Crash of a Rockwell Grand Commander 690A in Taos: 1 killed

Date & Time: Mar 29, 1992 at 1900 LT
Registration:
N111FL
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Taos - Tulsa
MSN:
690-11163
YOM:
1974
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
2200
Captain / Total hours on type:
120.00
Aircraft flight hours:
3404
Circumstances:
The airplane impacted slightly rising terrain in a 15° left bank, slight nose up attitude while descending shortly after takeoff in dark night IMC. There were rain and snow showers in the area and it was devoid of visible ground reference lights. The difference between the takeoff heading and the impact heading was 75° and the airplane had traveled 3,987 feet from the departure end of the runway at initial impact. The wreckage subsequently traveled an additional 837 feet through the brush. The pilot stated that the takeoff was normal in all aspects and all of the airplane systems were operating normally. He stated that the last thing he remembered was passing through 8,500 feet with a rate of climb of 1,500 feet per minute. The airport elevation was 7,091 feet. He did not recall the radio altimeter alert or the warning light activating. No evidence of pre-impact failure or malfunction was found during the investigation. Rescue of the occupants were delayed due to the weather, darkness, and spurious elt signals masked by the wreckage.
Probable cause:
The pilot in command's failure to maintain the climb after departing the runway environment. Factors were the weather conditions and the dark night.
Final Report:

Crash of a Rockwell Grand Commander 690 in Wichita: 2 killed

Date & Time: Nov 2, 1991 at 1206 LT
Registration:
N799V
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Wichita - Phoenix
MSN:
690-11407
YOM:
1977
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
4900
Captain / Total hours on type:
1078.00
Aircraft flight hours:
3480
Circumstances:
The pilot and his wife departed Wichita, Kansas with a destination of Phoenix, Arizona. Eight minutes after takeoff, while in a climb to 15,000 feet, the passenger contacted departure control and communicated that she thought that her husband might be dead. While departure control was getting a pilot to assist in the situation, the passenger, who was not a pilot attempted to fly the aircraft. A witness reported a rapid series of climbs and descents just before both horizontal stabilizers and the rudder separated from the aircraft. The aircraft then entered a spin terminating with ground impact. The aircraft was consumed by a post-crash fire. Both occupants were killed.
Probable cause:
Incapacitation of the pilot in command, followed by the loss of control and an inflight breakup with a unqualified person on the controls.
Final Report:

Crash of a Rockwell Grand Commander 690A off San Andrés: 9 killed

Date & Time: Sep 7, 1991 at 2325 LT
Registration:
HK-2415
Survivors:
No
MSN:
690-11100
YOM:
1973
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
9
Circumstances:
Following an uneventful flight from the continent, the crew established initial contact with local ATC at 2324LT on approach to San Andrés-Sesquicentenario Airport. A minute later, while descending by night and poor weather conditions, the twin engine aircraft entered an uncontrolled descent and crashed in the sea few km offshore. SAR operations were initiated but eventually suspended a week later as no trace of the aircraft nor the nine occupants was found.
Probable cause:
Due to lack of evidences, the exact cause of the accident could not be determined. However, it is believed that the loss of control on approach by night and limited visibility due to poor weather conditions occurred after the pilot-in-command suffered a spatial disorientation while flying over water without any ground visual references.

Crash of a Rockwell Grand Commander 690B in La Paz

Date & Time: May 30, 1991
Operator:
Registration:
FAB-023
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
La Paz - Tarija
MSN:
690-11562
YOM:
1979
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed in unknown circumstances while taking off from La Paz-El Alto Airport. All eight occupants were rescued while the aircraft was destroyed.

Crash of a Rockwell Grand Commander 690 in Abasolo: 3 killed

Date & Time: Jan 10, 1991
Operator:
Flight Type:
Survivors:
No
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
The aircraft (exact type unknown) was completing an illegal flight from Colombia. Apparently, the pilot was trying to land on a ranch property called Las Malvinas when the aircraft crashed in unknown circumstances nar Abasolo. All three occupants were killed and a load of 180 kilos of cocaine was found among the debris.

Crash of a Rockwell Grand Commander 690A in Ryderwood: 5 killed

Date & Time: Nov 30, 1990 at 1841 LT
Operator:
Registration:
N400N
Flight Type:
Survivors:
Yes
Site:
Schedule:
Nanaimo - Kelso
MSN:
690-11156
YOM:
1974
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
11714
Captain / Total hours on type:
2647.00
Circumstances:
As the flight was approaching the destination, at night, the pilot obtained vectors for a descent over mountainous terrain. During the approach, he cancelled the IFR flight plan and the aircraft descended below radar coverage. Subsequently, the aircraft crashed in mountainous terrain, northwest of the destination airport. Impact occurred in a wooded area at an elevation of about 2,700 feet. The ELT did not activate during the accident. A search was initiated on 12/1/90, but the aircraft and surviving passenger were not found until the next day. The Canadian ATP pilot and other four passengers were fatally injured. After initial impact with trees, the main portion of the fuselage traveled about 1,000 feet before coming to rest. No preimpact mechanical problem was found.
Probable cause:
The pilot's improper inflight planning and failure to maintain proper altitude in mountainous terrain at night.
Final Report:

Crash of a Rockwell Grand Commander 690B in Byram Lake Reservoir

Date & Time: Sep 22, 1990 at 1005 LT
Registration:
N81628
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Charleston - White Plains
MSN:
690-11396
YOM:
1977
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
11000
Captain / Total hours on type:
1243.00
Circumstances:
During an IFR flight the pilot executed a forced landing in a reservoir after the engines quit due to fuel exhaustion. The pilot reported that the airplane was fueled, topped off, the night before departure from Charleston. Examination of the airplane showed the outboard fuel filler port cap on the left wing was not present. The majority of the liquid drained from the main fuel sump was water. The inboard and outboard fuel filler caps were present on the right wing. All six occupants were rescued.
Probable cause:
The pilot's improper aircraft preflight (fuel cap not properly secured) which resulted in fuel siphoning and fuel exhaustion.
Final Report:

Crash of a Rockwell Grand Commander 690A in Little Rock: 1 killed

Date & Time: May 17, 1988 at 0532 LT
Operator:
Registration:
N660RB
Flight Type:
Survivors:
No
Schedule:
Atlanta – Memphis – Little Rock
MSN:
690-11305
YOM:
1976
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
6410
Captain / Total hours on type:
1562.00
Aircraft flight hours:
6577
Circumstances:
The pilot had just returned from vacation in the Bahamas before starting a flight from Little Rock to Atlanta with an intermediate stop at Memphis. This itinerary was followed by a return flight to Little Rock via a reverse routing. Witnesses reported the pilot said he had only 2 hours of sleep before departing Little Rock and that he was really tired. Also, company personnel noted the pilot looked 'extremely tired' and was 'really dragging' prior to the last leg of the flight from Memphis to Little Rock. According to ATC personnel, the flight was routine until the aircraft was arriving at Little Rock. During arrival, the pilot was cleared to descend from 7,000 feet to 2,000 feet at his discretion for a visual approach to runway 22. At 0522 cdt, the pilot reported the airport in sight and was cleared for a visual approach. About 4 minutes later, he again reported the airport in sight and was cleared to land. At 1031, radar contact was lost and the aircraft crashed about 4 miles west of the airport. Initial impact was in an open field while descending in a relatively level attitude. The aircraft became airborne for about 3/4 mile, then crashed out of control in the Arkansas River. The pilot, sole on board, was killed.
Probable cause:
Occurrence #1: loss of control - in flight
Phase of operation: approach
Findings
1. (c) judgment - poor - pilot in command
2. (f) light condition - dawn
3. Descent - initiated
4. (c) level off - not performed - pilot in command
5. (c) fatigue (lack of sleep) - pilot in command
----------
Occurrence #2: in flight collision with terrain/water
Phase of operation: approach
Final Report:

Crash of a Rockwell Grand Commander 690B in Albuquerque

Date & Time: Oct 8, 1987 at 1615 LT
Registration:
N711TT
Flight Type:
Survivors:
Yes
Schedule:
Oklahoma City - Albuquerque
MSN:
690-11362
YOM:
1976
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
7230
Captain / Total hours on type:
1086.00
Aircraft flight hours:
1829
Circumstances:
Aircraft was landing on runway 17 at Coronado Airport, 9 NM north of Albuquerque, NM Intl Airport. Pilot said he brought props into reverse and aircraft went off right side of runway. Pilot brought props out of reverse, realigned aircraft on runway, and reversed props again. Aircraft went off right side of runway and collided with runway lights and culverts. Right main and nose landing gears collapsed. Witnesses said approach was too fast with high sink rate that was arrested in landing flare. Pilot said he did not think there had been any mechanical failure or malfunction, but later wrote he thought left prop failed to reverse. Examination of aircraft revealed both prop blade tips curled opposite direction of rotation about 6 inches from tip.
Probable cause:
Occurrence #1: loss of control - on ground/water
Phase of operation: landing - roll
Findings
1. (f) airspeed (vref) - excessive - pilot in command
2. (c) directional control - not maintained - pilot in command
3. (f) planned approach - poor - pilot in command
----------
Occurrence #2: on ground/water collision with object
Phase of operation: landing - roll
Findings
4. (f) object - runway light
----------
Occurrence #3: gear collapsed
Phase of operation: landing - roll
Final Report:

Crash of a Rockwell Grand Commander 690A in Hilliard: 2 killed

Date & Time: Jun 24, 1987 at 0235 LT
Operator:
Registration:
N57169
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Jacksonville - Atlanta
MSN:
690-11203
YOM:
1974
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
6129
Captain / Total hours on type:
170.00
Aircraft flight hours:
6970
Circumstances:
Radar data indicated the aircraft climbed normally to 9,200 feet at which time some maneuver was performed with the aircraft. The aircraft then entered a near vertical dive and the last radar hit was at 6,900 feet. Examination of the aircraft revealed it experienced an inflight structural breakup and there was no evidence to indicate prebreakup failure or malfunction of the aircraft structure, flight controls, engines, engine mounts, autopilot, or systems. The operator reported one employee overheard the pilot and passenger talk about rolling the aircraft prior to departure, and two company employees reported being onboard when the pilot had rolled it on prior occasions. One of these was at night. Both occupants were killed.
Probable cause:
Occurrence #1: abrupt maneuver
Phase of operation: climb - to cruise
Findings
1. (c) aerobatics - performed - pilot in command
2. (c) overconfidence in personal ability - pilot in command
----------
Occurrence #2: loss of control - in flight
Phase of operation: maneuvering
Findings
3. (c) directional control - not maintained - pilot in command
4. (c) altitude - not maintained - pilot in command
5. Light condition - dark night
----------
Occurrence #3: airframe/component/system failure/malfunction
Phase of operation: descent - uncontrolled
Findings
6. (c) design stress limits of aircraft - exceeded - pilot in command
----------
Occurrence #4: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Final Report: