Commando 43-47056
Aircraft Identification
VARIANT: Curtiss C-46A-55-CK Commando
USAF SERIAL NUMBER (S/N): 43-47056
CURTISS CONSTRUCTION NUMBER (C/N): 127
COMMANDO LINE NUMBER (L/N): CK104
FATE: Written off
Operational Record
November 1944
43-47056 - USAAF (USA)
27 November 1944
Delivered from the Curtiss-Wright factory in Louisville, KY.
November 1944 to 1956
50693 - US MARINE CORPS (USA)
27 November 1944
Transferred as R5C-1 and delivered to NAS San Diego, CA.
29 November 1944
Assigned to Homeland Defense Network (HDN), Marine Fleet Air, West Coast.
Assigned to Homeland Defense Network (HDN), MAG-35. [same day!]
February 1945
Assigned to VMR-352 based at MCAS Ewa, HI.
15 May 1945
Assigned to VMR-953 based at MCAS Ewa, HI.
31 May 1945
Assigned to VMR-952 based on Guam, Marianna Islands.
May 1947
Assigned to VMR-252 based at MCAS El Toro, CA.
June 1947
Assigned to NAS San Diego, CA.
August 1947
Assigned to NAS Columbus, OH.
Unknown date to March 1960
AN-??? - LANICA (LINEAS AEREAS DE NICARAGUA) (NICARAGUA)
Unknown date
Purchased or leased from AAXICO.
March 1960 to February 1965
YS-012C - AESA (AEROLINEAS EL SALVADOR SA) (EL SALVADOR)
31 March 1960
Transferred from LANICA to Salvadorian subsidiary AESA as the airline's first aircraft.
Christened "Ciudad de San Salvador".
Operated in cargo configuration, mainly on the San Salvador to Miami, FL cargo route.
13 February 1965
Damaged beyond repair in Miami, FL in a takeoff accident (2/2 fatalities).
The Commando was conducting a night cargo flight between Miami, FL and San Salvador, El Salvador with only two pilots onboard. Shortly after takeoff, the left engine failed. The crew was apparently unable to feather the propeller, thence the airplane could not maintain altitude. Reports vary as to whether the pilot carried out a forced landing or the aircraft stalled and crashed - in any case, the wreckage ended up in an automobile junkyard near the runway end where it caught fire and exploded. Both pilots were killed.
The NTSB report attributed the engine failure to a fatigue fracture of the crankshaft, while the inability of the propeller to feather was apparently caused by oil contamination - both attributed to poor maintenance. The aircraft was also improperly loaded at the time of the accident.
Right: YS-012C in AESA colors, unknown date and location.
Photo credit: Larry Johnson / AV.CA
Last edited: 14/03/2021