xAir T

raffic M

ode

rnization

(ATM)

&

x

Pe

rform

an

ce B

ased N

avig

ation

(PBN)

Aug

ust

2012

x

Air T

raffic M

an

age

me

nt (A

TM) &

x

Pe

rform

an

ce B

ased N

avig

ation

(PBN)

Ho

neyw

ell.co

m

Why

ATM &

PBN?

SAFETY

Honeyw

ell P

roprieta

ryHO

NEYW

ELL/HUGH

ES PRO

PRIETAR

Y

Ho

neyw

ell.co

m

ATM &

PBN

The

Mo

vem

ent

is G

lobal

and

Happ

ening

No

w

A ph

ased d

ecom

missio

ning of

VOR

s

Blo

ck Upg

rades

aimed

at facilitating

interop

erability

,

harm

onizatio

n a

nd m

odernizatio

n of

air tra

nsp

ortatio

n

wo

rldw

ide.

Honeyw

ell P

roprieta

ry

A ph

ased w

ithdra

wal

of C

AT I ILS

sho

uld co

mm

en

ce n

o late

r th

an

2012.

HON

EYWELL/HUG

HES

PROPR

IETARY

A ph

ased d

ecom

missio

ning of

VOR

s

sho

uld b

e co

mpleted

by 2015

.

Ho

neyw

ell.co

m

ATM &

PBN

The

Mo

vem

ent

is G

lobal

and

Happ

ening

No

w

Honeyw

ell P

roprieta

ry

Ho

neyw

ell.co

m

ICAO

Glob

al Air

Na

vigatio

n Pla

n fo

r A

TMB

lock

0 in

2013

Honeyw

ell P

roprieta

ry

Ho

neyw

ell.co

m

Blo

ck 0

in

2013

ICAO

Glob

al Air

Na

vigatio

n Pla

n fo

r A

TM

Honeyw

ell P

roprieta

ry

= ATM

& PB

N E

nabled

by H

on

eyw

ell Tech

nology

or E

xpe

rtise=

ATM &

PBN

En

abled by

Ho

ney

well

Techn

ology o

r E

xpe

rtise

Ho

neyw

ell.co

m

Ho

ney

well

& H

ughes

Offe

r a

Bro

ad B

asis of

RN

P

Exp

ertise

Aircraft Eq

uipag

eAircraft

Equip

age

RNP O

peratio

ns

RNP O

peratio

ns

Op

eratio

nal

Appro

valO

pe

ration

al App

roval

Honeyw

ell P

roprieta

ry

Honeyw

ell Eq

uipm

ent

-FMS

software

upgrad

es to

bring

low

RNP cap

ability to

most

Honeyw

ell eq

uipped

aircraft-In

ertial

Refe

rence

Units

-WAAS

GPS

-Display Syste

ms

-EGPW

S

Pro

cedu

re a

nd D

ataba

se

Valid

ation

-Initial

validatio

n of

all p

ublic RN

P AR

pro

cedure

s & valid

ation

eve

ry 28

day

cycle

RN

P M

onito

ring-

Re

cord

keeping

of op

erato

rs RN

P AR

ope

ration

s

RN

P B

en

efits-

Red

uced

Op

erating

Co

sts-

Bette

r A

ccess

-In

crea

sed S

afety

Consulta

ncy

Service

s-O

peratio

nal app

roval

subm

ittal

packag

e fo

r AC90

-101

com

pliance

& FAA

coordin

ation

-Timely

and

efficient

integratio

n

of req

uirem

ents

into cu

rrent

flight op

eratio

ns

Ho

neyw

ell.co

m

PBN

Specificatio

ns

Ove

rview

Honeyw

ell P

roprieta

ry

DEP

or A

PPEN

ROU

TE

Ho

neyw

ell.co

m

2xR

NP

2xR

NP

ANP

(NM)

Containment limit

Containment limit FMC

positio

n

RN

P-x

is airc

raft

path

confo

rma

nce

with

accu

racy x

or

bette

r, 95%

of th

e

time

.

PBN

Co

ntainm

ent

Limits

are

2xR

NP

Honeyw

ell P

roprieta

ry

1xR

NP

Containment limit

Containment limit

Desired

track

E

xam

ple: R

NP

-1

states th

at th

e

aircraft

is w

ithin a

radius

of 1

na

utical

mile

, 95%

of th

e

time

.

Ho

neyw

ell.co

m

PBN

On

-Bo

ard

Acc

uracy

Mo

nitoring

& R

epo

rting

Honeyw

ell P

roprieta

ry

HON

EYWELL/HUG

HES

PROPR

IETARY

Ho

neyw

ell.co

m

Inefficie

nt R

outing

s a

re Elim

inated

via PB

NHoneywell

Prop

rietary

Ho

neyw

ell.co

m

PBN

= A

ccu

racy a

nd R

epeatability

Airc

raft fly

a sp

ecific p

ath b

etwee

n 3

-dimen

sion

ally d

efined

points

in sp

ace

L

ateral

gro

und

track w

ith V

ertical

path

guid

an

ce

N

avig

ation

al p

erfo

rman

ce m

onito

ring a

nd ale

rting

Honeyw

ell P

roprieta

ry

Ho

neyw

ell.co

m

PBN

Facilitates

Acc

uracy

, S

afety, &

Cap

acity

Honeyw

ell P

roprieta

ry

Ho

neyw

ell.co

m

Le

veraging

PBN

for D

epa

rture

Be

nefits

(SID)KD

FW repla

ced co

nve

ntional

gro

und

based

dep

artu

res with

RN

AV b

ased

dep

artu

res

and

incre

ased

the efficie

ncy

of th

eir airsp

ace

.

KDFW

replaced

conve

ntional

gro

und

based

dep

artu

res with

RN

AV b

ased

dep

artu

res

and

incre

ased

the efficie

ncy

of th

eir airsp

ace

.

Honeyw

ell P

roprieta

ry

Ho

neyw

ell.co

m

Le

veraging

PBN

for E

nro

uteB

en

efitsE

xisting Q

-Ro

ute in

United

States

Satellite

Satellite

--ba

sedb

ased

QQ--R

oute

Ro

ute

606 N

M tra

ck

606 N

M tra

ck

Leg

acy

Gro

und

Leg

acy

Gro

und

--ba

sed

ba

sed

Na

vaidN

avaid

Ro

ute

Ro

ute

641 N

M tra

ck m

iles

641 N

M tra

ck m

iles

Honeyw

ell P

roprieta

ryH

ON

EY

WE

LL/HU

GH

ES

PR

OP

RIE

TA

RY

606 N

M tra

ck

606 N

M tra

ck

mile

sm

iles

Th

e Q

The

Q--R

oute

achie

ves a

34 N

M sa

vings in

R

oute

achie

ves a

34 N

M sa

vings in

track

mile

s p

er flight

. This

is a

6% red

uctio

n

track

mile

s p

er flight

. This

is a

6% red

uctio

n

of th

e o

verall

distan

ce.

of th

e o

verall

distan

ce.

A

5 m

inute

redu

ction

of

flying tim

e is

A

5 m

inute

redu

ction

of

flying tim

e is

realized

using

the

Qre

alized u

sing th

e Q

--Ro

ute.

Ro

ute.

This

equ

ates to

a fu

el sa

vings of

This

equ

ates to

a fu

el sa

vings of

appro

ximately

300lbs p

er flight

.

appro

ximately

300lbs p

er flight

.

(A320/B737)(A320/B737)

QQ

--Ro

utes a

re n

ot subje

ct to

Gro

und

Ro

utes a

re n

ot subje

ct to

Gro

und

--ba

sed

ba

sed

Na

vigatio

n Aid

failure

s o

r o

utage

s.

Na

vigatio

n Aid

failure

s o

r o

utage

s.

Ho

neyw

ell.co

m

Le

veraging

PBN

for A

rrival B

en

efits (STA

R)

< 2

,000

Altitude

(ft M

SL)T

rackC

olor

< 2

,000

Altitude

(ft M

SL)T

rackC

olor

< 2

,000

Altitude

(ft M

SL)T

rackC

olor

PDX

PDX

PDX

Gro

und

Tra

cks for co

nve

ntion

alco

nve

ntion

algro

und

based

and

radar ve

ctor flight

patte

rns

Gro

und

Tra

cks for co

nve

ntion

alco

nve

ntion

algro

und

based

and

radar ve

ctor flight

patte

rns

Honeyw

ell P

roprieta

ry

> 24

,00010

,000

24,000

8,000

10,000

6,000

8,000

4,000

6,000

2,000

4,000

< 2

,000

> 24

,00010

,000

24,000

8,000

10,000

6,000

8,000

4,000

6,000

2,000

4,000

< 2

,000

> 24

,00010

,000

24,000

8,000

10,000

6,000

8,000

4,000

6,000

2,000

4,000

< 2

,000PD

X

Ho

neyw

ell.co

m

Le

veraging

PBN

for A

rrival B

en

efits (STA

R)

Altitude

(ft M

SL)T

rackC

olor

Altitude

(ft M

SL)T

rackC

olor

Altitude

(ft M

SL)T

rackC

olor

PDX

PDX

Gro

und

Tra

cks for PB

N R

NAV

based

flight p

attern

sG

round

Tra

cks for PB

N R

NAV

based

flight p

attern

s

Honeyw

ell P

roprieta

ry

> 24

,00010

,000

24,000

8,000

10,000

6,000

8,000

4,000

6,000

2,000

4,000

< 2

,000(ft

MSL)

Colo

r

> 24

,00010

,000

24,000

8,000

10,000

6,000

8,000

4,000

6,000

2,000

4,000

< 2

,000(ft

MSL)

Colo

r

> 24

,00010

,000

24,000

8,000

10,000

6,000

8,000

4,000

6,000

2,000

4,000

< 2

,000(ft

MSL)

Colo

r

PDX

Ho

neyw

ell.co

m

Honeyw

ell P

roprieta

ry

Case

Studies &

Exa

mples

Ho

neyw

ell.co

m

Ne

wa

rk/Ne

w Y

ork

Airspace

Red

esign

Honeyw

ell P

roprieta

ry

Ho

neyw

ell.co

m

PBN

= O

pe

ration

al B

en

efit

Imp

roved

Access

Honeyw

ell P

roprieta

ryH

UG

HE

S P

RO

PR

IET

AR

Y

ILS RW

11 580

/5000ILS

RW 11

580/5000

GLS

RW 11

308/5000

G

LS RW

11 308

/5000

Imp

roved

Access

Lo

we

r M

inimu

ms

Ho

neyw

ell.co

m

PBN

= O

peratio

nal

Ben

efit

Honeyw

ell P

roprieta

ry

PS

P V

OR

PS

P V

OR

--B A

pp

roa

chB

Ap

pro

ach

VO

R a

pp

roa

ch m

inim

um

s: 18

26

/3V

OR

ap

pro

ach

min

imu

ms: 1

82

6/3

PS

P R

NA

V R

NP

Z R

wy

13

RP

SP

RN

AV

RN

P Z

Rw

y 1

3R

RN

AV

(RN

P) M

inim

um

s 27

7/1

R

NA

V (R

NP

) Min

imu

ms 2

77

/1

GB

AS.

The P

recision

Appro

ach

for th

e F

uture

Ho

neyw

ell.co

m

NiBiInte

rnatio

nal

Airpo

rt

Cu

rrent

Op

eratio

ns

Curre

nt O

peratio

nal

Enviro

nm

ent

:

Runw

ays:

11L/29R -10

,499ft x

148ft

11R/29L -12

,467ft x

148ftHoneyw

ell P

roprieta

ry

Appro

ach

es:

ILS

DM

E 11L

, 11R

(CAT

II)

VOR

DM

E 11L

, 11R

, 29L

, 29R

N

DB

11L, 29R

SIDs &

STARs:

4 STAR

s (path

based)

4 SID

s (path

based)HON

EY

WE

LL/HU

GH

ES

PR

OP

RIE

TA

RY

Ho

neyw

ell.co

m

Current

Infra

structure

Honeyw

ell P

roprieta

ry

Infra

structure

NiBiInternational

Airport

VVNB

Ho

neyw

ell.co

m

Cu

rrent

Dep

artu

res:

1.

VOR

s &

ND

Bs a

re

mand

atory

(NOB

, VPH

,

KW

)

2.

Req

uires tight

aircraft

perfo

rman

ce to

maintain

NiBiInte

rnatio

nal

Airpo

rt (VVN

B)

Cu

rrent

SIDs

Honeyw

ell P

roprieta

ry

perfo

rman

ce to

maintain

clear of

special

use

airspace

per SID

SIDs in

WH

ITESID

s in

WH

ITESID

s in

WH

ITESID

s in

WH

ITE

HONEYW

ELL/HUGHES

PROPRIETARY

Ho

neyw

ell.co

m

Cu

rrent

Arrival

and

Tra

nsitio

ns:

1.

VOR

s &

ND

Bs a

re

mand

atory

(VPH, NO

B,

CAB

, BQ

, M

C, K

W)

2.

Req

uires tight

aircraft

NiBiInte

rnatio

nal

Airpo

rt

Cu

rrent

STAR

s

Honeyw

ell P

roprieta

ry

2.

Req

uires tight

aircraft

perfo

rman

ce to

maintain

clear of

special

use

airspace

per STAR

HONEYW

ELL/HUGHES

PROPRIETARY

Ho

neyw

ell.co

m

Perfo

rmance Based

Navigation Benefits

NiBiInternational

Honeyw

ell P

roprieta

ry

NiBiInternational

Airport

VVNB

Ho

neyw

ell.co

m

NiBiInte

rnatio

nal

Airpo

rt -STA

R

PBN

Co

ncept

HO

NE

YW

ELL/H

UG

HE

S P

RO

PR

IET

AR

Y

Honeyw

ell P

roprieta

ry

Optim

ize p

rofile d

esce

nts apply ve

rtical fe

ature

s to cu

rrent

STARs th

at h

ave

dem

onstrated

benefits in

pre

vious im

plem

entatio

ns:

1.

~600lbs of

fuel

saving

s per flight

2.

Red

uced

ATC/Pilot co

mm

unicatio

ns by

up to

70%3.

Red

uced

Noise

impacts fo

r th

e co

mm

unitie

s4.

Flight tim

e red

uctio

ns of

~2

min

s per flight

5.

Flight Idle

desce

nts from

cruise flight

to sh

ort

final

6.

Avoid

s Restricted/P

rohibited Airsp

ace

Optim

ize p

rofile d

esce

nts apply ve

rtical fe

ature

s to cu

rrent

STARs th

at h

ave

dem

onstrated

benefits in

pre

vious im

plem

entatio

ns:

1.

~600lbs of

fuel

saving

s per flight

2.

Red

uced

ATC/Pilot co

mm

unicatio

ns by

up to

70%3.

Red

uced

Noise

impacts fo

r th

e co

mm

unitie

s4.

Flight tim

e red

uctio

ns of

~2

min

s per flight

5.

Flight Idle

desce

nts from

cruise flight

to sh

ort

final

6.

Avoid

s Restricted/P

rohibited Airsp

ace

Ho

neyw

ell.co

m

Fro

m th

e O

ptimized

Profile

Desce

nts, n

ew

wayp

oints can b

e add

ed to

allow

for m

ultiple

appro

ach

transitio

ns to

a single

or m

ultiple ru

nw

ays. This p

rovid

es g

reate

r fle

xibility a

nd

predictability

for ATC

and

Pilots.

Fro

m th

e O

ptimized

Profile

Desce

nts, n

ew

wayp

oints can b

e add

ed to

allow

for m

ultiple

appro

ach

transitio

ns to

a single

or m

ultiple ru

nw

ays. This p

rovid

es g

reate

r fle

xibility a

nd

predictability

for ATC

and

Pilots.

NiBiInte

rnatio

nal

Airpo

rt (VVN

B)R

NAV

STARS

Optim

ized P

rofile D

escents

Honeyw

ell P

roprieta

ryHO

NEYWELL/HUG

HES PRO

PRIETARY

Ho

neyw

ell.co

m

NiBiInte

rnatio

nal

Airpo

rt (VVN

B)G

BAS/G

LS App

roach

Radiu

sR

adius--toto

--fix tu

rns a

re

fix tu

rns a

re

used

to a

void

used

to a

void

prohibited

prohibited

airspace

airspace

AAG

BAS/GLS

final

G

BAS/GLS

final

appro

ach

segm

ent

app

roa

ch seg

ment

pro

vide

s p

recisio

n

pro

vide

s p

recisio

n

landing

minim

um

sla

nding m

inimu

ms

Honeyw

ell P

roprieta

ry

GBAS/G

LS with

RN

P

GBAS/G

LS with

RN

P

fusio

n p

rovid

es:

fusio

n p

rovid

es:

Im

pro

ved a

ccess

Impro

ved a

ccess

In

creased

safetyIn

creased

safety

Low

er M

inimum

sLow

er M

inimum

s

HO

NE

YW

ELL/H

UG

HE

S P

RO

PR

IET

AR

Y

Ho

neyw

ell.co

m

The cu

rrent

arrivals co

uld b

e m

odified to

pro

vide additio

nal

flexibilitie

s to N

oiBai

.

Exa

mple

s Includ

e:

1.

Use

RN

AV (R

NP)

with rep

eatable

curved

path

s to e

ach

runw

ay e

nd.

2.

Use

RN

AV (R

NP)

to sh

orte

n flight

tracks to

each

runw

ay e

nd.

The cu

rrent

arrivals co

uld b

e m

odified to

pro

vide additio

nal

flexibilitie

s to N

oiBai

.

Exa

mple

s Includ

e:

1.

Use

RN

AV (R

NP)

with rep

eatable

curved

path

s to e

ach

runw

ay e

nd.

2.

Use

RN

AV (R

NP)

to sh

orte

n flight

tracks to

each

runw

ay e

nd.

NiBiInte

rnatio

nal

Airpo

rt (VVN

B)M

odification

of E

xisting STA

Rs

Honeyw

ell P

roprieta

ryHO

NEYWELL/HUG

HES PRO

PRIETARY

Ho

neyw

ell.co

m

NiBiInte

rnatio

nal

Airpo

rt (VVN

B)R

NAV

Ru

nw

ay T

ran

sition

s

Honeyw

ell P

roprieta

ry

RN

AV p

aths fro

m cu

rrent

arrivals co

uld se

rve

multiple

runw

ays, o

r p

rovid

e m

ultiple tra

nsitio

ns to

the sa

me ru

nw

ay

RN

AV p

aths fro

m cu

rrent

arrivals co

uld se

rve

multiple

runw

ays, o

r p

rovid

e m

ultiple tra

nsitio

ns to

the sa

me ru

nw

ay

HO

NE

YW

ELL/H

UG

HE

S P

RO

PR

IET

AR

Y

Ho

neyw

ell.co

m

NiBiInte

rnatio

nal

Airpo

rt (VVN

B)G

BAS/G

LS App

roach

A red

uctio

n of

10 N

M fo

r a

n a

verag

e

aircraft co

nfiguring

for app

roach

save

s:

Th

ree m

inute

s of flight

time

Honeyw

ell P

roprieta

ry

RN

AV (R

NP)

can cu

rve th

e fin

al app

roach

to b

egin o

n th

e d

ow

nw

ind leg

and

pro

vide

lateral

and

vertical

guid

ance

to th

e ru

nw

ay e

nd o

r to

a G

LS inte

rcept.

A

GNSS

appro

ach

with a

4 N

M fin

al w

ould

save

10.6

NM

per flight

.

Th

ree m

inute

s of flight

time

82

.7 kilog

ram

s of fu

el

104

litres

of fu

el

HO

NE

YW

ELL/H

UG

HE

S P

RO

PR

IET

AR

Y

Ho

neyw

ell.co

m

PBN

En

route

Ben

efits B

etwee

nNiBi&

Tn

S

n N

ht

Intern

ation

al Airp

orts

(VVNB

-VVTS)L

ega

cy G

rou

ndL

ega

cy G

rou

nd--

ba

sed

ba

sed N

avaid

Na

vaidR

oute

R

oute

(W1)

(W1)

690 N

M tra

ck m

iles

690 N

M tra

ck m

iles

Th

e Q

The

Q--R

oute

achie

ves a

32 N

M

Ro

ute a

chieve

s a

32 N

M

saving

s in

track

mile

s p

er flight

sa

vings in

track

mile

s p

er flight

versu

s th

e W

1 ro

uting.

versu

s th

e W

1 ro

uting.

This

results

in a

5% red

uctio

n of

the

This

results

in a

5% red

uctio

n of

the

ove

rall dista

nce

flow

n.

ove

rall dista

nce

flow

n.

A

4 m

inute

redu

ction

of

flying tim

e is

A

4 m

inute

redu

ction

of

flying tim

e is

realized

using

the

Qre

alized u

sing th

e Q

--Ro

ute.

Ro

ute.

This

equ

ates to

a fu

el sa

vings of

This

equ

ates to

a fu

el sa

vings of

appro

ximately

250

appro

ximately

250 lb

slb

sp

er flight

.

pe

r flight

.

Satellite

Satellite

--ba

sedb

ased

QQ--R

oute

Ro

ute

Honeyw

ell P

roprieta

ryH

ON

EY

WE

LL/HU

GH

ES

PR

OP

RIE

TA

RY

appro

ximately

250

appro

ximately

250 lb

slb

sp

er flight

.

pe

r flight

.

(A320/B737)(A320/B737)

QQ--R

oute

Ro

ute

658 N

M tra

ck

658 N

M tra

ck

mile

sm

iles

Dire

ct Q

Dire

ct Q

--Ro

uteR

oute

623 N

M tra

ck

623 N

M tra

ck

mile

sm

iles

A

direct

QA

direct

Q--ro

ute o

ver L

ao

s

route

ove

r L

ao

s

and

Ca

mb

odia w

ould

net

a 67

a

nd C

am

bodia

wo

uld n

et a

67

NM

saving

s in

track

mile

s

NM

saving

s in

track

mile

s

from

a W

1 ro

uting .

from

a W

1 ro

uting .

A

redu

ction

of 8

min

utes of

A

redu

ction

of 8

min

utes of

flying tim

e a

nd 450

flying

time

and

450 lb

slb

sof

fuel

of

fuel

saving

s p

er flight

wo

uld b

e

saving

s p

er flight

wo

uld b

e

gain

ed ve

rsus u

sing th

e W

1

gain

ed ve

rsus u

sing th

e W

1

routing

.

routing

.

HONEYW

ELL/HUGHES

PROPRIETARY

Ho

neyw

ell.co

m

The

curre

nt a

rrivals co

uld b

e utilized

to p

rovid

e additio

nal

flexibilitie

s

to N

oiBai

.

Exa

mple

s In

clude

:

1.

Use

RN

AV (R

NP)

with rep

eatable

curved

path

s to

ea

ch

run

way

end

.

The

curre

nt a

rrivals co

uld b

e utilized

to p

rovid

e additio

nal

flexibilitie

s

to N

oiBai

.

Exa

mple

s In

clude

:

1.

Use

RN

AV (R

NP)

with rep

eatable

curved

path

s to

ea

ch

run

way

end

.

NiBiInte

rnatio

nal

Airpo

rt (VVN

B)G

BAS/G

LS App

roach

RW 11

L/R

RW 29

L/R

Honeyw

ell P

roprieta

ry

RF

turn

transitio

ns ca

n

pro

vided

defin

ed

separatio

n b

etween

airspace

or airp

orts

HONEYW

ELL/HUGHES

PROPRIETARY

Ho

neyw

ell.co

m

NiBiInte

rnatio

nal

Airpo

rt

Ru

nw

ay 11

L/R D

ual

Feed

Honeyw

ell P

roprieta

ry

A red

uctio

n of

10nm

for a

n a

verag

e aircraft

config

uring

for this

appro

ach

save

s:

2.86

min

utes of

flight tim

e

182lbs of

fuel

27

.5 g

allons

HO

NE

YW

ELL/H

UG

HE

S P

RO

PR

IET

AR

Y

Ho

neyw

ell.co

m

Current

Infastructure

Honeyw

ell P

roprieta

ry

Infastructure

Nng

International Airport

VVDN

Ho

neyw

ell.co

m

Cu

rrent

Dep

artu

res:

1.

VOR

s &

ND

Bs a

re

mand

atory

(DAN

, DJ)

2.

Req

uires tight

aircraft

perfo

rman

ce to

maintain

clear of

special

use

Nng

Intern

ation

al Airp

ort

(VVNB)

Cu

rrent

SIDs

Honeyw

ell P

roprieta

ry

clear of

special

use

airspace

per SID

SIDs in

WH

ITESID

s in

WH

ITESID

s in

WH

ITESID

s in

WH

ITE

HONEYW

ELL/HUGHES

PROPRIETARY

HONEYW

ELL/HUGHES

PROPRIETARY

Ho

neyw

ell.co

m

Cu

rrent

Arrival

and

Tra

nsitio

ns:

1.

VOR

s &

ND

Bs a

re

mand

atory

(DAN

, DJ)

2.

Req

uires tight

aircraft

perfo

rman

ce to

maintain

Nng

Intern

ation

al Airp

ort

(VVNB)

Cu

rrent

STAR

s

Honeyw

ell P

roprieta

ry

perfo

rman

ce to

maintain

clear of

special

use

airspace

per STAR

HONEYW

ELL/HUGHES

PROPRIETARY

Ho

neyw

ell.co

m

Perfo

rmance Based

Navigation Benefits

Honeyw

ell P

roprieta

ry

Navigation Benefits

Nng

International Airport

VVDN

Ho

neyw

ell.co

m

Nng

Intern

ation

al Airp

ort

(VVD

N)G

BAS/G

LS App

roach

Honeyw

ell P

roprieta

ry

HO

NE

YW

ELL/H

UG

HE

S P

RO

PR

IET

AR

Y

Existing

wayp

oints

Existing

wayp

oints

sea

mle

ssly co

nn

ect

se

am

lessly

con

ne

ct

into cu

rrent

airspa

ce

into cu

rrent

airspa

ce

structu

restru

cture

GLS

Final

Appro

ach

G

LS Fin

al App

roa

ch

segm

ents

segm

ents

Ho

neyw

ell.co

m

Nng

Intern

ation

al Airp

ort

(VVD

N)RW

35L /

35R G

BAS/G

LS App

roach

Honeyw

ell P

roprieta

ryH

ON

EY

WE

LL/HU

GH

ES

PR

OP

RIE

TA

RY

Stagge

red fin

al seg

me

nts

Stagge

red fin

al seg

me

nts

allow

for futu

re

allow

for futu

re

simulta

ne

ou

s d

epe

nde

nt

simulta

ne

ou

s d

epe

nde

nt

pa

rallel app

roa

che

sp

arallel

appro

ach

es

RF

turn

to fin

al

RF

turn

to fin

al

pro

vide

s fo

r a

pre

cise

pro

vide

s fo

r a

pre

cise

path

path

HO

NE

YW

ELL/H

UG

HE

S P

RO

PR

IET

AR

Y

Ho

neyw

ell.co

m

PBN

En

route

Ben

efits B

etwee

n

Nng

& T

n S

n N

ht

Intern

ation

al Airp

orts

(VVDN

-VVTS)L

ega

cy G

rou

ndL

ega

cy G

rou

nd--

ba

sed

ba

sed N

avaid

Na

vaidR

oute

(W1)

Ro

ute (W

1)353

NM

track

mile

s353

NM

track

mile

s

Th

e Q

The

Q--R

oute

achie

ves a

21 N

M

Ro

ute a

chieve

s a

21 N

M

saving

s in

track

mile

s p

er flight

sa

vings in

track

mile

s p

er flight

versu

s th

e W

1 ro

uting.

versu

s th

e W

1 ro

uting.

This

results

in a

This

results

in a

55% red

uctio

n of

the

%

redu

ction

of th

e

ove

rall dista

nce

flow

n.

ove

rall dista

nce

flow

n.

A

3 m

inute

redu

ction

of

flying tim

e is

A

3 m

inute

redu

ction

of

flying tim

e is

realized

using

the

Qre

alized u

sing th

e Q

--Ro

ute.

Ro

ute.

This

equ

ates to

a fu

el sa

vings of

This

equ

ates to

a fu

el sa

vings of

appro

ximately

137

appro

ximately

137 lb

slb

sp

er flight

.

pe

r flight

.

Honeyw

ell P

roprieta

ryH

ON

EY

WE

LL/HU

GH

ES

PR

OP

RIE

TA

RY

appro

ximately

137

appro

ximately

137 lb

slb

sp

er flight

.

pe

r flight

.

(A320/B737)(A320/B737)

Satellite

Satellite

--ba

sedb

ased

QQ--R

oute

Ro

ute

332 N

M tra

ck

332 N

M tra

ck

mile

sm

iles

Dire

ct Q

Dire

ct Q

--Ro

uteR

oute

326 N

M tra

ck

326 N

M tra

ck

mile

sm

iles

A

direct

QA

direct

Q--ro

ute o

ver

route

ove

r

Ca

mb

odia w

ould

net

a 27

NM

C

am

bodia

wo

uld n

et a

27 N

M

saving

s in

track

mile

s fro

m a

sa

vings in

track

mile

s fro

m a

W1

routing

.W

1 ro

uting.

A

redu

ction

of 4

min

utes of

A

redu

ction

of 4

min

utes of

flying tim

e a

nd 184

flying

time

and

184 lb

slb

sof

fuel

of

fuel

saving

s p

er flight

wo

uld b

e

saving

s p

er flight

wo

uld b

e

gain

ed ve

rsus u

sing th

e W

1

gain

ed ve

rsus u

sing th

e W

1

routing

.

routing

.

HONEYW

ELL/HUGHES

PROPRIETARY

Ho

neyw

ell.co

m

Track Mile Savings

RN

AV (R

NP)

can cu

rve th

e fin

al app

roach

to b

egin o

n th

e d

ow

nw

ind leg

and

pro

vide

lateral

and

vertical

guid

ance

to th

e ru

nw

ay e

nd o

r to

a G

LS inte

rcept. This app

roach

with

a 4

nm

final

would

save

~10

.6nm

per flight

.

Time

& Dista

nce

Sa

vings

Pe

rform

an

ce B

ased N

avig

ation

Honeyw

ell P

roprieta

ryHO

NEYWELL/HUG

HES PRO

PRIETARY

Ho

neyw

ell.co

m

Track Mile Savings

A red

uctio

n of

10nm

for a

n a

verag

e aircraft

config

uring

for app

roach

save

s:

2.86

min

utes of

flight tim

e

182lbs of

fuel

27

.5 g

allons

Time

& F

uel

Sa

vings

Pe

rform

an

ce B

ased N

avig

ation

Honeyw

ell P

roprieta

ryHO

NEYWELL/HUG

HES PRO

PRIETARY

Ho

neyw

ell.co

m

The cu

rrent

arrivals co

uld b

e utilized

to p

rovid

e additio

nal

flexibilitie

s.

Exa

mple

s Includ

e:

1.

Use

RN

AV (R

NP)

with rep

eatable

curved

path

s to e

ach

runw

ay e

nd.

2.

Use

RN

AV (R

NP)

to sh

orte

n flight

tracks to

each

runw

ay e

nd.

3.

Use

RN

AV (R

NP)

to p

rovid

e n

ew

tracks to

each

runw

ay .

The cu

rrent

arrivals co

uld b

e utilized

to p

rovid

e additio

nal

flexibilitie

s.

Exa

mple

s Includ

e:

1.

Use

RN

AV (R

NP)

with rep

eatable

curved

path

s to e

ach

runw

ay e

nd.

2.

Use

RN

AV (R

NP)

to sh

orte

n flight

tracks to

each

runw

ay e

nd.

3.

Use

RN

AV (R

NP)

to p

rovid

e n

ew

tracks to

each

runw

ay .

Stabilized App

roach

esP

erfo

rma

nce

Based

Na

vigatio

n

Honeyw

ell P

roprieta

ryHO

NEYWELL/HUG

HES PRO

PRIETARY

Ho

neyw

ell.co

m

Current

Infra

structure

Honeyw

ell P

roprieta

ry

Infra

structure

Tn Sn Nht

International Airport

VVTS

HUGH

ES PRO

PRIETAR

Y

Ho

neyw

ell.co

m

Curre

nt O

peratio

nal

Enviro

nm

ent

:

Runw

ays:

07L/25R -10

,000ft x

148ft

07R/25L -12

,467ft x

148ft

Tn

S

n N

ht

Intern

ation

al Airp

ort

(VVTS)

Cu

rrent

Op

eratio

ns

Honeyw

ell P

roprieta

ry

Appro

ach

es:

ILS

DM

E 25L

, 25R

VO

R D

ME

07L, 07R

, 25L

, 25R

N

DB

07L, 07R

, 25L

, 25R

SIDs &

STARs:

1 STAR

(path

based)

3 SID

s (path

based)

HO

NE

YW

ELL/H

UG

HE

S P

RO

PR

IET

AR

Y

Ho

neyw

ell.co

m

Curre

nt D

epartu

res:

1.

VOR

s & N

DB

s are

mand

atory

(TSN, VTV

, G

N, SG

, AC)

2.

Req

uire tight

aircraft

perfo

rmance

to m

aintain cle

ar

of p

rohibited, d

ang

er a

nd

Tn

S

n N

ht

Intern

ation

al Airp

ort

(VVTS)

Cu

rrent

Op

eratio

ns

Honeyw

ell P

roprieta

ry

of p

rohibited, d

ang

er a

nd

restricted

are

as a

nd p

erfo

rm

per SID

SIDs in

WH

ITESID

s in

WH

ITESID

s in

WH

ITESID

s in

WH

ITE

HONEYW

ELL/HUGHES

PROPRIETARY

Ho

neyw

ell.co

m

Cu

rrent

Arrival

and

Tra

nsitio

ns:

1.

VOR

s &

ND

Bs a

re

mand

atory

(TSN, AC)

Tn

S

n N

ht

Intern

ation

al Airp

ort

(VVTS)

Cu

rrent

Op

eratio

ns

Honeyw

ell P

roprieta

ry

HONEYW

ELL/HUGHES

PROPRIETARY

Ho

neyw

ell.co

m

Perfo

rmance Based

Navigation Benefits

Tn S

n Nht

Honeyw

ell P

roprieta

ry

Navigation Benefits

Tn Sn Nht

International Airport

VVTS

Ho

neyw

ell.co

m

Tn

S

n N

ht

Intern

ation

al Airp

ort

(VVTS)

Multiple

Tra

nsitio

n O

PD

Honeyw

ell P

roprieta

ry

Optim

ize p

rofile d

esce

nts apply ve

rtical fe

ature

s to cu

rrent

STARs th

at h

ave

dem

onstrated

benefits in

pre

vious

imple

mentatio

ns:

1.

~600lbs of

fuel

saving

s per flight

2.

Red

uced

ATC/Pilot co

mm

unicatio

ns by

up to

70%3.

Red

uced

Noise

impacts fo

r th

e co

mm

unitie

s4.

Flight tim

e red

uctio

ns of

~2

min

s per flight

5.

Flight Idle

desce

nts from

cruise flight

to sh

ort

final

Optim

ize p

rofile d

esce

nts apply ve

rtical fe

ature

s to cu

rrent

STARs th

at h

ave

dem

onstrated

benefits in

pre

vious

imple

mentatio

ns:

1.

~600lbs of

fuel

saving

s per flight

2.

Red

uced

ATC/Pilot co

mm

unicatio

ns by

up to

70%3.

Red

uced

Noise

impacts fo

r th

e co

mm

unitie

s4.

Flight tim

e red

uctio

ns of

~2

min

s per flight

5.

Flight Idle

desce

nts from

cruise flight

to sh

ort

final

HONEYW

ELL/HUGHES

PROPRIETARY

Ho

neyw

ell.co

m

Tn

S

n N

ht

Intern

ation

al Airp

ort(VVTS)

RF

Tra

nsitio

ns

4sm

SAPEN

Honeyw

ell P

roprieta

ry

RN

AV p

aths fro

m cu

rrent

arrivals co

uld se

rve

multiple

runw

ays, o

r p

rovid

e m

ultiple tra

nsitio

ns to

the sa

me ru

nw

ay

RN

AV p

aths fro

m cu

rrent

arrivals co

uld se

rve

multiple

runw

ays, o

r p

rovid

e m

ultiple tra

nsitio

ns to

the sa

me ru

nw

ayVTV

VOR

LANHI

RN

AV (R

NP)

can cu

rve th

e fin

al app

roach

to b

egin o

n th

e d

ow

nwind

leg a

nd p

rovid

e

lateral

and

vertical

guid

ance

to th

e ru

nw

ay

end

or to

a G

LS inte

rcept. This app

roach

with a

4nm

final

would

save

~10

.6nm

per

flight.

HONEYW

ELL/HUGHES

PROPRIETARY

Ho

neyw

ell.co

m

Tn

S

n N

ht

Intern

ation

al Airp

ort

(VVTS)

GB

AS/GLS

Appro

ach

4.0

NM

GLS

Final

4

.0 N

M G

LS Fin

al

Appro

ach

segm

ent

App

roa

ch seg

me

nt

Honeyw

ell P

roprieta

ry

Existing

IAF w

aypoints

E

xisting IAF

wayp

oints

sea

mle

ssly co

nn

ect

se

am

lessly

con

ne

ct

into cu

rrent

airspa

ce

into cu

rrent

airspa

ce

structu

restru

cture

Airsp

ace

Airsp

ace

Ch

alleng

ed

Ch

alleng

ed

En

viron

me

ntE

nviro

nm

ent

S

ma

rtPath

Pre

cision

S

ma

rtPath

Pre

cision

Final

La

nding

Final

La

nding

minim

um

sm

inimu

ms

C

oupled

Auto

matic

C

oupled

Auto

matic

La

ndingL

anding

HO

NE

YW

ELL/H

UG

HE

S P

RO

PR

IET

AR

Y

Ho

neyw

ell.co

m

Tn

S

n N

ht

Intern

ation

al Airp

ort

(VVTS)

RW

25L /

25R G

BAS/G

LS App

roach

RF

turn

to fin

al

RF

turn

to fin

al

pro

vide

s fo

r a

pre

cise

pro

vide

s fo

r a

pre

cise

path

avoiding

p

ath a

voiding

Honeyw

ell P

roprieta

ryH

ON

EY

WE

LL/HU

GH

ES

PR

OP

RIE

TA

RY

Prohibited

Airspa

ceP

rohibited Airsp

ace

path

avoiding

p

ath a

voiding

prohibited

airspa

cep

rohibited airsp

ace

GBAS/G

LS with

RN

P

GBAS/G

LS with

RN

P

fusio

n p

rovid

es:

fusio

n p

rovid

es:

Im

pro

ved a

ccess

Impro

ved a

ccess

In

creased

safetyIn

creased

safety

Low

er M

inimum

sLow

er M

inimum

s

HO

NE

YW

ELL/H

UG

HE

S P

RO

PR

IET

AR

Y

Ho

neyw

ell.co

m

Fro

m th

e O

ptimized

Profile

Desce

nts, n

ew

wayp

oints can b

e add

ed to

allow

for m

ultiple

appro

ach

transitio

ns to

a single

or m

ultiple ru

nw

ays. This p

rovid

es g

reate

r fle

xibility a

nd

predictability

for ATC

and

Pilots.

Fro

m th

e O

ptimized

Profile

Desce

nts, n

ew

wayp

oints can b

e add

ed to

allow

for m

ultiple

appro

ach

transitio

ns to

a single

or m

ultiple ru

nw

ays. This p

rovid

es g

reate

r fle

xibility a

nd

predictability

for ATC

and

Pilots.

Tn

S

n N

ht

Intern

ation

al Airp

ort

(VVTS)

Optim

ized P

rofile D

ecent

Honeyw

ell P

roprieta

ry

HONEYW

ELL/HUGHES

PROPRIETARY

Ho

neyw

ell.co

m

RF

turn

transitio

ns ca

n

pro

vided

defin

ed

separatio

n b

etween

airspace

or airp

orts

Tn

S

n N

ht

Intern

ation

al Airp

ort

(VVTS)

Use

of R

F T

ran

sition

s

Honeyw

ell P

roprieta

ry

The

curre

nt a

rrivals co

uld b

e utilized

to p

rovid

e additio

nal

flexibilitie

s

to Ta

nso

nnh

at.

Exa

mple

s In

clude

:

1.

Use

RN

AV (R

NP)

with rep

eatable

curved

path

s to

ea

ch

run

way

end

.

The

curre

nt a

rrivals co

uld b

e utilized

to p

rovid

e additio

nal

flexibilitie

s

to Ta

nso

nnh

at.

Exa

mple

s In

clude

:

1.

Use

RN

AV (R

NP)

with rep

eatable

curved

path

s to

ea

ch

run

way

end

.

HONEYW

ELL/HUGHES

PROPRIETARY

Ho

neyw

ell.co

m

RN

AV App

roach

from

the d

ow

nw

ind

Tn

S

n N

ht

Intern

ation

al Airp

ort

(VVTS)

RW 25

L/R T

ran

sition

s

Honeyw

ell P

roprieta

ry

HONEYW

ELL/HUGHES

PROPRIETARY

Ho

neyw

ell.co

m

SAPEN

Tn

S

n N

ht

Intern

ation

al Airp

ort

(VVTS)

Use

of R

F T

ran

sition

s

Honeyw

ell P

roprieta

ry

RN

AV p

aths fro

m cu

rrent

arrivals co

uld se

rve

multiple

runw

ays, o

r p

rovid

e m

ultiple tra

nsitio

ns to

the sa

me ru

nw

ay

RN

AV p

aths fro

m cu

rrent

arrivals co

uld se

rve

multiple

runw

ays, o

r p

rovid

e m

ultiple tra

nsitio

ns to

the sa

me ru

nw

ay

VTV VO

R

LANHI

HONEYW

ELL/HUGHES

PROPRIETARY

Ho

neyw

ell.co

m

The cu

rrent

arrivals co

uld b

e utilized

to p

rovid

e additio

nal

flexibilitie

s to Ta

nso

nnh

at.

Exa

mple

s Includ

e:

1.

Use

RN

AV (R

NP)

with rep

eatable

curved

path

s to e

ach

runw

ay e

nd.

2.

Use

RN

AV (R

NP)

to sh

orte

n flight

tracks to

each

runw

ay e

nd.

The cu

rrent

arrivals co

uld b

e utilized

to p

rovid

e additio

nal

flexibilitie

s to Ta

nso

nnh

at.

Exa

mple

s Includ

e:

1.

Use

RN

AV (R

NP)

with rep

eatable

curved

path

s to e

ach

runw

ay e

nd.

2.

Use

RN

AV (R

NP)

to sh

orte

n flight

tracks to

each

runw

ay e

nd.

Tn

S

n N

ht

Intern

ation

al Airp

ort

(VVTS)

Red

uced

Track

Miles

Honeyw

ell P

roprieta

ry

HONEYW

ELL/HUGHES

PROPRIETARY

Ho

neyw

ell.co

m

Track Mile Savings

RN

AV (R

NP)

can cu

rve th

e fin

al app

roach

to b

egin o

n th

e d

ow

nw

ind leg

and

pro

vide

lateral

and

vertical

guid

ance

to th

e ru

nw

ay e

nd o

r to

a G

LS inte

rcept. A

GNSS

appro

ach

with a

4nm

final

would

save

~10

.6nm

per flight

.

Tn

S

n N

ht

Intern

ation

al Airp

ort

(VVTS)

Red

uced

En

viron

mental

Imp

act

Honeyw

ell P

roprieta

ry

HONEYW

ELL/HUGHES

PROPRIETARY

Ho

neyw

ell.co

m

Track Mile Savings

A red

uctio

n of

10nm

for a

n a

verag

e aircraft

config

uring

for app

roach

save

s:

2.86

min

utes of

flight tim

e

182lbs of

fuel

27

.5 g

allons

Tn

S

n N

ht

Intern

ation

al Airp

ort

(VVTS)

Real

Saving

s

Honeyw

ell P

roprieta

ry

HONEYW

ELL/HUGHES

PROPRIETARY

Ho

neyw

ell.co

m

Le

veraging

PBN

for E

nro

uteB

en

efitsP

otientalQ

-Ro

ute fo

r Vietn

am

Leg

acy

Gro

und

Leg

acy

Gro

und

--ba

sed

ba

sed

Na

vaidN

avaid

Ro

ute (W

1)R

oute

(W1)

690 N

M tra

ck m

iles

690 N

M tra

ck m

iles

Th

e Q

The

Q--R

oute

achie

ves a

31 N

M sa

vings in

R

oute

achie

ves a

31 N

M sa

vings in

track

mile

s p

er flight

versu

s th

e W

1 ro

uting.

track

mile

s p

er flight

versu

s th

e W

1 ro

uting.

This

results

in a

5% red

uctio

n of

the

ove

rall

This re

sults in

a 5%

redu

ction

of th

e o

verall

distan

ce flo

wn

.dista

nce

flow

n.

Dire

ct Q

Dire

ct Q

--Ro

uteR

oute

623 N

M tra

ck

623 N

M tra

ck

mile

sm

iles

Honeyw

ell P

roprieta

ry

distan

ce flo

wn

.dista

nce

flow

n.

A

4 m

inute

redu

ction

of

flying tim

e is

realized

A

4 m

inute

redu

ction

of

flying tim

e is

realized

using

the

Qu

sing th

e Q

--Ro

ute.

Ro

ute.

This

equ

ates to

a fu

el sa

vings of

This

equ

ates to

a fu

el sa

vings of

appro

ximately

250

appro

ximately

250 lb

slb

sp

er flight

. (A320/B737)

pe

r flight

. (A320/B737)

Satellite

Satellite

--ba

sedb

ased

QQ--R

oute

Ro

ute

658 N

M tra

ck

658 N

M tra

ck

mile

sm

iles

A

direct

QA

direct

Q--ro

ute o

ver L

ao

s a

nd C

am

bodia

ro

ute o

ver L

ao

s a

nd C

am

bodia

wo

uld n

et a

67 N

M sa

vings in

track

mile

s

wo

uld n

et a

67 N

M sa

vings in

track

mile

s

from

a W

1 ro

uting .

from

a W

1 ro

uting .

A

redu

ction

of 8

min

utes of

flying tim

e a

nd

A red

uctio

n of

8 m

inute

s of

flying tim

e a

nd

450

450 lb

slb

sof

fuel

saving

s p

er flight

wo

uld b

e

of fu

el sa

vings p

er flight

wo

uld b

e

gain

ed ve

rsus u

sing th

e W

1 ro

uting.

gain

ed ve

rsus u

sing th

e W

1 ro

uting.

HONEYW

ELL/HUGHES

PROPRIETARY

Ho

neyw

ell.co

m

Gro

und

Based

Aug

mentatio

n Syste

m (G

BAS)

1.

4.

Why a

ugm

ent

GPS

for p

recisio

n

appro

ach?

How

do w

e

aug

ment

GPS

for

pre

cision

appro

ach?H

oneyw

ell P

roprieta

ry

5.

3.

2.

2.

2.

2.

65

Ho

neyw

ell.co

m

Sm

artP

ath G

BAS

Valu

e S

um

mary

E

nha

nced

Safety

:S

ma

rtPath

Imp

roves

Safety

FAA

Certificatio

n P

edigree

Sig

nal

Stability (im

mu

ne to

sign

al b

end

s inh

ere

nt in

ILS)

Wake

Vo

rtex M

itigatio

n

Cu

stom

izable G

lide P

aths / App

roach

es

In

creased

Airpo

rt C

apacity

:S

ma

rtPath

Unlo

cks C

apacity

O

ffers

precisio

n app

roach

wh

ere

ILS ca

nn

ot d

ue to

geog

raphy

En

ables fle

xible app

roach

es (26)

, im

pro

ved acc

uracy

vers

us ILS

Honeyw

ell P

roprieta

ry

Airp

ort

ben

efits fro

m in

creased

reve

nu

e (la

ndings fees

, co

ncessio

ns, etc

.) a

nd co

st

avoid

an

ce (cap

acity in

crease

w/o

adding ru

nw

ays)

L

ow

er Life

-cycle C

ost:S

ma

rtPath

is M

ore

Co

st Efficie

nt Th

an

ILS

On

e S

martP

athG

BAS Statio

n se

rves all

run

ways

, initial

acquisitio

n co

st is

low

er

L

ow

er m

ainten

an

ce co

sts / L

ow

er flight

insp

ection

costs

E

nviro

nm

entally

Frie

ndly: R

edu

ced N

oise /

Sho

rter R

outes

V

ariable

glide slop

es, RNAV/RNP

to G

LS fin

als

Airline fu

el &

em

ission

saving

s, in

creased

sched

ule fle

xibility, a

void n

oise violatio

ns

Airp

orts

increased

capacity

and

sched

ule fle

xibility, im

pro

ved co

mm

unity

relation

s

66

Ho

neyw

ell.co

m

Wh

at is

a S

martP

ath G

BAS?

Ho

neyw

ells S

ma

rtPath

is th

e first

, a

nd o

nly, FAA

-appro

ved C

AT-I

GBAS

It w

ill p

rovid

e C

AT I/II/III

pre

cision

appro

ach

and

landing

capability

Honeyw

ell P

roprieta

ry

Integ

rity M

onito

ring Alg

orith

ms

FAA

-certified

DO-278

Softw

are

M

ainten

an

ce D

ata T

erm

inal

(MD

T)

Re

mote

Satellite

Meas

ure

ment

Unit

(RSMU)

Differe

ntial G

PS (DG

PS) C

ontrol

&

VHF

Data

Bro

adc

ast (VD

B) C

abinet

Air T

raffic C

ontrol

Status

Unit

(ATSU)

VHF

Data

Bro

adcast

(VDB)

Ante

nn

a

G

PS R

eceiver p

ackaged

in a

n

en

viron

mentally

protectiv

e

en

closu

re

Multi

-path

Limiting

Ante

nn

a

Req

uires site

su

rvey

and

placem

ent

again

st siting/in

stallation

crite

ria

SLS

Status P

an

el in

stalled in

Air T

raffic C

ontrol

To

wer o

r

other lo

cation

67

Ho

neyw

ell.co

m

GLS

Uses

Existing

Aircraft

Architectu

re

Red

uces

Training

Co

sts &

Maxim

izes O

peratio

nal

Ben

efits

ILS

look

alike

Glid

eslop

e

Localize

r

Honeyw

ell P

roprieta

ryH

ON

EY

WE

LL -C

ON

FID

EN

TIA

L

68

GLS

GPS

Landing

System

ILS

Instru

ment

Landing

System

Ho

neyw

ell.co

m

Flexible

Appro

aches

& G

lidep

aths

Addition

al G

BAS

Be

nefits

Honeyw

ell P

roprieta

ry69

No

ILS C

learzo

nes

Req

uired

Ho

neyw

ell.co

m

RNP cu

rved

approach

Variable

GLS

segm

ents

(as close

as 4NM

from

landing

thresh

old)

-R

NAV/R

NP

for c

urved

segm

ents/G

LS

for fin

al app

roach

segm

ent

-ILS

: stabilized

on

the

localize

r at

10

NM

or m

ore

-G

LS: m

ultiple fin

al app

roach

segm

ents

as clo

se as

4NM

-R

NP

minim

um

s

250

RN

AV/RN

P &

GLS

Fu

sion

Maxim

izes O

peratio

nal

Ben

efits

Honeyw

ell P

roprieta

ry

-R

NP

minim

um

s

250

-R

NP

is a

no

n-p

recision

appro

ach-

GLS

minim

um

s 200

C

at I

-C

at II/III

2012-2014

-G

LS is

precisio

n app

roach

-R

NP

.3N

M: R

NP/AR

-G

LS fin

al: n

o R

NP/AR

-R

NAV/G

LS fastest/easiest

imple

me

ntation

HO

NE

YW

ELL -

CO

NF

IDE

NT

IAL

70

Ho

neyw

ell.co

m

GLS

Allo

ws fo

r P

rogra

mm

able To

uchd

ow

n P

oints a

nd G

SA

n ILS

system

pro

vides a

single fixed

vertical

path

. G

BAS p

rovid

es a

variable

pre

cision

path

that

allow

s an airp

ort

to p

erfo

rm ro

utine m

aintenance

on a

ny ru

nw

ay with

out

unnece

ssary

runw

ay clo

sure

while supp

orting

traffic separatio

n.

An ILS

system

pro

vides a

single fixed

vertical

path

. G

BAS p

rovid

es a

variable

pre

cision

path

that

allow

s an airp

ort

to p

erfo

rm ro

utine m

aintenance

on a

ny ru

nw

ay with

out

unnece

ssary

runw

ay clo

sure

while supp

orting

traffic separatio

n.

Honeyw

ell P

roprieta

ry

ILS

Tou

chdo

wn

Point

GLS

Prog

ram

mable

Tou

chdo

wn

Point

Ho

neyw

ell.co

m

GLS

Allo

ws fo

r P

rogra

mm

able To

uchd

ow

n P

oints a

nd P

athH

on

eyw

ell

Ho

ney

well

Sm

artP

athS

martP

athSyste

mSyste

m

GLS

Cap

abilities: D

efinable

Tou

chdo

wn

Point

GLS

Cap

abilities: D

efinable

Tou

chdo

wn

Point

An ILS

system

pro

vides a

single d

efined

vertical

path

that

place

s the aircraft

at th

e sa

me

point

on th

e ru

nw

ay e

ach

landing

. H

ow

eve

r, S

martP

athG

LS app

roach

es ca

n p

rovid

e

variable

geom

etric path

s and

multiple

touchd

ow

n p

oints to th

e sa

me ru

nw

ay.

Ho

ney

well

H

on

eyw

ell S

martP

athS

martP

athSyste

mSyste

m

GLS

Cap

abilities: D

efinable

Tou

chdo

wn

Point

GLS

Cap

abilities: D

efinable

Tou

chdo

wn

Point

An ILS

system

pro

vides a

single d

efined

vertical

path

that

place

s the aircraft

at th

e sa

me

point

on th

e ru

nw

ay e

ach

landing

. H

ow

eve

r, S

martP

athG

LS app

roach

es ca

n p

rovid

e

variable

geom

etric path

s and

multiple

touchd

ow

n p

oints to th

e sa

me ru

nw

ay.

Honeyw

ell P

roprieta

ryHUG

HES

PROPR

IETARY

GLS

G

LS

Prog

ram

mable

P

rogra

mm

able

Tou

chdo

wn

To

uchd

ow

n

Point

Point

GLS

G

LS

Prog

ram

mable

P

rogra

mm

able

Tou

chdo

wn

To

uchd

ow

n

Point

Point

GLS

G

LS

Prog

ram

mable

P

rogra

mm

able

Tou

chdo

wn

To

uchd

ow

n

Point

Point

ILS To

uch

do

wn

Po

int

Ho

neyw

ell.co

m

GB

AS G

uida

nce

Imple

me

ntation

Pilot

MM

R GPS

Ante

nnaA

utopil

Cock

pitD

isplays

AircraftAircraf

tS

urfa

cG

PS e

rror co

rrectio

ns,

A-380

GLS

Optio

nA

-320

GLS

option

A-340

GLS

option

A-330

GLS

option

A-350

GLS

Ba

sic

737NG

GLS

forw

ard

fit,

retrofit787

GLS

ba

sic747

-8

GLS

ba

sic

Honeyw

ell P

roprieta

ry

GPS

Ante

nna

DGPS

Com

pute

s

Diffe

rential

Corre

ctions

Pro

vides Integ

rityC

heck

Pro

vides App

roach

Coordin

ates

Diffe

rential

Co

rrectio

ns,

Integrity

Status a

ndApp

roa

ch C

oo

rdinate

s

Tra

nsm

itter

Encod

er

Decod

er

Receive

r

Data

Bro

adca

stM

onito

r

Bro

adca

st Info

rmatio

n

DATALIN

K

VHF

Data

Bro

adca

st (VD

B)Local

Gro

und

Facility

PilotInte

rface

Autopilot

Surfa

ces

DGPS

Diffe

rential

GPS

MM

R

Multi

-Mod

e R

eceive

r (G

PS, VD

B, ILS

,

etc)VD

B

VHF

Data

Bro

adca

st (Link

to aircraft)

GPS

erro

r co

rrectio

ns,

integrity

, AN

D p

ath

points

73

Ho

neyw

ell.co

m

GB

AS C

ertificatio

n Tim

eline

Timelin

e

201112

1314

1516

Ho

neyw

ellS

ma

rtPath

CAT

-I(2009)

ICAO

GAST

-DR

equire

ments

CAT

-IIIC

ertificatio

nFAA

CAT

-IIIP

rocu

rem

ent

Multi

-GNSS

2020+

CAT

-III (G

AST-D)

De

velopm

ent

FAA

CA

T-III Prototype S

oftware (G

round)

CAT

-IIw/Io

no

Mo

nitor

Honeyw

ell P

roprieta

ry

Req

uirem

ents

(2010)

Germ

any

Australia

Gro

und

System

Certificatio

ns

USA

Leg

end

Com

plete

Planned

De

velopm

ent

GB

AS: C

lear FA

A F

und

ed P

ath to

CA

T-III

Ce

rtification

74

Sm

artP

ath C

ertificatio

n

Ce

rtification

Pro

cessP

rocess

BSD1Slide 75

BSD1

Lets m

ove th

is sectio

n rig

ht a

fter th

e sa

les se

ction and before th

e RFI a

nd io

no se

ctions...

- can w

e add a slid

e detailin

g FAA in

veste

ments th

at a

re cu

rrent a

nd fu

ture m

onies th

at w

e w

ill rece

ive and w

hat th

e fu

ndings a

re use

dfor?

- lets a

dd an arro

w fo

r HON CATIII S

TRAP in

vestm

ent to

timelin

e slid

e

e362453, 1

1/27/2011

Ho

neyw

ell.co

m

CAT

-I C

ertificatio

n Ph

ase

s

Syste

m D

esig

n App

roval

(SDA)

Ma

nufa

cture

r

Gro

und

station syste

m d

esig

n m

eets req

uirem

ents

D

evelop

ed to

approp

riate d

esig

n a

ssura

nce

levels

F

acility

Appro

val

Ow

ne

r/ANSP/Airpo

rt

Gro

und

station in

stalled

Flight te

st co

mpleted

, app

roach

flyability, VD

B co

verag

e

Honeyw

ell P

roprieta

ry

VD

B =

VHF

Data

Bro

adca

st (i

.e. g

rou

nd-to

-airbo

rne

sign

al in

spa

ce)

Mainte

nance

tech

nicians train

ed, ce

rtified

ANSP =

Air N

avig

ation

Se

rvice P

rovid

er (e

.g. FAA

in th

e U

.S.)

S

ervice

Appro

val

Op

erato

r/Airline

Aircraft

equipp

ed

Pilot, cre

ws train

ed

SmartP

ath: W

orld

s First, F

AA-Approved and Intl C

AT-I G

BAS

Ho

neyw

ell.co

m

Sm

artP

ath C

ertificatio

ns

First

To C

ertify:

Bre

men G

erm

any;

Germ

an Typ

e App

roval

received

30 N

ov

1stInte

rnatio

nal

Certificatio

n of

Sm

artP

athSyd

ney A

ustralia

Q1 2012

New

ark N

ew

Jersey Q

2 2012

Honeyw

ell P

roprieta

ry

New

ark N

ew

Jersey Q

2 2012

Malag

a Sp

ain Q

4 2012

Bra

zil Q

2 2013

Ho

neyw

ell.co

m

Sum

mary/D

iscussio

n

The

GBAS

Era

is h

ere

Air

Na

vigatio

n S

ervice

Pro

vide

rs (e

.g. FAA

, A

sA, D

FS, AEN

A),

OEM

s, a

nd Airlin

es re

cognize

the

Valu

e P

ropo

sition

A

single S

ma

rtPath

at a

n airp

ort

P

rovid

es p

recisio

n app

roa

ch to

all ru

nw

ay e

nds

R

eplace

s m

ultiple ILS

s

En

ables n

um

ero

us additio

nal

air op

eratio

ns

P

rovid

es p

recisio

n app

roa

ch w

he

re a

n ILS

can

not

Honeyw

ell P

roprieta

ry

P

rovid

es p

recisio

n app

roa

ch w

he

re a

n ILS

can

not

Syste

m siting

, op

eratio

n, a

nd m

ainten

an

ce ve

ry efficie

nt

Sm

artP

ath re

ceived FAA

appro

val

Gro

wth

to C

at II/III

Airb

orn

e eq

uipag

e in

crea

sing

G

lobal

GBAS/G

LS re

alization

is a

ccelerating

-n

ow

is th

e tim

e to

inco

rpo

rate G

BAS into

you

r pla

ns

Ho

ney

well

can

pro

vide

a total

Pe

rform

an

ce B

ased N

avig

ation

solution

pro

viding valu

e to

ANSP

s, airlin

es, a

nd th

e flying

public