Crash of a Rockwell Grand Commander 680 in North Bend: 3 killed

Date & Time: Jun 1, 1995 at 1554 LT
Operator:
Registration:
N6877S
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
North Bend - North Bend
MSN:
680-462-132
YOM:
1958
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
1450
Aircraft flight hours:
4785
Circumstances:
Approximately two minutes after takeoff, witnesses saw the airplane pull up sharply into a steep climb from underneath an 800-foot ceiling. The airplane went into an uncontrolled, nearly vertical dive and impacted into a river. The pilot did not hold multi-engine or instrument ratings. Individuals who knew the pilot, including an instructor who had flown with him, stated that they had doubted the pilot's competence but that the pilot had been confident of his own flying ability.
Probable cause:
The pilot initiating flight into weather conditions beyond what he was capable of handling. The pilot's overconfidence in his personal ability and the low ceiling were factors in the accident.
Final Report:

Crash of a Rockwell Grand Commander 680F near Cloncurry: 2 killed

Date & Time: Nov 9, 1994 at 1015 LT
Operator:
Registration:
VH-SPP
Flight Phase:
Survivors:
No
Schedule:
Cloncurry - Cloncurry
MSN:
680-1128-74
YOM:
1961
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
11400
Captain / Total hours on type:
710.00
Aircraft flight hours:
7546
Circumstances:
The aircraft was engaged in aero-magnetic survey operations in an area which extended from approximately 40–130 km south of Cloncurry. The task involved flying a series of north-south tie lines spaced 2 km apart at a height above ground of 80 m and a speed of 140 kts. At this speed, each tie line occupied about 20 minutes of flight time. The flight was planned to depart Cloncurry at 0700–0730 EST and was to return by 1230 to prepare data collected during the flight for transfer to the company’s head office. An employee of the operating company saw the crew (pilot and equipment operator) preparing to depart the motel for the airport at about 0500. No person has been found who saw the crew at the aerodrome or who saw or heard the aircraft depart. At about 1000, three witnesses at a mining site in the southern section of the survey area saw a twin-engine aircraft at low level heading in a northerly direction. One of these witnesses, about 1.5 hours later, saw what he believed was the same aircraft flying in an easterly direction about 1 km from his position. Between 1000 and 1030, two witnesses at a mine site some 9 km north of the survey area (and about 5 km west of the accident site) heard an aircraft flying in a north-south direction, apparently at low level. On becoming aware that the aircraft had not returned to Cloncurry by 1230, a company employee at Cloncurry initiated various checks at Cloncurry and other aerodromes in the area, with Brisbane Flight Service, and with the company’s head office later in the afternoon. At about 2030, the employee advised the company chief pilot that the aircraft was overdue. The chief pilot contacted the Civil Aviation Authority Search and Rescue organisation at about 2045 and search-and-rescue action was initiated. The burnt-out wreckage of the aircraft was found early the following morning approximately 9 km north of the survey area.
Probable cause:
For reason(s) which could not be conclusively established, the pilot shut off the fuel supply to the left engine and feathered the left propeller. For reason(s) which could not be conclusively established, the pilot lost control of the aircraft.
Final Report:

Crash of a Rockwell Grand Commander 680 near Väsby: 2 killed

Date & Time: Jul 7, 1994 at 1815 LT
Operator:
Registration:
SE-GUO
Flight Phase:
Survivors:
No
Schedule:
Eskilstuna - Eskilstuna
MSN:
680-0535-204
YOM:
1957
Location:
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
4500
Captain / Total hours on type:
3000.00
Aircraft flight hours:
9965
Circumstances:
In the afternoon, the aircraft departed Eskilstuna Airport, carrying one geotechnician and one pilot for a low level survey mission on behalf of the Swedish Geological Service. Approaching the area of Väsby under visual flight rules conditions, while flying at an altitude of 30-50 metres, the aircraft collided with power cables. The right wing was partially sheared off then the airplane entered an uncontrolled descent and crashed 180 metres further. Both occupants were killed. There was no fire.
Probable cause:
It was determined that the accident was caused by the crew not being able to see in time those unknown to them and difficult-to-detect antenna cables emanating from the top of the telemast.
Contributing to the accident was the lack of information about the mast's special design in aviation publications.
Final Report:

Crash of a Rockwell Grand Commander 680F near Chihuahua: 3 killed

Date & Time: Jun 3, 1993
Registration:
N8676D
Flight Phase:
Flight Type:
Survivors:
No
MSN:
680-1160-84
YOM:
1962
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
3
Aircraft flight hours:
31073
Circumstances:
Crashed in unknown circumstances in the region of Chihuahua, killing all three occupants.

Crash of a Rockwell Grand Commander 680FL in Lester: 1 killed

Date & Time: Dec 25, 1992 at 2137 LT
Operator:
Registration:
N111MN
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Seattle - Spokane
MSN:
680-1806-150
YOM:
1968
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
3108
Captain / Total hours on type:
138.00
Aircraft flight hours:
11219
Circumstances:
After departure, the airplane intercepted airway V-2, and appeared to climb normally until reaching 8,300 feet (9,000 assigned) while tracking approximately 110° magnetic. Radar analysis showed the airplane at 128 kias when it abruptly turned left 30° and then appeared to recover. Voice communication during this event was normal with no change in the pilot's level of anxiety. Immediately thereafter, the heading changed over 90° to the left (northbound), and a maximum 6,750 fpm rate of descent developed before the heading stabilized and the descent slowed. The airplane's ground impact site was approximately 1 nm southwest of the last radar target. Wreckage distribution was roughly parallel to V-2. The airplane impacted the mountainside in a steep nose low, left wing down attitude. The engines, propellers/governors were disassembled and inspected with no evidence of mechanical malfunction. Exam of the left propeller indicated low power on impact. There was no evidence of significant icing/turbulence. The pilot, sole on board, was killed.
Probable cause:
The exact cause of the accident could not be determined.
Final Report:

Crash of a Rockwell Grand Commander 680 in Titusville

Date & Time: Aug 5, 1990 at 0940 LT
Operator:
Registration:
N599BB
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
680-372-57
YOM:
1956
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
3000
Captain / Total hours on type:
1.00
Circumstances:
About 5-10 min after takeoff the pilot leaned the mixture on a rough running engine. About 30 minutes later the left engine began to overspeed. The pilot was unable to feather the prop. The pilot returned toward the departure point with max power on the right engine. Unable to reach the airport, an emergency landing was made on a highway, directional control was lost, and the airplane collided with trees. Last annual was in 1978. Left propeller start lock pin blade L3 corroded, in extended position. Left propeller pitch control cable separated, frayed, corroded. General deterioration of piston rings and #6 conrod. Right prop governor control cables corroded, frayed. Right engine #5 intake pipe connection and hose missing. All compression rings pistons #1 and #5 severely worn, top two compression rings piston #2 seized. No record that the airplane had been inspected by an a&p mechanic or FAA approved airframe repair station. Pilot stated flight manual not available or used during ground or flight operations.
Probable cause:
The pilot's decision to continue the flight with a known unairworthy mechanical condition resulting in a subsequent loss of engine power and forced landing.
Final Report:

Crash of a Rockwell Grand Commander 680E in Hassela: 2 killed

Date & Time: Jul 25, 1990
Operator:
Registration:
SE-FTP
Flight Phase:
Survivors:
No
MSN:
680-0623-1
YOM:
1958
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Aircraft flight hours:
8346
Circumstances:
The crew was completing a survey flight at low level when the right wing failed. The aircraft went out of control and crashed near Hassela. Both crew members were killed.
Probable cause:
Failure of the right wing in flight due to fatigue cracks.

Crash of a Rockwell Grand Commander 680FLP in Kona: 1 killed

Date & Time: Sep 10, 1989 at 1518 LT
Registration:
N22LR
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Kona - Honolulu
MSN:
680-1503-18
YOM:
1965
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
203
Captain / Total hours on type:
23.00
Aircraft flight hours:
4790
Circumstances:
As the aircraft was departing from runway 17, smoke was observed coming from the right engine. The pilot confirmed a loss of power and made a right turn back toward the runway, then reported he had 'lost both engines.' The aircraft was extensively damaged during a landing on rough, rocky terrain about 1/4 mile southwest of the runway threshold. Investigation revealed the aircraft had just changed ownership. During pre-purchase inspection in Florida, metal particles were found in the oil screens of both engines. Oil was changed and flushed, but metal particles were found after another engine run. In May 1989, the right engine was replaced with an engine from another aircraft. The aircraft was flown to Oakland, CA, where it was painted and new interior was installed. A local mechanic noted metal particles in both eng oil screens and recommended oil analysis, but ferrying pilot refused. After flight to Hawaii, no oil stain noted on fuselage before flight on 9/9/89. Exam of wreckage revealed both engines failed from detonation. Heavy oil streaks found behind right engine, some streaks of oil found behind left engine. Right engine crankshaft/rod bearing surface was 0.010' under standard, but rod bearings were standard size. While the passenger was seriously injured, the pilot was killed.
Probable cause:
Inadequate maintenance, and operation by the pilot with known deficiencies in the aircraft. Factors related to the accident were: excessive wear in both engines, improper use of powerplant controls by the pilot, subsequent overtemperature/detonation in both engines, improper emergency procedures by the pilot (including premature gear extension and/or failure to properly reduce drag on the aircraft after loss of engine power), and the pilot's lack of experience in multi engine and this make and model of aircraft.
Final Report:

Crash of a Rockwell Grand Commander 680FP off Kristiansand

Date & Time: May 3, 1989
Operator:
Registration:
TF-AFM
Flight Type:
Survivors:
Yes
MSN:
680-1420-148
YOM:
1964
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was completing a flight from Sweden to Iceland when he encountered engine problems and decided to divert to Kristiansand Airport. On final approach, the aircraft crashed in the sea few km short of runway 04. Both pilots were rescued while the aircraft was damaged beyond repair.

Crash of a Rockwell Grand Commander 680E in King Island

Date & Time: Jul 14, 1988 at 2017 LT
Operator:
Registration:
VH-CAY
Flight Type:
Survivors:
Yes
Schedule:
Melbourne – King Island
MSN:
680-0855-76
YOM:
1959
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The King Island aerodrome weather was forecast to include temporary periods of moderate to heavy rain showers, six eighths of cloud cover base 800 feet and visibility reduced to 3000 metres. The forecast surface wind was 340 degrees at 20-30 knots. The pilot's qualifications required a minimum visibility of 5000 metres for operation at night in Visual Meteorological Conditions, (NGT VMC). It was planned that another pilot, qualified for Instrument Flight Rules (IFR) operations, would act as pilot in command, but he became unavailable. The flight plan submitted by the pilot indicated he would be operating under the IFR category and when queried on taxiing he confirmed that this was so. Shortly after DEPARTURE, the pilot requested a weather report from an IFR pilot who had just landed at King Island. This gave a cloud base of 2000 feet, heavy rain showers and visibility of 2000 metres. Flares had been laid to allow the other pilot to use Runway 35 because of the strong northerly wind. The pilot of VH-CAY activated the electric lighting for Runway 28. He reported that the weather was satisfactory enroute and he could see lights ahead on the island. On crossing the coast flight conditions became rough in moderate to severe turbulence. The pilot advised he arrived over the aerodrome at 1500 feet above mean sea level and observed the lighted wind sock was horizontal, with the direction fluctuating rapidly between north and west. He turned to the south and broadcast his intention to land on Runway 28. Neither the pilot nor the passenger had any further recall of the events leading to the accident. VH-CAY was heard passing over the aerodrome and the engine sound was very loud, suggesting to the listener that the aircraft was low. It had been raining continuously for more than an hour, sometimes very heavily, and it was still raining at the time. The aircraft was subsequently seen flying at a very low height some six kilometres south of the aerodrome, tracking approximately north. It was raining very heavily in that area and the wind was very strong. Soon afterwards there was a sound of impact and a flash of light. The aircraft had struck the tops of trees 30 feet high, then descended to the ground. After the aircraft came to rest it was destroyed by a fire. Both occupants were seriously injured.
Probable cause:
Examination of the wreckage was severely hampered by the extreme fire damage sustained, but no evidence was found of any defects that might have contributed to the accident. The aircraft had evidently been under control at the time it collided with the trees. A post analysis of the conditions by the Bureau of Meteorology indicated the possible presence of strong up and down drafts, horizontal wind shear, turbulence, and estimated visibility as 2-3000 metres in rain. The evidence suggested that the pilot may have been lower than he believed as the aircraft overflew the
aerodrome. Having passed overhead, there there would have been few external visual references under the existing conditions to alert him that the aircraft was inadvertently being descended into the ground.
Significant Factors:
The following factors were considered relevant to the development of the accident:
1. The pilot attempted to conduct an operation for which he was not qualified.
2. Severe weather conditions in the destination aerodrome area with strong winds, turbulence, heavy rain and poor visibility.
3. The pilot continued flight into adverse weather conditions.
4. The pilot may have misread his altimeter and been lower than intended.
5. The pilot may have unintentionally descended the aircraft into the ground in conditions of poor visibility.
Final Report: