飞行翻译_公务机_公务航空_Business Jet_Business Aviation

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Emergency stow – A thrust reverser emergency stow system is installed to stow an unlocked thrust reverser. Selecting the respective UNLK switch/light on the THRUST REVERSER panel directs 14th-stage bleed air to the PDU to stow the unlocked reverser.

NOTE
While the UNLK switch/light is selected, 14th-stage bleed air is continuously applied to the PDU, even if the reverser returns to the stowed position.

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Oct 05/06 

The CF 34–3B engine controls consist of the following:
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Thrust levers

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Thrust reversers

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Engine start/ignition panel

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Engine control panel

The EICAS page and SUMMARY page provide analog and digital engine information, and system warning/caution and advisory messages.
Engine Starting

Engine Start/Ignition Panel
Figure 19.10.15

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Oct 05/06 

ENGINE CONTROL Panel
Figure 19.10.16

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Thrust Levers
Figure 19.10.17

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Oct 05/06 

GND SPOILERS/THRUST REVERSER Panel Figure 19.10.18
Oil System

Impending Bypass and Chip Detector Annunciators (JB5)
Figure 19.10.19

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Oct 05/06 

N1 Indications
Figure 19.10.20

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ITT Indications
Figure 19.10.21

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N2 Indications
Figure 19.10.22

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Engine Secondary Indications
Figure 19.10.23

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Oct 05/06 

Message Meaning Aural Warning (If Any)
WARNING (Triple Chime) “ENGINE OIL” WARNING
(Triple Chime) Either the APR has failed or it is not armed (APR to arm and N1 >79% and both eng speed switches on).

APR has been inadvertently activated on both engines.
The engine comparator has sensed a discrepancy in the respective engine
parameters (N1, ITT or N2).
Respective fuel filter is in impending bypass mode.

Insufficient pressure at the respective engine pump inlet.

Reverser moved away from fully stowed position without a deploy command.