Zone

Crash of a Cessna 340A in Orlando: 3 killed

Date & Time: May 1, 1987 at 1548 LT
Type of aircraft:
Registration:
N8716K
Flight Type:
Survivors:
No
Schedule:
Huntsville – Orlando
MSN:
340A-0629
YOM:
1978
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
2335
Captain / Total hours on type:
340.00
Circumstances:
The two aircraft, a Cessna 340A and a North American SNJ-4, collided in flight at approximately 3,000 feet msl over Orlando, FL in VMC with a visibility of 7 miles. Both aircraft were in contact with and being radar vectored by Orlando Approach Control. The Cessna 340 was in level flight and the SNJ was completing a right turn and still descending to 1,500 feet when the collision occurred. Both aircraft were operating under IFR flight rules with the Cessna 340 being vectored to runway 18R at Orlando-Intl (MCO) and the SNJ being directed to Orlando-Executive Airport (ORL). The accident occurred 7 miles northwest of ORL in the MCO Airport radar service outer area. During the vectoring, there was a lack of coordination between controllers during a transfer of control. The receiving controller failed to maintain radar target identification. There was also a lack of traffic advisories. The aircraft pilots were limited in their ability to see due to aircraft structure and relative positions to each other. After the collision, both aircraft crashed in uncontrolled descent. All four occupants in both aircraft were killed.
Probable cause:
Occurrence #1: midair collision
Phase of operation: cruise - normal
Findings
1. (c) crew/group coordination - not performed - atc personnel (dep/apch)
2. (f) radar, approach/departure - inadequate
3. (c) identification of aircraft on radar - inadequate - atc personnel (dep/apch)
4. (f) traffic advisory - not issued - atc personnel (dep/apch)
5. (f) visual lookout - inadequate - pilot in command
6. (f) visual lookout - inadequate - pilot of other aircraft
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Occurrence #2: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Final Report:

Crash of a Piper PA-60 Aerostar (Ted Smith 600) in Eva: 6 killed

Date & Time: Sep 13, 1985 at 1111 LT
Registration:
N680CC
Flight Type:
Survivors:
No
Schedule:
Lakeland - Huntsville
MSN:
60-0031
YOM:
1970
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
6
Captain / Total flying hours:
1993
Captain / Total hours on type:
97.00
Circumstances:
During an IFR arrival/descent, the pilot stated he 'had to feather one engine, I have an oil leak and I'm just trying to descend . . .' he then said he was descending thru 5,300 feet. As he continued the approach, he informed the controller he would be unable to go around since the hydraulic system was powered by the affected right engine. Subsequently, the pilot said he was at 1,500 feet and was having a hard time holding altitude. A witness heard and saw the aircraft in a level attitude at low altitude, then saw the aircraft dive toward the ground. It impacted in a steep descent just short of a long field and burned. The right propeller was feathered, but there was no evidence of oil starvation in either engine. The pilot's neighbor said he (the pilot) was aware of a hydraulic leak, but he was awaiting the annual inspection (due in September) to repair it. An exam revealed the flaps were partially extended, the landing gear control was in the 'up' position, and the gear was down. The flight manual stated that with a hydraulic failure downstream of the accumulator, the flap handle should be in 'neutral' to prevent gear and flap extension. The flap control could not be found. All six occupants were killed.
Probable cause:
Occurrence #1: airframe/component/system failure/malfunction
Phase of operation: descent - normal
Findings
1. (c) reason for occurrence undetermined
2. (f) fluid - leak
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Occurrence #2: loss of engine power (partial) - nonmechanical
Phase of operation: descent - normal
Findings
3. Miscellaneous - intentional
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Occurrence #3: forced landing
Phase of operation: descent - emergency
Findings
4. (f) maintenance - inadequate - company/operator management
5. (f) operation with known deficiencies in equipment - performed - pilot in command
6. (c) emergency procedure - improper - pilot in command
7. Hydraulic system - pressure too low
8. (f) gear extension - inadvertent
9. (f) lowering of flaps - inadvertent
10. Level off - not possible
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Occurrence #4: loss of control - in flight
Phase of operation: descent - emergency
Findings
11. (c) airspeed (vmc) - not maintained - pilot in command
----------
Occurrence #5: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Final Report:

Crash of a Buhl CA-6 Standard AirSedan in Huntsville

Date & Time: Sep 11, 1933
Registration:
CF-ACX
Survivors:
Yes
MSN:
44
YOM:
1929
Country:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Upon landing at Huntsville Airport, the engine exploded. The airplane went out of control, veered off runway and came to rest, bursting into flames. The airplane was destroyed by fire and there were no casualties.
Probable cause:
Engine explosion upon landing.