Country

Crash of a Dassault Falcon 10 in Rancho Murieta: 3 killed

Date & Time: Oct 15, 1987 at 1528 LT
Type of aircraft:
Registration:
N121FJ
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Rancho Murieta - San José
MSN:
192
YOM:
1981
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
8407
Captain / Total hours on type:
1200.00
Aircraft flight hours:
475
Circumstances:
The aircraft flew to the airport for a sales demonstration flight. The crew boarded the aircraft and taxied out for departure. Witnesses, including two pilots with aerobatic experience, watched the aircraft departure, make a left traffic pattern and do a low fly-by down the runway. At the departure end of the runway, the aircraft pitched up into a steep climb. At 600 feet agl, the aircraft entered a left aileron roll, which the witnesses said was 'smooth, coordinated and with the nose on the point.' At the inverted point of the roll, the roll changed from an aileron to a barrel roll. One pilot witness said that it appeared the 'crew lost it at the top' and that the crew 'held the back pressure too long at the top.' At the 270° point of the roll, the aircraft was seen to 'fall out' or 'dish out' of the roll; it recovered to wings level flight at about 100 feet agl in a very nose high attitude settling into the ground with a high vertical descent rate. No preimpact eng or control system malfunctions were found. All three occupants were killed.
Probable cause:
The National Transportation Safety Board determines the probable cause(s) of this accident to be:
In flight loss of control by the pilot flying while performing an Intentional low level aerobatic maneuver.
Findings
Occurrence #1: loss of control - in flight
Phase of operation: maneuvering
Findings
1. (c) judgment - poor - pilot in command
2. (c) aerobatics - intentional - pilot in command
3. (f) ostentatious display - pilot in command
4. (f) altitude - inadequate - pilot in command
5. (c) flight controls - improper use of - pilot in command
----------
Occurrence #2: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Final Report:

Crash of a Dassault Falcon 10 near Haenertsburg: 4 killed

Date & Time: Oct 2, 1986
Type of aircraft:
Operator:
Registration:
3D-ART
Survivors:
No
Site:
MSN:
61
YOM:
1975
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
Following an uneventful flight, the crew started the approach to Pietersburg-Gateway Airport. On descent, the crew encountered poor weather conditions and the visibility was limited. Due to excessive workload in the cockpit, the crew failed to realize his altitude was insufficient when, at an altitude of 5,200 feet, the aircraft struck the slope of a mountain located near Haenertsburg, about 55 km east of Pietersburg Airport. The aircraft was destroyed upon impact and all four occupants were killed.
Probable cause:
It was determined that the crew failed to obtain proper weather bulletin prior to departure. After being stresses by an excessive workload, the crew failed to follow the published procedures and initiated the descente prematurely, causing the aircraft to descend below the minimum prescribed altitude. In consequence, the accident was the result of a controlled flight into terrain.

Crash of a Dassault Falcon 10 in Coatesville

Date & Time: Feb 27, 1986 at 2230 LT
Type of aircraft:
Operator:
Registration:
N821LG
Survivors:
Yes
Schedule:
New York-JFK – Lexington
MSN:
170
YOM:
1980
Crew on board:
2
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
8260
Captain / Total hours on type:
963.00
Aircraft flight hours:
1447
Circumstances:
As the aircraft was climbing thru 19,000 feet at night, the #2 generator (gen) light came on. The flight crew noted there was no output from the #2 gen and it would not reset. They then checked the #1 gen voltage and noted it was 14 to 15 volts. The crew reduced the electrical load; however, about 5 minutes later, the batteries became discharged and there was a total loss of electrical power. Using a flashlight, the crew diverted to the Chester County Airport which had a 4,600 feet runway. The gear was extended with the emergency system. The elevator trim was inoperative, so both pilots applied back pressure on the yoke to overcome the nose down tendency. After landing about 1/4 of the way down the runway, the crew tried to use the thrust reversers, but the reversers were inoperative. Subsequently, the aircraft continued off the side and beyond the end of the runway, hit a wooden beam and a snowbank, then came to rest in a ditch. An investigation revealed a shaft failure of the #2 gen (starter/gen) and worn brushes in the #1 gen. With total electrical failure, the following were also inoperative: wing flaps, anti-skid, capt's airspeed indicator and altimeter, nose wheel steering, cockpit lighting.
Probable cause:
Occurrence #1: airframe/component/system failure/malfunction
Phase of operation: cruise
Findings
1. (f) maintenance - inadequate - other maintenance personnel
2. (c) electrical system, generator - worn
3. (c) electrical system, generator - failure,total
4. Electrical system, battery - exhaustion
5. Electrical system - inoperative
6. Comm/nav equipment - inoperative
7. Flt control syst, stabilator trim - inoperative
8. Flight control, flap - inoperative
9. Landing gear, steering system - inoperative
10. Landing gear, anti-skid brake system - inoperative
11. Thrust reverser - inoperative
----------
Occurrence #2: loss of control - on ground/water
Phase of operation: landing - roll
Findings
12. (f) light condition - dark night
13. Performed
14. Precautionary landing - performed
15. (f) directional control - not maintained - pilot in command
16. Ground loop/swerve - uncontrolled
----------
Occurrence #3: overrun
Phase of operation: landing - roll
Findings
17. (f) powerplant controls - improper use of - pilot in command
----------
Occurrence #4: on ground/water collision with object
Phase of operation: landing - roll
----------
Occurrence #5: on ground/water encounter with terrain/water
Phase of operation: landing - roll
Final Report:

Crash of a Dassault Falcon 10 in Châlons-Vatry : 2 killed

Date & Time: Jan 15, 1986
Type of aircraft:
Operator:
Registration:
F-GBTC
Flight Type:
Survivors:
No
MSN:
124
YOM:
1978
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
Crashed on final approach to Châlons-Vatry Airport while on a positioning flight. Both pilots were killed.

Crash of a Dassault Falcon 10 in DuPage

Date & Time: Sep 23, 1985 at 1025 LT
Type of aircraft:
Operator:
Registration:
N700DK
Survivors:
Yes
Schedule:
Elkhart – DuPage
MSN:
191
YOM:
1981
Location:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
2697
Captain / Total hours on type:
375.00
Aircraft flight hours:
537
Circumstances:
The Falcon 10 touched down long and fast on a wet runway, experienced hydroplaning and went off the end of the runway, struck a drainage ditch and collapsed the landing gear. The nose gear came back and bent the throttle quadrant bracket, pulled the fuel controls to 90% power. This pushed the aircraft on its belly another 1,000-1,600 feet until it came to a stop on a hillside. Both pilots were uninjured.
Probable cause:
Occurrence #1: on ground/water encounter with terrain/water
Phase of operation: landing - roll
Findings
1. (c) in-flight planning/decision - improper - pilot in command
2. (c) planned approach - improper - pilot in command
3. (c) proper touchdown point - exceeded - pilot in command
4. (c) airspeed - excessive - pilot in command
----------
Occurrence #2: complete gear collapsed
Phase of operation: landing - roll
Findings
5. Landing gear, main gear - overload
6. Landing gear, nose gear - overload
Final Report:

Crash of a Dassault Falcon 10 in Chicago: 2 killed

Date & Time: Jan 30, 1980 at 1548 LT
Type of aircraft:
Operator:
Registration:
N253K
Flight Phase:
Survivors:
Yes
Schedule:
Chicago - Battle Creek
MSN:
10
YOM:
1974
Crew on board:
2
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
3453
Captain / Total hours on type:
635.00
Copilot / Total flying hours:
8845
Copilot / Total hours on type:
1163
Aircraft flight hours:
3196
Circumstances:
The airplane was unable to takeoff from Chicago-Merrill C. Meigs Airport runway 18, overran and crashed into Lake Michigan. A pilot and a passenger were killed while four other occupants were seriously injured. The aircraft came to rest in 25 feet of water about 300 feet past the runway end.
Probable cause:
The flightcrew's failure to release the parking brake before the takeoff roll was started, which resulted in significant wheel/brake drag and a nosedown pitching moment that inhibited the aircraft's capability to effect a normal acceleration and rotation for takeoff. Contributing to the accident was the lack of adequate company checklist procedures to insure the timely release of the parking brakes.
Final Report:

Crash of a Dassault Falcon 10MER at Toul-Rosières AFB

Date & Time: Jan 30, 1980
Type of aircraft:
Operator:
Registration:
39
Flight Type:
Survivors:
Yes
MSN:
039
YOM:
1975
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Aircraft flight hours:
2659
Circumstances:
The airplane suffered an accident at Toul-Rosières AFB. There were no casualties but the airplane was written off.

Crash of a Dassault Falcon 10 in Denver: 4 killed

Date & Time: Apr 3, 1977 at 0452 LT
Type of aircraft:
Operator:
Registration:
N60MB
Flight Phase:
Survivors:
Yes
Schedule:
Denver - Cheyenne
MSN:
15
YOM:
1974
Location:
Crew on board:
2
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
16122
Captain / Total hours on type:
800.00
Aircraft flight hours:
1425
Circumstances:
Few minutes after takeoff from Denver-Stapleton Airport, while climbing to an altitude of 12,000 feet, the crew reported hydraulic problems and was cleared to return. Shortly later, the airplane entered an uncontrolled descent and crashed in a field located 10 miles northeast of Stapleton Airport. A passenger was seriously injured while four other occupants were killed.
Probable cause:
Uncontrolled descent for undetermined reasons.
Final Report:

Crash of a Dassault Falcon 10 in Romorantin-Lanthenay: 2 killed

Date & Time: Oct 31, 1972
Type of aircraft:
Operator:
Registration:
F-WFAL
Flight Phase:
Flight Type:
Survivors:
No
MSN:
001
YOM:
1970
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
The crew (a pilot and a flight engineer) were engaged in a test flight on this first Dassault Falcon 10 prototype of the French manufacturer Avions Marcel Dassault (Dassault Aviation). While cruising at an altitude of 15,000 feet and a speed of 360 knots, control was lost. The airplane entered a dive and crashed in an open field located in Loreux, about 8 km northeast of Romorantin-Lanthenay. The aircraft was destroyed and both occupants were killed.
Crew:
Alain Tretout, pilot,
Jacques Ladeux, flight engineer.
Probable cause:
It is believed that the tail separated in flight following an excessive pressure on the vertical stab while cruising at high speed.