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737-300/400/500MAINTENANCE MANUAL
c) Make sure the difference between the left tab up position LTUP and the left tab neutral position LTNP is
1.24 +/- 0.12 inches.
d) Make sure the difference between the right tab up position RTUP and the right tab neutral position RTNP is 1.24 +/- 0.12 inches.
4) Set the FLT CONTROL A switch to OFF and the FLT CONTROL B switch ON.
5) Move the captain's control column aft until it touches the stop and hold. a) Make sure the trailing edge of the right elevator moves
up 14.60 +0.30/-0.55 inches from the index mark.
6) Move the captain's control column forward until it touches the stop and hold. a) Make sure the trailing edge of the right elevator moves
down 10.55 +0.60/-0.30 inches from the index mark. 7) Set the FLT CONTROL B switch to OFF.
(t) AIRPLANES WITH THE MECHANICAL STOPS ON THE ELEVATOR BUS CRANK (FIG. 505); Calculate the tab travel: 1) Move the captain's control column aft until it touches the
stop and hold. a) Make sure the trailing edge of the right elevator moves up 14.00 +0.30/-0.56 inches from the index mark. b) Measure and write the left tab down position (LTDP).
Elevator Tab Neutral Position Adjustment
Figure 511
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MAINTENANCE MANUAL
HINGE FITTING NO. 2
HINGE FITTING NO. 1
HINGE FITTING NO. 3
SEE B
HINGE FITTING NO. 4
SEE B
HINGE FITTING NO. 5
SEE B
A
SEE A
HINGE FITTING NO. 6
ELEVATOR
FRONT SPAR
NUT ELEVATOR BEARING PLATE
WASHER COTTER PIN
PLATE BOLT (3 PLACES)
STABILIZER
TRAILING EDGE RIB WASHER HINGE BEARING BOLT (HEAD OUTBOARD)
HINGE FITTING
FWD PLATE
TYPICAL INSTALLATION FOR NO. 3 THRU NO. 5 ELEVATOR HINGE FITTINGS B Elevator Hinge Locations Figure 512
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B
INBD
B
FWD
A
A
C
REAR SPAR
2
1
C
A
A
FWD
3 2
A
BEARING
RETAINER
LINK
FWD
C
BEARING
RETAINER
BEARING LINK
FWD RETAINER LINK FWD
B
C
Elevator Tab Hinge Locations
Figure 513
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