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Door Attachment Fittings
________________________
 A.  The openings for the forward entry and the galley doors are provided with hinge fittings, guide cams, and latch and stop fittings.
 B.  The openings for the aft entry door and for both cargo doors are provided with hinge, latch, and stop fittings.
 C.  The openings for the emergency exit hatches are provided with latch and stop fittings.
 D.  The opening for the lower nose compartment external access door is provided with hinge and latch fittings.
 E.  The opening for the electronic compartment external access door is provided with latch fittings and a pair of rails on which the door slides clear when opened.
 F.  The nose landing gear wheel well doors are hinged from fittings on the lower edges of the wheel well.
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
FRAME, 
BODY STA. 706 
STUB FRAME, 
BODY STA. 695 
FRAME, 
BODY STA. 685 
LINK SUPPORT BEAM 
TO BODY FRAME 
MAIN LANDING GEAR 
SUPPORT BEAM 
WALKING BEAM 
MAIN LANDING GEAR 
SIDE STRUT 
MAIN LANDING GEAR  INBD 
MAIN LANDING GEAR 
ACTUATOR CYLINDER  FWD 

Landing Gear Attachment Fittings
Figure 1 (Sheet 1)

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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

737-300/400/500
MAINTENANCE MANUAL

SPAR WING REAR 
BEARING SUPPORT TRUNNION TO BODY FRAME LINK, SUPPORT BEAM 
MAIN LANDING GEAR 
TO REAR SPAR FITTING PIN, SUPPORT BEAM  SUPPORT LINK ACTUATOR  STABILIZING LINK  FWD BEARING SPHERICAL  INBD SUPPORT BEAM MAIN LANDING GEAR 

Landing Gear Attachment Fittings
Figure 1 (Sheet 2)

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 EQUIPMENT ATTACHMENT FITTINGS - DESCRIPTION AND OPERATION
_________________________________________________________
 1.  General_______
 A.  This section describes the fittings on the fuselage used for the
 attachment of seats and miscellaneous equipment.

 2.  Seat Attachment Fittings________________________
 A.  Four seat tracks extend over the length of the passenger cabin. The tracks are attached to the tops of the floor beams and allow the seats to be installed at any of the closely spaced locations provided in the tracks. The fore and aft spacing between the seats can thus be varied to arrange different classes of accommodation. The two tracks on one side of the airplane support all the seats on that side of the airplane.
 B.  The forward flight attendant's seat is attached to the partition forward of the forward entry door. The aft flight attendant's seat is attached to the forward side of the aft lavatory partition.
 C.  The flight crew seat mountings are attached directly to the control cabin floor structure.
 3.  Miscellaneous Equipment Attachment Fittings___________________________________________
 A.  Fittings are provided on the fuselage structure for the attachment of the air conditioning and electronic equipment, instrument panels, galley and toilet equipment, water tanks, APU and cargo retaining nets.
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