747-8 Airport Compatibility - North · PDF file747-8 Airport Compatibility ACI-NA Operations...

747-8 Airport CompatibilityACI-NA Operations and Technical Affairs Committee Meeting - Boston21 September 2008

Kaz KonyaBoeing Airport Technology Group

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.

COPYRIGHT © 2006 THE BOEING COMPANY

New wing design

Modern flight deck

Next-generation alloys

Intercontinental and Freighter: 5.6-m (18.3-ft) stretch

787 technologyengines

Innovative interior features

A new 747 that leverages 787 technologies

747-8 747-8FMTOW: 442,255 kg (975,000 lb) 442,255 kg (975,000 lb)

MLW: 309,350 kg (682,000 lb) 343,370 kg (757,000 lb)

MZFW: 291,205 kg (642,000 lb) 325,225 kg (717,000 lb)


747-8 vs. 747-400 Comparison

797-CO-0256 12/8/06-CF

747-8 (ft/m) 747-400 (ft/m)

Span 224.4/68.4 213.0/64.9

Length 250.2/76.3 231.8/70.7

Height 64.2/19.6 64.0/19.5

747-8747-400

747-85.7 ft (1.8 m)

wider each side747-8

0.2-ft (0.1 m) higher

747-818.4-ft (5.6 m) longer


Passenger Firm Config

On track for 2009 freighter and 2010 Intercontinental entry into service

Freighter delivery

Assembly

Roll out Airplane design

Design refinement

Customer discussions

Test and certification

Engine test

Intercontinental delivery

Programlaunch

Freighter Firm Config


12


105 Announced Orders

4

As of May 23, 2008

20

7

13 14

510

5

10

5

747-8 747-8F


Boeing Large Twin-Aisle Family

250

51 more seats

Three-classseating

350

747-400/-400ER416 seats

777-300/-300ER365 seats

777-200/-200ER/-200LR301 seats

747-8467 seats

450

787-9250–290 seats


• Revenue payload does not include tare weight.0

45(100)

136(300)

91(200)

747-8F

747-400BCF747-400F/-ERF

767-300F767-300BCF

767-200SF

757-200SF

737-700C

777 Freighter

Revenue payload 1,000-kg (1,000-lb)

MD-11BCF

16% increase

Extending the complete Boeing freighter family


The 220-in stretch offers 51 more seats and 26% additional cargo volume

747-8 Intercontinental467 passengers

+3 first

Wingbox

Wheelwell

+60 in(1.5 m)

26 first89 business352 economy

+9 business +39 economy

+2 Pallet +2 LD-1/3

+ 1.5 m(+60 in)

Additional seats and cargo

+80 in(2.0 m)

+ 4.1 m(+160 in)


16% more volume than the 747-400F 747-8 Freighter134 tonnes

Main deck

Forward lower hold Aft lower hold

Bulk513cu ft

692.7 m3

(24,462 ft3)

2,385 ft32,792 ft3 Bulk520 ft3

68.7 m3

(2,425 ft3)82.3 m3

(2,905 ft3)

(27) 96-in x 125-in x 10-ft contoured pallets [21.1 m3 (750 ft3)](5) 96-in x 125-in x 8-ft contoured pallets [17.4 m3 (613 ft3)](2) 96-in x 125-in x 8-ft contoured pallets [15.3 m3 + 17.2 m3 (540 + 607 ft3)](12) 96-in x 125-in contoured pallets [11.8 m3 (415 ft3)](2) LD-1/3 containers [5.0 m3 (175 ft3)]

* Excludes bulk cargo

Additional pallets and containers

Total volume* = 844 m3 (29,792 ft3)


The new wing design provides additional performance with lower noise

New advanced technology airfoils

New corrosion resistant flap tracks

New Improved rigging

New flap track carriages

New fly by wire Spoilers & Outboard

Ailerons

New Aileron droop

New efficient raked tip design

New double-slotted inboard and single slotted outboard flaps

New Krueger flaps with gapped configuration


Cleaner, quieter and more efficient16% reduction in carbon emissions52% below CAEP/6 limits for NOx30% smaller noise footprint16% more fuel efficient

Compared to 747-400, except for NOx


The 747-8 meets the latest emission standards

Cleaner

747 emissions

777-NO-2008 10/6/06 AS/GG

ICAO standards %

0

10

20

30

40

50

60

70

80

90

100

110

747-8 747-8 747-8 747-8

CAEP/6 limit (2008)

Hydrocarbons CarbonMonoxide

Smoke Nitrogenoxides

Nominal

NominalNominal

Nominal

• Applicable to 747-8 data, “nominal emissions expectation provided with no implied guarantee or commitment on the part of GEAE”


Getting quieter with each generation

Better

Noise margin, EPNdB

-30

-20

-10

0

747-200 747-400 747-8

Margin to Chapter 3 London departure/arrival

Noise level, EPNdB

90919293949596979899

100101102103

747-200

747-400

747-8 747-200

747-400

747-8

Departure

QC1

Better

QC2

QC4

QC8

QC16

Arrival


747-8 Airport Regulatory Activities

European airport operational plan – BACG

U.S. airports operational plan

Operations at other world regions

Wake vortex work


Large Aircraft in Operation

747-400Lockheed C5Antonov 124A380

747-8

Operations are allowed at Code E airports with certain operational mitigation measures to ensure safety

64.967.9

73.379.8

68.4

Wing span E 65m F 80m

Main gear outer wheel span 9m 14m 16mD / E F

747-400Lockheed C5Antonov 124A380

747-8

12.611.4

8.014.3

12.7


Operational Guidelines are Airplane-Specific

RWY - TWY separationTWY - TWY separationTWY - object separationTL - object separation

OFZILS critical area

RWY widthTWY widthU-turn widthTWY turn fillet

12.7m(41.7 ft)

19.6m(64.2 ft)

RWY shoulder widthTWY shoulder width

68.4m (224.4 ft)

41.7m (136.7 ft)

Critical airport dimensions will be driven by aircraft spans* and height- 747-8 has same dimensions as 747-400 except for minor wingspan

increaseA380 versus 747-8: Conclusions and recommendations will be different

* Wingspan, outer engine span and main landing gear span


Level of Acceptability –Example: Taxiway-to-Object Separation

17.5m

17.5m

<17.5m

57.5m

51.7m

< 51.7m

ICAO Code F standard• For new design/construction

Equivalent level of safety provided• No aeronautical (safety) study

required

ICAO recommends aeronautical study• Process permitted in Annex 14• BACG adopted 9.0 m

80 m span

747-8 (68.4 m span)

747-8 (68.4 m span)


Boeing 747-8 Airport Compatibility Group (BACG)

Operational guidelines were developed for member airportsMembers include German and French CAA, European airports, airlines, ACI, IATA, and BoeingExpect other CAAs to joinTwo meetings completed – March 2007, October 2007

Operational guidelines finalized and circulated for approval

Approval expected in late 2008


Example of BACG Output

ICAO standards and recommended practices (SARPS)

Annex 14Aerodrome Design Manuals, Part 1 and 2

Item Width of straight taxiway

Unless otherwise indicated, the requirements are applicable to all types of taxiways.A14 P3.9

Minimum clearance between outer main wheel and taxiway edge: 4.5m for both E and F[RP] A14 P3.9.3

Width of straight portion:- 23m for code letter E- 25m for code letter F[RP] A14 P3.9.5

Taxiway width = 2 x clearance distance from wheel to pavement edge + max wheel track

Code letter E: 23m = 2x4.5m+14m

Code letter F: 25m = 2x4.5m+16m

ADM pt2 p1.2.7+ table 1-1

Origin of the 4.5m clearance distance unknown

Minimum taxiway width of 23 meters (equal to Code letter E requirements)

Wheel-to-edge minimum clearance of 4.5m for Code letter E and F aircraft

Outer wheel span of 12.7m results in outer tire edge to pavement edge (for 23m taxiway) compliant with the ICAO requirement of 4.5m clearance

Various taxiway deviation studies conducted to date show that 4.5m clearance is adequate for safe taxiing

ICA

O S

AR

Psan

d A

DM

ICA

O ra

tiona

leB

AC

Gag

reem

ent

Just

ifica

tion

mat

eria

l

ICAO justification materialInformation and formula describing the SARPS

Justification materialInformation used to justify the proposed guidelines for the 747-8 operations

BACG AgreementProposal for 747-8 operations – Application of ICAO requirements to the 747-8 for infrastructure and operations that currently do not meet the Code Letter F specifications


Taxiway Separations –BACG Guidelines

ICAO Annex 14Volume 1

Separationdistancesbetween

(unit in meters)

Formula

Code E / F Provisional New F*

1 2 3 4 5 6 7TWY centerline and TWY centerline

Wing span+ wingtip clearance= TOTAL

65 / 8015 / 17.580 / 97.5

801595

651176

8011 91

68.411

79.4

TWY centerline and object

½ wing span+ wingtip clearance= TOTAL

32.5 / 4015 / 17.5

47.5 / 57.5

401555

32.59

41.5

409

49

34.29

43.2

Aircraft stand taxilane centerline and object

½ wing span+ wingtip clearance= TOTAL

32.5 / 4010 / 10.5

42.5 / 50.5

4010.550.5

32.57.540

407.5 47.5

34.27.5 41.7

ICAOEurope ANP

Doc 7754747-400

AACG

A380-800

BACG

747-8

* Provisional New Code F: Planned adoption by ICAO Council in March 2009

BACG agreement is compatible with Code E spec airports – Compare red numbers under columns 3 and 7

Document 7754 has provided a history of safe 747-400 operations


U.S. Airports Operational Plan747-8 is accommodated through Modification of Standard (MOS) process

Deviation from FAA Group VI standardsAirplane specific / airport specific

First 747-8 MOS meeting held in April 2008 in Washington DCFAA process/expectations describedAttended by 17 U.S. and Canadian airportsSecond meeting planned for 6 October 2008

45m wide runway operational approvalContinuing discussions with FAA to finalize the test plan

Engineering BriefsEB73 - Use of Group V (Code E) taxiway width approved for 747-8EB74 - Group VI runway width currently specified pending 45m (150’) wide runway approvalEB77 (draft) - Taxiway edge margin of 15 ft for Group VI airplanesEB78 (draft) - Taxiway separation criteria based on specific airplane wing span


Operational Plans for Other World Regions

Discussions under way with individual CAAs

CAAs being contacted by Boeing

Airports being contacted by airlines


747-8 Wake Vortex

A group comprising FAA, EASA, JAA, EUROCONTROL, and Boeing was formed in 2007 to recommend the wake vortex separation and associated safety requirements for the 747-8

Team structure (Steering Group / Working Group), membership and process is similar to that used for the A380

Recommendations to ICAO 3rd quarter 2009


Summary

747-8 is 747-400 with minor dimensional changes− Small wingspan increase of 3.5m (11.4 ft)− Outer main gear wheel span of 12.7m (41.7 ft) remains in Code D/E− Outer engine span remains same as 747-400 and blast contours

compatible with Code E (Group V) rwy and twy shoulder widths

747-8 can be accommodated at ICAO Code E / FAA Group V airports with minimum disruptions or modifications

Recent history of successful implementation of operational guidelines− Many years of safe 747-400 operations in Europe with ICAO Europe

(AOPG Document 7754) guidelines of reduced clearance taxiing

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