Airbus A320 SOP 08cNPA Approachselected

Citation preview

PF PRECISION APPROACH PNF (SELECTED) NON

Initial APP

Final APP

Interm. APP

FAF

IAF

D

MDA/H

FLYING REF : TRACK/FPA (FPD) A320 - Version 03a

PF

PNF 1.a. INITIAL APPROACH

SEAT BELTS..…………………...…………..ON/AUTO

ENG MODE sel .....……………...….…AS RQRD NAV ACCURACY .....…………….....…MONITOR

When cleared to 3700 ft : DESCENT .....……………………………....…INITIATE

FMA BARO REF : QNH APPROACH C/L VAPP SPEED CSTR AT FAF…………..INSERT

 LS P/B is OFF except for LOC only approaches.

PF

PNF 1.b. INITIAL APPROACH

When ATC gives radar vector HDG ……………………………………………SELECT

FMA Approx 15 NM from touchdown : APPR PHASE……………………………....ACTIVATE POSITIONING……………………………....MONITOR MANAGED SPEED……………………………CHECK SPEEDBRAKES…………………………….AS RQRD ND MODE RANGE………………………….AS RQRD

ND MODE RANGE……………………… AS RQRD

 Manual Approach phase activation on the PERF page APPR phase

NO AUTOACTIVATION :

 For Lateral positioning properly monitor F-PLN sequencing  For Vertical positioning : Use the Energy Circle

D

PF

PNF 2. INTERMEDIATE APPROACH

RADAR TILT........……………...………...ADJUST When cleared for approach : TRK/FPA………………………………………SET

FMA FLAPS 1

At green dot speed below VFE next : DECEL TOWARDS S SPEED..……..…CHECK

TCAS……………………………………TA or TA/RA

FLAPS 2

At S speed, below VFE next : DECEL TOWARDS F SPEED………….CHECK When FLAPS 2 :

GEAR DOWN ECAM WHEEL PAGE……………………...CHECK GROUND SPOILERS………………………….ARM AUTO BRAKE……………………………CONFIRM

When L/G down, below VFE next When FLAPS 3, below VFE next :

FLAPS 3 FLAPS FULL

DECEL TOWARDS VAPP ………………CHECK TRK FPA

PF

PNF 3.a. FINAL APPROACH

0.3 NM before the FAF : FPA TO FINAL APPROACH PATH..….SET AND PULL

FMA After the FAF : ANNOUNCE……………”SET GA ALT xx FT”

GO AROUND ALTITUDE.………………………..SET ANNOUNCE…………………..”GA ALT xx FT SET” A/THR..……………………….CHECK SPEED MODE

Check that the A/C is actually on the descent path :  Bird below the horizon  Consistent V/S

PNF Xchecks Altitudes and Distances with Landing charts

 Slope gradient (θ) calculation : θ(°) = θ(%) x 0.6

PF

PNF 3.b. FINAL APPROACH

WING A. ICE (if not required)…………………..OFF EXTERIOR LIGHTS………………………………SET SLIDING TABLE………………………………STOW

SLIDING TABLE……………………………….STOW LDG MEMO ……..…….....………CHECK NO BLUE

CABIN REPORT………..OBTAIN (CM1) CABIN CREW……………………ADVISE

LANDING C/L FLT PARAMETERS…………………….…..CHECK

OBSERVE ECAM MEMO

PF

PNF 3.c. FINAL APPROACH

At MDA/H +100 ft : MONITOR OR ANNOUNCE………..”ONE HUNDRED ABOVE” At MDA/H :

MONITOR OR ANNOUNCE………………..”MINIMUM“

ANNOUNCE ....…………………………”LANDING” or …………………“GO AROUND/FLAPS”

”LANDING”

MDA/H

AP off FDs off Set Runway Track

PF

NAV ACCURACY

PNF

1.a. INITIAL APPROACH SEAT When BELTS..…………………...…………..ON/AUTO GPS PRIMARY avail No NAV ENG ACCURACY required MODE sel .....……………...….…AS RQRD NAV ACCURACY .....…………….....…MONITOR When cleared to 3700 ft : DESCENT .....……………………………....…INITIATE

When GPS PRIMARY lost

FMA BARO : QNH Use REF raw data to check NAV ACCURACY APPROACH C/L

PROG

+

VAPP SPEED CSTR AT FAF…………..INSERT If check is negative use Selected guidance for ILS interception If the FMGS detects low NAV ACCURACY, then the  LS P/B is OFF exceptenhanced for LOC only approaches. modes of the EGPWS are automatically deactivated

PF

STABILIZED APPROACH

PNF

1.a. INITIAL APPROACH SEAT BELTS..…………………...…………..ON/AUTO

ENG MODE sel .....……………...….…AS RQRD NAV ACCURACY .....…………….....…MONITOR

When cleared to 3700 ft : DESCENT .....……………………………....…INITIATE

Entering VAPP as …will displace the

FMA BARO REF :atQNH SPEED CONSTRAINT FAF ... APPROACH C/L D upstream

. F-PLN A page

D

VAPP SPEED CSTR AT FAF…………..INSERT

ND

 LS P/B is OFF except for LOC only approaches.

PF

PNF

1.b. INITIAL APPROACH PF When ATC gives radar vector HDG ……………………………………………SELECT ARC, or….. ROSE VOR

PNF

FMA

GS • • • TAS • • • • • • /• •

GS • • • TAS • • • • • • /• •

• • • • • • • °

• • • • • • • °

• • • NM

• • • NM

Approx 15 NM from touchdown : APPR PHASE……………………………....ACTIVATE POSITIONING……………………………....MONITOR MANAGED SPEED……………………………CHECK SPEEDBRAKES…………………………….AS RQRD • • :• •

• • • NM

• • •: •

GS • • • TAS• • • • • • /••

• • • NM

ROSE NAV

• • • NM

• • • NM

ND MODE RANGE……………………… AS RQRD

 Manual Approach phase activation on the PERF page APPR phase

• • • • • • •°

• • :• •

• • • NM

ND MODE RANGE………………………….AS RQRD

ROSE VOR, or……

• • • NM

NO AUTOACTIVATION :

 For Lateral positioning properly monitor F-PLN sequencing with navaid raw data  For Vertical positioning : Use the Energy Circle

• • • NM

D

PF

F-PLN SEQUENCING

PNF

1.b. INITIAL APPROACH When ATC gives radar vector HDG ……………………………………………SELECT  GO AROUND mode :

TOGA

FMA

Approx 15 NM from touchdown : APPR PHASE……………………………....ACTIVATE POSITIONING……………………………....MONITOR SEQUENCING MANAGED SPEED……………………………CHECK SPEEDBRAKES…………………………….AS RQRD ND MODE RANGE………………………….AS RQRD FAF

NO SEQUENCING

ND MODE RANGE……………………… AS RQRD C FAF

 Manual Approach phase activation on the PERF page

B A

NAV mode

APPR phase

No NAV mode NO AUTOACTIVATION :

 For Lateral positioning properly monitor F-PLN sequencing

F-PLAN is automatically sequenced in case of radial inbound

 For Vertical positioning : Use the Energy Circle

D

FAF

INTCP

QFU C IN BND

PF

PNF 2. INTERMEDIATE APPROACH

RADAR TILT........……………...………...ADJUST When cleared for approach : TRK/FPA………………………………………SET

FMA FLAPS 1

At green dot speed below VFE next : DECEL TOWARDS S SPEED..……..…CHECK

TCAS……………………………………TA or TA/RA

FLAPS 2

At S speed, below VFE next : DECEL TOWARDS F SPEED………….CHECK When FLAPS 2 :

GEAR DOWN ECAM WHEEL PAGE……………………...CHECK GROUND SPOILERS………………………….ARM AUTO BRAKE……………………………CONFIRM

When L/G down, below VFE next When FLAPS 3, below VFE next :

FLAPS 3isis recommended   ItIt recommended to to select select FLAPS FLAPS FULL FULL at at VFE VFE next next -- 15 15 knots knots to to minimize minimize flaps flaps wear. wear. FLAPS FULL

DECEL TOWARDS VAPP ………………CHECK TRK FPA

PF

GO AROUND ALTITUDE

PNF

3.a. FINAL APPROACH 0.3 NM before the FAF : FPA TO FINAL APPROACH PATH..….SET AND PULL

FMA In some cases the G/A ALT is under the current altitude of the A/C

 The pilot should delay the G/A ALT selection below G/A ALT ANNOUNCE……………”SET GA ALT xx FT” GO AROUND ALTITUDE.………………………..SET After the FAF :

ANNOUNCE…………………..”GA ALT xx FT SET”

GO AROUND ALT ........... …………….....SET

Check that the A/C is actually on theG/Adescent path : ALT  Bird below the horizon

Delay it A/THR..……………………….CHECK SPEED MODE  Slope gradient (θ) calculation : GO AROUND ALT ...........…………….....SET

θ(°) = θ(%) x 0.6

 Consistent V/S

If the GO AROUND setting is not done correctly ALT * will engage PNF Xchecks Altitudes and Distances with Landing charts

PF

PNF

FLT PARAMETERS 3.b. FINAL APPROACH

Announce any deviation in excess of FLT PARAMETERS : WING A. ICE (if not required)…………………..OFF

SLIDING TABLE………………………………STOW

EXTERIOR LIGHTS………………………………SET 7° COURSE BANK SLIDING TABLE……………………………….STOW 1/2 dot 5° ADF (VOR) 10 LDG MEMO ……..…….....………CHECK NO BLUE 10

CABIN REPORT………..OBTAIN (CM1) CABIN CREW……………………ADVISE Speed Target VAPP - 5kt +10 kt

SPD

Vapp

10

10

+10° LANDING C/L & Vapp

PITCH SINK RATE 1 0 -2.5° FLT1 0 PARAMETERS…………………….…..CHECK 1000 ft/min 10

OBSERVE ECAM MEMO _ FT HIGH or LOW At altitude check points