Ground Emergencies Flashcards

1
Q

Abort Start Procedures

A

In the AUTO start mode, if a no start is detected or if a hung
or hot start is projected, the PMU should terminate the start
sequence. However, the engine start should be aborted manually in the following situations

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2
Q

Manual Abort Start situations

A

• ITT rate of increase appears likely to exceed 1000 °C
(hot start) tell maintenance time and degree of overtemp
• Normal N1 increase is halted (hung start)
• No rise of ITT is evident within 10 seconds after fuel
fuel flow indications (no start)
• BAT BUS annunciator illuminates during the start
sequence
• PCL is moved or the ST READY annunciator extinguishes during the start sequence

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3
Q

If start is initiated with PCL in OFF position, how do you abort?

A

select auto/reset on STARTER switch

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4
Q

If start is initiated with PCL out of OFF but not past IDLE gate, how do you abort?

A

either select auto/reset or bring PCL bank to OFF

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5
Q

If start is initiated with PCL past IDLE gate, how do you abort?

A

bring the PCL back to off

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6
Q

Cautions with Motoring Run Procedure

A
  • if start used external power is aborted (PMU or manual) do not attempt subsequent starts
  • Repeated PMU aborted starts attempts are indicative of engine malfunction
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7
Q

During ground starts, what parameters could cause the PMU to abort?

A

weak battery, high OAT, high pre-start ITT, high density altitude, tailwind

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8
Q

If battery start is aborted (PMU/manual) do you connect external power?

A

Yes, and attempt restart if no engine malfunctions are evident and no limits exceeded

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9
Q

Motoring Run Procedure

A

Perform after an aborted start, to clear engine of residual fuel/ lower ITT

  1. PCL - OFF
  2. IGNITION switch - NORM
  3. Propeller area - Clear
  4. STARTER switch-MANUAL for 20 seconds
  5. STARTER switch - NORM
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10
Q

Is the starter switch spring loaded from manual to norm?

A

No

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11
Q

Motor Run starter delay cycle to cool engine

A

30 sec, 2 min, 5 min, 30 min

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12
Q

FIRE WARNING ON GROUND

A
  • Primary indication is FIRE light with MASTER WARNING with other indications (visual, high ITT, Fluctuating/ high fuel flow)
  • Any indication of FIRE shutdown, Emergency ground egress
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13
Q

EMERGENCY ENGINE SHUTDOWN ON THE

GROUND

A
    1. PCL - OFF
    1. FIREWALL SHUTOFF HANDLE - PULL
    1. Emergency ground egress - As required
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14
Q

5 situations to EMERGENCY ENGINE SHUTDOWN ON THE GROUND

A

engine fire, prop strike, or chip light; if the aircraft appears likely to depart the prepared surface; or should any other serious ground emergency occur

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15
Q

EMERGENCY GROUND EGRESS

A
  1. ISS mode selector – SOLO
  2. Seat safety pin – Install (BOTH)
  3. PARKING BRAKE – As required
  4. Canopy – Open
    IF CANOPY CANNOT BE OPENED OR SITUATION
    REQUIRES RIGHT SIDE EGRESS:
  5. CFS handle – Rotate and pull (BOTH)
  6. Release restraints
  7. BAT, GEN, and AUX BAT switches – OFF
  8. Evacuate aircraft
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16
Q

Why confirm ISS SOLO during Emergency ground egress?

A

could lead to inadvertent ejection of one or both seats

17
Q

Why confirm ejection pin being in?

A

during egress inadvertent activation of handle could lead to ejection seat activating leading to serious injury/ death

18
Q

If canopy can’t open CFS system fails in Emergency ground egress fails?

A

Ejection is only option, assume body position.

19
Q

How to prevent injury if using CFS?

A

ensure O2 mask is on and visor down

20
Q

TAKEOFF EMERGENCIES decision factors

A

● Runway length and condition, terminal weather conditions and area traffic.
● If any system emergency affecting safety of flight is
experienced prior to liftoff, the takeoff should be aborted.

21
Q

ABORT

A
    1. PCL – IDLE

* 2. BRAKES – AS REQUIRED

22
Q

After Max braking following an Abort, what are the considerations

A

Hot brakes could occur from max braking, don’t taxi or park in congested areas until brakes cool, DON’T set parking brake

23
Q

BARRIER ENGAGEMENT

A

Don’t call to raise barriers and steer around it, to include departing prepared surface or ejection before entering barrier (so to speak)

24
Q

Warnings with Barriers

A
  • Significant aircraft damage can be anticipated when engaging a raised web barrier and webbing may preclude normal canopy opening.
  • If contact with a lowered BAK-15 is imminent, discontinue braking before reaching lowered barrier, then recommence once past
    barrier. In the unlikely event that webbing catches on aircraft, there may be unexpected directional control problems.
25
Q

AIRCRAFT DEPARTS PREPARED SURFACE

A

If it appears likely that the aircraft will depart the prepared surface, execute the Emergency Engine Shutdown On The Ground procedure.

26
Q

TIRE FAILURE DURING TAKEOFF

A

IF THE DECISION IS MADE TO STOP: 1. Abort
IF TAKEOFF IS CONTINUED:
2. Gear and flaps position – Do not change
3. Straight-in approach–Execute

27
Q

How should you land following a Tire Failure?

A

Land on side of runway corresponding to the good tire (put drag in the middle). Maintain directional control using rudder, brakes, and nose wheel steering as required.

28
Q

ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF (SUFFICIENT RUNWAY REMAINING STRAIGHT AHEAD)

A
    1. AIRSPEED – 110 KNOTS (MINIMUM)
    1. PCL – AS REQUIRED
    1. EMER LDG GR HANDLE – PULL (AS REQUIRED)
    1. Flaps – As required