initiate a missed approach.
Probable cause:
The flight's unstabilized approach and excessive speed. Contributing to the excessive touchdown speed was the presence of a tailwind at landing.
Final Report:
Crash of a Raytheon 390 Premier I in Blackbushe
Date & Time:
Apr 7, 2004 at 0932 LT
Registration:
N200PR
Survivors:
Yes
Schedule:
Farnborough - Blackbushe
MSN:
RB-79
YOM:
2001
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total hours on type:
413.00
Circumstances:
After takeoff the pilot was unable to raise the landing gear and was presented with failure indications affecting both the lift dump and anti skid systems. Following a successful landing at Farnborough, and discussions with the aircraft's maintenance organisation, the aircraft was flown to Blackbushe for further technical investigation. After landing on Runway 26 the aircraft left the runway, struck a series of obstructions and was destroyed: there was no fire and the pilot was uninjured. The support bracket for the right main landing gear weight-on-wheels switch was found to have sustained a pre-impact failure which accounted for the indications reported by the pilot. Five recommendations have been made as a result of this investigation.
Probable cause:
The support bracket for the right main landing gear weight-on-wheels switch was found to have sustained a pre-impact failure which accounted for the indications reported by the pilot.
Final Report:
Crash of a Raytheon 390 Premier I in Santo Domingo
Date & Time:
Jan 8, 2003 at 1824 LT
Registration:
N390RB
Survivors:
Yes
Schedule:
Santo Domingo - Santo Domingo
MSN:
RB-26
YOM:
2002
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The aircraft overran the runway and came to rest in a parking lot, while landing at Herrera International Airport, Santo Domingo, Dominican Republic, while on a 14 CFR Part 91 positioning flight. Visual meteorological conditions prevailed at the time and a visual flight rules flight plan was filed. The airplane received substantial damage and the airline transport-rated pilot, copilot, and two passengers received minor injuries. The flight originated from Las Americas International Airport, Santo Domingo, Dominican Republic, the same day, about 1810. The pilot stated they made a normal approach and landing on runway 19 at Herrera International Airport. Once on the ground they activated lift dump spoilers, but the system failed. They were unable to stop the airplane on the remaining runway. The airplane came to a stop, inverted beyond a street that is at the end of the runway.
