B767 ATA 25 Student Book

TRAINING MANUALFOR TRAINING PURPOSES ONLY

B767-3S2F ATA 25-00 Page - 1 3/15/13 EFF - ALL

CH 25

EQUIPMENT AND FURNISHING



TABLE OF CONTENTS

INTRODUCTION ................................................................................... 4

CAPTAIN'S AND FIRST OFFICER'S SEATS ....................................... 6

GALLEY .............................................................................................. 10

LOWER CARGO LOADING ............................................................. ... 12

EMERGENCY LOCATOR. ........................................................ .......... 16

EMERGENCY ESCAPE ROPES...........................................................18



STUDENT NOTES:



INTRODUCTION

General

Equipment/furnishings provide for the comfort and convenience of passengers and crew members, for handling and stowing cargo, and for ensuring passenger and crew safety in an emergency.

Flight Compartment

Seats for the captain, first officer, and one or two observers, are in the flight compartment. Flight compartment accommodations provide crew comfort and safety.

Main Cabin

The main cabin contains manual loading cargo system and AYK hazard shipping container system.

Cargo Compartments

Forward, aft, and bulk cargo compartments are in the lower lobe. Containerized cargo is stored in the forward and aft cargo compartments. Loose baggage is stored in the bulk cargo compartments, aft of the cargo compartment.

Emergency Equipment

Escape ropes in the flight compartment provide means of escape through flight compartment windows.



INTRODUCTION



CAPTAIN’S AND FIRST OFFICER’S SEATS

General

The captain's and first officer's seats mount on curved tracks allowing forward and aft adjustment through a range of 11 inches. The aft ends of the seat tracks are curved so that seats move outboard during the last four inches of aft travel to facilitate ingress/egress. Holes in the track provide for seat location.

Seats adjust vertically through a range of 6.5 inches. Backrests recline through a range of 25 degrees. Seat bottoms tilt through a range of a ten degrees. Armrests adjust up and down six inches. Armrests pivot up to be parallel to the backrest and slide to a stowed position which provides additional clearance for ingress/egress. Lumbar support adjustment knobs on each side of the backrest adjust the lumbar support vertically and forward/aft.

Control handles for seat adjustment are below the seat bottom, on the inboard side. Handles pull up to adjust seat. Handles are labeled: T for thigh adjustment (seat bottom tilt), V for vertical adjustment, H for horizontal adjustment, and R for recline adjustment. The armrest adjustment thumbscrew is on the underside of the armrest. Power adjustment control consists of two 3-way momentary action toggle switches, spring-loaded to the center (off) position, located forward of the fore/aft manual adjustment handles.

Restraints in the seats are crotch straps, lap belts, and inertial shoulder harness. The seat back can be used as a flotation device. Life vest stowage is provided in the back of the seats.

The seats can be removed by removing the forward limit stop on the forward outboard track and moving the seats forward until they clear the tracks.Installation is in the reverse order.



CAPTAIN’S AND FIRST OFFICER’S SEATS



GEAR PIN BOX/HAZ-MAT POUCH

General Location

Gear pin box and haz-mat pouch located on left side of flight deck aft of captain’s seat.



GEAR PIN BOX/HAZ-MAT POUCH



GALLEY

General

Electrical power for 115 volt AC powered equipment in the forward galley comes from the right generator bus. Electrical power for 28 volt DC powered controls for the forward galleys comes from the right bus. The forward galley is rated at 20 kva.



GALLEY



LOWER CARGO LOADING

General

There are three compartments in the lower lobe for cargo accommodations: the forward, aft and bulk cargo compartments. A divider (net) separates the bulk cargo compartment from the aft cargo compartment. The bulk cargo compartment has no conveying equipment. Bulk cargo is loaded and unloaded manually, and is restrained by cargo nets.

Containerized Cargo Compartments

The forward cargo compartment is divided into 8 bays and has a maximum capacity of 16 ld-2 containers. The compartment is also capable of handling ld-3, ld-4, and ld-8 containers. The aft compartment is similar to the forward compartment except the aft end of the compartment is equipped with retractable stops to permit loading cargo into the bulk cargo compartment when required and is divided into 7 bays. The aft compartment maximum capacity is 14 ld-2 containers. It can also handle the ld-3, ld-4 and ld-8 containers. The forward and aft cargo compartment doors are on the right side of the airplane.

Bulk Cargo Compartment

The capacity of the compartment is 430 cubic feet. Cargo is stowed in the compartment and secured by cargo nets. It is normally loaded through an inward opening door on the left side of the airplane.

When the bulk cargo door is open, the door protector can be manually raised. The door protector is lowered manually before door closure to insure that the area behind the door remains clear of cargo. The bulk cargo is held in place by nets, attached by snap fasteners to tie down fittings and surface mounted anchor fittings.



LOWER CARGO LOADING



LOWER CARGO HANDLING SYSTEM

General

The cargo handling system gets power for control and operating from the ground handling bus. The PSEU supplies the cargo door position. The cargo handling system operates only if the cargo door is fully open.

Operation

The forward exterior control panel controls the position of these electrical/mechanical components:

• Center stop/guide/lock • Auxiliary stop/guide/lock • Rollout stops • Power drive units • Lateral guides.

To supply power to the systems, these conditions must be true:

• Ground handling bus has power • Cargo door full open • SYSTEM POWER switch is ON.

Use the switches on the forward exterior control panel to configure the system. The switches let you set the type of operation (LOCK, LOAD, UNLOAD) and the forward interior panel lets you adjust for the type of cargo you need to load or unload (CONTAINERS OR PALLETS).

You use the cargo control joystick to move the ULDs FORWARD, AFT, IN or OUT. The cargo system controller uses manual inputs for system configuration and joystick position to operate the components.

The aft cargo system is similar to the forward system except for pallet operation.



LOWER CARGO HANDLING SYSTEM



EMERGENCY LOCATOR

Emergency Locator Transmitter (ELT)

The Emergency Locator Transmitter sends a signal when you put it in water. It is located on the back wall of Flight Deck.



EMERGENCY LOCATOR



EMERGENCY EQUIPMENT ESCAPE ROPES

General

The escape ropes are installed in compartments above the No. 2 windows inthe flight compartment.



ESCAPE ROPES



EMERGENCY DESCENT DEVICES

Purpose

The descent devices are used by the flight crew to evacuate the flight deck in an emergency.

Location

The six descent devices are installed on the rigid barrier, at ceiling height, across from the flight crew entry door. In use, the descent devices are removed from their container and will slowly lower the crew members to the ground.

Physical Description

The descent device is a coil of steel tape which is connected to the airplane at one end and has a handle attached to the other. The descent devices are housed in a container which has a hinged door on the bottom.

OperationThe weight of the flight crew member causes a spring-loaded brake inside the descent device to slow the tape uncoiling, which allows the flight crew member to be slowly lowered to the ground.

The emergency descent devices are designed to be maintenance free. They are time-controlled items, requiring removal and return to the manufacturer for inspection and recertification at the end of their warranty period, every five calendar years.

The only tasks required to be performed are removal, installation, and external cleaning. Inspection is limited to external condition, overall cleanliness, integrity of the safety deal, and compliance to warranty expiration date.

Inspection

The descent device must be removed from the container assembly for inspection. Open the container door and pull the descent device from the container by its handle.

The emergency descent device handle safety seals are the primary indicator that the handle has been extended. If only one side of the handle has safety

tape, do nothing. If both safety seals are broken or missing, remove the unit and inspect for proper stowage of the handle.

The safety tape over the grommet and grommet sealant at the opposite end of the descent device must also be inspected. If either the grommet safety tape or the grommet sealant has been broken, remove the unit and return it to an approved facility for overhaul.

If both are intact, check the expiration date of the unit on the handle/side plate. If expired, the unit must be replaced.

If grease or oil is found within the device casing, the unit must be replaced.

WARNING: DO NOT PUT LUBRICANTS INTO THE DESCENT DEVICE CASING. LUBRICANTS IN THE DESCENT DEVICE CAN CAUSE A MALFUNCTION WITH THE DESCENT DEVICE AND CAUSE INJURIES TO PERSONS.

Re-stow the descent device by inserting it into the container and pushing upward until the spring detent engages.



EMERGENCY DESCENT DEVICES

B767 ATA 25 Student Book

Documents

Transcript of B767 ATA 25 Student Book