CONTROL PANEL ASSEMBLY 2A1 REPAIR (cont)

CONTROL PANEL ASSEMBLY 2A1 REPAIR (cont) - TM-1-1270-476-30_337

CONTROL PANEL ASSEMBLY 2A1 REPAIR (cont) - TM-1-1270-476-30_339

TM-1-1270-476-30 Aviation Intermediate Manitenance Manual Target Acquisition Designation Sight (TADS) Assembly AN/ASQ-170
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TM 1-1270-476-30 4-248 4-29. CONTROL PANEL ASSEMBLY 2A1 REPAIR (cont) 14. SHOCK PAD REPLACEMENT REMOVAL a. Remove night filter assembly, 16 below. b. Remove damaged shock pad (1) by cutting and scraping with knife. INSTALLATION c. Prepare control panel assembly (2) by roughening surface contact area with 180 grit abrasive paper. d. Apply adhesive sealing compound to both contact surfaces (2 and 3) (para 2-6). e. Install night filter assembly (4), 16 below. f. Press new shock pad (1) to control panel assembly (2). g. Ensure night filter (4) moves properly. h. Tape shock pad (1) to control panel assembly (2). CURE i. Remove tape after curing for 24 hours at 67 to 87°F. END OF TASK

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