Crash of a Douglas C-118A Liftmaster in Candle

Date & Time: Aug 1, 2019 at 1400 LT
Type of aircraft:
Operator:
Registration:
N451CE
Flight Type:
Survivors:
Yes
Schedule:
Fairbanks – Candle
MSN:
43712/358
YOM:
1953
Location:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
9910
Captain / Total hours on type:
147.00
Copilot / Total flying hours:
8316
Copilot / Total hours on type:
69
Aircraft flight hours:
42037
Circumstances:
The flight crew was landing the transport-category airplane at a remote, gravel-covered runway. According to the captain, the terrain on the approach to the runway sloped down toward the approach end, which positioned the airplane close to terrain during the final stages of the approach. A video recorded by a bystander showed that while the airplane was on short final approach, it flew low on the glidepath and dragged its landing gear through vegetation near the approach end of the runway. The video showed that, just before the main landing gear wheels reached the runway threshold, the right main landing wheel impacted a dirt and rock berm. The captain said that to keep the airplane from veering to the right, he placed the No. 1 and No. 2 engine propellers in reverse pitch. The flight engineer applied asymmetric reverse thrust to help correct for the right turning tendency, and the airplane tracked straight for about 2,000 ft. The video then showed that the right main landing gear assembly separated, and the airplane continued straight down the runway before veering to the right, exiting the runway, and spinning about 180°, resulting in substantial damage to the fuselage. On-site examination of the runway revealed several 4-ft piles of rocks and dirt at the runway threshold, which is likely what the right main landing wheel impacted. Given that the airplane landing gear struck vegetation and rocks on the approach to the runway, it is likely that they were below the proper glidepath for the approach. The crew stated there were no preaccident mechanical malfunctions or anomalies that would have precluded normal operation.
Probable cause:
The pilot's failure to maintain an adequate glidepath during the approach, which resulted in the airplane impacting rocks and dirt at the runway threshold, a separation of the right main landing gear, and a loss of directional control.
Final Report:

Crash of a Douglas C-118B Liftmaster at Patriot Hills Base Camp

Date & Time: Nov 26, 1993
Type of aircraft:
Registration:
N1597F
Flight Type:
Survivors:
Yes
Schedule:
Punta Arenas - Patriot Hills
MSN:
43700
YOM:
1953
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The four engine aircraft was completing a cargo flight from Punta Arenas, carrying two passengers, six crew members and several sleigh dogs. On final approach, the captain decided to slightly deviate from the approach path to avoid local patches of fog and thus maintaining a visual contact with the ground. At an altitude of 450 feet, he increased engine power but the aircraft continued to descent until it struck the ground near the camp. All eight occupants and all animals were evacuated safely while the aircraft was damaged beyond repair.

Crash of a Douglas C-118A Liftmaster in the Caribbean Sea: 3 killed

Date & Time: Sep 18, 1992
Type of aircraft:
Operator:
Registration:
YV-502C
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Willemstad - Miami
MSN:
44656
YOM:
1955
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
While cruising by night on a cargo flight from Willemstad-Hato Airport to Miami-Intl Airport, the four engine aircraft entered an uncontrolled descent and crashed in the Caribbean Sea. Few debris floating on water and the dead body of the copilot were found about 210 km northwest of Curaçao Island. The aircraft was flying in poor weather conditions with thunderstorm activity and turbulences when the accident occurred.