B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 05-002 USA MIL-P-8116 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00)
Material No. 05-027 USA MIL-L-81309
RUST INHIBITOR(FOR CORROSION USE 15-004)
(Ref. 20-31-00)
Material No. 11-004 USA MIL-T-81533
1.1.1TRICHLOROETHANE (METHYL CHLOROFORM)
(Ref. 20-31-00)
Material No. 16-003 F ASNB70720
COATING (OBSOLETE USE 16-021) (Ref. 20-31-00)
1EFF : ALL 1 23-11-11Page 406 1 1 Aug 01/02 1 1 1CES 1 C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
23-11-00-710-001 Operational Test of the HF System 53-45-11-000-001 Removal of the Dorsal Fin 321AL 53-45-11-400-001 Installation of the Dorsal Fin 321AL 55-32-11-400-001 Installation of the Vertical Stabilizer Leading-Edge
R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-210, 301-399, 401-499,
23-11-11-991-001 Fig. 401
**ON A/C 106-149, 211-299,
23-11-11-991-001-A Fig. 401A
**ON A/C ALL
3. Job Set-up
__________
Subtask 23-11-11-860-050
A. Aircraft Maintenance Configuration
(1)
Make sure that the access platform is in position at Zone 322.
(2)
Make sure that the access panels 321AL and 322AL are removed (Ref. TASK 53-45-11-000-001).
1EFF : ALL 1 23-11-11Page 407 1 1 Aug 01/05 1 1 1CES 1 Subtask 23-11-11-865-051
B. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
**ON A/C 001-049, 101-105, 151-199,
49VU COM/HF1 1RE1 HA14 **ON A/C 051-099, 106-149, 201-299, 301-399,
49VU COM HF1 1RE1 HA14 **ON A/C ALL
4. Procedure
_________ R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-210, 301-399, 401-499,
(Ref. Fig. 401/TASK 23-11-11-991-001)
**ON A/C 106-149, 211-299,
(Ref. Fig. 401A/TASK 23-11-11-991-001-A)
1EFF : ALL 1 23-11-11Page 408 1 1 Aug 01/05 1 1 1CES 1 **ON A/C ALL
Subtask 23-11-11-910-051
A. Preparation for Installation WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL
_______ MATERIALS ONLY WITH A GOOD SUPPLY OF AIR. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
WARNING : DO NOT GET THE FLUID ON YOUR SKIN OR IN YOUR EYES. IF YOU DO:
_______
-FLUSH IT AWAY WITH CLEAN WATER
-GET MEDICAL AID.
(1) Clean the component interface and/or the adjacent area with CLEANING AGENTS (Material No. 11-004) and a lint-free cloth.
NOTE : The antenna mounting screws give electrical bonding between
____ the antenna and the fuselage structure.
(2) Do an inspection of the component interface and/or the adjacent area.
(3) Apply the SPECIAL MATERIALS (Material No. 05-002) to all the screws. R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-210, 301-399, 401-499,
Subtask 23-11-11-420-050
B. Installation of the HF Antenna
(1)
Put the antenna (1) on the antenna supports (6) and install with the screws (4) and the washers (5).
(2)
Connect the feedlines (2) and (7) to the antenna (1) with the cap nuts (3).
(3)
Apply the STRUCTURE PAINTS (Material No. 16-003) to all the screw heads.
1EFF : ALL 1 23-11-11Page 409 1 1 Aug 01/05 1 1 1CES 1
(4) Examine the antenna assembly for the condition of the
moisture-removing oil layer, SPECIAL MATERIALS (Material No. 05-027). Apply a new layer if necessary.
R **ON A/C 106-149, 211-299,
Subtask 23-11-11-420-050-A
B. Installation of the HF Antenna
(1)
Put the antenna (1) on the antenna supports (6) and install with the screws (4) and the washers (5).
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