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53-43-11Page 409
FAIRINGS - DESCRIPTION AND OPERATION
____________________________________
1.
General
_______ The dorsal fin 321AL is made of layers of glassfiber reinforced plastic over a honeycomb core. It is installed at the leading edge of the vertical stabilizer to fuselage joint. The dorsal fin helps the directional stability of the aircraft. It also makes the air flow smoothly around the joint and keeps turbulance to a minimum. The removal of the dorsal fin gives access to the HF and VOR antenna connections.
2.
Component Location
__________________
(Ref. Fig. 001)
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Dorsal Fin - Component Location
Figure 001
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Feb 01/98
CES
DORSAL FIN - REMOVAL/INSTALLATION
_________________________________
TASK 53-45-11-000-001
Removal of the Dorsal Fin 321AL
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)
R No specific 1 ACCESS PLATFORM 6M (20 FT)
R No specific 1 CRANE HEIGHT 10 M (33 FT)
98D55307531001 1 SLING - DORSAL FIN, LEADING EDGES, END CAP
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
53-45-11-991-001 Fig. 401
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3. Job Set-up
__________
(Ref. Fig. 401/TASK 53-45-11-991-001)
Subtask 53-45-11-865-050
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 105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02 105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01 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 53-45-11-010-050
B. Get Access
R (1) Put the ACCESS PLATFORM 6M (20 FT) in position at Zone 321.
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.
(2)
Remove and discard the self-adhesive disc from the hoisting point (1).
(3)
Remove and retain the plastic plug from the hoisting point (1).
(4)
Install the hoisting lug (2) in the hoisting point (1) with the eye-end out.
R (5) Put the CRANE HEIGHT 10 M (33 FT) in position.
(6) Attach the SLING - DORSAL FIN, LEADING EDGES, END CAP (98D55307531001) to the hoisting lug (2).
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Dorsal Fin 321AL.
Figure 401/TASK 53-45-11-991-001
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Feb 01/98
CES
4. Procedure
_________
Subtask 53-45-11-020-050
A. Removal:
(1)
Remove the screws (3) from the dorsal fin (4). NOTE : Identify the length of the screws for the installation
____
procedure.
(2)
With the aid of the crane, carefully disengage and lift the dorsal fin (4) from the aircraft.
NOTE : The HF antenna is installed below the dorsal fin.
____
(3)
Lower the dorsal fin (4) on to a satisfactory support.
(4)
Disconnect the sling.
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TASK 53-45-11-400-001
Installation of the Dorsal Fin 321AL
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
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