Crash of an Antonov AN-12 in Sanaa: 58 killed

Date & Time: Jul 14, 1992 at 1200 LT
Type of aircraft:
Operator:
Flight Type:
Survivors:
No
Schedule:
Hadibu - Aden
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
52
Pax fatalities:
Other fatalities:
Total fatalities:
58
Circumstances:
The four engine aircraft departed Hadibu Airport (Socotra) on a flight to Aden, carrying 52 passengers and six crew members, among them 36 civilians and 16 military personnels. On approach to Aden-Khormaksar Airport, the crew was instructed by ATC to initiate a go-around and to follow a holding pattern as the airport was closed to traffic due to poor weather conditions with a sandstorm. Few minutes later, the captain was cleared to divert to Sanaa Airport located 300 km north of his position. On approach to Sanaa Airport, the aircraft crashed in unknown circumstances in a desert area located 10 km short of runway. All 58 occupants were killed.

Crash of a Beriev BE-12P near Veshenskaya

Date & Time: Jul 14, 1992
Type of aircraft:
Registration:
40 yellow
Flight Type:
Survivors:
Yes
MSN:
9 6 014 04
YOM:
1969
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The aircraft was engaged in a fire fighting mission and its crew just landed on the Don River to perform a scooping mission when it collided with a flock of birds that struck the right engine. The aircraft veered to the right and came to rest on the shore. All four crew members escaped uninjured while the aircraft was damaged beyond repair.
Probable cause:
Birdstrike.

Crash of a Dornier DO.28D-2 Skyservant at Büchel AFB: 2 killed

Date & Time: Jul 10, 1992
Type of aircraft:
Operator:
Registration:
58+58
Flight Type:
Survivors:
No
Schedule:
Büchel AFB - Büchel AFB
MSN:
4133
YOM:
1972
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
The crew was completing a local training flight at Büchel AFB. During a single engine approach, the crew initiated a go-around procedure when the aircraft stalled and crashed one km short of runway 03/21 threshold. The aircraft was destroyed and both occupants were killed.
Crew:
OLt Johannes Asanger,
Maj Eckhard Südmeyer.

Crash of a Cessna 650 Citation III in Concepción: 3 killed

Date & Time: Jul 9, 1992
Type of aircraft:
Operator:
Registration:
E-302
Flight Type:
Survivors:
No
Schedule:
Santiago - Concepción
MSN:
650-0033
YOM:
1984
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
On final approach to Concepción-Carriel Sur Airport, the crew encountered poor weather conditions with overcast at 750 metres and broken at 300 metres. On final, the crew informed ATC he just passed over the inner marker when the aircraft struck the slope of a mountain (435 metres high) located 4 km short of runway 20 threshold. All three crew members were killed. At the time of the accident, wind was blowing from the north at 23 knots. For unknown reasons, the crew was completing the approach at an insufficient altitude.

Crash of an Antonov AN-12A in Norilsk: 10 killed

Date & Time: Jun 22, 1992 at 1245 LT
Type of aircraft:
Operator:
Registration:
CCCP-11896
Flight Type:
Survivors:
Yes
Schedule:
Andijan – Omsk – Norilsk
MSN:
3 3 409 06
YOM:
1963
Country:
Region:
Crew on board:
7
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
10
Aircraft flight hours:
15654
Aircraft flight cycles:
6487
Circumstances:
The aircraft was completing a cargo flight from Andijan to Norilsk with an intermediate stop in Omsk, carrying five passengers, seven crew members and a load of 12 tons of fruits. En route from Omsk to Norilsk, the crew was forced to divert to Igarka Airport due to poor weather conditions at destination. Finally, the aircraft departed Igarka on the last leg of the day. Upon arrival at Norilsk, weather conditions were as follow: overcast with clouds down to 100 metres, visibility 2,410 metres, mist, heavy rain falls, OAT 0° and humidity 98%. On short final, after he established a visual contact with the ground, the captain realized that his position was wrong as the airplane was approaching the runway 220 metres from its threshold but 330 metres to the left of its extended centerline. The captain decided to initiate a go-around procedure when the aircraft pitched up to an angle of 16°. With such excessive angle of attack, the aircraft rolled to the left then struck the ground to the left of the runway. It rolled for about 60 metres then took off again. With a nose-up attitude of 14°, the aircraft climbed with a rate of 7 metres per second until the height of 55 metres then stalled again. It rolled to the right by angle of 45° and struck the ground at a speed of 200 km/h before crashing 1,332 metres past the runway end. The copilot and a passenger were seriously injured while 10 other occupants were killed.
Probable cause:
The accident was the consequence of a wrong approach configuration on part of the crew who allowed the aircraft to deviate from the approach glide above the permissible limit. The following contributing factors were reported:
- Unsatisfactory crew interactions during the approach procedure,
- Once the decision altitude was reached, the captain unreasonably left the controls to the copilot,
- The crew decided to continue the descent beyond the minimum decision height without visual contact with the runway/approach lights,
- The decision to initiate a go-around procedure was taken too late,
- The performance level of the crew may have been reduced due to a long shift,
- Poor weather conditions at destination airport.

Crash of a Boeing 737-2A1C in Cruzeiro do Sul: 3 killed

Date & Time: Jun 22, 1992 at 0605 LT
Type of aircraft:
Operator:
Registration:
PP-SND
Flight Type:
Survivors:
No
Schedule:
Rio Branco - Cruzeiro do Sul
MSN:
21188
YOM:
1975
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
4581
Captain / Total hours on type:
3081.00
Copilot / Total flying hours:
2437
Copilot / Total hours on type:
337
Aircraft flight hours:
31980
Circumstances:
While descending to Cruzeiro do Sul Airport by night and good weather conditions, the crew encountered problems with the intermittent activation of a warning light in the instrument panel, warning them of a fire in the cargo compartment. On final approach, the aircraft struck trees and crashed in a dense wooded area located in hilly terrain. The wreckage was found 15 km from runway 10 threshold and all three occupants were killed.
Probable cause:
The following findings were reported:
a. Human Factor
(1) Physiological Aspect
- There was no evidence of this aspect contributing to the occurrence of the accident.
(2) Psychological Aspect - Contributed
- The psychological aspect contributed through the generation of a high level of anxiety to perform the landing and in the diversion of the focus of attention during the approach manoeuvres to land.
- The psychological aspect was influenced by the activation of the smoke alarm which generated an increase in the workload on board.
b. Material Factor
- There were no indications that this factor contributed to the accident.
c. Operational Factor
(1) Deficient Instruction
- Although the instruction was carried out in accordance with what the standards recommend, the failures that contributed to the accident are characteristic of lack of experience in facing abnormalities simultaneously with the maintenance of flight control. Such failures could be avoided with more adequate simulator instructions and training involving the cockpit management aspects.
(2) Poor Maintenance - Undetermined .
- It was not possible to determine the cause of the activation of the 'Aft Cargo Smoke' alarm and whether the maintenance services contributed to this occurrence.
(3) Deficient Cockpit Coordination
- Inadequate performance of the duties assigned to each crew member. The procedures foreseen for the execution of descent by instrument have been modified and some have been deleted depending on the appearance of a complicator element (smoke alarm).
(4) Influence of the environment
- The dark night contributed to the creation of the 'black hole' phenomenon, or 'background figure', making it difficult to perceive external references for a possible identification of the vertical distance of the aircraft from the ground.
(5) Deficient Oversight
- The supervision, at cockpit level, contributed to the accident by the inadequate management of the resources available for the flight in the cockpit.
- Company level supervision contributed to the accident by not identifying the need for cockpit management training and providing it to the crew involved.
- Supervision, at company level, was also inadequate when climbing to the same mission, two pilots unfamiliar with the airplane to be used and in night operation.
(6) Other Operational Aspects
- The failure to comply with several 'Callouts', the non-use of the radio altimeter and the inadequate use of the 'altitude alert', as an aid to the accomplishment of the descent procedure, contributed to the occurrence of the accident.
Final Report:

Crash of a Beechcraft 200 Super King Air in Wilmington: 4 killed

Date & Time: Jun 16, 1992 at 1447 LT
Operator:
Registration:
N32HG
Survivors:
No
Schedule:
Baltimore - Wilmington
MSN:
BB-146
YOM:
1976
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
10378
Captain / Total hours on type:
800.00
Aircraft flight hours:
6718
Circumstances:
Witnesses observed the airplane on a 'normal' final approach, then saw it drop 'low and slow, retract the gear and roll to the left into the trees.' Examination of the engines revealed that the left engine failed because of a fatigue failure of a compressor turbine blade. Examination of the right engine revealed no evidence of malfunction that would have prevented the use of full power. The aircrew was experienced and well trained. The radar data confirmed a drop in airspeed just before the airplane contacted the trees. All four occupants were killed.
Probable cause:
The pilot's improper execution of an emergency procedure, after an engine failure, which resulted in a loss of airspeed and subsequent stall at an altitude too low for recovery. A factor related to the accident was the fatigue failure of a compressor turbine blade and the subsequent engine failure.
Final Report:

Crash of an Antonov AN-32B in Marromeu

Date & Time: Jun 10, 1992 at 0920 LT
Type of aircraft:
Registration:
CCCP-48058
Flight Type:
Survivors:
Yes
Schedule:
Beira - Marromeu
MSN:
28 07
YOM:
1991
Location:
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The aircraft was completing a cargo flight from Beira, carrying a load of foodstuffs. After touchdown, the captain realized he landed on the wrong runway that was only 2,600 feet long but failed to initiate a go-around procedure. Unable to stop within the remaining distance, the aircraft overran and came to rest few dozen metres further. All five occupants were slightly injured and the aircraft was damaged beyond repair.
Probable cause:
The crew mistakenly landed on the wrong runway (too short for such aircraft) and failed to initiate a go-around. It was reported that interferences occurred on frequency during the approach, causing the pilots to misinterpret ATC instructions.

Crash of a Beechcraft C99 Airliner in Anniston: 3 killed

Date & Time: Jun 8, 1992 at 0853 LT
Type of aircraft:
Operator:
Registration:
N118GP
Survivors:
Yes
Schedule:
Atlanta - Anniston - Tuscaloosa
MSN:
U-185
YOM:
1982
Flight number:
8G861
Crew on board:
2
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
1700
Captain / Total hours on type:
24.00
Copilot / Total hours on type:
90
Aircraft flight hours:
9725
Aircraft flight cycles:
11109
Circumstances:
This was the first day on duty in the southern region operation for both pilots. In addition, they had never flown together. During the flight, the flight crew lost awareness of their airplane's position, erroneously believed that the flight was receiving radar services from ATC, and commenced the approach from an excessive altitude and at a cruise airspeed without accomplishing the published procedure specified on the approach chart. The crew believed that the airplane was south of the airport, and turned toward the north to execute the ILS runway 05 approach. In actuality, the airplane had intercepted the back course localizer signal, and the airplane continued a controlled descent until it impacted terrain. The captain and two passengers were killed while the copilot and two other passengers were seriously injured.
Probable cause:
The failure of senior management of GP Express to provide adequate training and operational support for the startup of the southern operation, which resulted in the assignment of an inadequately prepared captain with a relatively inexperienced first officer in revenue passenger service, and the failure of the flightcrew to use approved instrument flight procedures, which resulted in a loss of situational awareness and terrain clearance. Contributing to the causes of the accident was GP Express' failure to provide approach charts to each pilot and to establish stabilized approach criteria. Also contributing were the inadequate crew coordination and a role reversal on the part of the captain and first officer.
Final Report:

Crash of a Casa 212 Aviocar 200 in Mayaguez: 5 killed

Date & Time: Jun 7, 1992 at 1434 LT
Type of aircraft:
Operator:
Registration:
N355CA
Survivors:
No
Schedule:
San Juan - Mayaguez
MSN:
234
YOM:
1982
Flight number:
AA5456
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
6634
Captain / Total hours on type:
2634.00
Aircraft flight hours:
14135
Circumstances:
The airplane crashed on approach 3/4 mile southwest of the airport. A witness heard sound he associated with props going into reverse, then observed airplane emerge from clouds in a nose-low attitude. CVR tape revealed sound of an abrupt change in frequency and amplitude 10 seconds prior to impact. Exam of the left engine beta indicator lamp revealed heavy oxide deposit and stretched coils indicative of the lamp being illuminated at impact; right engine beta lamp was destroyed. Power levers and (beta mode) trigger locks operated normally; trigger return springs intact. Flight idle stops showed no evidence of excessive wear or deformation. The power lever (beta) blocking device lockout solenoid was tested electrically and functioned normally. The rigging of the beta lockout device could not be checked due to impact damage. The operator conducted a funct test of the electrical or backup beta blocking devices on the remaining 8 Casa 212 airplanes; 3 were found to be inoperative. Neither the manufacturing nor operator had an inspection or funct test requirement for the blocking devices. All five occupants were killed.
Probable cause:
The failure of the beta blocking device for undetermined reason(s), and the second-pilot's inadvertent activation of the power lever, or levers, aft of the flight idle position and into the beta range, resulting in a loss of airplane control.
Final Report: