A hot start occurs when an aircraft engine—typically a turbine or jet engine—experiences abnormally high exhaust gas temperatures (EGT) during engine start-up, potentially exceeding manufacturer limits. This can lead to engine damage if not immediately addressed. A hot start usually results from early fuel introduction, slow rotation (N2), or insufficient airflow during light-off.
| Cause | Description |
|---|---|
| Premature fuel introduction | Fuel introduced before sufficient airflow (N2) is established |
| Weak starter performance | Starter fails to accelerate core fast enough to cool combustion |
| Hot ambient conditions | Reduce the cooling effect of air and raise baseline EGT |
| Residual heat | Recent shutdown may leave engine components already hot |
| Ignition system faults | Improper timing or delayed combustion may spike temperatures |
| Indicator | Observation |
|---|---|
| EGT rise | Rapid, steep increase beyond limits during start |
| N2/N1 lag | Rotor speeds remain low or slow to stabilize |
| Smoke/smell | May be visible from exhaust in severe cases |
| Warnings | Engine monitoring system alerts or redlining gauges |
Always refer to the Aircraft Flight Manual (AFM) or QRH (Quick Reference Handbook) for aircraft-specific procedures.
| Type | Description | Action |
|---|---|---|
| Hot Start | EGT exceeds limits | Cut fuel immediately |
| Hung Start | N2 fails to reach idle RPM | Abort start and cool down |
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