a380 aircraft characteristics airport and maintenance planning ac
The content of this document is the property of Airbus. manual is issued for the A380 series aircraft to provide necessary data to airport operators ...
A380-800
Mar 2 2006 A380 Flight Deck and Systems Briefing for Pilots ... Airbus family aircrafts. ... Vertical speed manual pressurization mode: If the.
TRAINEES BOOKLET (FCTP extracts) A380 This document must be
Feb 5 2009 A380 JEPPESEN LEAFLET. -Airbus Training Airport
@AIRBUS
Dec 1 2016 manual is issued for the A380 series aircraft to provide necessary data to airport operators
DEPARTMENT OF TRANSPORTATION
May 27 2014 Airspeed Limits. Refer to the FAA approved Airbus Model A380-841
ENGINEERING BRIEF NO. 65A USE OF 150-FOOT- (45-M) WIDE
Dec 10 2007 150-Foot Wide Runways for Airbus A380 Operations
TYPE-CERTIFICATE DATA SHEET
Feb 7 2003 An agency of the European Union. TYPE-CERTIFICATE. DATA SHEET. No. EASA.A.110. AIRBUS A380. Type Certificate Holder: AIRBUS S.A.S.
Airbus A380-800 Report of the FCL/OPS Subgroup Report Revision
Jul 18 2011 EASA Operational Evaluation Board Airbus A380 – FCL & OPS ... 13 A380 Three Engine Ferry Flight (3EFF) ... Flight Crew Operating Manual.
DEPARTMENT OF TRANSPORTATION
Nov 8 2017 Refer to the FAA approved Airbus Model A380-841
Airplane Flying Handbook (FAA-H-8083-3B) Chapter 3
The flight instructor must impart competent knowledge of these basic flight maneuvers so that the beginning pilot is able to combine them at a performance level
STL 945.1380/05 Issue 1
A380A380--800800
Flight Deck and Systems Briefing for PilotsFlight Deck and Systems Briefing for PilotsIssue 02 - March 2006
Customer Services
STL 945.1380/05 Issue 2 Flight Deck and Systems Briefing for PilotsIntentionally Left Blank
STL 945.1380/05 Issue 2 Flight Deck and Systems Briefing for Pilots This brochure is issued for informational purposes only.It must not be used as an official reference.
Should any deviation appear between the information provided in this brochure and that published in the applicable operational or technical manuals, the latter shall prevail at all times. Any questions you may have on this brochure should be submitted to:AIRBUS SAS
Flight Operations Support and Services
Customer Services Directorate
1, Rond-Point Maurice Bellonte, BP33
31707 BLAGNAC Cedex - FRANCE
TELEX: AIRBU 530526F
SITA: TLSBI7X
Telefax: 33 5 61 93 29 68
A380-800
Flight Deck and Systems
Briefing for Pilots
STL 945.1380/05 Issue 2 Flight Deck and Systems Briefing for PilotsIntentionally Left Blank
STL 945.1380/05 Issue 2 Flight Deck and Systems Briefing for Pilots A380 Flight Deck and Systems Briefing for PilotsContents 1.General
2.ATA 25 Flight Deck Layout
3.ATA 21 & 36 Air Systems
4.ATA 22 Auto Flight System (AFS)
5.ATA 23 Communication
6.ATA 24 Electrical System
7.ATA 26 Fire and Smoke Protection
8.ATA 27 Flight Controls
9.ATA 27 Slats and Flaps
10.ATA 28 Fuel System
11.ATA 29 Hydraulic System
12.ATA 30 Ice and Rain Protection
13.ATA 31 Indicating/Recording Systems
14.ATA 32 Landing Gear
15.ATA 34 Navigation
16.ATA 35 Oxygen
17.ATA 42 Avionics Networks and IMA
18.ATA 45 Onboard Maintenance System (OMS)
19.ATA 46 Information Systems
20.ATA 49 Auxiliary Power Unit (APU)
21.ATA 70 EnginesList of Abbreviations
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STL 945.1380/05 Issue 1
1. General Flight Deck and Systems Briefing for PilotsFlight Deck and Systems Briefing for Pilots
1.Introduction
- General - Certification Basis - Dimensions 2.General Arrangement
- Typical Cabin Layout - Cargo Hold Capacity 3.Design Specifications
4.Performance
- General - Payload/Range - Takeoff Performance - Initial Cruise Altitude Capability 5.Weight and Balance
6.Ground Maneuvering Capability
Contents
STL 945.1380/05 Issue 2 Flight Deck and Systems Briefing for PilotsA380 General1.Introduction
The A380 is a Very Long Range (VLR), subsonic, civil transport aircraft. The design combines the in-service experience gained from the A330 and A340 aircraft operated all around the world with new technology developed specifically for the A380 program. The general arrangement is a four-engine configuration with rearward swept low wing and a conventional tail. The basic model is the A380-800 Long Range passenger model. • Design, construction and type certificate: JAR 25 at change 15 (FAR 25 amendments 1 to 98 exc. 87 and 96)Noise requirements: JAR 36 (plus 2 NPAs) equivalent to ICAO Annex 16 (Chapter 4)
Emission requirements: JAR 34
GeneralDimensions
Certification Basis
1.2 STL 945.1380/05 Issue 2 Flight Deck and Systems Briefing for PilotsA380 General2.General Arrangement
The A380 has a full-length double-deck fuselage.
The two passenger decks are referred to as the main and upper deck. Both decks are connected by cabin stairs and galley lifts.The cockpit is located between these two decks (
Refer to
Flight Deck Layout
The typical cabin layout is 555 seats. The passenger seating layout may vary, depending on the Operator's requirements. The two passenger decks offer a wide range of cabin arrangement possibilities.Each deck can have up to:10 seats abreast in each row of the main deck
8 seats abreast in each row of the upper deck.
Each deck can either be serviced from the main deck only, or from both decks simultaneously. The A380-800 aircraft has 8 pairs of large passenger doors (Type A). Five pairs are on the main deck and three pairs are on the upper deck.Typical Cabin Layout
Typical and Optional Arrangement
1.3 STL 945.1380/05 Issue 2 Flight Deck and Systems Briefing for PilotsA380 General2.General Arrangement
The lower deck is divided into three different cargo compartments: The forward cargo compartment, the aft cargo compartment, and the bulk cargo compartment.Cargo Hold Capacity 1.4 STL 945.1380/05 Issue 2 Flight Deck and Systems Briefing for PilotsA380 General3.Design Specifications
Design Weights
Design Speeds
372 000 kg394 000 kg510 000 kg512 000 kg
Option 1
361 000 kg386 000 kg560 000 kg562 000 kg
Standard
Option 2
571 000 kg
MRW366 000 kg
MZFW391 000 kg
MLW569 000 kg
MTOWDesign Specifications
= 0.55 M LE = 250 kt CAS V LE = 250 kt CAS (extension) = 250 kt CAS (retraction) = 220 kt CAS (gravity extension) V LO = 0.96 M D = 375 kt CAS V D = 0.89 M MO = 340 kt CAS V MO 1.5 STL 945.1380/05 Issue 2 Flight Deck and Systems Briefing for PilotsA380 General3.Design Specifications
•Pavement Strength•Slats and Flaps Design Speeds
182103323Landing
Design Speeds
VFE kt (CAS)
Ailerons (°)
Flaps (°)
Slats (°)
Function
Configuration
55 67 88 110
63 69 83 111
1400 x 530 x R23
Cat A Cat B Cat C Cat D
Cat A Cat B Cat C Cat D
Rigid Pavement
Flexible Pavement
ACNMain Landing Gear &
Body Landing Gear
tires (radial)Note : The Nose Landing Gear is equipped with 2 radial 1 270 x 455 x R22 tires. 1.6 STL 945.1380/05 Issue 2 Flight Deck and Systems Briefing for PilotsA380 General4.Performance
The A380 can be powered by two engine types:•The Rolls-Royce TRENT 900
The Engine Alliance GP7200.
General
Payload/Range
1.7 STL 945.1380/05 Issue 2 Flight Deck and Systems Briefing for PilotsA380 General4.Performance
Takeoff PerformanceInitial Cruise Altitude Capability 1.8 STL 945.1380/05 Issue 2 Flight Deck and Systems Briefing for PilotsA380 General5.Weight and Balance
1.9 STL 945.1380/05 Issue 2 Flight Deck and Systems Briefing for PilotsA380 General6.Ground Maneuvering Capability
The A380 can be towed or pushed up to a nosewheel
angle of 70 degrees from the aircraft centreline, at all weights up to the maximum ramp weight without mechanically disconnecting the steering.The A380 is capable of towbarless towing.
119.836.52
R5176.453.76R4107.232.66R3
150.9167.0
36.35ft
46.0150.91
11.08m69.5°70°
Type of turn 1:-
Asymmetric thrust
Differential braking
Effective Steering AngleSteering AngleAR6Y
1.10STL 945.1380/05 Issue 1
2. ATA 25 Flight Deck Layout Flight Deck and Systems Briefing for PilotsFlight Deck and Systems Briefing for Pilots
1.General
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