Thrust Reverser System
Figure 001
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Thrust Reverser Control Power Supplies
Figure 002
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Cockpit Component Location
Figure 003
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Throttle Control Lever
Figure 004
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3. Indicating
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**ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
(Ref. Fig. 005)
R **ON A/C 106-149, 303-399, 401-499,
(Ref. Fig. 005A)
**ON A/C ALL
The thrust reverser system and thrust reverser operating sequences are monitored through warnings and REV indication on the lower ECAM display unit. Pressure switch, stow position switches and deploy position switches information are sent to the ECU. ECAM warning will be displayed in case of fault detection: these warnings are NO GO conditions for the aircraft dispatch.
A. Thrust reverser stow position indicating In case of fault during flight phase, an ECAM warning will be displayed. An amber REV indication will also be displayed: It first flashes for 9 seconds and then remains steady. As the stow position is maintained by redundant means, this fault does not affect the stow position integrity.
B. Thrust reverser operation indicating
(1) Deploy sequence On ground during deployment, an amber REV indication will come on ECAM in view at the midle of the N1 dial when at least one reverser blocker door is unstowed or unlocked (stroke > 1%). This indication will change to green colour when the reverser doors are fully deployed and the max reverser thrust can be commanded by the ECU.
(2) Stow sequence During stowage phase, the indication changes to amber when one door at least is less than 95% and disappears when all the doors are stowed.
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Thrust Reverser Indications
Figure 005
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Thrust Reverser Indications
Figure 005A
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THRUST REVERSER CONTROL AND INDICATING - ADJUSTMENT/TEST
________________________________________________________
TASK 78-31-00-710-042
Operational Test of the Thrust Reverser System
1. Reason for the Job
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Self Explanatory
2. Job Set-up Information
______________________
A. Referenced Information
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REFERENCE DESIGNATION
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24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 31-32-00-860-012 Procedure to Get Access to the SYSTEM REPORT/TEST/ENG
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