come on after approximately 6 seconds. 4) Make sure the GPS annunciator on the IRS MSU (P5) comes on after approximately 6 seconds. 5) Push one of the master caution lights (P10) to stop the flashes.
(c)
Close the GPS 1 circuit breaker on the P6 panel and the GPS 2 circuit breaker on the P18 panel.
(d)
Make sure the GPS annunciator on the IRS MSU goes off.
(e)
Stop for approximately 5 minutes until the GPS L and GPS R positions are shown again.
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A
737-300/400/500MAINTENANCE MANUAL
S 865-021
(4) Remove electrical power if it is not necessary (AMM 24-22-00/201).
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737-300/400/500MAINTENANCE MANUAL
GPS SENSOR UNIT - REMOVAL/INSTALLATION
______________________________________
1. General
_______
A. This procedure has two tasks. The first task is the removal of a GPS Sensor Unit (GPSSU). The second task is the installation of a GPSSU.
B. There are two GPSSUs installed on the airplane. They are located above the ceiling between stations 500A and 500C approximately three feet to the right of the centerline.
TASK 34-58-11-024-001
2. GPS Sensor Unit Removal (Fig. 401)
_______________________
A. References
(1)
AMM 20-40-12/201, Electrostatic Discharge Sensitive Devices
(2)
AMM 25-21-45/401, Sculptured Ceiling Panels
B. Access
(1) Location Zone
107 Forward Half of Cabin, Right
C. Removal Procedure
S 864-002
(1) Open these circuit breakers and attach DO-NOT-CLOSE tags:
(a)
On the electronic load circuit breaker panel P6: 1) GPS 1
(b)
On the electronic load circuit breaker panel P18: 1) GPS 2
S 014-003
(2) Remove the right ceiling panel at station 500A (or 500B) to get access to the left (or right) GPSSU (AMM 25-21-45/401).
NOTE: The GPSSUs are located above the overhead stowage bins,
____ approximately three feet to the right of the centerline.
S 914-006
CAUTION: DO NOT TOUCH THE GPSSU BEFORE YOU DO THE PROCEDURE FOR DEVICES
_______ THAT ARE SENSITIVE TO ELECTROSTATIC DISCHARGE. ELECTROSTATIC DISCHARGE CAN CAUSE DAMAGE TO THE GPSSU.
(3) Do the procedure for devices that are sensitive to static discharge (AMM 20-40-12/201).
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A
737-300/400/500
MAINTENANCE MANUAL
SCULPTURED
CEILING
PANEL GPSSU
(ABOVE STOWAGE BIN)
SEE A
CURVED
CEILING
PANEL
FWD PANEL TRANSITION
STOWAGE BIN PANEL CEILING LOWERED
PASSENGER CABIN
WASHER (TYPICAL) (TYPICAL) SCREW
FWD
GPSSU
A
Global Positioning System Sensor Unit Installation
Figure 401
F08894
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