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Figure 6-5 ENGINE SERVICE INTERFACES -RIGHT SIDE
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DRAWING NUMBER TITLE
22-33-11 THRUST MANAGEMENT SYSTEM ENGINE SIGNALS
24-11-11 GENERATOR DRIVE -LEFT
24-21-11 POWER & REGULATION -LEFT GENERATOR
26-11-11 FIRE DETECTION -LEFT ENGINE
26-11-12 OVERHEAT DETECTION -LEFT ENGINE
26-11-12 OVERHEAT DETECTION -RIGHT ENGINE
26-11-21 FIRE DETECTION -RIGHT ENGINE
29-11-11 ENGINE HYDRAULIC PUMP -LEFT SHUTOFF & DEPRESS
36-11-61 AIR SUPPLY BLEED AIR -LEFT ENGINE HIGH PRESSURE CONTROL
36-23-11 AIR SUPPLY BUILT-IN TEST EQUIPMENT -LEFT
73-21-11 EEC CONTROL & INDICATION DISCRETES
73-21-13 THROTTLE LEVER ANGLE RESOLVER
73-21-14 EEC DATA BUSSES
73-21-15 EEC ECS DISCRETES
73-21-16 EEC ANTI-ICE DISCRETES
73-21-17 EEC DISCRETES
73-31-11 FUEL FLOW INDICATING SYSTEM
73-33-11 ENGINE FUEL PRESSURE INDICATION
73-34-11 ENGINE FUEL FILTER BYPASS WARNING
74-31-11 ENGINE IGNITION -LEFT ENGINE
75-32-12 VARIABLE BYPASS/STATOR VANES SERVO CONTROL SYSTEM -LEFT
76-11-11 ENGINE FUEL CONDITIONING CONTROL
76-11-21 FLIGHT/GROUND IDLE SELECT
77-12-11 ENGINE TACHOMETER SYSTEM -N1
77-12-12 ENGINE TACHOMETER SYSTEM -N2
77-21-11 ENGINE INDICATION -EXHAUST GAS TEMPERATURE
77-31-11 AIRBORNE VIBRATION MONITORING SYSTEM
78-31-11 THRUST REVERSER COWL DOOR OPENING SYSTEM -LEFT
78-34-11 THRUST REVERSER CONTROL -LEFT ENGINE
78-36-11 THRUST REVERSER POSITION INDICATING SYSTEM -LEFT ENGINE
79-31-11 OIL QUANTITY
79-32-11 ENGINE OIL PRESSURE INDICATION
79-33-11 LOW OIL PRESSURE WARNING SYSTEM
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Figure 6-6 ELECTRICAL WIRING DIAGRAMS (Continued)
DRAWING NUMBER TITLE
79-34-11 ENGINE OIL -TEMPERATURE INDICATION
79-35-11 ENGINE OIL -FILTER BYPASS WARNING
80-11-11 STARTING SYSTEM -LEFT
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6.6.4 Engine Hydraulic Interfaces for Test Cell 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：757 PW2000 Series Engine Ground Handling Document 发动机地面处理文件(24)
