Eagle ICA-D212-725, Instructions Manual

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ICA-D212-725 (53)
Page 2 of 19
CHAPTER 53 – FUSELAGE (53-00-00)
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COPYRIGHT
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2007 BY DART AEROSPACE LTD.
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THIS DOCUMENT IS PRIVATE AND CONFIDENTIAL AND IS SUPPLIED ON THE EXPRESS CONDITION THAT IT IS NOT TO BE USED FOR ANY PURPOSE OR COPIED OR COMMUNICATED TO ANY
OTHER PERSON WITHOUT WRITTEN PERMISSION FROM DART AEROSPACE LTD.
Revision: 4
Date: 11.06.01
TABLE OF CONTENTS
Table of Contents ............................................................................................................................................. 2
List of Figures ................................................................................................................................................... 2
53.1 Fuselage ............................................................................................................................................... 3
53.2 Forward Fuselage ................................................................................................................................ 3
53.3 Crew Seat Tracks ................................................................................................................................. 3
53.3.1 Crew Seat Tracks - Removal ....................................................................................................... 3
53.3.2 Crew Seat Tracks - Inspection ..................................................................................................... 3
53.3.2 Crew Seat Tracks - Installation .................................................................................................... 4
53.4 Tension Rod Assembly ........................................................................................................................ 4
53.4.1 Tension Rod Assembly - Removal ............................................................................................... 4
53.4.2 Tension Rod Assembly - Inspection............................................................................................. 4
53.4.3 Tension Rod Assembly - Installation ............................................................................................ 4
53.5 Tailboom ............................................................................................................................................. 10
53.5.1 Removal ..................................................................................................................................... 10
53.5.2 Inspection ................................................................................................................................... 10
53.5.3 Repair ......................................................................................................................................... 11
53.5.4 Installation .................................................................................................................................. 11
53.6 Generic Sheet Metal Part Replacement Procedure ........................................................................... 12
LIST OF FIGURES
Figure 53-1. Eagle Single Helicopter Fuselage and Major Components ..................................................... 5
Figure 53-2. Forward Fuselage .................................................................................................................... 6
Figure 53-3. Crew Seat Track Assemblies - Removal and Installation ........................................................ 7
Figure 53-4. Tension Rod Assembly - Removal and Installation ................................................................. 8
Figure 53-5. Tension Rod Assembly - Damage Limits ................................................................................. 9
Figure 53-6. Tailboom ................................................................................................................................. 13
Figure 53-7. Control Disconnect Points for Tailboom Removal ................................................................. 14
Figure 53-8. Tailboom Support Assembly, T102012 .................................................................................. 15
Figure 53-9. Tailboom Attaching Bolts ....................................................................................................... 16
Figure 53-10. Tail Rotor Gearbox Support Fitting - Damage and Corrosion Limits (Sheet 1 of 3) .......... 17
Figure 53-10. Tail Rotor Gearbox Support Fitting - Damage and Corrosion Limits (Sheet 2 of 3) .......... 18
Figure 53-10. Tail Rotor Gearbox Support Fitting - Damage and Corrosion Limits (Sheet 3 of 3) .......... 19