Presented by Dan Cohen-Nir, Programs Director Airbus Americas, Inc. ACI-NA Operations & Technical Affairs Committee March 5, 2013 St Petersburg, Florida
Airbus family key figures A320 family: A take-off or landing every 2.5 seconds, 7 billion passengers carried since first flight in 1988 1,734 neo orders A330 family: A take-off or landing every 25 seconds, More than 800 A330s sold since 787 launch A350 XWB: First Flight mid 2013 592 firm orders from 34 customers A380: Takes-off or lands about every 6 minutes 125 flights per day and 1.5 million passengers per month Page 2
March 5, 2013 A320 Family Recent Milestones Sharklet Retrofit Authorization to Offer in October Sharklet A320 with CFM engines certified in November Flight test results show better than expected fuel fuel-burn burn savings up to 4% 1st delivery with Sharklets to in December 2012 1st delivery with Sharklets to in February 2013 (110 airplane retrofit from 2014 approved in March 2013) Firm order for 130 A321neo by American Airlines R t 42 per month Rate th Production P d ti att all ll time ti high hi h Page 3
Sharklet General arrangement Sharklets 117 ft 5 in 8.0 ft Same for A319, A320 and A321 Page 4
Airport Categories and Indices (sharklet outfitting) A319 A320 A321 Wingspan 117 ft 5 in 35.80 m 117 ft 5 in 35.80 m 117 ft 5 in 35.80 m ICAO Code letter C C C FAA Airplane/Taxiway Design Groups 3/3 3/3 3/3 Overall Length 111 ft 0 in 33.84 m 123 ft 3 in 37.57 m 146 ft 0 in 44.51 m RFF Category (ICAO) 6 6 7 ARFF Index (FAA) B B C Page 5
A321 door L2 vs. engine nacelle locations 45 ft 5 in (13,84 m) Nose to center of free aisle 50 ft 6 in (15.39 m) Nose to engine nacelle front Page 6
A321neo Airbus Cabin-Flex Option Option to add an additional overwing exit Option to de-activate door 2* Door 3 moved back by 4 frames * In combination with additional overwing exit Page 7
HT T T March 5, 2013 A321neo Option 2b: High Density single-class layout Basic floor plan: 220 seats (max exit) Cabin-Flex + Space-Flex: 236 seats A A A A A A A Page 8
A320 Family continuous innovation Sharklets Universal IFE Space-Flex platform Landing Gear Fuel pumps New APU BTV* Maintenance programme 2012 2013 2014 2015 2016 2017 EFB OANS ROPS Full LED etaxi* Cabin-Flex Improved Reduced Reduced Improved comfort fuel burn DMC capability Improved navigation Page 9 ROPS: Runway End Overrun Protection / OANS: On-board Airport Navigation System *Project study
A350 XWB Design and Commercial Updates Page 10
Electrical design Aux Gen L Aux Gen R RAT AC Start Gen R1 AC Start Gen R2 RA GNR R APB WIPS RT Bkup Bus TRU 28 Vdc C2-TRU P600 ELCU R BTB RdcT ELCU MN Bat To CRN R APU SC RCB R TRU Rly ELCU HBB 28 Vdc HBB R-TRU E- BPSU P200 R1 BTB BB ISO Rly +-130 Vdc +-130 Vdc R28Vd Vdc F/O Instr Bus E- BPSU R1 GCB R1 GNR R2 GNR To CRN R2 GCB R1 SC 235 Vac Bus R1 235 Vac Bus R2 R3 BTB WIPS R BB R2 R1 ATRUC R2 Rly R2 ATUC ATRUC ELCU ELCU BTB ELCU 230/ 115 ATU R 115 Vac R BSB ELCU R EPC P400 R EP R1 CC CAC R1 Inboard ATRU BC ELCU P49 Hot BB SPUC APU SPU Bat To CRN P800/E6 R1 +/-270 Vdc Hyd C2 L2RFCR RF MC Ram Fan RFCR R2RFC SPUB R2 CC ATRU R2 +/-270 Vdc CNGC NGC OJ MC HNGC R2 SC R2 HD CAC Hyd R2 NGS L Outboard Installed power: 550 kva 3 Electrical Networks 115 V AC 230 V AC 28 V DC Nickel-Cadmium batteries in flight test and development phases Design flexibility for Li-Ion battery installation Simple architecture, thanks to the use of bleed air Page 11
Airplane Dimensions Code E / ADG-V design Span 212 5 64.75m Fuselage Length 237 1 72.25m Height 56 0.3 17.08m Fuselage height 239 6.09m Fuselage width (constant part) 234 5.96m A350-1000 Span 212 5 64.75m Fuselage Length 214 1 65.26m Height 55 11 17.05m A350-900 Fuselage height 239 6.09m Fuselage width (constant part) 234 5.96m Span 212 5 64.75m Fuselage Length 193 3 58.91m Height 55 11 17.05m A350-800 Fuselage height 239 6.09m Fuselage width (constant part) 234 5.96m Page 12
Airplane Pavement Loading A350 XWB Airplane Classification Numbers Flexible Pavement Rigid id Pavement High Medium Low Very High Medium Low Ultra Low Low A B C D A B C D A350-800 63 66 75 103 60 66 77 90 A350-900 66 70 80 110 64 71 83 96 A350-1000 56 62 76 105 57 73 93 112 Assumptions A350-800 A350-900 A350-1000 Max Ramp Weight [kg] 259,900 268,900 308,900 Max Take-Off Weight [kg] 259,000 268,000 308,000 Max aft Center of Gravity % 35 33 34 Loaded Tire Pressure kpa 1,590 1,660 1,500 Page 13
A350 XWB margins to Chapter / Stage 5 limits EPNdB margin Cumulative flyover, sideline and approach noise margins to Chapter or Stage 5 Subject to certification Assumption: CAEP recommended stringency levels at - 7 db vs. Chapter 4 All A350s XWB will be compliant with future regulation Subject to certification Page 14
The A380 commercial figures 262 firm orders 99 deliveries 163 order backlog As of March 1 st, 2013 Page 15
A380 the airline flagship 19 A380 31 A380 12 A380 10 A380 6 A380 8 A380 5 A380 5 A380 3 A380 99 A380s delivered to 9 operators In-service fleet as of March 1 st, 2013 Page 16
A380 December 2012 Tour Enthusiastic response Page 17
The A380 network as of March 1 st,2013 65 routes - 31 airports March 5, 2013 London Amsterdam Moscow Manchester Frankfurt Toronto Paris Munich Zurich Rome New York Washington DC Houston Miami Jeddah Dubai Guangzhou Kuala Lumpur Singapore Beijing Seoul Bangkok Shanghai Hong Kong Tokyo San Francisco Los Angeles Johannesburg Sydney Singapore Airlines Emirates Airline Qantas Airways Air France Lufthansa Korean Air China Southern Malaysia Airlines Thai Airways Melbourne Auckland Additional airline-announced / seasonal routes for 2013 shown dotted Page 18
New A380-designed terminals coming on line Airports welcome the A380 and plan around it Page 19
How to get more information from Airbus March 5, 2013 Visit us on line at www.airbus.com/support/airport-operations/ A full range of documentation including airplane characteristic for airport planning manuals, airplane rescue and firefighting charts, pavement load bearing publications, simplified AutoCAD drawings (including A350-900) and general information documentation Email Airbus Front Desk: airport.compatibility@airbus.com For airport-specific compatibility studies on the full range of Airbus airplanes (civil and military) Contact Airbus Americas Inc. D C h Ni Dan Cohen-Nir Phone: 1 202-331-2235 dan.cohennir@airbus.com Page 20
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