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Crash of a Piper PA-46-350P Malibu Mirage in Saint Augustine

Date & Time: Mar 23, 2023
Registration:
N280KC
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Saint Augustine – Jacksonville
MSN:
46-36219
YOM:
1999
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Shortly after takeoff from Saint Augustine Airport, while in initial climb, the airplane contacted trees and crashed in a wooded area, bursting into flames. Both occupants and their dog escaped with minor injuries. The airplane was destroyed by a post crash fire.

Crash of a Learjet 25 in Saint Augustine

Date & Time: Jul 21, 2007 at 1410 LT
Type of aircraft:
Operator:
Registration:
N70SK
Flight Type:
Survivors:
Yes
Schedule:
Gainesville - Saint Augustine
MSN:
25-49
YOM:
1970
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4620
Captain / Total hours on type:
250.00
Copilot / Total flying hours:
2453
Copilot / Total hours on type:
368
Aircraft flight hours:
15812
Circumstances:
About 5 miles from the destination airport, the flight was cleared by air traffic control to descend from its cruise altitude of 5,000 feet for a visual approach. As the first officer reduced engine power, both engines "quit." The captain attempted to restart both engines without success. He then took control of the airplane, and instructed the first officer to contact air traffic control and advise them that the airplane had experienced a "dual flameout." The captain configured the airplane by extending the landing gear and flaps and subsequently landed the airplane on the runway "hard," resulting in substantial damage to the airframe. Both engines were test run following the accident at full and idle power with no anomalies noted. Examination of the airplane revealed that it was equipped with an aftermarket throttle
quadrant, and that the power lever locking mechanism pins as well as the throttle quadrant idle stops for both engines were worn. The power lever locking mechanism internal springs for both the left and right power levers were worn and broken. Additionally, it was possible to repeatedly move the left engine's power lever directly into cutoff without first releasing its power lever locking mechanism; however, the right engine's power lever could not be moved to the cut off position without first releasing its associated locking mechanism. The right throttle thrust reverser solenoid installed on the airplane was found to be non-functional, but it is not believed that this component contributed to the accident. No explicit inspection or repair instructions were available for the throttle quadrant assembly. Other than the throttle quadrant issues, no other issues were identified with either the engines or airframe that could be contributed to both engines losing power simultaneously.
Probable cause:
A loss of power on both engines for an undetermined reason.
Final Report:

Crash of a Piper PA-31-310 Navajo in Clearwater: 2 killed

Date & Time: Aug 21, 2003 at 1648 LT
Type of aircraft:
Registration:
N93DC
Flight Type:
Survivors:
Yes
Site:
Schedule:
Saint Augustine - Clearwater
MSN:
31-7712017
YOM:
1977
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
760
Copilot / Total flying hours:
600
Aircraft flight hours:
6019
Circumstances:
The airplane experienced an in-flight loss of control and crashed into a residential area. The flight departed VFR and when near the destination airport flew between areas with VIP Level 5 reflectivity. There was no record of a preflight weather briefing. The flight continued towards the destination airport and encountered lesser intensity reflectivity. An individual at the destination airport reported hearing an occupant of the airplane ask, "...for an advisory for the field", and "...what the weather was like." The individual at the airport advised that the winds appeared to be in favor for runway 16, which was left hand traffic, the runway was wet, and the rain seemed to be letting up. There were no further communications from the accident aircraft. A pilot-rated witness located north of the destination airport, and nearly due west of the accident site reported seeing the airplane on what he thought was final approach to runway 16, but the airplane was "very low." The witness reported the airplane made a, "sudden, sharp turn to the left [flying eastbound]." He then lost sight of the airplane and proceeded to the accident site. Another pilot-rated witness who was located in a vehicle approximately 1/4 mile west-northwest of the accident site reported observing an airplane flying from the northwest. The airplane banked to the left flying eastbound at a, "...very slow airspeed and banking and yawing left and right." While flying eastbound it appeared to him that whomever was flying the airplane was executing a go-around as evidenced by the landing gear retracting, followed by the flaps. The airplane then appeared to climb which appeared very unstable, again yawing left and right. The airplane then banked to the right, stalled, and entered a spin impacting the ground. Still another witness who was located approximately 1/10th of a nautical mile east-southeast from the accident site reported he came out of his house after the rain ended and was facing west. He saw the accident airplane from the northwest and thought it had descended lower than normal. The airplane was flying above the tops of nearby trees and while flying in a southeasterly direction, pitched up, "darn near got 90 degrees", rolled to the left, and descended straight down. He reported that he did not hear the engines, and thought he should have been able to hear them if the pilot had "revved them up." He estimated his view of the flight lasted approximately 10-15 seconds, and couldn't tell if the landing gear was extended. He did not see any smoke trailing the airplane, and after the impact he ran into his house, called 911, got into his car, and drove to the scene. He heard an explosion, and saw flames. He got to the airplane and helped rescue a passenger who was beating on the aircraft's door. The airplane descended nearly vertical in a residential area and damaged trees approximately 30 feet above ground level. A post crash fire consumed the cockpit, cabin, portions of both wings, and portions of both engines. Examination of the flight controls, both engines, propellers, and propeller governors revealed no evidence of preimpact mechanical failure or malfunction. Accessories of both engines including the magnetos were destroyed by the post crash fire. Additionally, both servo fuel injectors were heat damaged which precluded bench testing. During disassembly of the right servo fuel injector, the hub stud was found separated from the hub at the fuel diaphragm. No determination was made whether this occurred during disassembly or occurred preimpact. No determination could be made as to who was operating the controls at the time of the accident.
Probable cause:
The failure of the flightcrew to maintain airspeed (Vs) resulting in an inadvertent stall, uncontrolled descent, and in-flight collision with the ground.
Final Report:

Crash of a Beechcraft C90 King Air in Saint Augustine: 2 killed

Date & Time: Apr 9, 1992 at 0710 LT
Type of aircraft:
Registration:
N105FL
Flight Type:
Survivors:
No
Schedule:
Tallahassee - Saint Augustine
MSN:
LJ-1215
YOM:
1989
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
7350
Captain / Total hours on type:
1600.00
Aircraft flight hours:
1338
Circumstances:
The airplane disappeared from radar about 1-1/2 mile short of the airport during a VOR runway 13 approach. Radar data shows that the altitudes, descent rates, and ground speeds were consistent with the approach profile. The last radar position of the airplane was at 100 feet on the runway extended centerline. The debris path was aligned on a 130° magnetic heading. Witnesses stated that the visibility was near zero in fog. Both occupants were killed.
Probable cause:
The pilot's failure to properly adhere to the published instrument approach procedure which resulted in descent below the minimum descent altitude. Factors which contributed to the accident were the low ceiling and fog.
Final Report:

Crash of an IAI-1124A Westwind I in Oxford

Date & Time: May 1, 1991 at 0920 LT
Type of aircraft:
Registration:
N445BL
Survivors:
Yes
Schedule:
Saint Augustine – Oxford
MSN:
382
YOM:
1982
Crew on board:
2
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
10990
Captain / Total hours on type:
2290.00
Circumstances:
The aircraft completed an instrument approach and landed hard on the runway surface first with the left gear then the right gear. The tires burst and the lower fuselage came into contact with the runway surface. After the nose gear touched down, the right main landing gear collapsed and the pilot lost control of the aircraft. It veered to the left and departed the runway, coming to rest approximately 150 to 200 yards from the point of departure. Initial touch down occurred about 12 feet from the threshold, ten feet left of centerline.
Probable cause:
The failure of the pilot to maintain the proper landing descent rate and the resultant right main landing gear assembly collapse.
Final Report:

Crash of a Beechcraft H18 in Saint Augustine: 2 killed

Date & Time: Dec 31, 1974 at 1025 LT
Type of aircraft:
Operator:
Registration:
N500MM
Survivors:
No
Schedule:
Saint Petersburg – Cocoa Beach – Saint Augustine
MSN:
BA-715
YOM:
1964
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
9293
Captain / Total hours on type:
100.00
Circumstances:
On approach to Saint Augustine Airport, the passenger reported to ATC that pilot had no control over aircraft after controls frozen. The airplane went out of control and crashed in flames, killing both occupants. The aircraft was totally destroyed by a post crash fire, precluding determination of cause.
Probable cause:
Loss of control on approach for undetermined reason. The following findings were reported:
- Fog,
- The passenger reported pilot had not control over aircraft,
- Controls frozen,
- Extensive fire damage precluded determination of cause.
Final Report:

Crash of a Consolidated B-24E-25-DT Liberator near Saint Augustine: 10 killed

Date & Time: Mar 5, 1944
Operator:
Registration:
41-28530
Flight Phase:
Flight Type:
Survivors:
No
MSN:
122/15645
Crew on board:
10
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
10
Circumstances:
The crew was engaged in a gunnery training mission. En route, while cruising, the engine number two caught fire. Shortly later, the aircraft exploded and crashed in a field located near Saint Augustine, some 30 miles southeast of Jacksonville. All ten occupants were killed.
Probable cause:
Engine fire and explosion in flight caused by a mechanical failure.