(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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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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