TCH.1C-27J-2-27JG
2-87
FLAP TRASDUCER VOLTAGE OUTPUT -
FUNCTIONAL TEST
INPUT CONDITION:
Aircraft Applicability:
04162, 04180
Required Conditions:
None
Recomended Personnel:
PROCEDURE
MECH.
CODE QTY
TOTAL TIME
(MIN.)
WORK
ZONE
Input Condition
ELT
1
20,00
Test
ELT
1
30,00
Periodicity: AR - AS REQUIRED
Total Maintenance Time: 50 (Min.)
Total Time Detention System: 50 (Min.)
AGE Required:
None
Consumable Material Required:
None
Safety Conditions:
None
PROCEDURE:
1.Ensure that the flaps are to UP (1) position (refer to
figure
2.Disconnect the aircraft connector (2TAF) from the BIU
NO. 2 (electrical rack (402 VE) ).
27-50-70
2-634