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Glide Slope Antenna Coaxial Relay Installation Figure 401 (Sheet 2)
EFFECTIVITY AF 121,122,152-156,158-160,162-
182,185-199, AND AF 157,161,183,184 WITH SB 34-2264; GN ALL; 799 Page 403 MD ALL; VM ALL Sep 25/94
34-31-10
GLIDE SLOPE ANTENNA  VOR/ILS  VOR/ILS 
COAXIAL RELAYS,  RECEIVER  RECEIVER 
B404 AND B405  NO. 3  NO. 1 
SEE  E 
P31 PANEL 
VOR/ILS  SEE  F 
RECEIVER 
NO. 2 
P32 PANEL 
GLIDE SLOPE ANTENNA 
SWITCHING PANEL 

LEFT G/S 
COAXIAL RELAY, 
B404 
RIGHT G/S 
COAXIAL RELAY, 
B405 
REMOVAL AND INSTALLATION 

Glide Slope Antenna Coaxial Relay Installation
Figure 401 (Sheet 3)

EFFECTIVITY

LH 001-010; AF 101-114;
799 Page 404
SN 301-350; IB 405; AZ 201-220
34-31-10
 Dec 25/91
VOR/ILS
VOR/ILS
RECEIVERGLIDE SLOPE ANTENNA
RECEIVER
COAXIAL RELAYS, NO. 3
NO. 1
B119, B404, AND B405 SEE G
P31 PANEL
SEE HVOR/ILS RECEIVER NO. 2 P32 PANEL
GLIDE SLOPE ANTENNA SWITCHING PANEL
G
CENTER G/S COAXIAL RELAY, B119
LEFT G/S COAXIAL RELAY, B404
RIGHT G/S COAXIAL RELAY, B405
REMOVAL AND INSTALLATION
H
Glide Slope Antenna Coaxial Relay Installation Figure 401 (Sheet 4)
EFFECTIVITY

AZ 221-299; IB 406-499;
799 Page 405
LH 011-050,055-099; SN 351-399
34-31-10
 Dec 25/91
 NOTE:____ Verify that AFCS is not engaged in VOR/LOC, ILS or LAND mode
 with channel A, B or C in command or glide slope antenna
 coaxial relay test will be inhibited.
 (4)  Actuate GLIDE SLOPE ANT TEST switches 1, 2 and 3 on panel P2 in
 turn.  Check that G/S-1 ANT, G/S-2 ANT or G/S-3 ANT annunciator
 comes on when the associated TEST switch is actuated and goes off
 when switch is released.
 (5)  Open GS2 circuit breaker on overhead circuit breaker panel P7.
 (6)  Deactivate reed proximity switches S397 and S424 on nose landing
 gear strut using ferrite bars to simulate a gear up condition for
 primary landing gear logic unit M93.  Check that G/S-1 ANT and
 G/S-3 ANT annunciators come on.
 (7)  Remove ferrite bars from switches S397 and S424.  Check that G/S-1
 ANT and G/S-3 ANT annunciators go out.
 (8)  Close GS2 circuit breaker and open GS1 circuit breaker on panel P7.
 (9)  Deactivate reed proximity switches S397 and S424 on nose landing
 gear strut using ferrite bars to simulate a gear up condition for
 alternate langing gear logic unit M809.  Check that G/S-2 ANT and
 G/S-3 ANT annunciators come on.

 (10)
 Remove ferrite bars from switches S397 and S424.  Check that G/S-2 ANT and G/S-3 ANT annunciators go out.

 (11)
 Close GS1 circuit breaker on panel P7.

 (12)
 Remove electrical power if no longer required (Ref 24-22-00).


 EFFECTIVITY
 LH 011-099; AF 115-199;

 AZ 221-299; SN 351-399; 
 IB 406-499; AT ALL; GN ALL;
 MD ALL; VM ALL  01 Page 406  Sep 25/9434-31-10
 GLIDE SLOPE ANTENNA HYBRID - REMOVAL/INSTALLATION
_________________________________________________
 1.  General
_______
 A.  The glide slope antenna hybrids (one on AF 121, 122, 152-156, 158-160, 162-182, 185-199, AND AF 157, 161, 183, 184 WITH SB 34-2264; GN ALL; MD ALL and VM ALL; and two on LH 001-010; AF 101-151; AZ 201-220; IB 405 and SN 301-350 are installed on the forward side of station 400 bulkhead in the lower forward equipment bay. The hybrids are secured to the mounting structure by screws and have provisions for connecting four coaxial cables.
 2.  Referenced Procedures
_____________________
 A.  34-31-00, VOR/ILS Navigation System - Adjustment/Test
 3.  Remove Glide Slope Antenna Hybrid
_________________________________
 A.  Disconnect coaxial cables from hybrid.
 B.  Remove screws securing hybrid to station 400 bulkhead. Use care not to drop hybrid as it comes loose from support.
 4.  Install Glide Slope Antenna Hybrid
__________________________________
 A.  Position hybrid on mounting base and install screws.
 B.  Connect coaxial cables to hybrid and hand-tighten.
 C.  Perform prepare-to-test and glide slope test portions of system test (Ref 34-31-00).
 
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