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19 Cards in this Set
- Front
- Back
- 3rd side (hint)
When are the power levers set to RAMP? |
For go around |
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In flight you see master caution and a flashing EEC fault light. |
Refer to the checklist, a flashing EEC should not be reset |
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An engine fails on final approach. What ATPCS functions do you expect to occur? |
Nothing, ATPCS is not available during approach (only in case of a go around) |
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Is the fuel heated before entering the HP fuel pump to prevent icing? |
Yes, by means of hot engine oil |
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The engine oil system: |
Serves the turbo machinery section, the reduction gear box and the propeller pitch change system |
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How is a failed engine detected by the ATPCS? |
When the torque meter drops below 18% |
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A gate prevents PL angle reduction below flight idle in flight as soon as: |
Both main landing gear absorbers are released |
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At take-off, what happens if an EEC FAULT occurs? |
Engine power remains vertically unchanged, the EEC FAULT light flashes and EEC de-selection is prohibited |
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During an ATPCS engine failure sequence, when does the ARM light extinguish? |
At the end of the autofeathering sequence |
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What is the maximum PLA available with the gust lock engaged? |
A few degrees below flight idle |
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The high energy ignition system consists of? |
Two ignition exciters and two spark igniters for each engine |
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Aircraft is on the ground, PWR MGT set at TO, ATPCS push button ON. The ATPCS is armed when: |
Both PL are above 49° and both torques are above 46% |
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During landing, when does the idle gate move rearwards to allow the PL to be moved to GI? |
As soon as one landing gear shock absorber is compressed |
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The accessory gearbox, which is driven by the HP spool, contains drives for the starter/generator and: |
The HP fuel pump and oil pump |
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What is the function of the EEC? |
-to provide up trim power in case of engine failure during take off and ensure, at a given engine rating, a constant PL position -to ensure minimum propeller speed control (and therefore ACW generator operation) on the ground and at low power |
What can it do during an engine failure and on the ground? |
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Illumination of the up trim light during take off when one engine fails indicates what? |
That the ATPCS has automatically increased torque on the live engine? |
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During a go around, with the PWR MGT selected to TO, the ATPCS: |
Is armed for auto feathering only |
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In the event on an EEC fault, the fault light will illuminate steady once the PL is retarded below 52° (green range) and: |
The system automatically reverts to the manual mode which follows the HMU base law. |
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When is the ignition activated during the engine start sequence? |
When the CL is moved away from FUEL SO |
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