(20) Remove the clamp (10) from the oil pressure transmitter (1).
(21) Put the protective caps on the open ends of the oil pressure transmitter (1).
B.
Install Oil Pressure Transmitter
(1) Make sure that the aircraft is in the same configuration as in the removal task.
(2) Remove the protective caps from the oil pressure transmitter (1) and the tee (4).
(3) Put the clamp (10) to the oil pressure transmitter (1).
(4) Hold the oil pressure transmitter (1), attach the clamp (10) to the bracket (14) with
screw (11), washer (12) and nut (13).
(5) Tighten the screw (11).
(6) Lubricate the new preformed packing (9) with the engine oil of the same
specification.
(7) Put the nut (7), retainer (8) and the preformed packing (9) to the tee (4).
(8) Install the tee (4) to the oil pressure transmitter (1).
(9) Tighten the nut (7).
(10) Remove the protective caps from the tubes (15) and (16).
(11) Connect the tubes (15) and (16) to the tee (4) (refer to AMM 20−06−03).
(12) Lubricate the new preformed packing (6) with the engine oil of the same
specification and install it to the union (5).
(13) Install the union (5) to the oil pressure transmitter (1).
(14) Remove the protective cap from the tube (3).
(15) Connect the tube (3) to the union (5) (refer to AMM 20−06−03).
(16) Remove the protective cap from the electrical connector (2).
(17) Connect the electrical connector (2) to the oil pressure transmitter (1).
(18) Do the engine start procedure for the related engine (refer to AMM 71−00−00).
(19) Examine all the connections at the oil pressure transmitter (1) and at the tube
assemblies for signs of oil leaks.
(20) Check for the correct operation of the oil pressure/temperature dual indicator in the
engine instrument panel in the flight compartment.
(21) Do the engine shutdown for the related engine (refer to AMM 71−00−00).
(22) Remove all tools, equipment and unwanted materials from the work area.
(23) Install the left side center panel 413 AL (engine No. 1) or 423 AL (engine No. 2)
(refer to AMM 71−10−00).
(24) Close the lower forward nacelle cowl (refer to AMM 71−10−00).
(25) Remove the main landing gear doors lock pin and close the doors.
D
SERIES 100
AIRCRAFT MAINTENANCE MANUAL
MASTER
EFFECTIVITY:
79−36−03
Page 202
Jul 15/2012
