TASK 76-11-02-400-802-F00
3. Engine Start Lever Lamps Installation
Figure 201 or Figure 202
A. General
(1) This task includes steps to install the Engine Start Lever Lamps.
(2) The lamps are installed in the Engine Start Lever Caps.
B. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
C. Lamp Installation
SUBTASK 76-11-02-420-009-F00
CAUTION
YOU MUST BE CAREFUL WHEN YOU REMOVE THE COMPONENTS FROM
THE CONTROL STAND. DAMAGE TO THE SWITCHES, LIGHTS,
LIGHTPLATES, NUTPLATES, WIRE BUNDLES AND THE PAINTED FINISH ON
ALL THE PARTS CAN OCCUR.
(1) Install LED Light [230] into the Lens Cap [229].
(2) Install Lens Cap [229] onto Engine Start Lever [201].
CAUTION
MAKE SURE THAT THE CAP IS CORRECTLY INSTALLED AND ALIGNED
WITH THE SWITCH LEVER. IF THE CAP IS NOT CORRECTLY ALIGNED
WITH THE SWITCH LEVER, DAMAGE TO THE SWITCH CAN OCCUR.
(a) Align Lens Cap [229] with Engine Start Lever [201]l.
NOTE: The Lens Cap contains a male keying feature and the Engine Start Lever
contains a female recess (Figure 201 or Figure 202). To prevent damage to the
switch (which can cause the fire indication light to not illuminate), the male keying
feature must be aligned with the female recess before you thread the Lens Cap
onto the Engine Start Lever. Once the male keying feature is aligned with the
female recess, the Lens Cap should easily thread onto the Engine Start Lever
and no excessive force or torque should be necessary. If excessive force or
torque is required to thread the Lens Cap onto the Engine Start Lever, that is an
indication that the male keying feature and the female recess are not correctly
aligned.
NOTE: If the terminal is too far forward and touches the bottom of the LED bulb, lightly
push the terminal away from the center. Then the end cap can be easily installed.
(b) Gently press Lens Cap [229] onto Engine Start Lever [201]and turn clockwise to tighten
cap.
NOTE: No tools are required to install cap, finger tighten only.
NOTE: If the cap does not thread easily, repeat step 2 above.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
CFM56 ENGINES (CFM56-7)
76-11-02
Page 204
D633A101-ILF Oct 15/2017
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF 625-627, 835, 838
To Next Page
Loading...
