Ground Emergencies Flashcards
Abort Start Procedures
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
Manual Abort Start situations
• 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
If start is initiated with PCL in OFF position, how do you abort?
select auto/reset on STARTER switch
If start is initiated with PCL out of OFF but not past IDLE gate, how do you abort?
either select auto/reset or bring PCL bank to OFF
If start is initiated with PCL past IDLE gate, how do you abort?
bring the PCL back to off
Cautions with Motoring Run Procedure
- 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
During ground starts, what parameters could cause the PMU to abort?
weak battery, high OAT, high pre-start ITT, high density altitude, tailwind
If battery start is aborted (PMU/manual) do you connect external power?
Yes, and attempt restart if no engine malfunctions are evident and no limits exceeded
Motoring Run Procedure
Perform after an aborted start, to clear engine of residual fuel/ lower ITT
- PCL - OFF
- IGNITION switch - NORM
- Propeller area - Clear
- STARTER switch-MANUAL for 20 seconds
- STARTER switch - NORM
Is the starter switch spring loaded from manual to norm?
No
Motor Run starter delay cycle to cool engine
30 sec, 2 min, 5 min, 30 min
FIRE WARNING ON GROUND
- 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
EMERGENCY ENGINE SHUTDOWN ON THE
GROUND
- PCL - OFF
- FIREWALL SHUTOFF HANDLE - PULL
- Emergency ground egress - As required
5 situations to EMERGENCY ENGINE SHUTDOWN ON THE GROUND
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
EMERGENCY GROUND EGRESS
- ISS mode selector – SOLO
- Seat safety pin – Install (BOTH)
- PARKING BRAKE – As required
- Canopy – Open
IF CANOPY CANNOT BE OPENED OR SITUATION
REQUIRES RIGHT SIDE EGRESS: - CFS handle – Rotate and pull (BOTH)
- Release restraints
- BAT, GEN, and AUX BAT switches – OFF
- Evacuate aircraft