PANEL CONTROL ASSEMBLY FOR BOEING 737 CIVIL AIRCRAFT. THE AUTOMATIC FLIGHT CONTROL SYSTEMS (AFCS) CONSIST OF THREE SYSTEMS: DIGITAL FLIGHT CONTROL SYSTEM (DFCS), YAW DAMPER SYSTEM & AUTOTHROTTLE SYSTEM. THE DFCS INCORPORATES TWO SPERATE CHANNELS. EACH CHANNEL CONTROLS THE PITCH AND ROLL AXES AND PROVIDES MACH TRIM AND SPEED TRIM CONTROL. THE MODE CONTROL PANEL IS MOUNTED ON THE GLARE SHIELD, ACCESSIBLE TO BOTH PILOTS. THE MCP CONSISTS OF A METAL HOUSING UNIT CONTAINING CONTROL SWITCHES, INDICATORS AND ELECTRONIC CIRCUITS ASSOCIATED WITH CONTROL FUNCTIONS GENERATED BY THE UNIT AND DISPLAYS OF STATUS AND MODES GENERATED BY THE FLIGHT CONTROL COMPUTER. THE FRONT PANEL OF THE UNIT IS EDGE LIGHTED. THE PANEL ALSO PROVIDES CONTROL OF PRESET HEADING, PRESET COURSE, ALTITUDE SELECT ENGAGE CONTROL, SPEED SELECTION AND VERTICAL SPEED SELECTION.

CLASSIFICATION HAS BEEN DETERMINED IN ACCORDANCE WITH THE FOLLOWING:- GENERAL INTERPRETATIVE RULES (GIR)S GIR 1 HAS BEEN USED TO CLASSIFY THIS PRODUCT BY THE TERMS OF HEADING 9014 - DIRECTION FINDING COMPASSES; OTHER NAVIGATIONAL INSTRUMENTS AND APPLIANCES. GIR 6 HAS BEEN USED TO CLASSIFY THE GOODS TO SUBHEADING LEVEL 901490 - PARTS AND ACCESSORIES. TARIC CODE 9014900010 OF INSTRUMENTS OF SUBHEADINGS 901410 AND 901420 FOR USE IN CIVIL AIRCRAFT. ALSO CLASSIFIED IN ACCORDANCE WITH:- HARMONISED SYSTEM EXPLANATORY NOTE (II)(B) (7) TO HEADING 9014