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Crash of a Learjet 25B in Del Rio: 1 killed

Date & Time: Sep 19, 2003 at 1710 LT
Type of aircraft:
Operator:
Registration:
N666TW
Flight Type:
Survivors:
Yes
Schedule:
El Paso – Del Rio
MSN:
25-116
YOM:
1973
Flight number:
AJI892
Location:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
4689
Captain / Total hours on type:
1348.00
Copilot / Total flying hours:
2783
Copilot / Total hours on type:
263
Aircraft flight hours:
15363
Circumstances:
The cargo flight was cleared for a visual approach to the 5,000-foot long, by 150-foot wide asphalt runway. Based on estimated landing weight of the aircraft, the Vref was estimated at 116 KIAS. Air traffic Control (ATC) radar data revealed that the flight maintained a ground speed above 190 knots on final approach, to include the touchdown zone for runway 13. The first evidence of braking was noted at a point 1,247 feet from the departure end of the runway. Braking signatures on the asphalt as well as off the pavement were consistent with an operational anti-skid system. Witnesses at the airport also observed the airplane flying very fast and touching down long. Both crewmembers, the 4,689-hour captain and the 2,873-hour first officer, were familiar with the airport, and the flight was 20 minutes ahead of its scheduled arrival time. The airplane overran the departure end of runway 13, impacted the airport perimeter fence, proceeded across a roadway, took out another fence, and collided with two trees in a cemetery. The airplane was found to be within weight and balance limits for all phases of the flight. The installed cockpit voice recorder (CVR) was found not to be functional.
Probable cause:
The pilot's misjudged distance and speed during the approach to landing, and his failure to obtain the proper touchdown point resulting in an overrun. A contributing factor was the pilot's failure to abort the landing.
Final Report:

Crash of a Cessna 414 Chancellor in Oklahoma

Date & Time: Jan 26, 2000 at 1100 LT
Type of aircraft:
Operator:
Registration:
N7VS
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Oklahoma City – El Paso
MSN:
414-0276
YOM:
1972
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
14432
Captain / Total hours on type:
1350.00
Circumstances:
The pilot reported that light snow was falling, with approximately 2 inches already on the ground, and the runway had been plowed approximately one hour prior to his departure. About 20 minutes had elapsed since the airplane had been towed from the '68 degree F' hangar. During the takeoff, the airplane accelerated 'normally' and became airborne after traveling about 2,160 feet down the 3,240-foot runway. After liftoff, the airplane did not climb above 25 or 30 feet agl. The airplane impacted an embankment at the end of the runway, continued across railroad tracks, and through a fence coming to rest in a brick storage yard about 800-1,000 feet from the departure end of the runway. The pilot stated that someone told him that the airport did not have any deicing equipment, therefore, he did not deice the airplane. The weather facility, located 5 miles from the accident site, reported the wind from 100 degrees at 7 knots, visibility 1/2 mile with snow and freezing fog, temperature 27 degrees F.
Probable cause:
The failure of the pilot to deice the airplane prior to departure.
Final Report:

Crash of a Dassault Falcon 20C in El Paso

Date & Time: Aug 28, 1998 at 0650 LT
Type of aircraft:
Operator:
Registration:
N126R
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Addison - El Paso - Memphis
MSN:
126
YOM:
1968
Flight number:
RLT126
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
3700
Captain / Total hours on type:
1850.00
Copilot / Total flying hours:
3636
Copilot / Total hours on type:
124
Aircraft flight hours:
16602
Circumstances:
The airplane was dispatched as a cargo flight to pick up a load of 118 boxes of automotive seatbelts. After refueling and loading the cargo on board, the flight crew taxied to runway 22 for a no-flap takeoff, which called for a V1 speed of 141 knots. The first officer was the flying pilot for this leg of the flight. The crew reported that the initial takeoff roll from the 11,009 foot runway was normal. At approximately 120 knots, the flight crew reported hearing a loud bang followed by a vibration. The captain called for the first officer to abort the takeoff. The captain later stated that he believed he saw the #2 engine "roll back." The flight crew reported that the brakes were not effective in slowing the airplane. A witness stated that the airplane was going west on the runway at a high rate of speed when it "went up to two feet, then came back down." Another witness stated that he saw the airplane "exit off the end of the runway" and after about "seventy-five to one hundred feet, the front wheels lifted off the ground about ten feet." The airplane overran the departure end of the runway, went through the airport's chain link perimeter fence, across a 4-lane highway, collided with 3 vehicles on the roadway, and went through a second chain link fence, before coming to rest. The airplane came to rest on its belly, 2,010 feet from the departure threshold of runway 22. The investigation revealed that the flight crew was provided an inaccurate weight for the cargo, and the airplane was found to be 942 pounds over the maximum takeoff weight at the time of the accident. The density altitude was calculated to be 5,614 feet at the time of the accident. Both crewmembers were current and properly certified; however, the captain had upgraded to his present position two months prior to the accident, and the first officer had accumulated a total of 123.8 hours in the Falcon 20 at the time of the accident. Both engines were operated in a test cell and performed within limits. About 90% of the right outboard main landing gear tire's retread was found on the runway approximately 7,200 feet from where the aircraft had commenced its takeoff roll. The operator stated that since the aircraft was over maximum gross weight, the long taxi to the runway could have resulted in the brakes and tires heating more than normal.
Probable cause:
The captain's decision to abort the takeoff at an airspeed above V1, which resulted in a runway overrun. Contributing factors were: the loading of an excessive amount of cargo by the shipper which resulted in an over gross weight airplane, the high density altitude, the separation of tire retread on takeoff roll, and the flight crew's lack of experience in the accident make and model aircraft.
Final Report:

Crash of a Piper PA-31P-350 Mojave in Denver

Date & Time: Dec 1, 1985 at 1808 LT
Type of aircraft:
Registration:
N9250Y
Flight Type:
Survivors:
Yes
Schedule:
El Paso – Denver
MSN:
31-8414029
YOM:
1984
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
1050
Captain / Total hours on type:
212.00
Aircraft flight hours:
296
Circumstances:
The pilot had been flying approximately 7 hours and was completing the flight at night when the accident occurred. He was using visual cues (the airport environment) to position the aircraft at a proper altitude for a visual approach and landing. The terrain south of the airport rises several hundred feet above the airport elevation. The terrain is sparsely lit. The aircraft touched down two miles short of runway 34R in an open pasture at an elevation of approximately 400 feet higher than the airport. The pilot had flown approximately one hour of night time in the last 90 days, according to his logbook. All three occupants were injured, two seriously.
Probable cause:
Occurrence #1: in flight collision with terrain/water
Phase of operation: approach
Findings
1. (f) light condition - dark night
2. (c) became lost/disoriented - inadvertent - pilot in command
3. (f) visual/aural perception - pilot in command
4. (f) fatigue - pilot in command
5. (f) lack of familiarity with geographic area - pilot in command
6. (f) lack of recent experience in type operation - pilot in command
7. (c) altitude - misjudged - pilot in command
8. Terrain condition - rising
9. (c) clearance - not maintained - pilot in command
Final Report:

Crash of a Vickers 648 Varsity I in El Paso

Date & Time: Dec 11, 1983 at 1415 LT
Type of aircraft:
Registration:
N65338
Flight Type:
Survivors:
Yes
Schedule:
El Paso - El Paso
YOM:
1953
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
1425
Captain / Total hours on type:
5.00
Aircraft flight hours:
7371
Circumstances:
The aircraft was on a flight from the El Paso Intl Airport to the West Texas Airport. A hard landing was made causing all three landing gear to collapse, folded the left wing aft just inboard of the engine and twisted the entire right wing about 30° leading edge down. According to the pilot the aircraft was flown with 30° of flaps on downwind and 47° of flaps on base. He also reported that both airspeed indicators were stuck at 110 knots. According to photographs taken by an unidentified party, the flaps were in the up position in the pattern and during touchdown. Touchdown was made with the right main gear off the right side of the rwy. The aircraft wheel track is only 4 feet less than the width of the runway. The pilot did not have a type rating nor authorization in lieu of a type rating for the 15 minutes ferry flight. The pilot had 4,140 hours copilot time in the aircraft, during which he had never landed the aircraft.
Probable cause:
Occurrence #1: hard landing
Phase of operation: landing - flare/touchdown
Findings
1. (c) judgment - poor - pilot in command
2. (c) overconfidence in personal ability - pilot in command
3. (f) flight/nav instruments,airspeed indicator - inoperative
4. (c) level off - misjudged - pilot in command
5. (c) inadequate initial training - pilot in command
6. (c) lack of total experience in type of aircraft - pilot in command
7. (c) unsuitable terrain or takeoff/landing/taxi area - selected - pilot in command
8. (c) proper alignment - not attained - pilot in command
----------
Occurrence #2: complete gear collapsed
Phase of operation: landing - flare/touchdown
Findings
9. Landing gear,main gear - overload
10. Landing gear,nose gear - overload
----------
Occurrence #3: airframe/component/system failure/malfunction
Phase of operation: landing - flare/touchdown
Findings
11. Wing - overload
Final Report:

Crash of a Lockheed 9D Orion in El Paso

Date & Time: Nov 21, 1933
Type of aircraft:
Operator:
Registration:
NC229Y
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
El Paso – Tucson
MSN:
200
YOM:
1933
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
After takeoff from El Paso Airport, while climbing to a height of about 800 feet, the engine caught fire. The pilot bailed out and abandoned the aircraft that entered a dive and crashed in a field. The pilot was uninjured and the aircraft was destroyed.
Probable cause:
Engine fire during climbout.