Crash of a Swearingen SA227AC Metro III in Twin Falls

Date & Time: Sep 24, 1987 at 2325 LT
Type of aircraft:
Operator:
Registration:
N2689E
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Twin Falls - Twin Falls
MSN:
AC-653
YOM:
1986
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
5800
Captain / Total hours on type:
2000.00
Aircraft flight hours:
774
Circumstances:
Check pilot was conducting captain proficiency check on another company pilot (pic) under dark night conditions. Subsequent to full stop landing on runway 25, takeoff checklist was recited. PIC commenced takeoff on runway 07. Check pilot simulated V1 engine cut after liftoff. PIC was unable to accelerate to V2, climb, or maintain directional control. Aircraft levelled off, air speed began to decay and aircraft drifted to the right. Check captain failed to take control or terminate engine cut simulation as evolution deteriorated. Aircraft collided with ILS glideslope tower marked by red obstruction lights. Loss of control followed when right wingtip/aileron separated. Aircraft then impacted ground and slid to a stop. Takeoff flap position should be 1/4. Both flaps found near 1/2 flap extended position. Handle found in 1/2 flap detent. Performances charts show aircraft able to reach V2 at 50 feet altitude in 6,500 feet roll, then +575 fpm climb (vyse) at acc wt.
Probable cause:
Occurrence #1: loss of engine power
Phase of operation: takeoff - initial climb
Findings
1. (c) preflight planning/preparation - inadequate - pilot in command
2. (c) raising of flaps - not performed
3. (c) checklist - inattentive - pilot in command
4. (f) emergency procedure - simulated - check pilot
5. Proper climb rate - not possible
6. Directional control - not possible
7. (c) supervision - inadequate - check pilot
----------
Occurrence #2: loss of control - in flight
Phase of operation: takeoff - initial climb
Findings
8. (f) object - tower (marked)
9. Wing, wingtip - separation
10. Flight control, aileron - loss, partial
----------
Occurrence #3: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Final Report:

Crash of a Let L-410MU in Yakutsk

Date & Time: Sep 24, 1987 at 2016 LT
Type of aircraft:
Operator:
Registration:
CCCP-67249
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Yakutsk - Yakutsk
MSN:
77 08 15
YOM:
1977
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew (two student pilots and one instructor) was completing a local training flight at Yakutsk-Magan Airport. Ready for takeoff, the crew increased engine power to 85% then released the brakes. After a course of less than 20 meters, the airplane 'sank' on its left after the brakes block of the left main gear broke off. Takeoff procedure was abandoned and the aircraft stopped on its left side and was damaged beyond repair. All three occupants escaped uninjured.

Crash of an Airbus A300B4-203 in Luxor: 5 killed

Date & Time: Sep 21, 1987 at 0903 LT
Type of aircraft:
Operator:
Registration:
SU-BCA
Flight Type:
Survivors:
No
Schedule:
Luxor - Luxor
MSN:
115
YOM:
1980
Location:
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
5
Aircraft flight hours:
20600
Aircraft flight cycles:
9200
Circumstances:
The crew was completing a local training flight at Luxor Airport, consisting of touch-and-go maneuvers. Following a wrong approach configuration, the pilot-in-command landed too far down the runway, about 700 meters past the runway threshold and to the right of the centerline. After touchdown, the right main gear struck runway lights. Unable to stop within the remaining distance, the aircraft overran, collided with the localizer antenna, went through a fence and came to rest, bursting into flames. The aircraft was destroyed and all five occupants were killed.
Probable cause:
Wrong approach configuration.

Crash of a Piper PA-31T-620 Cheyenne II in Munich: 9 killed

Date & Time: Aug 11, 1987 at 1528 LT
Type of aircraft:
Registration:
D-ILRA
Flight Type:
Survivors:
No
Site:
Schedule:
Landsberg - Munich
MSN:
31-8020009
YOM:
1980
Location:
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
9
Circumstances:
The twin engine aircraft departed Landsberg-Penzing Airport on a training flight to Munich, carrying one passenger (a secretary of the Southern Bavarian Air Office), one instructor and one pilot. On final approach to Munich-Riem Airport runway 07, at an altitude of 200 feet, the instructor decided to reduce the power on the right engine while the pilot was expecting to initiate a go-around procedure according to the training program. He elected to add power on the left engine but the aircraft lost height, struck the roof of a McDonald's restaurant located in the district of Trudering and eventually crashed in flames on a bus. The aircraft, the restaurant, the bus and several other vehicles were destroyed and seven people were killed, all three occupants in the aircraft and four passengers in the bus. Few days later, two other victims died from their injuries. 30 other people were injured, some of them seriously.
Probable cause:
It was determined that the instructor's decision to reduce power was taken at a critical stage of flight because the aircraft was approaching at a too low altitude of 200 feet and flying vertical to a populated area. Also, the pilot was expecting to initiate a go-around according to the training program.

Crash of a Rockwell Aero Commander 520 in Addison

Date & Time: Jul 27, 1987 at 1101 LT
Registration:
N4164B
Flight Type:
Survivors:
Yes
Schedule:
Addison - Addison
MSN:
520-69
YOM:
1953
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
1176
Captain / Total hours on type:
206.00
Aircraft flight hours:
1920
Circumstances:
Aircraft was destroyed when it struck power lines and the ground during a single engine go-around. Following a left engine shut down due to severe vibrations, the pilot overflew one airport to return to his home base. En route, he elected not to go to full power due to a 3 minutes limitation he did not want to exceed. The pilot overshot the runway while manually extending the nose gear and elected to attempt a right 270° turn to return to final while at 100-150 feet agl. Nose landing did not extend due to hydraulic pump being on left engine and no pressure. During the turn, the pilot lost control and the aircraft struck the wires. Investigation revealed that one of the blade pitch change links on the left prop had disconnected, allowing one blade to free float. The link pin assembly had backed out as a result of the safety screw backing out due to damaged and stripped threads and an improper length screw being installed. Props had 1/4' safety screws installed instead of 3/8'.
Probable cause:
Occurrence #1: airframe/component/system failure/malfunction
Phase of operation: cruise - normal
Findings
1. (c) propeller system/accessories, pitch change mech - disconnected
2. Propeller feathering - not possible
3. (c) propeller system/accessories, pitch change mech - stripped thread
4. (c) maintenance, overhaul - inadequate - other maintenance personnel
5. (c) propeller system/accessories, pitch change mech - incorrect
6. (c) maintenance, installation - improper - pilot in command
7. Emergency procedure - improper - pilot in command
----------
Occurrence #2: forced landing
Phase of operation: descent - emergency
----------
Occurrence #3: loss of control - in flight
Phase of operation: go-around (vfr)
Findings
8. (f) go-around - attempted - pilot in command
9. (c) airspeed (vmc) - not maintained - pilot in command
10. (c) diverted attention - pilot in command
----------
Occurrence #4: in flight collision with object
Phase of operation: descent - uncontrolled
Findings
11. Object - wire, transmission
Final Report:

Crash of a Canadian Vickers PBV-1A Canso in Lac-Caché: 1 killed

Date & Time: Jul 18, 1987
Registration:
C-FPQP
Flight Type:
Survivors:
Yes
Schedule:
Lac-Caché - Lac-Caché
MSN:
CV-407
YOM:
1944
Flight number:
Tanker 16
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
The crew was completing a training mission at Lac-Caché, consisting of touch-and-go and scooping maneuvers. For unknown reasons, the seaplane landed hard, overturned and sank. One pilot was killed and the second was injured.

Crash of a Beriev BE-12 in Lake Donuzlav

Date & Time: Jun 17, 1987
Type of aircraft:
Operator:
Registration:
16
Flight Type:
Survivors:
Yes
MSN:
8 6 012 02
YOM:
1968
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was completing a training mission on Lake Donuzlav. The seaplane landed hard, bounced then came to rest and sank. All four crew members were rescued.

Crash of a Cessna T303 Crusader near Saga: 4 killed

Date & Time: May 15, 1987 at 0952 LT
Type of aircraft:
Operator:
Registration:
JA5277
Flight Phase:
Flight Type:
Survivors:
No
Site:
MSN:
303-00279
YOM:
1984
Location:
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
4419
Captain / Total hours on type:
1072.00
Copilot / Total flying hours:
3186
Copilot / Total hours on type:
843
Circumstances:
Three student pilots and one instructor were on board this Crusader to complete a training mission. While in cruising altitude under VFR mode over the north part of the Ariake Sea, the pilot-in-command lost control of the aircraft that entered a dive and crashed 3,6 km south of the Suminoe harbor. The aircraft disintegrated on impact and all four occupants were killed.
Probable cause:
It is believed that the loss of control occurred during a VFR training flight while the crew was performing emergency procedures. The crew was unable to recover the aircraft.
Final Report:

Crash of a Learjet 35A in Pittsburgh: 2 killed

Date & Time: May 12, 1987 at 1057 LT
Type of aircraft:
Operator:
Registration:
N100EP
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Pittsburgh - Teterboro
MSN:
35-150
YOM:
1978
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
10211
Captain / Total hours on type:
3838.00
Aircraft flight hours:
4203
Circumstances:
The copilot (dual student) was to get a prof check on the 1st leg of the flight with a simulated single engine power loss on takeoff. According to witnesses, the takeoff was normal until lift off approximately 3,200 feet down the runway; but after lift-off, the aircraft climbed only about 50 feet and didn't seem to accelerate. They reported the nose pitched up and the aircraft went in a steep bank attitude near the departure end of the runway. Subsequently, it descended and crashed in wooded terrain in a right wing down, nose high attitude. A bystander tried to get in the aircraft to rescue the pilots, but the door was jammed and he was unable to break the cabin windows. A fire erupted and engulfed the aircraft. Due to rough terrain, there was a delay in getting fire fighting equipment to the accident site. No preimpact mechanical failures were found. The gear, flaps and spoilers were found in the retracted position. For takeoff, the flaps should have been extended to the 8° or 20° position. The stall speeds for 20°, 8° and no flaps were 104.5, 109.0 and 119.5 knots, respectively. The captain was an FAA designated flight examiner and a certified flight instructor (cfi).
Probable cause:
Occurrence #1: loss of control - in flight
Phase of operation: takeoff - initial climb
Findings
1. Emergency procedure - simulated - pilot in command (cfi)
2. (c) raising of flaps - premature - copilot/second pilot
3. (c) airspeed - inadequate
4. (c) stall - inadvertent
5. (c) supervision - inadequate - pilot in command (cfi)
----------
Occurrence #2: in flight collision with terrain/water
Phase of operation: takeoff
Final Report:

Crash of a Beechcraft 200 Super King Air in Johannesburg: 3 killed

Date & Time: Apr 13, 1987
Operator:
Registration:
ZS-KMT
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Johannesburg - Johannesburg
MSN:
BB-767
YOM:
1981
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
The crew (two instructeurs and three student pilots) departed Johannesburg-Rand Airport for a local training flight. After takeoff, while in initial climb, an instructor simulated an engine failure. The aircraft stalled and crashed on dorms located near the airport and dedicated to the Germiston Mining employees. Three crew members were killed while two others were injured. There were no casualties on the ground.