VERTICAL STABILIZER TIP - DESCRIPTION AND OPERATION
___________________________________________________
1. General_______
R The vertical stabilizer tip is the upper fairing with the identification
R 324AT
2. Component Location__________________
R (Ref. Fig. 001)
R 3. Description___________
R A. Vertical Stabilizer Tip Structure
R (1) The vertical stabilizer tip is made of laminations of Glass Fiber
R Reinforced Plastic (GFRP) on a honeycomb core. It is attached to the
R leading-edge end-rib and the stabilizer spar box. Countersunk screws
R are used to attach it.
R (2) A light-alloy lightning conductor is bonded along the top of the tip.
R Two lightning conductors are laminated to the left-hand and
R right-hand outer surface. A fourth lightning conductor is laminated
R to the inner surface of the tip. A static discharger is attached to
R the lightning conductor on the top of the tip.
R (3) The vertical stabilizer tip has a hoisting point. The hoisting point
R has a threaded sleeve which is bonded into the tip. When hoisting
R point is not in use, a plastic insert is fitted in the threaded
R sleeve. The hoisting point is covered with a self adhesive disc which
R makes a smooth surface with the contour of the tip.
Vertical Stabilizer Tip
Figure 001
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TIP - VERTICAL STABILIZER - REMOVAL/INSTALLATION
________________________________________________
TASK 55-34-11-000-001
R Removal of the Vertical Stabilizer Tip
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
CAUTION : MAKE SURE YOU DO NOT DAMAGE THE ANTENNA.
_______
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
No specific crane
No specific warning notice
No specific access platform 10.5 m (34 ft. 5 in.)
98D55307531001 1 SLING - DORSAL FIN, LEADING EDGES, END CAP
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
23-61-41-000-001 Removal of the Static Discharger 29-00-00-864-001 Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action 55-34-11-991-001 Fig. 401
3. Job Set-up__________
Subtask 55-34-11-865-050
A. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11 49VU FLIGHT CONTROLS/THS/ACTR/MOT2 19CE2 B09 49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08 49VU AUTO FLT/FAC1/28VDC 5CC1 B04 49VU AUTO FLT/FAC1/26VAC 14CC1 B03 105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02 105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01 105VU FLT CTL/SEC1/STBY SPLY 22CE B01 121VU AUTO FLT/RUDDER/TRIM/IND 15CC M20 121VU AUTO FLT/FAC2/28VDC 5CC2 M19 121VU AUTO FLT/FAC2/26VAC 14CC2 M18 121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19 121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18 121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17 121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16 121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
Subtask 55-34-11-864-050
B. Depressurize the Green, Yellow and Blue hydraulic systems (Ref. TASK 29-00-00-864-001).
Subtask 55-34-11-010-050
C. Get Access
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