Crash of a Partenavia AP.68TP-100 Victor in Gragnano: 4 killed

Date & Time: Jul 30, 1982 at 1100 LT
Type of aircraft:
Operator:
Registration:
I-RAIP
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Naples - Naples
MSN:
6003
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
The crew consisting of one test pilot, one radio navigator and two engineers departed Naples-Capodichino in the morning on a local test flight. En route, the twin engine airplane suffered a structural failure and the tail detached. Out of control, the aircraft entered a dive and crashed on the slope of a mountain located near Gragnano, about 27 km southeast of Naples. The aircraft was destroyed and all four occupants were killed.
Probable cause:
The exact cause of the accident could not be determined with certainty. However, it is believed that the tail separated as the consequence of in-flight vibrations.

Crash of a Beechcraft C18S in Sheridan

Date & Time: Jul 17, 1982 at 1900 LT
Type of aircraft:
Registration:
N4758N
Flight Type:
Survivors:
Yes
Schedule:
Sheridan - Sheridan
MSN:
8440
YOM:
1945
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4000
Captain / Total hours on type:
500.00
Aircraft flight hours:
4000
Circumstances:
The aircraft was on a functional check flight. According to the pilot and a witness (employed by the pilot), the left brake was locked during touchdown. Subsequently, the aircraft nosed over and a ground fire erupted which destroyed the plane. The pilot reported that the left brake had locked due to rust and corrosion and that the aircraft logbooks were destroyed in the fire. The pilot, sole on board, was uninjured.
Probable cause:
Occurrence #1: nose over
Phase of operation: landing - flare/touchdown
Findings
1. (c) landing gear,normal brake system - corroded
2. (c) maintenance - improper - other maintenance personnel
3. (c) landing gear,normal brake system – locked
Final Report:

Crash of a Dornier DO228-100 near Igenhausen: 3 killed

Date & Time: Mar 26, 1982 at 1800 LT
Type of aircraft:
Operator:
Registration:
D-IFNS
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Oberpfaffenhofen - Oberpfaffenhofen
MSN:
4358
YOM:
1981
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Aircraft flight hours:
210
Aircraft flight cycles:
180
Circumstances:
The twin engine airplane departed Oberpfaffenhofen Airport at 1727LT on a local test flight with one pilot and two inspectors from the UK CAA. The flight was part of the UK Civil Aviation Authority's certification program for the type. En route, the airplane entered a nose-down attitude then dove into the ground and crashed in a wooded area. The aircraft was totally destroyed and all three occupants were killed. The loss of control occurred after the crew selected nose-down trim.

Crash of a Cessna 411 in Brisbane: 5 killed

Date & Time: Jan 5, 1982 at 1201 LT
Type of aircraft:
Operator:
Registration:
VH-AYE
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Brisbane - Brisbane
MSN:
411-0288
YOM:
1969
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
2128
Captain / Total hours on type:
302.00
Aircraft flight hours:
4500
Circumstances:
At 1201 EST, shortly after taking off from Runway 10L at Archerfield Airport, the airplane crashed into an annex attached to a Thiess Contractors workshop located in Kerry Road, Archerfield. The accident site was 455 metres east-north-east from the departure end of the runway. The pilot and four workmen taking their lunch break in the annex were killed. The aircraft and the annex were destroyed by impact forces and the following explosion and fire. The accident occurred during a test flight following corrective maintenance. The aircraft had completed a periodic inspection on 23 December 1981 but, during the next 10 days, a problem was experienced with the control of the left hand propeller. Following maintenance on 4 January to rectify the problem, the pilot elected to test fly the aircraft prior to its intended use for endorsement training at 1500 hours on the day of the accident.
Probable cause:
The cause of the accident was that following a reduction of power from the left engine, the pilot failed to maintain flying speed. The cause of the reduction of power was not determined. The accident may have been avoided if the pilot had employed the correct procedures following a reduction of power from the left hand engine.
Final Report:

Crash of a Piper PA-60 Aerostar (Ted Smith 600) off Sebastian: 2 killed

Date & Time: Dec 8, 1981 at 0911 LT
Operator:
Registration:
N6897X
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Vero Beach - Vero Beach
MSN:
60-8265-005
YOM:
1981
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
8000
Captain / Total hours on type:
6.00
Circumstances:
The crew departed Vero Beach Airport on a local post production test flight. En route, while cruising along the coast, the twin engine airplane entered an uncontrolled descent and crashed in the Atlantic Ocean about 16 miles off shore. Both pilots were killed and the aircraft was destroyed.
Probable cause:
The exact cause of the accident could not be determined.
Final Report:

Crash of a Douglas C-53D-DO Skytrooper in Cali

Date & Time: Aug 3, 1981
Operator:
Registration:
FAC-1128
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Cali - Cali
MSN:
4824
YOM:
1941
Country:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was engaged in a local post maintenance test flight at Cali-Palmaseca Airport. Shortly after takeoff, while in initial climb, one of the engine failed. The captain attempted an emergency landing when the airplane crashed on a farm near the airport. All four occupants were injured while there were no casualties on the ground.
Probable cause:
Engine failure after takeoff for unknown reasons.

Crash of a Cessna 404 Titan in Belton: 1 killed

Date & Time: Jun 30, 1981 at 1125 LT
Type of aircraft:
Operator:
Registration:
N6810N
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Wichita - Wichita
MSN:
404-0853
YOM:
1981
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
6500
Captain / Total hours on type:
500.00
Circumstances:
The pilot, sole on board, departed Wichita on a test flight. En route, the twin engine airplane entered a steep descending turn then crashed in a field located in Belton, south of Kansas City, Missouri. The aircraft was destroyed and the pilot was killed.
Probable cause:
Uncontrolled descent and subsequent crash due to pilot incapacitation. The following contributing factors were reported:
- Moderate obese pilot,
- High blood pressure,
- Witnesses reported pilo looked tired,
- Speech slurred.
Final Report:

Crash of a Mitsubishi MU-2B-10 Marquise near Miami

Date & Time: May 13, 1981 at 1316 LT
Type of aircraft:
Operator:
Registration:
N92JR
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Miami - Miami
MSN:
006
YOM:
1967
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
3260
Captain / Total hours on type:
85.00
Circumstances:
The twin engine airplane was engaged in a local post maintenance test flight at Miami and was carrying one engineer and one pilot. While flying at low height, both engines lost power. The pilot attempted an emergency belly landing in an field. While both occupants escaped uninjured, the aircraft was damaged beyond repair.
Probable cause:
Wheels-up landing due to inadequate preflight preparation. The following contributing factors were reported:
- Mismanagement of fuel,
- Miscalculated fuel consumption,
- Fuel exhaustion,
- Inadequate maintenance and inspection,
- 100 hours inspection in progress,
- Fuel quantity indicating system not calibrated.
Final Report:

Crash of a Cessna 421B Golden Eagle II in Lafayette: 2 killed

Date & Time: Mar 27, 1981 at 1415 LT
Operator:
Registration:
N900E
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Lafayette - Lafayette
MSN:
421B-0359
YOM:
1973
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
2000
Captain / Total hours on type:
68.00
Circumstances:
The twin engine airplane was engaged in a local post maintenance test flight with two pilots on board. After takeoff, while in initial climb, the airplane rolled to the right then became uncontrollable and crashed. Both occupants were killed.
Probable cause:
Uncontrolled collision with ground during initial climb due to inadequate maintenance and inspection. The following contributing factors were reported:
- The pilot-in-command failed to maintain flying speed,
- Engine structure: cylinder assembly, unapproved modification,
- Engine structure: piston, piston rings, wrong parts,
- Engine structure: valve assemblies, leak, over torqued,
- Unfavorable wind conditions with wind gusting up to 40 knots,
- Witness reported smoke from engine.
Final Report:

Crash of a Swearingen SA227TT Merlin IIIC in San Marcos

Date & Time: Mar 24, 1981 at 1100 LT
Operator:
Registration:
N1011R
Flight Type:
Survivors:
Yes
Schedule:
San Marcos - San Marcos
MSN:
T-303E
YOM:
1979
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
7922
Captain / Total hours on type:
112.00
Circumstances:
The crew was completing a local test flight at San Marcos Airport. Following several circuits, the crew initiated a new approach with the copilot at controls. Due to an improper level off, the twin engine airplane landed hard and came to rest. All four occupants escaped uninjured while the aircraft was damaged beyond repair.
Probable cause:
Hard landing caused by an improper level off on part of the pilot at controls and an inadequate supervision of flight on part of the pilot-in-command. This was a manufacturer's test flight with an FAA copilot at controls.
Final Report: