747-8 Airport Compatibility ACI-NA

Transcription

1 747-8 Airport Compatibility ACI-NA April 7, 2010 Karen Dix-Colony Airport Technology Proprietary: The information contained herein is proprietary to The Boeing Company and shall not be reproduced or disclosed in whole or in part or used for any reason except when such user possesses direct, written authorization from The Boeing Company. The statements contained herein are based on good faith assumptions and provided for general information purposes only. These statements do not constitute an offer, promise, warranty or guarantee of performance. Actual results may vary depending on certain events or conditions. This document should not be used or relied upon for any purpose other than that intended by Boeing.

2 Agenda Introduction to Airport Plan Airplane Configuration Engine Exhaust Velocities Ground Maneuvering Boeing Support to US Airports Questions

3 Leveraging the latest technology Intercontinental and Freighter: 5.6-m (18.3-ft) stretch New wing design 787 Technology engines Innovative interior features Updated systems Feature-rich baseline Modern flight deck Next-generation alloys & materials COPYRIGHT 2006 THE BOEING COMPANY 3

4 Cleaner, quieter and more efficient 16% reduction in carbon emissions 52% below CAEP/6 limits for NOx 30% smaller noise footprint 16% more fuel efficient

5 Quiet for Communities 30% smaller noise footprint over the dba Takeoff noise contours MTOW Mission ,000 lbs ,000 lbs ,000 lbs SEA _033-1

6 747-8 program schedule Program Launch Freighter Firm Configuration Intercontinental Firm Configuration 747-8F Start of Major Assembly 747-8F First Flight 747-8F Enters Service Enters Service

7 108 Announced Orders As of February COPYRIGHT 2006 THE BOEING COMPANY COPYRIGHT 2006 THE BOEING COMPANY

8 Airport Plan World Airports

9 Airport Compatibility Strategy Boeing To build on existing relationships through Industry and Regulatory contacts AIRPORT COMPATIBILITY Airlines To build on existing relationships at the airports with station managers and handling agents

10 US Airports - Destinations and Alternates

11 Boeing Airport Compatibility Commitment US Destination Airports Priority IATA ICAO MOS BOEING AIRLINES Airport City Approved Preparing Submitted Regulatory Pavement Parking 0 ATL KATL X Hartsfield - Jackson Atlanta I Atlanta 0 IAH KIAH George Bush Intercontinental/H Houston 0 ORD KORD X Chicago-O'Hare Intl Chicago 1 ANC PANC X Stevens Anchorage Intl Anchorage 1 DFW KDFW X Dallas-Ft Worth Intl Dallas/Fort Worth 1 IND KIND Indianapolis Intl Indianapolis 1 JFK KJFK X Kennedy Intl New York 1 LAX KLAX X Los Angeles Intl Los Angeles 1 MIA KMIA X Miami Intl Miami 1 SEA KSEA X Seattle-Tacoma Intl Seattle 1 SFO KSFO X San Francisco Intl San Francisco 2 DOV KDOV X Dover Afb Dover-Cheswold Dover AFB 2 HNL PHNL Honolulu Intl Honolulu 2 HSV KHSV X Huntsville Intl-Jones Huntsville 2 PDX KPDX Portland Intl Portland 2 SUU KSUU X Travis Afb Fairfield 2 TOL KTOL Toledo Express Toledo 2 WRI KWRI X Mc Guire Afb Fort Dix 3 CHS KCHS X Charleston Afb/Intl Charleston 3 RFD KRFD Chicago/Rockford Intl Chicago 3 SDF KSDF Louisville Intl-Standiford Louisville 4 BGR KBGR X Bangor Intl Bangor 4 BOS KBOS Logan Intl Boston 4 CLT KCLT Charlotte/Douglas Intl Charlotte 4 DEN KDEN Denver Intl Denver 4 DTW KDTW Detroit Metro Wayne Co Detroit 4 EWR KEWR X Newark Liberty Intl New York 4 IAD KIAD X Washington Dulles Intl Washington 4 MCO KMCO Orlando Intl Orlando 4 PHL KPHL Philadelphia Intl Philadelphia Notes Airlines Desire Approval ASAP Approval Required by 12/2010 Approval Required by 12/2011

12 747-8 Airplane Configuration

13 747-8 Intercontinental General Arrangement 224 ft 5 in (68.4 m) 73 ft 9 in (22.5 m) 160 in (4.1 m) 60 in (1.5 m) 64 ft 2 in (19.6 m) 12 ft 7 in (3.8 m) 36 ft 1 in (11.0 m) 25 ft 5 in (7.7 m) 97 ft 4 in (29.7 m) 243 ft 6 in (74.2 m) 10 ft 1 in (3.1 m) 250 ft 2 in (76.3 m)

14 747-8 Freighter General Arrangement 224 ft 5 in (68.4 m) 73 ft 9 in (22.5 m) 160 in (4.1 m) 60 in (1.5 m) 64 ft 2 in (19.6 m) 12 ft 7 in (3.8 m) 36 ft 1 in (11.0 m) 25 ft 5 in (7.7 m) 97 ft 4 in (29.7 m) 243 ft 6 in (74.2 m) 10 ft 1 in (3.1 m) 250 ft 2 in (76.3 m)

15 747-8 vs Comparison (ft/m) (ft/m) Span 224.4/ /64.9 Length 250.2/ /70.7 Height 64.2/ / ft (0.1 m) higher ft (1.8 m) wider each side ft (5.6 m) longer

16 747-8 Intercontinental General Characteristics CHARACTERISTICS UNITS ER MAX DESIGN POUNDS 878, , ,000 TAXI WEIGHT KILOGRAMS 398, , ,613 MAX DESIGN POUNDS 875, , ,000 TAKEOFF WEIGHT KILOGRAMS 396, , ,253 MAX DESIGN POUNDS 652, ,000 / 652,000 (2) 682,000 LANDING WEIGHT KILOGRAMS 295, ,537 / 295, ,350 MAX DESIGN ZERO POUNDS 555, ,000 / 555,000 (2) 642,000 FUEL WEIGHT KILOGRAMS 251, ,847 / 251, ,206 MAX STRUCTURAL POUNDS 156, ,700 / 148,100 (2) 169,100 PAYLOAD KILOGRAMS 70,851 62,006 / 67,177 76,702 SEATING THREE-CLASS CAPACITY 23FC + 80 BC EC 23FC + 80 BC EC 25 FC + 89 BC EC MAX CARGO 30 LD-1 OR 5 96" PALLETS + 14 LD-1 1 BODY TANK + 28 LD-1 OR 4 96" PALLETS + 14 LD1 OR 2 BODY TANKS + 24 LD-1 38 LD-1 OR 7 96" PALLETS + 16 LD-1 MAXIMUM FUEL US GALLONS 57,065 (1) 60,305 (2) / 63,545 (2) (1) CAPACITY LITERS 216, ,279 / 240, ,411 NOTES: (1) INCLUDES TAIL FUEL, GE ENGINES (2) BASIC (1 AUX TANK) / MAX (2 AUX TANKS)

17 747-8 Freighter General Characteristics CHARACTERISTICS UNITS F ERF MAX DESIGN POUNDS 878, , ,000 TAXI WEIGHT KILOGRAMS 398, , ,613 MAX DESIGN POUNDS 875, , ,000 TAKEOFF WEIGHT KILOGRAMS 396, , ,253 MAX DESIGN POUNDS 652,000 (1) 653,000 (1) 759,000 LANDING WEIGHT KILOGRAMS 295, , ,277 MAX DESIGN ZERO POUNDS 610,000 (2) 611,000 (2) 719,000 FUEL WEIGHT KILOGRAMS 276, , ,133 MAX STRUCTURAL POUNDS 248, ,600 (3) 295,200 PAYLOAD KILOGRAMS 112, , ,900 MAX CARGO CUBIC FEET 27,467 27,467 29,805 CUBIC METERS (4) MAXIMUM FUEL US GALLONS 53,765 53,765 60,210 CAPACITY LITERS 203, , ,920 NOTES: (1) OPTION FOR 666,000 LB (302,093 KG) (2) OPTION FOR 635,000 (288,031 KG) ONLY WITH 811,000 (367,863 KG) MTOW (3) OPTION FOR 272,600 LB (123,649 KG) ONLY WITH 811,000 LB (367,863 KG) MTOW (4) EXCLUDES BULK CARGO 797-CO CF

18 747-8 Airport Compatibility Large Airplane Comparison Critical model shown in red ER ER A A Wingspan 224.4ft (68.4 m) ft (64.9 m) ft (64.8 m) ft (63.4 m) ft (79.8 m) Length ft (76.3 m) ft (70.7 m) ft (73.9 m) ft (75.4 m) ft (72.7 m) Tail height (max) 64.2 ft (19.6 m) 64.0 ft (19.5 m) 61.4 ft (18.7 m) 58.7 ft (17.9 m) 80.2 ft (24.4 m) Wheelbase (to turning centroid) 92.3 ft (28.1 m) 79.1 ft (24.1 m) ft (30.6 m) ft (33.2 m) 97.8 ft (29.8 m) Cockpit-to-main gear ft (30.5 m) 86.6 ft (26.4 m) ft (34.2 m) ft (37.4 m) ft (31.9 m) Main gear span (to outer tire edges) 41.7 ft (12.7 m) 41.3 ft (12.6 m) 42.3 ft (12.9 m) 41.3 ft (12.6 m) 46.9 ft (14.3 m) Outer engine span ft (41.7 m) ft (41.7 m) 63.0 ft (19.2 m) ft (38.5 m) ft (51.4 m) Wingtip height (min) 19.7 ft (est) (6.0 m) 16.7 ft (5.1 m) 23.6 ft (7.2 m) 19.4 ft (5.9 m) 17.1 ft (5.2 m) Max taxi weight 978,000 lb (443,610 kg) 913,000 lb (414,130 kg) 777,000 lb (352,440 kg) 840,400 lb (381,200 kg) 1,258,000 lb (571,000 kg)

19 747-8 ACN (Aircraft Classification Number) Flexible Pavement

20 747-8 ACN (Aircraft Classification Number) Rigid Pavement

21 ACN Competitive Comparison ACN 90 Pavement loading is similar to today s widebody airplane fleet Boeing will work with the airlines and airports to resolve potential pavement loading concerns FB RB ,600 kg 978,000 lb F 348,700 kg 768,800 lb ER 352,400 kg 777,000 lb ER 414,130 kg 913,000 lb Maximum ramp weight Flexible pavement ACN's are based on Alpha Factors approved by ICAO in October 2007 A ,000 kg 1,239,000 lb A ,200 kg 840,400 lb

22 ACN / PCN Method What is ACN/PCN? ACN (Aircraft Classification Number) describes the relative load intensity of an airplane s main landing gear. ACN was adopted by ICAO and member nations as the official method for reporting a relative comparison of airplane loading intensity and replaces all previous methods by which manufacturers report aircraft loading characteristics. PCN (Pavement Classification Number) describes the actual load-carrying capacity of an airport runway, taxiway or ramp. PCN was adopted by ICAO and member nations as the official method for reporting airport pavement strength. PCN is not pavement design. PCN Rating Number 2 types of Pavement ACN 72RBWT 2 types of basis for evaluation 4 strengths of soil support 4 tire pressure ranges ACN PCN means Unrestricted MTOW

23 ACN / PCN Method (cont) ACN s are determined by airplane manufacturers: - Published in Airplane Characteristics for Airport Planning documents. - Also shown in ICAO Annex 14 and Jeppesen. PCN s are established by the airport authorities of the various nations: - Published in the Aeronautical Information Publications (AIP) - US airports publish in the Airport Master Record FAA Form Also shown in the Jeppesen Airport Directory. - Airports are the only authority to allow or disallow aircraft usage of the pavement. Comparing ACN to PCN allows for a more accurate determination of pavement capability Many airlines will only use PUBLISHED pavement ratings or official letter from airport when determining airport compatibility.

24 ACN / PCN Method (cont) Boeing will assist you in your PCN analysis

25 Engine Exhaust Velocities

26 Exhaust Wake Velocity Contours Runway and taxiway shoulder widths relate to engine jet blast* Same outer engine span as Same breakaway velocity contour width as ER (applies to TWY shoulders) Slightly wider takeoff velocity contour than ER but within Group V runway shoulders outer engine height above ground at center of thrust is slightly higher (0.9 ft, 0.3m) than * 35 mph (56 km/hr) velocity contour is used for shoulder design purpose

27 747-8 Engine Height Above Ground Outboard Engines 52 in / 132 cm to 67 in / 171 cm 52 in / 132 cm to 67 in / 171 cm Inboard Engines 24 in / 60 cm to 32 in / 80 cm 28 in / 71 cm to 36 in / 91 cm

28 Exhaust Velocity Contours at Breakaway Thrust is Same Width as ER m ft mph (120 km/h) 50 mph (80 km/h) 35 mph (56 km/h) Distance from A/P center line mph (120 km/h) 50 mph (80 km/h) 35 mph (56 km/h) ~ 25 (~ 7.6 m) Sea level, standard day Static A/P No wind All engines running Level tarmac ft m A/P Tail Distance downstream of engine nozzle exit

29 Takeoff Thrust Exhaust Velocity Contour widths are Within Group V Shoulder Width m ft mph (80 km/h) 75 mph (120 km/h) 50mph (80 km/h) 35 mph (56 km/h) Distance from A/P center line Sea level, standard day Static A/P No wind All engines running m Distance downstream of engine nozzle exit ft

30 Ground Maneuvering

31 747-8 Footprint Fits Inside Footprint ft (12.7 m) ft (12.6 m) ft (12.9 m) ft (24.1m) ft (28.1m) ft (30.6 m) Wheelbase dimension represent distance from nose to effective turn center

32 Same Proven Steering System as Existing 747s has the same body gear steering systems as today s 747 s Max 70 deg Body gear angle (deg) Gear nearest turn center Gear furthest from turn center Nose gear Nose gear angle (deg) Nose gear Body gear 0 to 20 degrees 0 20 to 70 degrees 0 to 13 degrees Wing gear Body gear Turn center Max 13 deg

33 747-8 Fillet Requirement taxiway turn fillet requirement is less demanding than the ER and A Cockpit over taxiway centerline Model ADG Tire edge to turn center A V 88 ft V 92 ft MD-11 IV 100 ft VI 100 ft DC-10 IV 103 ft V 106 ft More demanding than 747-8

34 747-8 Can Operate on Group V Fillet with Adequate Clearance FAA Lead-in to Fillet FAA Lead-in to Fillet Outside Edge of Wing Gear Paths

35 U-Turn Width Requirement o turn requirement is less demanding than the ER and A Minimum width of pavement ER A A FAA Airplane Design Group V VI V V VI Maximum steering angle, no differential braking 154 ft (47 m) 172 ft (52 m) 185 ft (57 m) 186 ft (57 m) 216 ft (66 m) U-turn width required can be reduced by using differential braking and/or asymmetrical thrust Widths do not take into account tire-edge clearance of 15 ft (4.5m) at both pavement edges

36 Existing 747 GSEs Are Compatible for Servicing Not impacted: Air conditioning Cargo loading Crew stairs Electrical power Engine start Fuel servicing Lavatory waste Potable water Galley trucks Cabin cleaning truck Jetbridges Impacted: Tow trucks Relative to

37 747-8 Intercontinental Ground Servicing Galley truck Lower lobe loader Container train Galley truck Hydrant fuel truck Potable water truck Container train Lower lobe loader Belt loader Baggage train Tow tug Galley truck Cabin cleaning Lavatory truck servicing truck Hydrant fuel truck Pneumatic power, air conditioning or ground electrical power is supplied by the airplane APU 797-AO CF

38 747-8 Freighter Ground Servicing Lower lobe loader Belt loader Lower lobe loader Main deck loader Water servicing truck Potable water truck Passenger stairs Main deck loader Hydrant fuel truck Air conditioning, pneumatic power and electrical power is supplied by the airplane APU 797-AO CF

39 Summary The is a derivative with a slight increase in wingspan The performs the same as or better the : Runway operating characteristics are same as or better than the Taxiing characteristics are very similar to current 747 s Boeing will provide technical support during your MOS development: Probability data of 747 taxi lateral deviation Specific aircraft performance data for runway and taxiway operations OFZ-related aircraft performance data

40 How Can Boeing Support Preparing for the At Your Airport?

41 MOS is Airplane-Specific Critical airport dimensions will be driven by aircraft spans* and height has same dimensions as except for minor wingspan increase A380 versus 747-8: Conclusions and recommendations will be different ft 68.4m (224.4 ft) 19.6m 64.2 ft (64.2 ft) RWY - TWY separation TWY - TWY separation TWY - object separation TL - object separation OFZ ILS critical area 12.7m 41.7 ft (41.7 ft) 41.7m (136.7 ft ft) RWY width TWY width U-turn width TWY turn fillet RWY shoulder width TWY shoulder width A380 * Wingspan, outer engine span and main landing gear span

42 Acceptability Level of Safety Example: Taxiway-to-Object Separation Group VI Span 262 ft 193 ft 62 ft FAA Group VI standard For new design/construction span ft 167 ft 55 ft EB 78 Provides same level of safety as design standard MOS approved at ADO level span ft < 167 ft <55 ft Perform safety study Statistics from taxiway deviation study can be used as justification Mitigation measures may be required MOS required, approval beyond ADO

43 747-8 FAA OFZ Compatibility OFZ (Obstacle Free Zone) U-shaped trough of obstacle free airspace centered along the runway for balked landing protection. OFZ increases in size with increase from wingspan and/or tail height. FAA is reviewing OFZ requirements Little or no impact expected for at 747 airports Runway Centerline 402 ft (120m) (Calculation is based on current FAA formula at sea level) Taxiway Centerline

44 Boeing Support to MOS Development Probability Statistics Example Background: Taxiway B is an ADG V taxiway. Taxilane W is designed for aircraft with a 125 ft wingspan (B ) or less. There is 219 ft between the centerlines of taxiway B and taxilane W. Having a B747-8 on taxiway B and a B on taxilane W would provide for 44.3 ft. between aircraft wingtips Standard/Requirement: Table 4-3. Wingtip Clearance Standards. Table 4-3 states that ADG VI taxiways shall have 62 ft. of wingtip clearance.

45 Boeing Support to MOS Development Probability Statistics Example...the risk of a B747-8 deviating from the taxiway centerline enough to impact a B on taxilane W... B on taxilane W is e-15, with a 95% confidence upper bound of e-14.

46 Unique Compatibility Requirements 180 o Turn (Not Required for MOS) Geometric U-Turn capability (no pilot technique) MTW and max aft cg

47 ACAP Airplane Characteristics for Airport Planners Preliminary ACAP currently available; Final ACAP available January

48 QUESTIONS?

49 Back-up

50 747-8 Intercontinental Door Locations 31 ft 2 in (9.5 m) 75 ft 0 in (22.9 m) 113 ft 9 in (34.7 m) 152 ft 0 in (46.3 m) 199 ft 4 in (60.7 m)

51 Improved Situation Awareness in Flight Deck Taxi-map (option) Global navigation satellite landing system (GLS) (new) less noise (signal interference) than ILS Navigation performance scales (NPS) (new) more accurate flight path information supporting required navigation performance (RNP) based arrival and departure procedures, better situation awareness Vertical situation display (VSD) (new) improves vertical awareness; path prediction relative to the ground; airplane shown in a vertical profile Integrated approach navigation (IAN) (new) ILS-like deviation alerts, same procedure for all approaches Tire pressure monitoring system (basic on -8; option on -400) reliability improved over the years Brake temperature monitoring system (basic since -400)

52 Low Speed Flying Characteristics Will be the Same as the Lateral handling qualities are anticipated to be the same as, or better than, those of the current 747 models retains Code E aircraft maneuverability The following are design improvements and new features for the Increased outboard aileron deflection to -30 (-25 on -400) Outboard aileron is more effective Use of spoilers 6 and 7 for lateral control Improves roll response rate and control FBW aileron and spoilers Allows tuning of roll control Increased spoiler effectiveness due to aft loading, flaps up and down Improves roll response Double-hinged lower rudder and spudders Improved directional control 60 ground spoilers improve braking, landing field length, and rejected takeoff performance (45 on -400) Drooped ailerons Improved takeoff and landing performance Revised rudder mechanism Eliminates exposure to single failure rudder hardovers

53 747-8 Landing Gear Footprint 10 ft 1 in (3.07 m) 92 ft 3 in (28.13 m)* 41 ft 9 in* (12.73 m) 36 ft 1 in (11.00 m) 12 ft 7 in (3.84 m) 36 in (0.91 m) CHARACTERISTICS UNITS MAX DESIGN POUNDS 877, ,000 TAXI WEIGHT KILOGRAMS 397, ,614 NOSE GEAR TIRE SIZE IN. 49x17, 32 PR * 50x20R22/26PR NOSE GEAR TIRE PSI 200 * 166 PRESSURE KG/CM * MAIN GEAR TIRE SIZE IN. H49x PR 52x21R22/36PR MAIN GEAR TIRE PSI PRESSURE KG/CM in* (1.44 m) typ in* (1.19 m) typ. * /-400ER have 41 ft 5 in (12.62 m) outer wheel span 78 ft 11.5 in (24.07 m) wheelbase 58 in x 44 in (1.47 m x 1.12 m) truck size