Ground accident of a Boeing 727-90C in Anchorage

Date & Time: Jun 9, 1987 at 0855 LT
Type of aircraft:
Operator:
Registration:
N766AS
Flight Phase:
Survivors:
Yes
MSN:
19728
YOM:
1968
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Aircraft flight hours:
49937
Circumstances:
The mechanic in charge of taxiing the Boeing 727 allowed an unauthorized avionics technician to occupy the pilot seat. They inadvertently deactivated the brake pressurization system and struck a passenger jetway at the terminal gate. An ensuing fire destroyed the airplane and a company ground vehicle and extensively damaged the jetway. The terminal gate was also damaged. A total of 11 persons were injured.
Probable cause:
Occurrence #1: on ground/water collision with object
Phase of operation: taxi
Findings
1. Object - airport facility
2. (c) brakes (normal) - inadvertent deactivation - company maintenance personnel
3. (f) planning/decision - inadequate - company maintenance personnel
4. (c) checklist - not used - company maintenance personnel
----------
Occurrence #2: fire
Phase of operation: other
Final Report:

Crash of a Britten-Norman BN-2A-22 Islander near Canaima: 10 killed

Date & Time: Jun 5, 1987
Type of aircraft:
Operator:
Registration:
YV-230C
Flight Phase:
Survivors:
No
Site:
MSN:
19
YOM:
1968
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
9
Pax fatalities:
Other fatalities:
Total fatalities:
10
Circumstances:
While cruising in poor weather conditions, the twin engine aircraft struck the slope of a mountain located in the region of Canaima. All 10 occupants were killed, among them nine tourists.

Crash of a PZL-Mielec AN-2R in Troitsko-Pechorsk

Date & Time: May 31, 1987
Type of aircraft:
Operator:
Registration:
CCCP-70814
Flight Phase:
MSN:
1G133-17
YOM:
1971
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
At takeoff, the engine failed and the aircraft crashed. Occupant fate unknown.
Probable cause:
It was determined that dry grass got stuck in the air intake, causing the engine to fail at takeoff.

Crash of a BAe 3101 Jetstream 31 in New Orleans

Date & Time: May 26, 1987 at 1645 LT
Type of aircraft:
Operator:
Registration:
N331CY
Flight Phase:
Survivors:
Yes
Schedule:
New Orleans - Valparaiso
MSN:
742
YOM:
1987
Flight number:
CO962
Crew on board:
2
Crew fatalities:
Pax on board:
9
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
7500
Captain / Total hours on type:
60.00
Copilot / Total flying hours:
3000
Copilot / Total hours on type:
18
Aircraft flight hours:
147
Circumstances:
Taxi clearance was received at 16:35 and the flight left gate 14B for runway 19. The airplane was cleared for takeoff at 16:44. Shortly after lifting off, at 200 feet above the ground, the engine torque gauges began to fluctuate erratically and the plane began to yaw back and forth. The captain believed the TTL (Torque Temperature Limiting) system may have been bypassing fuel to the engines (a situation that could occur when power levers are advanced too far forward). He then slightly decreased the power settings which resulted in even greater torque oscillations and greater yawing. The captain believed both engines were malfunctioning for some unknown reason and landed back on runway 19, because a 90° turn for runway 28 seemed impossible. The aircraft overran the runway, struck a 6 feet high chain link fence, struck a concrete barrier and skidded across the Route 61 highway before coming to rest on a parking lot.
Probable cause:
A breakdown of the flight crew coordination which resulted in their failure to comply with the Before Takeoff Checklist and advance the RPM levers to the high RPM position, and the flight crew's failure to diagnose and remedy engine oscillations on initial climbout. Contributing to the flight crew's failure to advance the RPM levers before take off was the fact that both crew members had limited experience in the BAe-3101 and extensive recent experience in other aircraft which use RPM control lever procedures that are different from the BAe-3101."
Final Report:

Crash of a De Havilland DHC-6 Twin Otter 300 in Ruteng: 8 killed

Date & Time: May 23, 1987
Operator:
Registration:
PK-NUW
Survivors:
No
MSN:
474
YOM:
1975
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
8
Circumstances:
On final approach in poor weather conditions, the aircraft struck trees, stalled and crashed in the jungle few km from the airport. All eight occupants were killed.

Crash of an Ilyushin II-62 in Warsaw: 183 killed

Date & Time: May 9, 1987 at 1112 LT
Type of aircraft:
Operator:
Registration:
SP-LBG
Survivors:
No
Schedule:
Warsaw - New York
MSN:
3344942
YOM:
1973
Flight number:
LO5055
Country:
Region:
Crew on board:
11
Crew fatalities:
Pax on board:
172
Pax fatalities:
Other fatalities:
Total fatalities:
183
Captain / Total flying hours:
19745
Captain / Total hours on type:
5546.00
Copilot / Total flying hours:
10957
Copilot / Total hours on type:
1966
Aircraft flight hours:
6972
Aircraft flight cycles:
1752
Circumstances:
At 10:18 flight LO5055 took off from Warsaw runway 33 for a flight to New York-JFK. The aircraft headed for the GRU VOR, which it passed at FL265, climbing to FL310. Two minutes later (at 10:41) the n°2 engine Low Pressure turbine shaft broke loose, followed by the failure of the turbine disc. Debris punctured the aft fuselage, causing a fire in the cargo hold. The elevator control system was severed and the n°1 engine had to be shut down. The flight crew immediately started an emergency descent to 4,000 metres. After shutting down both n°1 and n°2 engine the crew mistakenly thought the fire was extinguished. They had decided to land at Modlin airport, but still unaware of the fire, changed to Warsaw-Okecie runway 33 because of better rescue equipment there. The flight started a left turn for runway 33 at 11:09 at an altitude of 1,450 metres and an airspeed of 480 km/h. The crew lost control during the turn and the Il-62 crashed into a forest, 6 km from the runway at an airspeed of 465 km/h and an 11° left bank and 12° nosedown. The aircraft disintegrated on impact and all 183 occupants were killed.
Probable cause:
The cause of the accident was the destruction of engine no.2 resulting in disconnection of the longitudinal control system from the control column, cabin depressurisation, damage to the electric system and fire. At the end stage of flight the fire caused the loss of the aircraft longitudinal control and the impact with the ground after 31 minutes as counted from the beginning of the emergency situation. The destruction of engine no.2 occurred without any signal from the warning/testing system. Under the circumstances the crew members were not able to stop the engine in good time, consequently an emergency situation was created on board the aircraft.

Crash of a Casa 212 Aviocar 200 in Mayaguez: 2 killed

Date & Time: May 8, 1987 at 0650 LT
Type of aircraft:
Operator:
Registration:
N432CA
Survivors:
Yes
Schedule:
San Juan - Mayaguez
MSN:
271
YOM:
1982
Flight number:
AA5452
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
9802
Captain / Total hours on type:
473.00
Copilot / Total flying hours:
4473
Copilot / Total hours on type:
459
Aircraft flight hours:
6264
Aircraft flight cycles:
11774
Circumstances:
On May 8, 1987, flight 5452, a commuter flight regularly scheduled to depart from San Juan, Puerto Rico, at 0615 local time, for a flight to Mayaguez, Puerto Rico, departed at 0620 with four passengers and two crewmembers. The captain was 15 minutes late when he arrived for the flight at 0600. The first officer arrived on time at 0545. The airplane, a CASA C-212~CC, was operated by Executive Air Charter, Inc., doing business as American Eagle. The flight was on a visual flight rules flight plan, and communications with the flight en route were reported to have been routine. The first officer handled the initial radio communications, and the captain made subsequent radio communications. While in the vicinity of Mayaguez, the captain cancelled the flight plan and proceeded to make a visual approach to runway 9. The captain did not make the customary in-range call to the operations agent at Mayaguez to report the flight’s arrival estimate and fuel requirements. Witnesses who observed the airplane on its downwind leg reported that it appeared normal. One witness said the airplane seemed too fast on the approach and appeared to overshoot the extended centerline on the baseleg turn to final. Another said the airplane “turned tighter” and did not extend the downwind leg as normal. He said as the airplane came toward him, the nose rose up quickly and then the airplane rolled to the right and nosed over. A third witness said the airplane made a violent turn, and he thought the engine noise was louder than normal. A fourth confirmed that the airplane made a shortened downwind leg, making a continuous left turn and sinking fast. He said that it turned rapidly to the right and nosed down and struck the ground. He then saw it pivot around and slide backwards. He stated that fire began when the right wing and engine separated from the airplane. A fifth witness, a company baggage handler, said he heard an explosion and saw flames come out of the right engine before it turned twice and struck the ground. A crop duster pilot reported that everything appeared normal until the airplane was about 1,000 feet from the runway and about 100 feet above the ground. He said at that point, he heard a sound similar to that of a turbo propeller airplane going into reverse pitch to slow down after landing. He said the airplane then yawed to the right, followed by a roll to the left, as if the pilot had attempted to counteract the yaw. The airplane then rolled back to the right and the right wing tip struck the ground. A fire erupted immediately, the airplane turned about 1800, and it came to rest upright. The four passengers on board reported that the flight was routine until the approach into Mayaguez. One passenger seated in 3A noticed that the noise from the engines was lower than usual and that it was not the normal engine sound. He thought afterward that perhaps an engine had stopped and that the noise was different on the right. He said the airplane was not shaking or vibrating. A second passenger seated in 4C reported that the airplane lost altitude abruptly and that it fell rapidly as it banked to the left on the approach. He said he heard strange sounds from the left side and that it was an engine or scraping noise. He stated that he saw a 1 l/2- to 2-foot long flame come from the left engine, but that it did not appear to be spreading. He reported that the airplane jerked before it hit the ground. The third passenger, seated in 6A, reported that she heard an unusual metallic sound similar to a landing gear retracting or extending immediately before the crash. The fourth passenger in seat 78 was asleep and did not awaken until the crash. He said that he thought the airplane made a hard or gear-up landing.
Probable cause:
Improper maintenance in setting propeller flight idle blade angle and engine fuel flow resulting in a loss of control from an asymmetric power condition. A factor contributing to the accident was the pilot's unstabilized visual approach.
Final Report:

Crash of an Avro 748-243-2 in Chiang Rai

Date & Time: Apr 28, 1987 at 1005 LT
Type of aircraft:
Operator:
Registration:
HS-THI
Survivors:
Yes
Schedule:
Chiang Mai - Chiang Rai
MSN:
1708
YOM:
1971
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
39
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Following an uneventful flight from Chiang Mai, the crew initiated the approach to Chiang Rai Airport in good weather conditions. The copilot was the pilot-in-command when the aircraft completed a gear up landing. It slid on runway for about 1,075 meters before coming to rest on the runway. All 43 occupants escaped uninjured while the aircraft was damaged beyond repair.
Probable cause:
It was determined that the crew failed to extend the landing gear on approach. The following contributing factors were reported:
- The crew failed to follow the approach checklist,
- Lack of crew coordination,
- The captain failed to supervise properly the copilot's actions.

Crash of a PZL-Mielec AN-2 in Smyshliayevka

Date & Time: Apr 24, 1987
Type of aircraft:
Operator:
Registration:
CCCP-17879
Flight Phase:
Survivors:
Yes
MSN:
1G205-20
YOM:
1983
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed after the crew got distracted in flight. There were no casualties.