Crash of a Cessna 340 in Falmouth: 1 killed

Date & Time: Aug 7, 1992 at 2150 LT
Type of aircraft:
Registration:
N194S
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Macon – Grand Rapids
MSN:
340-0167
YOM:
1972
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
142
Captain / Total hours on type:
25.00
Aircraft flight hours:
2762
Circumstances:
The airplane was cruising at 16,500 feet at night when radar and radio contact were lost. The pilot made no distress radio calls. Recorded radar data showed the airplane in a left descending turn. Other airplanes were deviating around weather in the area. Ground witnesses heard the airplane prior to impact and reported rain. The pilot started flying lessons in march and received his multi-engine rating in june. He had a total of 142 hours flight time, with 25 hours in this make and model airplane and 9 hours total night time. The pilot was not instrument rated.
Probable cause:
The improper decision by the non-instrument-rated pilot to attempt VFR flight into instrument meteorological conditions resulting in a loss of airplane control and subsequent inadvertent spiral and collision with the ground. Factors related to the accident were: the pilot's lack of total flight experience; the pilot's lack of flight time in this make and model airplane; and his overconfidence in his own ability.
Final Report:

Crash of a GAF Nomad N.22B in Richardsville

Date & Time: May 4, 1991 at 1715 LT
Type of aircraft:
Operator:
Registration:
N5590M
Flight Phase:
Survivors:
Yes
Schedule:
Bowling Green - Racine
MSN:
083
YOM:
1978
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
6400
Captain / Total hours on type:
40.00
Aircraft flight hours:
770
Circumstances:
The pilot had just leveled at 4,000 feet when the right engine lost power. He immediately turned back toward his departure field but could not maintain altitude with the remaining engine. He then elected to make a gear up landing in an open field. On touchdown, the aircraft sustained substantial damage as it came to a stop in the grassy field. The pilot and passenger exited through the forward doors without further incident. Both occupants escaped uninjured.
Probable cause:
The loss of engine power brought on by a failure of the no.2 main engine bearing. Contributing to the accident was the lack of sufficient power on the remaining engine to maintain level flight.
Final Report:

Crash of a Swearingen SA227AC Metro III in Cincinnati

Date & Time: Nov 8, 1990 at 2223 LT
Type of aircraft:
Operator:
Registration:
N445AC
Flight Type:
Survivors:
Yes
Schedule:
Cincinnati - Cincinnati
MSN:
AC-445
YOM:
1981
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
3918
Captain / Total hours on type:
1019.00
Aircraft flight hours:
15616
Circumstances:
The pilot, a company check airman, and an FAA inspector were on board the aircraft for a checkride which was intended to reassess the pilot's competency. A maintenance test (aileron rigging) was to be performed in conjunction with the check ride. The first maneuver to be performed was a no-flap landing. All three pilots stated that the pilot had difficulty managing the aircraft while in the traffic pattern; airspeeds were too slow, and the pilot was constantly manipulating power. The pilot never called for the before landing checklist, and the aircraft touched down on the runway with the landing gear up. The check pilot stated that the landing gear warning horn came on briefly, but the pilot added power and silenced the horn. The FAA inspector was seated in a passenger seat for takeoff and landing, and was not aware that the landing gear was not extended.
Probable cause:
The pilot-in-command's failure to extend the landing gear prior to touchdown. Checkride-induced pressure was a contributing factor, and inadequate supervision by the check pilot was a factor.
Final Report:

Crash of a Beechcraft 100 King Air in Mayfield: 6 killed

Date & Time: Sep 15, 1989 at 2110 LT
Type of aircraft:
Operator:
Registration:
N887PE
Survivors:
No
Schedule:
Orlando - Mayfield
MSN:
B-49
YOM:
1970
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
6
Captain / Total flying hours:
8000
Captain / Total hours on type:
400.00
Aircraft flight hours:
9386
Circumstances:
During arrival, the flight was issued the current Paducah altimeter setting. The pilot requested vectors for an approach to runway 18, but the ARTCC controller (ctlr) could not accommodate the request. The pilot was cleared for a VOR/DME-a approach. MDA for the approach was 1,080 feet msl (600 feet agl). At 2108 cdt, the flight changed to the FBO frequency. FBO personnel observed the aircraft fly over the airport and advised that it was too low. One of the pilots replied that they would be 'staying under the clouds.' The pilots had planned to land on runway 36, but reported they lost sight of the runway and would change to runway 18. Subsequently, the aircraft collided with a tree about 1 mile north-northeast of the airport, while on a westerly heading (approximately position of base leg for a VFR pattern). The aircraft came to rest about 700 feet west of the tree and was destroyed by impact and fire. No preimpact part failure/malfunction of the aircraft was found. Approximately 30 miles west at Paducah, the weather was in part: 200 feet scattered, 900 feet overcast visibility 3 miles with rain and fog, wind from 360° at 7 knots. The airport manager estimated there was a 200 feet ceiling at the airport. All six occupants were killed.
Probable cause:
Failure of the pilot to follow ifr procedures and maintain the minimum descent altitude (MDA). Factors related to the accident were: darkness, the adverse weather conditions, and the tree.
Final Report:

Crash of a Beechcraft E18S in Cincinnati: 1 killed

Date & Time: Mar 9, 1989 at 0617 LT
Type of aircraft:
Operator:
Registration:
N3281T
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Cincinnati – Detroit
MSN:
BA-611
YOM:
1962
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
10560
Captain / Total hours on type:
15.00
Aircraft flight hours:
13262
Circumstances:
N3281T was attempting an instrument departure when it crashed left of the extended centerline of runway 18. The flight was observed climbing through 200 feet prior to descending to the ground. Prior to taxiing to takeoff the pilot failed to deice the airframe. Airplanes on the parking ramp around N3281T deiced prior to takeoff. Weather reports indicated that temp/dew point were 26 and 23° respectively. The surface observation also reported fog as a restriction to visibility. According to the airplane's handbook that tests prove that a coat of frost on a wing can destroy its lift. The pilot, sole on board, was killed.
Probable cause:
Pilot attempted a takeoff with coating of frost on the airframe which resulted in a loss of lift during climbout.
Final Report:

Crash of a Beechcraft B90 King Air in Paducah

Date & Time: Jan 7, 1989 at 1935 LT
Type of aircraft:
Registration:
N784K
Flight Type:
Survivors:
Yes
Schedule:
Shenandoah - Decatur
MSN:
LJ-427
YOM:
1969
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
1061
Captain / Total hours on type:
115.00
Aircraft flight hours:
5293
Circumstances:
During a return flight at night to Decatur, AL, the pilot noted his weather radar was inoperative. He visually avoided thunderstorms (tstms), which had been forecasted. While avoiding tstms, he noted a reduction in engine power, a slight yaw, indications of fuel flow irregularity and that the left and right boost pumps were inoperative. These occurred at about the time, he saw a white arc which he said had jumped from the prop, spinner or nacelle area to the aircraft's nose. Due to the weather, he elected to divert to Paducah. After the airport was in sight, he needed to lose altitude before landing and was cleared to make a 360° turn. While turning, he lost sight of the airport, then rolled out on the wrong heading and started flying toward a strobe light at an industrial complex. When he realized his error and saw the airport, he turned toward the runway; but as he was maneuvering, the aircraft lost altitude, hit trees and crashed. An examination of the engines and fuel pumps revealed no indication of a preimpact failure. No physical evidence of a lightning strike was found, but the nose and engines were badly damaged from impact.
Probable cause:
Pilot failed to maintain proper altitude while maneuvering to land. Probable contributing factors were inoperative weather radar, thunderstorms, lightning, an undetermined electrical problem, dark night, the pilot's improperly planned approach and visual perception, and the trees.
Occurrence #1: in flight encounter with weather
Phase of operation: cruise
Findings
1. (f) flight/nav instruments, weather radar system - inoperative
2. (f) weather condition - thunderstorm
3. (f) weather condition - lightning
4. (f) electrical system - undetermined
5. Fuel system, electric boost pump - inoperative
----------
Occurrence #2: in flight collision with object
Phase of operation: approach
Findings
6. (f) light condition - dark night
7. (f) planned approach - improper - pilot in command
8. (f) visual/aural perception - pilot in command
9. Maneuver - initiated
10. (f) object - tree(s)
11. (c) proper altitude - not maintained - pilot in command
----------
Occurrence #3: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Final Report:

Crash of a Beechcraft E18S in Cynthiana

Date & Time: Apr 29, 1988 at 1230 LT
Type of aircraft:
Registration:
N300W
Flight Type:
Survivors:
Yes
Schedule:
Rochester – Louisville – Huntsville
MSN:
BA-92
YOM:
1955
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
1800
Captain / Total hours on type:
900.00
Aircraft flight hours:
9048
Circumstances:
The pilot was repositioning the airplane from an on-demand air taxi freight flight. He was en route from Rochester, NY to Huntsville, AL with a planned refuel stop at Louisville, KY. Near Falmouth, KY he changed his destination to Lexington 'due to a developing engine problem'. He saw the airport at Cynthiana and elected to land there. While on downwind, he noted the left engine cowling turning black and on base noted flames from the left engine. He reptd shutting the engine down and feathering the propeller but did not activate the fire extinguisher. During the landing roll, the airplane departed the runway to the right, and collided with the airport wind 't', a pole and a 't' hangar. Post accident investigation revealed that the left prop was not feathered and the fuel was not shut off. The left brake was ineffective due to fire damage. The evidence indicated that the fire began in the vicinity of the left engine accessory section. The specific fuel source of the fire was not identified.
Probable cause:
Occurrence #1: fire
Phase of operation: approach - vfr pattern - downwind
Findings
1. 1 engine
2. (c) fluid, fuel - leak
3. (f) fire extinguishing equipment - not used - pilot in command
4. (f) procedures/directives - not followed - pilot in command
----------
Occurrence #2: on ground/water collision with object
Phase of operation: landing - roll
Findings
5. (f) landing gear, normal brake system - burned
6. Object - airport facility
7. Object - pole
8. Object - building (nonresidential)
Final Report:

Crash of a Hawker-Siddeley HS.125-400A in Lexington: 2 killed

Date & Time: Dec 5, 1987 at 1450 LT
Type of aircraft:
Registration:
N400PH
Survivors:
Yes
Schedule:
Dallas - New York
MSN:
25180
YOM:
1968
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
20565
Aircraft flight hours:
5710
Circumstances:
While en route at FL370, the pilots declared an emergency, reported a fire in the right engine and requested vectors to the nearest suitable airport. They were vectored toward the Lexington-Blue Grass Airport and circled to descend. Shortly after declaring an emergency, the pilots reported they secured the right engine and extinguished the fire light. As the aircraft was on final approach to land, the local controller (using binoculars) confirmed that both the gear and flaps were extended. However, as the aircraft continued onto a short final approach, an increase in its pitch attitude was noted. It then dropped below the level of the runway threshold and impacted in a pasture short of the runway. After initial impact, the aircraft went thru a stone fence, hit 2 utility poles, crossed a highway, came to rest at the perimeter fence and burned. An auto was damaged by debris; 2 occupants received minor injuries. An investigation revealed the aircraft impacted with the gear extended, but the flaps and flap handle were found in the up position. An examination of the right engine revealed its outer exhaust cone was cracked in the vicinity of a fire detection loop. No other preexisting mechanical problems were evident. Both pilots were killed and both passengers were seriously injured.
Probable cause:
Occurrence #1: airframe/component/system failure/malfunction
Phase of operation: cruise - normal
Findings
1. (f) exhaust system, exhaust cone/tailpipe (jet engine) - cracked
2. (f) exhaust system, exhaust cone/tailpipe (jet engine) - leak
3. (f) engine compartment - overtemperature
----------
Occurrence #2: loss of engine power
Phase of operation: cruise
Findings
4. 1 engine
5. Emergency procedure - intentional
----------
Occurrence #3: in flight collision with terrain/water
Phase of operation: approach - vfr pattern - final approach
Findings
6. Precautionary landing - initiated
7. (c) raising of flaps - inadvertent
8. (c) stall/mush - inadvertent - pilot in command
Final Report:

Ground accident of a Beechcraft 200C Super King Air in Madisonville

Date & Time: Jun 24, 1987 at 1215 LT
Registration:
N617MS
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Madisonville - Marion
MSN:
BL-35
YOM:
1981
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
11875
Captain / Total hours on type:
2310.00
Aircraft flight hours:
2940
Circumstances:
The aircraft struck a 2-feet high Avgas pump while the pilot was taxiing around another aircraft that was parked. The nose gear collapsed and a small fire resulted. The pilot and passenger evacuated the aircraft. Line personnel were unable to extinguish the fire with hand-held extinguishers. The aircraft was subsequently engulfed by the fire and was destroyed. A large dry chemical fire extinguisher was located next to the pump at the time, but line personnel were unable to get to it due to the fire. The black top around the pump had recently been resurfaced and no safety markings, lights or barricades were in place around the pump (except for the large fire extinguisher). The pump was originally located next to the ramp edge, but subsequent expansion of the ramp left the pump surrounded by pavement.
Probable cause:
Occurrence #1: on ground/water collision with object
Phase of operation: taxi - to takeoff
Findings
1. (f) airport facilities, obstruction marking - inadequate
2. (f) other airport/runway maintenance - inadequate - airport personnel
3. (f) object - airport facility
4. (c) visual lookout - inadequate - pilot in command
----------
Occurrence #2: nose gear collapsed
Phase of operation: taxi - to takeoff
Findings
5. Landing gear, nose gear - overload
----------
Occurrence #3: fire
Phase of operation: standing
Final Report:

Crash of a Lockheed C-130A Hercules at Fort Campbell AFB: 3 killed

Date & Time: Sep 9, 1986
Type of aircraft:
Operator:
Registration:
56-0468
Flight Type:
Survivors:
Yes
MSN:
3076
YOM:
1957
Crew on board:
5
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
After landing at Fort Campbell AFB, the crew encountered technical problems and the aircraft was unable to stop within the remaining distance. It overran and came to rest few dozen yards further. Two crew members were seriously injured while three others were killed.
Probable cause:
Loss of control after touchdown due to the failure of a throttle cable.