Section V. REPAIR OF EXTENSION CABLE

TM 9-1270-212-14&P

Section V. REPAIR OF EXTENSION CABLE

5-25. Installation (fig. 5-6).

5-23. Removal (fig. 5-6).

a. HSS XM128 (AH- 1S(Mod) Helicopter).

a. HSS XM128 (A H-1S(Mod) Helicopter).

NOTE

(1) Secure the cable mounting bracket assembly and

the gunner-linkage-assembly aft mounting bracket to the

Before the extension cable can be removed

airframe with the two mounting screws retained in

from an AH-1S(Mod) helicopter, the gunner

paragraph 5-23a(3).

linkage assembly must be removed (paragraph

5-13).

(2) Connect cable connector A3P1 from the gunner

linkage assembly to W1P1 on the extension cable.

(1) Disconnect connector W1P2 from the EIA.

(2) Disconnect the four cable clamps that secure the

(3) Route the extension cable along the airframe and

cable to the airframe. Retain the clamps and the screws and

connect cable connector W1P2 to J4 on the EIA.

washers.

(4) Secure the cable to the airframe with the four

(3) Remove the two screws that secure the cable

cable clamps and their mounting screws and washers. These

mounting bracket assembly and the gunner-linkage

items were retained in paragraph 5-23a(2).

assembly aft mounting bracket to the airframe. Retain the

screws.

(5) Refer to paragraph 5-19 for the gunner linkage

assembly installation procedures.

(1) Disconnect connector W1P2 from the EIA and

connector W1P1 from A3P1 on the gunner linkage.

(2) Remove the screw which secures each of the

(1) Secure the cable mounting bracket assembly to

three cable clamps to the airframe. Remove the clamps.

the airframe with the two screws retained in paragraph

Retain the clamps and screws.

5-23b(3).

(3) Remove the two screws that secure the cable

(2) Route the extension cable along the airframe and

mounting bracket assembly to the airframe. Retain the

connect W1P1 to A3P1 on the gunner linkage and W1P2 to

screws.

J4 on the EIA.

5-24. Disassembly and AssembIy (fig. B-15).

(3) Slip the three cable clamps on the cable and

Remove items (2) through (5). Assemble in reverse

secure each cable clamp to the airframe with a screw. The

disassembly sequence.

clamps and screws were retained in paragraph 5-23b(2).

5-15