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Engine Core Fire In Flight

G500 Emergency Procedures

This is a work in progress


AFM Procedure

[AFM, §04-10-]

Possible Cause

Engine fire loop senses fire in engine core (Zone 2) of the engine.

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Corrective Action

  1. Affected Engine . . . Confirm

  2. POWER LEVER (Affected Engine) . . . IDLE

  3. FUEL CONTROL (Affected Engine) . . . OFF

  4. NOTE

    Do not discharge the fire bottle.

  5. FIRE Handle (Affected Engine) . . . Pull

  6. ENG BLEED AIR (Affected Engine) . . . OFF

  7. Isolation Valve . . . Open (Depressed)

  8. GEN (Affected Engine). . . OFF

  9. TCAS . . . TA only

  10. WAI . . . Deselect Auto

  11. Fuel Balance Monitor and Maintain

    1. Refer to 02-08-60, Fuel Balancing in Flight.

  12. If fire indications remain:

    1. Airplane . . . Land as soon as possible

  13. If fire indications clear:

    1. NOTE

      The Engine Fire Protection loop are continually monitored by the DCN. Performing a fire test in flight or during a fire procedure is not required.

    2. Airspeed . . . 285 KCAS / 0.90M maximum

    3. Airplane . . . Land at nearest suitable airport

    4. WARNING

      ENGINE MUST NOT BE RESTARTED AFTER A FIRE WARNING AND THE FIRE HANDLE MUST NOT BE RESET.

  14. Refer to 04-08-30, One Engine Inoperative Landing Procedure.

References

Gulfstream GVII-G500 Airplane Flight Manual, Revision 1, August 31, 2018

Revision: 2019-04-30
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