Figure 2020 - Ref: 48370095/ 48370096 - Electrical Installation (Sheet 4 of 6)
Page 2022
B/E AEROSPACE
COMPONENT MAINTENANCE MANUAL
MILLENNIUM. 88813 SERIES
Figure 2020 - Ref: 48370095/ 48370096 - Electrical Installation (Sheet 5 of 6)
Page 2023
B/E AEROSPACE
COMPONENT MAINTENANCE MANUAL
MILLENNIUM. 88813 SERIES
Figure 2020 - Ref: 48370095/ 48370096 - Electrical Installation (Sheet 6 of 6)
Page 2024
B/E AEROSPACE
COMPONENT MAINTENANCE MANUAL
MILLENNIUM. 88813 SERIES
DISASSEMBLY
1. General
WARNING: BEFORE SERVICING SEATS HAVING POWER COMPONENTS, DISCONNECT POWER TO THE SEAT TO AVOID ELECTRICAL SHOCK.
CAUTION: DO NOT REMOVE RIVETED ASSEMBLIES OR SUBASSEMBLIES UNLESS DAMAGE MAKES IT NECESSARY TO REPLACE A PROCURABLE PART. (REFER TO THE ILLUSTRATED PARTS LIST FOR A LIST OF PROCURABLE PARTS.) IF YOU REMOVE AND INSTALL RIVETS AGAIN AND AGAIN, YOU WILL DAMAGE ADJACENT SURFACES AND MAKE THE RIVET HOLES LARGER.
CAUTION: DO NOT DISASSEMBLE RIVETED, CEMENTED, OR BONDED SUB-ASSEMBLIES. IF THE ASSEMBLY IS DAMAGED AT THESE POINTS, YOU MUST REPLACE THE ENTIRE ASSEMBLY.
A. This section gives complete disassembly instructions for the full seat assembly. If you must repair or replace a part or subassembly, disassemble only as much as necessary to repair or replace the damaged part or subassembly.
B. Read all instructions and look at the related illustrations before starting disassembly.
C. Identify all parts with a label as you remove them.
D. TESTING AND FAULT ISOLATION (Page Block 1000) contains procedures you can use to make an analysis of the operation and condition of subassemblies. It contains a table that identifies possible malfunctions and gives procedures to correct the malfunctions.
E. SCHEMATIC AND WIRING DIAGRAMS (Page Block 2000) contains procedures, notes, warnings and cautions for the electrical system.
F. INSPECTION/CHECK (Page Block 5000) contains procedures you can use to inspect parts and subassemblies. Inspections will help you make a decision to set adjustments, clean subassemblies and repair or replace damaged parts.
G. REPAIR (Page Block 6000) contains procedures you can use to make small repairs.
2. Removal of the Seat Assembly from the Aircraft
CAUTION: DO NOT SLIDE THE SEAT ASSEMBLY ACROSS ABRASIVE SURFACES; THIS WILL CAUSE TOO MUCH WEAR ON THE TRACK STUDS AND FITTINGS.
Seat assemblies are attached to the aircraft seat tracks with a stud and anti-rattle clamp located at the bottom of the forward leg and a track fitting assembly located at the bottom of the rear leg. See Figure 3001 for examples.
Page 3001
B/E AEROSPACE
COMPONENT MAINTENANCE MANUAL
MILLENNIUM. 88813 SERIES
Figure 3001
A. Loosen the stud under the front of the leg by loosening the anti-rattle nut.
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