PRECISION APPROACH PNF

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1 NON PF PRECISION APPROACH (SELECTED) Initial APP Interm. APP Final APP IAF FAF D MDA/H FLYING REF : TRACK/FPA (FPD) A320 - Version 03a

2 1.a. INITIAL APPROACH SEAT BELTS ON/AUTO ENG MODE sel AS RQRD NAV ACCURACY MONITOR When cleared to 3700 ft : DESCENT INITIATE BARO REF : QNH APPROACH C/L VAPP SPEED CSTR AT FAF..INSERT LS P/B is OFF except for LOC only approaches.

3 When ATC gives radar vector HDG SELECT Approx 15 NM from touchdown : APPR PHASE...ACTIVATE POSITIONING...MONITOR MANAGED SPEED CHECK SPEEDBRAKES.AS RQRD ND MODE RANGE.AS RQRD 1.b. INITIAL APPROACH Manual Approach phase activation on the PERF page ND MODE RANGE AS RQRD APPR phase NO AUTOACTIVATION : D For Lateral positioning properly monitor F-PLN sequencing For Vertical positioning : Use the Energy Circle

4 RADAR TILT ADJUST 2. INTERMEDIATE APPROACH When cleared for approach : TRK/FPA SET At green dot speed below VFE next : DECEL TOWARDS S SPEED.... CHECK At S speed, below VFE next : FLAPS 1 FLAPS 2 TCAS TA or TA/RA DECEL TOWARDS F SPEED.CHECK When FLAPS 2 : GEAR DOWN When L/G down, below VFE next FLAPS 3 When FLAPS 3, below VFE next : FLAPS FULL DECEL TOWARDS VAPP CHECK ECAM WHEEL PAGE...CHECK GROUND SPOILERS.ARM AUTO BRAKE CONFIRM TRK FPA

5 0.3 NM before the FAF : FPA TO FINAL APPROACH PATH...SET AND PULL After the FAF : 3.a. FINAL APPROACH 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 : Slope gradient (θ) calculation : Bird below the horizon Consistent V/S θ( ) = θ(%) x 0.6 Xchecks Altitudes and Distances with Landing charts

6 3.b. FINAL APPROACH SLIDING TABLE STOW WING A. ICE (if not required)..off EXTERIOR LIGHTS SET SLIDING TABLE.STOW LDG MEMO..... CHECK NO BLUE CABIN REPORT..OBTAIN (CM1) CABIN CREW ADVISE LANDING C/L FLT PARAMETERS...CHECK OBSERVE ECAM MEMO

7 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 MDA/H LANDING AP off FDs off Set Runway Track

8 NAV ACCURACY 1.a. INITIAL APPROACH SEAT When BELTS ON/AUTO GPS PRIMARY avail No NAVENG ACCURACY MODE sel required AS RQRD When cleared to 3700 ft : DESCENT INITIATE When GPS PRIMARY lost BARO REF : QNH APPROACH C/L NAV ACCURACY MONITOR Use raw data to check NAV ACCURACY 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 modes approaches. of the EGPWS are automatically deactivated + PROG

9 STABILIZED APPROACH 1.a. INITIAL APPROACH SEAT BELTS ON/AUTO ENG MODE sel AS RQRD When cleared to 3700 ft : DESCENT INITIATE BARO REF : QNH Entering VAPP as SPEED CONSTRAINT at FAF... will displace the D. APPROACH C/L upstream D NAV ACCURACY MONITOR VAPP SPEED CSTR AT FAF..INSERT F-PLN A page ND LS P/B is OFF except for LOC only approaches.

10 PF 1.b. INITIAL APPROACH When ATC gives radar vector HDG SELECT ROSE VOR ARC, or.. GS TAS / Approx 15 NM from touchdown : APPR PHASE...ACTIVATE POSITIONING...MONITOR MANAGED SPEED CHECK NM NM SPEEDBRAKES.AS RQRD ND MODE RANGE.AS RQRD NM : GS TAS / NM GS TAS / NM NM : ROSE VOR, or ND MODE RANGE AS RQRD NM : ROSE NAV Manual Approach phase activation on the PERF page NM NM APPR phase NO AUTOACTIVATION : D For Lateral positioning properly monitor F-PLN sequencing with navaid raw data For Vertical positioning : Use the Energy Circle

11 F-PLN SEQUENCING When ATC gives radar vector HDG SELECT GO AROUND mode : Approx 15 NM from touchdown : TOGA APPR PHASE...ACTIVATE POSITIONING...MONITOR MANAGED SPEED CHECK SEQUENCING SPEEDBRAKES.AS RQRD ND MODE RANGE.AS FAF RQRD 1.b. INITIAL APPROACH NO SEQUENCING ND MODE C FAFRANGE AS RQRD Manual Approach phase activation on the PERF page NAV mode APPR phase B A No NAV mode NO AUTOACTIVATION : D 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 INTCP QFU C IN BND FAF

12 RADAR TILT ADJUST When cleared for approach : TRK/FPA SET At green dot speed below VFE next : 2. INTERMEDIATE APPROACH FLAPS 1 DECEL TOWARDS S SPEED.... CHECK At S speed, below VFE next : FLAPS 2 TCAS TA or TA/RA DECEL TOWARDS F SPEED.CHECK When FLAPS 2 : GEAR DOWN When L/G down, below VFE next FLAPS 3 When FLAPS 3, below VFE next : FLAPS FULL DECEL TOWARDS VAPP CHECK ECAM WHEEL PAGE...CHECK GROUND SPOILERS.ARM AUTO BRAKE CONFIRM It is recommended to select FLAPS FULL at VFE next - 15 knots to minimize flaps wear. TRK FPA

13 GO AROUND ALTITUDE 0.3 NM before the FAF : FPA TO FINAL APPROACH PATH...SET AND PULL 3.a. FINAL APPROACH In some cases the G/A ALT is under the current altitude of the A/C After the FAF : The pilot should delay the G/A ALT selection below G/A ALT ANNOUNCE SET GA ALT xx FT GO AROUND ALTITUDE...SET ANNOUNCE.. GA ALT xx FT SET GO AROUND ALT......SET A/THR...CHECK Delay it SPEED MODE Check that the A/C is actually on the descent path : Slope gradient (θ) calculation : G/A ALT Bird below the horizon Consistent V/S GO AROUND ALT......SET θ( ) = θ(%) x 0.6 If the GO AROUND setting is not done correctly ALT * will engage Xchecks Altitudes and Distances with Landing charts

14 FLT PARAMETERS SLIDING TABLE STOW 3.b. FINAL APPROACH Announce any deviation in excess of FLT PARAMETERS : WING A. ICE (if not required)..off BANK EXTERIOR 7 LIGHTS SET COURSE CABIN REPORT..OBTAIN (CM1) SLIDING TABLE.STOW 1/2 dot (VOR) 5 ADF LDG MEMO..... CHECK NO BLUE SPD VAPP - 5kt Vapp & Speed Target +10 kt Vapp CABIN CREW ADVISE LANDING C/L PITCH SINK RATE 10 FLT10 PARAMETERS...CHECK ft/min OBSERVE ECAM MEMO _ FT HIGH or LOW At altitude check points

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