Crash of a Piper PA-31-350 Navajo Chieftain in Dayton: 1 killed

Date & Time: Dec 7, 2004 at 0140 LT
Operator:
Registration:
N54316
Flight Type:
Survivors:
No
Schedule:
Knoxville – Dayton
MSN:
31-7405436
YOM:
1974
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
3800
Captain / Total hours on type:
350.00
Aircraft flight hours:
9900
Circumstances:
The pilot was conducting a cargo flight in night instrument meteorological conditions, and was cleared for the ILS Runway 6L approach. The pilot reported that he was established on the localizer, and the control tower stated that the touchdown and mid-point "RVR" was 1,800 feet, and the roll-out "RVR" was 1,600 feet. The pilot also was instructed, and acknowledged, to make a right turn off the runway, after landing. There were no further communications from the airplane. The airplane's last radar target was observed at an altitude of 1,200 feet msl, and a ground speed of 130 knots. The airplane impacted trees, and came to rest inverted on airport property, on a bearing of 053 degrees, and a distance of 1/2 mile to the runway. Examination of the airplane did not reveal any pre-impact mechanical failures. A weather observation taken at the airport about the time of the accident included, winds from 140 degrees at 9 knots, 1/8 mile visibility, runway 06L visual range variable between 1,800, and 2,000 feet in fog, vertical visibility 100 feet, and a temperature and dew point 54 degrees F. The airport elevation was 1,009 feet msl. Review of the approach diagram for the ILS Runway 6L approach revealed a decision height of 1,198 feet msl, and an approach minimum of 1,800 feet runway visual range (RVR), or 1/2 mile visibility. The pilot had accumulated about 3,800 hours of total flight experience, which included about 350 hours in the same make and model as the accident airplane, and 250 total hours logged in instrument meteorological conditions.
Probable cause:
The pilot's failure to maintain adequate altitude\clearance while on approach, which resulted in an in-flight collision with trees. Factors in the accident were the fog and low ceiling conditions.
Final Report:

Crash of a Cessna 421B Golden Eagle II in Collegedale: 5 killed

Date & Time: Dec 2, 2004 at 1324 LT
Operator:
Registration:
N421SD
Flight Phase:
Survivors:
Yes
Schedule:
Collegedale – Knoxville
MSN:
421B-0386
YOM:
1973
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
4475
Captain / Total hours on type:
2000.00
Aircraft flight hours:
6808
Circumstances:
The airline transport pilot (ATP) stated the airplane was between 200 to 300 feet on initial takeoff climb when the right engine lost power and the airplane yawed to the right. The pilot lowered the nose of the airplane to gain airspeed, pulled the right power lever rearward and nothing happened. The pilot did not feather the right propeller and started moving switches in the vicinity of the boost pump switches. The ATP passenger stated, he did not think the left engine was producing full power. He scanned the instruments with his eyes looking at the manifold pressure gauges. "One needle was at zero and the other was at 25-inches. The manifold pressure should have been 39-inches of manifold pressure. The ATP passenger observed trees to their front and thought the pilot was trying to make a forced landing in an open field to their left. The ATP passenger realized the airplane was going to collide with the trees. Just before the airplane collided with the trees, the pilot feathered the right engine. The ATP passenger observed the right propeller going into the feather position, and the propeller came to a complete stop. Examination of the right engine revealed no anomalies. Examination of the left engine revealed the starter adapter gear teeth had failed due to overload.
Probable cause:
The pilot's improper identification of a partial loss of engine power on initial takeoff climb resulting in a collision with trees and the ground. A factor was a partial failure of the left engine starter adapter due to overload.
Final Report:

Crash of a Cessna 421B Golden Eagle II near Knoxville: 1 killed

Date & Time: Jun 9, 1988 at 1203 LT
Registration:
N700SC
Flight Phase:
Survivors:
No
Schedule:
Indianapolis - Jacksonville
MSN:
421B-0910
YOM:
1975
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
435
Captain / Total hours on type:
250.00
Aircraft flight hours:
3516
Circumstances:
During an IFR flight at FL170, the pilot reported airframe icing and requested a higher altitude. The pilot climbed to FL210 where he started a descent and reported loss of manifold pressure in the left engine. The pilot indicated that weather was in his flight path and descent was required to avoid icing. 90 seconds later the pilot transmitted '...losing it...'. Radar data indicated aircraft had an inflight breakup at approximately 17,000 feet msl. There was no evidence of mechanical or structural malfunction prior to the breakup. The aircraft did not have a complete current annual and de-ice equipment was inoperative. The pilot had no actual instrument experience and was not certified for multi engine IFR flight. The pilot had a medical history of anxiety attacks and had been taking prescription medication, Xanax and Tofranil, for approximately three years prior to the accident. The blood contained 1.2 mcg/ml of imipramine (Tofranil) and 2.6 mcg/ml desipramine (metabolite of Tofranil). Xanax (alprazolam) was not reported in blood toxicology. These drugs have been known to produce side effects that include poor judgement. The pilot, sole on board, was killed.
Probable cause:
Occurrence #1: in flight encounter with weather
Phase of operation: cruise - normal
Findings
1. (f) weather condition - thunderstorm
2. (f) weather condition - icing conditions
3. (f) flight control surfaces/attachments - ice
4. (f) weather condition - rain
5. (f) weather condition - turbulence
6. (c) in-flight planning/decision - poor - pilot in command
7. (c) impairment (drugs) - pilot in command
8. (c) flight into known adverse weather - intentional - pilot in command
9. (f) lack of total instrument time - pilot in command
10. (f) operation with known deficiencies in equipment - performed - pilot in command
----------
Occurrence #2: loss of engine power (partial) - nonmechanical
Phase of operation: cruise
Findings
11. 1 engine
12. Engine assembly - undetermined
----------
Occurrence #3: airframe/component/system failure/malfunction
Phase of operation: descent - uncontrolled
Findings
13. (f) operation with known deficiencies in equipment - performed - pilot in command
14. (c) design stress limits of aircraft - exceeded - pilot in command
----------
Occurrence #4: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Findings
15. Terrain condition - residential area
Final Report:

Crash of a Rockwell Aero Commander 500B in Salisbury: 5 killed

Date & Time: Mar 31, 1978 at 1116 LT
Operator:
Registration:
N313UT
Flight Phase:
Survivors:
No
Schedule:
Salisbury - Knoxville
MSN:
500-1183-93
YOM:
1962
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
5600
Captain / Total hours on type:
2412.00
Circumstances:
After takeoff from Salisbury-Wicomico County Regional Airport, while climbing, the pilot reported a double engine failure and attempted to return for an emergency landing. On final, while turning back to airport with the left throttle at idle, the airplane stalled and crashed half a mile short of runway. The aircraft was destroyed and all five occupants were killed.
Probable cause:
Double engine failure during initial climb and subsequent stall and crash due to improperly serviced aircraft by ground crew. The following contributing factors were reported:
- Fuel contamination - exclusive of water in fuel,
- Improper fuel grade,
- Operational supervisory personnel: inadequate supervision/training of ramp crews,
- Failure of both engines,
- Improper emergency procedures,
- Failed to follow approved procedures,
- High obstructions,
- Kerosene mixed with 100LL.
Final Report:

Crash of a Piper PA-31-310 Navajo near Chatsworth: 1 killed

Date & Time: Jul 5, 1974
Type of aircraft:
Registration:
N11HW
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Knoxville - Rome
MSN:
31-362
YOM:
1968
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
2000
Circumstances:
En route from Knosville to Rome, the pilot encountered poor weather conditions with thunderstorm activity, clouds and heavy rain falls. While flying in clouds at an altitude of 4,000 feet, the airplane struck tree tops and crashed on the slope of a mountain. The wreckage was found five days later and the pilot, sole on board, was killed.
Probable cause:
The pilot continued VFR flight into adverse weather conditions. The following contributing factors were reported:
- Inadequate preflight preparation,
- High obstructions,
- Rain,
- Thunderstorm activity with heavy rain falls,
- Mountain peaks shrouded in clouds,
- Aircraft hit the mountain at about 4,000 feet.
Final Report:

Crash of a Rockwell Aero Commander 680T off New Orleans: 3 killed

Date & Time: Dec 5, 1971 at 2323 LT
Operator:
Registration:
N78D
Survivors:
No
Schedule:
Knoxville - New Orleans
MSN:
680-1580-33
YOM:
1966
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
5812
Circumstances:
On a night approach to New Orleans-Lakefront Airport, the pilot encountered poor weather conditions with low ceiling. Unable to locate the runway, he abandoned the approach and initiated a go-around. Few minutes later, during a second attempt to land, he decided to descend below MDA when the twin engine airplane struck the water surface and crashed into Lake Pontchartrain few miles short of runway. All three occupants were killed but only two bodies were recovered.
Probable cause:
Improper IFR operation on part of the pilot. The following factors were reported:
- Low ceiling,
- Pilot fatigue,
- The pilot descended below minimums and below MDA on localizer approach,
- Crashed into lake on second attempt to land.
Final Report:

Crash of a Cessna 421A Golden Eagle I in Athens: 2 killed

Date & Time: Aug 20, 1971 at 0005 LT
Type of aircraft:
Registration:
N3198K
Survivors:
No
Schedule:
Knoxville - Athens
MSN:
421A-0008
YOM:
1967
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
2900
Captain / Total hours on type:
49.00
Circumstances:
On a night approach to Athens-McMinn County Airport, the pilot lost control of the aircraft that crashed in flames by the runway. The aircraft was destroyed and both occupants were killed.
Probable cause:
Uncontrolled collision with ground caused by improper operation of the flight controls. The pilot lost control of the aircraft during turning pull-up type maneuver after low pass over the runway.
Final Report:

Crash of a Vickers 745D Viscount near Parrottsville: 39 killed

Date & Time: Jul 9, 1964 at 1815 LT
Type of aircraft:
Operator:
Registration:
N7405
Flight Phase:
Survivors:
No
Site:
Schedule:
Philadelphia – Washington DC – Knoxville – Huntsville
MSN:
103
YOM:
1955
Flight number:
UA823
Crew on board:
4
Crew fatalities:
Pax on board:
35
Pax fatalities:
Other fatalities:
Total fatalities:
39
Captain / Total flying hours:
15665
Captain / Total hours on type:
1700.00
Copilot / Total flying hours:
7715
Copilot / Total hours on type:
2100
Aircraft flight hours:
23804
Circumstances:
A United Air Lines, Inc., Vickers Viscount 745D, N7405, Flight 823, crashed 2-1/4 rules northeast of Parrottsville Tennessee, at 1815 e.s.t., July 9, 1964. Thirty-four passengers and the four crew members died in the crash. One passenger died of injuries following a free fall from the aircraft before the crash. The aircraft was destroyed by fire and impact damage. Flight 823 was a regularly scheduled operation from Philadelphia, Pennsylvania, to Huntsville, Alabama, with en route stops at Washington, D. C., and Knoxville, Tennessee. The flight operated without any reported discrepancies or difficulties until approximately 1810 e.s.t., when it was observed flying at low altitude trailing smoke. The flight continued in a southwesterly direction and at a point approximately 1.6 nautical rules before the impact site, a passenger was seen falling from the aircraft, and a short time later a cabin window was seen falling. The aircraft was then observed going into a nose-high attitude, the left wing and the nose went down, and the aircraft dived into the ground, exploded, and burned.
Probable cause:
The Board determines that the probable cause of this accident was an uncontrollable in-flight fire of undetermined origin, in the fuselage, which resulted in a loss of control of the aircraft.
Final Report:

Crash of a Beechcraft E18S near Knoxville: 6 killed

Date & Time: Mar 21, 1964 at 1155 LT
Type of aircraft:
Operator:
Registration:
N110WB
Flight Phase:
Survivors:
No
Site:
MSN:
BA-263
YOM:
1957
Crew on board:
2
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
6
Captain / Total flying hours:
12450
Captain / Total hours on type:
800.00
Circumstances:
While cruising in a limited visibility due to snow showers, the twin engine aircraft struck the slope of a mountain and crashed in flames near Knoxville. All six occupants were killed. At the time of the accident, the ceiling was at 2,000 feet and the visibility was limited due to snow falls. Also, the mountain was shrouded in clouds.
Probable cause:
Inadequate flight preparation on part of the flying crew who continued under VFR mode into adverse weather conditions and flew at an altitude below obstructing terrain.
Final Report:

Crash of a Lockheed L-188A Electra in Knoxville

Date & Time: Aug 6, 1962 at 1731 LT
Type of aircraft:
Operator:
Registration:
N6102A
Survivors:
Yes
Schedule:
Dallas – Little Rock – Memphis – Knoxville – Washington DC – New York
MSN:
1019
YOM:
1958
Flight number:
AA414
Crew on board:
5
Crew fatalities:
Pax on board:
67
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
20634
Captain / Total hours on type:
878.00
Copilot / Total flying hours:
11000
Copilot / Total hours on type:
423
Aircraft flight hours:
6947
Circumstances:
On August 6, 1962, at 1731 e.s.t., Flight 414, an American Airlines, Inc., Lockhead Electra, N 6102A, crashed during a landing on runway 4L at McGhee-Tyson Airport, Knoxville, Tennessee. Sixty-seven passengers and five crew members were on board the aircraft. All escaped injury except one passenger who suffered a minor injury. The aircraft was substantially damaged. During the landing made by the captain in an area of thunderstorm activity and heavy rain showers, the aircraft skidded to the right off the runway. It struck a newly constructed taxiway the surface of which was approximately 17 inches above ground level, causing failure of the right main landing gear. The right wing became separated front the aircraft. The remainder of the aircraft continued to deviate to the right off the side of the runway for a short distance and came to rest 3,010 feet from the approach end of the runway on a heading of 200 degrees magnetic.
Probable cause:
The Board determines that the probable cause of this accident was the loss of directional control as a result of the improper technique employed in a crosswind landing in adverse weather conditions.
Final Report: