Crash of a Fokker F27 Friendship 500 near Rodez: 5 killed

Date & Time: Jan 28, 1979 at 1726 LT
Type of aircraft:
Operator:
Registration:
F-BYAH
Flight Type:
Survivors:
Yes
Site:
Schedule:
Rodez - Rodez
MSN:
10570
YOM:
1978
Location:
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
6367
Captain / Total hours on type:
1021.00
Copilot / Total flying hours:
1991
Copilot / Total hours on type:
1178
Aircraft flight hours:
1704
Aircraft flight cycles:
1366
Circumstances:
The crew departed Rodez-Marcillac Airport at 1715LT on a local test flight following a two-month maintenance period after the aircraft was suffering vibrations during preceding flights. On board were two pilots of Air Rouergue, two engineers from the same operator, a Fokker technician and one pilot from Air Alpes. The test program was short, about 15 minutes, with two circuits planned at an altitude of 7,000 feet over the Rodez beacon. On approach to runway 31, the crew was supposed to complete a level off at 4,400 feet QNH but continued the descent until the airplane struck a mountain shrouded in clouds and located about 17 km from the airport. One of the passenger was seriously injured while five other occupants were killed.
Probable cause:
Failure of the crew to level off at the prescribed altitude either due to inadequate monitoring when passing through 4,400 feet or an altimeter setting error by confusion between QNH and QFE. Other factors were a lack of flight preparation; non use of the radio altimeter and a possible CofG outside limits affecting the longitudinal maneuverability. Also, no approach card was evident in the cockpit for this aerodrome and the presence of an additional person on the flight deck may have distracted the crew.
Final Report:

Ground accident of a Lockheed C-130H Hercules in Milan

Date & Time: Jan 23, 1979
Type of aircraft:
Operator:
Registration:
MM62000
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
4497
YOM:
1973
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Technicians were engaged in ground tests at Malpensa Airport. While parked on the ramp, an engine run-up was initiated when the airplane jumped over the chocks and eventually struck obstacles and came to rest. There were no injuries.

Crash of a Grumman G-21A Goose off Christiansted

Date & Time: Nov 5, 1978 at 0939 LT
Type of aircraft:
Operator:
Registration:
N74676
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Christiansted - Christiansted
MSN:
1172
YOM:
1942
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
8943
Captain / Total hours on type:
443.00
Circumstances:
The seaplane was engaged in a test flight out from Christiansted on behalf of the FAA. While flying off Christiansted, the pilot encountered engine problems and decided to ditch the aircraft few miles offshore. All three occupants were rescued while the aircraft was damaged beyond repair.
Probable cause:
Ditching following a double engine failure after the pilot attempted operation with known deficiens in equipment. The following contributing factors were reported:
- Improper in-flight decisions,
- Attempted operation beyond experience/ability level,
- Failure of both engines,
- Aircraft came to rest in water,
- 25 rpm flux reported on left engine previous three days of flight,
- 200 rpm during climbout and continued flight.
Final Report:

Crash of a Cessna 421B Golden Eagle II in Stansted: 1 killed

Date & Time: Sep 4, 1978 at 1518 LT
Operator:
Registration:
G-AYMM
Flight Type:
Survivors:
Yes
Schedule:
Cambridge - Stansted
MSN:
421B-0033
YOM:
1970
Location:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
3113
Captain / Total hours on type:
1401.00
Aircraft flight hours:
2472
Circumstances:
The aircraft was engaged upon a flight test for the renewal of its Certificate of Airworthiness (CofA). The sole occupants were the pilot and an observer. Following an ILS approach to runway 23 at Stansted Airport an overshoot (go-around) was initiated and at about 200 feet the starboard engine cut out. The commander attempted unsuccessfully to restart the engine by use of the starter motor. The aircraft lost speed and height and crashed just outside the airport. The observer was killed and the pilot injured.
Probable cause:
The accident was caused by the pilot failing to feather the propeller and raise the flaps after the starboard engine had cut during an overshoot manoeuvre. A contributory factor is considered to have been the absence of any prescribed procedure in the Flight Manual to meet this eventuality. The reason for the malfunction of the starboard engine both during the stall test and later during the overshoot could not be determined.
Final Report:

Crash of a Piper PA-31-350 Navajo Chieftain in Mena

Date & Time: Jul 12, 1978 at 1015 LT
Registration:
N404RC
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Mena - Mena
MSN:
31-7552060
YOM:
1975
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
3815
Captain / Total hours on type:
125.00
Circumstances:
The pilot, sole on board, was performing a local test flight at Mena Airport. During initial climb, one of the engine failed. He elected to return but misjudged his altitude and clearance when the airplane struck trees and crashed near the airport. The aircraft was destroyed and the pilot was injured.
Probable cause:
Powerplant failure for undetermined reasons. The following findings were reported:
- Misjudged altitude and clearance,
- High obstructions,
- Complete engine failure,
- Forced landing of airport on land.
Final Report:

Crash of a Fairchild C-119G Flying Boxcar in Greybull: 3 killed

Date & Time: Jun 10, 1978 at 1700 LT
Operator:
Registration:
N3560
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Greybull - Greybull
MSN:
10957
YOM:
1952
Flight number:
Tanker 140
Crew on board:
3
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
4250
Captain / Total hours on type:
400.00
Circumstances:
The aircraft was engaged in a local test flight at Greybull Airport and was carrying one passenger and three crew members. After takeoff, while climbing, the crew encountered technical problems with the right engine. The captain elected to return and initiated a turn when the aircraft lost height and crashed. All three crew members were killed while the passenger was seriously injured.
Probable cause:
The exact cause of the accident could not be determined.
Final Report:

Crash of a Tupolev TU-144D in Kladkovo: 2 killed

Date & Time: May 23, 1978 at 1855 LT
Type of aircraft:
Operator:
Registration:
CCCP-77111
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Ramenskoye - Ramenskoye
MSN:
10 06 2
YOM:
1978
Country:
Region:
Crew on board:
8
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Aircraft flight hours:
9
Aircraft flight cycles:
5
Circumstances:
Built by the Voronezh Aircraft Factory, the airplane came out of the plant last April 27. Test flights were conducted on April 27, May 12, 16 and 18. On May 23, the crew completed a fifth test flight from 1111LT and 1307LT without any incidents. At 1730LT, the crew departed Ramenskoye Airport near Moscow to proceed to a series of various tests on engines, generators, to evaluate the airtightness of the cabin as well as the stability and the controllability of the aircraft at an altitude of 12,000 meters. When all these checks were completed, the crew reduced his altitude to 3,000 meters then carried out the test of the auxiliary power unit (APU). For the next two minutes, engines n°3 and 4 were shut down in accordance with the test program. About a minute after the shutdown of the engine n°4, a burning smell was felt in the cabin and smoke spread through the air conditioning system, followed by a black and thick smoke. The captain decided to return to his departure point but quickly realized that this would be impossible. He reduced his altitude and attempted an emergency landing in a pasture. At a speed of 380 km/h, at an estimated height of four to six meters, the airplane struck and cut between 70 and 100 trees before falling to the ground. It then slid for about 620 meters before coming to rest in flames, some 46 kilometers southeast of Ramenskoye runway 30 threshold. Six crew members were rescued while two engineers were killed.
Probable cause:
According to the investigating committee, a fuel line broke up 27 minutes before engine start. This allowed eight tons of fuel to leak into several compartments of the right wing and a fire erupted when the auxiliary power unit was triggered. All various analysis carried out by investigators did not make it possible to determine precisely the causes of the fuel leakage by the fact that all the incriminated components were totally destroyed by a post crash fire. However, experts believe that it is likely that the leak would be the result of the failure of a fuel system hose connected to the engine n°1.

Crash of a Beechcraft 65-88 Queen Air in Camarillo: 3 killed

Date & Time: Aug 25, 1977 at 1600 LT
Type of aircraft:
Operator:
Registration:
N711KW
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Van Nuys - Van Nuys
MSN:
LP-38
YOM:
1966
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
5610
Captain / Total hours on type:
30.00
Circumstances:
The crew departed Van Nuys for a local test flight. En route, a fire erupted in the left wheel well and spread to the left wing that detached in flight. Out of control, the airplane entered a dive and crashed in flames. All three occupants were killed.
Probable cause:
In-flight fire during normal cruise for undetermined reasons. The following findings were reported:
- Fire in brakes, wheel assembly, wheel well,
- Fire in wing,
- Separation in flight,
- In-flight loss of left wing,
- Severe fire in left wheel well aft of left engine firewall, source undetermined.
Final Report:

Crash of a Let 410 in Uherské Hradiště: 4 killed

Date & Time: Jul 7, 1977
Type of aircraft:
Operator:
Registration:
OK-162
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
d’Uherské Hradiště - d’Uherské Hradiště
MSN:
X03
YOM:
1970
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
The crew (two pilots and two technicians) departed d’Uherské Hradiště-Kunovice Airport for a local test flight on this third L-410 prototype. While cruising at a relative low altitude, the pilot-in-command lost control of the airplane that dove into the ground and crashed in a field located in Nedakonice, few km from the airfield. The aircraft was destroyed and all four occupants were killed.
Probable cause:
It is believed that the loss of control occurred when the tail separated in flight after severe actions were performed on the rudder by the pilot.

Crash of a PZL-Mielec AN-2TP in Chokurdakh: 1 killed

Date & Time: Mar 6, 1977 at 1530 LT
Type of aircraft:
Operator:
Registration:
CCCP-40572
Flight Phase:
Flight Type:
Survivors:
No
MSN:
1G84-25
YOM:
1967
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Aircraft flight hours:
7735
Aircraft flight cycles:
7673
Circumstances:
In the morning, the crew completed two flights in the area. Due to engine problems, a technician was asked to make some engine test run. While the aircraft was parked on the ground, a technician proceeded to an engine test but forgot to install chocks on wheels. After the engine was started, power was added. The pilot who was standing by the door fell out of the plane that started to roll. After takeoff, the airplane climbed to a height of 12 meters, made a sharp turn to the left, stalled and crashed upside down. The technician, sole on board, was killed. It was determined that when the airplane started to roll quite roughly, the technician fell down from the pilot seat. Then, after liftoff, the cargo shifted to the rear of the cabin, causing the aircraft to stall.
Probable cause:
The technician in charge to proceed to an engine test started the engine and added full power without preparing the airplane properly and installing chocks on wheels prior to the test. The aircraft then moved roughly and became uncontrollable.