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B.  LoctiteTM products or equivalent are required for seat assembly.
2. Installation of Seat Assembly on Aircraft
A.  Clean floor tracks, studs, and track fittings when seats are moved. This will prevent unwanted wear on fastener assemblies.
B.  To attach the seat assemblies to the aircraft, put the track studs and track fittings at the bottom of the leg assemblies into matching notches in the floor track.
C. Slide the seat assembly forward or aft approximately one-half inch until the locking mechanism on the track fitting can be pressed into an access hole.
WARNING:  BE SURE TO TIGHTEN ALL SCREWS, BOLTS AND NUTS TO THE CORRECT TORQUE VALUE. IF YOU DO NOT USE THE CORRECT TORQUE VALUE, THE SEAT OR PARTS OF THE SEAT COULD BECOME LOOSE. THIS COULD CAUSE DAMAGE OR INJURY. IF THE TORQUE VALUE IS NOT SHOWN, USE THE TORQUE VALUES GIVEN IN TABLE 8001 IN THE FITS AND CLEARANCES (PAGE BLOCK 8000) SECTION. WHEN TIGHTENING A NUT AND BOLT THAT ARE USED TOGETHER, MEASURE THE TORQUE VALUE ON THE NUT. IF THE NUT CANNOT BE ACCESSED OR A NUT IS NOT USED, MEASURE THE TORQUE ON THE BOLT.
D. To lock the track fitting into position, tighten the Allen screw, which will push the arm against the top surface of the aircraft floor tracks.
E.  Tighten the anti-rattle nut under the forward leg hand tight plus 1/4-turn.
Page 7001
B/E AEROSPACE
COMPONENT MAINTENANCE MANUAL
MILLENNIUM. 88813 SERIES

3.  Storage Instructions
A.  General
The seat is essentially corrosion resistant and special preservation is not required.

B.  Procedures
(1)  
Wrap the seat assembly in waterproof wrapping paper (Federal Specification UU-P- 217 or equivalent) or a plastic cover. Use tape (Federal Specification JAN-P-127 or equivalent) to secure the wrapping paper or cover.

(2)  
Identify the seat assembly part number and overhaul date on a tag or in a convenient location on the seat assembly wrapper.

(3)  
Store the seat assembly in a cool, dry place away from sunlight and heat sources.

4.  Assembly Procedures
A.  Assembly of the Spreader Assembly
(Refer to IPL FIG 19)

(1)  
Install the artic roller shaft (10, -10A) onto the spreader (45, -45A).

(2)  
Attach the articulation roller (5) to the artic roller shaft (10) with the screw (15) and washer (20).

(3)  
Attach the eyebolt (25) with the nut (35) and washer (30).

(4)  
Install the bushing (-40) or spline nut (-40A).

B.  Assembly of the Leg Assembly
(Refer to IPL FIG 18)

(1)  
Attach the front stud (15) and anti-rattle nut (10) to the machined leg (5), and secure with the set screw (20) and nylon ball (25).

(2)  
Attach the leg doublers (30) with the screw (35), washer (40), and nut (45).

(3)  
Attach the track fitting assembly (50) with the screw (55), washers (60, 65), and nut (70). NOTE: Torque the nut (70) to 90 ± 10 IN-LB.
　
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