Crash of a Cessna 340A in Valencia: 2 killed

Date & Time: Jun 11, 1985 at 1156 LT
Type of aircraft:
Operator:
Registration:
EC-DFC
Flight Phase:
Flight Type:
Survivors:
No
MSN:
340A-0270
YOM:
1976
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
Shortly after takeoff, the aircraft suffered an engine failure. Control was lost and the aircraft crashed, bursting into flames. Both pilots were killed.
Probable cause:
Engine failure during initial climb for unknown reasons.

Crash of a Cessna 340 near Las Vegas: 1 killed

Date & Time: Oct 29, 1984
Type of aircraft:
Registration:
N4001Q
Flight Type:
Survivors:
No
Site:
MSN:
340-0001
YOM:
1971
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
5715
Circumstances:
The pilot was carrying illegal cargo (marijuana) in N4001Q. During a low high speed pass at night over an intended landing area, the aircraft struck rising terrain. There was approximately 800 lbs of marijuana on the aircraft. The aircraft was destroyed and the pilot, sole on board, was killed.
Probable cause:
Occurrence #1: in flight collision with terrain/water
Phase of operation: maneuvering
Findings
1. (f) light condition - dark night
2. (c) visual lookout - not possible - pilot in command
3. (f) terrain condition - rising
4. (c) low pass - attempted - pilot in command
Final Report:

Crash of a Cessna 340A in Cincinnati: 4 killed

Date & Time: Jun 20, 1984 at 1217 LT
Type of aircraft:
Registration:
N5345J
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Cincinnati – Williamsburg
MSN:
340A-0418
YOM:
1978
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
1900
Aircraft flight hours:
1000
Circumstances:
Pilot requested fuel from fbo but failed to make it clear what type he wanted. The fbo personnel misunderstood the pilot's request and refueled the aircraft with 'Jet-A' instead of aviation grade gasoline. The pilot did not monitor the refueling process and failed to recognize the wrong fuel as stated on fuel receipt. The pilot did not realize the improper fuel on his preflight of the aircraft. The aircraft departed and shortly there after the pilot radioed that he was returning to the airport because of a serious problem. Witnesses near the accident site stated that the aircraft was in a left bank (about 45° bank angle) before impact in a densely wooded area. The aircraft was destroyed and all four occupants were killed.
Probable cause:
Occurrence #1: loss of engine power (partial) - nonmechanical
Phase of operation: takeoff - initial climb
Findings
1. (c) fluid,fuel - improper
2. (c) refueling - improper - fbo personnel
3. (f) information unclear (phraseology) - pilot in command
4. (f) fbo personnel
5. (f) refueling - inattentive - pilot in command
6. (c) aircraft preflight - inadequate - pilot in command
----------
Occurrence #2: forced landing
Phase of operation: descent - emergency
----------
Occurrence #3: in flight collision with object
Phase of operation: descent - emergency
Findings
7. Object - tree(s)
----------
Occurrence #4: fire/explosion
Phase of operation: other
Final Report:

Crash of a Cessna 340A in Goulburn: 4 killed

Date & Time: May 16, 1984 at 2304 LT
Type of aircraft:
Operator:
Registration:
VH-BYB
Flight Type:
Survivors:
No
Site:
Schedule:
Sydney - Goulburn
MSN:
340A-0411
YOM:
1978
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
Prior to departure the pilot had received a weather forecast which indicated that fog could be expected at the destination. Adequate fuel was carried in the aircraft tanks to allow for a considerable period of holding and/or a diversion to another aerodrome if required. After an apparently normal flight of 35 minutes the aircraft arrived in the Goulburn area and the pilot reported his intention to carry out a standard instrument approach. The manoeuvres associated with this procedure do not involve flight over the city of Goulburn, however witnesses observed the aircraft as it circled over the city several times at a relatively low height. It was then seen to roll and descend steeply before striking two houses. A fierce fire broke out which engulfed the aircraft and both residences. The three persons on board the aircraft and a person in one of the houses received fatal injuries. A detailed inspection of the wreckage revealed that the camshaft of the left engine had failed in flight and the pilot had apparently feathered the propeller. The engine was not operating at the time of impact. No other defect or malfunction was discovered which might have contributed to the development of the accident. It was determined that the particular camshaft had failed from fatigue cracking, resulting from defective manufacture. It was considered likely that when the aircraft arrived over Goulburn, shallow fog obscured all or part of the aerodrome. The lights of the city would have been clearly visible and the pilot probably decided to use the city, rather than the nearby radio navigation aid, as a convenient holding point while waiting for conditions at the aerodrome to improve. During a series of left hand orbits, and after advising his intention to conduct an instrument approach, the pilot experienced a complete failure of the left engine. In order to realise the available single-engine performance of the aircraft the pilot had to perform a series of checks and actions which would result in the applicable propeller being feathered; any unnecessary aerodynamic drag being reduced; and an appropriate airspeed being established. It was determined that although the propeller had probably been feathered, the landing gear, which had evidently been lowered previously, had not been raised to reduce drag. In addition, an analysis of radar returns from the aircraft, recorded at Canberra, indicated that the airspeed at which the aircraft was flying shortly before radar contact was lost, was less than the optimum figure. The final manoeuvre described by witnesses was consistent with that which follows a loss of control in twin engine aircraft when power is being supplied by only one engine and the speed is below the minimum required for full control. The reason the pilot did not raise the landing gear and maintain the required minimum control speed could not be established.
Probable cause:
Failure of the left engine in flight due to defective manufacture of camshaft. The following contributing factors were reported:
- Fatigue failure of camshaft,
- Complete loss of power from left engine,
- Aircraft not reconfigured for optimum single engine performance,
- Airspeed fell below minimum for effective control,
- Insufficient height for recovery.
Final Report:

Crash of a Cessna 340 in Ephrata

Date & Time: Nov 26, 1983 at 1411 LT
Type of aircraft:
Registration:
N98567
Survivors:
Yes
Site:
Schedule:
Seattle – Ephrata
MSN:
340-0036
YOM:
1972
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4948
Captain / Total hours on type:
1590.00
Aircraft flight hours:
1951
Circumstances:
The aircraft collided with a hilltop during a missed approach in IMC weather. The aircraft was on an IFR flight plan. The pilot stated visual contact was established at about 2,000 feet msl but ground features were masked in snow. When the pilot did not see the airport at the proper time he commenced a missed approach and the aircraft struck the ground. Investigation revealed that the obs (vor course indicator) was set on 222° instead of 202° for the published inbound heading. The resultant course passed directly over the accident site. The aircraft was not observed on radar because of its low alt. The pilot, sole on board, was seriously injured.
Probable cause:
Occurrence #1: in flight collision with terrain/water
Phase of operation: missed approach (IFR)
Findings
1. (c) procedures/directives - inaccurate - pilot in command
2. (c) ifr procedure - inaccurate - pilot in command
3. (c) equipment,other - not corrected - pilot in command
Final Report:

Crash of a Cessna 340A near Orangeville: 1 killed

Date & Time: Nov 20, 1983 at 1255 LT
Type of aircraft:
Registration:
N85JK
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Savannah – Fort Lauderdale
MSN:
340A-0700
YOM:
1979
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
The aircraft disappeared from radar coverage while in cruise flight at 10,000 feet msl near Orangeville, FL. The ATC transcript revealed that the pilot had been inquiring about the weather ahead of him and was cleared to descend to 6,000 feet in order to get below strong headwinds. One minute later he transmitted that he was going to stay at 10,000 feet because he did not have any choice (strong turbulence). His last transmission stated the weather was getting worse. The aircraft has not been located.
Probable cause:
Occurrence #1: missing aircraft
Phase of operation: unknown
Findings
1. Reason for occurrence undetermined
Final Report:

Crash of a Cessna 340 in Rock Springs: 3 killed

Date & Time: Apr 26, 1983 at 1103 LT
Type of aircraft:
Registration:
N5415M
Flight Type:
Survivors:
No
Schedule:
Rock Springs - Rock Springs
MSN:
340-0028
YOM:
1972
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
4281
Captain / Total hours on type:
31.00
Aircraft flight hours:
2022
Circumstances:
The aircrew of a Cessna 340, N5415M, were scheduled for an air taxi check ride with an inspector at Jackson, WY, later in the afternoon. They had planned to takeoff from Rock Springs, WY, practice at few instrument approaches at Rock Springs, then proceed to Jackson. After taking off, they made an NDB approach, made a missed approach, then began an ILS approach. A Beech Bonanza, N1825F, was on a flight from Scottsbluff, NE to Rock Springs. During arrival to Rock Springs, the Bonanza pilot was monitoring the position of a King Air that was ahead of him and also on an approach to the same airport. All three aircraft were using the same frequency and all three were providing reports of their respective positions. At approximately 1103 mdt, witnesses heard N5415M and N1825F collide, then saw the aircraft and pieces of wreckage falling. An investigation revealed the Cessna was inbound toward the outermarker (270° course) and the Bonanza was in level flight, heading approximately 219°. Both aircraft were operating VFR. All six occupants in both aircraft were killed.
Probable cause:
Occurrence #1: midair collision
Phase of operation: approach - iaf to faf/outer marker (IFR)
Findings
1. Radar traffic information service - not used - pilot in command
2. (c) visual lookout - inadequate - copilot/second pilot
3. (c) visual lookout - inadequate - pilot of other aircraft
----------
Occurrence #2: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Final Report:

Crash of a Cessna 340A in Aspen: 4 killed

Date & Time: Feb 15, 1983 at 0813 LT
Type of aircraft:
Registration:
N33340
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Aspen – South Bend
MSN:
340A-0529
YOM:
1978
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
3193
Aircraft flight hours:
724
Circumstances:
Prior to departure the flight was given an IFR clearance which began at Herls intersection (16 miles NNE) and to cross Herls at or above 16,000 feet msl. Departure airport field elevation is 7,793 feet. Flights are required to proceed VFR to the initial fix of the IFR clearance. After takeoff the aircraft was observed heading northeast toward the mountains. Aircraft departing Aspen usually fly a northern heading, then turn northeast after clearing the mountains. Witnesses stated that the weather was good in the valley north of the airport, but the mountain tops east of the airport were obscured by low clouds. The aircraft crashed 3 1/2 miles northeast of the airport at the 9,000 feet level of an 11,000 feet mountain. The last time the pilot had flown into Aspen was in 1980. All four occupants were killed.
Probable cause:
Occurrence #1: in flight encounter with weather
Phase of operation: climb - to cruise
Findings
1. (c) preflight planning/preparation - inadequate - pilot in command
2. (c) VFR procedures - not followed - pilot in command
3. (f) lack of familiarity with geographic area - pilot in command
4. (f) weather condition - clouds
5. (f) weather condition - obscuration
6. (c) VFR flight into IMC - continued - pilot in command
----------
Occurrence #2: in flight collision with terrain/water
Phase of operation: climb - to cruise
Findings
7. (f) terrain condition - high terrain
8. (f) terrain condition - mountainous/hilly
9. (f) terrain condition - rising
Final Report:

Crash of a Cessna 340A off Monterey

Date & Time: Jan 2, 1983 at 1720 LT
Type of aircraft:
Operator:
Registration:
N1947E
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Monterey – Oakland
MSN:
340A-0677
YOM:
1978
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
3200
Captain / Total hours on type:
41.00
Circumstances:
The aircraft began to lose power at about 400 feet agl after takeoff and the pilot elected to land along the shoreline in the ocean. The aircraft ditched about 100 yards off shore. All 4 occupants were able to exit thru the airstair door and received only minor injuries. The aircraft sank after about 5 minutes. It was not recovered from the 27 feet deep water. Two occupants swam ashore and two were rescued by the coast guard. The line attendant who serviced the aircraft mistook it for a king air. The pilot requested that all four tanks be topped off. The line attendant added 110 gallons of Jet A fuel.
Probable cause:
Occurrence #1: loss of engine power(partial) - mechanical failure/malfunction
Phase of operation: takeoff - initial climb
Findings
1. (c) fluid,fuel grade - improper
2. (c) maintenance,service of aircraft/equipment - improper - airport personnel
3. (c) aircraft service - inattentive - pilot in command
----------
Occurrence #2: ditching
Phase of operation: landing - flare/touchdown
Final Report:

Crash of a Cessna 340 in Benavides: 2 killed

Date & Time: Dec 16, 1982 at 1830 LT
Type of aircraft:
Registration:
N5906M
Flight Type:
Survivors:
No
Schedule:
Guadalajara - Benavides
MSN:
340-0064
YOM:
1972
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
579
Circumstances:
A deer hunter saw the aircraft on a final approach to an open field at dusk, with the gear and flaps down. He stated that when it was at about 100 feet agl, the nose pitched down and the plane struck the ground and burst into flames. The aircraft was loaded with an estimated 600 lbs of marijuana, most of which was consumed by fire. A high altitude navigational chart was found near the wreckage. The chart contained a line between two navigational points (one in mexico and one in the united states). The aircraft had been stolen. Both occupants were killed.
Probable cause:
Occurrence #1: loss of control - in flight
Phase of operation: approach - VFR pattern - final approach
Findings
1. Stolen aircraft/unauthorized use - performed - pilot in command
2. (f) light condition - dusk
3. (c) airspeed - not maintained - pilot in command
4. (c) stall - inadvertent - pilot in command
----------
Occurrence #2: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Final Report: