On-ground helicopter engine starter interrupt system that prevents engine start up when either the throttle is open or the fuel control is engaged (or both) for reciprocating and turbine helicopters

An on-ground engine starter interrupt system of a helicopter that prevents engine start up for reciprocating and turbine helicopters when at least one of the throttle is open and the fuel control is engaged, said on-ground engine starter interrupt system comprising:

• a first electrical position switch S1;
• a second electrical position switch S2, wherein at least one of the first electrical position switch S1 and the second electrical position switch S2 is positioned via a mounting bracket next to at least one of a throttle linkage of the helicopter and a fuel control of the helicopter to detect its position as being in one of an open position and a closed position;
• a first relay R1 that is connected in series to an existing engine starter signal wire and which provides a starter signal to the first electrical position switch S1;
• a second relay R2 that is used to isolate the starter interrupt circuit after a normal engine start;
• and
• an indicator light L1, wherein the first electrical position switch S1, the second electrical position switch S2, the first relay R1, and the second relay R2 are connected to control linkage that detects when at least one of the throttle of the helicopter is open and the fuel control of the helicopter is engaged, wherein an engine starter signal is interrupted when at least one of the throttle and the fuel control is in the open position, as detected by at least one of the first electrical position switch S1 and the second electrical position switch S2, and the indicator lamp L1 is lighted to indicate that at least one of the throttle and the fuel control is in the open position, wherein the engine starter signal is supplied to the engine starter switch for engagement when the throttle of the helicopter and the fuel control of the helicopter are in the closed position.