A320 Neo Sharklet Entry Into Service (1)

December 24, 2017 | Author: bashirsba | Category: Airbus, Takeoff, Jet Aircraft, Aviation, Aerospace
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Sharklet structure of A320neo...

Description

Sharklet Entry Into Service Presented by

Jean-Paul POURTAU A320neo & Sharklets projects manager Customer Services - A320 Family Programme - SBS

A320 Family Regional Seminar

Content 1

Sharklet benefits

2

Technical & project highlights

3

Entry Into Service

4

Sharklet retrofit solutions

5

Summary

Page 2 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

A320 Family Regional Seminar

Firm orders for Sharklets so far

Orders from 28 customers worldwide Page 3 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

A320 Family Regional Seminar

Sharklets reduce fuel burn A320 Block fuel improvement vs. current Wingtip fences

4%

$150k fuel savings per year per aircraft

3%

Fuel burn reduction

$275k fuel savings per year per aircraft

Attractive savings

2%

1% 0

1000

2000

3000 Sector length (nm)

3.5% fuel burn savings on long sectors

Page 4 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

A320 Family Regional Seminar

Sharklets improve take-off performance • If facing obstacles or climb limitations, Sharklets will increase takeoff weight by:

• Improving second segment performance • Clearing more obstacles

Washington

Better take-off capability

Corfu Madeira

Kathmandu

Lanzarote

Quito

Canberra

Improved operational efficiency around the world

Page 5 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

A320 Family Regional Seminar

Sharklets reduce engine maintenance costs Reduce take-off thrust for same take-off weight

Up to 4% additional take-off derate Longer Time on Wing Engine DMC per FH - $

Reduced engine maintenance cost

up to 4% reduced thrust up to 2% lower cost Derate - %

Up to 2% reduction in engine maintenance costs thanks to improved take-off performance Page 6 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

Lower engine DMC

A320 Family Regional Seminar

Improved climb performance with Sharklets Altitude (ft) 40000

600nm

530nm

38000 36000 34000 32000 30000 Sector profile

Higher initial cruise altitude

Page 7 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

Higher optimum altitude

A320 Family Regional Seminar

Sharklets benefits summary Fuel burn reduction

Attractive savings

More efficient family

Lower CO2 emissions

More payload & range

Better take-off capability

Lower engine DMC

Higher optimum altitude

Sharklets increase A320 Family value Page 8 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

A320 Family Regional Seminar

Content 1

Sharklet

2

Technical & project highlights

3

Entry Into Service

4

Sharklet retrofit solutions

5

Summary

Page 9 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

A320 Family Regional Seminar

Sharklets design →Single piece design →Multi-lug and tension bolt →Innovative materials →Lightning strikes protection →New LED nav & strobe lights

Airbus design with state-of-the-art materials Page 10 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

A320 Family Regional Seminar

Sharklets design: new wing-sharklet join Rib 27 (wing-side) z y x

z y x

Rib 27A (sharklet-side)

Simple connection: tension bolts and barrel nuts; multi-lugs and pins Page 11 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

A320 Family Regional Seminar

Centre wing box changes Changes No changes Changes without assembly jigs modification

Minor design changes for adapted centre wing box reinforcement (A319/A320)

Page 12 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

A320 Family Regional Seminar

Wing changes (A320) Covers: Skin thickness increase outboard of Rib 11. Topskin material 7449 Bottomskin material 2024HDT. Strip milling introduced in change area.

Stringers: Increased height outboard of Rib 11. New btm material 2026.

Mid and Outer Rear Spars: Front spar Web thickness increase ~ 1mm outboard of Rib 9 Flange changes outboard of Rib 25 New crack stopper outboard rib 24

Fixed Trailing Edge: Aileron Hinge bracket changes

y Rib 11

x

Fixed Leading Edge: Bolting and rivet changes outboard of Slat 4

Rib 27: New large machined rib concept Introduction of support straps to stringers

Ribs 12 to 26: System penetrations maintained. Thicker web features and taller stringer cut outs. Larger cleats used to fit larger fasteners.

Front Spar: Front spar Web thickness increase ~1mm outboard of Rib 9 Flange changes outboard of Rib 23

Page 13 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

Systems Installation: New looms for Sharklet, routed outside rib 27. Centre Tank Vent Pipe Modified.

A320 Family Regional Seminar

Computers updated for Sharklet No sharklets capability - Std & P/N

Sharklets capability - Std & P/N

MOD

Certif

ELAC

B L94

3945128210 or 3945129104

B L96

3945128212 or 3945129106

160015/P121 27

Nov 2012

SEC

B’ 122

B372BBM0103

B’ 121

B372BBM0104

160014/P121 25

Nov 2012

FCDC

58

15370-1520

59

160051/P129 77

Oct 2012

FAC

B 620

B397BAM0620

B 622

B397BAM0622

160011/P121 26

Nov 2012

FWF

H2 F6

350E053021111

H2 F7

350E053021212

153741/P130 23

Dec2012

PDB TAV

G2831AAB03

G2831AAC01

160016/P121 28

Oct 2012

PDB HWL

PS4087592-902 or HNP53AD06-2002

PS4087592-903 or HNP53AD06-2003

160017/P121 29

Oct 2012

Software upgrade via software upload or OBRM Page 14 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

A320 Family Regional Seminar

Sharklet introduction – certification • The Sharklet is certified through a significant major change (classification according to EASA Part 21). The target date for the official approval is end of November 2012 for A320. • The sharklet doesn’t create any new model. For that reason, it remains as part of the existing EASA TC.

• Schedule

2011 1Q

2Q

3Q

4Q

2012 1Q

Page 15 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

2Q

3Q

4Q

2013 1Q

2Q

3Q

4Q

2014 1Q

2Q

3Q

4Q

A320 Family Regional Seminar

Sharklets and provisions ramp-up

Q2 2012

Q4 2012

Provisioned wings EIS Start of ramp-up

1st Sharklets certification, EIS and start of ramp-up

Q4 2013

Q1 2014

Provisioned Aircraft Sharklets available reach full production rate for all deliveries

2012

2013 Provisions ramp-up Sharklets ramp-up

From 2014, every A320 Family delivery can benefit from Sharklets Page 16 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

2014

A320 Family Regional Seminar

Content 1

Sharklet benefits

2

Technical & project highlights

3

Entry Into Service

4

Sharklet retrofit solutions

5

Summary

Page 17 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

A320 Family Regional Seminar

EIS preparation with Airlines • Dedicated communication to every Operator delivered with Sharklet







Maintenance • • • •

Technical Publications Ground Support Equipments Scheduled maintenance Structure Repair Manual (SRM)

Flight Ops & Training • • • • • •

Aircraft Flight Manual (AFM) & Flight Crew manuals (FCOM) Perfo databases Configuration Deviation List (CDL) Master Minimum Equipment List (MMEL) Weight & Balance Manual (WBM) Training

Others • • •

Spares support Transportation Supplier contract

→Provides detailed information → Allows tailored support to sharklet Operators → Very useful feedback gathered

EIS plan under deployment, reviewed with every sharklet Operator Page 18 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

A320 Family Regional Seminar

Tech Pubs • Minor adaptations for reinforced Aircraft and sharklet Aircraft • AMM • Removal / Installation tasks (sharklet, nav and strobe lights) • Trial performed on Aircraft (see dedicated slide) : AMM validated with minor adaptations •

needed. Sharklet removal / installation duration: around 6 h (excluding sealant curing time)

• Inspections for Schedule maintenance • No or minor update identified on Aircraft structure • New tasks for Rib 27 and sharklet inspections.

• Other minor adaptations

• TSM: no impact identified to this date • IPC: 80 items identified as modified further review on-going. • ASM / AWM: 6 items identified( ATA 33) on-going. Page 19 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

A320 Family Regional Seminar

GSE • 7 specific tools considered for Sharklet Removal / installation Hoist – Sharklet - 98D57356715 Extractor - Lower Pins - 98D57304000 Grid - Nut Torque - 98D57304001 Collar - Aileron - 98D27104005 Protector - Manhole - 98F57004049 Protector - Sharklet - 98D57304003 Torque Tool - TBC + Fuel LEL measuring device

Fuel LEL measuring tool* * Picture given as illustration only

• No specific tools needed for lights Page 20

GSE are planned available for loan and sales stock

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

A320 Family Regional Seminar

AMM & GSE on Aircraft validation • Maintenance trial performed 24-26 sept 2012 on Flight Test Aircraft

• Sh arklet Removal/Installation • Lights and PSU Removal/Installation → Final draft AMM and GSE final concept used

AMM & GSE validated with minor update needed (ongoing) Sharklet removal / installation in less than one shift Page 21 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

A320 Family Regional Seminar

Scheduled Maintenance • Reinforced a/c with WTF: no maintenance program change considered. • Sharklet Aircraft: preliminary assessment done • Minimum impact on existing inspection • update of interval / threshold • No new task except for sharklet

• New inspections on sharklet and RIB27 • RIB 27 lug inspection • Sharklet inspection (borescope) • Threshold/Interval considered: 12 YE / 12 YE

• MRBR/ALS part2 dossier under preparation for Certification • Reviewed during A318 / A319 / A320 / A321 STRUCTURE WORKING GROUP - SAFAM SWG MEETING 27

• 11th – 12th September 2012, Toulouse, France Page 22

Minimum impact is targeted for sharklet Aircraft

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

A320 Family Regional Seminar

SRM • Complete revalidation of existing SRM is ongoing for both reinforced Aircraft and Sharklet Aircraft

• Objective is to complete all SRM task revalidation by end 2013 • Outlook today indicated 65% temporary & ADL revalidated for Sharklet Aircraft A320 EIS: • Nose Fwd fuselage (s11/12), Fwd fuselage (s13/14), Aft fuselage (s18), Aft Tail cone (s19.1), PAX doors, landing gear doors, belly fairings, VTP,THS, rudder, elevator, pylons

• SRM introduction includes Aircraft reinforcement and sharklet modifications into repairs / ADL effectivity list.

• Repairs shown as not applicable would need RAS in case-by-case basis • Sharklet device ADL/Repairs on-going: • Metallic Leading Edge ADL (Scratches, Gouges, Abrasions, Corrosion and Dents) • Lightning Strike damage • Sharklet composite structure repairs

• Sharklet SRM coverage will be maintained vs current A320. Same level of reparability vs current A320 family Page 23 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

A320 Family Regional Seminar

Impact Flight Ops & Training Domain • AFM / FCOM: • To be updated to reflect Perfo improvements • Minor adaptation to reflect sharklet impact on systems

• WBM :

no change for A320 possible minor changes on Weight and CG data for A319 or A321

• MMEL: • Update of perfo charts • Possible update due to introduction of LAF (Load Alleviation Function)

• Maintenance & Flight training: Minor update

(mainly on Familiarization

training)

• No impact on crew qualification – same type rating Page 24 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

A320 Family Regional Seminar

Impact Flight Ops & Training Domain - dispatch • Dispatch after sharklet heavy damage (out of SRM and CDL scope) • Ferry Flight with damaged sharklet removed and replaced by a complete wingtip (modified wingtip compatible with reinforced wing). • Benefit: Wingtip & fence can be transported in A320 Family. Sharklet can’t. • Will be managed through AFM specific instructions. Targeted at 1Q13 • Perfo penalties under definition → Flight Tests to be completed by end Oct2012

• CDL : complete scope under review • Available at 1st EIS: static discharger. • Other CDL items under review: nav & strobe lights glazing's , PSU access door Page 25 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

A320 Family Regional Seminar

Flight Ops : performance tools update • Impact on performance applications • PEP •

[Performance Program] → new version 5.2.1 with new performance Database FlySmart with Airbus (former LPC NG) → new version L3.2 with new performance Database Pre-requisite: version L3.0 shall be already in service in the Airline

• Availability • PEP 5.2.1 and PAADMIN 7.1 • FlySmart with Airbus

20 Nov 2012 10 Dec 2012

• with same performance database as AFM / pending AFM approval A320 CFM (A320-216 & -214): A320 IAE (A320-232 & -233):

Page 26 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

30 Nov 2012 20 Dec 2012

A320 Family Regional Seminar

Spare & transportation • Spare sharklets • Two sets of sharklets planned to be available at EIS in Airbus to support the fleet. One set in Singapore and one in Hamburg at EIS.

• Out of production secured Parts that will be out of production after Aircraft reinforcement is standard in production have been identified and secured for aftermarket (Airbus Material, Logistics and Suppliers in Hamburg).

• Sharklet transportation • Airworthy box defined → (H)1186mm X (W)1722mm x (L)4572mm

• Fits in A330/A340 and cargo • Do not fit into A320 Family Aircraft Page 27 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

A320 Family Regional Seminar

Content 1

Sharklet benefits

2

Technical & project highlights

3

Entry Into Service

4

Sharklet retrofit solutions

5

Summary

Page 28 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

A320 Family Regional Seminar

Sharklets for the A320 Family Production line ‰New-build aircraft delivered with: • Modified structure (centre wing box and wing) • Required flight computers functionality • Sharklets

Production retrofit ‰New-build aircraft delivered with modified structure ‰To be retrofitted post-delivery: • Flight computers functionality • Sharklets

In-service retrofit ‰Retrofit: • Wing structure reinforcement • Sharklets • Flight computer functionality

Page 29 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

A320 Family Regional Seminar

Sharklet “production” retrofit: Airbus solution

Production retrofit availability target : H1 2013 Page 30 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

A320 Family Regional Seminar

Sharklet “in-service” retrofit: Airbus solution

In-service retrofit availability target : end 2013 Page 31 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

A320 Family Regional Seminar

Sharklet in-service retrofit Impact on the aircraft

9 Pre-requisites (flight computers): • FMGC • SEC • ELAC • FAC • FCDC • FWC

Embodiment time : 10 days Aircraft downtime : 15 days

Page 32 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

A320 Family Regional Seminar

Content 1

Sharklet benefits

2

Technical & project highlights

3

Entry Into Service

4

Sharklet retrofit solutions

5

Summary

Page 33 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

A320 Family Regional Seminar

Key messages

Q2 2012

Q4 2012

Provisioned wings EIS Start of ramp-up

1H2013

1st Sharklets certification, EIS and start of ramp-up

2012

2013 Provisions ramp-up Sharklets ramp-up EIS preparation with Airlines

Page 34

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

1Q2014

Retrofit solution for ProvisionedRetrofit solution for non Provisioned Aircraft Aircraft

2014

A320 Family Regional Seminar

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. 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. 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. AIRBUS, its logo, A300, A310, A318, A319, A320, A321, A330, A340, A350, A380, A400M are registered trademarks.

Page 35 © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

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