Subtask 53-15-11-420-053
E. Installation of the Support Equipment.
(1)
Put the lifting equipment with a capacity of 50 kg (110.2311 lb) in position.
(2)
Put the SLING-RADOME (98D53103500000) (42) under tension.
4. Procedure
_________ Subtask 53-15-11-020-052
A. Disconnection of the Component.
(Ref. Fig. 402/TASK 53-15-11-991-002)
CAUTION : MOVE THE RADOME CAREFULLY TO PREVENT DAMAGE TO THE RADAR.
_______
(1)
Disconnect the bonding leads (8).
(a)
Remove the nuts (6), the bolts (10) and the washers(9).
(b)
Let the bonding leads (8) hang.
(2)
Disconnect the rods (13) from the hinge fittings (7) of the radome.
(a)
Remove the cotter pins (18) and discard them.
(b)
Remove the nuts (17).
(c)
Remove the bolts (11) from the rods (13).
(d)
Push the rods (13) forwards. Subtask 53-15-11-210-050
B. Inspection of the Radome Sling.
(1)
Make sure that the SLING-RADOME (98D53103500000) is under tension. Subtask 53-15-11-020-050
C. Removal of the Radome. CAUTION : MOVE THE RADOME CAREFULLY TO PREVENT DAMAGE TO THE RADAR.
_______
(1) Remove the cotter pins (2) and discard them.
EFF : ALL
53-15-11Page 404
Radome
Figure 402/TASK 53-15-11-991-002
EFF : ALL 53-15-11 Page 405
Feb 01/98
CES
(2) Remove the nuts (3) with the washers (4).
(3) Remove the bolts (5).
R R (4) Remove the radome (19) and install it in TROLLEY - RADOME (98D53103013000).
Subtask 53-15-11-020-054
D. Removal of the Support Equipment
(1) Remove the SLING-RADOME (98D53103500000).
EFF : ALL
53-15-11Page 406
TASK 53-15-11-400-001
Installation of the Radome
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific lifting equipment
No specific spring scale
No specific warning notice
R No specific Torque Wrench : range 0.00 to 1.20 m.daN
R (0.00 to 9.00 lbf.ft)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-004 USA MIL-PRF-23827 TYPE I
SYNTH.ESTER BASED GREASE HIGH PRESSURE
(Ref. 20-31-00)
Material No. 05-001 USA SAE-AS8660
INSULATING AND SEALING GREASE SILICONE
(Ref. 20-31-00)
Material No. 11-003 USA ASTM D 740
METHYL-ETHYL-KETONE (Ref. 20-31-00)
Material No. 19-003 USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
2 cotter pins 53-15-11 01A-040 18 cotter pins 53-15-11 03 -010
EFF : ALL
53-15-11Page 407
D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
20-28-00-869-002 Table of the Maximum Permitted Resistance Values
20-28-00-912-004 Electrical Bonding of Components With Conductive Bolts and Screws and Bonding Straps in the Fuselage and in the Wings (this does not include the tanks)-
53-15-11-010-001 Opening of the Radome 110AL
53-15-11-410-001 Closing of the Radome 110AL
53-15-11-991-002 Fig. 402
53-15-11-991-003 Fig. 403
**ON A/C 001-049, 051-061, 101-105, 201-203,
53-15-11-991-012 Fig. 404
R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
53-15-11-991-012-A Fig. 404A
**ON A/C ALL
53-15-11-991-006-A Fig. 405
53-15-11-991-015 Fig. 406
53-15-11-991-014 Fig. 407
