Zone

Crash of a Beechcraft 200 Super King Air in Bayview

Date & Time: Dec 10, 2004 at 1250 LT
Operator:
Registration:
N648KA
Flight Phase:
Survivors:
Yes
Schedule:
Bayview - Houston
MSN:
BB-648
YOM:
1980
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
5800
Captain / Total hours on type:
400.00
Aircraft flight hours:
6532
Circumstances:
While attempting to depart from the 3,500-foot long grass airstrip with a 14 knot quartering tailwind, the 5,800-hour pilot reported that at an airspeed of approximately 95 knots, "the airplane yawed left and rolled left abruptly as the aircraft came off the ground briefly." The airplane settled back onto the ground, before again climbing back into the air approximately 20 degrees left of the runway heading. Subsequently, the airplane’s landing gear struck tree tops before it impacted the ground. A passenger added that he "noticed the flaps were up during takeoff." Approximately three minutes after the accident, a weather reporting station located 5.6 nautical miles southwest of the accident site reported wind from 010 degrees at 14 knots. Examination of the engines revealed rotational scoring throughout the first and second stage turbines. No mechanical anomalies were observed.
Probable cause:
The pilot's failure to maintain directional control as result of his improper runway selection for takeoff. A contributing factor was the prevailing right quartering tailwind.
Final Report:

Crash of a Learjet 24D in Tampico: 3 killed

Date & Time: Jan 2, 1998 at 1110 LT
Type of aircraft:
Registration:
XA-RRK
Survivors:
Yes
Schedule:
Houston - Tampico
MSN:
24-307
YOM:
1975
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
10911
Copilot / Total flying hours:
5761
Aircraft flight hours:
8095
Circumstances:
On approach to Tampico-General Francisco Javier Mina Airport, the crew established on the ILS. The aircraft descended below the glide and MDA until it struck the ground and crashed in a lagoon located 12,8 km short of runway. A pilot and two passengers were killed while five other occupants were injured. The aircraft was destroyed.
Probable cause:
The decision of the crew to continue the approach under VFR mode in IMC conditions (foggy conditions), allowing the aircraft to descend below the minimum descent altitude until impact with the ground.
Final Report:

Crash of a Partenavia P.68C Victor near Tilden

Date & Time: Apr 25, 1985 at 1300 LT
Type of aircraft:
Operator:
Registration:
N76L
Flight Phase:
Survivors:
Yes
Schedule:
Corpus Christi - Houston
MSN:
292
YOM:
1983
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
6020
Captain / Total hours on type:
712.00
Aircraft flight hours:
727
Circumstances:
After approximately 1.5 hours of pipeline patrol flight at a planned altitude of 500 feet agl the aircraft flew into the flat terrain in a landing attitude. The aircraft went through a wire fence, heavy brush and small trees before coming to rest 437 feet from initial ground contact with all 3 gear collapsed. A physical examination and the pilot's statement indicate that the pilot was operating under an extreme amount of stress which may have resulted in chronic fatigue at the time of the accident. According to the pilot, he was accustomed to a very heavy flight schedule. The chief pilot attempted to assign an additional pilot but company budget constraints prevented such an assignment.
Probable cause:
Occurrence #1: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Findings
1. (c) proper altitude - not maintained - pilot in command
2. (c) descent - inadvertent - pilot in command
3. (f) fatigue (chronic) - pilot in command
4. Company-induced pressure - company/operator management
5. Terrain condition - ground
----------
Occurrence #2: complete gear collapsed
Phase of operation: other
Findings
6. Landing gear - overload
Final Report:

Crash of a Beechcraft 65-A80 Queen Air near Madisonville: 3 killed

Date & Time: Jul 2, 1981 at 1230 LT
Type of aircraft:
Registration:
N100UV
Flight Phase:
Survivors:
No
Schedule:
Houston - Dallas
MSN:
LD-151
YOM:
1964
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
398
Circumstances:
While in cruising altitude in marginal weather conditions on a flight from Houston to Dallas, the pilot lost control of the airplane that entered a dive. During the descent, wings and stabs separated and the aircraft crashed near Madisonville. All three occupants were killed.
Probable cause:
Loss of control in flight after the pilot suffered a spatial disorientation. The following contributing factors were reported:
- The pilot exceeded designed stress limits of aircraft,
- The pilot attempted operation beyond experience/ability level,
- Lack of familiarity with aircraft,
- Thunderstorm activity,
- Wings: spars,
- Flight control surfaces: horizontal stabilizer, attachments,
- Overload failure,
- Separation in flight,
- Aircraft observed falling from clouds with wings and stabs separated,
- Pilot lacked recent instrument experience and multi-engine instrument time.
Final Report:

Crash of a Piper PA-31-310 Navajo near Hammond: 3 killed

Date & Time: May 1, 1981 at 0726 LT
Type of aircraft:
Registration:
N3544J
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Houston - Mineral Wells
MSN:
31-8012004
YOM:
1980
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
2200
Circumstances:
En route from Houston to Mineral Wells, the pilot encountered poor weather conditions with thunderstorm activity and turbulences. While flying in adverse weather conditions, he suffered a spatial disorientation and lost control of the airplane that dove into the ground and crashed in a field near Hammond, bursting into flames. All three occupants were killed.
Probable cause:
Uncontrolled descent and subsequent crash after the pilot continued VFR flight into adverse weather conditions. The following contributing factors were reported:
- The pilot suffered a spatial disorientation,
- Fog,
- Turbulences associated with clouds and thunderstorms,
- Thunderstorm activity,
- Visibility 2 miles or less.
Final Report:

Crash of a Mitsubishi MU-2B-35 Marquise in Lajitas: 2 killed

Date & Time: Apr 19, 1981 at 1620 LT
Type of aircraft:
Registration:
N500GL
Flight Phase:
Survivors:
Yes
Schedule:
Lajitas - Houston
MSN:
579
YOM:
1973
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
9
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
5000
Captain / Total hours on type:
4400.00
Circumstances:
After takeoff from Lajitas Airfield, the twin engine airplane encountered difficulties to gain height. It struck power cables then crashed, bursting into flames. The pilot and one passenger were killed while eight other occupants were injured, five of them seriously.
Probable cause:
Collision with wires/poles during initial climb after the pilot selected the wrong runway relative to existing wind. The following contributing factors were reported:
- The pilot misused or failed to use flaps,
- The pilot failed to abort takeoff,
- Airport conditions,
- High density altitude, about 4,800 feet,
- Rough/uneven terrain,
- 1% upslope runway,
- Aircraft near max gross weight,
- Aircraft CofG at limit,
- Wind gusting 15 knots.
Final Report:

Crash of a Rockwell Aero Commander 700 in Palacios

Date & Time: Jan 26, 1981 at 1640 LT
Operator:
Registration:
N703SA
Flight Phase:
Survivors:
Yes
Schedule:
Palacios - Houston
MSN:
700-31
YOM:
1980
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
3034
Captain / Total hours on type:
410.00
Circumstances:
After takeoff from Palacios Airport, while climbing, both engines lost power. The pilot was cleared to return for an emergency landing and initiated a turn. While flying at low height, the twin engine airplane struck power cables and crashed in a field. All four occupants were slightly injured.
Probable cause:
Partial loss of power on both engines due to inadequate preflight preparation. The following contributing factors were reported:
- Improperly serviced aircraft by ground crew,
- Improper fuel-grade,
- High obstructions (power cables),
- Forced landing off airport on land,
- Aircraft serviced with Jet A fuel.
Final Report:

Crash of a Learjet 25B near Conlon: 2 killed

Date & Time: Apr 11, 1980 at 1719 LT
Type of aircraft:
Registration:
N25TA
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Vernal - Houston
MSN:
25-196
YOM:
1975
Location:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
7800
Captain / Total hours on type:
1000.00
Circumstances:
While cruising at an altitude of 41,200 feet, the airplane entered an uncontrolled descent following an airframe failure in flight. The airplane crashed in an open field and was totally destroyed. Both pilots who were completing a ferry flight from Vernal to Houston were killed.
Probable cause:
Airframe failure in flight, separation in flight and subsequent uncontrolled descent for undetermined reasons.
Final Report:

Crash of a Douglas DC-9-14 in Baton Rouge

Date & Time: Mar 17, 1980 at 1645 LT
Type of aircraft:
Operator:
Registration:
N9103
Survivors:
Yes
Schedule:
Houston - Baton Rouge
MSN:
45796/74
YOM:
1966
Crew on board:
4
Crew fatalities:
Pax on board:
46
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
15732
Captain / Total hours on type:
8720.00
Circumstances:
The airplane landed in rain falls with a 18 knots tailwind about 2,000 feet down runway 13 which is 5,800 feet long. Unable to stop within the remaining distance, the airplane overran and came to rest in a ditch about 350 feet further and 200 feet to the right of the extended centreline. All 50 occupants escaped without injuries while the aircraft was damaged beyond repair. At the time of the accident, the total weight of the airplane was 71,000 lbs.
Probable cause:
Overshoot on landing and subsequent overrun and collision with ditch because ATC cleared the aircraft to wrong runway for existing conditions. The following contributing factors were reported:
- Improper in-flight decisions on part of the pilot-in-command,
- Improper operation of brakes and flight controls on part of the pilot-in-command,
- Rain,
- Wet runway,
- Downwind,
- Haze,
- Aircraft over 25,000 lbs upon landing on runway 13, restricted to zero tailwind/10 knots crosswind when wet,
- Runway 22 available,
- Spoilers not used after touchdown.
Final Report:

Crash of a Beechcraft 65-90 King Air near Leeville: 2 killed

Date & Time: Dec 22, 1979 at 0135 LT
Type of aircraft:
Operator:
Registration:
N724N
Flight Phase:
Survivors:
No
Schedule:
Houston - Tampa
MSN:
LJ-82
YOM:
1966
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
2404
Circumstances:
While in cruising altitude on a night flight from Houston to Tampa, the pilot encountered poor weather conditions with icing. After the pilot suffered a spatial disorientation, the twin engine airplane entered an uncontrolled descent and partially disintegrated in the air before crashing in a lake located near Leeville. Both occupants were killed.
Probable cause:
Uncontrolled descent and subsequent airframe failure in-flight after the pilot suffered spatial disorientation. The following contributing factors were reported:
- The pilot exceeded designed stress limits of the aircraft,
- Incorrect weather briefing,
- Icing conditions including sleet, freezing rain,
- Flight control surfaces: horizontal stabilizer, attachments,
- Wing spars,
- Overload failure,
- Separation in flight,
- Aircraft came to rest in water.
Final Report: