The Curtiss Commando Page
The Curtiss Commando Page

Commando 42-96580

Aircraft Identification

VARIANT: Curtiss C-46A-45-CU Commando

USAF SERIAL NUMBER (S/N): 42-96580

CURTISS CONSTRUCTION NUMBER (C/N): 30242

COMMANDO LINE NUMBER (L/N): CU778

FATE: Written off

Operational Record

  July 1944 to April 1946

  42-96580 - USAAF (USA)


1 July 1944

Delivered from the Curtiss-Wright factory in Buffalo, NY.

9 August 1944

Assigned to ATC India-China Division.

Unknown date

Assigned to Karachi, Sindh, India.

   April 1946 to 1956

  42-96580 - INDIAN GOVERNMENT (INDIA)


10 April 1946

Purchased.

  1956 to November 1956

  N7840B - PALM AIRCRAFT SALES (USA)


1956

Purchased and ferried from India to the USA. [Palm Aircraft Sales probable but TBC]

  November 1956 to 1957

  YV-C-JTE - RANSA (RUTAS AEREAS NACIONALES SA) (VENEZUELA)


5 November 1956

Leased from Palm Aircraft Sales.

  1957 to March 1959

  N7840B - RIDDLE AIRLINES (USA)


1957

Leased from Palm Aircraft Sales.

30 March 1959

Damaged beyond repair near Alma, GA in an accident due to an inflight fire (2/2 fatalities).

Crew:
Capt Eugene P. Nesselhaus
F/O Robert H. Gillespie

The Commando was operating a night cargo flight between Orlando, FL and Atlanta, GA. Enroute, the crew reported to ATC that a fire erupted in the cabin and requested permission to divert to the nearest airport. Shortly later, the airplane went out of control and crashed in flames in a prairie near Alma, GA. The aircraft disintegrated on impact and both crew members were killed. Prior to the crash, the fire was observed by ground witnesses burning through the fuselage, allowing burning cargo and debris to be scattered over a large area. After making several left orbits, the burning aircraft plunged to the ground.

The cause of the accident was determined to be the ignition of cargo in the aft belly compartment caused by contact with an unguarded light bulb. The fire then breached the compartment wall, and damaged a hydraulic unit or line in the wing center section area at the rear spar, igniting the flammable hydraulic fluid.

Total airframe time 5,455 hours.

Last edited: 07/01/2020