(f)
F80001-1 - Aft Body Jack Pad Adapter
(g)
5923-010 - Axle Jacks - Regent Model (or equivalent)
B. References
(1) AMM 32-00-01/201, Ground Lock Assemblies
C. Access
(1) Location Zones
2 Lower Half of the Fuselage
204 Nose Landing Gear
310 Left Main Landing Gear
410 Right Main Landing Gear
D. Procedure
S 492-002
(1)
Install the ground lockpins in all landing gear (AMM 32-00-01/201).
S 722-003
(2)
Make sure that the airplane gross weight and the center of
gravity (CG) are at the approved limits.
S 862-004
(3)
Set the stabilizer, the aileron, and the rudder trim controls to 0.
S 862-005
CAUTION: DO NOT LIFT THE AIRPLANE ON JACKS AT JACK POINTS A, B, C, AND D
_______
IN WINDS MORE THAN 35 MPH. IF YOU DO NOT OBEY THESE
INSTRUCTIONS, DAMAGE TO THE AIRPLANE CAN OCCUR.
(4) Make sure the airplane is turned into the wind if it is possible, when it is out of the hangar.
NOTE: There is no wind restriction when you use axle jacks at the
____
airplane axles.
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07-11-11
ALL ú ú 01 Page 203 ú Mar 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
JACK POINTS BODY BUTTOCK GROUND (INCHES) HEIGHT ABOVE MAXIMUM LOAD (POUNDS) 3 JACK ADAPTER ATTACH BOLT
AND LOCATION STA LINE MINIMUM 1 MAXIMUM 2
A RIGHT WING 580 114.5R 64 90.5 43,560 NAS514P1032-24
F80060-6
B LEFT WING 580 114.5L 64 90.5 43,560 NAS514P1032-24
C AFT BODY 1088 10R 101 121.5 15,720 F80001-1 NONE
D FORWARD BODY 294.5 47.5L 58 83.5 13,890 15,400 F80000-7 NONE NAS1305-14 NONE 5
E NOSE GEAR AXLE 287.8 0
F MAIN GEAR AXLE 698 103 SEE CHART BELOW 62,200 NONE NONE
JACK POINT DATA
TIRE SIZE CONDITION DISTANCE FROM THE GROUND TO THE BOTTOM OF THE JACK PAD CLEARANCE BETWEEN THE TIRES
MAIN GEAR H40 X 14.5-19 TIRE CHANGE ON RIM FLAT NORMAL 17.9 6.8 9.4 12.64 10.0 14.3
NOSE GEAR 27 X 7.75-15 NORMAL TIRE CHANGE ON RIM FLAT 13.3 7.5 9.6 6.3 4 4.2 7.2
LANDING GEAR TIRE DATA
THE SHOCK STRUTS ARE DEFLATED AND THE WHEELS ON RIM.
THE AIRPLANE IS ON JACKS WITH A 2.5-INCH CLEARANCE BELOW THE MAIN GEAR.
737-300 AIRPLANES;
THE SUM OF THE JACK LOADS AT POINTS A THRU D MUST BE LESS THAN 95,000 POUNDS.
IF THERE IS A 2-INCH TIRE CLEARANCE
TIGHTEN BOLTS AT 160 TO 200 POUND-INCHES.
Jack Points and Landing Gear Tire Data
Figure 202
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
07-11-11
ALL ú
ú 03 Page 204
ú Nov 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 602-006
CAUTION:_______ DO NOT DEFLATE THE SHOCK STRUTS IF YOU DO A GEAR RETRACTION
TEST. THE SHOCK STRUTS MUST BE FILLED CORRECTLY AND NOT
INFLATED ABOVE THE CORRECT PRESSURE. DAMAGE TO THE WHEEL WELL
AND THE SHOCK STRUT WILL OCCUR.
THE SHOCK STRUT MUST BE FULLY DEFLATED BEFORE THE OLEO LOCK
ASSEMBLY INSTALLATION. IF THE SHOCK STRUT IS NOT DEFLATED, YOU
CAN CAUSE DAMAGE TO THE LOCK ASSEMBLY WHEN YOU LIFT THE
AIRPLANE ON JACKS.
(5) When you lift the airplane on jacks to make the airplane level or to weight it, or for general maintenance, it is optional to deflate the shock struts of the landing gear.
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