Mahindra GIPPSAERO GA8-TC 320 - Emergency Procedures Check Lists

CASA Approved
C01-01-08 5 Feb 2009 Page 3-3
Section 3
Model GA8-TC 320 Emergency Procedures
3.3. EMERGENCY PROCEDURES CHECK LISTS
3.3.1. Engine Failures
Engine Failure During Take-off Run
1. Throttle ...............................................CLOSED
2. Brakes ................................................APPLY
3. Wing Flaps .........................................UP
4. Master Switches Bus 1 and Bus 2 .....OFF
5. Ignition ................................................OFF
6. Fuel Shutoff Valve ..............................OFF
Engine Failure Immediately After Take-off
1. Airspeed .............................................64 - 71 KIAS. Refer paragraph 3.2 for weight specic speed
2. Ignition ................................................OFF (As time permits)
3. Fuel Shutoff Valve ..............................OFF (As time permits)
4. Master Switches Bus 1 and Bus 2 .....OFF
5. Wing Flaps .........................................FULL RECOMMENDED
6. Braking ...............................................HEAVY AFTER TOUCHDOWN
Engine Failure During Flight
1. Airspeed .............................................69 - 78 KIAS. Refer paragraph 3.2 for weight specic speed
2. Fuel Pump ..........................................ON-CHECK FUEL PRESSURE
3. Fuel Shutoff Valve ..............................CONFIRM ON
4. Fuel Quantity ......................................CHECK
5. Mixture ...............................................RICH
6. Alternate Air .......................................SELECT ON
7. Oil .....................................................CHECK TEMP AND PRESSURE
8. Ignition ................................................CYCLE BOTH-L-R-BOTH
9. Throttle ...............................................CHECK LINKAGE OPERATION
10. Starter ..............................................ACTIVATE IF PROP STOPPED
NOTES:
(a) If engine does not restart commence forced landing procedure.
(b) If clear symptoms of a mechanical failure exist, or if the engine has seized due
to the loss of oil pressure, do not attempt a restart.
(c) If engine operates with only L or R magneto selected, leave the ignition switch
in the operative position whilst a suitable landing area is selected.
(d) At high elevations or altitudes roughness or loss of power may result from
over-richness. In these cases the mixture should only be adjusted sufciently
to obtain smooth running. Observe instruments for temperature rise. Rough
engine operation due to over-richness is most usually encountered at altitudes
above 5000 ft.