Crash of a Grumman G-44 Widgeon near Pelican: 1 killed

Date & Time:
Type of aircraft:
Operator:
Registration:
N67794
Flight Phase:
Survivors:
Yes
Schedule:
Sitka – Pelican – Hoonah – Juneau
MSN:
1321
YOM:
1943
Flight number:
ACA060
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
14000
Captain / Total hours on type:
600.00
Aircraft flight hours:
2763
Circumstances:
Flight 60 originated at Sitka, Alaska, with stops scheduled at Pelican City, Hoonah, and Juneau, the destination. Before departure from Sitka, the dispatcher in Juneau issued clearance for the flight to proceed DVFR (Defense Visual Flight Rules) to Hoonah and wait, if necessary, at that station for weather to improve in the Juneau area. The flight plan indicated estimated time from Sitka to Juneau, including stops, would be two hours and fifty minutes. Fuel consumption was estimated at 60 gallons, with 20 gallons re-serve upon arrival at Juneau. Gross weight of all disposable load at takeoff was 1,401 pounds, 30 less than the maximum allowable. The flight departed Sitka at 1153 with Captain James C. Rinehart (pilot), four passengers, cargo, mail, and baggage. The route between Sitka and Pelican City follows the North Pacific shore. The flight landed at Pelican City at 1235. Two passengers deplaned and 88 pounds of baggage, mail, and cargo were taken off; 159 pounds of cargo were added. The aircraft was not refueled. The pilot reported by radio that the flight departed Pelican City at 1305 en route to Hoonah. This was the last radio contact. When the flight became overdue at Hoonah, search operations were instituted. The Coast Guard was notified at 1655 and began search. At approximately 0800 the following morning, the pilot of a private aircraft located the wreckage in a mountain pass several miles southeast of Pelican City. A Coast Guard and civilian ground rescue party arrived the afternoon of November 5, rendered first aid to the two passengers, and stayed until the survivors and the body of the pilot were evacuated by helicopter on November 6.
Probable cause:
The Board determines that the probable cause of this accident was loss of control of the aircraft during a steep turn in severe turbulence while the pilot was attempting to conduct visual flight at less than the required altitude and weather minimums. The following findings were reported:
- Weather conditions within the pass were: Rain, fog, severe turbulence, and low ceiling, with the base of the clouds extending about halfway down the 3,000-foot mountain slopes,
- Flight 60 crashed one-fourth mile due south of the summit of the pass about 1.500 feet above mean sea level, the pilot having negotiated about three miles of its 10-mile length,
- The aircraft struck the ground on a west heading at a sharp bend in the narrow pass, having encountered strong turbulence in a steep left bank at low altitude,
- The pilot had reversed course when the accident occurred,
- The two passengers survived but the pilot was fatally injured,
- Alaska Coastal Airlines flights in this type aircraft are restricted to Defense Visual Flight Rules operations,
- The Alaska Coastal Airlines operations manual specified that the pass must be flown at 3,000 feet altitude,
- The pilot was attempting to negotiate the pass at less than the altitude specified in the operations manual and in weather conditions which were lower than DVFR requirements.
Final Report:

Crash of a Convair T-29A-CO in Tucson: 4 killed

Date & Time:
Type of aircraft:
Operator:
Registration:
50-0189
Flight Type:
Survivors:
Yes
MSN:
219
YOM:
1951
Location:
Crew on board:
3
Crew fatalities:
Pax on board:
12
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
Shortly after takeoff from Tucson Airport, while climbing by night, the crew informed ATC about an engine failure and received the permission to return for an emergency landing. While completing a last turn at low height, the aircraft hit power cables and crashed near the runway threshold. Four occupants were killed while 11 others were injured.
Probable cause:
Engine failure during initial climb.

Crash of a North American B-25 Mitchell near Nebraska City: 3 killed

Date & Time:
Operator:
Flight Phase:
Flight Type:
Survivors:
No
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
Crashed in unknown circumstances about five miles north of Nebraska City, killing all three crew members.

Crash of a Boeing RB-50G ELINT near Willows: 13 killed

Date & Time:
Type of aircraft:
Operator:
Registration:
47-154
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Biggs - Biggs
MSN:
15838
YOM:
1947
Crew on board:
17
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
13
Circumstances:
The heavy bomber was engaged in a training mission out from Biggs AAF in El Paso, Texas. While cruising by night in light rain conditions, the airplane went out of control and entered a dive. Three crew members were able to bail out before the aircraft crashed in a field located about three miles southeast of Willows. They were found alive as well as a fourth crew member who was found seriously wounded in the wreckage. All 13 other occupants were killed.
Crew:
Maj John M. Wirt, †
Cpt Keith B. Wright, †
Maj Park B. Herrick, †
M/Sgt Charles M. Ford, †
A2c Daniel A. Baca, †
M/Sgt Clarence Foster, †
A2c Eddie L. Wynne, †
M/Sgt Junior Townsend, †
Cpt Otto Robinson, †
1st Lt John T. Vaughn, †
M/Sgt Howard J. Hansen, †
A2c Williams S. Myers, †
1st Lt John Swisher, †
T/Sgt Natividad Vasquez,
S/Sgt Joseph E. Wittens,
A1c John B. Patton,
Sgt Frank M. Imely.

Crash of a Fairchild C-119G Flying Boxcar at Pope AFB: 2 killed

Date & Time:
Operator:
Registration:
52-5859
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Pope - Pope
MSN:
11018
YOM:
1952
Crew on board:
5
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
Shortly after takeoff from Pope AFB, while climbing, an engine failed. The aircraft stalled and crashed on a barrack under construction. Two crew members were killed while ten other occupants were injured as well as two workers on the ground.
Probable cause:
Engine failure after takeoff.

Crash of a Fairchild C-82A Packet near Fawnskin: 1 killed

Date & Time:
Type of aircraft:
Operator:
Registration:
45-57744
Flight Phase:
Flight Type:
Survivors:
Yes
Site:
Schedule:
Norton - Ogden-Hill
MSN:
10114
YOM:
1945
Crew on board:
9
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
The crew departed Norton AFB in San Bernardino on a flight to Ogden-Hill AFB, Utah. Few minutes after takeoff, while cruising above the mountains, an engine failed. As the pilot was unable to maintain a safe altitude, he ordered his crew to bail out. Few minutes later, he crashed with the airplane in a wooded and mountainous area located in Fawnskin, near Big Bear Lake. Unfortunately, Captain Charles M. Eckstein was unable to escape in a timely manner and was killed in the crash. All other crew members were found alive.
Probable cause:
Engine failure in flight.

Crash of a Curtiss C-46D-15-CU Commando in Santa Clarita

Date & Time:
Type of aircraft:
Operator:
Registration:
44-78035
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Burbank - Mather
MSN:
33431
YOM:
1945
Crew on board:
3
Crew fatalities:
Pax on board:
17
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
An engine caught fire in flight. All 20 occupants decided to bail out and abandoned the aircraft that dove into the ground and crashed in Santa Clarita. All 20 occupants were found uninjured while the aircraft was destroyed.
Probable cause:
Engine fire in flight.

Crash of a Grumman G-21A Goose into the King Salmon Bay: 5 killed

Date & Time:
Type of aircraft:
Operator:
Registration:
N742
Flight Phase:
Survivors:
Yes
Schedule:
Sitka – Juneau
MSN:
B022
YOM:
1943
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
5
Circumstances:
After taking part to a fish regulation conference in Sitka, all passengers were returning to Juneau when they decided to perform a low pass over the King Salmon Bay (east part of the Admiralty Island) to make a stream survey of the salmon run conditions. At a height of 100 feet, while making a turn to the left, the aircraft hit the ground. The left wing and the left engine were sheared off and the seaplane crashed into the King Salmon Bay. Debris were scattered for more than 200 yards over the creek. A passenger who was seriously wounded was able to reach the shore and was spotted by a bush pilot about 24 hours later and transferred to a hospital in Juneau. As soon as the mishap was known to the USFWS, they sent their vessel christened 'Grizzly Bear' and three planes but reached the crash site on the morning of September 3 only. On site, they noted that all five other occupants have been killed in the crash and that the airplane was totally destroyed.
Crew:
Robert Meeks, pilot. †
Passengers:
George B. Kelez, †
Richard Schuman, †
Larry Kelleon, †
Pattie David Bidwell, †
Gomer Hilsinger.

Crash of a Convair B-36D-1-CF Peacemaker at Biggs AAF: 1 killed

Date & Time:
Type of aircraft:
Operator:
Registration:
44-92097
Flight Type:
Survivors:
Yes
Schedule:
Biggs - Biggs
MSN:
92
YOM:
1946
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
The crew was completing approaches and landings at Biggs AAF, El Paso, Texas. On final approach by night, the engine lost power. The airplane lost height and crashed 1,300 feet short of runway threshold and came to rest in flames. A crew member was killed.
Probable cause:
Engine loss of power on final approach.

Crash of a Convair RB-36H-25-CF Peacemaker at Ellsworth AFB: 26 killed

Date & Time:
Type of aircraft:
Operator:
Registration:
51-13722
Flight Type:
Survivors:
Yes
Schedule:
Ellsworth - Ellsworth
Crew on board:
4
Crew fatalities:
Pax on board:
23
Pax fatalities:
Other fatalities:
Total fatalities:
26
Circumstances:
Aircraft Commander Lt Col Wray Cotterill, Pilot 1st Lt Roger Bumps, Co-pilot Captain Neal Williams and a crew of twenty-four took off in RB-36H, 51-13722 of the 77th Strategic Reconnaissance Squadron of the 28th Strategic Reconnaissance Wing from Ellsworth AFB at 4:15 in the morning on August 27, 1954. The crew had just returned from a thirty day leave. Captain Williams had finished a 20-hour mission just 32 hours earlier. Their flight took them to Kansas City, Missouri; Little Rock, Arkansas; Dallas, Texas; and back to Little Rock for radar bombing practice. They flew to Kansas City again and then returned to Ellsworth AFB after flying 3,594 air miles. At 9:00 in the evening the pilots began to practice Planned Position Indicator Ground Control Approaches (GCA PPI) using Air Surveillance Radar. They entered the pattern for Runway 12. GCA PPI was not as precise as GCA precision approach. The minimum altitude for GCA approach was 3,864 feet. The approaches were flown at 145 miles per hour. The landing gear remained retracted. The flaps were lowered to 20 degrees and the landing lights were extended. The night was clear and visibility exceeded 15 miles. During the first four approaches, Lt Bumps flew from the right seat and Captain Williams observed from the left seat. A pair of North American F-86D Sabre Dogs took off from Runway 30 at 9:30. Their pilots noticed that the red obstruction lights on a low range of hills 1-3/4 miles northwest of the runway were not working. The lead pilot notified the Ellsworth tower that the obstruction lights were out. It was not known at the time that they had been disabled by a lightning strike the night before. The civilian Senior Electrician of Air Installations was called shortly before 10:00 P.M. and notified that the obstruction lights needed to be repaired. He assembled a crew at the AIO electrical shop and prepared to drive out to the lights. On the fourth approach, ground control advised Lt Bumps that the obstruction lights northwest of the field were not working. After the fourth pass over the airfield, Col Cotterill moved into the left hand seat to fly the next approach. Col Cotterill flew the approach higher than the glide path specified by the GCA operator. Before the sixth approach, Captain Williams replaced Lt Bumps in the right hand seat. It is believed that Col Cotterill flew the next approach. The RB-36H was flying at 145 miles per hour on a heading of 147 degrees (true), descending at 750 feet per minute when the left wing struck one of the inoperative obstruction lights. Seventy feet beyond the obstruction light the lower fuselage struck the ground 8,777 feet short and 225 feet right of the centerline of Runway 12 at 10:11 P.M. Mountain Standard Time. The impact point was at an elevation of 3,394 feet, 148 feet higher than the runway. The tail section broke away from the fuselage and came to rest 275 feet from the first point of impact. E.C.M. Captain Philip Toups, 1st Lt Roger Bumps and E.C.M. A/1C John Harvey were rescued from the wreckage while 24 other occupants were killed. Cpt Toups died five days after the crash. A/1C Harvey succumbed to his injuries after six days. Eventually, only 1st Lt Roger Bumps survived the crash.
Crew:
Lt Col Wray Cotterill, pilot,
Cpt Neal Williams, copilot,
1st Lt Roger Bumps, copilot,
Maj Martin Margolin, navigator.
Passengers:
Maj Harold Chambers, photo navigator,
Cpt James MacDaniel, radar navigator,
Cpt Roy Wegner, engineer,
M/Sgt William Ratagick, engineer,
A1c Glenn Kerri, ECM,
T/Sgt Charles Briggs, ECM
Cpt Philip Toups, ECM,
A1c John Harvey, ECM,
M/Sgt Carl Boyd, radio operator,
A1c James Swanson, radio operator,
A1c Russell Wilson, photo,
A2c Allen Jenkins, photo,
M/Sgt Dean McKever, gunner,
A1c John Baker, gunner,
A1c George Gross, gunner,
S/Sgt Dennis Murphy, gunner,
A2c George Hertnecky, gunner,
A2c William Lynch, radio operator,
2nd Lt Richard Crittenden, navigator,
2nd Lt Joseph Mullan, engineer,
A2c Marcel Herbert, photo,
A2c Billy Campbell, photo,
A2c Donald Wolf, gunner.
Source & photos: http://www.air-and-space.com
Probable cause:
Several factors contributed to the crash. The altimeter error for the RB-36H was estimated at -160 feet to 270 feet. An additional local terrain effect introduced an additional error of -70 feet to 70 feet. The Rapid City GCA radar was miscalibrated. The range value shown on the radar at the point of impact was off by 1/2 mile. Since the GCA radar indicated that the airplane was 1/2 mile closer than it actually was, it placed the glide slope 150 feet low. In the months preceding and following the crash, at least six pilots reported that GCA instructions might have caused them to land short or that GCA had reported them over the end of the runway before they actually reached it.