(2)  
AMM 24-22-00/201, Manual Control

 (3)  
AMM 34-11-00/501, Pitot-Static System

 (4)  
AMM 34-11-01/501, Pitot-Static System

 (5)  
AMM 34-12-00/501, Air Data System

 (6)  
AMM 34-12-01/501, Air Data System

 (7)  
AMM 34-31-00/501, VOR/ILS Navigation System

 (8)  
AMM 34-31-02/501, VOR/ILS Navigation System

 B.  Access
 (1)  Location Zones
 101/102 Flight Compartment

 C.  Prepare for the Test
 S 865-001
 (1)  
Make sure that these circuit breakers are closed:

 (a)  P18 Circuit Breaker Panel
 1) GND PROXIMITY WARN AC
 2) RADIO ALTM-1
 3) AIR DATA CMPTR-1
 4) VHF NAV-1(VOR/ILS and G/S)
 5) CAPT ALTIM (26V AC)
 6) Flight Interphone
 7) Internal Lighting

 (2)  
Supply electrical power (AMM 24-22-00/201).

 S 865-002
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH SUNDSTRAND MK II GPWC ú

 34-42-00
 ú ú 04 Page 501 ú Jul 12/01

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 865-077
 (3)  
Make sure that the VOR/ILS-1 is tuned to an ILS frequency
 (AMM 34-31-00/501).

 S 865-082

 (4)  
Make sure that the VOR/ILS-1 is tuned to an ILS frequency
 (AMM 34-31-02/501).

 S 865-017

 (5)  
Make sure the flight interphone system is operational
 (AMM 23-51-00/501).

 S 865-018

 (6)  
Make sure the landing gear selector is in the DN position.

 S 865-019

 (7)  
Make sure the landing flaps are in the UP position.

 S 865-020

 (8)  
Make sure the DIM & TEST and the INDICATOR LIGHTS circuit breakers on panel P6 are closed.

 S 755-021

 (9)  
Make sure the failure flags on the captain's and the first officer's radio altimeter indicators do not show.

 S 865-022

 (10)
 Make sure the altitude pointers show 0 to -10 feet.

 S 755-024

 (11)
 Make sure the captain's and the first officer's PULL UP and BELOW G/S indicators are off.

 S 865-026

 (12)
 Make sure the VHF NAV switch on pilots' overhead panel is in the NORMAL position.

 S 755-027

 (13)
 On the first officer's instrument panel, make sure that the ground proximity INOP indicator light is off.

 S 865-028

 (14)
 Make sure that the FLAP/GEAR INHIBIT switch is set at NORMAL position.

 D. GPWC Self-Test
 S 865-034
 (1)  Push the ground proximity INOP indicator.
 (a)  Make sure that the indicator comes on when pushed.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH SUNDSTRAND MK II GPWC ú

 34-42-00

 ú ú 06 Page 502 ú Mar 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 S 745-035
 (2)  Push and hold the ground proximity SYS TEST switch on the first officer's instrument panel for at least 5 seconds.
 (a)  Make sure that the PULL UP, BELOW G/S, INOP indicator lights come on and that loud aural warning consists of GLIDE SLOPE and WHOOP-WHOOP PULL UP occur.
 NOTE: The WHOOP-WHOOP PULL UP aural warning can repeat up to 7
____
 times.

 S 745-038
 (3)  Release the SYS TEST switch.
 (a)  Make sure all the GPWS indicators go off.
 S 865-039
 (4)  Open the AIR DATA COMPTR-1 circuit breaker.
 (a)  Make sure that the INOP indicator comes on.
 S 745-040
 (5)  Push the SYS TEST switch for 5 seconds.
 (a) Make sure that the INOP and BELOW G/S indicators come on, and that one cycle of loud GLIDE SLOPE aural warning occurs.
　
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