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Crash of a Cessna 340A in Temple: 3 killed

Date & Time: Jan 17, 2002 at 1522 LT
Type of aircraft:
Registration:
N339S
Survivors:
Yes
Site:
Schedule:
League City – Killeen
MSN:
340A-0712
YOM:
1979
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
3464
Captain / Total hours on type:
10.00
Aircraft flight hours:
5877
Circumstances:
While on an IFR clearance, the pilot reported to approach control that he was unable to maintain 4,000 feet msl, and did not give a reason. Shortly thereafter, the pilot contacted approach control and stated that he had "fuel starvation" in the right engine and the left engine had just quit. Radar data depicted the aircraft at an altitude of 3,400 feet. The controller asked the pilot if they were completely without power, and the pilot responded, "yes, we're now gliding." The controller gave the pilot instructions to the nearest airport, which was approximately 4.5 nautical miles away. After passing 2,100 feet, the pilot informed the controller that he would be landing short. During the forced landing, the airplane struck the top of a tree, crossed over a house, struck another tree, struck a telephone wire which crossed diagonally over a street, and then cleared a set of wires which paralleled the street. The airplane then impacted a private residence within a residential area, and a fire erupted damaging the airplane and the private residence. Ten gallons of fuel were drained from the left locker tank, which supplements the left main fuel tank. Examination of the airframe and engines did not disclose any structural or mechanical anomalies that would have prevented normal operation. Examination of the propeller revealed that neither propeller had been
feathered.
Probable cause:
The pilot's mismanagement of fuel, which resulted in a total loss of engine power due to fuel starvation. Contributing factors were the pilot's failure to follow the checklist to feather the propellers in order to reduce drag.
Final Report:

Crash of a Saab 340B in Killeen

Date & Time: Mar 21, 2000 at 1914 LT
Type of aircraft:
Operator:
Registration:
N353SB
Survivors:
Yes
Schedule:
Dallas - Killeen
MSN:
353
YOM:
1993
Flight number:
AA3789
Location:
Crew on board:
3
Crew fatalities:
Pax on board:
33
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
12518
Captain / Total hours on type:
9251.00
Copilot / Total flying hours:
2105
Copilot / Total hours on type:
1040
Aircraft flight hours:
11976
Circumstances:
The captain was the flying pilot for the night landing on runway 01 in instrument meteorological conditions (IMC), with a right cross wind from 110 degrees at 14 gusting 18 knots, drizzle, and a wet runway. Prior to starting the approach, the flightcrew determined that the landing approach speed (Vref) and the approach speed (Vapp) were 122 and 128 knots, respectively. DFDR data showed the airplane flying on autopilot as it passed the middle marker at 200 feet AGL at 130 knots on the ILS approach. Approximately 3 seconds after the first officer called "runway in sight twelve o'clock," the captain disconnected the autopilot, while at a radio altitude of 132 feet and on a heading of approximately 18 degrees. Within approximately 11 seconds after the autopilot disconnect, the glideslope and localizer deviation increased. The first officer called "runway over there." Approximately 5 seconds before touchdown, the airplane rolled right, then left, then right. DFDR data-based performance calculations showed the airplane crossed the threshold at an altitude of 35 feet and 130 knots. The airplane touched down 2,802 feet from the approach end of the 5,495-foot runway (844- foot displaced threshold) at 125 knots on a heading of 10 degrees. The airplane overran the runway and struck a ditch 175 feet beyond the departure end of the runway. Landing roll calculations showed a ground roll of 2,693 feet after touchdown, consisting of 1,016 feet ground roll before braking was initiated and 1,677 feet ground roll after braking was initiated until the airplane exited the pavement. According to Saab, for a wet runway, the aircraft would have needed 1,989 feet from the time of braking initiation to come to a complete stop. The American Eagle Airlines, Inc., FAA approved aircraft operating manual (AOM), states in part: Stabilized approaches are essential when landing on contaminated runways. Landing under adverse weather conditions, the desired touch-down point is still 1,000 feet from the approach end of the runway. Touchdown at the planned point. Cross the threshold at Vapp, then bleed off speed to land approximately Vref -5. Use reverse, if needed. To achieve maximum braking effect on wet runway, apply maximum and steady brake pressure. In 1992, the City of Killeen submitted a proposal that included extending the north end of runway 01 by 194 feet. The FAA originally disapproved the proposal, in part, because the runway extension decreased the length of the runway safety area (RSA) which was already shorter than the recommended 1,000 feet for a 14 CFR Part 139 certificated airport. The proposal was subsequently approved and a drainage ditch was installed in the north RSA, perpendicular to the runway and approximately 175 feet north of the departure end of runway 01. In 1993, the airport received FAA Part 139 certification. The 1998 and 1999, FAA airport certification inspection reports noted the inadequate RSA; however, neither letter of correction, sent from the FAA to the City of Killeen following the inspections, mentioned the RSA. Following this accident, the ILS runway 01 was flight checked by the FAA and all components were found to be operating within prescribed tolerances. Examination of the airplane found no anomalies that would have prevented it from operating per design prior to departing the runway and encountering the ditch.
Probable cause:
The captain's failure to follow standard operating procedure for landing on a contaminated runway in that he touched down long, which combined with his delayed braking resulted in a runway overrun. Contributing factors were the captain's failure to maintain runway alignment following his disconnect of the autopilot, the gusty crosswind and the wet runway. In addition, the following were contributing factors:
(1) the airport operator's failure to fill in a ditch in the runway safety area,
(2) the FAA's granting of 14 CFR Part 139 approval to the airport when the runway safety area (RSA) did not meet the recommended length for a Part 139 airport, and
(3) the FAA's continued lack of acknowledgement to the airport of the inadequate RSA following their annual airport inspection checks.
Final Report:

Crash of a Lockheed C-130E Hercules in Fort Hood: 8 killed

Date & Time: Mar 12, 1985
Type of aircraft:
Operator:
Registration:
64-0549
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Dyess AFB - Gray AAF
MSN:
4044
YOM:
1965
Location:
Crew on board:
8
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
8
Circumstances:
The four engine aircraft was completing a training mission from Dyess AFB (Abilene) to the Gray AAF near Killeen, carrying eight crew members. En route, while flying at low height and dropping sand bags, the airplane went out of control and crashed near Fort Hood. All eight crew members were killed.

Crash of a Rockwell Aero Commander 560A in Belton

Date & Time: May 26, 1973 at 1400 LT
Operator:
Registration:
N2269B
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Killeen - Killeen
MSN:
560A-263
YOM:
1955
Location:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
440
Captain / Total hours on type:
30.00
Circumstances:
The crew was completing a local training flight out from Killeen Airport. While cruising at a relative low altitude, the right engine failed. The pilot-in-command elected to make an emergency landing when the aircraft crashed in an open field located in Belton. The aircraft was damaged beyond repair and all three occupants escaped uninjured.
Probable cause:
Failure of the right engine in flight for undetermined reason. The following factors were reported:
- Improper operation of powerplant,
- Improper emergency procedures,
- Intentional wheels-up landing,
- Rough terrain,
- The pilot did not apply adequate power to left engine after failure of the right engine.
Final Report:

Crash of a Beechcraft 99A Airliner in Killeen

Date & Time: Jan 12, 1971 at 1820 LT
Type of aircraft:
Operator:
Registration:
N12RA
Survivors:
Yes
Schedule:
Dallas – Killeen
MSN:
U-131
YOM:
1969
Location:
Crew on board:
2
Crew fatalities:
Pax on board:
13
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4200
Captain / Total hours on type:
1000.00
Circumstances:
On approach to Killeen Airport, the crew encountered marginale weather conditions with fog and ceiling. He was informed from ATC about a visibility below minima but the captain decided to continue the descent until the aircraft struck the ground short of runway and came to rest. The aircraft was damaged beyond repair and all 15 occupants were injured, nine of them seriously.
Probable cause:
Improper IFR operation on part of crew. The following factors were reported:
- Low ceiling and fog,
- The pilot knew that weather was below VOR minimums from ATC and another pilot who had to divert to alternate airport.
Final Report:

Crash of a Boeing KC-135A-BN Stratotanker near Killeen: 4 killed

Date & Time: Mar 31, 1959 at 1145 LT
Type of aircraft:
Operator:
Registration:
58-0002
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Bergstrom - Bergstrom
MSN:
17747
YOM:
1959
Location:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
The crew departed Bergstrom AFB (Austin) on a B-52 refuelling mission. En route, while cruising in a low pressure area with turbulences, the airplane went out of control, dove into the ground and crashed in a huge explosion. All four crew members were killed. Brand new, the airplane has been delivered six weeks prior to the accident.
Crew:
Lt Rodney Anderlitch,
Maj Jesse Lee Myrick,
Lt Philip Camillo de Bonis,
Sgt Herman Allison Clark.
Probable cause:
Following severe turbulences in-flight, the pylon of two engines failed, causing the engine to detach. One of them struck the empennage that was partially sheared off. The aircraft went out of control and crashed.