A350 vs A330 Aircraft Systems Comparison

Flight Deck and Systems Briefing for Pilots A350 ↔ A330 Comparison Issue 2.0 – Sep 2013 A350 ↔ A330 Comparison This brochure is issued by Customer Services for information 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 S.A.S. All rights reserved. Confidential and proprietary document. AIRBUS Flight Operations and Training Support Customer Services Directorate 1, Rond-Point Maurice Bellonte, BP33 31707 BLAGNAC Cedex – FRANCE Telefax: +33 5 61 93 29 68 E-mail: fltops.A350std@airbus.com PR1010081 A350 ↔ A330 Comparison Intro - 2 / 9 Proprietary document By taking delivery of this Brochure, you accept on behalf of your company to comply with the following. No other property rights are granted by the delivery of this Brochure than the right to read it, for the sole purpose of information. This Brochure, its content, illustrations and photos shall not be modified nor reproduced without prior written consent of Airbus S.A.S. This Brochure and the materials it contains shall not, in whole or in part, be sold, rented, or licensed to any third party subject to payment or not. This Brochure may contain market-sensitive or other information that is correct at the time of going to press. This information involves a number of factors which could change over time, affecting the true public representation. Airbus assumes no obligation to update any information contained in this document or with respect to the information described herein. The statements made herein do not constitute an offer or form part of any contract. They are based on Airbus information and are expressed in good faith but no warranty or representation is given as to their accuracy. When additional information is required, Airbus S.A.S can be contacted to provide further details. Airbus S.A.S shall assume no liability for any damage in connection with the use of this Brochure and the materials it contains, even if Airbus S.A.S has been advised of the likelihood of such damages. This licence is governed by French law and exclusive jurisdiction is given to the courts and tribunals of Toulouse (France) without prejudice to the right of Airbus to bring proceedings for infringement of copyright or any other intellectual property right in any other court of competent jurisdiction. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Statement of offer The A350 XWB program is currently in development. The description provided in this document including characteristics, features and functions represents the currently best available knowledge. Final description of basic and customization optional features may evolve through the design development process. Airbus reserves the right to change, remove or add features and/or characteristics of the basic aircraft design and of the customization possibilities described in this document. The terms and conditions under which the A350 XWB will be finally offered will be determined in the Purchase Agreement between Airbus and the Buyer relating to the sale and purchase of the A350 XWB aircraft. In the event of any inconsistency between the provisions of this document and the provisions of the Purchase Agreement, the provisions of the Purchase Agreement shall prevail. PR1010081 A350 ↔ A330 Comparison Intro - 3 / 9 Preamble Objective of the document © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. In the scope of the Airbus Flight operational Commonality demonstration, this document provides a comparison between A350 and A330 to help substantiate the training credits. It illustrates by ATA chapters the Common and Specific features (functions) of each aircraft. It focuses primarily on the human machine interface from a pilot’s perspective. PR1010081 A350 ↔ A330 Comparison Intro - 4 / 9 Airbus Commonality Philosophy Current Status Definitions Same/Common Type Rating (STR - CTR): A single licence endorsement for 2 aircraft with familiarisation or difference training. Cross Crew Qualification (CCQ): Shortened training instead of full transition training to acquire an aircraft type rating. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Mixed Fleet Flying (MFF) : The operation of multiple aircraft types, requiring different type ratings, with one pool of pilots. 11 aircraft models PR1010081 A350 ↔ A330 Comparison 4 basic types Intro - 5 / 9 Airbus Commonality Philosophy Expanding the family with the A350 XWB A350 XWB commonality with the A330 Around 75% of the A350 XWB aircraft sold to date have been ordered by A330 operators. Consequently, Airbus has decided to pursue regulatory approval of a Common Type Rating for the A330 and A350 XWB. If granted, A330 pilots are expected to qualify on the A350 XWB without full flight simulator time and to then be able to fly both aircraft under a single license endorsement. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. A350 XWB commonality with the A320 Family, A340 and A380 CCQ, which includes full flight simulator sessions, will be available for A320 Family, A340 and A380 pilots. Airbus will also support airlines wishing to implement MFF with A350 XWB and A320 Family, A340 or A380 aircraft. PR1010081 A350 ↔ A330 Comparison Intro - 6 / 9 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Cockpit overview PR1010081 A350 ↔ A330 Comparison Intro - 7 / 9 Contents © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. How to Use the Brochure ATA 25 ATA 21 & 36 ATA 22 ATA 23 ATA 24 ATA 26 ATA 27 ATA 28 & 47 ATA 29 ATA 30 ATA 31 ATA 32 ATA 33 ATA 34 ATA 35 ATA 42 ATA 45 ATA 46 ATA 49 ATA 52 ATA 70 PR1010081 A350 ↔ A330 Comparison General Characteristics Flight Deck Layout Air Systems Automatic Flight System Communications Electrical System Fire and Smoke Protection Flight Controls Fuel System Hydraulic System Ice and Rain Protection Indicating and Recording Landing Gear Lights Navigation Oxygen System Avionics Network Onboard Maintenance System Information Systems and ATC Communication System Auxiliary Power Unit Doors Engines Abbreviations Intro - 8 / 9 How to use the brochure Each slide is built in the same way. The differences are highlighted using: • A yellow background, or • An arrow with a legend on a yellow background. ATA Chapter System described Highlight of the differences © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. The described system on the A330 The described system on the A350 ATA and page number PR1010081 A350 ↔ A330 Comparison Intro - 9 / 9 A350 A330 Comparison Flight↔ Deck and Systems Briefing for Pilots General General – General Arrangement A330-200 A350-900 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. 17.30 m 17.05 m 58.37 m 66.8 m 60.30 m 64.75 m 18.74 m The A330 is a medium to long range passenger aircraft. PR1010081 A350 ↔ A330 Comparison 21 m The A350 is a long range passenger aircraft. GENERAL - 2 / 8 General – General Arrangement A330-200 A350-900 A350-900 A330-200 A330-200 A350-900 60.30 m (198 ft) 64.75 m (212 ft 5.2 in) Fuselage length 58.37 m( 191 ft 3 in) 66.8 m (219 ft 2.0 in) Fuselage cross-section (constant part) 5.64 m (222 in) width 6.09 m (239.8 in) height 5.96 m (234.6 in) width Overall height 17.30 m (57 ft 1 in) 17.05 m(55 ft 3.0 in) © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Wing span Typical layout: 256 seats Typical layout: 315 seats The A330 has the following lower deck cargo compartments: • Forward cargo compartment (14 AKE (LD3) or 4 pallets 96”) • Aft cargo compartment (12 AKE (LD3) or 4 pallets 96”) • Bulk cargo compartment (695 ft3). The A350 has the following lower deck cargo compartments: • Forward cargo compartment (20 AKE (LD3) or 6 pallets 96”) • Aft cargo compartment (16 AKE (LD3) or 5 pallets 96”) • Bulk cargo compartment (400 ft3). PR1010081 A350 ↔ A330 Comparison GENERAL - 3 / 8 General – Design Weights A330-200 A350-900 A330-200 A350-900 Maximum Take Off Weight (MTOW) 238 000 kg 524 700 lb 275 000 kg 606 271 lb Maximum Landing Weight (MLW) 182 000 kg 401 241 lb 207 000 kg 456 356 lb Maximum Zero Fuel Weight (MZFW) * Fuel density: 0.8 kg/l 168 000 kg 370 376 lb 195 700 kg 431 444 lb 139 090 l (111 272 kg) 36 744 US Gal (245 313 lb) 140 795 l (110 524 kg) 37 194 US Gal (248 306 lb) Maximum fuel capacity* © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. * Fuel density: 0.785 kg/l Note: the weights depend on the Weight Variant of the aircraft. PR1010081 A350 ↔ A330 Comparison GENERAL - 4 / 8 General – Design Speeds A330-200 A350-900 A330-200 A350-900 Maximum operating speed (VMO) 330 kt CAS 340 kt CAS Maximum operating Mach (MMO) 0.86 0.89 Maximum landing gear operating speed (VLO) 250 kt CAS 200 kt CAS (gravity extension) 250 kt CAS 250 kt CAS (gravity extension) Maximum landing gear extended speed (VLE) 250 kt CAS 250 kt CAS © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. The A350 has greater maximum operating speed and MACH number. PR1010081 A350 ↔ A330 Comparison GENERAL - 5 / 8 General – Pavement Strength A330-200 ACN Flexible pavement © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Rigid pavement A350-900 A330-200 A350-900 Cat A 53 66 Cat B 62 70 Cat C 73 79 Cat D 86 109 Cat A 58 64 Cat B 63 71 Cat C 72 82 Cat D 98 95 PR1010081 A350 ↔ A330 Comparison GENERAL - 6 / 8 General – Weight and Balance © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. A330-200 A350-900 Takeoff Flight Landing Zero Fuel PR1010081 A350 ↔ A330 Comparison GENERAL - 7 / 8 General – Payload Range A330-200 Standard day conditions Typical international flight profile 95 kg per passenger including baggage. A350-900 315 passengers © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. 246 passengers PR1010081 A350 ↔ A330 Comparison GENERAL - 8 / 8 A350 A330 Comparison Flight↔ Deck and Systems Briefing for Pilots Flight Deck Layout ATA 25 ATA 25 – Cockpit view A330-200 The cockpit layout is similar. A350-900 Overhead panel Glareshield Main instrument panel © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Pedestal The A330 Cockpit has: • A captain seat • A first officer seat • A third occupant seat • A fourth occupant seat (optional) • A coat stowage. Third and fourth occupants each have a console with an oxygen mask. Each pilot has an optional EFB integrated to the sliding table. Each pilot lateral console has: • One sidestick • One steering handwheel • One oxygen mask. PR1010081 A350 ↔ A330 Comparison The A350 Cockpit has: • A captain seat • A first officer seat • A third occupant seat • A fourth occupant seat • A coat stowage. Each pilot lateral console has: • One sidestick • A steering handwheel • One oxygen mask • One stowed laptop. Third and fourth occupants each have a console with an oxygen mask. The cockpit is also equipped with an Onboard Maintenance Terminal (OMT) for maintenance staff. ATA 25 - 2 / 8 ATA 25 – Main Controls © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. A330-200 PR1010081 A350 ↔ A330 Comparison The controls layout is similar. A350-900 ATA 25 - 3 / 8 ATA 25 – Main Instrument Panel A330-200 A350-900 Autoland Autoland HUD CP MASTER WARN/CAUT Priority stick MASTER WARN/CAUT Priority stick FCU FCU EFIS CP PFD AFS CP ND EFIS CP EFIS CP LG ND PFD OIS PFD and ND ISIS AFS CP EFIS CP ED, SD, Mailbox and WD L G PFD and ND MFDs ECAM SWITCHING DCDU (optional) DCDU (optional) OIS ISIS (optional) ISIS © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. SWITCHING SD ED PFD ED Mailbox SD WD ND Memo, WD VD Permanent data Permanent data Note: Differences are explained in the other chapters. PR1010081 A350 ↔ A330 Comparison ATA 25 - 4 / 8 ATA 25 – Pedestal A330-200 A350-900 SWITCHING ECP MCDU © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. RMP T R I M THRUST LEVERS T R I M ACP CKPT LT CKPT LT SURV ATC ENG MASTER SPEED BRAKE RMP RMP ECP SPEED BRAKE SURV FLAPS PRK ACCU BRK TRIMs LG CKPT GRVTY CKPT LT EXTN DOOR FLAPS PRK BRK COCKPIT DOOR KCCU ENG MASTER RMP ACP THRUST LEVERS KCCU MCDU RMP MCDU printer printer RUDDER TRIM PR1010081 A350 ↔ A330 Comparison Note: Differences are explained in the other chapters. ATA 25 - 5 / 8 ATA 25 – Overhead A330-200 A350-900 CKPT DOOR CTLR RESET MAINTENANCE RESET BAT RESET MAINTENANCE RESET CVR CABIN FIRE ADIRS CVR FIRE © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. ACP EVAC APU FIRE HYD F/CTL FUEL RMP FUEL EMER ELEC F/CTL CARGO AIR COND ELEC GPWS OXYGEN AIR CALLS WIPER FUEL JETTISON (optional) ANTI ICE EXT LT CARGO SMOKE VENT CABIN P A P U * EMER ELEC INT LT SIGNS PR1010081 A350 ↔ A330 Comparison WIPER ENG MODE OIS ADIRS HYD F/CTL FUEL F/CTL ELEC CARGO AIR COND ELT * RCDR OXYGEN WIPER *** AIR EVAC CALLS GND HYD ANTI ICE EXT LT VENT CABIN P A P U INT LT ** WIPER SIGNS Note: Differences are explained in the other chapters. ATA 25 - 6 / 8 *** CARGO SMOKE MLG BAY FIRE CAB SMOKE ** ENG ATA 25 – Field of Vision A330-200 A350-900 Requirements A330 Visibility Requirements © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Captain field of vision PR1010081 A350 ↔ A330 Comparison Captain field of vision ATA 25 - 7 / 8 ATA 25 – Flight Crew Rest Compartment A350-900 The A330 has an optional Flight Crew Rest Compartment (FCRC). The FCRC is between the cockpit wall and the right hand door 1. The A350 has an optional Flight Crew Rest Compartment (FCRC). The FCRC is in an area above the aircraft forward doors (right hand door 1 and left hand door 1). © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. A330-200 FCRC typical layout PR1010081 A350 ↔ A330 Comparison ATA 25 - 8 / 8 A350 A330 Comparison Flight↔ Deck and Systems Briefing for Pilots Air Systems ATA 21 & 36 ATA 21 & 36 – Bleed Air Systems A330-200 The pneumatic system supplies high pressure air for: • Air conditioning • Wing ice protection system • Engine anti-ice • Engine starting • Pack bay ventilation turbofan actuation. • Thrust reversers (GE powered aircraft only) • Hydraulic reservoir pressurization • Water pressurization. High pressure air is supplied from five sources: • Two Engine bleed systems • The Auxiliary Power Unit (APU) bleed system • Two high pressure ground connections. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. There is one crossbleed valve. BLEED SD Page PR1010081 A350 ↔ A330 Comparison A350-900 The pneumatic system supplies high pressure air for: • Air conditioning and pressurization • Engine and wing ice protection system • Engine start • Pack bay ventilation system • The conditioned service air system (Used to supply the fuel tank inerting system). High pressure air is supplied from five sources: • Two engine bleed systems • The Auxiliary Power Unit (APU) bleed system • Two high pressure ground connector. There is one crossbleed valve. BLEED SD Page ATA 21 - 2 / 10 ATA 21 & 36 – Air Conditioning System A330-200 A350-900 The air conditioning system is fully automatic. This system provides continuous air renewal and maintains a constant selected temperature in the following zones: • Cockpit • Cabin zones (6 independent zones) • Crew rest compartment, if installed • Cargo compartments. The air conditioning system is fully automatic. This system provides continuous air renewal and maintains a constant selected temperature in the following zones: • Cockpit • Cabin zones (7 independent zones) • Crew rest compartments, if installed • Cargo compartments. The cabin crew can change the temperature of the cabin zones. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. The A330 has one emergency ram air inlet. COND SD Page PR1010081 A350 ↔ A330 Comparison The A350 has one emergency ram air inlet. COND SD Page ATA 21 - 3 / 10 ATA 21 & 36 – Air Conditioning System A330-200 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. CRUISE SD Page PR1010081 A350 ↔ A330 Comparison A350-900 CRUISE SD Page ATA 21 - 4 / 10 ATA 21 & 36 – Cabin Pressure A350-900 In normal operations, the pressurization system is fully automatic. This system regulates the cabin air pressure. The maximum cabin pressure will not exceed an equivalent cabin altitude of 8 000 ft. In normal operations, the pressurization system is fully automatic. This system regulates the cabin air pressure. The maximum cabin pressure will not exceed an equivalent cabin altitude of 6 000 ft for short-range missions and 7 800 ft for long-range missions. The Cabin Pressure Control System has: • Two outflow valves • Two independent cabin pressure controllers. The Cabin Pressure Control System (CPCS) has: • Two outflow valves • Two outflow valve controllers. Under abnormal operating conditions, the CPCS is: • Fully manual, the flight crew increases or decreases the Cabin altitude, or • Semi-automatic, the flight crew select a landing field elevation (the cabin altitude varies according to a pre-programmed law). Under abnormal operating conditions, the CPCS is semi-automatic. There are two semi-automatic pressurization modes: • Cabin altitude manual pressurization mode • Vertical speed manual pressurization mode. In addition, to protect the aircraft from structural damage, there are: • Three safety valves • One negative relief valve. In addition, to protect the aircraft from structural damage, there are: • One overpressure relief valve • Two negative relief valves. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. A330-200 CAB PRESS SD Page PR1010081 A350 ↔ A330 Comparison CAB PRESS SD Page ATA 21 - 5 / 10 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. ATA 21 & 36 – Cabin Pressure A330-200 A350-900 CRUISE SD Page CRUISE SD Page PR1010081 A350 ↔ A330 Comparison ATA 21 - 6 / 10 ATA 21 & 36 – Ventilation A330-200 A350-900 The avionics ventilation system ventilates: • The cockpit panels • The main avionics bay (left and right sides). The avionics ventilation system ventilates: • The cockpit panels • The main avionics bay (left and right sides). The avionics ventilation system has: • A blowing system with: • Two cabin fans • Two blowing fans • Recirculation valves that partially close to ensure sufficient air flow to avionics when the packs are OFF • An extraction system with : • One extraction fan • One extract valve • One overboard valve. The avionics ventilation system has: • A blowing system with: • Two filters • Two blowing fans • A backup supply from the mixer unit via two backup valves • An extraction system with : • Two extraction fans • One extract valve • One overboard valve. An optional ground cooling system ensures the cooling of the avionics when the aircraft is on ground. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Other systems ensure: • Cabin air recirculation • Lavatory and galleys air extraction • Batteries ventilation • Pack bay ventilation • Bulk cargo ventilation • Aft cargo ventilation, if installed • Fwd cargo ventilation, if installed. PR1010081 A350 ↔ A330 Comparison An optional ground cooling system ensures the cooling of the avionics when the aircraft is on ground. Other systems ensure: • Cabin air recirculation • Lavatory and galleys air extraction • Supplemental cooling, if installed • Pack bay ventilation • Bulk cargo ventilation • Battery ventilation • Aft cargo ventilation, if installed • Fwd cargo ventilation, if installed • Cockpit high ventilation for smoke removal. ATA 21 - 7 / 10 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. ATA 21 & 36 – Ventilation A330-200 A350-900 COND SD Page COND SD Page PR1010081 A350 ↔ A330 Comparison ATA 21 - 8 / 10 ATA 21 & 36 – Controls and Indicators © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. A330-200 AIR control panels PR1010081 A350 ↔ A330 Comparison A350-900 AIR control panels ATA 21 - 9 / 10 ATA 21 & 36 – Controls and Indicators A330-200 A350-900 OPTIONAL CARGO AIR COND Control Panel OPTIONAL VENT Control Panel © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. CARGO AIR COND and VENTILATION Control Panels AIR and CABIN PRESS Control Panels AIR and CABIN PRESS Control Panels CABIN PRESS CP is different due to the new functions. PR1010081 A350 ↔ A330 Comparison ATA 21 - 10 / 10 A350 A330 Comparison Flight↔ Deck and Systems Briefing for Pilots Automatic Flight System ATA 22 ATA 22 – AFS Architecture A330-200 A350-900 The Automatic Flight System (AFS) includes: • The Flight Guidance (FG) • The Flight Management (FM) • The Flight Envelope (FE). The Automatic Flight System (AFS) includes: • The Flight Guidance (FG) • The Flight Management System (FMS) • The Flight Envelope (FE). The FG, FM and FE are located on the Flight Management, Guidance and envelope Computers (FMGC). The AFS has two FMGCs. The AFS has: • Three Primary (PRIM) flight control and guidance computers • Three Flight Management Computers (FMCs) The PRIMs host the FG and the FE. The FMCs host the FMS. The flight crew interfaces with the Automatic Flight System (AFS) via: • One AFS Control Panel (AFS CP) • Three Multipurpose Control Display Units (MCDUs), including one on standby • Two Primary Flight Displays (PFDs) and two Navigation Displays (NDs) • One sidestick pushbutton on each sidestick • Two thrust levers and two A/THR instinctive disconnect pushbuttons. The flight crew uses the following controls and displays to interface with the AFS: • One AFS Control Panel (AFS CP) • Two Multifunction Displays (MFDs) with a FCU backup page • Two Primary Flight Displays (PFDs) and two Navigation Displays (NDs) • One sidestick pushbutton on each sidestick • Two thrust levers and two A/THR instinctive disconnect pushbuttons • Two Keyboard and Cursor Control Units (KCCUs) . © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. PFD PFD ND ND PFD ND PFD ND Sidesticks AFS CP AFS CP MFD Sidesticks FMGC FG FE MCDU FM MCDU Thrust Levers PR1010081 A350 ↔ A330 Comparison PRIM FG FE FMC FMS F/CTL FCU Backup KCCU Thrust Levers ATA 22 - 2 / 10 ATA 22 – Flight Guidance A330-200 A350-900 The PRIMs operate the FG. Each PRIM can operate: • One or both APs • The two FDs • The A/THR. Only the master FMGC controls the active A/THR. The other FMGC is in standby for A/THR control. When one AP is engaged, the associated A/THR has priority. When both APs are engaged (or neither of the APs), the A/THR 1 has priority. In the case of a failure of the master PRIM: • The slave 1 PRIM becomes the master, and the slave 2 PRIM becomes the slave 1 PRIM • The engaged AP, FDs and A/THR do not disconnect. They are transferred to the new master PRIM. The engaged AP/FD modes are displayed on the Flight Mode Annunciator (FMA). The engaged AP/FD modes are displayed on the Flight Mode Annunciator (FMA). New AP/FD modes are available in: • A/THR column mode: • BTV • Lateral mode column: • F-LOC (and F-LOC* capture mode) • Vertical mode column: • F-G/S (and F-G/S* capture mode) • TCAS. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. The FMGCs operate the FG. Each FMGC can operate: • One Autopilot (AP) • One Flight Director (FD) • One Autothrust (A/THR) channel. Autothrust Operation AP / FD Lateral Modes AP / FD Vertical Modes AP, FD, A/THR Engagement Status Approach Capabilities PR1010081 A350 ↔ A330 Comparison Autothrust Operation AP / FD Lateral Modes AP / FD Vertical Modes AP, FD, A/THR Engagement Status Approach Capabilities ATA 22 - 3 / 10 ATA 22 – Controls and Indicators A330-200 AUTO LAND Light AUTO LAND Light FMA FD Bars © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Two PFDs, one per Flight Crewmember A350-900 AUTO LAND Light AUTO LAND Light The FD pb is on the AFS CP and controls both FDs. FMA Two FD pbs, one per Flight Crewmember; each pb controls the display of the FD bars on the corresponding PFD FD Bars Two PFDs,One per Flight Crewmember A/THR Instinctive Disconnect pb FCU Thrust Levers Two Sidesticks, one per Flight Crewmember PR1010081 A350 ↔ A330 Comparison AFS CP A/THR Instinctive Disconnect pb Two Sidesticks, one per Flight Crewmember Thrust Levers ATA 22 - 4 / 10 ATA 22 – Flight Management System A330-200 A350-900 There are Flight Management (FM) parts in each FMGC, one for each pilot. There are two Flight Management Systems (FMS), one for each pilot. The flight crew uses the following controls and displays to interface with each FMS : • 1 MCDU • 1 ND • 1 PFD • 1 EFIS CP. Each FMS uses a computer, referred to as Flight Management Computer (FMC). There are three FMCs. In normal operation: • FMC-A provides data to FMS 1 • FMC-B provides data to FMS 2 • FMC-C is on standby, and can operate instead of either FMC-A or FMC-B. A third MCDU is on standby in the case of a failure of one of the other two. On the pedestal, a FM selector enables one FM to provide data to both sides. FMS 1 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. PFD FMS 2 ND EFIS CP EFIS CP MCDU MCDU ND PFD The flight crew uses the following controls and displays to interface with each FMS: • 1 MFD • 1 ND • 1 PFD • 1 EFIS CP On the main instrument panel, a • 1 KCCU. FMS selector enables one FMC to provide data to both sides. FMS 1 PFD ND FMS 2 EFIS CP EFIS CP MFD MFD KCCU KCCU ND PFD MCDU FMGC 1 FMGC 2 FMC-A FMC-B FMC-C PR1010081 A350 ↔ A330 Comparison ATA 22 - 5 / 10 ATA 22 – Flight Management System A330-200 A350-900 The FMS display has a new design. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. The FM includes all basic functions: • Flight planning (lateral and vertical) • Navigation • Prediction and optimization of performance • Management of the displays • One Secondary Flight Plan (SEC F-PLN) • Fuel management functions. The FMS includes all basic functions: • Flight planning (lateral and vertical) • Navigation • Prediction and optimization of performance • Management of the displays • Three Secondary Flight Plans (SEC F-PLNs). In addition to the basic functions, the FMS has: • Enhanced fuel management functions, for example with the Long Range Cruise (LRC) mode • A FMS Landing System (FLS) function • Diversion aid functions, for example the WHAT IF function that assists the flight crew to manage a diversion due to one engine out or depressurization • A Takeoff Securing (TOS) function • A Takeoff Monitoring (TOM) function. PR1010081 A350 ↔ A330 Comparison ATA 22 - 6 / 10 ATA 22 – Flight Management System A330-200 These functions are not installed on the A330. A350-900 WHAT IF Function The WHAT IF function prepares prediction scenarios. The objective of this function is to assist the flight crew to make decisions in the case of a diversion. The Fuel Penalty Factor Function The objective of the fuel penalty factor function is to provide the flight crew with FMS fuel predictions that take an abnormal aircraft configuration into account. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. The FMS Landing System The FMS Landing System (FLS) function provides the flight crew with cockpit indications and guidance to fly a LOC only, VOR, NDB, LCTR, VOR/DME or RNAV approach (that includes GPS approach) in an ILS look alike method. PR1010081 A350 ↔ A330 Comparison ATA 22 - 7 / 10 ATA 22 – Flight Management System A350-900 Takeoff Securing function The A330 will optionally have the Takeoff Securing (TOS) function. The TOS function of the A330 checks the following: • Takeoff speeds that are inserted in the FMS • Zero Fuel Weight (ZFW) value. Takeoff Securing function The A350 has the Takeoff Securing (TOS) function. The TOS function of the A350 checks the following: • Takeoff speeds that are inserted in the FMS • Zero Fuel Weight (ZFW) value • Aircraft position (checks if the aircraft is on the right runway) • Runway limitations and available distance • Flex temperature. Takeoff Monitoring function The Takeoff Monitoring (TOM) function is under development for its deployment on the A330. Takeoff Monitoring function The A350 has the Takeoff Monitoring (TOM) function. The TOM function is a complement of the TOS function. The TOM function evaluates the acceleration profile in order to alert the flight crew if the acceleration capability of the aircraft is degraded. The TOM function aims to prevent tailstrikes and runway overruns. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. A330-200 PR1010081 A350 ↔ A330 Comparison ATA 22 - 8 / 10 ATA 22 – Controls and Indicators © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. A330-200 Two NDs, one per Flight Crewmember PR1010081 A350 ↔ A330 Comparison A350-900 Each ND includes a Vertical Display (VD) that displays the flight path and ground obstacles. Two NDs, one per Flight Crewmember ATA 22 - 9 / 10 ATA 22 – Controls and Indicators A330-200 A350-900 FMS Selector FM selector on the SWITCHING panel © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. CAPT MFD F/O MFD Two MFDs, one per Flight Crewmember Three MCDUs, one per Flight Crewmember and one on standby. PR1010081 A350 ↔ A330 Comparison Two KCCUs, one per Flight Crewmember ATA 22 - 10 / 10 A350 A330 Comparison Flight↔ Deck and Systems Briefing for Pilots Communication ATA 23 ATA 23 – External Communications A330-200 A350-900 The A330 is equipped with: • Three Very High Frequency (VHF) voice and data transceivers (either 3 channels in voice mode or 2 channels in voice mode and one in data mode) • Two High Frequency (HF) voice and data transceivers • One SATCOM system • One Selective Calling (SELCAL) system. The A350 is equipped with: • Three Very High Frequency (VHF) voice and data transceivers (either 3 channels in voice mode or 2 channels in voice mode and one in data mode) • One High Frequency (HF) voice and data transceiver, with a second optional HF transceiver • One SATCOM system • One Selective Calling (SELCAL) system • One gatelink system for ground communications with the airline (wired or wireless). The A330 has an Emergency Locator Transmitter (ELT). The A350 has an Emergency Locator Transmitter (ELT). VHF 3 ELT VHF 3 HF Antenna © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. VHF 1 SATCOM ELT VHF 1 HF Antenna Gatelink (wireless, optional) SATCOM VHF 2 VHF 2 PR1010081 A350 ↔ A330 Comparison Gatelink (wired) ATA 23 - 2 / 6 ATA 23 – Internal Communications A330-200 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. The Internal communication is possible between: • The captain • The first officer • The third occupant • The fourth occupant (optional) • The cabin crew • The ground crew • The passengers (for cockpit or cabin announcements). PR1010081 A350 ↔ A330 Comparison Internal Communications are similar. A350-900 The Internal communication is possible between: • The captain • The first officer • The third occupant • The fourth occupant (optional) • The cabin crew • The ground crew • The passengers (for cockpit or cabin announcements). ATA 23 - 3 / 6 ATA 23 – Controls and Indicators A330-200 A350-900 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. RMP and ACP RMP The A350 RMP includes functions of the A330 RMP, the A330 ACP and the A330 ATC control panel. Loudspeaker volume push-to-talk (optional) ATC Control Panel Loudspeaker volume push-to-talk (optional) Each A350 RMP displays the three main frequencies on the same page. Several pages allow the pilots to display the different means of communication (VHF, HF, SATCOM, SQWK). The flight crew can load a VHF frequency or a SATCOM number from the mailbox. PR1010081 A350 ↔ A330 Comparison ATA 23 - 4 / 6 ATA 23 – Controls and Indicators © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. A330-200 A350-900 The EVAC control panel is located with the CALLS control panel. EVAC Control Panel CALLS Control Panel PR1010081 A350 ↔ A330 Comparison CALLS and EVAC Control Panels ATA 23 - 5 / 6 ATA 23 – Controls and Indicators A330-200 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. ELT Control Panel (optional) PR1010081 A350 ↔ A330 Comparison A350-900 ELT Control Panel ATA 23 - 6 / 6 A350 A330 Comparison Flight↔ Deck and Systems Briefing for Pilots Electrical System ATA 24 ATA 24 – Electrical Generation AC A350-900 Two generators power the electrical network of the A330. There is one generator per engine. The generators provides 115 V Alternative Current (AC) to the electrical networks. Four generators power the electrical network of the A350. There are two variable frequency generators on each engine. The generators provides 230 V AC to the electrical networks. The Auxiliary Power Unit (APU) drives one generator that provides 115 V AC to the electrical networks. The APU drives one fixed frequency generator which provides 230 V AC to the electrical networks. An emergency generator is driven by the GREEN HYD circuit (which is driven by the Ram Air Turbine (RAT) if the normal GREEN HYD generation is not available). The emergency generator provides 115 V AC to the essential systems. An emergency generator is located in the Ram Air Turbine (RAT). The RAT generator provides 230 V AC to the systems necessary in emergency electrical configuration. Two ground connectors provide 115 V AC to the electrical networks. Two ground connectors provide 115 V AC to the electrical networks. In that case, the ATUs supply the 230 V AC networks using the 115 V AC from the ground connectors. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. A330-200 PR1010081 A350 ↔ A330 Comparison Automatic Transfer Units (ATUs) supplies the 115 V AC network using the 230 V AC. ATA 24 - 2 / 6 ATA 24 – Electrical Generation DC A330-200 A350-900 Three Transformer/Rectifier (TR) units provide 28 V Direct Current (DC) to the DC network. One of those TR is dedicated to power supply of essential systems. Four TR provide 28 V DC to the DC network. The TR use the 230 V AC network. TR EMER 1 and 2 are dedicated to emergency configuration. Two batteries (BAT 1 and BAT2) are connected to the DC network. The APU BAT is dedicated to the APU start. A fourth TR is dedicated to APU start and APU battery charge. One of the batteries is dedicated to APU start. Four identical batteries are connected to the DC network. EMER BAT 1 and 2 can provide temporary supply in an emergency configuration. Any TR, BAT 1 and BAT 2 can provide supply for APU start. BAT 1 EMER BAT 1 EMER BAT 2 BAT 2 DC 1 EMER DC 1 EMER DC 2 DC 2 DC BAT BAT 1 BAT 2 TR EMER 2 STAT INV 1 TR 1 EMER AC 1 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. DC 1 DC 2 DC ESS APU BAT STAT INV EMER GEN TR ESS TR1 GEN 1 ATU 1A TR APU AC 2 APU GEN GEN 2 115 V AC 230 V AC 28 V DC Reconfiguration PR1010081 A350 ↔ A330 Comparison AC 1B ATU 1B ATU EMER 1 EMER AC 1 TR2 EMER AC 2 ATU EMER 2 RAT AC 2B EMER AC 2 ATU 2B APU START TR 2 AC ESS AC 1 AC 1A TR EMER 1 AC 1A AC 1B AC 2B AC 2A GEN 1A GEN 1B GEN 2B GEN 2A APU GEN ATA 24 - 3 / 6 AC 2A ATU 2A ATA 24 – Electrical Distribution A330-200 A350-900 The 230 V AC network supplies the large power consumers. The 230 V AC network has: • Four AC busbars • Two AC emergency busbars. The 115 V AC network supplies all AC consumers and has: • Two AC busbars • One AC essential busbar. The 115 V AC network supplies the commercial loads and some essential loads. The 115 V AC network has: • Four AC busbars • Two AC emergency busbars. The 230 V AC network supplies the 115 V AC network via Auto Transformer Units (ATU). When the generators and the APU are not operating, the ATU converts the 115 V AC which comes from the Ground Power Unit (GPU) into 230 V AC. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. The 28 V DC network supplies DC consumers and has: • Two DC busbars • One DC essential busbar • One DC battery busbar Bus TIE contactors operate automatically to enable any reconfiguration. The 28 V DC network supplies DC consumers and has: • Two DC busbars • Two DC emergency busbars. Bus TIE contactors operate automatically to enable any reconfiguration. A SIDE 1&2 pb can isolate both sides of the the Electrical Power Distribution Centers (EPDC). Two identical and independent electrical networks ensure redundancy, even in Emergency Electrical (EMER ELEC) configuration. PR1010081 A350 ↔ A330 Comparison ATA 24 - 4 / 6 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. ATA 24 – Controls and Indicators A330-200 A350-900 ELEC AC SD Page ELEC AC SD Page ELEC DC SD Page PR1010081 A350 ↔ A330 Comparison ELEC DC SD Page ATA 24 - 5 / 6 ATA 24 – Controls and Indicators A330-200 A350-900 The BAT control panel is next to the MAINTENANCE control panel. RAT MAN ON guarded pb BAT Control Panel The RAT MAN ON guarded pb is on the EMER ELEC Control Panel © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. EMER ELEC PWR Control Panel EMER ELEC PWR Control Panel ELEC Control Panel PR1010081 A350 ↔ A330 Comparison ELEC Control Panel ATA 24 - 6 / 6 A350 A330 Comparison Flight↔ Deck and Systems Briefing for Pilots Fire and Smoke Protection ATA 26 ATA 26 – Overview A330-200 A350-900 The A350 has a: • Fire and overheat detection system for: • The engines • The Auxiliary Power Unit (APU) • Fire and overheat detection system for: • The engines • The Auxiliary Power Unit (APU) • The Main Landing Gear (MLG) bay • Smoke detection system for: • The avionics bay • The optional In-Flight Entertainment (IFE) center • The cargo compartments • The lavatories • The optional crew rest compartments. • Smoke detection system for: • The avionics bay • The optional In-Flight Entertainment Center (IFEC) • The cargo compartments • The lavatories • The optional crew rest compartments. • Fire extinguishing system for: • The engines • The APU • The cargo compartments • The lavatory waste bins. • Fire extinguishing system for: • The engines • The APU • The cargo compartments • The lavatory waste bins. In addition, the A330 has portable fire extinguishers. In addition, the A350 has portable fire extinguishers. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. The A330 has a: A smoke alert is triggered on the Flight Attendant Panels (FAPs) in the case of smoke detection in: • Any lavatory. PR1010081 A350 ↔ A330 Comparison A smoke alert is triggered on the Flight Attendant Panels (FAPs) in the case of smoke detection in: • Any lavatory • The optional IFEC • The optional crew rest compartments. ATA 26 - 2 / 6 ATA 26 – Control and indicators A330-200 A350-900 The FIRE CP includes the APU FIRE controls. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. APU FIRE Control Panel There is one FIRE TEST pb for the engines and the APU. FIRE Control Panel PR1010081 A350 ↔ A330 Comparison FIRE Control Panel ATA 26 - 3 / 6 ATA 26 – Control and indicators © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. A330-200 COND SD Page PR1010081 A350 ↔ A330 Comparison A350-900 COND SD Page ATA 26 - 4 / 6 ATA 26 – Control and indicators A330-200 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. PAX SYS SMOKE pb CARGO SMOKE and VENTILATION Control Panels PR1010081 A350 ↔ A330 Comparison A350-900 A MLG BAY FIRE light is near the CARGO SMOKE CP CARGO SMOKE, VENT and CABIN SYS SMOKE Control Panels ATA 26 - 5 / 6 ATA 26 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Intentionally Left Blank PR1010081 A350 ↔ A330 Comparison ATA 26 - 6 / 6 A350 A330 Comparison Flight↔ Deck and Systems Briefing for Pilots Flight Controls ATA 27 ATA 27 – Control Surfaces A330-200 A350-900 The A330 has: • 4 ailerons • 2 elevators • 1 rudder • 12 spoilers • 14 slats • 4 flaps • 1 Trimmable Horizontal Stabilizer (THS) The A350 has: • 4 ailerons • 2 elevators • 1 rudder • 14 spoilers • 12 slats • 2 Droop Nose Devices (DNDs) • 4 flaps • 1 Trimmable Horizontal Stabilizer (THS) Three Hydraulic (HYD) circuits power the actuators of all the control surfaces. A 2 Hydraulic and 2 Electric (2H/2E) circuits system powers the actuators of all the control surfaces. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Trimmable Horizontal ailerons Stabilizer rudder spoilers spoilers flaps slats ailerons Trimmable Horizontal Stabilizer rudder flaps slats elevators elevators Primary Flight Controls Flaps and Slats PR1010081 A350 ↔ A330 Comparison Droop Nose Devices ATA 27 - 2 / 12 ATA 27 – Flight Control Computers A330-200 A350-900 The A330 has: • Three Primary (PRIM) flight control computers • Two Secondary (SEC) flight control computers • In the case of total flight control computer failure: • On A330 Enhanced, a mechanical backup link controls the THS and a Backup Control Module (BCM) controls the rudder • On A330 Classic, a mechanical backup link controls the THS and another mechanical backup link controls the rudder. The A350 has: • Three Primary (PRIM) flight control and guidance computers • Three Secondary (SEC) flight control computers • One Backup Control Module (BCM) for inboard ailerons, elevators and rudder control. Mechanical link TRIM wheels © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. SPEED BRAKE lever In the case of computer or electrical generation failure, a Backup Power Supply (BPS) provides electrical power to the BCM. The YELLOW HYD circuit supplies the BPS. SPEED BRAKE lever PRIM PRIM PRIM PRIM PRIM PRIM Flight Control Surfaces Actuators PRIM SEC Sidesticks PRIM PRIM SEC Flight Control Surfaces Actuators Sidesticks PITCH TRIM sw BCM Rudder Pedals (A330 Enhanced only) BCM Rudder Pedals Rudder Trim Selector Mechanical link (A330 Classic only) PR1010081 A350 ↔ A330 Comparison Rudder Trim Selector ATA 27 - 3 / 12 ATA 27 – Flight Control Laws A330-200 A350-900 The A350 has three flight control laws : • Normal Law • Alternate Law • Direct Law. In the case of failure of the flight controls computers (PRIM1, PRIM2, PRIM3, SEC1 and SEC2), the horizontal trimmable plane is controlled by a mechanical backup. On the A330 Enhanced, the rudder is controlled by a BCM. On the A330 Classic, the rudder is controlled by a mechanical backup. In the case of failure of the flight controls computers (PRIM1, PRIM2, PRIM3, SEC1, SEC2 and SEC3) flight crewmembers’ inputs are transferred to control surface actuators via the BCM. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. The A330 has three flight control laws: • Normal Law • Alternate Law • Direct Law. Control Law Pitch Normal law Normal Normal All active Lateral Protections In normal law, a derotation law provides a comfortable nosewheel touchdown without interfering with the prompt activation of all the decelerating devices. Autopilot Control Law Pitch Lateral Available Normal law Normal Normal All active Protections Autopilot Available Depending on the failure, Normal some protections may still be Depending Alternate Normal or available. However, these on the law Direct protections are degraded and failure are therefore indicated as lost. Alternate Normal law Depending on the failure, Normal some protections may still be Available (no available. However, these or Direct protections are degraded and autoland) are therefore indicated as lost. Direct law Direct law Direct Direct Direct All lost PR1010081 A350 ↔ A330 Comparison Not available Direct All lost Not available ATA 27 - 4 / 12 ATA 27 – Controls and Indicators A330-200 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. F/CTL SD Page PR1010081 A350 ↔ A330 Comparison A350-900 F/CTL SD Page ATA 27 - 5 / 12 ATA 27 – Controls and Indicators A330-200 A350-900 The left F/CTL CP includes a SEC 3 pb. The PRIM 3 is on the left F/CTL CP. Left FLT CTL Computers Control Panel Left F/CTL Computers Control Panel © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. A TURB DAMPG pb is on the right F/CTL CP. Right FLT CTL Computers Control Panel PR1010081 A350 ↔ A330 Comparison Right F/CTL Computers Control Panel ATA 27 - 6 / 12 ATA 27 – Controls and Indicators A330-200 A350-900 Sidestick Priority Light Sidestick Priority Light Spoiler position indication. TRIM at takeoff is automatically set and displayed below the PFD. It is displayed on ground only. TRIM Indicator below PFD © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. TRIM Wheels PITCH TRIM sw The PITCH TRIM is manually controlled by a switch. PR1010081 A350 ↔ A330 Comparison ATA 27 - 7 / 12 ATA 27 – Control and Indicators A330-200 A350-900 SPEED BRAKE Lever © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. SPEED BRAKE Lever RUDDER TRIM Selector Panel The RUDDER TRIM indication is displayed on the lower part of the PFD and on the F/CTL SD page when needed. RUD TRIM Selector PR1010081 A350 ↔ A330 Comparison ATA 27 - 8 / 12 ATA 27 – Slats and Flaps A330-200 A350-900 SLATS Slats Gearbox Motor SFCC 1 SFCC 2 BLUE HYD 230 V AC EMER 1 feedback feedback GREEN HYD YELLOW HYD Motor Slats Gearbox SFCC 1 Motor SFCC 2 YELLOW HYD feedback feedback feedback Motor feedback GREEN HYD SLATS YELLOW HYD Motor Flaps Gearbox Motor © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. FLAPS Motor Flaps Gearbox Motor GREEN HYD FLAPS The A350 has two new functions dedicated to load optimization: • Differential Flaps Settings (DFS) • Variable camber. The DFS performs small flaps deflections (4° maximum) either symmetrically or differentially. The variable camber adapts slightly the flaps deflection (in or out) during the cruise. The objectives of both functions are: • Optimizing the load and the lateral trim function • Minimizing drag. The Adaptive Dropped Hinge Flap (ADHF) is an automatic function which controls the spoilers and flaps motion when the flaps are extended. The objective of the ADHF is to improve the aerodynamics of the wing during low speed phases. PR1010081 A350 ↔ A330 Comparison ATA 27 - 9 / 12 ATA 27 – Flaps and Slats A330-200 FLAPS Lever Position 0 Configuration on ECAM A350-900 Maximum Speed Flight Phase FLAPS Lever Position VMO/MMO Cruise 0 240 kt Holding 1 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Maximum Speed Flight Phase VMO/MMO Cruise 255 kt Holding 220 kt Takeoff, Approach 212 kt Takeoff, Approach 195 kt Takeoff 190 kt Approach, Landing 186 kt Landing 1 215 kt Takeoff 2 196 kt Takeoff, Approach 3 186 kt Takeoff, Landing FULL Configuration on ECAM 180 kt 2 3 Landing FULL The 1+F configuration is available for takeoff and approach. In addition, there is a 3+S configuration for approach and landing. PR1010081 A350 ↔ A330 Comparison ATA 27 - 10 / 12 ATA 27 – Control and Indicators A330-200 A350-900 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. FLAPS Position Indicator below PFD Slats and Flaps positions is displayed below both PFDs. FLAPS Position Indicator on E/WD PR1010081 A350 ↔ A330 Comparison ATA 27 - 11 / 12 ATA 27 – Control and Indicators A330-200 A350-900 FLAPS Lever © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. FLAPS Lever A flaps lever override mechanism allows the pilots to extend the flaps by one step if the flap lever is jammed. PR1010081 A350 ↔ A330 Comparison ATA 27 - 12 / 12 A350 A330 Comparison Flight↔ Deck and Systems Briefing for Pilots Fuel System ATA 28 & 47 ATA 28 & 47 – Fuel Tank Arrangement and Quantity A330-200 A350-900 Center Tank Center Tank Inner Tank Wing Tank Outer Tank Vent Tank Surge Tank © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Trim Tank VOLUME WEIGHT USABLE FUEL (Fuel specific density : 0.80 kg/L) USABLE FUEL (Fuel specific density : 0.80 kg/L) Outer Tanks Inner Tanks Center Tank Trim Tank Total Wing Tanks Center Tank Total L 7 300 84 000 41 650 6 230 139 180 L 59 238 82 421 141 659 US Gal 1 928 22 190 11 002 1 646 36 766 US Gal 15 649 21 773 37 005 Kg 5 840 67 200 33 320 4 984 111 344 Kg 47 390 65 937 113 327 Lb 12 892 148 345 73 554 11 002 245 792 Lb 104 477 145 366 249 843 VOLUME WEIGHT The A330 and the A350 have similar fuel quantities. PR1010081 A350 ↔ A330 Comparison ATA 28 - 2 / 8 ATA 28 & 47 – Fuel Distribution A330-200 The A330 has: • Two main pumps in each inner tank • One standby pump in each inner tank • Two pumps in the center tank (these pumps feed the inner tanks) • One Crossfeed Valve (X-FEED). The outer tanks feed the inner tanks by gravity. A350-900 The A350 has: • One main pump in each wing tank • One standby pump in each wing tank • One left pump in the center tank • One right pump in the center tank • Two Crossfeed Valves (X-FEED). The center tank pumps produce more pressure than the wing tank pumps, and therefore preferentially supply fuel to the engines. Any inner tank pump can supply fuel to both engines. Any pump is sufficient to supply fuel to both engines. The APU is fed from the left inner tank or from the trim tank. Two pumps (AFT and FWD) feed the APU. The APU is fed via the pumps of the fuel tanks. If the pressure is too low, a dedicated pump at the rear of the center tank feeds the APU. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. The A350 doesn’t have a trim tank. PR1010081 A350 ↔ A330 Comparison ATA 28 - 3 / 8 ATA 28 & 47 – Fuel System Monitoring and Inerting A330-200 A350-900 The A330 has: • Two Fuel Control and Monitoring Computers (FCMCs) • A fuel tank inerting system, optional. The A350 has: • Two Fuel Quantity and Management Systems (FQMSs) • A fuel tank inerting system. The FCMCs provide the following functions: • Fuel quantity measurement and indication • Center of gravity calculation • Fuel temperature indication • Control of the fuel transfer to the inner tanks for engine feed • Control of the fuel transfer to and from the trim tank for CG control • Jettison control (optional) • Fuel leak detection. The FQMSs provide the following functions: • Fuel quantity measurement and indication • Center of gravity calculation • Fuel temperature indication • Refuel control • Jettison control (optional) • Fuel leak detection. The objective of the fuel tank inerting system is to feed the fuel tanks with inert gas while fuel is consumed, in order to provide a flammability protection. A fuel jettison system is available as an option. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. The A330 has two refuel couplings, one under each wing. PR1010081 A350 ↔ A330 Comparison The objective of the fuel tank inerting system is to feed the fuel tanks with inert gas while fuel is consumed, in order to provide a flammability protection. A fuel jettison system is available as an option. The A350 has two standard refuel couplings under the right hand wing and can optionally have two more standard refuel couplings under the left hand wing. ATA 28 - 4 / 8 ATA 28 & 47 – Controls and Indicators A330-200 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. FUEL SD Page PR1010081 A350 ↔ A330 Comparison A350-900 FUEL SD Page ATA 28 - 5 / 8 ATA 28 & 47 – Controls and Indicators A330-200 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. CRUISE SD Page Permanent Data A350-900 CRUISE SD Page Permanent Data The Permanent Data displays the Fuel On Board (FOB) value. PR1010081 A350 ↔ A330 Comparison ATA 28 - 6 / 8 ATA 28 & 47 – Controls and Indicators A330-200 A350-900 REFUEL pb © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. FUEL INR TK SPLIT Control Panel REFUEL pb FUEL JETTISON Control Panel (optional) FUEL Control Panel PR1010081 A350 ↔ A330 Comparison JETTISON Control Panel (optional) FUEL Control Panel ATA 28 - 7 / 8 ATA 28 & 47 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Intentionally Left Blank PR1010081 A350 ↔ A330 Comparison ATA 28 - 8 / 8 A350 A330 Comparison Flight↔ Deck and Systems Briefing for Pilots Hydraulic System ATA 29 ATA 29 – Hydraulic Generation A330-200 A350-900 The A330 has three independent hydraulic circuits: • The YELLOW hydraulic circuit • The GREEN hydraulic circuit • The BLUE hydraulic circuit. The A350 has two independent and identical hydraulic circuits: • The YELLOW hydraulic circuit • The GREEN hydraulic circuit. The YELLOW, GREEN and BLUE circuits have: • One hydraulic reservoir • One Engine Driven Pump (EDP) • One Electric Motor Pump (EMP) • One accumulator • One Fire Shutoff Valve (FSOV). Each circuit has: • One hydraulic reservoir • Two Engine Driven Pumps (EDPs) • One Electric Motor Pump (EMP) • One accumulator • Two Fire Shutoff Valves (FSOV) • One cooling system • A Hydraulic System Monitoring Unit (HSMU). In addition, the GREEN circuit has: • A second EDP • A second FSOV • A Ram Air Turbine (RAT) driven pump. A Hydraulic System Monitoring Unit (HSMU) monitors the three circuits. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. GREEN EMP BLUE EMP BLUE EDP YELLOW EMP YELLOW EDP If an hydraulic circuit fails, the electric circuits take over due to the 2 Hydraulic Circuits / 2 Electric Circuits (2H/2E) architecture. Main actuators can be controlled by hydraulic or electrical power sources. GREEN EMP YELLOW EDP GREEN EDP GREEN EDP YELLOW EMP YELLOW EDP GREEN EDP GREEN EDP RAT PR1010081 A350 ↔ A330 Comparison ATA 29 - 2 / 6 ATA 29 – Distribution and Monitoring A330-200 A350-900 The hydraulic generation system provides hydraulic consumers with the required amount of hydraulic flow and pressure to ensure: • Primary and secondary flight controls operation • Landing gear retraction/extension and associated doors closure/opening • Wheel brake operation • Nose wheel steering • Cargo doors actuation. The hydraulic generation system provides hydraulic consumers with the required amount of hydraulic flow and pressure to ensure: • Primary and secondary flight control operation • Nose and main landing gear retraction/extension and associated doors closure/opening • Wheel brake operation • Nose wheel Steering • Cargo doors actuation • Backup Power Supply (BPS). The EMPs provide hydraulic pressure on ground and, in some failure cases, in flight. The Ram Air Turbine (RAT) can pressurize the GREEN hydraulic circuit, in the case of an emergency. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. The HSMU performs the following functions: • Pump and reservoir pressure measurement • Hydraulic fluid quantity and temperature measurement • Position of the FSOVs and FSOVs closure • EMP, its start-up and shutdown • FAULT light illumination logic • LEAK MEASUREMENT VALVE control • RAT extension. Each hydraulic circuit is pressurized at 3 000 psi. PR1010081 A350 ↔ A330 Comparison The EMPs provide hydraulic pressure on ground only, when all engines are off. The HSMUs monitors and or controls: • Pump and reservoir pressure measurement • Hydraulic fluid quantity and temperature measurement • Position of the FSOVs and FSOVs closure • EMP, its start-up and shutdown • The depressurization of the EDPs • Fuel/hydraulic heat exchanger control, for hydraulic circuit cooling. Each hydraulic circuit is pressurized at 5 000 psi. ATA 29 - 3 / 6 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. ATA 29 – Controls and Indicators A330-200 A350-900 HYD SD Page HYD SD Page PR1010081 A350 ↔ A330 Comparison ATA 29 - 4 / 6 ATA 29 – Controls and Indicators A330-200 A350-900 The different EMP pushbuttons are on a separated control panel, next to the HYD Control Panel. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. GND HYD Control Panel HYD Control Panel PR1010081 A350 ↔ A330 Comparison HYD Control Panel ATA 29 - 5 / 6 ATA 29 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Intentionally Left Blank PR1010081 A350 ↔ A330 Comparison ATA 29 - 6 / 6 A350 A330 Comparison Flight↔ Deck and Systems Briefing for Pilots Ice and Rain Protection ATA 30 ATA 30 – Ice protection A330-200 A350-900 The A330 has: • Two ice detectors • One visual ice indicator. The A350 has: • Two ice detectors • Two visual ice indicators. The following parts of the aircraft are protected against ice accretion via electrical heating: • Static probes • Pitot probes • Angle of Attack (AOA) probes • Total Air Temperature (TAT) probes • Cockpit windows • Water/waste drain masts. The following parts of the aircraft are protected against ice accretion via electrical heating: • Integrated Static Probes (ISP) • Multifunction Probes (MFP) • Side Slip Angle (SSA) probes • Static and Pitot probes (Standby probes) • Cockpit windows • Water/waste drain masts. The following parts of the aircraft are protected against ice accretion via hot Bleed Air: • Engines nacelles • Slats 4, 5, 6 and 7 on each wing. The following parts of the aircraft are protected against ice accretion via hot Bleed Air: • Engine nacelles • Slats 3, 4 and 5 on each wing. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Wing Anti-Ice Wing Anti-Ice Engine Anti-Ice Engine Anti-Ice Water/Waste Drain Mast Heating Windows Heating Probes Heating Probes Heating Ice Detection PR1010081 A350 ↔ A330 Comparison Water/Waste Drain Mast Heating Windows Heating Ice Detection ATA 30 - 2 / 6 ATA 30 – Rain Removal A330-200 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. The A330 has: • Rain repellent • Wipers. PR1010081 A350 ↔ A330 Comparison Rain Removal is similar. A350-900 The A350 has: • Rain repellent • Wipers. ATA 30 - 3 / 6 ATA 30 – Controls and Indicators © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. A330-200 BLEED SD Page PR1010081 A350 ↔ A330 Comparison ANTI-ICE indications on the BLEED SD page are similar. A350-900 BLEED SD Page ATA 30 - 4 / 6 ATA 30 – Controls and Indicators A330-200 A350-900 ANTI ICE Control Panel © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. ANTI ICE Control Panel and PROBE/WINDOW HEAT pb RAIN RPLNT pb and WIPER selector PR1010081 A350 ↔ A330 Comparison RAIN RPLNT pb and WIPER selector ATA 30 - 5 / 6 ATA 30 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Intentionally Left Blank PR1010081 A350 ↔ A330 Comparison ATA 30 - 6 / 6 A350 A330 Comparison Flight↔ Deck and Systems Briefing for Pilots Control and Display System and Recording Systems ATA 31 ATA 31 – Overview of the CDS A330-200 A350-900 EFIS CP EFIS CP HUD (Optional) EFIS CP EFIS CP HUD CP (optional) HUD CP (optional) OIS PFD ND © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. ISIS DCDU (optional) E/ WD PFD/ND ND PFD ECP MCDU PR1010081 A350 ↔ A330 Comparison MCDU ED WD SD PFD/ND OIS MFDs SD DCDU (optional) HUD (Optional) KCCU KCCU ISIS ECP ISIS (optional) ATA 31 - 2 / 24 ATA 31 – Overview of the CDS A330-200 A350-900 The A330 has: • 6 identical Display Units (DUs) • 1 Integrated Standby Instrument System (ISIS) • 2 EFIS Control Panel (EFIS CP) • 1 ECAM Control Panel (ECP). © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. DMC 1 DMC 3 The A350 has: • 6 identical Display Units (DUs) • 1 Integrated Standby Instrument System (ISIS) and a second ISIS as an option • 2 Head-Up Displays (HUDs), optional • 2 EFIS Control Panels (EFIS CPs) • 1 ECAM Control Panel (ECP) • 2 optional HUD control panels • 2 Keyboard and Cursor Control Units (KCCUs) • 2 Onboard Information System (OIS) keyboards. DMC 2 Control and Display System (CDS) FWS FWC FWC11 SDAC SDAC12 Aircraft system sensors SURV, ATC, FMS, FCU BACKUP, OIS Aircraft Systems NAV and AFS sensors The Display Management Computers (DMCs) process the data and create video signals displayed on the DUs. Each DMC manages two DUs. PR1010081 A350 ↔ A330 Comparison Concentrator and Multiplexer for Video (CMV) Each DU has a built-in calculator able to process all the available displays and functions. Each DU is connected to the different networks. ATA 31 - 3 / 24 ATA 31 – Display Units A330-200 A350-900 The A330 has six 6 x 6 inches Display Units (DUs). The A350 has six 12 x 8 inches Display Units (DUs). The A330 has: • Four DUs for the Electronic Flight Instrument Systems (EFIS): • Two DUs for the Primary Flight Displays (PFDs) • Two DUs for the Navigation Displays (NDs) • Two DUs for the Electronic Centralized Aircraft Monitor (ECAM): • One DU for the Engine and Warning Display (EWD) • One DU for the System Display (SD). The A350 has: • Two DUs for the Electronic Flight Instrument Systems (EFIS) • One DU for the Electronic Centralized Aircraft Monitoring (ECAM) • One DU for the Multifunction Displays (MFDs) • Two DUs for the Onboard Information Systems (OIS). In the case of a failure, the DUs automatically reconfigure. The flight crew can manually reconfigure the DUs. In the case of a failure, the DUs automatically reconfigure. The flight crew can also manually reconfigure the DUs via the DISPLAY CYCLE pb. 12 inches (30.5 cm) PR1010081 A350 ↔ A330 Comparison 8 inches (20.3 cm) 6 inches (15.25 cm) © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. 6 inches (15.25 cm) ATA 31 - 4 / 24 ATA 31 – EFIS: PFD A330-200 A350-900 Flight Mode Annunciator (FMA) Flight Mode Annunciator (FMA) Complete Basic T ILS deviation / marker Radio altitude © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Outer DU Complete Basic T ILS deviation / marker Radio altitude Memo Zone Aircraft Configuration Indication Limitations Zone (in flight) Pitch TRIM (on ground only) Rudder Trim Indication (When different from zero) The lower part of the PFD: • Displays memos and limitations • Displays pitch trim indications (on ground only) • Indicates the position of the slats/flaps, speedbrakes, and landing gear • Displays rudder trim indications (only when needed). PR1010081 A350 ↔ A330 Comparison Inner DU ATA 31 - 5 / 24 ATA 31 – EFIS: ND A330-200 A350-900 Navigation Display (ND) Navigation Display (ND) © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Inner DU Vertical Display (VD) The Vertical Display (VD) displays: • FMS flight path • Current flight path • Safety altitudes • Constrains • Weather radar information • Surveillance (SURV) information. Inner DU PR1010081 A350 ↔ A330 Comparison ATA 31 - 6 / 24 ATA 31 – ECAM A330-200 A350-900 Mailbox Engine Display (ED) Engine Display (ED) Memo Zone Limitation Zone System Display (SD) Warning Display (WD) Center Upper DU Permanent Data © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Center Upper DU System Display (SD) The permanent data zone includes the Fuel On Board (FOB) and a time reference. Permanent Data The WD displays: • Limitations and memos • ECAM alerts and associated: • Sensed abnormal or emergency procedures • Deferred procedures • Not-sensed abnormal or emergency procedures. Center Lower DU The SD can display dispatch messages. The memo zone displays: • Memos • ECAM alerts The ECAM manages the abnormal checklists. The MFDs display the normal checklists. PR1010081 A350 ↔ A330 Comparison ATA 31 - 7 / 24 ATA 31 – ECAM: WD A330-200 A350-900 The A330 not-sensed abnormal and emergency procedures are available in the Quick Reference Handbook (QRH). On the A350, the flight crew can manually activate and display not-sensed procedures (abnormal and emergency procedures) on the WD, by using the ECP. The flight crew can also activate and display deferred procedures. Emergency procedures are directly accessible and displayed in red. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. WD RCL LAST pb DEFRD pb ABN pb Abnormal procedures are accessible via submenus in white. TICK pb (one per flight crewmember) RCL ALL pb Wheel (one per flight crewmember) CLEAR pb (one per flight crewmember) QRH PR1010081 A350 ↔ A330 Comparison ECP ATA 31 - 8 / 24 ATA 31 – ECAM: WD and SD A330-200 A350-900 On the A330, the flight crew can refer to the ECAM alerts to access the MEL items in the MEL. On the A350, the flight crew uses the dispatch messages to access the MEL items. The flight crew can display the dispatch messages on the SD via the DISPCH pb on the ECP. Dispatch Message ECAM Alert © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. ECAM Alert on WD Dispatch Messages on SD DISPCH pb ECP PR1010081 A350 ↔ A330 Comparison ATA 31 - 9 / 24 ATA 31 – ECAM and DCDU A330-200 A350-900 Mailbox © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Data-link Control and Display Unit (DCDU) , optional Center Upper DU PR1010081 A350 ↔ A330 Comparison ATA 31 - 10 / 24 ATA 31 – MFD and MCDU A330-200 A350-900 Captain (CAPT) Multifunction Display (MFD) First Officer (F/O) Multifunction Display (MFD) © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Center Lower DU Multipurpose Control Display Units (MCDU) The MCDUs are used for: • The Flight Management System (FMS) • Maintenance purposes. The MFDs are used for: • The Flight Management System (FMS) • The Flight Control Units (FCU) backup • Air Traffic Control (ATC) datalink • SURV • Normal checklists. The flight crew uses the Keyboard Cursor and Control Units (KCCUs) to interface with the MFDs. PR1010081 A350 ↔ A330 Comparison ATA 31 - 11 / 24 ATA 31 – MFD : Checklists A330-200 A350-900 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Checklist Page on MFD QRH The flight crew can access the checklists in the Quick Reference Handbook (QRH). PR1010081 A350 ↔ A330 Comparison The flight crew can access checklists on the MFD, by using the KCCU. ATA 31 - 12 / 24 ATA 31 – OIS A330-200 A350-900 The A330 has an optional OIS, independent of the CDS. Some applications are available via FlySmart with Airbus. (Refer to ATA 46 – Information Systems and ATC Communication System). © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Onboard Information System (OIS) The OIS provides applications for: • Performance computation • Documentation (FCOM, AFM, CDL, MMEL, FCTM, CCOM, WBM, airline documentation) • Other tools: • e-Flight Folder, optional • e-Logbook • Airline Operational Control (AOC), optional • e-Charts. A keyboard in the sliding table provides control of the OIS to each flight crewmember. The KCCU also controls the OIS. Note: The OIS can be displayed on the center lower DU by pressing the OIS ON CENTER pb. PR1010081 A350 ↔ A330 Comparison ATA 31 - 13 / 24 ATA 31 – HUD A330-200 A350-900 The A330 has no HUD. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Head-Up Display (HUD) The Dual HUD is optional on A350. The HUD automatically adapts the symbols to the following flight phases: • Taxi • Takeoff • Rollout or rejected takeoff • Flight. PR1010081 A350 ↔ A330 Comparison ATA 31 - 14 / 24 ATA 31 – KCCU A330-200 A350-900 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. The A330 has no KCCU. Multipurpose Control Display Units (MCDU) The MCDU has a keyboard and shortcut keys that are used only with the applications of the MCDU. PR1010081 A350 ↔ A330 Comparison Keyboard and Cursor Control Unit (KCCU) There is a KCCU for each flight crewmember. The KCCUs enable the flight crew to interface with the ND, MFD, the mailbox and the OIS. ATA 31 - 15 / 24 ATA 31 – Controls A330-200 EFIS CP PFD ND CAPT EFIS CP CAPT and F/O ECP A350-900 EFIS CP EFIS CP EWD SD PERM ND PFD ND PFD F/O EFIS CP ECP EFIS CP ED SD PERM Keyboard CAPT EFIS CP KCCU Keyboard CAPT and F/O ECP Mailbox WD MFD MFD KCCU KCCU ECP ND PFD Keyboard F/O EFIS CP KCCU Keyboard Each flight crew member can use the EFIS CP to control the EFIS. The flight crew can use the ECP to control the SD and the E/WD. The flight crew can use the ECP to control the SD and the WD. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Each flight crewmember can use the EFIS CP to control the EFIS. Each flight crewmember can use the KCCU to interface with: • Both MFDs • One OIS • One ND • The mailbox. Each flight crewmember can use the keyboard to interface with the OIS. PR1010081 A350 ↔ A330 Comparison ATA 31 - 16 / 24 ATA 31 – Clock A330-200 A350-900 Permanent Data The time is displayed on the permanent data zone. Clock © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Digital Clock Note: The A330 has one Clock, either the digital clock or the basic clock. TIME Page of the MFD Permanent Data PR1010081 A350 ↔ A330 Comparison The POSITION/ TIME page of the MFD displays the time reference used by the aircraft. The flight crew can: • Change the time reference • Create time markers • Display the block time, flight time, date, or UTC only • Display departure and arrival airport local times. ATA 31 - 17 / 24 ATA 31 – Video A330-200 The A330 has no CMV. A350-900 The Concentrator and Multiplexer for Video (CMV) manages different video sources: • The Cockpit Door Surveillance System (CDSS) • The Cabin Video Monitoring System (CVMS) as an option • The External and Taxiing Aid Camera System (ETACS) as an option • The Airport Navigation Function (ANF). © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. The VIDEO pb displays the video on the SD. ECP PR1010081 A350 ↔ A330 Comparison The VIDEO knob enables the flight crew to select the video source to be displayed on the SD. ATA 31 - 18 / 24 ATA 31 – Video: CDSS and CVMS A330-200 A350-900 The A330 has no CVMS. The A330 has a CDSS. Cockpit Door Surveillance System (CDSS) Cabin Video Monitoring System (CVMS), option © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Cockpit Door Surveillance System (CDSS) on Lower ECAM, option The Cockpit Door Surveillance System (CDSS) enables the flight crew to identify people requesting to enter the cockpit. The video is displayed on the center lower DU. The CDSS enables the flight crew to identify people requesting to enter the cockpit. The flight crew can display the video of the CDSS on the lower ECAM by pressing the VIDEO pb on the CKPT DOOR CP. The flight crew can display the video from the CVMS and the CDSS on the SD by pressing the VIDEO pb on the ECP and selecting the source with the VIDEO knob. PR1010081 A350 ↔ A330 Comparison The CVMS enables the flight crew to monitor different areas of the cabin. ATA 31 - 19 / 24 ATA 31 – Video: ETACS A330-200 A350-900 The A330 has no ETACS. ETACS on A340-600 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. External and Taxiing Camera System (ETACS), option The ETACS displays the videos from the tail camera and from the camera that is below the fuselage. The flight crew can display the ETACS on the PFD by pressing the TAXI pb on the EFIS CP. PR1010081 A350 ↔ A330 Comparison ATA 31 - 20 / 24 ATA 31 – Controls and Indicators A330-200 A350-900 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. DISPLAY CYCLE pb Attentiongetters EFIS CP Attentiongetters EFIS CP HUD CP (option) PR1010081 A350 ↔ A330 Comparison ATA 31 - 21 / 24 ATA 31 – Controls and Indicators © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. A330-200 A350-900 The ECP includes more controls dedicated to abnormal and emergency procedures. ECP PR1010081 A350 ↔ A330 Comparison ECP ATA 31 - 22 / 24 ATA 31 – Recording Systems A330-200 A350-900 The A330 has: • A Cockpit Voice Recorder (CVR) • A Digital Flight Data Recorder (DFDR) • A linear 3-axis accelerometer • A Virtual Digital ACMS Recorder (VDAR), optional. The A350 has: • A Cockpit Voice Recorder (CVR) • A Digital Flight Data Recorder (DFDR) • A linear 3-axis accelerometer • A Virtual Digital ACMS Recorder (VDAR) • A Virtual Quick Access Recorder (VQAR) • An optional Quick Access Recorder (QAR). Cockpit Area Microphone (CAM) Cockpit Area Microphone (CAM) •Voice Communications •Audio Signals •Voice Communications •Audio Signals Datalink Recordings CVR Panel CVR Panel CVR © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Datalink Recordings Aircraft Systems CVR Aircraft Systems DFDR DFDR VDAR (optional) VDAR VQAR Linear 3-axis accelerometer PR1010081 A350 ↔ A330 Comparison Linear 3-axis accelerometer QAR ATA 31 - 23 / 24 ATA 31 – Control and Indicators A330-200 A350-900 CVR Control Panel CVR Control Panel © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. RCDR GND CTL pb ACMS TRIGGER pb, DFDR EVENT pb and RCDR GND CTL pb ACMS PRINT pb and DFDR EVENT pb PR1010081 A350 ↔ A330 Comparison All recording systems controls are on the overhead panel. ATA 31 - 24 / 24 A350 A330 Comparison Flight↔ Deck and Systems Briefing for Pilots Landing Gear ATA 32 ATA 32 – Landing Gear A330-200 A350-900 Wheelbase: 28.66 m Wheelbase: 25.37 m Wheeltrack: 10.60 m Wheeltrack: 10.68 m © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. The A330 has: • Two Main Landing Gears (MLG) equipped with four wheels • One Nose Landing Gear (NLG) equipped with two wheels. The A350-900 has: • Two Main Landing Gears (MLG) equipped with four wheels • One Nose Landing Gear (NLG) equipped with two wheels. Minimum turn width with symmetrical thrust and no braking. Minimum turn width with symmetrical thrust and no braking. 43.58 m PR1010081 A350 ↔ A330 Comparison 51.01 m ATA 32 - 2 / 10 ATA 32 – Braking and Steering A330-200 In the case of GREEN HYD failure, steering control is provided by differential braking actions on the pedals. Steering: GREEN HYD © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Normal braking: GREEN HYD Alternate braking: BLUE HYD Braking Modes (A330) HYD power supply NORMAL GREEN ALTERNATE with A-SKID BLUE ALTERNATE without A-SKID PARKING / ULTIMATE A350-900 The Autobrake (AUTO BRK) function is available in three levels: LOW, MED, MAX. Steering : YELLOW HYD Main Landing Gear braking: Front wheels, YELLOW HYD Aft wheels, GREEN HYD. The AUTO BRK function is available. The Brake To Vacate (BTV) function optimizes the braking. Braking Performances Braking Modes (A350) HYD power supply Cockpit interface A-SKID, AUTO Pedals, AUTO BRK BRK, differential panel braking Normal NORMAL GREEN and YELLOW Pedals, AUTO BRK panel Pedals, A-SKID, differential braking Normal ALTERNATE with A/SKID ACCUs Pedals, AUTO BRK panel BLUE ACCUs Pedals Differential braking Degraded EMERGENCY ACCUs Pedals BLUE ACCUs PRK BRK Lever PRK BRK N/A PARKING / ULTIMATE ACCUs PRK BRK lever Cockpit interface Available functions In the case of steering actuation failure, steering control is provided by the Backup Steering Function (BSF). The BSF allows the pilot to steer the aircraft through differential braking controlled with the steering handwheel. Available functions A/SKID, AUTO BRK, BTV, ADB, differential braking A/SKID, AUTO BRK, ADB, differential braking ADB, limited brake pressure, differential braking Braking performances Normal Normal Degraded PRK BRK *Note: On A330, the limited brake pressure to 1000 psi is currently introduced on the fleet. PR1010081 A350 ↔ A330 Comparison ATA 32 - 3 / 10 N/A ATA 32 – Landing Gear Retraction and Extension A330-200 The GREEN HYD supplies power to the MLG and the NLG for extension and retraction. A350-900 The GREEN HYD supplies power to the MLG for extension and retraction. The YELLOW HYD supplies power to the NLG for extension and retraction. The maximum speed with landing gear extended (VLE) is 250 kt. The maximum speed for extension and retraction of landing gear (VLO) is 250 kt. The maximum speed for extension and retraction of landing gear (VLO) is 250 kt. The landing gear can be extended by gravity up to a speed of 200 kt. The landing gear can be extended by gravity up to a speed of 250 kt. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. The maximum speed with landing gear extended (VLE) is 250 kt. PR1010081 A350 ↔ A330 Comparison ATA 32 - 4 / 10 ATA 32 – Antiskid, Autobrake and BTV A330-200 A350-900 The A350 is fitted with Brake To Vacate (BTV) system. BTV is an autobrake function that adapts the braking to a selected exit of a runway and the selected runway condition or braking action. The A330 has no BTV. BTV optimizes the use of brakes and thrust reversers devices and permits to reduce the runway occupation time. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. On A330, the autobrake has three levels of braking: LOW, MED, MAX. BRAKE Control Panel PR1010081 A350 ↔ A330 Comparison BTV on ND BRAKE Control Panel ATA 32 - 5 / 10 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. ATA 32 – Controls and Indicators A330-200 A350-900 WHEEL SD Page WHEEL SD Page The brake pressure and the ACCUs pressure are displayed on the WHEEL SD Page PR1010081 A350 ↔ A330 Comparison ATA 32 - 6 / 10 ATA 32 – Controls and Indicators © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. A330-200 A350-900 L/G position Indication LDG GEAR Lever PR1010081 A350 ↔ A330 Comparison LDG GEAR Lights L/G Lever The L/G position indication is below each PFD. ATA 32 - 7 / 10 ATA 32 – Controls and Indicators A330-200 A350-900 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Thrust Levers On the runway, A/THR instinctive disconnect pushbuttons used for Autobrake disconnection PARK BRK Handle PR1010081 A350 ↔ A330 Comparison PARK BRK Handle ATA 32 - 8 / 10 ATA 32 – Controls and Indicators A330-200 A350-900 An ACCUS REINFLATE pb enables the flight crew to reinflate the ACCUs using the electrical motor pumps. ACCUs and alternate BRAKES pressure indicator © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. ACCUs pressure indicator and ACCUS REINFLATE pb The ACCUs Pressure Indicator is on the Pedestal. The ACCUs pressure indicator only displays the available pressure in the different ACCUs. PR1010081 A350 ↔ A330 Comparison ATA 32 - 9 / 10 ATA 32 – Controls and Indicators © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. A330-200 A350-900 The L/G GRVTY EXTN is on the pedestal LDG GEAR GRVTY EXTN Control Panel PR1010081 A350 ↔ A330 Comparison L/G GRVTY EXTN Control Panel ATA 32 - 10 / 10 A350 A330 Comparison Flight↔ Deck and Systems Briefing for Pilots Lights ATA 33 ATA 33 – Interior Lighting A330-200 Interior Lighting is similar. A350-900 The A350 cockpit has: • Utility lights • Ambient lights • Area and panel lights. The emergency lighting includes: • The ambient lights of the cockpit • Cabin emergency lighting • Emergency Exit lights (EMER EXIT LT). The emergency lighting includes: • The ambient lights of the cockpit • Cabin emergency lighting • Emergency Exits Light (EMER EXIT LT). Emergency lights come automatically ON when: • The flight crew sets the EMER EXIT LT switch to ARM, and • The aircraft electrical supply is degraded. Emergency lights come automatically ON when: • The flight crew sets the EMER EXIT LT switch to ARM, and • The aircraft electrical supply is degraded. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. The A330 cockpit has: • Utility lights • Ambient lights • Area and panel lights. PR1010081 A350 ↔ A330 Comparison ATA 33 - 2 / 6 ATA 33 – Controls and Indicators A330-200 A350-900 INT LT and SIGNS Control Panels INT LT and SIGNS Control Panels © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. FLOOD LT and INTEG LT knobs MAP LT and CONSOLE LT knobs, one per flight crewmember FLOOD LT knob CKPT LT Control Panel Left and right LT Control Panels, one per flight crewmember PR1010081 A350 ↔ A330 Comparison The dome lighting is controlled by a DOME LT knob. ATA 33 - 3 / 6 ATA 33 – Exterior Lighting A330-200 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. The A330 has: • Navigation lights • Landing lights • Taxi lights • Runway turnoff lights • Takeoff lights • Logo lights • Beacon lights • Strobe lights • Wing and engine scan lights PR1010081 A350 ↔ A330 Comparison Exterior Lighting is similar. A350-900 The A350 has: • Navigation lights • Landing lights • Taxi lights • Runway turnoff lights • Takeoff lights • Logo lights • Beacon lights • Strobe lights • Wing and engine scan lights • Taxi camera lights (optional) ATA 33 - 4 / 6 ATA 33 – Controls and Indicators A330-200 EXT LT Control Panels are similar. A350-900 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. The control of the runway turn off lights is integrated to the NOSE light sw, on the TAXI position. EXT LT Control Panel PR1010081 A350 ↔ A330 Comparison EXT LT Control Panel ATA 33 - 5 / 6 ATA 33 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Intentionally Left Blank PR1010081 A350 ↔ A330 Comparison ATA 33 - 6 / 6 A350 A330 Comparison Flight↔ Deck and Systems Briefing for Pilots Navigation and Surveillance ATA 34 ATA 34 – Navigation A350-900 The navigation system of the A330 provides: • Flight and navigation parameters • Navigation aids tuning and reception • Navigation back-up. The navigation system of the A350 provides: • Flight and navigation parameters • Navigation aids tuning and reception • Navigation backup. The following systems are providing navigation parameters to the navigation system: • Air Data and Inertial Reference System (ADIRS) • Radio NAVAIDS • Two Radio Altimeters (RAs) • Multi-Mode Receivers (MMRs). The following systems are providing navigation parameters to the navigation system: • Air Data and Inertial Reference System (ADIRS) • Three Radio Altimeters (RAs) • Multi-Mode Receivers (MMRs), that include GNSS and Radio NAVAIDS. The A330 has a back-up navigation system that has: • One standby magnetic compass • One Integrated Standby Instrument System (ISIS). The A350 has a backup navigation system that has: • One standby magnetic compass • One Integrated Standby Instrument System (ISIS) and a second one as an option. The navigation and surveillance system also provides: • Surveillance function. The navigation and surveillance system also provides: • Surveillance function • Airport Navigation Function (ANF). © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. A330-200 PR1010081 A350 ↔ A330 Comparison ATA 34 - 2 / 12 ATA 34 – ADIRS A330-200 A350-900 The A330 has three Air Data and Inertial Reference Units (ADIRUs). Each ADIRU has an Air Data Reference (ADR) part and an Inertial Reference (IR) part. The A350 has three Air Data and Inertial Reference Units (ADIRUs). Each ADIRU has an Air Data Reference (ADR) part and an Inertial Reference (IR) part. The ADR part determines the flight parameters. Each ADR is connected to : • One Pitot probe • Two static ports • One Angle of Attack (AOA) probe • One Total Air Temperature (TAT) probe. The ADR part determines the flight parameters. Each ADR is connected to: • One Multi-Function Probe (MFP), which provides the total pressure, TAT and AOA measurement • Two Integrated Static Probes (ISPs) • One Side Slip Angle (SSA) probe • One Outside Air Temperature (OAT) probe. The Integrated Standby Instrument System (ISIS) (or the standby instruments on an A330 Classic) receives air data from the same probes as ADIRU 3. The Integrated Standby Instrument System (ISIS) receives data from a dedicated Pitot probe and dedicated static probes. ADIRU 1 ADIRU 3 TAT ADIRU 1 ADIRU 2 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Pitot Probe Static Ports ADIRU 2 ISIS TAT ISIS AOA ADIRU 3 AOA Pitot Probe Static Ports AOA OAT Pitot Probe Static Ports The IR part determines the navigation parameters (orientation). The IR uses: • Data from internal gyros and accelerometers sensors • MMR data (optional). MFP ISPs SSA OAT MFP ISPs SSA Pitot Probe MFP ISPs SSA The IR part determines the navigation parameters (aircraft position, time function and orientation). The IR uses: • Data from internal gyros and accelerometers sensors • MMR data • FMS computed position. Note: The FMGC computes the aircraft position, based on data received from the ADIRS (mixed with other data). PR1010081 A350 ↔ A330 Comparison Static Probe ATA 34 - 3 / 12 ATA 34 – Standby Instruments A330-200 The A330 has: • One Integrated Standby Instrument System (ISIS) • One standby magnetic compass • One Digital Distance and Radio Magnetic Indicator (DDRMI). A350-900 The A350 has: • One Integrated Standby Instrument System (ISIS) and a second one as an option • One standby magnetic compass. On the ISIS, two modes are available: • Standby Flight Display (SFD) • Standby Navigation Display (SND). The ISIS receives: • Air Data from standby Pitot probe and standby static ports • IR data from the ADIRU 1 or 3 • LOC & G/S deviation, identifier & frequencies, GPS position and ground speed from ILS 1 or MMR 1. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. ISIS Note: Oldest versions of the A330 do not have ISIS, but have a standby attitude indicator, a standby air speed indicator and a standby altitude indicator. The ISIS receives: • Air data from a dedicated Pitot probe and a dedicated static probe • IR data from the ADIRU 1 or 3 • LOC & G/S deviation, identifier & frequencies, GNSS position and ground speed from the MMR 1. ISIS in SFD Mode If only one ISIS is installed, it can display only the SFD. If the second optional ISIS is installed, both ISIS cannot display the same mode and there is always one SFD displayed. ISIS in SND Mode PR1010081 A350 ↔ A330 Comparison ATA 34 - 4 / 12 ATA 34 – Surveillance A330-200 A350-900 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. The A350 has two independent and fully redundant Surveillance (SURV) systems. The A330 has the following surveillance functions: • Weather Radar • Traffic Alert and Collision Avoidance System (TCAS) • Terrain Awareness and Warning System (TAWS) • Transponder (XPDR). The A350 has the following surveillance functions: • Weather Radar (WXR) • Traffic Alert and Collision Avoidance System (TCAS) including AP/FD TCAS and Aircraft Traffic Situational Awareness (ATSAW) • Terrain Awareness and Warning System (TAWS) • Transponder (XPDR). TAWS The TAWS function provides a: • Basic ground proximity warning (GPWS modes 1 to 5) • Terrain (TERR) awareness, alert and display • Database including terrain. TAWS The A350 TAWS is an enhanced version of previous TAWS. The TAWS function provides a: • Basic ground proximity warning (GPWS modes 1 to 5) • Terrain (TERR) and obstacle awareness, alert and display function • Database including terrain, obstacle, runways, specific areas. The TAWS function displays information on the PFD and ND. AP/FD TCAS The AP/FD TCAS is currently under development to be installed on the A330. AP/FD TCAS The AP/FD TCAS is an AP/FD vertical mode that provides vertical guidance in the case of a TCAS Resolution Advisory (TCAS RA) alert. This function provides clear flying orders via the FD bars. Those orders are designed to avoid potential over-reactions and to minimize the deviation from the initial ATC clearance. If the auto pilot is engaged, the AP/FD TCAS automatically performs the avoidance procedure. If both APs and FDs are disengaged, the FD automatically engage. A smart altitude capture is provided to avoid spurious TCAS alert. ATSAW The ATSAW function is under development and will be available on the A330, as an option. ATSAW The ATSAW displays the traffic information from the ADS-B according to the situation. PR1010081 A350 ↔ A330 Comparison ATA 34 - 5 / 12 ATA 34 – Airport Navigation Function A330-200 The A330 has no Airport Navigation Function (ANF). A350-900 The Airport Navigation Function (ANF) provides the flight crew with a moving airport map, that is displayed on the ND. The ANF uses: • Airport data stored in an airport database • Aircraft data mainly from the FMS and the ADIRS • Flight crew data entries. The ANF can display the traffic of other aircraft on the airport (future evolution). © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. The flight crew uses the KCCU to interface with the ANF. PR1010081 A350 ↔ A330 Comparison ATA 34 - 6 / 12 ATA 34 – Airport Navigation Function A330-200 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. The A330 has no Airport Navigation Function (ANF). A350-900 The ANF displays ground clearance information to help the flight crew correctly maneuver the aircraft during taxi. The ground clearance are transferred via the Controller/Pilot Datalink Communication (CPDLC). The path requested by the flight crew is blue before acknowledgment and becomes green after acknowledgment. (the information presented is not yet available , it is a future evolution.) PR1010081 A350 ↔ A330 Comparison ATA 34 - 7 / 12 ATA 34 – Runway Proximity Advisory A330-200 A350-900 The A330 has an optional Runway Awareness and Advisory System (RAAS) that enhances the flight crew’s awareness of the aircraft position on ground. The A350 has a runway proximity advisory that warns the flight crew when the aircraft approaches a runway. The runway proximity advisory: • Reduces the risk of runway incursions • Improves runway situational awareness. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. The RAAS triggers aural alerts in the three following cases: • When approaching the runway (e.g. “Approaching three two right”) • When the aircraft is on the runway and aligned with the runway direction (e.g. “On runway three two right”) • If the aircraft speed exceeds 40 knots, while not on a runway (“On taxiway! On taxiway!”). The Takeoff Securing (TOS) function is currently under development to be installed on the A330. PR1010081 A350 ↔ A330 Comparison When the aircraft approaches a runway: • The runway name pulses on the ND • The runway flashes on the airport map. Note: There is no audio indication. The Takeoff Securing (TOS) function checks that the aircraft prepares to take off on the runway defined on the FMS takeoff page. The TOS function checks other parameters. For more information on TOS, refer to ATA 22 chapter. ATA 34 - 8 / 12 ATA 34 – ROW/ROP A330-200 ROW/ROP is currently under development to be installed on the A330. A350-900 The Runway Overrun Warning and Runway Overrun Protection (ROW/ROP) are two functions designed to enhance the safety during final approach, landing and deceleration. ROW enhances the pilot situational awareness of the predicted braking distances. ROW encourages to go around or to correct the flight parameters. ROW triggers cautions or warnings on PFD and aural alerts. ROW also displays on ND the predicted area where the aircraft will stop. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. The ROW/ ROP transition point is the point where the aircraft is confirmed to be on ground. If a runway end overrun is detected, ROP commands the maximum braking (in autobrake mode) and triggers alerts on the PFD with associated aural alerts. Example of ROW Cautions and Warnings ROW on ND Example of ROP Warnings PR1010081 A350 ↔ A330 Comparison ATA 34 - 9 / 12 ATA 34 – Controls and Indicators © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. A330-200 SWITCHING Panel PR1010081 A350 ↔ A330 Comparison A350-900 ATT HDG and AIR DATA Selectors ATA 34 - 10 / 12 ATA 34 – Controls and Indicators © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. A330-200 ADIRS Control Panel PR1010081 A350 ↔ A330 Comparison A350-900 ADIRS Control Panel ATA 34 - 11 / 12 ATA 34 – Controls and Indicators A330-200 A350-900 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. WX/RADAR Control Panel Radio Management Panels (RMPs) The flightcrew can change the squawk on the RMPs or on the MFD SURV page. ATC/TCAS Control Panel SURV Panel PR1010081 A350 ↔ A330 Comparison ATA 34 - 12 / 12 A350 A330 Comparison Flight↔ Deck and Systems Briefing for Pilots Oxygen System ATA 35 ATA 35 – System Description A330-200 A350-900 The A350 has: • A fixed oxygen system in the cockpit • A fixed oxygen system in the cabin • Protective Breathing Equipments (PBEs) for the cockpit and the cabin. The oxygen for the flight crew is stored in one oxygen cylinder. This oxygen cylinder can be replaced by two smaller oxygen cylinders, that together contain more oxygen. The oxygen for the flight crew is supplied by two segregated systems. Each system has one oxygen bottle. Two additional oxygen cylinders can be optionally installed. A chemical system provides oxygen for the cabin crew and the passengers. Optional gaseous items can extend the supply duration. A chemical system provides oxygen to the cabin crew and the passengers. Optional items (chemical or gaseous) can extend the supply duration. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. The A330 has: • A fixed oxygen system in the cockpit • A fixed oxygen system in the cabin • Protective Breathing Equipments (PBEs) for the cockpit and the cabin. PR1010081 A350 ↔ A330 Comparison ATA 35 - 2 / 4 ATA 35 – Controls and Indicators A330-200 Controls and Indicators are similar. A350-900 OXYGEN RESET pb © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. OXYGEN TMR RESET pb OXYGEN Control Panel PR1010081 A350 ↔ A330 Comparison OXYGEN Control Panel ATA 35 - 3 / 4 ATA 35 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Intentionally Left Blank PR1010081 A350 ↔ A330 Comparison ATA 35 - 4 / 4 A350 A330 Comparison Flight↔ Deck and Systems Briefing for Pilots Avionics Network ATA 42 ATA 42 – IMA A330-200 A350-900 On the A330, computers are assigned to specific systems. It is a conventional type of avionics. On the A350, computers can monitor and control several systems via several applications. This type of avionics is called Integrated Modular Avionics (IMA). The IMA has: • Core Processing Input / Output Modules (CPIOMs) • Common Remote Data Concentrators (CRDCs). The CPIOMs: • Are directly connected to the Avionics Network • Host several applications, in order to monitor and control several aircraft systems • Transmit signals compatible with: • The Avionics Network • The conventional avionics. Computer The CRDCs: • Gather data from sensors and actuators • Provide these data to all relevant systems via the Avionic Network. Computer © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Computer Computer Computer CRDC Computer CRDC ... Computer Computer Computer PR1010081 A350 ↔ A330 Comparison CRDC CPIOM CPIOM Network 1 Network 2 ... ATA 42 - 2 / 4 ATA 42 – Avionics Network A330-200 The A330 has conventional avionics. A350-900 The avionics network of the A350 is based on a series of Ethernet switches. The Ethernet switches are linked in a way that allows data to be transmitted to a system even in the case of the failure of one Ethernet switch. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Conventional avionics is used as a backup on some systems. PR1010081 A350 ↔ A330 Comparison ATA 42 - 3 / 4 ATA 42 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Intentionally Left Blank PR1010081 A350 ↔ A330 Comparison ATA 42 - 4 / 4 A350 A330 Comparison Flight↔ Deck and Systems Briefing for Pilots Onboard Maintenance System ATA 45 ATA 45 – Onboard Maintenance System A330-200 The A330 has a Central Maintenance System (CMS) support for: • Aircraft servicing • Line, scheduled and unscheduled maintenance • Aircraft configuration and reconfiguration monitoring. A350-900 which provides The A350 has an Onboard Maintenance System (OMS) which provides support for: • Aircraft servicing • Line, scheduled and unscheduled maintenance • Aircraft configuration and reconfiguration monitoring. The CMS has the following functions: • Identification of system failures • Preventive maintenance support • Aircraft configuration management. The OMS has the following functions • Identification of system failures • Preventive maintenance support • Aircraft configuration management • A technical logbook (e-logbook) • An optional cabin logbook (Digital Cabin Logbook). The maintenance team accesses the CMS via the MCDUs. The maintenance team accesses the OMS via the Onboard Maintenance Terminal (OMT) or the Portable Multipurpose Access Terminal (PMAT). The OMT is next to the third occupant seat. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. The PMAT enables the maintenance team to access the OMS via network ports installed at various aircraft locations. PR1010081 A350 ↔ A330 Comparison ATA 45 - 2 / 2 A350 A330 Comparison Flight↔ Deck and Systems Briefing for Pilots Information Systems and ATC Communication System ATA 46 ATA 46 – Onboard Information System A330-200 A350-900 The A330 has an optional Electronic Flight Bag (EFB). The EFB provides: • Flight Operations solutions: • Performance calculation • Electronic manuals (FCOM, MEL) • Electronic charts (airport maps, departure, en route, arrival charts, etc.) • Maintenance solutions: • AirN@v with access to AMM, IPC, TSM and TFU • Airbus Onboard Maintenance Tool (AOMT). The A350 has an Onboard Information System (OIS). The OIS provides: • Flight Operations solutions: • Performance calculation • Electronic documentation (FCOM, AFM, MEL, FCTM, CCOM, airline documentation) • e-Flight Folder • e-Logbook • Airline Operational Control (AOC), optional • e-Charts. For each flight crewmember, the EFB includes: • An Onboard Information Terminal (OIT) that is installed in the sliding table • An OIT keyboard unit that is stored in the lateral stowage. For each flight crewmember, the OIS includes: • A Display Unit (DU), also called Onboard Information Terminal (OIT), located on the outer DU • A keyboard and pointing device • A server switch • A laptop used for Flight Operation applications. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Note: The flight crewmembers can use the KCCUs to control their OIS. The OIS can be displayed on the center lower DU, via OIS ON CENTER pbs. PR1010081 A350 ↔ A330 Comparison ATA 46 - 2 / 8 ATA 46 – Airline Operational Control A330-200 AOC functions are similar. A350-900 The A350 has an optional Airline Operational Control (AOC) function. The AOC enables the Airline to: • Manage flight operations • Check the weather status • Manage departure, takeoff, flight or gates (OOOI) • Manage flight parameters • Receive specific messages at a predefined time during the flight (e.g. when the landing gear is up). The AOC enables the Airline to: • Manage flight operations • Check the weather status • Manage departure, takeoff, flight or gates (OOOI) • Manage flight parameters • Receive specific messages at a predefined time during the flight (e.g. when the landing gear is up). © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. The A330 has an optional Airline Operational Control (AOC) function. PR1010081 A350 ↔ A330 Comparison ATA 46 - 3 / 8 ATA 46 – ATC Communication System A350-900 The A330 has an ATC Communication (ATCCOM) system that provides data communication between the aircraft and the ATC centers. The A350 has an ATC Communication (ATCCOM) system that enables data communication between the aircraft and the ATC centers. The datalink is made via the VHF, HF or SATCOM communication systems. The datalink is made via the VHF, HF or SATCOM communication systems. The ATCCOM includes: • Future Air Navigation System A (FANS A), that uses ACARS network, optional • Future Air Navigation System B (FANS B), that uses the Aeronautical Telecommunication Network (ATN), optional • ARINC 623 Services, optional. The ATCCOM includes: • Future Air Navigation System A (FANS A), that uses ACARS network • Future Air Navigation System B (FANS B), that uses the Aeronautical Telecommunication Network (ATN) • ARINC 623 Services. FANS A and FANS B provide the following functions: • Notification • Controller/Pilot Data Link Communications (CPDLC) • Automatic Dependent Surveillance (ADS). FANS A and FANS B provide the following functions: • Notification • Controller/Pilot Data Link Communications (CPDLC) • Automatic Dependent Surveillance (ADS-C). The ARINC 623 Services provides: • A clearance function for oceanic and departure clearances • A Digital Automatic Terminal Information Service (D-ATIS). The ARINC 623 Services provides: • A clearance function for oceanic and departure clearances • A Digital Automatic Terminal Information Service (D-ATIS). The flight crew interfaces the ATCCOM via: • The Datalink Control and Display Units (DCDUs) • The Multipurpose Control and Display Units (MCDUs). The flight crew interfaces with the ATCCOM via: • The mailbox • The ATCCOM MFD Pages • The KCCUs. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. A330-200 PR1010081 A350 ↔ A330 Comparison ATA 46 - 4 / 8 ATA 46 – Controls and Indicators A330-200 A350-900 CAPT OIS ON CENTER pb F/O OIS ON CENTER pb © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. OIS Panel Electronic Flight Bag (EFB), Optional Onboard Information System (OIS) PR1010081 A350 ↔ A330 Comparison ATA 46 - 5 / 8 ATA 46 – Controls and Indicators © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. A330-200 A350-900 OIS Panel PR1010081 A350 ↔ A330 Comparison ATA 46 - 6 / 8 ATA 46 – Controls and Indicators A330-200 ATC MSG pb A350-900 ATC MSG pb © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Datalink Control and Display Unit (DCDU) Mailbox The Mailbox is used to display ATC messages and to control the sending of messages. The MFD Page is used to: • Compose messages • Receive D-ATIS • Connect to a datalink service. ATCCOM MFD Page PR1010081 A350 ↔ A330 Comparison ATA 46 - 7 / 8 ATA 46 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Intentionally Left Blank PR1010081 A350 ↔ A330 Comparison ATA 46 - 8 / 8 A350 A330 Comparison Flight↔ Deck and Systems Briefing for Pilots Auxiliary Power Unit ATA 49 ATA 49 – APU A330-200 A350-900 The A350 has an Auxiliary Power Unit (APU) that provides: • Electrical Power (230 V, 150 kVA) • Bleed Air. The APU has: • One Electronic Control Box (ECB) • One electrical generator • One electrical starter. The APU has: • One Electronic Control Box (ECB) • One combined starter and generator system. The following power sources can start the APU: • The APU battery • The normal electrical network of the aircraft, via the APU Transformer/Rectifier (APU TR) • The External Power (GPU), via the APU Transformer/Rectifier (APU TR). The following power sources can start the APU: • The aircraft batteries • The normal electrical network of the aircraft • The External Power (GPU). © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. The A330 has an Auxiliary Power Unit (APU) that provides: • Electrical Power (115 V, 115 kVA) • Bleed Air. APU Operating Flight Envelope PR1010081 A350 ↔ A330 Comparison APU Operating Flight Envelope ATA 49 - 2 / 4 ATA 49 – Controls and Indicators © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. A330-200 APU SD Page PR1010081 A350 ↔ A330 Comparison APU SD Pages are similar. A350-900 APU SD Page ATA 49 - 3 / 4 ATA 49 – Controls and Indicators © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. A330-200 APU Control Panel PR1010081 A350 ↔ A330 Comparison APU Control Panels are similar. A350-900 APU Control Panel ATA 49 - 4 / 4 A350 A330 Comparison Flight↔ Deck and Systems Briefing for Pilots Doors ATA 52 ATA 52 – Exterior doors A330-200 A350-900 The A330 has: • Six passenger doors (three on each side) • Two cabin emergency exits • Three lower deck cargo doors (one by compartment) • Three cockpit emergency exits (two sliding windows and the cockpit door) • An internal and an external avionics access doors. The A350 has: • Eight passenger doors (four on each side) • Three lower deck cargo doors (one per compartment) • Two cockpit emergency exits (an escape hatch and the cockpit door) • An internal and an external avionics access doors. The bulk cargo door is on the right hand side. The bulk cargo door is on the left hand side. Passenger Doors Emergency Cabin Exit Escape Hatch Sliding Window Passenger Doors Bulk Door © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Cargo Doors Cargo Doors Passenger Doors Sliding Window Emergency Cabin Exit Avionics Bay Door PR1010081 A350 ↔ A330 Comparison Passenger Doors Avionics Bay Door Bulk Door ATA 52 - 2 / 6 ATA 52 – Cockpit Access A350-900 The A330 has an intrusion and penetration resistant door. This door is electrically controlled and has a mechanical opening device. The A350 has an intrusion and penetration resistant door. This door is electrically controlled and has a mechanical opening device. The flight crew can open the door by using a switch on the pedestal. In the case of a failure of the opening system, the flight crew can open the door by using a mechanical backup. The flight crew can open the door by using a switch on the pedestal. In the case of a failure of the opening system, the flight crew can open the door by using a mechanical backup. The cabin crew uses a keypad to: • Enter a code to request access to the cockpit • Enter an emergency code to access to the cockpit. The cabin crew uses a keypad to: • Enter a code to request access to the cockpit • Enter an emergency code to access to the cockpit. Maintenance teams can disable the cockpit door locking system using a switch on the overhead panel. This switch is optional. Maintenance teams can disable the cockpit door locking system using a pb on the overhead panel. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. A330-200 PR1010081 A350 ↔ A330 Comparison ATA 52 - 3 / 6 ATA 52 – Controls and Indicators © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. A330-200 DOOR/OXY SD Page PR1010081 A350 ↔ A330 Comparison The DOOR parts of the SD pages are similar. A350-900 DOOR SD Page ATA 52 - 4 / 6 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. ATA 52 – Controls and Indicators A330-200 A350-900 COCKPIT DOOR Control Panel CKPT DOOR Control Panel PR1010081 A350 ↔ A330 Comparison ATA 52 - 5 / 6 ATA 52 – Controls and Indicators A330-200 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. CKPT DOOR CONT Panel A350-900 CKPT DOOR CTRL Panel CKPT DOOR LOCKG SYS pb CKPT DOOR BK UP Panel PR1010081 A350 ↔ A330 Comparison On the maintenance panel, a CKPT DOOR LOCKG SYS pb deactivates the door locking system. ATA 52 - 6 / 6 A350 A330 Comparison Flight↔ Deck and Systems Briefing for Pilots Engines ATA 70 ATA 70 – Engines A330-200 A350-900 The A350 has two: • Rolls Royce Trent XWB. Each engine provides from 64 000 to 72 000 lb of thrust (maximum takeoff at MSL), depending on the engine type and variant. Each engine provides 84 000 lb of thrust (maximum takeoff at MSL). PW and RR engines are equipped with thrust reversers powered by hydraulic circuits. GE engines are equipped with thrust reversers powered by pneumatic. RR engines are equipped with thrust reversers powered by electrical networks. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. The A330 has two: • Rolls Royce Trent 700, or • General Electric CF6-80, or • Pratt & Whitney PW4000. PR1010081 A350 ↔ A330 Comparison ATA 70 - 2 / 6 ATA 70 – Controls and Indicators A330-200 A350-900 ECAM © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Engine Display (ED) E/WD The reference is the THRUST parameter which is valid for any engine. The THR parameter is a percentage of the maximum thrust available (100%THR corresponds to the maximum thrust, when thrust lever are set to TOGA detent and all engine bleeds are off). The ED displays the thrust produced by the engine at the different thrust settings. Note: This is the Engine Display for RR powered A330. The Engine display is slightly different, depending on the engine type. PR1010081 A350 ↔ A330 Comparison ATA 70 - 3 / 6 ATA 70 – Controls and Indicators A330-200 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. ENGINE SD Page A350-900 ENG SD Page Note: This is the ENG SD Page for RR powered A330. On GE and PW powered A330, there is neither N2% nor N3 indications. PR1010081 A350 ↔ A330 Comparison ATA 70 - 4 / 6 ATA 70 – Controls and Indicators A330-200 A350-900 Thrust Levers © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Thrust Levers ENG MASTER Control Panel PR1010081 A350 ↔ A330 Comparison The FIRE and FAULT lights are on the ENG MASTER switches. ENG MASTER Control Panel ENG START Selector ATA 70 - 5 / 6 ATA 70 – Controls and Indicators A330-200 A350-900 ENG FADEC GND PWR pbs © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. ENG FADEC GND PWR pbs RR and PW powered A330 only ENG Control Panel PR1010081 A350 ↔ A330 Comparison Note: The N1 MODE pushbuttons are installed only on RR and PW powered A330. ENG Control Panel ATA 70 - 6 / 6 List of Abbreviations © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. A • • • • • • • • • • • • • • • • • • • • • • • • A/THR AC ACMS ACP ACUTE ADB ADHF ADIRS ADIRU ADS AFM AFS AFS CP A-ICE ALT AOA AOC AP APPR APU ATC ATSAW ATU AVNCS Autothrust Alternating Current Aircraft Condition Monitoring System ATC Control Panel Airbus Cockpit Universal Thrust Emulator Automatic Differential Braking Adaptive Dropped Hinge Flap Air Data and Inertial Reference System Air Data and Inertial Reference Unit Automatic Dependent Surveillance Airplane Flight Manual Automatic Flight System AFS Control Panel Anti-Ice Altitude Angle-of-Attack Airline Operational Control Autopilot Approach Auxiliary Power Unit Air Traffic Control Aircraft Traffic Situation Awareness Automatic Transfer Unit Avionics PR1010081 A350 ↔ A330 Comparison B • • • • • C • • • • • • • • • • • • • • • • • • BAT BCM BPS BITE BTV Battery Backup Control Module Backup Power Supply Built-In Test Equipment Brake To Vacate C/L CAM CAPT CCOM CDL CDS CDSS CG CL CMS CMV CP CPDLC CPIOM CRDC CRZ CVMS CVR Checklist Cockpit Area Microphone Captain Cabin Crew Operating Manual Configuration Deviation List Control and Display System Cockpit Door Surveillance System Center of Gravity Climb Central Maintenance System Concentrator and Multiplexer for Video Control Panel Controller/Pilot Datalink Communication Core Processing Input/Output Module Common Remote Data Concentrators Cruise Cabin Video Monitoring System Cockpit Voice Recorder ABB.1 List of Abbreviations D • • • • • • • • • • © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. E • • • • • • • • • • • • • • F D-ATIS DC DCDU DDRMI DFS DFDR DMC DME DND DU Digital Automatic Terminal Information Service Direct Current Data-link Control and Display Unit Digital Distance and Radio Magnetic Indicator Differential Flaps Setting Digital Flight Data Recorder Display Management Computer Distance Measuring Equipment Droop Nose Device Display Unit ECAM ECB ECP ED EDP EFB EFIS EIS e-Logbook ELT EMP ETACS EVAC EXT Electronic Centralized Aircraft Monitoring Electronic Control Box ECAM Control Panel Engine Display Engine Driven Pump Electronic Flight Bag Electronic Flight Instrument System Entry Into Service Electronic Logbook Emergency Locator Transmitter Electric Motor Pump External and Taxiing Aid Camera System Evacuation External PR1010081 A350 ↔ A330 Comparison • • • • • • • • • • • • • • • • • • F/CTL F-PLN F/O FADEC FAP FCDC FCMC FCOM FCTM FCU FD FE FG FL FLS FMA FMC FMGC • • • • • • • FMS FOB FQMS FSOV FWC FWD FWS Flight Controls Flight Plan First Officer Full Authority Digital Engine Control Flight Attendant Panel Flight Control Data Concentrator Fuel Control and Monitoring Computers Flight Crew Operating Manual Flight Crew Training Manual Flight Control Unit Flight Director Flight Envelope Flight Guidance Flight Level FMS Landing System Flight Mode Annunciator Flight Management Computer Flight Management, Guidance and envelope Computer Flight Management System Fuel On Board Fuel Quantity and Management System Fire Shutoff Valve Flight Warning Computer Forward Flight Warning System ABB.2 List of Abbreviations G • • • • • • • • • • H © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. • • • • I • • • • • • • G/S GA GEN GLS GNSS GPS GPU GPWS HDG HF Glide slope Go-Around Generator GNSS Landing System Global Navigation Satellite System Global Positioning System Ground Power Unit Ground Proximity Warning System Heading High Frequency HP HSMU HUD HYD High Pressure Hydraulic System Monitoring Unit Head-Up Display Hydraulic K • KCCU L • • • • • • • • • • • M IFE ILS IMA IP IR ISIS ISP In-Flight Entertainment Instrument Landing System Integrated Modular Avionics Intermediate Pressure Inertial Reference Integrated Standby Instrument System Integrated Static Probe PR1010081 A350 ↔ A330 Comparison • • • • • • • • • Keyboard and Cursor Control Unit LCD LCTR LDG L/G LGCIS LGERS LOC LP LRC LRU LVL Liquid Crystal Display Locator Landing Landing Gear Landing Gear Control and Indicating System Landing Gear Extension and Retraction System Localizer Low Pressure Long Range Cruise Line Replaceable Unit Level MCT MCDU MEL MFD MFP MLG MLW MMO MMR Maximum Continuous Thrust Multipurpose Control Display Units Minimum Equipment List Multifunction Display Multifunction Probe Main Landing Gear Maximum Landing Weight Maximum Operating Mach Multi-Mode Receiver ABB.3 List of Abbreviations • • • • • N • • • • O MSG MSL MTOW MTW MZFW Message Mean Sea Level Maximum Takeoff Weight Maximum Taxi Weight Maximum Zero Fuel Weight NAV NAVAID ND NLG Navigation (Radio) Navigation Aid Navigation Display Nose Landing Gear © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. • OIS • OMS • OMT Onboard Information System Onboard Maintenance System Onboard Maintenance Terminal P • • • • • • • Q • QRH R • • • • • • S • • • • • • PR1010081 A350 ↔ A330 Comparison pb PBE PFD PMAT PRIM Ps Pt Pushbutton Protective Breathing Equipment Primary Flight Display Portable Multipurpose Access Terminal Primary Flight Controls and Guidance Computer Static Pressure Total Pressure Quick Reference Handbook RA RAT RMP ROP ROW RWY Radio Altimeter/Altitude, Resolution Advisory Ram Air Turbine Radio Management Panel Runway Overrun Protection Runway Overrun Warning Runway SATCOM SD SEC SELCAL SFCC SFD Satellite Communication System Display Secondary Flight Controls Computer Selective Calling Slats/Flaps Control Computer Standby Flight Display ABB.4 List of Abbreviations • • • • • • © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. T • • • • • • • • • • • • • SND SQWK SSA STBY SURV sw Standby Navigation Display Squawk Side Slip Angle Standby Surveillance system Switch T/C T/D TAT TAWS TCAS TEMP TERR THR THS T.O TOM TOS TR Top of Climb Top of Descent Total Air Temperature Terrain Awareness and Warning System Traffic Collision Avoidance System Temperature Terrain Thrust Trimmable Horizontal Stabilizer Takeoff TakeOff Monitoring TakeOff Securing Transformer Rectifier V • • • • • • • • • • • V/S VD VDAR VENT VHF VLE VLO VLS VMO VOR VV W • WBM • WTB • WXR X • X-FEED • XFR Z • ZFWCG • ZFW PR1010081 A350 ↔ A330 Comparison Vertical Speed Vertical Display Virtual Digital ACMS Recorder Ventilation Very High Frequency Maximum Landing Gear Extended Speed Maximum Landing Gear Operating Speed Lowest Selectable Speed Maximum Operating Speed VHF Omnidirectional Range Velocity Vector Weight and Balance Manual Wing Tip Brakes Weather Radar Crossfeed Transfer Zero Fuel Weight Center of Gravity Zero Fuel Weight ABB.5 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Intentionally Left Blank PR1010081 A350 ↔ A330 Comparison ABB.6 This document and all information contained herein is the sole property of AIRBUS S.A.S. No intellectual property rights are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of AIRBUS S.A.S. This document and its content shall not be used for any purpose other than that for which it is supplied. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. The statements made herein do not constitute an offer. They are based on the mentioned assumptions and are expressed in good faith. Where the supporting grounds for these statements are not shown, AIRBUS S.A.S. will be pleased to explain the basis thereof. AN EADS COMPANY PR1010081 A350 ↔ A330 Comparison

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