Engine failure before rotation (abort)
If collision is likely:
3. EJECT
Engine Flameout
Indications - Loss of power, ITT below 400 C, Ng decreasing below 80% (70% in PMS MAN)
If normal engine indications not restored:
EO2 will last typically for less than 5 min
6. EO2 - Pull (If above 10000ft and monitor contents)
7. OXYGEN - OFF
8. Throttle - FUEL OFF
9. Gliding Checks
If normal engine indications restored:
Engine failure after take-off
Anti-skid is INOP after EMER LDG GR handle has been operated
If unable to reach landing area:
1. EJECT
If runway avail:
When a/c has stopped:
8. BATT 1 and BATT 2 - OFF
Engine fire on the ground
With BATTs and GENs off anti-skid is not available, use wheel brakes with care
Smoke or fumes in the cockpit
EO2 will last typically for less than 5 minutes
If fumes continue:
4. GEN 1 and GEN 2 - OFF
If fumes still continue:
If fumes still continue, consider the following actions according to the severity of the smoke/fumes and the aircraft flight conditions:
8. GEN 1 - OFF
NOTE: The SFD will be the only remaining functional electrical service. It will operate for at least 30 minutes on a fully charged emergency battery. NAV 1 will not operate
Engine fire in the air
EO2 will last typically for less than 5 mins
If fire confirmed:
If fire goes out or is not confirmed:
15. Land as soon as possible; using minimum power
If fire persists:
EJECT
Incipient spin
Controls - Neutral smoothly
Erect Spin
When the spin stops:
Erect Spin
When the spin stops: