Emergency Procedures Flashcards
1
Q
Abort Start
A
- ITT looks like it will exceed 1000*C (hot start)
- N1 increase is halted (hung)
- No rise in ITT 10sec after fuel flow (no start)
- ITT looks like it will remain b/w 871-1000 for > 5 sec
- BAT BUS illuminates
- PCL is moved out of ST READY
2
Q
Emergency Engine Shutdown on the Ground
A
- Engine Fire (Fire, FEVER indications)
- CHIP light
- Prop Strike
- Likely to depart a prepared surface
Memory Aid => don’t CHIP your PROP on a FIRERY SURFACE
3
Q
Emergency Ground Egress
A
- Smoke/ Fumes/ Electrical Fire
- Fuel Leak
- FIRE
4
Q
Takeoff vs Abort
A
- Rwy length/ condition, weather, area traffic
- Adequate directional control cannot be maintained or any system affecting the safety of flight is compromised prior to Max Abort Speed, abort the takeoff
5
Q
Abort
A
- Below Max Abort Speed and an emergency requiring an Abort
- sound judgement/ decision making
6
Q
Barrier Engagement
A
- Eject or Depart prepared surface before engaging
7
Q
Tire Failure During Takeoff
A
- Loud popping noise
- yawing motion
- bumpy motion on the ground
- burnt rubber smell
8
Q
Engine Failure Immediately After Takeoff (Sufficient Rwy Remaining Ahead)
A
- Total loss in power and rapid reduction in airspeed
- ensure adequate rwy ahead for a full-stop landing before end of rwy
- *TECHNIQUE: if gear handle is already up, this checklist should not be used
9
Q
Engine Failure in Flight
A
- depending on airspeed, N1 will indicate 0% within 5 seconds
- Loss of power and airspeed
- Rapid decay of N1, Torque, and ITT
- prop movement toward feather
- Torque indicates 0%
SECONDARY:
- Reduced RPM, rapidly decreasing ITT, lower than normal oil pressure
- GEN, OBOGS FAIL, OIL PX, FUEL PX (GOOF) lights
10
Q
Airstart if failed engine
A
Perform only if failure was NOT due to Frozen, Fire or FOD (FFF)
11
Q
PMU Norm Airstart
A
- FFF doesn’t apply
- PMU FAIL not illuminated
12
Q
PMU Off Airstart
A
- FFF doesn’t apply
- PMU FAIL illuminated
13
Q
Immediate Airstart
A
- FFF doesn’t apply
- Engine failure occurs at low altitude and thrust requirement is critical
14
Q
Uncommanded Power Changes/ Loss of Power
A
- Uncommanded reduction in Power/ Thrust
- Lower than expected fuel flow
- Uncommanded decrease in N1**
- High RITT
- N1 still greater than 0%
15
Q
Uncommanded Prop Feather
A
- Rapid reduction in Np accompanied by high torque **
- Increase in prop noise
- Noticeable loss in thrust
- possible engine/ airframe vibrations
- Possible PMU FAIL light
