AIRBUS - AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING ppt

LOCATIONS CHGCODE DESCRIPTIONS OF CHANGE FIGURE Doors Clearances - Main Landing Gear Doors Bogie PART EFFECTIVITYADDED/REVISED/DELETEDSubject 2-7-8 ADDED/REVISED/DELETED PART EFFECTIVITY

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AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING

AC

The content of this document is the property of Airbus.

It is supplied in confidence and commercial security on its contents must be maintained.

It must not be used for any purpose other than that for which it is supplied, nor may information contained in it be disclosed to unauthorized persons.

It must not be reproduced in whole or in part without permission in writing from the owners of the copyright Requests for reproduction of any data in this document and the media authorized for it must be addressed to Airbus.

AIRBUS S.A.S.

Customer Services Technical Data Support and Services

31707 Blagnac Cedex FRANCE

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HIGHLIGHTS Revision No 27 - Jun 01/12

THE MFP AND AC MANUALS

PART EFFECTIVITYADDED/REVISED/DELETED

PAYLOAD DELETED

AND COMPLETED TITLE OFILLUSTRATIONS

DESCRIPTION TITLE UPDATEDFIGURE General Aircraft Dimensions -

Wing Tip Fence

Section 2-3

Subject 2-3-0

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LOCATIONS CHG

CODE

DESCRIPTIONS OF CHANGE

SHOW THE DIMENSIONS FOR A LIGHTAND HEAVY WEIGHT VARIANT

DELETED THE TERM ”OWE”

FIGURE Ground Clearances - Ground

Clearances with Sharklets

FIGURE Ground Clearances - Flaps and

Flap Track Fairings When Flaps Fully

Extended

FIGURE Ground Clearances - Flaps and

Flap Track Fairings When Flaps Fully

FIGURE Ground Clearances - Aileron Up

and Spoilers 1 to 5 Extended

ADDED/REVISED/DELETEDFIGURE Typical Configuration - Typical

Configuration Single-Class, High Density

PART EFFECTIVITYADDED/REVISED/DELETEDFIGURE Typical Configuration - Typical

Configuration Two-Class

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PART EFFECTIVITYADDED/REVISED/DELETEDFIGURE Passenger Compartment Cross-

section Economy Class, 6 Abreast

-Wider Aisle

PART EFFECTIVITYADDED/REVISED/DELETEDFIGURE Passenger Compartment Cross-

section - Passenger Compartment

Cross-section, First-class

Subject 2-6-0

ADDED/REVISED/DELETEDFIGURE Cargo Compartments -

Locations, Dimensions and Loading

ADDED/REVISED/DELETEDFIGURE Doors Clearances - Forward

Passenger / Crew Doors

PART EFFECTIVITYADDED/REVISED/DELETEDSubject 2-7-2

ADDED/REVISED/DELETED

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ADDED/REVISED/DELETEDFIGURE Doors Clearances - Aft Passenger

/ Crew Doors

ADDED/REVISED/DELETEDFIGURE Doors Clearances - Forward

Cargo Compartment Door

ADDED/REVISED/DELETEDFIGURE Doors Clearances - Aft Cargo

Compartment Door

ADDED/REVISED/DELETEDFIGURE Doors Clearances - Bulk Cargo

Compartment Door

ADDED/REVISED/DELETEDFIGURE Doors Clearances - Main Landing

Gear Doors

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LOCATIONS CHG

CODE

FIGURE Doors Clearances - Main Landing

Gear Doors (Bogie)

ADDED/REVISED/DELETEDFIGURE Doors Clearances - APU and

Nose Landing Gear Doors

FIGURE Landing Gear - Main Landing

Gear - Twin Wheel

Gear Dimensions - Twin Wheel

Gear - Four Wheels - Bogie

Gear Dimensions - Four Wheels - Bogie

FIGURE Landing Gear - Nose Landing

Gear

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FIGURE Landing Gear Maintenance Pits

-Maintenance Pit Envelopes

FIGURE Landing Gear Maintenance Pits

-Maintenance Pit Envelopes

FIGURE Auxiliary Power Unit - Access

FIGURE Power Plant Handling - Major

Dimensions - CFM56 Series Engine

FIGURE Power Plant Handling - Fan

Cowls - CFM56 Series Engine

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LOCATIONS CHG

CODE

FIGURE Power Plant Handling - Thrust

Reverser Cowls - CFM56 Series Engine

Dimensions - IAE V2500 Series Engine

FIGURE Power Plant Handling - Fan

Cowls - IAE V2500 Series Engine

FIGURE Power Plant Handling - Thrust

Reverser Halves - IAE V2500 Series

Engine

FIGURE Jacking for Maintenance

-Jacking Point Location

-Forward Jacking Point

FIGURE Loads at the Aircraft Jacking

Points Forward Fuselage Jacking Point

-Twin Wheel/Bogie

FIGURE Loads at the Aircraft Jacking

Points - Wing Jacking Point Rib 8 - Twin

Wheel/Bogie

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LOCATIONS CHG

CODE

-Location of Shoring Cradles

FIGURE Landing Gear Jacking for Wheel

Change MLG Jacking Point Location

-Twin Wheels

Change - MLG Jacking with Cantilever

Jack - Twin Wheels

Change Loads at MLG Jacking Points

-Twin Wheels

Change - MLG Jacking Point Location

Bogie

-Bogie Version

-77 000 kg

Change - NLG Jacking - Point Location

Change - Loads at NLG Jacking Points

Change Loads at NLG Jacking Points

-77 000 kg

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Subject 3-2-0

ADDED/REVISED/DELETEDSubject 3-2-1

ADDED/REVISED/DELETEDFIGURE Payload / Range - CFM56-5A

series engine

PART EFFECTIVITYADDED/REVISED/DELETEDFIGURE Payload / Range - CFM56-5B

series engine

PART EFFECTIVITYADDED/REVISED/DELETEDFIGURE Payload / Range - IAE V2500-

A1 series engine

PART EFFECTIVITYADDED/REVISED/DELETEDFIGURE Payload / Range - IAE V2500-

A5 series engine

PART EFFECTIVITYADDED/REVISED/DELETEDSection 3-3

Subject 3-3-0

ADDED/REVISED/DELETEDFIGURE FAR / JAR Take-off Weight

Limitation - ISA Conditions CFM56

series engine

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LOCATIONS CHG

CODE

FIGURE FAR / JAR Take-off Weight

Limitation - ISA Conditions IAE V2500

series engine

ADDED/REVISED/DELETEDFIGURE FAR / JAR Take-off Weight

Limitation - ISA +15˚C (+59˚F)

Conditions CFM56 series engine

PART EFFECTIVITYADDED/REVISED/DELETEDFIGURE FAR / JAR Take-off Weight

Limitation - ISA +15˚C (+59˚F)

Conditions IAE V2500 series engine

Subject 3-4-0

ADDED/REVISED/DELETEDFIGURE FAR / JAR Landing Field Length

- CFM56 series engine

PART EFFECTIVITYADDED/REVISED/DELETEDFIGURE FAR / JAR Landing Field Length

- IAE V2500 series engine

Subject 3-5-0

ADDED/REVISED/DELETEDFIGURE Final Approach Speed - CFM56

series engine

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Section 4-1

Subject 4-1-0

ADDED/REVISED/DELETEDSection 4-2

Subject 4-2-0

ADDED/REVISED/DELETEDFIGURE Turning Radii, No Slip Angle -

Turning Radii Dual Landing Gear

FIGURE Turning Radii, No Slip Angle

-Turning Radii Dual Landing Gear

-Turning Radii Bogie Landing Gear

Subject 4-4-0

Visibility from Cockpit in Static Position N

FIGURE Visibility from Cockpit in Static

Position

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LOCATIONS CHG

CODE

FIGURE Binocular Visibility Through

Windows from Captain Eye Position

ADDED/REVISED/DELETEDFIGURE 135˚ Turn - Runway to Taxiway

- Cockpit Over Centerline Method

PART EFFECTIVITYADDED/REVISED/DELETEDFIGURE 135˚ Turn - Runway to Taxiway

- Judgemental Oversteering Method

Subject 4-5-2

ADDED/REVISED/DELETEDFIGURE 90˚ Turn - Runway to Taxiway -

Cockpit Over Centerline Method

PART EFFECTIVITYADDED/REVISED/DELETEDFIGURE 90˚ Turn - Runway to Taxiway -

Judgemental Oversteering Method

FIGURE 135˚ Turn - Taxiway to Taxiway

Subject 4-5-5

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LOCATIONS CHG

CODE

FIGURE 90˚ Turn - Taxiway to Taxiway

THE GATE” TO ”TYPICAL RAMPLAYOUT - OPEN APRON” ADDED

”STAND SAFETY LINE” DEFINITION.DESCRIPTION TITLE UPDATEDFIGURE Typical Ramp Layout - Open

Apron - Bulk Loading

FIGURE Typical Ramp Layout - Open

Apron - ULD Loading

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LOCATIONS CHG

CODE

AN OPEN APRON” TO ”TYPICAL RAMPLAYOUT - GATE” ADDED ”STANDSAFETY LINE” DEFINITION

DESCRIPTION TITLE UPDATED

Terminal Operation - Minimum Servicing

Turn Round Time

CONNECTIONS LAYOUT TABLE

PART EFFECTIVITYADDED/REVISED/DELETEDFIGURE Ground Service Connections -

Ground Service Connections Layout

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Grounding Points

ADDED/REVISED/DELETEDFIGURE Hydraulic System - Green System

Ground Service Panel

PART EFFECTIVITYADDED/REVISED/DELETEDFIGURE Hydraulic System - Blue System

Ground Service Panel

PART EFFECTIVITYADDED/REVISED/DELETEDFIGURE Hydraulic System - Yellow

System Ground Service Panel

ADDED/REVISED/DELETEDFIGURE Ground Service Connections -

External Power Receptacles

ADDED/REVISED/DELETEDNOTE AMENDED

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Refuel/Defuel Couplings

Gravity Refuel Couplings

Overpressure Protector and NACA Flame

Arrestor

AND NACA FLAME ARRESTORILLUSTRATION

ILLUSTRATION ADDEDSubject 5-4-7

OPTIONAL FOR A320

UPDATED ACCESS PANEL 133AL ASOPTIONAL FOR A320

PART EFFECTIVITYADDED/REVISED/DELETEDNOTE AMENDED

FIGURE Ground Service Connections

-Potable Water Ground Drain Panel

Engine Oil Tank CFM56 Series Engine

IDG Oil Tank CFM56 Series Engine

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LOCATIONS CHG

CODE

FIGURE Ground Service Connections

-Starter Oil Tank CFM56 Series Engine

Engine Oil Tank IAE V2500 Series

Engine

IDG Oil Tank IAE V2500 Series Engine

Starter Oil Tank IAE V2500 Series

Engine

APU Oil Tank

Waste Water Ground Service Panel

Subject 5-5-0

ADDED/REVISED/DELETEDCROSS REFERENCED DOCUMENTARYUNIT ADDED/REVISED/DELETEDFIGURE Engine Starting Pneumatic

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LOCATIONS CHG

CODE

FIGURE Engine Starting Pneumatic

Requirements - Low Ambient

Temperature -40˚C (-40˚F) CFM56

series engine

Requirements - Low Ambient

Temperature -40˚C (-40˚F) IAE V2500

series engine

PART EFFECTIVITYADDED/REVISED/DELETEDFIGURE Engine Starting Pneumatic

Requirements - Medium Ambient

Temperature +15˚C (+59˚F) CFM56

series engine

Requirements - Medium Ambient

Temperature +15˚C (+59˚F) IAE

V2500 series engine

PART EFFECTIVITYADDED/REVISED/DELETEDFIGURE Engine Starting Pneumatic

Requirements - High Ambient

Temperature +55˚C (+131˚F) CFM56

series engine

Requirements - High Ambient

Temperature +50˚C (+122˚F) IAE

V2500 series engine

Subject 5-6-0

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LOCATIONS CHG

CODE

ADDED A NOTE FOR GROUNDPNEUMATIC POWER REQUIREMENTS.PART EFFECTIVITY

Subject 5-6-1

ADDED/REVISED/DELETEDFIGURE Ground Pneumatic Power

Requirements - Heating

ADDED/REVISED/DELETEDFIGURE Ground Pneumatic Power

Requirements - Cooling

Subject 5-7-0

ADDED/REVISED/DELETEDFIGURE Preconditioned Airflow

Requirements

Subject 5-8-0

FIGURES CORRESPONDING TO TYPICALTOW BAR CONFIGURATION DELETEDPART EFFECTIVITY

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EXTERNAL CLEANING AREAS.

Engine Exhaust Velocities Contours

-Ground Idle Power

ADDED/REVISED/DELETEDFIGURE Engine Exhaust Velocities -

Ground Idle Power CFM56 series engine

PART EFFECTIVITYADDED/REVISED/DELETEDFIGURE Engine Exhaust Velocities -

Ground Idle Power IAE V2500 series

engine

Engine Exhaust Temperatures Contours

-Ground Idle Power

ADDED/REVISED/DELETEDFIGURE Engine Exhaust Temperatures -

Ground Idle Power CFM56 series engine

PART EFFECTIVITYADDED/REVISED/DELETEDFIGURE Engine Exhaust Temperatures -

Ground Idle Power IAE V2500 series

engine

-Breakaway Power

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LOCATIONS CHG

CODE

FIGURE Engine Exhaust Velocities

-Breakaway Power CFM56 series engine

Breakaway Power IAE V2500 series

engine

-Breakaway Power

Breakaway Power CFM56 series engine

Breakaway Power IAE V2500 series

engine

-Takeoff Power

ADDED/REVISED/DELETEDFIGURE Engine Exhaust Velocities -

Takeoff Power CFM56 series engine

Takeoff Power IAE V2500 series engine

-Takeoff Power

Takeoff Power CFM56 series engine

Takeoff Power IAE V2500 series engine

Subject 6-2-0

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ADDED/REVISED/DELETEDFIGURE Airport and Community Noise -

CFM56-5A series engine

PART EFFECTIVITYADDED/REVISED/DELETEDFIGURE Airport and Community Noise -

CFM56-5B series engine

PART EFFECTIVITYADDED/REVISED/DELETEDFIGURE Airport and Community Noise -

IAE V2500 series engine

Subject 6-3-0

ADDED/REVISED/DELETEDFIGURE Danger Areas of Engines -

CFM56 series engine

PART EFFECTIVITYADDED/REVISED/DELETEDFIGURE Danger Areas of Engines - IAE

V2500 series engine

ADDED/REVISED/DELETEDFIGURE Danger Areas of Engines -

CFM56 series engine

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Subject 6-4-0

ADDED/REVISED/DELETEDFIGURE Exhaust Velocities and

Temperatures - APU APIC &

GARRETT

PART EFFECTIVITYADDED/REVISED/DELETEDCHAPTER 7

Section 7-3

Subject 7-3-0

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LOCATIONS CHG

CODE

Section 7-4

Subject 7-4-0

SECTION 7-4-1 LANDING GEAR LOADING

ON PAVEMENT

ADDED/REVISED/DELETEDFIGURE Landing Gear Loading on

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Flexible Pavement Requirements - U.S.

Army Corps of Engineers Design Method

SECTION 7-5-1 FLEXIBLE PAVEMENTREQUIREMENTS

Flexible Pavement Requirements - U.S

Army Corps of Engineers Design Method

CODE ”P”

PART EFFECTIVITYADDED/REVISED/DELETEDCROSS REFERENCED DOCUMENTARYUNIT ADDED/REVISED/DELETEDNOTE AMENDED

FIGURE Flexible Pavement Requirements

- Flexible Pavement Requirements

R

Section 7-6

Subject 7-6-0

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SECTION 7-6-1 FLEXIBLE PAVEMENTREQUIREMENTS.

Flexible Pavement Requirements - LCN

Conversion

CODE ”P”

PART EFFECTIVITYADDED/REVISED/DELETEDFIGURE Flexible Pavement Requirements

Rigid Pavement Requirements - Portland

Cement Association Design Method

SECTION 07-07-01 RIGID PAVEMENTREQUIREMENTS (PCA)

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LOCATIONS CHG

CODE

Rigid Pavement Requirements - Portland

Cement Association Design Method

CODE ”P”

PART EFFECTIVITYADDED/REVISED/DELETEDCROSS REFERENCED DOCUMENTARYUNIT ADDED/REVISED/DELETEDNOTE AMENDED

FIGURE Rigid Pavement Requirements

(Reference: Portland Cement Association)

Rigid Pavement Requirements - LCN

Conversion

PART EFFECTIVITYADDED/REVISED/DELETEDFIGURE Rigid Pavement Requirements -

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ADDED/REVISED/DELETEDFIGURE Radius of Relative Stiffness -

(Effect E and µ on ”L” values)

Subject 7-9-0

SECTION 7-9-1 AND 7-9-2

Aircraft Classification Number - Flexible

Pavement

CODE ”P”

PART EFFECTIVITYADDED/REVISED/DELETEDFIGURE Aircraft Classification Number

Flexible Pavement

R

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Aircraft Classification Number - Rigid

Pavement

CODE ”P”

PART EFFECTIVITYADDED/REVISED/DELETEDFIGURE Aircraft Classification Number

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FIGURE Highly Flammable and Hazardous

Materials and Components

FIGURE FWD and AFT Lower Deck

Cargo Doors

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LIST OF EFFECTIVE CONTENT Revision No 27 - Jun 01/12

CODE

LAST REVISION DATE

Subject 2-3-0

FIGURE Ground Clearances - Flaps and Flap Track Fairings When

Flaps Fully Extended

FIGURE Ground Clearances - Flaps and Flap Track Fairings When

Flaps Fully Extended

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CONTENT CHG

CODE

FIGURE Typical Configuration - Typical Configuration Single-Class,

High Density

Subject 2-5-0

FIGURE Passenger Compartment Cross-section - Economy Class, 6

Abreast - Wider Aisle

FIGURE Passenger Compartment Cross-section - Passenger

Compartment Cross-section, First-class

Subject 2-6-0

FIGURE Cargo Compartments - Locations, Dimensions and Loading

Subject 2-7-2

Subject 2-7-3

Subject 2-7-4

Subject 2-7-5

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CONTENT CHG

CODE

Subject 2-7-6

Subject 2-7-7

Subject 2-7-8

Subject 2-7-9

Subject 2-8-0

Subject 2-9-0

FIGURE Landing Gear - Main Landing Gear Dimensions - Four

Wheels - Bogie

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CONTENT CHG

CODE

Subject 2-10-0

Subject 2-11-0

Subject 2-12-0

FIGURE Power Plant Handling - Major Dimensions - CFM56 Series

FIGURE Power Plant Handling - Thrust Reverser Cowls - CFM56

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CONTENT CHG

CODE

Subject 2-14-0

FIGURE Loads at the Aircraft Jacking Points - Forward Fuselage

Jacking Point - Twin Wheel/Bogie

FIGURE Loads at the Aircraft Jacking Points - Wing Jacking Point

Rib 8 - Twin Wheel/Bogie

FIGURE Landing Gear Jacking for Wheel Change - MLG Jacking

Point Location - Twin Wheels

FIGURE Landing Gear Jacking for Wheel Change - MLG Jacking with

Cantilever Jack - Twin Wheels

FIGURE Landing Gear Jacking for Wheel Change - Loads at MLG

Jacking Points - Twin Wheels

Point Location Bogie

Jacking Points - Bogie Version

Jacking Points - 77 000 kg

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CONTENT CHG

CODE

FIGURE Landing Gear Jacking for Wheel Change NLG Jacking

Subject 3-3-0

Subject 3-3-1

FIGURE FAR / JAR Take-off Weight Limitation - ISA Conditions

CFM56 series engine

FIGURE FAR / JAR Take-off Weight Limitation - ISA Conditions

IAE V2500 series engine

Subject 3-3-2

FIGURE FAR / JAR Take-off Weight Limitation - ISA +15˚C

(+59˚F) Conditions CFM56 series engine

FIGURE FAR / JAR Take-off Weight Limitation - ISA +15˚C

(+59˚F) Conditions IAE V2500 series engine

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CONTENT CHG

CODE

Subject 3-4-0

Subject 3-4-1

Subject 3-5-0

CHAPTER 4

Subject 4-1-0

Subject 4-2-0

FIGURE Turning Radii, No Slip Angle - Turning Radii Dual Landing

Subject 4-4-0

FIGURE Binocular Visibility Through Windows from Captain Eye

Position

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CONTENT CHG

CODE

Subject 4-5-0

Subject 4-5-1

FIGURE 135˚ Turn - Runway to Taxiway - Cockpit Over Centerline

FIGURE 90˚ Turn - Runway to Taxiway - Cockpit Over Centerline

Subject 4-5-4

FIGURE 135˚ Turn - Taxiway to Taxiway - Cockpit Over Centerline

Method

Subject 4-5-5

FIGURE 90˚ Turn - Taxiway to Taxiway - Cockpit Over Centerline

Method

Subject 4-6-0

CHAPTER 5

Subject 5-0-0

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CONTENT CHG

CODE

Subject 5-1-3

Subject 5-2-0

Subject 5-3-0

Subject 5-4-0

Subject 5-4-1

FIGURE Ground Service Connections - Ground Service Connections

Layout

Subject 5-4-2

Subject 5-4-3

Tiêu đề	Aircraft Characteristics Airport And Maintenance Planning
Trường học	Airbus S.A.S.
Chuyên ngành	Aircraft Characteristics
Thể loại	Technical Data Support and Services
Năm xuất bản	2005
Thành phố	Blagnac Cedex

Định dạng
Số trang	607
Dung lượng	5,65 MB