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System Description
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Require immediate crew attention. These messages are accompanied by flashing master warning, triple chime attenson with or without voice message or dedicated tone. Require immediate crew awareness and future crew action may be required in the form of alternate system selection or performance limitation. These message are accompanied by flashing master caution and a single chime. Indicate safe or normal system operation which require crew awareness, over and above the dark cockpit philosophy. Indicate minor failures or reduction in systems capability, which require no crew action.

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12/29/15

Overview

The engine nacelle electrical harnesses are attached to the pylon interface firewall with connectors. The harnesses in the nacelle electrically connect components on the engine to the aircraft systems.

There are three primary electrical harnesses in each nacelle: the full authority digital electronic control (FADEC) electrical harness, the generator control harness and the fire detection harness.

300_7150_00


12/29/15

Full Authority Digital Engine Control (FADEC) Electrical Harness

The FADEC electrical harness carries signals between the electronic control unit (ECU) and the aircraft systems. These signals control and operate the engine systems and supply data for display in the flight compartment. The harness is a loom of screened wires with four connectors. The harness is connected to the pylon interface, ECU, engine internal wiring harness, and thrust reverser. Clips attach the harness to the engine between the forward engine mount frame and the thrust reverser. Spring clips are installed around the top of the forward engine mount frame and at the thrust reverser interface. Grommets attached to the harness are installed in the spring clips.

300_7150_002

300_7150_002a


12/29/15

Generator Control Harness

The generator control harness carries signals to and from the generator. These signals control and operate the generator and supply data for display in the flight compartment. The harness is a loom of four screened wires with two connectors at each end. The harness is connected to the pylon interface and the generator. Grommets attached to the harness are installed in the spring clips between the fan inlet housing and the forward outer fan duct. P-clips attach the harness to the bottom of the forward outer fan duct between the generator and the pylon interface.

300_7150_003

1787


Fire Detection Harness

The fire detection harness assembly has the following three fire detection harnesses:

  • Gearbox
  • Zone 2
  • Pylon

The harnesses connect the sensing elements of the engine fire detection system. The gearbox fire detection harness connects the wet bay sensing element to the gearbox sensing element. The zone 2 harness connects the gearbox sensing element to the zone 2 sensing element and the zone 2 sensing element to the pylon fire detection harness. The pylon fire detection harness connects the zone 2 fire detection harness to the pylon sensing element.

The fire detection harnesses are installed around the engine with spring clips and P-clips which are attached to the engine and the outer fan duct. The harnesses have eye-end connectors attached to the electrical connectors on the sensor wires with screws, nuts and washers. The zone 2 fire detection harness and pylon fire detection harness are connected by an electrical connector.

300_7150_004

300_7150_005


12/29/15

System Interface

The engine electrical harnesses interface with the following systems/components:

  • Engine Fire Detection System
  • Fuel Control System
  • Fuel Indication System
  • Full-Authority Digital Engine Control (FADEC) System

10/22/20

Component Location Index

Component Location Index
IDENT DESCRIPTION LOCATION IPC REF
     - LEFT ENGINE ELECTRONIC CONTROL UNIT (ECU) A HARNESS PANEL(S) 432BT/BB
ZONE(S) 430
71-50-05
     - RIGHT ENGINE ELECTRONIC CONTROL UNIT (ECU) A HARNESS PANEL(S) 442BT/BB
ZONE(S) 440
71-50-05
     - LEFT ENGINE ELECTRONIC CONTROL UNIT (ECU) B HARNESS PANEL(S) 432BT/BB430 71-50-05
     - RIGHT ENGINE ELECTRONIC CONTROL UNIT (ECU) B HARNESS PANEL(S) 442BT/BB
ZONE(S) 440
71-50-05
     - LEFT ENGINE GENERATOR CONTROL ELECTRICAL HARNESS PANEL(S) 432BB
ZONE(S) 430
71-50-15
     - RIGHT ENGINE GENERATOR CONTROL ELECTRICAL HARNESS PANEL(S) 442BB
ZONE(S) 440
71-50-15
     - LEFT ENGINE  ZONE 2 FIRE DETECT ELECTRICAL HARNESS PANEL(S) 432BT/BB
ZONE(S) 430
71-50-19
     - RIGHT ENGINE ZONE 2 FIRE DETECT ELECTRICAL HARNESS PANEL(S) 442BT/BB
ZONE(S) 440
71-50-19
     - LEFT ENGINE PYLON FIRE DETECT ELECTRICAL HARNESS PANEL(S) 432BT/BB
ZONE(S) 430
71-50-23
     - RIGHT ENGINE PYLON FIRE DETECT ELECTRICAL HARNESS PANEL(S) 442BT/BB
ZONE(S) 440
71-50-23
     - LEFT ENGINE GEARBOX FIRE DETECT ELECTRICAL HARNESS PANEL(S) 432BT/BB
ZONE(S) 430
71-50-27
     - RIGHT ENGINE GEARBOX FIRE DETECT ELECTRICAL HARNESS PANEL(S) 442BT/BB
ZONE(S) 440
71-50-27


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