Crash of a Swearingen SA227AC Metro III in San Antonio

Date & Time: Sep 18, 1992 at 1310 LT
Type of aircraft:
Operator:
Registration:
N2183A
Flight Type:
Survivors:
Yes
Schedule:
San Antonio - San Antonio
MSN:
AC-422
YOM:
1981
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
6000
Captain / Total hours on type:
650.00
Aircraft flight hours:
17936
Circumstances:
The pilot was conducting a functional test flight and qualitative engineering evaluation of the airplane's longitudinal control during landing. During final approach to runway 12L, he reduced the engines to the flight idle positions and established 95 kias. He was unable to raise the nose of the airplane during the flare to arrest the descent rate and landed hard onto the runway. The airplane was taxied to the ramp and secured. No mechanical failure was found or reported.
Probable cause:
The landing capability of the airplane was exceeded. The lack of performance data was a factor in the accident.
Final Report:

Crash of a Cessna 421B Golden Eagle II in San Antonio

Date & Time: Mar 3, 1989 at 0245 LT
Registration:
N5999M
Survivors:
Yes
Schedule:
Memphis - San Antonio
MSN:
421B-0242
YOM:
1972
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
732
Captain / Total hours on type:
34.00
Aircraft flight hours:
2897
Circumstances:
The airplane had made one approach, followed by a missed approach during a dark night with low ceilings and low visibility. During the next approach the airplane was high on the glide slope and touched down fast and long. The airplane hit the terrain 300 feet past the end of the runway, hit a second time 115 feet further down, then flew into the ils localizer. Part of the left wing burned. There were no indications of an attempted go-around.
Probable cause:
The failure of the pilot to follow the proper procedures/directives by not following the glideslope which resulted in not being able to attain the proper touchdown point.
Final Report:

Crash of a Lockheed 18 LodeStar in Dallas

Date & Time: Dec 7, 1987 at 1729 LT
Type of aircraft:
Registration:
N400NY
Flight Type:
Survivors:
Yes
Schedule:
San Antonio - Dallas
MSN:
18-2379
YOM:
1943
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
11500
Captain / Total hours on type:
782.00
Aircraft flight hours:
8735
Circumstances:
The right engine of the aircraft failed three times in flight. After the last failure near the middle marker the pilot feathered the propeller. The aircraft collided with power lines and the ground about 400 yards short of runway 31 at the Redbird Airport. The right fuel selector was positioned to the left rear tank and the left selector was positioned to the off position. The left wing tanks were intact and empty. Both engines had failed due to fuel exhaustion. Two airports were overflown that were adequate for landing and that had fuel available. This was the co-pilot's first flight.
Probable cause:
Occurrence #1: loss of engine power (total) - nonmechanical
Phase of operation: approach - faf/outer marker to threshold (ifr)
Findings
1. (c) fluid, fuel - exhaustion
2. (f) preflight planning/preparation - inadequate - pilot in command
3. (c) fuel consumption calculations - improper - pilot in command
4. (c) refueling - not obtained - pilot in command
5. (f) in-flight planning/decision - poor - pilot in command
----------
Occurrence #2: forced landing
Phase of operation: descent - emergency
----------
Occurrence #3: in flight collision with object
Phase of operation: descent - emergency
Findings
6. (f) object - wire, transmission
----------
Occurrence #4: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Findings
7. (f) terrain condition - rough/uneven
Final Report:

Crash of a Cessna 208 Caravan I in Bulverde

Date & Time: Sep 4, 1987 at 2245 LT
Type of aircraft:
Operator:
Registration:
N807LA
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
San Antonio – Dallas
MSN:
208-0026
YOM:
1985
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
3100
Captain / Total hours on type:
750.00
Aircraft flight hours:
222
Circumstances:
After leveling at 5,500 feet, the standby power annunciator light illuminated, followed by loss of oil pressure. The pilot turned back toward the airport, but there was a progressive loss of engine power and the prop went to a feathered position. During an emergency landing at night, the aircraft hit a power line and trees, then crashed. During an engine teardown, disassembly of the reduction gearbox scavenge pump revealed that a retaining nut and tang washer (w/i the scavenge pump) had backed off and lodged between the spur gears, which resulted in a sheared scavenge pump drive shaft. In turn, this resulted in the loss of oil pressure and allowed the prop to feather.
Probable cause:
Occurrence #1: airframe/component/system failure/malfunction
Phase of operation: cruise - normal
Findings
1. (c) lubricating system, oil scavenge pump - loose
2. (c) lubricating system, oil scavenge pump - jammed
3. (c) lubricating system, oil scavenge pump - failure, total
4. Initiated
----------
Occurrence #2: loss of engine power (total) - mech failure/malf
Phase of operation: cruise
Findings
5. (c) fluid, oil - starvation
----------
Occurrence #3: forced landing
Phase of operation: descent - emergency
----------
Occurrence #4: in flight collision with object
Phase of operation: landing
Findings
6. (f) light condition - night
7. (f) object - wire, transmission
8. (f) object - tree(s)
----------
Occurrence #5: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Final Report:

Crash of a Beechcraft B60 Duke in Wall

Date & Time: May 27, 1987 at 0851 LT
Type of aircraft:
Operator:
Registration:
N4314W
Flight Phase:
Survivors:
Yes
Schedule:
San Angelo – San Antonio
MSN:
P-264
YOM:
1974
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
2553
Captain / Total hours on type:
250.00
Aircraft flight hours:
2645
Circumstances:
Aircraft was destroyed during an attempted off airport emergency landing following a dual engine failure while leveling off at cruise flight. Pilot stated that left engine, then right engine surged and quit as he was leveling off at 9,000 feet msl. At the time of the engine failures the fuel totalizer was reading 60 gallons, but the aircraft fuel gauges were reading empty. Pilot broke out of overcast at 3,500 msl (about 1,200 feet agl) and was unable to find a suitable clear area to land before committing to an emergency landing in trees. Gear was down, flaps were up and neither engine was feathered at impact. Pilot stated that he knew he was out of gas when both engines quit and that he did not attempt an air start. Both occupants were seriously injured.
Probable cause:
Occurrence #1: loss of engine power (total) - nonmechanical
Phase of operation: cruise - normal
Findings
1. (c) fluid,fuel - exhaustion
2. (c) refueling - disregarded - pilot in command
3. (c) fuel consumption calculations - not performed - pilot in command
4. (c) complacency - pilot in command
----------
Occurrence #2: forced landing
Phase of operation: descent - emergency
Findings
5. Weather condition - low ceiling
6. Emergency procedure - not performed - pilot in command
7. Propeller feathering - not performed - pilot in command
----------
Occurrence #3: in flight collision with object
Phase of operation: landing - flare/touchdown
Findings
8. (f) object - tree(s)
9. (f) terrain condition - high obstruction(s)
10. (f) terrain condition - none suitable
Final Report:

Crash of a Beechcraft B90 King Air 90 near Charlotte: 7 killed

Date & Time: May 5, 1982 at 1519 LT
Type of aircraft:
Operator:
Registration:
N98949
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Laredo - San Antonio
MSN:
LJ-407
YOM:
1968
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
7
Captain / Total flying hours:
7385
Captain / Total hours on type:
35.00
Aircraft flight hours:
2915
Circumstances:
The pilot and 6 passengers were returning home after fishing in Mexico. After clearing customs at Laredo, TX, they departed on the next leg of the flight. The pilot was cleared to 11,000 ft, but got off course. He commented that an instrument had popped, he then requested 7,000 ft, but due to other traffic, his request was delayed. While still at 5,000 ft, he stated, "hey, i'm in the middle of the top of this stuff." Approximately 7 minutes after being cleared to 7,000 ft, controllers noted that the aircraft began descending. They attempted to call the pilot, but were unable. An investigation revealed the aircraft had crashed after the outer wing panels and the empennage had separated. The exact sequence of the in-flight break-up was not determined. Radar info indicated the aircraft had entered several vertical oscillations of several hundred feet before descending. An examination of the fracture surfaces revealed only overload failure. Other pilots reported clouds between 3,000 & 6,500 feet with only light turbulences. The aircraft was estimated to be approximately 65 lbs over the max gross weight limit and loaded near the aft CofG. All seven occupants were killed in the accident.
Probable cause:
Occurrence #1: loss of control - in flight
Phase of operation: cruise - normal
Findings
1. Aircraft weight and balance - exceeded - pilot in command
2. (f) weather condition - clouds
3. (f) weather condition - turbulence in clouds
4. (c) reason for occurrence undetermined
----------
Occurrence #2: airframe/component/system failure/malfunction
Phase of operation: descent - uncontrolled
Findings
5. (c) design stress limits of aircraft - exceeded
6. Wing,spar - overload
7. Wing,spar - separation
8. Horizontal stabilizer surface - overload
9. Horizontal stabilizer surface - separation
10. Vertical stabilizer surface - overload
11. Vertical stabilizer surface - separation
----------
Occurrence #3: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Final Report:

Crash of a Piper PA-31-350 Navajo Chieftain in San Antonio: 3 killed

Date & Time: Apr 18, 1982 at 2017 LT
Operator:
Registration:
N3580D
Flight Phase:
Survivors:
No
Schedule:
San Antonio - Midland
MSN:
31-8052084
YOM:
1980
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
3
Aircraft flight hours:
650
Circumstances:
The pilot was trying to land after both engines failed during takeoff after the aircraft was refueled with jet fuel instead of gasoline. The weather was IFR with fog, low ceiling and rain. The aircraft collided with trees during a forced landing and was destroyed by fire after impact. All three occupants were killed.
Probable cause:
Occurrence #1: loss of engine power(total) - nonmechanical
Phase of operation: takeoff - initial climb
Findings
1. (c) fluid,fuel - improper
2. (c) maintenance,service of aircraft/equipment - improper - fbo personnel
3. (c) inadequate training - company/operator management
4. (c) annunciator panel light(s) - improper
----------
Occurrence #2: forced landing
Phase of operation: landing
----------
Occurrence #3: in flight collision with terrain/water
Phase of operation: maneuvering - turn to landing area (emergency)
Findings
5. (f) light condition - dark night
6. (f) weather condition - low ceiling
7. (f) weather condition - fog
8. (f) object - tree(s)
----------
Occurrence #4: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Final Report:

Crash of a Cessna 414 Chancellor in Winkler County

Date & Time: May 22, 1981 at 1700 LT
Type of aircraft:
Registration:
N4200C
Survivors:
Yes
Schedule:
San Antonio - Winkler County
MSN:
414-0516
YOM:
1974
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4441
Captain / Total hours on type:
1456.00
Circumstances:
On final approach to Winkler County Airport, the twin engine airplane stalled and crashed, bursting into flames. Both occupants escaped with minor injuries while the aircraft was damaged beyond repair.
Probable cause:
Stall on final approach after the pilot failed to maintain flying speed. The following contributing factors were reported:
- Unfavorable wind conditions,
- Downdrafts, updrafts,
- Wind gusts to 18 knots.
Final Report:

Crash of a Piper PA-61 Aerostar (Ted Smith Aerostar 601P) near New Braunfels: 2 killed

Date & Time: Feb 17, 1979 at 1435 LT
Operator:
Registration:
N9779Q
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
San Antonio – Lake Charles
MSN:
61-0407-143
YOM:
1977
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
1200
Circumstances:
While in cruising altitude on a flight from San Antonio to Lake Charles, the twin engine airplane went out of control, entered a dive and crashed near New Braunfels, Texas. The aircraft was totally destroyed by impact forces and a post crash fire and both occupants were killed.
Probable cause:
Uncontrolled descent and subsequent ground collision after the pilot attempted operation beyond experience/ability level. The following contributing factors were reported:
- Improper IFR operation,
- Suffered a spatial disorientation,
- One day prior to the accident, flight instructor recommended the pilot not to fly IFR till 10 hours additional dual instruction received.
Final Report:

Crash of a Douglas DC-6 in Omaha: 7 killed

Date & Time: Dec 6, 1978 at 1725 LT
Type of aircraft:
Operator:
Registration:
TP-203
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Omaha – San Antonio – Mexico City
MSN:
43129/106
YOM:
1948
Crew on board:
4
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
7
Circumstances:
Shortly after takeoff from Omaha-Eppley Airport, while climbing, the airplane suffered an engine fire. It stalled and crashed in a huge explosion on a dyke located near the runway end. The aircraft was totally destroyed and all seven occupants were killed. The airplane was en route to Mexico following maintenance at Omaha facilities.
Probable cause:
Engine fire for unknown reasons. An oil leak was reported.