Crash of a Beechcraft C-45H Expeditor in Pearl Harbour: 11 killed

Date & Time: Dec 5, 1981 at 1908 LT
Type of aircraft:
Registration:
N8185H
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Honolulu - Honolulu
MSN:
AF-381
YOM:
1953
Crew on board:
1
Crew fatalities:
Pax on board:
11
Pax fatalities:
Other fatalities:
Total fatalities:
11
Captain / Total flying hours:
375
Circumstances:
The twin engine airplane departed Honolulu Airport to take part to a local airshow, carrying 11 skydivers and one pilot. While making a turn toward the jump area, the airplane entered a spin. Four occupants parachuted before the airplane crashed in Pearl Harbour. Only one passenger survived the crash and was seriously injured while 11 other occupants were killed. The airplane was destroyed.
Probable cause:
The airplane stalled and entered a spin after the pilot failed to maintain flying speed. The following contributing factors were reported:
- Inadequate preflight preparation,
- Improperly loaded aircraft,
- Unqualified person operated aircraft,
- Estimated CofG 10 inches behind limit.
Final Report:

Crash of a Cessna 402C off Pacific Grove

Date & Time: Dec 3, 1981 at 1445 LT
Type of aircraft:
Operator:
Registration:
N2611C
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Oakland - Honolulu
MSN:
402C-0071
YOM:
1979
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
6140
Captain / Total hours on type:
620.00
Circumstances:
En route from Oakland to Honolulu, both engines failed. The pilot reduced his altitude and ditch the aircraft off Pacific Grove. The pilot was rescued while the aircraft sank and was lost.
Probable cause:
engine failure in normal cruise due to fuel starvation for undetermined reasons. The following contributing factors were reported:
- Fuel starvation,
- Complete failure both engines,
- Forced landing off airport on water,
- Ferry fuel system installed,
- High fuel consumption.
Final Report:

Crash of a Mitsubishi MU-2B-30 Marquise off Pago Pago: 1 killed

Date & Time: Nov 22, 1981 at 1546 LT
Type of aircraft:
Registration:
N109TW
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Honolulu - Pago Pago
MSN:
543
YOM:
1971
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
While approaching Pago Pago on a flight from Honolulu, the pilot reported problems with fuel transfer. Shortly later, the airplane crashed into the ocean about 40-45 miles north of Pago Pago. The aircraft sank and the pilot was killed.
Probable cause:
Engine failure or malfunction and subsequent ditching due to fuel starvation for undetermined reasons. The following contributing factors were reported:
- Fuel starvation,
- Aircraft came to rest in water,
- Forced landing off airport on water.
Final Report:

Crash of a Piper PA-60 Aerostar (Ted Smith 600) off Honolulu: 1 killed

Date & Time: Jun 19, 1981
Operator:
Registration:
ZK-EHR
Flight Phase:
Flight Type:
Survivors:
No
MSN:
60-0312-116
YOM:
1977
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
The pilot, sole on board, was completing a delivery flight, the airplane being transferred to its new owner. In unclear circumstances, the aircraft crashed into the sea off Honolulu. Despite intensive search, the aircraft and the pilot were not recovered.
Probable cause:
Due to lack of evidences, the cause of the accident could not be determined.

Crash of a Beechcraft D18S in Honolulu: 2 killed

Date & Time: Jan 8, 1980 at 0635 LT
Type of aircraft:
Registration:
N641E
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Honolulu – Kahului
MSN:
A-265
YOM:
1946
Location:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
11625
Captain / Total hours on type:
6900.00
Circumstances:
Following a night takeoff from Honolulu, while climbing at a height of 600 feet, the airplane collided with a 35 feet wooden utility pole and 50 feet tubular steel microwave antenna tower. It crashed in flames and both occupants were killed.
Probable cause:
Collision with wires/poles due to inadequate preflight preparation on part of the crew. The following contributing factors were reported:
- Continued VFR flight into adverse weather conditions,
- Low ceiling,
- Rain,
- Thunderstorm activity,
- Visibility 3 miles or less.
Final Report:

Crash of a Lockheed 18-56 LodeStar in Palmyra Island

Date & Time: Jan 5, 1980 at 0700 LT
Type of aircraft:
Registration:
N163R
Flight Type:
Survivors:
Yes
Schedule:
Honolulu - Palmyra
MSN:
2492A
YOM:
1943
Crew on board:
2
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The twin engine airplane was completing a flight from Honolulu to the Palmyra Atoll, carrying amateur radio operators. After touchdown, the airplane went out of control, veered off runway and collided with trees. The aircraft was damaged beyond repair and all nine occupants evacuated, some of them were injured. On approach, the pilot estimated cross wind gusting to 15 knots but the wind was calm below tree level on runway.
Probable cause:
Ground loop upon touchdown and subsequent collision with trees due to improper compensation for wind conditions. The following contributing factors were reported:
- Windshear,
- Visibility 3 mils or less.
Final Report:

Crash of a Beechcraft C-45H Expeditor in the Pacific Ocean: 1 killed

Date & Time: Nov 4, 1979 at 1529 LT
Type of aircraft:
Registration:
N145DC
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
San Jose - Honolulu
MSN:
AF-564
YOM:
1953
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
En route from San Jose to Honolulu on a delivery flight, the pilot informed ATC about an engine failure and elected to ditch the airplane about 1,500 km northwest of Honolulu. The aircraft came to rest in water and the pilot was killed.
Probable cause:
Powerplant failure for undetermined reasons.
Final Report:

Crash of a Douglas C-47B-50-DK off Honolulu: 2 killed

Date & Time: Jul 20, 1979 at 1930 LT
Registration:
N63250
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
San Jose - Honolulu
MSN:
17062/34329
YOM:
1945
Location:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
8000
Circumstances:
While approaching Honolulu on a ferry flight from San jose, California, the crew declared an emergency via an auxiliary emergency system that all communication and navigation systems failed. Few minutes later, the airplane crashed into the ocean off Honolulu. SAR operations were initiated but eventually abandoned few days later as no trace of the aircraft nor the two crew members was found.
Probable cause:
Double engine failure in flight following a fuel exhaustion. The following contributing factors were reported:
- The crew became lost/disoriented,
- Failure of the communications and navigations equipment,
- Failure of the Loran receiver,
- Communications failure,
- Failure of both engines,
- Forced landing off airport on water,
- Aircraft not recovered,
- Pilot reported HF radio and Loran inoperative,
- Lost,
- No fuel.
Final Report:

Crash of a Douglas DC-10-10 in Los Angeles: 2 killed

Date & Time: Mar 1, 1978 at 0925 LT
Type of aircraft:
Operator:
Registration:
N68045
Flight Phase:
Survivors:
Yes
Schedule:
Los Angeles - Honolulu
MSN:
46904
YOM:
1972
Flight number:
CO603
Crew on board:
14
Crew fatalities:
Pax on board:
186
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
29000
Captain / Total hours on type:
2911.00
Copilot / Total flying hours:
10000
Copilot / Total hours on type:
1249
Aircraft flight hours:
21358
Circumstances:
On March 1, 1978, Continental Air Lines, Inc., Flight 603, a McDonnell Douglas DC-10-10 (N68045), was a scheduled flight from Los Angeles International Airport, California, to Honolulu, Hawaii. At 0857:18, Flight 603 called Los Angeles clearance delivery and was cleared for the route of flight which was to have been flown. About 2 min later, the flight received permission from Los Angeles ground control to push back from the gate. At 0901:37, Flight 603 was cleared by ground control to taxi to runway 6R. The runway was wet, but there was no standing water. At 0922:29, Los Angeles local control cleared Flight 603 to taxi into position on runway 6R and hold. At 0923:17, local control cleared Flight 603 for takeoff; however, the flightcrew did not acknowledge the instructions and did not comply with them. At 0923:57, local acknowledged the instructions. The captain stated that he delayed control, again, cleared the flight for takeoff. This time the flightcrew acknowledgment of the takeoff clearance because he believed that he had initially been given the clearance too soon after a heavy jet aircraft had made its takeoff. The flightcrew stated that acceleration was normal and that all engine instruments were in the normal range for takeoff. As the airspeed approached the V1 speed of 156 kns, the captain heard a loud "metallic bang" which was followed immediately by "a kind of quivering of the plane." The flightcrew noticed that the left wing dropped slightly. A rejected takeoff was begun immediately; however, according to the digital flight data recorder (DFDR), the airspeed continued to increase to about 159 kns as the rejected takeoff procedures were begun. The captain stated that he applied full brake pressure while simultaneously bringing the thrust levers back to idle power. Reverse thrust levers were actuated and full reverse thrust was used. The flightcrew stated that they noted good reverse thrust. First, the aircraft moved to the left of the runway centerline and appeared tb the flightcrew to be decelerating normally. With about of deceleration had decreased, and they believed that the aircraft would 2,000 ft of runway remaining, the flightcrew became aware that the rate not be able to stop on the runway surface. The captain stated that he maintained maximum brake pedal force and full reverse thrust as he steered the aircraft to the right of the runway centerline in an effort "to go beside the stanchions holding the runway lights" immediately off of the departure end of runway 6R. He stated further that he encountered no problems with directional control of the aircraft throughout the rejected takeoff maneuver. The aircraft departed the right corner of the departure end of runway 6R. About 100 ft beyond the runway, the left main landing gear broke through the nonload-bearing tar-macadam (tarmac) surface and failed rearward. Fire erupted immediately from this area. The aircraft dropped onto the left wing and the No. 1 (left) engine and rotated to the left as it continued its slide along the surface. It stopped between two of the approach light stanchions for runway 24L about 664 ft from the departure end of runway 6R and about 40 ft to the right of the runway 6R extended centerline; it came to rest on a heading of 008°, in an 11° left wing low, 1.3° noseup attitude. When the aircraft came to a stop, the evacuation was begun immediately. Two passengers were killed while all other occupants were evacuated, some of them with serious injuries.
Probable cause:
The National Transportation Safety Board determined that the probable cause of the accident was the sequential failure of two tires on the left main landing gear and the resultant failure of another tire on the same landing gear at a critical time during the takeoff roll. These failures resulted in the captain's decision to reject the takeoff. Contributing to the accident was the cumulative effect of the partial loss of aircraft braking because of the failed tires and the reduced braking friction achievable on the wet runway surface which increased the accelerate-stop distance to a value greater than the available runway length. These factors prevented the captain from stopping the aircraft within the runway confines. The failure of the left main landing gear and the consequent rupture of the left wing fuel tanks resulted in an intense fire which added to the severity of the accident.
Final Report:

Crash of a Beechcraft C-45G Expeditor off Honolulu

Date & Time: Dec 17, 1977 at 1558 LT
Type of aircraft:
Operator:
Registration:
N2874G
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Honolulu - Kahului
MSN:
AF-168
YOM:
1952
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
1984
Captain / Total hours on type:
251.00
Circumstances:
Shortly after takeoff from Honolulu Airport, while in initial climb, the airplane lost height and crashed into the sea few hundred yards offshore. The pilot was rescued while the aircraft was lost.
Probable cause:
Engine malfunction during climb due to material failure. The following contributing factors were reported:
- Powerplant - propeller and accessories: governors,
- engine structure: other,
- Unfavorable wind conditions,
- Aircraft came to rest in water,
- Left propeller governor drive gears failed,
- Right engine operated at full power failed over water short of airport, landed on reef.
Final Report: