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Crash of a Beechcraft C90 King Air in Royal: 2 killed

Date & Time: Jan 3, 1995 at 1817 LT
Type of aircraft:
Registration:
N101GA
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Hot Springs - Pueblo
MSN:
LJ-11
YOM:
1965
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
4000
Captain / Total hours on type:
185.00
Aircraft flight hours:
7507
Circumstances:
The pilot obtained a weather briefing, filed an IFR flight plan, and took off at night on a flight from Hot Springs, Arkansas, to Pueblo, Colorado. About one minute later, he advised air traffic control that he needed to return to Hot Springs. He then contacted the airplane operator and said the heater was not working. The operator suggested that he return for repairs. The pilot was then heard to say, 'oh, shoot!' No further radio transmissions were received from the flight. The airplane cut a 400 foot swath through trees, and the wreckage path measured 940 feet. With exception of a heater problem, no pre impact mechanical failure was evident. Both occupants were killed.
Probable cause:
The pilot inadvertently allowed the airplane to descend and collide with trees, after he became diverted by an inoperative cabin heater. Darkness was a related factor.
Final Report:

Crash of a Swearingen SA227AC Metro III in Hot Springs: 3 killed

Date & Time: Aug 25, 1992 at 0515 LT
Type of aircraft:
Operator:
Registration:
N342AE
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Hot Springs - Hot Springs
MSN:
AC-545
YOM:
1983
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
2828
Captain / Total hours on type:
667.00
Aircraft flight hours:
19889
Circumstances:
The maintenance test flight was being flown following completion of airworthiness directive 87-02-02 requiring the mandatory replacement of all primary flight control cables. Following lift-off, witnesses observed the airplane start a rapid roll to the right until initial impact was made with the ground by the right wing tip. Examination of the wreckage revealed the a half turn in the routing of the replaced flight control cable was inadvertently omitted on both control columns which would result in the ailerons operating in reverse of the commanded input. The passenger was the quality control inspector who had inspected and signed off the maintenance performed. According to other company personnel, he had briefed the crew prior to the flight on the purpose of the test flight and the extent of the maintenance that the airplane had undergone. All three occupants were killed.
Probable cause:
Inadequate maintenance and inspection by the operator's maintenance personnel, and the failure of the pilot-in-command to assure proper travel direction of the airplane's primary flight controls after being made aware of the nature of the maintenance performed.
Final Report:

Ground fire of a Swearingen SA226TC Metro II in Hot Springs

Date & Time: Aug 27, 1983 at 2003 LT
Type of aircraft:
Registration:
N503SS
Flight Phase:
Survivors:
Yes
Schedule:
Dallas - Hot Springs - Little Rock
MSN:
TC-229E
YOM:
1977
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
5120
Captain / Total hours on type:
3000.00
Circumstances:
Turning onto the runway the copilot observed a flash behind his instrument panel. He then received an electrical shock to his right arm from the right console. A fire then erupted at the lower right hand corner of his instrument panel. The crew and pax evacuated the aircraft. The interior of the aircraft was consumed by fire as well as most of the upper half of the fuselage. Examination of the right side wire bundle revealed numerous indications of arcing between wires and from wires to ground. One wire was arced at a point in line with a plastic oxygen line. There was also an oily residue inside the wire bundle. A small section of the right brake pressure line exhibited signs of elect arcing. The hydraulic system pressure gage copper line also showed signs of arcing. The plastic oxygen lines from the the cockpit side of the forward pressure bulkhead to the cockpit outlets had been consumed by fire and the oxygen supply was depleated.
Probable cause:
Occurrence #1: fire
Phase of operation: taxi - to takeoff
Findings
1. (c) fuselage,instrument/electrical panel - shorted
2. (c) fuselage,instrument/electrical panel - arcing
3. (c) electrical system, electric wiring - arcing
4. (c) electrical system, electric wiring - contamination
5. (c) electrical system, electric wiring - fire
6. (c) oxygen system, crew - burst
7. (c) fuselage, instrument/electrical panel - fire
8. (c) fuselage - fire
Final Report:

Crash of a Rockwell Aero Commander 560 at Tinker AFB: 1 killed

Date & Time: Jan 18, 1979 at 0306 LT
Operator:
Registration:
N2684B
Flight Type:
Survivors:
Yes
Schedule:
Hot Springs - Tinker
MSN:
560-184
YOM:
1954
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
392
Circumstances:
While approaching Tinker AFB by night, the crew encountered low visibility due to foggy conditions and initiated a go-around maneuver. The crew attempted four other approaches that were abandoned due to poor visibility. During the fifth approach, the crew declared an emergency due to low fuel then the airplane stalled and crashed. A pilot was killed while the second occupant was seriously injured.
Probable cause:
Stall during a missed approach due to improper in-flight decisions. The following contributing factors were reported:
- Improper IFR operation,
- Failed to maintain flying speed,
- Low ceiling,
- Fog,
- Zero visibility,
- Low on fuel,
- Adverse/unfavorable weather,
- Flight path erratic during 5th attempted approach,
- Emergency declared due low fuel.
Final Report:

Crash of a Beechcraft C90 King Air in Pontiac: 2 killed

Date & Time: Sep 23, 1977 at 1409 LT
Type of aircraft:
Operator:
Registration:
N23796
Flight Phase:
Survivors:
No
Schedule:
Moline - Hot Springs
MSN:
LJ-737
YOM:
1977
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
3000
Captain / Total hours on type:
10.00
Circumstances:
While cruising at an altitude of 21,000 feet in marginal weather conditions, the airplane went out of control, spiraled to the ground and crashed in a field. The aircraft was totally destroyed and both occupants were killed.
Probable cause:
Airframe failure in flight and uncontrolled descent for undetermined reasons. The following findings were reported:
- Overload failure,
- Separation in flight,
- Rudder, horizontal stabilizers, elevators, outboard section of left wing separated in flight.
Final Report:

Crash of a Lockheed 18-56-23 LodeStar near Uniontown: 6 killed

Date & Time: Oct 6, 1957 at 1655 LT
Type of aircraft:
Operator:
Registration:
N80G
Flight Phase:
Survivors:
No
Site:
Schedule:
Cleveland – Hot Springs – Johnstown
MSN:
2351
YOM:
1943
Crew on board:
2
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
6
Captain / Total flying hours:
10000
Captain / Total hours on type:
3000.00
Copilot / Total flying hours:
3600
Copilot / Total hours on type:
200
Aircraft flight hours:
4608
Circumstances:
N80G departed Cleveland, Ohio, at approximately 1208LT for Ingalls Field Airport, Hot Springs, Virginia. The crew consisted of Captain Warren F. Noonan and Copilot Theodore O. Krauss. The purpose of the flight was to pick up passengers at Hot Springs, then fly to Johnstown, Pennsylvania, for an additional passenger, and return to Cleveland. The flight landed at Ingalls Field Airport sometime between 1300 and 1400 without incident. No records of aircraft arrival times are kept at this airport. N80G departed Hot Springs at approximately 1545LT with four passengers on board. The aircraft was observed to take off on the northeast runway and to climb to an altitude below the clouds. It was then observed to fly in a northwesterly direction for approximately four or five miles. About 1650, over an hour after takeoff and just before the aircraft struck the mountain, it was heard by a number of persons who lived within a radius of 10 miles of the accident scene; none saw it. The airplane hit trees and crashed in a wooded area, killing all six occupants.
Probable cause:
The Board determines that the probable cause of this accident was the action of the pilot in attempting VFR flight under instrument conditions over mountainous terrain. The following findings were reported:
- The crew was probably briefed by the U. S. Weather Bureau for the trip to Hot Springs and return, prior to departure from Cleveland,
- The VFR flight from Cleveland to Hot Springs was routine,
- The weather conditions north and east of Hot Springs at the time of the return required flight in accord with instrument flight rules; this was not done,
- No telephone or aircraft radio contacts wore made by the crew with any CAA communications station, either to file a flight plan or request weather information,
- The aircraft was heard but not seen flying a northeasterly heading in the overcast near the accident site,
- The aircraft was equipped for instrument flight.
Final Report: