Crash of a Cessna 402A in Kahului

Date & Time: Apr 29, 1987 at 0854 LT
Type of aircraft:
Registration:
N4588Q
Flight Type:
Survivors:
Yes
Schedule:
Kahului - Lanai
MSN:
402A-0088
YOM:
1969
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
6650
Circumstances:
Shortly after takeoff, the pilot requested an 'immediate downwind' to return to the airport and was cleared to land. When asked if equipment was needed, he replied, 'negative, sir, a little matter of fuel.' A witness said the aircraft appeared very low on final approach with both props turning. The aircraft crash landed short of the runway, went thru a perimeter fence and came to rest on an incline about 10 feet short of the runway. The pilot received a head injury and couldn't remember many details of the occurrence. In an early interview, he induced there was a partial power loss and the aircraft yawed, but he couldn't remember which engine 'cut out first.' Later, he was unable to recall losing power. Six gallons of fuel was found in the left main tank, about 1.5 gallon was in the right main tank. The left fuel selector was found in the 'main' position, but due to damage and rescue activities, the position of the right fuel selector was not determined. Both auxiliary pump switches were in the 'off' position. The left propeller control was in the feather position, but neither propeller had feathered. Each main tank held one gallon of unusable fuel. A test of the pilot's blood showed 0,45‰ alcohol.
Probable cause:
Occurrence #1: loss of engine power (partial) - nonmechanical
Phase of operation: approach
Findings
1. (c) preflight planning/preparation - inadequate - pilot in command
2. (f) refueling - not performed - pilot in command
3. (f) fluid, fuel - low level
4. Precautionary landing - initiated
5. (c) fluid, fuel - starvation
6. (c) fuel supply - inadequate - pilot in command
7. (f) impairment (alcohol) - pilot in command
----------
Occurrence #2: forced landing
Phase of operation: descent - emergency
Findings
8. (c) planning/decision - improper - pilot in command
----------
Occurrence #3: in flight collision with terrain/water
Phase of operation: landing
Findings
9. (f) terrain condition - rough/uneven
----------
Occurrence #4: on ground/water collision with object
Phase of operation: landing
Findings
10. (f) object - fence
Final Report:

Crash of a Consolidated PBY-5A Catalina off Kahului

Date & Time: Apr 14, 1986
Type of aircraft:
Registration:
C-FSAT
Flight Type:
Survivors:
Yes
MSN:
21986
YOM:
1943
Location:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
After being stores for almost a year, the seaplane was engaged in a local test flight in the region of Kahului. Upon landing on sea, it collided with reef and came to rest. There were no casualties but the aircraft was damaged beyond repair.
Probable cause:
Collision with reef upon landing.

Crash of a Douglas C-54G-10-DO Skymaster in Kahului

Date & Time: Jun 29, 1983 at 0210 LT
Type of aircraft:
Registration:
N300JT
Flight Type:
Survivors:
Yes
Schedule:
Hilo - Kahului
MSN:
36072
YOM:
1945
Location:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
7200
Captain / Total hours on type:
375.00
Aircraft flight hours:
55517
Circumstances:
During arrival, a descent was begun from 8,000 to 7,000 feet msl at 0151 hst. At 0155 hst, the aircrew was cleared for a visual approach from 7,000 feet msl and a rapid descent was started with 20° of flaps and approximately 25 inches ap (manifold pressure). The aircraft was maneuvered to intercept the ILS localizer and glide slope as a reference. After intercepting the glide slope at about 3,000 feet, the pilot-in-command (pic) called for 2,250 rpm and gear extension. While descending thru approximately 2,000 feet, he noticed the aircraft slowing down and descending below the glide slope, so he called for a power increase to 27 inches map. At about that time, the aircrew noted that the engines were not responding and had lost power. Subsequently, a forced landing was made in a sugar cane field with the gear in a transient position. The fuel selectors were found positioned to fuel tanks containing fuel, but the positioning during the descent was not verified. The temperature and dew point were 72° 65° F. This would have been barely within the envelope for carburetor ice on icing probability charts. All three occupants were uninjured.
Probable cause:
Occurrence #1: loss of engine power(total) - nonmechanical
Phase of operation: approach - FAF/outer marker to threshold (IFR)
Findings
1. (f) weather condition - carburetor icing conditions
2. (c) carburetor heat - improper use of - pilot in command
3. (c) fuel system,carburetor - ice
4. (f) aircraft performance,two or more engines - inoperative
----------
Occurrence #2: forced landing
Phase of operation: landing - flare/touchdown
----------
Occurrence #3: in flight collision with terrain/water
Phase of operation: landing - flare/touchdown
Findings
5. (f) light condition - night
6. (f) wheels up landing - performed - pilot in command
Final Report:

Crash of a Convair CV-440 Metropolitan in Pearl Harbor

Date & Time: Jan 17, 1982 at 2245 LT
Operator:
Registration:
N21DR
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Honolulu - Kahului
MSN:
325
YOM:
1956
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
3550
Captain / Total hours on type:
88.00
Aircraft flight hours:
40846
Circumstances:
After liftoff, the pilot called for the landing gear to be raised. As the plane was climbing through about 100 feet agl, the pilot noted a loss of power in the right engine and saw a fire light. Ground witnesses heard a muffled explosion and saw smoke and fire trailing from the right engine. The right engine was feathered and the pilot attempted to return to the airport, but was unable to maintain altitude. The plane was ditched near the entrance of Pearl Harbor. A tear down of the right engine revealed that the top ring lands of the n° 10 and n°14 pistons were broken and the top ring was missing from each of the pistons. Also, the rear counterbalance drive intermediate gear was worn and 11 gear teeth were missing. Additionally, the rear counterbalance drive gear was worn.
Probable cause:
Loss of engine power and mechanical failure during initial climb due to partial piston failure. The following findings were reported:
- Engine assembly, ring, partial failure,
- Fire, explosion,
- Dark night.
Final Report:

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 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:

Crash of a Beechcraft E18S off Maui Island

Date & Time: Jun 12, 1974 at 1240 LT
Type of aircraft:
Registration:
N39A
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Honolulu - Van Nuys
MSN:
BA-115
YOM:
1955
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
16640
Captain / Total hours on type:
2000.00
Circumstances:
The pilot, sole on board, was performing a ferry flight from Honolulu to Van Nuys, California. While cruising along the coast of the Maui Island, both engines failed simultaneously. Unable to maintain a safe altitude, he ditched the aircraft 22 miles offshore. The pilot was rescued while the aircraft sank and was lost.
Probable cause:
Double engine failure in flight following a fuel exhaustion. The following factors were reported:
- Inadequate preflight preparation,
- Improper in-flight decisions,
- Mismanagement of fuel,
- Miscalculated fuel consumption,
- Fuel exhaustion,
- Pilot became lost/disoriented,
- HF communication inoperative.
Final Report:

Crash of a Beechcraft H18 near Hilo: 11 killed

Date & Time: Apr 11, 1974 at 0941 LT
Type of aircraft:
Operator:
Registration:
N28358
Flight Phase:
Survivors:
No
Site:
Schedule:
Kailua-Kona – Kahului
MSN:
BA-755
YOM:
1969
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
10
Pax fatalities:
Other fatalities:
Total fatalities:
11
Captain / Total flying hours:
4490
Captain / Total hours on type:
522.00
Circumstances:
While flying in poor weather conditions, the twin engine airplane struck the slope of a mountain located northwest of Hilo. The wreckage was found a day later and all 11 occupants have been killed.
Probable cause:
It was determined that the pilot was flying under VFR mode in adverse weather conditions. High obstructions and low ceiling were considered as contributing factors.
Final Report:

Crash of a Beechcraft SNB-5 Navigator in Kahului: 1 killed

Date & Time: Jan 15, 1966 at 0247 LT
Type of aircraft:
Registration:
N86454
Flight Type:
Survivors:
No
Site:
MSN:
4488
YOM:
1943
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
10000
Captain / Total hours on type:
130.00
Circumstances:
While approaching Kahului Airport by night under VFR mode, the pilot got disoriented and was unable to locate Kahului Airport. He flew past the destination over dark unlighted terrain when the twin engine airplane struck a hill and crashed in flames. The pilot was killed. At the time of the accident, the ceiling was about 2,000 feet with rain showers.
Probable cause:
The pilot got disoriented and was unable to locate the airport until the airplane struck the ground.
Final Report:

Crash of a Beechcraft C-45H Expeditor in Kahului: 2 killed

Date & Time: Nov 12, 1965 at 1415 LT
Type of aircraft:
Registration:
N9915Z
Flight Type:
Survivors:
No
Site:
Schedule:
Honolulu – Kahului
MSN:
AF-684
YOM:
1954
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
11272
Captain / Total hours on type:
500.00
Circumstances:
While approaching Kahului Airport in poor weather conditions, the twin engine aircraft struck the slope of a mountain located few miles from the airfield and was destroyed upon impact. The wreckage was found in a inaccessible area a day later and both occupants have been killed.
Probable cause:
The pilot got disoriented in IFR conditions for undetermined reason. The airplane was under control at impact.
Final Report: