Crash of a Cessna 411 in Middlefield: 5 killed

Date & Time: Apr 18, 1982 at 1759 LT
Type of aircraft:
Operator:
Registration:
N3228R
Flight Type:
Survivors:
No
Schedule:
Middlefield - Middlefield
MSN:
411-0228
YOM:
1966
Crew on board:
2
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
6000
Aircraft flight hours:
2126
Circumstances:
The purpose of the flight was to prepare for a FAA part 135 air taxi check ride which was scheduled later that week. The aircraft was observed during the approach with one engine shut down. During the turn to final the aircraft crashed half a mile from runway 28. All five occupants were killed.
Probable cause:
Occurrence #1: loss of engine power(total) - nonmechanical
Phase of operation: approach - VFR pattern - base leg/base to final
Findings
1. (f) in-flight planning/decision - improper - pilot in command
2. (f) emergency procedure - simulated - pilot in command
----------
Occurrence #2: loss of control - in flight
Phase of operation: approach - VFR pattern - base leg/base to final
Findings
3. (c) planned approach - poor - pilot in command
4. (c) airspeed (VMC) - not maintained - pilot in command
----------
Occurrence #3: in flight collision with terrain/water
Phase of operation: approach - VFR pattern - base leg/base to final
Final Report:

Crash of a Cessna 414A Chancellor in Jackson

Date & Time: Mar 23, 1982 at 0930 LT
Type of aircraft:
Registration:
N37174
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Jackson - Jackson
MSN:
414A-0252
YOM:
1979
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4500
Captain / Total hours on type:
57.00
Circumstances:
At approximately 90 knots after liftoff from a touch-and-go the copilot, who was flying from the left seat, indicated problems with the right engine. The pilot had been observing trucks on the right side of the runway. He stated they could have set it back down except he thought they might swerve into the trucks. He was not specifically looking at the instruments because of the trucks. He took control and the aircraft settled adjacent to the runway and burst into flames. Inspection of the right engine revealed all but one of the 12 spark plugs were sooty. The plugs were installed in a new engine and the engine obtained takeoff rpm.
Probable cause:
Occurrence #1: loss of engine power
Phase of operation: takeoff - initial climb
Findings
1. (c) reason for occurrence undetermined
----------
Occurrence #2: in flight collision with terrain/water
Phase of operation: takeoff - initial climb
Findings
2. (c) flight/navigation instrument(s) - inattentive - pilot in command
Final Report:

Crash of a Boeing KC-135A-BN Stratotanker in Greenwood: 27 killed

Date & Time: Mar 19, 1982 at 2110 LT
Type of aircraft:
Operator:
Registration:
58-0031
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Sawyer - Chicago
MSN:
17776/246
YOM:
1959
Crew on board:
4
Crew fatalities:
Pax on board:
23
Pax fatalities:
Other fatalities:
Total fatalities:
27
Aircraft flight hours:
9249
Circumstances:
The four engine airplane departed Kenneth Ingalls Sawyer AFB on a flight to Chicago-O'Hare Airport, carrying 23 passengers and a crew of four. After being cleared to descend from 22,000 feet to 8,000 feet, the crew reduced his speed when at an altitude of 13,700 feet, at a speed of 313 knots, the airplane suffered an in-flight explosion. Both wings detached, all four engines separated as well as the stabs and out of control, the airplane dove into the ground and crashed in an open field located in Greenwood, about 37 miles northwest of Chicago Airport. The aircraft was totally destroyed and all 27 occupants were killed.
Probable cause:
The exact cause of the accident could not be determined with certainty. Considered as 'most probable' was an over-pressurization under the cargo floor, an area that houses fuel and other potential sources of ignition. An explosion caused by the ignition of accumulated combustible vapors occurring in that area could, in fact, rapidly propagate to adjacent areas where fuel is present. There was also 'strong evidence' of explosive over-pressures in the forward, aft and upper fuel tank areas. Significantly, investigation showed that were the walls or fittings of the rubber bladder cells containing the volatile liquid to fail, fuel or vapor could be released into the tank cavity and in turn migrate to other part of the aircraft.

Crash of a De Havilland DH.104 Dove 1 at Yelahanka AFB

Date & Time: Mar 15, 1982
Type of aircraft:
Operator:
Registration:
HW204
Flight Type:
Survivors:
Yes
Schedule:
Yelahanka - Yelahanka
MSN:
04081
YOM:
1947
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was engaged in a local training flight at Yelahanka Airbase. Control was lost upon landing after the crew attempted to land on one engine. There were no casualties.

Crash of a Boeing KC-135A-BN Stratotanker near Luke AFB: 4 killed

Date & Time: Mar 13, 1982 at 1050 LT
Type of aircraft:
Operator:
Registration:
57-1489
Flight Type:
Survivors:
No
Schedule:
Phoenix - Luke AFB
MSN:
17560/169
YOM:
1958
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
3604
Captain / Total hours on type:
370.00
Aircraft flight hours:
10650
Circumstances:
The KC-135A aircraft departed Phoenix-Sky Harbor International Airport at 0755 MST for a scheduled 3-hour and 30-minute flight. After completing the navigation leg, the aircraft descended into the Phoenix area for transition at Luke AFB. After completing one TACAN approach at Luke AFB, the KC-135A aircraft was vectored to Phoenix-Sky Harbor International Airport for an ILS touch-and-go landing. The aircraft was then vectored back to the final approach course for a TACAN runway 03 left approach at Luke AFB. The KC-135A aircraft was cleared for the approach to Luke AFB, and after the final approach fix radio call, a midair collision occurred with a Grumman American Yankee civilian aircraft. The empennage of the KC-135A separated, rendering the aircraft incapable of flight and it was destroyed upon ground impact. The Grumman American Yankee aircraft was destroyed during the midair collision. The four crew members in the KC-135A and the two civilians in the Grumman American Yankee were fatalities.
Crew:
LT Col James N. Floor,
Lt Col Ted L. Beam,
Maj Truman R. Young Jr.,
T/Sgt Donald J. Plough.
Probable cause:
The USAF KC-135 was on an IFR flight plan and executing a TACAN 03L approach to Luke AFB. The AA-1 had departed Sky Harbour Airport and had been released by phoenix TRSA. The AA-1 was heading westerly in airspace designated as a special traffic area and was required to have been at or below 2,000 ft msl. A pilot of another aircraft who was trailing the AA-1 stated that a low broken cloud cover was encountered and he had to descend to about 2,000 ft to remain 500 ft below the bases. He stated the pilot of the AA-1 did not descend but appeared to be skimming along in and out of the bases of the clouds. He noticed the KC-135 descending through the cloud deck followed immediately by the collision. The collision occurred about 5 mi south of Luke AFB at an altitude of 2,500 ft msl. The logbook of the AA-1 pilot indicated this was his first trip to the phoenix area. Luke AFB was depicted on the north side of the sectional chart only. VOR airway #16 was split along an e-w line with the northern and southern halves being depicted on each side of the chart.

Occurrence #1: midair collision
Phase of operation: cruise - normal
Findings
1. En route charts - inadequate
2. (c) vfr procedures - improper - pilot in command AA-1
3. (f) lack of familiarity with geographic area - pilot in command AA-1
Final Report:

Crash of a Britten-Norman BN-2A-9 Islander in Netheravon AFB

Date & Time: Feb 20, 1982 at 1255 LT
Type of aircraft:
Operator:
Registration:
G-BBRP
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Netheravon - Netheravon
MSN:
371
YOM:
1973
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
3422
Captain / Total hours on type:
235.00
Aircraft flight hours:
5466
Circumstances:
The accident occurred whilst the aircraft was taking off on a parachute dropping flight with the pilot and eight parachutists on board. Shortly after takeoff, at a height of about 50 feet above ground level, the pilot detected a loss of power from the port engine. He then selected the flaps up, but whilst he was about to commence the shut down and propeller feathering drills for the port engine, the starboard engine also appeared to lose power. In the subsequent attempt to land the aircraft straight ahead, the pilot was unable to reduce a high sink rate and a heavy landing resulted. The aircraft sustained severe damage that was beyond economic repair, but there were no injuries to those on board.
Probable cause:
The accident was caused by the fact that the pilot was unable to reduce the aircraft's rate of descent sufficiently to prevent a heavy landing. Contributory factors were the loss of all power from the port engine due to fuel mismanagement and the pilot's decision initially to attempt to continue the take-off.
Final Report:

Crash of an Antonov AN-24RV in Constanţa: 7 killed

Date & Time: Jan 25, 1982
Type of aircraft:
Operator:
Registration:
YR-BMD
Flight Type:
Survivors:
No
Schedule:
Constanţa - Constanţa
MSN:
57310202
YOM:
1975
Country:
Region:
Crew on board:
7
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
7
Circumstances:
The crew arrived at Constanţa-Mihail Kogălniceanu Airport from Bucharest to complete a local training mission. On final approach, at an altitude of about 40 meters, the airplane banked left to an angle of 40° then lost height and crashed, bursting into flames. The aircraft was destroyed and all seven crew members were killed.
Probable cause:
Failure of the feathering system on the left engine which caused the propeller to go to ground pitch while the crew was simulating a failure of the left engine.

Crash of a Douglas C-54E-15-DO Skymaster in Nouméa: 7 killed

Date & Time: Jan 21, 1982 at 2104 LT
Type of aircraft:
Operator:
Registration:
49148/F-YEGA
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Nouméa - Nouméa
MSN:
27374
YOM:
1944
Region:
Crew on board:
7
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
7
Circumstances:
The crew was completing a local training flight at Nouméa-La Tontouta consisting of touch-and-go maneuvers. After takeoff, while climbing by night, the crew initiated a turn when the four engine airplane struck the slope of Mt Kokoreta at an altitude of 1,002 meters and located 10 km east of the airfield. The aircraft was destroyed and all seven crew members were killed.
Crew:
LdV Guy Celton, pilot,
MP Marcel Crusson, copilot,
MP Monroe Podlesnik, mechanic,
1st M Bernard Lefuraut, mechanic,
1st M Claude Wullaert, navigator,
1st M Jean Decoudu, electronics,
M Paul Gavard-Pivet, mechanic.
Probable cause:
It is believed that the accident was the consequence of a controlled flight into terrain consecutive to an error on part of the crew who mistakenly initiated a turn opposite to the published procedures for departure.

Crash of a Douglas DC-3A in Miami

Date & Time: Jan 21, 1982 at 0154 LT
Type of aircraft:
Operator:
Registration:
N211TA
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Opa Locka - Opa Locka
MSN:
6342
YOM:
1942
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
10856
Captain / Total hours on type:
5900.00
Aircraft flight hours:
37721
Circumstances:
During a touch and go the dual student added power rapidly and the left engine sputtered causing the aircraft to swerve left. The instructor took control but felt resistance on the controls from the student. He then reduced power on both engines and the reapplied power at which time he felt both engines come up to power. At this point, the left wing caught scrub trees 90 feet to the left of the runway.
Probable cause:
Non mechanical partial loss of engine power during takeoff due to improper use of the throttle/power control on part of the dual student. The following findings were reported:
- Inadvertent ground loop/swerve,
- Directional control not maintained by dual student,
- Relinquishing of control not performed by dual student,
- Inadequate supervision on part of the pilot-in-command (CFI),
- Ground collision with object,
- Trees.
Final Report:

Crash of a Convair HC-131A Samaritan in Corpus Christi

Date & Time: Jan 18, 1982
Type of aircraft:
Operator:
Registration:
52-5786
Flight Type:
Survivors:
Yes
Schedule:
Corpus Christi - Corpus Christi
MSN:
53-6
YOM:
1954
Crew on board:
8
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was completing a local training flight at Corpus Christi Airport. Following an approach in reduced visibility due to foggy conditions, the airplane landed hard on runway 10R. Upon touchdown, the aircraft went out of control, veered off runway and came to rest. All eight crew members evacuated safely while the aircraft was damaged beyond repair.