Crash of a Lockheed L-1049 Super Constellation in the Grand Canyon: 70 killed

Date & Time: Jun 30, 1956 at 1031 LT
Operator:
Registration:
N6902C
Flight Phase:
Survivors:
No
Site:
Schedule:
Los Angeles – Kansas City – Washington DC
MSN:
4016
YOM:
1952
Flight number:
TW002
Crew on board:
6
Crew fatalities:
Pax on board:
64
Pax fatalities:
Other fatalities:
Total fatalities:
70
Captain / Total flying hours:
14922
Captain / Total hours on type:
7208.00
Copilot / Total flying hours:
6976
Copilot / Total hours on type:
825
Aircraft flight hours:
10519
Circumstances:
On June 30, 1956, at 0901, Trans World Airlines Flight 2, a regularly scheduled passenger service, took off from runway 25 of the Los Angeles Inter-national Airport. Flight 2 was on an instrument flight rules (IFR) flight plan from Los Angeles, California, to Kansas City, Missouri, via Green Airway 5, Amber Airway 2, Daggett direct Trinidad, direct Dodge City, Victor Airway 10 Kansas City. The flight plan also proposed a cruising altitude of 19,000 feet, a .JPG"> airspeed of 270 knots, and a departure time of 0830. The Trans World flight crew consisted of Captain Jack S. Gandy, Copilot James H. Ritner, Flight Engineer Forrest D. Breyfogle, night Engineer Harry H. Allen (aboard as an additional crew member), and Hostesses Tracine E. Armbruster and Beth E. Davis. Preparations for Flight 2 were routine except that departure was delayed a few minutes by minor maintenance on the aircraft. The flight was dispatched with 3,300 gallons of fuel and the load manifest showed the gross weight of the aircraft at takeoff was 108,115 pounds, well, under the maximum allowable of 113,200 pounds. The load was properly distributed with respect to center of gravity limitations of the aircraft. As requested. the flight, after takeoff, contacted the Los Angeles tower radar departure controller, and was vectored through an overcast which existed in the Los Angeles area. After reporting "on top" (2,400 feet) the flight switched to Los Angeles Air Route Traffic Control Center (referred to as Los Angeles Center) frequency, 118.9 mcs., for its en route clearance. This clearance specified the routing as filed in the flight plan, however, the controller specified that the flight climb to 19,000 feet in VFR conditions. Immediately thereafter TWA 2 asked for a routing change to Daggett via Victor Airway 210. This was approved in a routine manner. At 0921, through company radio communications, Flight 2 reported that it was approaching Daggett and requested a change in flight plan altitude assignment from 19,000 to 21,000 feet. ARTC (Los Angeles Center) advised they were unable to approve the requested altitude because of traffic (United Air Lines Flight 718). Flight 2 requested a clearance of 1,000 feet on top. Ascertaining from the radio operator that the flight was then at least 1,000 on top, ARTC cleared the flight. At 0959 Trans World 2 reported its position through company radio at Las Vegas. It reported that it had passed Lake Mohave at 0955, was 1,000 on top at 21,000 feet, and estimated it would reach the 321-degree radial of the Winslow omni range station (Painted Desert) at 1031 with Farmington next. This was the last radio communication with the flight.
Probable cause:
The Board determines that the probable cause of this mid-air collision was that the pilots did not see each other in time to avoid the collision. It is not possible to determine why the pilots did not see each other, but the evidence suggests that it resulted from any one or a combination of the following factors: Intervening clouds reducing time for visual separation, visual limitations due to cockpit visibility, and preoccupation with normal cockpit duties, preoccupation with matters unrelated to cockpit duties such as attempting to provide the passengers with a more scenic view of the Grand Canyon area, physiological limits to human vision reducing the time opportunity to see and avoid the other aircraft, or insufficiency of en route air traffic advisory information due to inadequacy of facilities and lack of personnel in air traffic control. The following findings were reported:
- Approaching Daggett, TWA 2 requested its company radio to obtain 21,000 feet as an assigned altitude, or 1,000 on top,
- Company radio requested 21,000 feet IFR from ARTC. This vas denied by ARTC. Request was then made for 1,000 on top. This was approved and clearance issued. The flight climbed to and proceeded at 21,000 feet,
- As an explanation for the denial of 21,000 feet, TWA 2 was furnished pertinent information on UA718,
- The last position report by each flight indicated it was at that time at 21,000, estimating the Painted Desert line of position at 1031,
- The Salt Lake controller possessed both position reports at approximately 1013, at which time both flights were in uncontrolled airspace,
- Traffic control services are not provided in the uncontrolled airspace and according to existing Air Traffic Control policies and procedures the Salt Lake controller was not required to issue traffic information; none was issued voluntarily,
- A general overcast with some breaks existed at 15,000 feet in the Grand Canyon area,
- Several cumulus buildups extending above flight level existed; one was nearly over Grand Canyon Village and others were north and northeast in the area of the collision,
- The collision occurred at approximately 1031 in visual flight rule weather conditions at about 21,000 feet,
- The collision in space was above a position a short distance west of the TWA wreckage area, 17 miles west of or approximately 3-1/2 minutes' flying time from the Painted Desert line of position,
- Under visual flight rule weather conditions it is the pilot's responsibility to maintain separation from other aircraft,
- At impact the aircraft relative to each other converged at an angle of about 25 degrees with the DC-7 to the right of the L-1049. The DC-7 was rolled about 20 degrees right wing down and pitched about 10 degrees nose down relative to the L-1049,
- There was no evidence found to indicate that malfunction or failure of the aircraft or their components was a factor in the accident.
Final Report:

Crash of a Beechcraft AT-11 Kansan near Tlacolulan: 3 killed

Date & Time: Jun 15, 1956 at 0130 LT
Type of aircraft:
Operator:
Registration:
BHB-1516
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Mexico City – Veracruz
MSN:
3969
YOM:
1943
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
While cruising by night, the twin engine aircraft hit the slope of Mt Torrecillas located near Tlacolulan. All three crew members were killed.

Crash of a Vickers 607 Valetta C.1 near Ipoh: 9 killed

Date & Time: Jun 15, 1956
Type of aircraft:
Operator:
Registration:
VX521
Flight Phase:
Flight Type:
Survivors:
No
Site:
YOM:
1950
Location:
Country:
Region:
Crew on board:
9
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
9
Circumstances:
The crew was completing a supply mission on behalf of the 110th Squadron. After the load has been dropped, while at an altitude of 500 feet, the aircraft was facing a mountain and the pilot made a sharp turn to the left when the aircraft stalled and crashed. The wreckage was found few days later and all nine crew members were killed.
Probable cause:
It was determined that the crew misjudged the distance with the ground, forcing the pilot to attempt a sharp turn to avoid collision. Investigations determined that the aircraft's speed was too low during the last turn, causing the airplane to stall and to crash.

Crash of a Douglas C-47-DL near Panzós: 30 killed

Date & Time: May 24, 1956 at 1020 LT
Operator:
Registration:
TG-AHA
Flight Phase:
Survivors:
Yes
Site:
Schedule:
Guatemala City – Santa Catalina la Tinta – Puerto Barrios
MSN:
6052
YOM:
1942
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
28
Pax fatalities:
Other fatalities:
Total fatalities:
30
Circumstances:
While cruising at an altitude of 10,000 feet in poor weather conditions, the airplane struck the slope of a mountain located in the Sierra de las Minas, about 20 km south of Panzós. Hours were necessary for the rescuers to reach the crash site. Five passengers were seriously injured while all 26 other occupants were killed. Four of the survivors died from their injuries in the following days.

Crash of a Rockwell Aero Commander 520 near Skilak Lake: 6 killed

Date & Time: Apr 9, 1956 at 1000 LT
Operator:
Registration:
N5386N
Flight Phase:
Survivors:
No
Site:
Schedule:
Anchorage – Seward
MSN:
520-7
YOM:
1952
Flight number:
CDV006
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
6
Captain / Total flying hours:
7000
Aircraft flight hours:
1136
Circumstances:
The aircraft departed Anchorage international Airport at 0905LT (scheduled time of departure 0845), destination Seward. The flight plan filed with the company by Pilot John Arthur Waide contained the following: Anchorage to Seward VFR via Skilak Lake, airspeed 145 knots, estimated time en route 45 minutes. All fuel tanks were full and the fuel on board was sufficient for six hours. The estimated time for arrival at Seward was 0950. Witnesses saw the airplane flying southeast toward Seward, heard it circle Upper Russian Lake and saw it pass them again flying west-northwest at 0951. At 1255 Flight 6 was still unreported and search and rescue procedures were initiated. On April 10, 1956, at approximately 1400, the wreckage was reported on the south slope of an unnamed mountain east of Skilak Lake at an elevation of approximately 3,000 feet MSL, near latitude 60 degree 24 'N, longitude 150 degree 03'W. The aircraft was destroyed and all six occupants have been killed.
Probable cause:
The Board determines that the probable cause of this accident was the pilot's action in continuing flight during instrument weather conditions on a planned VFR flight through a mountain pass, and striking a mountainside while attempting to climb out. The following findings were reported:
- The gross weight at the time of takeoff exceeded the allowable gross. The weight was properly distributed. The overload was not a factor in the accident,
- At the time of takeoff the weather observations and forecast indicated that VFR flight over the route involved would be extremely marginal. These forecasts were available to the dispatcher and the pilot,
- The dispatching of the flight was at the discretion of the pilot in command. The assistance of the dispatcher in planning the flight was solely advisory in nature,
- Pilot Waide partially traversed a route segment through mountain passes in which conditions of ceiling and visibility were below VFR minimums, and were deteriorating,
- In attempting return through a pass after reversing his course, he lost visual contact and attempted to climb above the terrain,
- During the climb through the clouds the aircraft struck a mountain slope.
Final Report:

Crash of a SNCAC NC.701 Martinet near Delémont: 4 killed

Date & Time: Apr 6, 1956
Type of aircraft:
Operator:
Registration:
F-UHAR
Flight Phase:
Flight Type:
Survivors:
No
Site:
Location:
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
The twin engine airplane was completing a liaison flight when it crashed in unknown circumstances in hilly terrain in Les Rindins, near Delémont. All four crew members were killed, among them Célerier Valmy.

Crash of a Douglas C-47B-35-DK in Largs: 1 killed

Date & Time: Mar 28, 1956
Operator:
Registration:
G-AMRB
Flight Type:
Survivors:
Yes
Site:
Schedule:
Liverpool – Glasgow
MSN:
16670/33418
YOM:
1945
Location:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
The crew was performing a positioning flight from Liverpool-Speke Airport to Glasgow-Renfrew Airport to embark passengers for Lourdes, France. On approach, the airplane was too low and struck the Greenside Hill located near Largs. The airplane was destroyed upon impact and both captain and the stewardess were seriously injured while the copilot was killed.
Crew:
Geoffrey Moss, pilot,
Noel C. A. Stanley, copilot, †
Hilda Phillips, stewardess.
Probable cause:
An error of airmanship on the part of the captain. During an instrument approach at night he permitted the aircraft to descend below the approved safety height and this resulted in the aircraft striking the ground.

Crash of a Douglas C-47D on Mt Fuji

Date & Time: Mar 4, 1956
Operator:
Registration:
44-77094
Flight Phase:
Flight Type:
Survivors:
Yes
Site:
MSN:
16678/33426
YOM:
1945
Location:
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed in unknown circumstances on the slope of Mt Fuji. Both crewmen were rescued while the aircraft was destroyed.

Crash of a Douglas C-47B-40-DK on Mt Lash Golath: 3 killed

Date & Time: Feb 25, 1956 at 1455 LT
Operator:
Registration:
AP-ACZ
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Gilgit – Chaklala
MSN:
16813/33561
YOM:
1945
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
The aircraft took off at 0820 hours West Pakistan Standard Time from Chaklala aerodrome on a charter flight to Gilgit. After landing at 1014 hours at Gilgit, the captain advised the passengers and ground staff that he would not carry passengers on the return flight due to the very bad weather conditions en route. At 1400, AP-ACZ departed Gilgit on the return flight and at 1410 was in wireless telegraphy communication with Gilgit aerodrome. At 1421, Chaklala passed on to the aircraft the latest MET observation and the transmission was acknowledged. Nothing further was heard from the aircraft until 1454 when the following SOS was picked up by the ground stations and two other aircraft: 'SOS APACZ INDUS mouth position trapped in bad weather, Indus mouth. Chaklala aerodrome acknowledged the SOS but failed to contact the aircraft. The flight crashed on the peak of Lash Golath mountain at a height of approximately 14,000 to 15,000 feet. All three crew members, the sole occupants, were killed.
Probable cause:
The accident was attributed to pilot error while he was attempting a flight beyond his ability or experience.
Final Report:

Crash of a Douglas C-47A-80-DL near Rascafría: 3 killed

Date & Time: Feb 24, 1956
Operator:
Registration:
43-15130
Flight Phase:
Flight Type:
Survivors:
Yes
Site:
MSN:
19596
YOM:
1944
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
While cruising at an altitude of 6,000 feet, the airplane struck a hill located 8 km south of Rascafría. Three crew members were killed while three others were injured.