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Crash of a Beechcraft A90 King Air in Tampa: 1 killed

Date & Time: Jun 12, 2006 at 1235 LT
Type of aircraft:
Operator:
Registration:
N7043G
Flight Type:
Survivors:
Yes
Schedule:
Sarasota - Tampa
MSN:
LM-37
YOM:
1967
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
2120
Captain / Total hours on type:
457.00
Copilot / Total flying hours:
1208
Copilot / Total hours on type:
44
Aircraft flight hours:
15671
Circumstances:
The first officer reported that during cruise flight, both propeller secondary low pitch stop (SLPS) lights illuminated, indicating the SLPS system prevented both propellers from going below the low pitch hydraulic mechanical stop. The right occurred first, then the left approximately 1 minute later. Emergency procedures to correct the condition were ineffective. The right propeller feathered at some point during the flight, and the first officer reported that while operating single engine, they experienced a problem with the propeller governor. The flight proceeded direct to an airport with short runways approximately 3.2 nautical miles (nm) northwest of their present position, rather than to an air carrier airport located 8.5 nm away. The captain entered a close-in right base to runway 35 (2,688 feet long runway), while flying at 155 knots (51 knots above single engine reference speed). He turned onto final approach with the landing gear and flaps retracted, but overshot the runway. The airplane contacted a taxiway near the departure end of intended runway, and then collided with several obstacles before coming to rest at a house located past the departure end of runway 35. A post crash fire consumed the cockpit, cabin, and sections of both wings. Post accident examination of the airframe, engines, and propellers revealed no evidence of preimpact failure or malfunction. No determination was made as to the reason for the annunciation of both SLPS lights.
Probable cause:
The poor in-flight planning decision by the captain for his failure to establish the airplane on a stabilized approach for a forced landing, resulting in the airplane landing on a taxiway near the departure end of the runway. Contributing to the accident were the failure or malfunction of the primary hydraulic low pitch stop of both propellers for undetermined reasons, the excessive approach airspeed and the failure of the captain to align the airplane with the runway for the forced landing.
Final Report:

Crash of a Cessna 402B in Tampa: 3 killed

Date & Time: Oct 27, 1997 at 1510 LT
Type of aircraft:
Registration:
N69293
Flight Type:
Survivors:
Yes
Schedule:
Sarasota - Tampa
MSN:
402B-0415
YOM:
1973
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
3050
Aircraft flight hours:
3622
Circumstances:
The flight had departed runway 32, under IFR, from a local reliever airport 35 miles south of the destination, and was cleared to intercept the ILS approach for runway 36R. Instrument meteorological conditions existed with a low scattered cloud layer beneath the 900 foot broken clouds. Visibility was 8 miles. The flight never stabilized on the inbound course and glide slope. After acquiring the runway visually, about 3 miles from the airport, the airplane dove for the runway, subsequently touching down with the landing gear retracted. The left propeller incurred greater damage than the right propeller. The airplane began to go around, pitched up, then entered a steep left, descending turn that continued until impact with the ground.
Probable cause:
The pilot's failure to follow the landing checklist and extend the landing gear for landing, and his failure to maintain VMC during a go-around. Factors were: the pilot's diverted attention due to a non-stabilized instrument approach and his lack of recent instrument experience.
Final Report:

Crash of a Cessna 402C near Andytown

Date & Time: Aug 25, 1993 at 0855 LT
Type of aircraft:
Operator:
Registration:
N206RH
Flight Phase:
Survivors:
Yes
Schedule:
Sarasota - Fort Lauderdale
MSN:
402C-0206
YOM:
1979
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
3000
Captain / Total hours on type:
2400.00
Aircraft flight hours:
12918
Circumstances:
The pilot was deviating around weather during descent when he noted the fuel flow and manifold pressure on the left engine oscillating. Because the propeller was still turning he elected not to feather the left propeller. The airplane would not maintain altitude so he lowered the landing gear and ditched the airplane in a swamp. Examination of the left fuel tank revealed the fuel float valve actuators and float arms excessively worn. This condition would allow unmetered air into the fuel lines. Also noted was the condition of one of the left fuel valves that could jam open allowing the fuel pickup to unport and induce excessive air into the fuel lines.
Probable cause:
The failure of the pilot to feather the propeller when the engine lost power, and his failure to follow the emergency procedure checklist. Contributing to the accident was the inadequate design of the fuel tank float valves which allowed for excessive wear and subsequent induction of unmetered air into the fuel lines.
Final Report:

Crash of a Cessna 402C in Clewiston: 2 killed

Date & Time: Jan 23, 1992 at 2022 LT
Type of aircraft:
Operator:
Registration:
N2714A
Flight Phase:
Survivors:
No
Schedule:
Fort Lauderdale - Sarasota
MSN:
402C-0209
YOM:
1980
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
5500
Captain / Total hours on type:
2250.00
Aircraft flight hours:
13708
Circumstances:
The scheduled passenger flight departed without a flight plan and was last heard from while descending in attempt to remain in VFR conditions. Witnesses on the ground stated that there was extremely heavy rain and thunderstorms at the time of the accident. The wreckage was located the next day and evidence indicated that the airplane hit the ground in a 50° nose down attitude at a high rate of speed. Both occupants were killed.
Probable cause:
Pilot-in-command's improper inflight decision to attempt to descend and remain in VFR conditions in an area of thunderstorms and heavy rain. Contributing to the accident was the pilot-in-command's loss of control in flight.
Final Report:

Crash of a Canadair C-4GM North Star in Sarasota

Date & Time: Sep 17, 1971 at 1320 LT
Type of aircraft:
Operator:
Registration:
CF-UXB
Survivors:
Yes
Schedule:
Sarasota - Miami - Cockburn Harbor
MSN:
117
YOM:
1948
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
14500
Captain / Total hours on type:
8500.00
Circumstances:
On approach to Miami Airport, the crew did not get three greens and decided to return to Sarasota. On approach, engine number one and four were shut down and both other engines at an altitude of 500 feet. The airplane belly landed and slid for 1,800 feet before coming to rest. Both crew members were uninjured while the aircraft was damaged beyond repair.
Probable cause:
Failure of the landing gear to extend properly. The following factors were reported:
- Material failure,
- Improperly installed,
- Inadequate maintenance and inspection,
- Intentional wheels-up landing,
- Suspected mechanical discrepancy,
- Left gear uplatch upper link assembly failed,
- Lower gear by emergency system due to improper blot installed.
Final Report:

Crash of a Lockheed 18-50 LodeStar in St Petersburg

Date & Time: Jan 10, 1955 at 0938 LT
Type of aircraft:
Operator:
Registration:
N33369
Flight Phase:
Survivors:
Yes
Schedule:
Orlando – Lakeland – Tampa – Saint Petersburg – Sarasota – Fort Myers – West Palm Beach – Miami
MSN:
2414
YOM:
1943
Flight number:
NA001
Crew on board:
3
Crew fatalities:
Pax on board:
10
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
13427
Captain / Total hours on type:
410.00
Copilot / Total flying hours:
3639
Copilot / Total hours on type:
43
Aircraft flight hours:
20627
Circumstances:
After a normal run-up the copilot taxied the aircraft to the end of the 5,010-foot runway. The aircraft was then lined up with the runway slightly to the right of the centerline, the tail wheel was locked, and power was applied. As the aircraft progressed down the runway the tail came up and the copilot applied forward pressure to the control column. Shortly thereafter the airplane began to swerve to the left and when this was corrected it went too far to the right. A series of over-corrections followed which resulted in several swerves in both directions. As these maneuvers began the crew noted a five-inch drop in the manifold pressure of the left engine. At a speed of approximately 80 knots the aircraft again began turning to the left. The captain immediately took over the controls when he noticed a second drop of 25 inches in manifold pressure of the same engine. Both throttles were closed at once and he tried unsuccessfully to stop the turn. The turn developed into a skid and the main landing gear of the aircraft collapsed, rupturing the right wing fuel tank. The airplane cam to rest on the sodded area, off the runway, heading 180 degrees from its original takeoff position. Fire immediately occurred near the right engine nacelle. Under the supervision of the stewardess all passengers left the aircraft in a rapid, orderly manner through the main cabin door. The pilots left through the cockpit windows. The captain and copilot entered the cabin and made a recheck after all passengers were reported out and away from the aircraft. Local weather conditions at the time were: Ceiling 30,000 feet scattered, 600 feet scattered, visibility 12 miles, temperature 70, dewpoint 67, wind south 7. Atmospheric conditions were not conducive to carburetor ice.
Probable cause:
The Board determines that the probable cause of this accident was the copilot's loss of directional control during the takeoff run and the inability of the captain to regain control of the aircraft, the latter possibly due to failure of the pedal mechanism. The following findings were reported:
- Directional control was lost in the takeoff run which resulted in a violent groundloop off the runway,
- There is no evidence indicating that structural failure or malfunction of controls occurred. However, there exists the indeterminable possibility that during takeoff run there was a failure of the pedal assembly,
- Subsequent engine tests gave no evidence of other than normal operation of the left engine. The right engine operated normally throughout the attempted takeoff.
Final Report:

Crash of a Douglas TC-47B-30-DK near Zephyrhills: 13 killed

Date & Time: Jul 25, 1945 at 1030 LT
Operator:
Registration:
44-76612
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Sarasota – Lake Charles
MSN:
16196/32944
YOM:
1945
Crew on board:
13
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
13
Circumstances:
The crew was performing a training mission from Sarasota to Lake Charles, Louisiana, with a group of 5 Dakota's. While cruising northeast of Tampa, weather conditions worsened with a squall line, heavy rain falls and turbulence. In flight, the left wing broke off. Out of control, the aircraft dove into the ground, partially disintegrated in the air and eventually crashed in a mangrove located southwest of Zephyrhills. All 13 occupants were killed.
Crew:
F/O Kenneth J. Drauch,
1st Lt James T. Havens,
1st Lt William E. Irby,
Pfc William B. Kennedy,
Avc Vernon L. Larson,
Avc Leland M. Leeds,
Avc Milton Lerner,
Avc Thomas B. Lloyd,
Avc Auton C. Martin,
Avc Richard P. McClellan,
Avc Peter P. Melnik,
1st Lt Michael J. Rossi,
Pfc Gerald U. Scruggs.
Probable cause:
Loss of the left wing in flight due to severe turbulence.

Crash of a Martin B-26A-1 Marauder in Sarasota: 5 killed

Date & Time: May 31, 1943
Type of aircraft:
Operator:
Registration:
41-7477
Flight Phase:
Flight Type:
Survivors:
No
MSN:
7477
YOM:
1941
Crew on board:
5
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
5
Circumstances:
Crashed in unknown circumstances near Sarasota-Bradenton Airport. All five crew members were killed.

Crash of a Martin B-26A-1 Marauder in Sarasota

Date & Time: Oct 23, 1942
Type of aircraft:
Operator:
Registration:
41-7478
Flight Type:
Survivors:
Yes
MSN:
7478
YOM:
1941
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
For undetermined reasons, the aircraft overshot and crashed. There was no casualties but the aircraft was destroyed.