Crash of a Cessna 207 Skywagon on Sitkinak Island

Date & Time:
Operator:
Registration:
N91117
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Sitkinak Island - Kodiak
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
1360
Captain / Total hours on type:
70.00
Circumstances:
Just after liftoff from Sitkinak Island Airport, while in initial climb, the airplane stalled and crashed at the edge of the runway. The pilot was seriously injured and the aircraft was written off.
Probable cause:
The pilot-in-command failed to obtain/maintain flying speed and failed to follow the approved procedures. The following factors were reported:
- Unfavorable winds conditions,
- Pilot attempted max performance takeoff in Robertson STOL aircraft,
- Quartering crosswind at 20 knots.
Final Report:

Crash of a Rockwell Aero Commander 500S Shire Commander in White Castle: 2 killed

Date & Time:
Operator:
Registration:
N9119N
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Patterson - Baton Rouge
MSN:
500-3087
YOM:
1970
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
1355
Captain / Total hours on type:
110.00
Circumstances:
The twin engine aircraft was flying at low height and low speed when control was lost. It crashed in an open field located in White Castle, killing both occupants.
Probable cause:
The pilot failed to obtain/maintain flying speed. Unwarranted low flying. Observers saw the aircraft at altitude too low for recovery.
Final Report:

Crash of a Douglas R4D-6 in Anchorage: 2 killed

Date & Time:
Type of aircraft:
Operator:
Registration:
N47
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Anchorage - Anchorage
MSN:
16407/33155
YOM:
1945
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
10401
Captain / Total hours on type:
5000.00
Circumstances:
The crew was engaged in a local training flight. After takeoff from runway 24, while in initiale climb, the airplane suffered two consecutive stalls then banked left and right. It lost height and crashed in a huge explosion, killing both pilots.
Probable cause:
The crew failed to obtain/maintain flying speed and inadequate supervision of flight on part of the pilot-in-command. When control was lost, gear was down, flaps were 3/4 down and the rudder trim was positioned full left. The aircraft was observed entering three stalls, two stalls normal recovery.
Final Report:

Ground collision of a Beechcraft E18S in Keokuk

Date & Time:
Type of aircraft:
Registration:
N29W
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Keokuk – Detroit
MSN:
BA-107
YOM:
1955
Location:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4128
Captain / Total hours on type:
600.00
Circumstances:
The crew was preparing the aircraft for a cargo flight to Detroit. On ground, the crew proceeded to an instruments check and started both engines without making an external visual check. A private Cessna 337 just landed and its pilot was taxiing to the parking when the Beechcraft moved and collided with the Cessna. Both aircraft caught fire and all three occupants were seriously injured.
Probable cause:
The crew started the engine without proper assistance and his attention was diverted from operation of the aircraft at that time. The following contributing factors were reported:
- The crew was preoccupied by cockpit check,
- Neither aircraft was chocked for engine start,
- No line personnel was available.
Final Report:

Crash of a Douglas DC-8-62 in New York

Date & Time:
Type of aircraft:
Operator:
Registration:
I-DIWZ
Survivors:
Yes
Schedule:
Rome - New York
MSN:
46026/452
YOM:
1969
Flight number:
AZ618
Crew on board:
10
Crew fatalities:
Pax on board:
146
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
13310
Captain / Total hours on type:
1362.00
Copilot / Total flying hours:
8114
Copilot / Total hours on type:
247
Circumstances:
Alitalia Flight 618 departed Rome at 10:22 local time for a non-stop flight to New York. The en route and descent were normal. After having descended to 6000 feet, the crew listed to the ATIS: "The seventeen hundred zulu weather Kennedy six hundred scattered measured ceiling eight hundred overcast four miles fog the winds are two one zero degrees at three and the altimeter three zero one five temperature seventy three expect ILS four right approach landing runway four right. Notice to Airmen glide slope out of service.". About this point in the flight, the first officer, at the request of the captain, took over the flight controls. He disengaged the autopilot and proceeded to comply with the various vectors provided by the approach controller. At 13:07 the controller instructed the flight to increase airspeed from 210 knots to 250 knots. Five minutes later the flight was instructed to reduce the speed to 200 knots. At 13:18:05, the flight was advised, "Alitalia six eighteen you’re three and a half from the marker, turn right zero two zero, cleared ILS four right approach." The DC-8 broke through the clouds at about 600 feet. The runway was in sight, but the plane appeared to be high and slightly on the right. The captain decided to perform a steep approach and took over the controls. He put the four engines at idle-reverse, then selected reverse thrust on Nos. 2 and 3 engines, deciding to select forward thrust when on the proper slope. too busy in rotating the aircraft, the captain could not leave the controls to regain forward thrust. The plane touched down very hard started to yaw to the left. It ground looped and came to rest with the fuselage split open aft of the wing and three out of four engines separated.
Probable cause:
The National Transportation Safety Board determines that the probable cause of this accident was the use of reverse thrust in flight, contrary to published procedures, with a resultant uncorrectable high sink rate. The captain's decision to use reverse thrust and not to execute a missed approach was a reaction under stress occasioned at least in part, by Air Traffic Control (ATC) instructions which led to positioning the aircraft too high and too close to the runway. ATC vectored the aircraft to the final approach path under IFR conditions and in the absence of an operating ILS glide slope.
Final Report:

Crash of a Beechcraft U-8F Seminole near Pikes Peak: 2 killed

Date & Time:
Type of aircraft:
Operator:
Registration:
62-3859
Flight Phase:
Flight Type:
Survivors:
No
Site:
MSN:
LF-57
YOM:
1962
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
The twin engine airplane took off at 0820LT on a three-hours training mission with two pilots on board. While cruising over mountainous terrain, the crew encountered fogg conditions when the aircraft struck the slope of a mountain located five miles southeast of Pikes Peak. Both occupants were killed.
Crew:
Ltc Thomas W. Wheat Jr.,
Ltc Donald Grostic.

Crash of a Douglas DC-8-63CF in New York: 11 killed

Date & Time:
Type of aircraft:
Operator:
Registration:
N4863T
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
New York – Washington DC – London
MSN:
45951/414
YOM:
1968
Flight number:
TV863
Crew on board:
11
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
11
Captain / Total flying hours:
22300
Captain / Total hours on type:
7100.00
Copilot / Total flying hours:
15775
Copilot / Total hours on type:
4750
Aircraft flight hours:
7878
Circumstances:
Approximately 1,500 feet from the initiation of the takeoff roll, the aircraft was observed rotating to an excessively nose-high attitude. The aircraft became airborne about 2,800 feet down the runway after which it continued to rotate slowly upward to an attitude estimated to be between 60° and 90° above the horizontal, at an altitude estimated to be between 300 and 500 feet above the ground. The aircraft rolled about 20° to the right, rolled back to the left until it reached approximately a vertical angle of bank, and then fell to the ground in that attitude. The aircraft was destroyed by impact forces and post impact fire. All 11 crew members, the only occupants of the aircraft, died in the accident.
Probable cause:
The Board determined that the probable cause of this accident was a loss of pitch control caused by the entrapment of a pointed, asphalt-covered object between the leading edge of the right elevator and the right horizontal spar web access door in the aft part of the stabilizer. The restriction to elevator movement, caused by a highly unusual and unknown condition, was not detected by the crew in time to reject the takeoff successfully. However, an apparent lack of crew responsiveness to a highly unusual emergency situation, coupled with the captain's failure to monitor adequately the takeoff, contributed to the failure to reject the takeoff.
Final Report:

Crash of a Beechcraft C-45H Expeditor in Lakewood

Date & Time:
Type of aircraft:
Operator:
Registration:
N9961Z
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Lakewood - Kenosha
MSN:
AF-751
YOM:
1954
Crew on board:
1
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
6150
Captain / Total hours on type:
80.00
Circumstances:
Following a short takeoff roll, the pilot initiated a left turn at low height when the airplane struck trees and crashed in flames in a wooded area. All seven occupants were injured, one seriously, and the aircraft was destroyed.
Probable cause:
Premature lift-off on part of the pilot who failed to obtain/maintain flying speed. The following contributing factors were reported:
- Rotation at mid-field,
- Presence of 60 feet tall trees.
Final Report:

Crash of a Douglas C-124C Globemaster II on Mt Pavlof: 7 killed

Date & Time:
Operator:
Registration:
52-1049
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
McChord - Cold Bay
MSN:
43958
YOM:
1952
Crew on board:
7
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
7
Circumstances:
In limited visibility, the crew started the descent to Cold Bay when the four engine aircraft struck the slope of the Pavlof Volcano located 36 miles northeast of Cold Bay. The aircraft disintegrated on impact and all seven crew members were killed. The airplane was inbound from McChord AFB, carrying seven tons of satellite observation equipment for use with the Optical Satellite Observing System. It is believed that the crew started the descent prematurely.

Crash of a Lockheed L-188CF Electra at Ogden-Hill AFB

Date & Time:
Type of aircraft:
Operator:
Registration:
N855U
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Ogden-Hill – Mountain Home – Spokane – Great Falls – Minot – Grand Forks
MSN:
2012
YOM:
1959
Flight number:
UV9524
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
16395
Captain / Total hours on type:
1022.00
Circumstances:
The airplane was engaged in a cargo flight from Ogden-Hill AFB to Grand Forks AFB, North Dakota, with intermediate stops in Mountain Home, Fairchild AFB (Spokane), Great Falls and Minot, carrying various equipment for the US Army. After liftoff from runway 32, while climbing, the pilot raised the landing gear when the airplane pitched down to 15°. It lost height and struck the ground 8,200 feet past the runway end, slid for about 2,600 feet before coming to rest in flames. All three crew members were injured and the aircraft was destroyed.
Probable cause:
Loss of control during initial climb caused by an inadequate preflight preparation on part of the crew who failed to follow the approved procedures. The following contributing factors were reported:
- Inadequate preflight on part of the flight engineer,
- Lack of action on part of the flying crew,
- Pressure to low on the hydraulic system, hydraulic pumps,
- Nosed over after takeoff, unable to control pitch,
- One hydraulic pump used while the company requested use of all three pumps for takeoff.
Final Report: