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R 2. Component Location
__________________
R -------------------------------------------------------------------------------R FIN | FUNCTIONAL DESIGNATION | PANEL|ZONE|ACCESS | ATA R | | | | DOOR | REF. R -------------------------------------------------------------------------------R 4102KS PRESS SW-HCV 78-31-16 R 4103KS1 SW-BLOCKER DOOR DEPLOY, L 78-31-17 R 4103KS2 SW-BLOCKER DOOR DEPLOY, R 78-31-17 R 4104KS1 SW-BLOCKER DOOR STOW, UPPER R 78-31-18 R 4104KS2 SW-BLOCKER DOOR STOW, LOWER R 78-31-18 R 4104KS3 SW-BLOCKER DOOR STOW, LOWER L 78-31-18 R 4104KS4 SW-BLOCKER DOOR STOW, UPPER L 78-31-18 R 3002KM1 LATCH-BLOCKER DOOR, UPPER R 78-31-19 R 3002KM2 LATCH-BLOCKER DOOR, LOWER R 78-31-19 R 3002KM3 LATCH-BLOCKER DOOR, LOWER L 78-31-19 R 3002KM4 LATCH-BLOCKER DOOR, UPPER L 78-31-19 R 3001KM1 ACTUATOR-BLOCKER DOOR, UPPER R 78-31-41 R 3001KM2 ACTUATOR-BLOCKER DOOR, LOWER R 78-31-41 R 3001KM3 ACTUATOR-BLOCKER DOOR, LOWER L 78-31-41 R 3001KM4 ACTUATOR-BLOCKER DOOR, UPPER L 78-31-41 R 4101KS1 HCU-THRUST REV, 1 78-31-51 R 4101KS2 HCU-THRUST REV, 2 78-31-51
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 Thrust Reverser System
 Figure 001

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 Thrust Reverser Control Power Supplies
 Figure 002

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E F 『 E C F M E E E E 56-5B E

 

 Cockpit Component Location
 Figure 003

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 Throttle Control Lever
 Figure 004

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 3. Indicating
__________
 **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

 F 『R EEFF : 001-049, 051-099, 101-105, 151-199, E Page 878-31-00
 E E201-299, 301-302, May 01/05 E E ECES E F 『 E C F M E E E E 56-5B E

 

 Thrust Reverser Indications
 Figure 005A

 F 『R EEFF : 106-149, 303-399, 401-499, E Page 978-31-00
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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
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
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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