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Characteristic speeds

How to use maneuvering speeds F, S, green dot ?

Presented by Yves LEMELLE

Director of A320/A330/A340 Flight Operational Standards

(2)

Introduction

May I fly below maneuvering speed ?

How much roll maneuverability when

below maneuvering speed?

How much Flap retraction for takeoff and

Go-Around?

Reduce speed

180 kt

(3)

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

Contents

Definitions & Principles

1

Maneuvering speeds - Takeoff & Go-Around

2

Maneuvering speeds - Approach

3

Maneuvering capability

4

(4)

Contents

Definitions & Principles

1

Maneuvering speeds - Takeoff & Go-Around

2

Maneuvering speeds - Approach

3

Maneuvering capability

(5)

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

Definitions - Vls

Lowest selectable speed

Represents minimum regulatory speeds depending on

flight phase (can be VMCA, VMCL or Vs1g limited)

Provides appropriate margin versus buffet at high

altitude

Provides appropriate bank angle maneuverability

(defined by regulation) in a stabilised turn

Vls

(6)

Definitions – F speed

Takeoff: Minimum speed for Flap retraction

Approach: Target speed for CONF 2 and 3

Also used as maneuvering speed

Displayed in CONF 2 and 3

F

speed

(7)

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

Definitions – S speed

Takeoff: Minimum speed for slats retraction

Approach: Target speed for CONF1

Also used as maneuvering speed

Displayed in CONF 1 and 1+F

S

speed

(8)

Definitions – GREEN DOT speed

Engine-out operating speed in clean CONF

Best lift to drag ratio speed

GREEN

DOT

speed

(9)

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

Principle of characteristics speeds

Pilot uses Characteristics speeds displayed on PFD:

As limits, to fly between Vls and Vmax (VLE, VFE, VMO, MMO)

As target maneuvering speed (F, S, Green Dot)

Automatisms use characteristics speeds for:

Predictions, or

Target speeds

Limits

(10)

Contents

Definitions & Principles

1

Maneuvering speeds - Takeoff & Go-Around

2

Maneuvering speeds - Approach

3

Maneuvering capability

(11)

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

Maneuvering speeds -

Takeoff

To assist pilots

Minimum speed to retract Flaps

while aircraft is accelerating.

At F speed: Select FLAPS 1

For CONF 3 takeoff:

select FLAPS 1 directly

Speed remains above Vls of CONF 1+F and below VFE

At S speed: Select FLAPS 0

(12)

Maneuvering speeds -

Takeoff

Takeoff at heavy weight:

Do not delay FLAPS 0 selection above S speed

=> prevents possible momentary VFE OVERSPEED warning

In CONF 1+F: S speed could be close to VFE

If FLAPS 0 selected above Flap autoretraction

speed (210 Kts on this example):

Possible VFE OVERSPEED warning if rapid

aircraft acceleration

(13)

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

Go Around below MLW

Maneuvering speeds -

Go-Around below MLW

At F select directly FLAPS 1 (as for takeoff)

Retract one step Flaps:

If LDG FLAPS FULL =>

Go-Around FLAPS 3

(14)

Why retract one step flaps only?

Maneuvering speeds -

Go-Around below MLW

Meets approach climb gradient requirements

Why not retract 2 steps flaps?

(Landing CONF3 – Go-Around CONF 1+F)

Would provide an approach climb performance better

than the minimum requirement

(15)

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

Maneuvering speeds –

Go-Around in overweight

landing

Conf FULL for landing

Retract one step Flaps for Go Around

15

(16)

Maneuvering speeds –

Go-Around in overweight

landing

Conf FULL for landing

Retract one step Flaps for Go Around

(17)

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

Maneuvering speeds –

Go-Around in overweight

landing

17

• If approach climb gradient performance is not met:

LDG

CONF 3

FLAPS

Retract 2 steps

Conf 3 for landing to get sufficient climb gradient performance in Go

Around

Retract 2 steps

for Go-Around:

To achieve the required climb gradient performance

Meets regulatory requirement of stall speed ratio between

landing and go-around configuration

Could result to slightly fly temporarily

below Vls after CONF 1+F selection.

(18)

Contents

Definitions & Principles

1

Maneuvering speeds - Takeoff & Go-Around

2

Maneuvering speeds - Approach

3

Maneuvering capability

(19)

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

Maneuvering speeds -

Approach

CONF 1 selection

S

F

F

Vapp

Managed Speed for approach

CONF 2 selection

CONF 3 selection

CONF FULL

selection

Green Dot

Speed target

Approach phase activation

Clean CONF

A/THR automatically decelerates the aircraft towards

maneuvering speed of selected CONF

A/THR does not allow the

speed to go below current

maneuvering speed

(20)

Maneuvering speeds - Approach

For Flap extension:

IAS must be below VFE next, but may be

above maneuvering speed.

Page 20

Recommended

(as per FCTM)

:

Next flap

config at maneuvering speed +10 kts:

To limit slats/flaps fatigue

(21)

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

Maneuvering speeds - Approach

Flap maneuvering speeds are recommended to fly the

aircraft in a given flaps configuration for:

Performance & fuel efficiency:

Comfort in cabin:

Holding pattern during initial approach:

Keep Clean CONF and fly Green Dot (best lift/drag ratio

)

Green Dot – Clean CONF

S - CONF 1

F- CONF 2

result in reasonable pitch attitudes (typically 5°)

(22)

Maneuvering speeds -

Approach

Flap maneuvering speeds are recommended to fly the

aircraft in a given flaps configuration for:

Comfort in aircraft maneuver:

• Green Dot, S, F are comfortable

• Particularly in turbulent conditions,or

• For turns at high bank angle

Flap maneuvering speeds are not limitations:

It is safe to fly between VLS and VMAX (VMO, VLE, VFE) :

The required aerodynamic margin is properly ensured

(23)

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

Contents

Definitions & Principles

1

Maneuvering speeds - Takeoff & Go-Around

2

Maneuvering speeds - Approach

3

Maneuvering capability

4

(24)

Maneuvering capability

(25)

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

Maneuvering capability

At V2, one engine out:

Stabilized turn at 30° bank before

alpha max

At V2 + 10, all engines operative:

Stabilized turn at 40° before

alpha floor

At Green Dot:

Stabilized turn at 45° bank before

alpha prot

At Vls

(final takeoff up to landing)

:

Stabilized turn at 40° bank before

alpha floor

(26)

Can I fly below Maneuvering speeds?

General rule: Fly approach maneuvers at the maneuvering

speed minimum

However if ATC speed constraint:

Selected speed

Possible to fly below maneuvering speed down to VLS. It enables

standard maneuvers:

Margin versus Valpha prot is reduced:

Margin could become small

in turbulent conditions, or with high

bank angle.

If such conditions are anticipated,

consider CONF change

Resume to managed speed when out of ATC constraint

(27)

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

Can I fly below Maneuvering speeds?

Example of pilot’s judgement:

Intermediate approach:

ATC speed restriction for significant

time:

If speed slightly lower than Flap

Maneuvering Speed:

May be advisable to keep

current Conf

For fuel efficiency

Maintain 180 kt

(28)

Conclusion

Maneuvering speeds are comfortable

Allowed to fly below maneuvering speed:

Pilot’s judgement according to anticipated maneuvers and

turbulence

Understand the aircraft: Tight turn close to Vls may activate

protections

Go Around:

Retract one step Flaps

(29)

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

© 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.

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