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EFFECTIVITY
GUN ALL 27-31-00
Page 598.18
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Elevator Hinge Assemblies
Figure 520 (Sheet 4 of 4)/27-31-00-990-820
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-00
Page 598.19
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Elevator Tab Hinge Assemblies
Figure 521 (Sheet 1 of 4)/27-31-00-990-823
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 156, 201-204, 206 PRE SB 737-55A1080 27-31-00
Page 598.20
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Elevator Tab Hinge Assemblies
Figure 521 (Sheet 2 of 4)/27-31-00-990-823
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 156, 201-204, 206 PRE SB 737-55A1080 27-31-00
Page 598.21
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Elevator Tab Hinge Assemblies
Figure 521 (Sheet 3 of 4)/27-31-00-990-823
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 156, 201-204, 206 PRE SB 737-55A1080 27-31-00
Page 598.22
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Elevator Tab Hinge Assemblies
Figure 521 (Sheet 4 of 4)/27-31-00-990-823
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 156, 201-204, 206 PRE SB 737-55A1080 27-31-00
Page 598.23
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Elevator Tab Hinge Assemblies
Figure 522 (Sheet 1 of 4)/27-31-00-990-824
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 001-099, 101-122, 155, 157, 205, 207-999; GUN 156, 201-
204, 206 POST SB 737-55A1080
27-31-00
Page 598.24
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Elevator Tab Hinge Assemblies
Figure 522 (Sheet 2 of 4)/27-31-00-990-824
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 001-099, 101-122, 155, 157, 205, 207-999; GUN 156, 201-
204, 206 POST SB 737-55A1080
27-31-00
Page 598.25
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Elevator Tab Hinge Assemblies
Figure 522 (Sheet 3 of 4)/27-31-00-990-824
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 001-099, 101-122, 155, 157, 205, 207-999; GUN 156, 201-
204, 206 POST SB 737-55A1080
27-31-00
Page 598.26
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Elevator Tab Hinge Assemblies
Figure 522 (Sheet 4 of 4)/27-31-00-990-824
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 001-099, 101-122, 155, 157, 205, 207-999; GUN 156, 201-
204, 206 POST SB 737-55A1080
27-31-00
Page 598.27
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
TASK 27-31-00-820-808
27. Elevator Tab Pushrod - Adjustment after the Elevator Power-Off Flight Test
(Figure 502, Figure 505, Figure 512)
NOTE: For each elevator tab, if both pushrods are adjusted, then the Elevator Power-Off Flight - Test,
TASK 27-31-00-710-803 is necessary. If only one pushrod is adjusted and you can verify that
the remaining rod has not been replaced or adjusted since the last flight test, then this flight
test is not necessary. If only one pushrod is adjusted and you cannot verify that the
remaining pushrod has not been replaced or adjusted since the last flight test, then the
Elevator Power-Off Flight - Test, TASK 27-31-00-710-803.
GUN 156, 201-204, 206 PRE SB 737-55A1080
NOTE: See Figure 508 or Figure 509.
GUN 001-099, 101-122, 155, 157, 205, 207-999; GUN 156, 201-204, 206 POST SB 737-55A1080
NOTE: See Figure 511.
GUN 101-122
NOTE: See Figure 517.
GUN 156, 201-204, 206 PRE SB 737-55A1080
NOTE: See Figure 518.
GUN 001-099, 155, 157, 205, 207-999; GUN 156, 201-204, 206 POST SB 737-55A1080
NOTE: See Figure 519.
GUN ALL
A. General
(1) Use this procedure to adjust the elevator tab if the number of turns of the stabilizer trim wheel
during the elevator power off flight test are more than the allowable limits.
GUN 156, 201-204, 206 PRE SB 737-55A1080
　
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