Crash of a Beechcraft F90 King Air in São Pedro da Aldeia: 8 killed

Date & Time: Oct 2, 1988
Type of aircraft:
Registration:
PT-LJR
Flight Phase:
Survivors:
No
MSN:
LA-93
YOM:
1981
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
8
Circumstances:
Crashed in unknown circumstances, killing all eight occupants.

Crash of a Piper PA-61P Aerostar (Ted Smith 601) in Columbus: 1 killed

Date & Time: Sep 30, 1988 at 2124 LT
Registration:
N14HR
Flight Phase:
Survivors:
No
Schedule:
Columbus – Doylestown
MSN:
61-0479-193
YOM:
1978
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
1802
Aircraft flight hours:
3075
Circumstances:
The airplane was destroyed when it collided with terrain shortly after departure. Two witnesses to the accident who saw the accident airplane lift off from the runway described the flight path as erratic in nature with random movement in all three axis, pitch, roll and yaw. The witnesses did not see the actual impact. Evidence shows that the upper half of the main entry clamshell door was not closed at impact. Radio transmissions from the accident airplane while in flight show a elevated voice level indicative of stress as the pic attempted to maintain control the airplane during pitch and roll excursions. The radio transmissions were unintelligible. The tower had cleared the aircraft to land on any runway. The pilot, sole on board, was killed.
Probable cause:
Aerodynamically stalled lifting surface causing an uncommanded pitch over at an altitude too low to affect a recovery.
Findings:
Occurrence #1: miscellaneous/other
Phase of operation: takeoff - initial climb
Findings
1. (f) door - not secured
2. (c) aircraft preflight - inadequate - pilot in command
----------
Occurrence #2: loss of control - in flight
Phase of operation: takeoff - initial climb
Findings
3. (c) door - open
4. (c) aircraft control - not maintained - pilot in command
5. (f) anxiety/apprehension - pilot in command
----------
Occurrence #3: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Findings
6. Terrain condition - ground
Final Report:

Crash of a Piper PA-31-310 Navajo near Santiago de Chile: 1 killed

Date & Time: Sep 20, 1988
Type of aircraft:
Operator:
Registration:
CC-CBO
Flight Phase:
Survivors:
No
Site:
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
Crashed in unknown circumstances in a mountainous area near Santiago. The pilot, sole on board, was killed.

Crash of a Beechcraft 60 Duke in Pageland: 3 killed

Date & Time: Aug 16, 1988 at 0735 LT
Type of aircraft:
Registration:
N21TP
Survivors:
No
Schedule:
Rock Hill – Pageland
MSN:
P-114
YOM:
1970
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
1250
Aircraft flight hours:
3833
Circumstances:
The airplane was observed to approach the airport from the northwest. As it crossed the northeast end of the runway, it initiated a right turn to cross the runway about the midpoint to a position for a left downwind for landing on runway 5. Its altitude was estimated to be about 200-300 feet above the ground and the landing gear was down. The witness did not observe the airplane further. It collided with the ground about 0.4 miles from the threshold. The morning sun was about 10° above the horizon and was about 33° to the right of the runway centerline. It would have been in the pilot's face during his flight from the last departure point. The landing runway sloped upward from the landing threshold. The lower-than-normal traffic pattern, the sun's position in relation to the airplane flight path, and the runway slope could have caused the pilot to perceive his altitude as being higher than it actually was. All three occupants were killed.
Probable cause:
Occurrence #1: in flight collision with terrain/water
Phase of operation: approach - vfr pattern - base leg/base to final
Findings
1. (f) light condition - sunglare
2. (f) terrain condition - uphill
3. (c) proper altitude - misjudged - pilot in command
4. (c) clearance - not maintained - pilot in command
5. (f) visual/aural detection - pilot in command
Final Report:

Crash of a Piper PA-60-700P Aerostar (Ted Smith 600) off Cocoa Beach: 1 killed

Date & Time: Jul 25, 1988 at 1729 LT
Registration:
N69RB
Flight Phase:
Survivors:
No
Schedule:
Stuart – Washington DC
MSN:
60-8423-019
YOM:
1984
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
2150
Captain / Total hours on type:
200.00
Aircraft flight hours:
506
Circumstances:
Flight entered near vertical descent while flying in area of level 1 and 2 thunderstorms just after pilot had called requesting permission to deviate around rain showers. A level 5 thunderstorm was present 8 miles west. The aircraft descended at rates up to 13,800 feet per minute. Witnesses saw aircraft exit bottom of clouds at approximately 4,000 feet in a near flat attitude and rotating around the yaw axis to the left. Engine sounds increased and decreased as the aircraft rotated and all components appeared to be present on the aircraft. No smoke or flame was visible. At approximately 500 feet above the water the rotation stopped and the nose dropped to a 30 to 70° nose down angle and both engines could be heard increasing in power. Before the recovery could be completed the acft struck the ocean. The pilot, sole on board, was killed.
Probable cause:
Occurrence #1: in flight encounter with weather
Phase of operation: cruise
Findings
1. Weather condition - thunderstorm, level II
2. (c) in-flight planning/decision - inadequate - pilot in command
3. Weather condition - turbulence (thunderstorms)
----------
Occurrence #2: loss of control - in flight
Phase of operation: cruise
Findings
4. (c) flight into known adverse weather - not corrected - pilot in command
5. (c) spatial disorientation - pilot in command
6. (c) stall/spin - inadvertent - pilot in command
----------
Occurrence #3: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Final Report:

Crash of a Grumman G-159 Gulfstream I in Cabimas

Date & Time: Jun 15, 1988
Type of aircraft:
Operator:
Registration:
YV-121CP
Survivors:
Yes
MSN:
150
YOM:
1964
Country:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
After touchdown at Cabimas-Oro Negro Airport, the crew started the braking procedure when the aircraft collided with a cow. The right engine and the right main gear were torn off and the aircraft came to rest. There were no injuries among the occupants while the animal was killed. The accident occurred in June 1988, exact date unknown.
Probable cause:
It was determined that the perimeter fence was damaged, allowing animals to enter the airport area. This was not noticed by the airport authorities.

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 Cessna 421A Golden Eagle I in Albuquerque: 2 killed

Date & Time: Mar 25, 1988 at 1801 LT
Type of aircraft:
Registration:
C-GVDG
Survivors:
No
Schedule:
Kansas City - Albuquerque
MSN:
421A-0067
YOM:
1968
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
2180
Captain / Total hours on type:
91.00
Circumstances:
The pilot and one passenger were on a business trip in the US from canada. The pilot had the aircraft fuel tanks 'topped off' prior to departure from Kansas City. The flight plan indicated 3 hours 30 min enroute to Albuquerque with 5 hours 30 min of fuel on board. Strong enroute winds and turbulence were forecast along the route of flight. The actual flight was 4.4 hrs. The aircraft crashed while turning from base leg to final at the Albuquerque Intl Airport. Examination of the wreckage revealed no evidence of fuel in or around the aircraft. The manufacturer recommends using the main tanks for 90 minutes before switching to any aux tank to prevent venting of return fuel overboard. Vented fuel will diminish fuel supply. Both occupants were killed.
Probable cause:
Occurrence #1: loss of engine power (partial) - nonmechanical
Phase of operation: approach - vfr pattern - base leg/base to final
Findings
1. (c) fuel system - not understood - pilot in command
2. (c) fluid, fuel - exhaustion
3. (c) fuel dumped - inadvertent - pilot in command
4. (f) weather condition - unfavorable wind
----------
Occurrence #2: loss of control - in flight
Phase of operation: descent - uncontrolled
Findings
5. (c) stall/spin - inadvertent - pilot in command
Final Report:

Crash of a Cessna 425 Conquest in Sanford: 1 killed

Date & Time: Feb 11, 1988 at 2212 LT
Type of aircraft:
Registration:
N6771Y
Survivors:
Yes
Schedule:
Atlanta - Sanford
MSN:
425-0019
YOM:
1981
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
8750
Aircraft flight hours:
2269
Circumstances:
The flight was cleared for a night ILS approach and advised that tower at destination had closed. Tower had reported at closing that fog was forming and the flight was advised of the fog. The aircraft was located on a remote part of the airport the next morning. The ELT had activated but the signal was weak due to crash damage. Passenger said they never saw runway lights, only taxi lights, and that pilot attempted to perform a go-around. Gear was retracted and aircraft hit level grassy area in a near level attitude. The pilot was not wearing a shoulder harness. The pax crouched in the aisle next to the pilot, helping him find the runway, not wearing restraining belts. No published approach plate for ILS procedure for that runway was found in aircraft. Toxicological report revealed pilot had 3 mcg/ml dextromethorphan, an ingredient found in over counter cold remedies. According to report, levels of that substance in blood greater than 0.1 mcg/ml was sufficient to cause drowsiness.
Probable cause:
Occurrence #1: in flight collision with terrain/water
Phase of operation: missed approach (ifr)
Findings
1. (f) weather condition - fog
2. (c) decision height - disregarded - pilot in command
3. (f) light condition - night
4. Meteorological services - not operating
5. (c) missed approach - improper - pilot in command
6. Control tower - not operating
7. (c) gear retraction - premature - pilot in command
8. (c) in-flight planning/decision - poor - pilot in command
9. (f) impairment (drugs) - pilot in command
10. Shoulder harness - not used - pilot in command
Final Report:

Crash of a Dassault Falcon 20D in Wheeling

Date & Time: Feb 1, 1988 at 1703 LT
Type of aircraft:
Operator:
Registration:
N287W
Survivors:
Yes
Schedule:
Akron - Wheeling
MSN:
194
YOM:
1969
Crew on board:
2
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
8175
Captain / Total hours on type:
2816.00
Aircraft flight hours:
7163
Circumstances:
The aircraft landed after an ILS approach to runway 03. According to the pilot shortly after touchdown he saw deer ahead on the runway. Before he could take evasive action the aircraft struck two deer. Afterwards brake pressure was lost. The pilot steered the aircraft onto grass off the right side of the runway to avoid going past the runway end and down a hill. Examination of the aircraft revealed that the deer were struck with the left main gear, fracturing a hydraulic brake line. All nine occupants escaped uninjured.
Probable cause:
Occurrence #1: on ground/water collision with object
Phase of operation: landing - roll
Findings
1. (f) weather condition - fog
2. (c) object - animal(s)
3. (c) clearance - not possible
----------
Occurrence #2: nose gear collapsed
Phase of operation: landing - roll
Findings
4. (c) landing gear, normal brake system - disabled
5. Brakes (normal) - unavailable
6. Landing gear, nose gear assembly - overload
Final Report: