STUDY of STUDY of SEAT ASSEMBLYSEAT ASSEMBLYB/E is the world's largest manufacturer of commercial and general aviation aircraft seats. Our global network of four seat manufacturing plants and two Dynamic Test Facilities gives B/E the capacity and flexibility to produce over 200,000 seats per year, equaling more than 50% of the world's total annual requirements. With an installed base of more than one million seats currently in service, and more manufacturing capacity in place than the rest of the industry combined.

14 AUG 2008

Index

000 Introduction001 SEAT INSTALLATION AREAS BASELINE 1a002 Ergonomics

a) Seat Utilization / Seat Mission 003 Design considerations004 General Design Parameters

a) Static and Dynamic Strengthb) Fatigue / Abusec) Safetyd) Comforte) Durabilityf) Maintainabilityg) Styling

005 Family of Seats Catalog Options006 Family of Seats007 Seat Type Dimensions

a) Standard Triple008 Seat Items and Location

009 SEAT DEFINITIONa) Seat Frame b) Leg restc) Armrestd) Headrest

010 Food Tray011 Special Seat Features012 EPML Installation013 SEB Installation (One drawing for each IFE supplier)014 AIRBUS INDUSTRY .

a) A 380 SUPPLIER STANDARD SEAT FEATURES

015 Center Console / Endbays a) Center Console Armrestb) Cocktail Traysc) Endbays

016 Backrest017 Placards018 Seat Covers and Upholstery

a) Upholstery Styles019 Safety Belts020 IFE Equipment

a) Audio IFE021 PC Power Port

a) PC Power and USB Portsb) Under seat Electronics Box (UEB)

022 Mechanical Controla) Seat Actuator Power Distribution

023 Trim and Finish 024 Composites Serve as Primary Structural Material025 Premium Class Product DEFINITION026 Minimum Catalog Qualification Requirements027 WINSTON SALEM 14 DIGIT PART NUMBER028 Main Cabin & Regional Existing Product Family 029 Premium Seating Lead Customers! 030 Premium Class Seating Solutions for All Pitches031 Minipod Lie Flat Customers032 Spectrum Installed Customer Base 033 THE END

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SEAT INSTALLATION AREAS BASELINE 1a

UPPER DECK

MAIN DECK

B/E considers thoroughly the optimal comfort levels for seating and full flat positions for a long haul flight. The seat shall be designed to fully accommodate an anthropometric range from the 50th percentile female to the 95th percentile male. design with a thorough ergonomic study including both empirical and scientific evaluations in detail in order to meet Air liners specific requirements.

ErgonomicsSeat Utilization / Seat Mission

All passengers enjoy greater privacy with a wrap-around shell and less exposed ottoman. The addition of an infinite position, manually deploying aisle arm provides increased privacy in bed mode, or additional sleeping width if desired by the passenger.

Aspects for design considerations

1. Privacy

Comfort is enhanced with the addition of several key features including: Premium Lounge position Greater bed lengthPatented Crystal Flex back diaphragm system for optimum support and best-in-class thermal comfort.Infinite-position arm height adjustment including a full-down position that significantly increases the bed width.Proven ergonomics.

2. Comfort

Substantial improvements in personal stowage are a hallmark of the B/E proposal. Improvements include stowage design space customizable. (e.g. amenities, literature, headsets, and water bottle).

3. Personal Stowage

A large (~11 x 20) meal table provides a rigid dining or work surface. The meal table adjusts fore and aft. Meal table is machined with laminated inserts.

Seat width (hip width) has been increased to 22 for all pax. Seat width can be further increased to 28 by adjusting the manually deployable armrest.

5.Seat Width

4. Meal Table

The Business Class seat will be certified for installation into the referenced aircraft. B/E will take responsibility to have Boeing approve the interface loads report.

Static and Dynamic StrengthThe Business Class seat meets or exceeds the following load requirements. In addition to aircraft in-flight loads and regulatory requirements:

STATIC:

Forward (static) 9.0gDown (static) 8.6gUp (static) 5.4gSide (static) 4.0gAft (static) 1.5g

250 lbsImpact (cart) loadEnd-bay Bumper 300 lbsFwd/Aft (in the extended position)Headrest150 lbsDown (evenly distributed over upper surface)Tray Tables300 lbsDownArmrests200 lbsAftSeat Backs

Ultimate LoadLoad directionComponent

General Design Parameters

DYNAMIC:

All testing will be conducted in accordance with an approved Dynamic Test Plan and data acquisition as per SAE J2111.All data presented in this report demonstrates compliance with the requirements of TSO-C127a.

14.0gVertical (60 degree)16.0gHorizontal

Inertial Load

Inertial Load DirectionIFE Functional Testing:

The finished seats will require function tests of IFE using test equipment provided by the IFE supplier.

50000Extension CycleLeg rest

50000@200lbsDownBottom Supports

50000@100lbsDown/Side (45 degree angle)Armrests300000@200lbsDown (uniformly distributed)Seat Bottom Cushions50000@25lbsMechanism Cycle

50000@150lbsDownIn-Arm Tray Tables

50000@25lbsMechanism Cycle

50000@150lbsDownSeat Back Tray Tables

100000@100lbsAft Assist (top corners of back)Backs

Fatigue / Abuse:

The Business Class seat meets or exceeds the following cycle test requirements. All mechanisms, including recline system and pneumatic lumber system, will be subject to cyclic testing and must pass pre-determined and agreed number of cycles before failure to show that the MTBUR (Mean Time Between Unit Replacement ) is not less than 20,000 cycles. All parts will be subject to static abuse load testing to show compliance with existing certification requirements at the time of the initial technical coordination meeting (ITCM).

Safety:

Seat Delethalization:All components used in the seat assembly are fabricated and assembled to provide the ultimate in safety characteristics. The seat design incorporates the strategic use of padding, and the absence of sharp edges or unnecessary protrusions. The use of an approved belt mounted air bag is standard.

Fire, Smoke and Toxicity Protection:The nonmetallic materials used in the construction of the Business Class seat meet the appropriate flammability requirements of the subsection of the FAR/JAR 25.853 when tested in accordance with Appendix F of that document. The toxicity requirements for B787 are not fully defined and no suitable materials are commercially available at the time of this proposal that meet the total requirements. B/E requires a Standard Specification deviation on certain flammability/smoke/toxicity requirements.

Seat Belt Attachment:The seat belt attachment fitting allows sufficient, but limited freedom of swivel of the seat belt, for load alignment.The seat belt fitting is located to allow the load applied by the seat belt to be consistent. An airbag belt is assumed.

Placards:High quality, color coded, bilingual and placards shall be used and recessed into the surface to improve the appearance of quality. Safety placards are to be installed in accordance with regulatory requirements, clearly visible to the passenger seated behind. English language will be positioned with French language below.Placards will be required restricting personal stowage during Taxi/Take-Off/Landing (TTOL).

Comfort:The Business Class seat has been designed to provide optimum comfort with minimal cushioning in accordance with approved orthopedic and independent ergonomic principles.The cushions are both attractive and functional. The back and bottom cushions distribute the passengers body weight and provide overall body support. The seat provides superior comfort with the seat in all positions. The seat will transition into a flat, in-flight, bed surface of 80 inches.The Business Class offering has several features designed to increase privacy while retaining a family seating capability. Specifically:

Large privacy wings for all aisle pax. . Patented Diamond LayoutPatented CrystalFlex comfort system . Aisle access for all passengersSelf-contained suite for all passengers . Infinite position movable arms.Partially shielded ottoman

Durability:The Business Class seat is extremely rugged, built to provide extended long service life with low maintenance costs. Materials and hardware utilized are of high strength aircraft quality.A positive method of locking is provided for all hardware.

Maintainability:All components which may require replacement or adjustment are readily accessible. Maintenance and/or removal can be accomplished using standard hand tools.High wear surfaces are protected from substantial abuse by utilizing durable injection molded materials and rub strips. Easily removable backs and tables reduce replacement labor time.The spring loaded shear pin is keyed in the up position, ensuring seat track engagement. Lock screw is flush with track fitting body when engaged and provides evidence of positive engagement.The minimum number of parts and efficient designs are utilized to lower inventory maintenance requirements.

Styling:

The seat creates an atmosphere of contemporary luxury and style. The arms, tables and cushions provide a balanced blend of contour and mass and provide an attractive comfortable form. Care has been taken to provide a finished appearance across the rear of the seat assembly. The crisp, clean side end bay design complements the styling utilized in modern aircraft interiors. Light colors are used to enhance the visual space of the cabin.

Aesthetic that is welcoming and appears comfortable Shapes that are simple and elegant Cabin layout that appears spacious Excellence in comfort in the lounge position A relaxed Lounge Taxi Takeoff and Landing (TTL) position A high quality restful sleep in the bed position A great sense of individual space and privacy

To accommodate a customers desired styling and brand recognition, a pallet of selectable features will be offered (Examples only) These features will largely be determined by the seat supplier, as approved by Boeing.

Optional head rest

Optional cup holder

Variable arm rest design

Choice of cushion shape, Foam density

Choice of color and dress cover material

Family of Seats Catalog Options

Optional head rest Articulation

Family of Seats

Tourist / Economy Seating

Using the Family of Seats philosophy, a similar design and certification approach would permit the development a common base structure or platform on which all these seats are based.

A Matrix of installation Limitations would accompany the seat family defining where and how the seats are approved to be installed in the passenger cabin.

Premium Seating(Business, First)

Premium EconomyDomestic Business

Enabling a family of seats approach for premium is a challenge but contains the same benefits as economy.

Standard Seat Side View

Seat Type Dimensions

Standard Seat Front View

CG16.97

35.89

BACK PIVOT16.01

FOOTRESTIF

INSTALLED

CUSHION18.50 MAX

SRP PER AS804916.91

18.64

.65

32.89

44.50

CRP16.38 +.50

-.25

1.00

BACK PIVOT18.35

28.50+.00-.25

PAN13.29

24.00+.00-.25

24.50

MIN3.00

2.5 10.00

1.55 (TYPE III EXIT ROWS ONLY)1.30-2.20 (ALL PLACEMENTS EXCEPT TYPE III EXIT ROWS)

SRP PER AS804914.62

42.73

CRP16.63

UNDERSEAT CLEARANCE10.83

MAX2.50

102

CG11.88

18.50

.78

TABLE TRAVEL3.00

8.75

2.99 MAXHEADREST TRAVEL(IF INSTALLED)

26.00

Standard Triple

Top View of Standard Seat, IAT and Exit Triple(Top View of Double Seats Follow Same Pattern)

KeyT = Tip of Seat BeltB = Buckle of Seat BeltP = PCUR = Recline ButtonA = Ashtray

T B T B B T

P P P

R R R

A A

TBTBBT

PP

RRR

AA

PAisle

Outboard Outboard

Seat Items and Locations

SEAT DEFINITION

Seat Frame = Leg + Front Stud + Rear Fitting

The frame structure consists of machined aluminum fore and aft sections, which are fixed to aluminum lateral tubes providing a rugged, rigid assembly to support the attachment points for the primary pax mechanism and shell surround. All major structural components are attached using aircraft grade hardware. There are no blind rivets or welding used on the primary structure..All assemblies are equipped with standard load aligning seat belt brackets, which are designed to reduce the possibility of failure by maintaining seat belt loads nearly constant regardless of the direction of loading.

Standard Features Standard Airbus seat width 61.75-inches Machined, anodized, aluminum system Offset legs in all locations for consistency One-piece front and rear leg molded endbay/bumper and hostess step CrystalFlex fabric bottom diaphragm suspension system Quick release, anti-rattle rear track fitting

Rear Foot Block/Track Fitting Front Track Fitting Seat Frame

+ =

Leg

+

Leg Assembly

Leg:Machined aluminum leg system One-piece unitFloor distortion tolerant rear track fitting Anti-rattle feature for the front fittingIntegral track cover & Anodized finish.

Front Stud and Anti-Rattle:Machined stud (P/N 22303107) andAnti-Rattle Nut (97123007)Zinc nickel plated per AMS 2417 Type 2

Rear Fitting:Machined Rear 3 stud track fittingSingle shear plungerStuds and shear plunger Zinc Nickel plated per AMS 2417 Type 2

Baggage RestraintFor Taxi/Take-Off/Landing, baggage is envisioned to be stored in the ottoman. Testing to allow ottoman stowage is included in the B/E proposal.

Seat BacksThe seat back shall recline smoothly and effortlessly with a reliable recline system. Backs are equipped with a 4-way electric lumbar. All structural members in the back of the seat are suitably recessed or rounded, to enhance comfort and to reduce the possibility of passenger injury. Seat back support assembly consists of a Crystal Flex supported diaphragm connected from the lateral composite back tube. This arrangement, a standard in B/E seating provides a suspension comfort system with enhanced thermal comfort for the passenger. Recline and ControlThe recline system shall be controlled by an infinitely variable electric actuation system. There should be individual circuit-breaker under each seat to cut off the electrical power for seat actuation. Backup manual override systems shall be required. Operation of manual overrides must be easy to use with minimal effort by one cabin crew.The seats shall be designed to allow recline of the passenger at any position between upright position (take-off and landing) and fully reclined position. Recline is powered up to 180. Bed shall be designed to accommodate aircraft flight attitude. Manual override shall be provided as well.Seat cradle directly linked with seat recline actuation with a range of positive inclination for upright, mid recline and full bed position.Seat translation is related and controlled by the recline button to full bed position. A visible means shall be provided to show the take-off and landing. The Manual override will have a mechanical override integrated.Leg restThe leg rest structure will provide comfort by means of an individually deployable leg rest platform that is infinitely adjustable and deploys to full horizontal position. In addition to this a fixed ottoman is also provided for maximized passenger comfort.The actuation system will have current sensing capability to avoid entrapment issues and the ottoman cushion/support will hinge to prevent passenger foot entrapment. The leg rest will have a mechanical override integrated into the bottom of the leg rest.

Independently-operated mechanical armrest is designed to comply with the handicap accessibility requirements of 14 CFR 382.7. The armrest is infinitely adjustable through the entire travel from full upright to bed height. The armrest mechanism has a damped motion and is counter-balanced to enhance a first class experience.

Armrests

Headrest

A four-way manually adjustable headrest with side ears is included in this quote. Size and shape to be determined by final styling of the back cushion. The headrest features a proven friction slide and pivot mechanism with 10 years of in-field reliability experience.

ARM REST/ ARMCAP/ ESCUTCHEON GAPS:Interface gaps in between all these components shall not exceed .08 inches

Tray Tables deploy from the console. A food tray will span across to the opposite arm to provide a large rigid meal surface. The tray will be 11 deep and approximately 20 wide. When deployed the tray retains a 9clearance from the bottom cushion to allow adequate thigh clearance. Rotation is not necessary to allow egress from the seat due to aisle access for all passengers and the deploying armrest

Food Trays

Food Tray Gaps:Food Tray in stowed position-gap between the top surface of the tray and the bottom edge of provision shall not exceed .125 inches.

Tray Tables

There are multiple stowage areas.Personal stowage space shall be provided with easy access by the passenger.

Stowage area under the ottoman provides stowage for items such as: Laptop Blankets Shoes HandbagA second stowage area above the console provides stowage for small items such

as: Eye-glasses Keys HeadsetsThis area can be used for amenities as well as a convenient area to stow in-flight

menus.A separate literature stowage area provides stowage for: In-flight magazine(A4 size) Safety Card (A8 size) Sick bag Reading materials

Stowage

Cocktail Table

It is a machined aluminum cocktail table with a recessed laminate top for each passenger. Depending on location, this area may be recessed specifically to hold a water bottle during flight.Individual cocktail trays deploy in front of the console and the side to improve egress

Ottoman Protection

Ottomans shall be protected from substantial impact damage from carts, trolleys and cabin luggage. The protection shall act, firstly, as an impact absorber, and secondly as a sacrificial part. In this case multiple rub strips will protect the ottoman and surrounding shell.

Seat Shell and Partition

The seat shell shall be designed in such a way to provide privacy to the passenger in different seating positions. Overall styling and color and trim to be determined by Air liner.

Material:

Composite Panel Honeycomb Core

Special Seat Features

01 EPML Installation 02 SEB Installation (One drawing for each IFE supplier)

EPML Installation

The EPML can be mounted in the left hand seats in the lower end bay shroud.

SEB boxes are installed on the seat frame structure and are designed to be light weight and rugged.

Ensures well positioned cabling and industry standard fasteners.

AIRBUS INDUSTRY . A 380 SUPPLIER STANDARD SEAT FEATURES

Note:Front Row Seats & Seats with Furniture not-included.B/C + and F/C as Full Sleeper (without environment)** Standard Screen sizes*** On customer request onlySeat Pitch Range as minimum guideline.

Noted standard features of the B/E offering include:4 way adjustable headrest4 way adjustable lumbarArmrests provide maximum living space between and under arms.2 Actuator DesignOptimized seating positions from dining through bed including a patented Z-bed position.

Standard Features

Center Console

9.5 inches wide Amenities Recess Leather wrapped padded armcap (leather CFE) Passenger Control Unit (Optional) PC Power Port (Optional)

Power Port Installation KID 12v DC Power Port is mounted in the amenities recess

of the center console

Center Console / Endbays

End bays

Two inch wide handicap arm with discrete latch Powder coated machined aluminum end bay Injection molded rear trim cap and non-handedrubstrip Passenger Control unit (Optional) Powder coated machined aluminum front row module Spring loaded injection molded armcap Injection molded non-handed rubstrip

Mechanical Controls PL Porter infinitely adjustable recline lock Tamper proof adjustment mechanism Six inch maximum recline availability Aluminum control button

Console Inside

Backrest

01 Backrest Structure 02 Literature Pocket

Backrest Structure

Constructed of a light weight composite material Slim line back shape with integral lumbar support Body comfort suspension system Back diaphragm made from a high strength

durable crystal flex fabric Energy-absorbing features meeting FAR 25.562

and TSO-C127a HIC requirements

Literature Pocket

Cloth covered wire spring Spring is attached directly to seat

structure Velcro attachment to seat structure

Placards

01 Life Vest Placards 02 Safety Information Placards / Locations 03 Translation

01 Life Vest Placards Integral life vest pouch and bottom

support Snap closure Red pull strap Placarding not required02 Safety Information Placards / Locations

Safety information hot stamped on the backrest food tray.

Location of safety information is available on the upper right and left corners of the tray (Placarding Optional)

The bottom cushion placard shows compliance with FAR 25.853(c) and JAR 25.853 (C)

03 Translation

The safety information can be printed in any translation with customer furnished camera ready art work. Artwork is needed 12 weeks prior to shipment of seats.

Other BFE (Buyer Furnished Equipment) Life JacketA life-jacket stowage container is to be located on each seat below the bottom cushion, so as to integrate with the seat styling. A red strap retains and offers the lifejacket to the passenger when pulled open.

Seat Covers and Upholstery

01 Foam / Density 02 Fire Blocking Layer 03 Seat Cover Fabric / Leather

Bottom CushionFoam densities and profile shall provide lumbar and pelvic support, and an equal distribution of pressure on the buttocks and thighs to minimize passenger discomfort in both upright and reclined position. Latest foam technology shall be considered if it is proven to be able to enhance the passenger comfort.The shape and size of the foam shall be standard where possible across the seat variants to reduce the variety of dress covers. B/E will work to provide a back and bottom cushion to human shape and size specification. The width of the bottom cushion is approximately 20. The length of the bottom cushion is approximately 19. The thickness of the cushion varies from 3 thick to 4 thick. The cushions are not to be considered as flotation devices.Each component used in the upholstery system must meet or exceed the requirements of the following:14CFR 25.853(a), Amendment 25-83.

01 Foam / Density Non-Flotation Molded Fire hard Foam 55 ILD Bottom Cushion & 35 ILD Headrest cushion02 Fire Blocking Layer Cushions are manufactured from Fire hard Foam and do not require a fire blocking layer unless leather is used.03 Seat Cover Fabric / Leather On dock date for fabric is 60 days prior to shipment of seats from B/E facility 10 linear yards of fabric required per color selection for flammability testing (if required) Preferred Fabrics:

Fabric color is optional Material composition 90% Wool/10% Nylon Material density 12 OZ/SQ2 CRP/SRP to be maintained within .50 inch of baseline certification

Style A : Simple roll-on dress covers, fitting the form and shape of the ergonomically designed SPECTRUM seating.

Upholstery Styles

Style B: A modern design accentuating the seat height and contour creating a look of enhanced space, while retaining the simple roll-on SPECTRUM dress cover system.

Style C: Accentuating a plush seating environment, this style enhances the look of seat width with the organic styled stitching giving added impression that the SPECTRUM seat surrounds the passenger in comfort.

Style D: Vertical organic lines, continue to enhance the seat height, while soft curves follow the natural shape of passengers...simple, comfortable and stylish SPECTRUM compliments any cabin decor scheme.

Style E: Soft curves continue the organic appeal while additional stitching accentuates the ergonomically designed SPECTRUM comfort system, creating a look of enhanced lumbar support for the traveler.

SeatbeltsStandard Seatbelts Amsafe P/N 2010-1-511-XXXX Series

TSO C22g, 30 buckle, fabric label Color is optional

Buckle (B) and Tip (T) locations From inboard to outboard (standard triple) TB/BT/BT

All safety belts are CFE and must be received 60 days prior to the first shipment of seats.

Optional Seatbelts Amsafe P/N 2011-1-55-XXXX Series

TSO C22g, 90 buckle, fabric label (CAA) Color is optional

Safety Belts for 9g / 16g programs Safety belts are CFE, installed by B/E Aerospace. Standard belts are 3000 lbs nylon with 15 inch fixed, and 30 inch

buckle side lengths. Color of safety belts is optional. Safety belts have cloth name tag sewn on. AmSafe P/N 502755-XXX-XXXX, Model 502758-1 (CAA) AmSafe P/N 502745-XXX-XXXX, Model 502758 (FAA)Other BFE (Buyer Furnished Equipment) seat belts The airbag seat belts shall meet TSO C22g. The belt buckle will release at 45 degrees. Length of seat belt should accommodate 5-95 percentile passengers, and belt buckle should be within 1.5 inches of the centre line of 50 percentile passenger with seat belt fastened.

IFE Equipment

01 Available PCU P/Ns 02 Available cable harness P/Ns 03 Available SEB P/Ns

01 Available PCU Part numbers

Matsushita Avionics RD-AX6737/6738-54Matsushita Avionics RD-AX6737/6738-52Matsushita Avionics RD-AX6737/6738-53Matsushita Avionics RD-AX6739/6740-54Matsushita Avionics RD-AX6739/6740-52Matsushita Avionics RD-AX6739/6740-53

02 Available cable harness part numbers

Matsushita Avionics RD-AM6625-XX

03 Available SEB part numbers

Matsushita Avionics RD-AX4431-10

In-flight Entertainment and CommunicationIFE equipment will be BFE. The mentioned IFE supplier is Thales or Panasonic. It is expected that the fitment of the equipment will follow IFE Supplier installation guidelines. The IFE equipment shall be adequately protected from fluid ingress. Either but not both IFE systems will be accommodated. The IFE system will be integrated into the seat design to minimize LRU times.

Integrated Handset The handset and cradle shall be installed to allow passengers easy access to the in-flight entertainment and services. The handset is to be mounted vertically in the center console or horizontally under the privacy panel armrest (pending industrial design). The position of the mounting shall be in such way that it will not cause any discomfort to the passenger; should not take up seating space, and shall not be easily accidentally activated by the passengers whilst in any seating position.

Remote Jack Module (RJM)The seat will provision for an RJM and located with easy access.

The design will provision for up to a 15 widescreen format SVDU installed at a fixed angle in the shell. The height of the monitor shall be determined to provide an ergonomically correct view angle to suit the specified anthropometrics range of occupant seated fully upright or in the reclined position.

Video Monitor (Smart video Display Unit)

In-seat Power Supply and Data Outlet(s) (ACOU)An 110V A/C in-seat power and data outlet shall be provided for each passenger place. The outlets shall be mounted within easy access by the passenger. The outlet sockets must be installed vertically to prevent fluid ingress.The outlet housing design shall appear integral to the seat. However, the installation shall be modular. The in-seat power supply outlet may also provision for up to two (2) data port outlets, and an external RCA jack for external video.Seat Electrical Boxes (SEB)All seat electrical boxes shall be mounted in order to allow adequate air for electronic cooling. If needed, a drip shield is to be installed about these boxes to prevent fluid spillage. The access shall be maintenance -friendly, and allow access to the seat electrical boxes without removing the seat from seat track.

Audio IFE

Standard Audio IFE N/A (not required if no IFE chosen)

Audio IFE Option Top mounting option

Installation with remote transducer

Inboard arms only Angled towards passenger

Side mounting option Integral transducer Inboard arms only

SPECTRUM Approved Systems MASC Rockwell Thales KID General Dynamics

See Table 01 for Approved IFE Components

Note: All cable lengths are pre-determined

Side Mounted Option

Top Mounted Option

P/N DESCRIPTIONP/N DESCRIPTION 700-2326-004 RH Side Mount PCU

RD-AX6739-XX Side Mounted PCU (LH) 700-2326-003 LH Side Mount PCURD-AX6740-XX Side Mounted PCU (RH) 700-2327-001 Top Mount PCURD-AX6733-XX Top Mounted PCU 700-2205-002 RJURD-AX6421-18 Dual Pin RJU 700-2323-002 SEBRD-AX6426-05 Single Pin RJU 749-0548-XXX In Seat HarnessRD-AX4431-10 SEB (Airbus)RD-AM7902-XX In Seat Harness TPLRD-AM7929-XX In Seat Harness DBL P/N DESCRIPTION

Z280H3030000 110V Oulet unitZ280H1030013 110V Oulet Front Plate

P/N DESCRIPTION Z285H0121110 ISPC (Double)177806-X01 PCU (Top & Side) Z280H1500XXX ISPS - PPUI Harness170777-25 RJU TBD DSEB - ISPC Harness177745-101 SEB Z270H3101XXX ISPC - ACOU Harness177925-101 SEB Terminator Z280H3105XXX ISPC - PPUI Harness177824-101 ISPC ATB01-12/XXX Bonding Cable177829-101 110V AC Outlet Unit177822-101 USB Incl Harness177180-000 PED In Use Light P/N DESCRIPTION177179-XXX ISPS - PPUI Harness 1171-1 110V Oulet Unit178208-00X SEB - PCU/RJU Harness 1170-1 ISPS177585-0XX Multi Power Harness 750-5150-402 In Use Light177178-XX ISPS - ACOU Harness 1170805 Cable Assy ISPS - OU

177590-XXX Grounding Harness 1170801 Cable Assy In Use Light1170803 Cable Assy Seat to Seat

GENERAL DYNAMICS (110V)

MASC

THALES

ROCKWELL

KID (110V)

SPECTRUM Approved Components

Table 01

PC Power and USB Ports

Standard PC Power and USB Ports N/A (not required if no IFE chosen)PC Power and USB Port Options 2 outlets per triple, 1 per double Mounted on front beam, beneath cushion Accommodates the following systems:

KID Thales General Dynamics

110V AC or 15V DC Systems PC power in-use indicator light location on

end bays See Table 25.21.016.01 for Approved IFE

Components

Power Port Example

Escape Path Lighting

PC Power In-Use Indicator Light

Location

Underseat Electronics Box (UEB)Standard UEB N/A (not required if no IFE chosen)

UEB Options Lightweight, rugged and mounted to a universal UEB

bracket on seat frame Accommodates MACS, Rockwell, KID and General

Dynamics systems Thales systems require a mounted UEB to the baggage

bar (not shown) Well-positioned for cabling and industry standard fasteners

Seat Actuator Power Distribution

Legrest actuator and Housipart comparisonLeg rest Housing Stress analysis @ 16g & Envelope comparison.

Recline (Rotary) actuator and Housing analysisRecline rest Housing Stress analysis @ 16g & Envelope comparison.

Seat Pan actuator and Housing analysisSeat pan Housing Envelope comparison.

Foot rest actuator and Housing analysisFoot rest Housing & Envelope comparison

Actuator major components and its function are as shown:

Trim and Finish

Available color scheme:- LT Grey (BAC7801)/Dark Grey (BAC7722)- LT Grey (BAC7734)/Dark Grey (NEO 0823)- LT Grey (57-1-8084)/Blue (7445)

Standard Options Trim and Finish Components

Armcaps Escutcheons Tray tables Powder coated surfaces

Choice of 4 color combinations* Option AC

Blue-Black 7923 and Pepperdust 7801 Option AD

Blue-Black 7923 and Light Gray 7734 Option BC

Dark Gray 7800 and Pepperdust 7801 Option BD

Dark Gray 7800 and Light Gray 7734

* Color swatches available upon request

Option AC Option AD

Option BC Option BD

Cross Reference:- BAC7801...... Pantone 4C-BAC7722...... Pantone 412C- BAC7734...... Pantone 429C- NEO 0823..... Pantone 432C- 57-1-8084..... Pantone 434C- 7745............. Pantone 2955U

NOTE: Pantone numbers provide closest available approximation to the actual color. Color chips available upon request.

Composites Serve as Primary Structural Material

Carbon laminateCarbon sandwichOther compositesAluminumTitanium

Composites50%

Aluminum20%

Titanium15%

Steel10%

Other5%

Minimum Catalog Qualification Requirements

An Airplane Passenger Seat That: Is Previously TSOd Meets the Target Weight Criteria (+ or (x)%) Can Be Manufactured/Assembled, Shipped by the

Supplier and received by Boeing in Less Than 4 Months

Fits Through the Airplane Door Or, is received in Component Modules Capable

of Fitting Through the Airplane Door Can Be Installed in the Airplane Within specified

time. Or, Modules Can Be Reassembled and Installed

Within specified time Has Boeing-Defined Standard Structural and

Electrical Interfaces Meets RM&T Requirements for:

(x) Number of Cycle Tests (y) Dollars per Flight Hour Maintenance Cost

Supplier data has been received and approved by Boeing for the seat model.

The seat model has successfully passed the FAI.

1 0 0 3 0 2 0 0 1 B 0

WINSTON SALEM 14 DIGIT PART NUMBER

FIRST (7) DIGITS IS THE PART BASE NUMBER

NEXT (3) DIGITSIS THE PART DASH

NUMBER

EVEN NUMBERS = 002

RIGHT HANDED

ODD NUMBER = 001

LEFT HANDED

NEXT (2) DIGITSIS THE PART TRIM AND FINISH

NEXT (2) DIGITSIS THE CUSTOMER COAD

1 1A

CENTER CONSOL 1003021001-AB01a

Main Cabin & RegionalExisting Product Family

Premium Seating Lead Customers!

42 Pitch 50 Pitch 55 Pitch

Millennium EMini POD

MillenniumConcept Side Sleep Seating

80 Pitch

Voyager Lie Flat

Super First ClassPOD

Premium Class Seating Solutions for All Pitches

Minipod Lie Flat Customers

Spectrum Installed Customer Base

Prepared & Compiled

REFERENCES

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