NON PF PRECISION (SELECTED) Initial APP Interm. APP Final APP IAF FAF D MDA/H FLYING REF : TRACK/FPA (FPD) - Version 02a
1.a. INITIAL SEAT BELTS.......ON/AUTO ENG MODE sel....... AS RQRD NAV ACCURACY...... MONITOR When cleared to 3700 ft : DESCENT...... INITIATE BARO REF : QNH C/L VAPP SPEED CSTR AT FAF..INSERT LS P/B is OFF except for LOC approaches.
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 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
RADAR TILT.........ADJUST 2. INTERMEDIATE A330/340-300 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
0.3 NM before the FAF : FPA TO FINAL PATH...SET AND PULL After the FAF : 3.a. FINAL A330/340-300 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
3.b. FINAL 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
PF 3.c. FINAL At MDA/MDH +100 ft : MONITOR OR ANNOUNCE.. ONE HUNDRED ABOVE At MDA/MDH : MONITOR OR ANNOUNCE.. MINIMUM ANNOUNCE... LANDING or GO AROUND/FLAPS MDA/MDH LANDING AP off FDs off Set Runway Track
NAV ACCURACY 1.a. INITIAL A340 / A330 SEAT When BELTS.......ON/AUTO GPS PRIMARY avail No NAVENG ACCURACY MODE sel required....... AS RQRD When cleared to an altitude : DESCENT...... INITIATE When GPS PRIMARY lost BARO REF : QNH C/L NAV ACCURACY...... MONITOR Use raw data to check NAV ACCURACY VAPP SPEED CSTR AT FAF..INSERT LS P/B is OFF except for LOC only approaches. Different approach strategies : If check is negative use Selected guidance for ILS interception + PROG If the FMGS detects low NAV ACCURACY, then the enhanced modes of the EGPWS are automatically deactivated
STABILIZED 1.a. INITIAL SEAT BELTS.......ON/AUTO ENG MODE sel....... AS RQRD When cleared to an altitude : DESCENT...... INITIATE BARO REF : QNH Entering VAPP as SPEED CONSTRAINT at FAF... will displace the D. C/L upstream NAV ACCURACY...... MONITOR VAPP SPEED CSTR AT FAF..INSERT LS P/B is OFF except for LOC only approaches. Different approach strategies : F-PLAN A F-PLN page page D ND
1.b. INITIAL PF 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
F-PLN SEQUENCING When ATC gives radar vector HDG SELECT GO AROUND mode : Approx 15 NM from touchdown : TOGA 1.b. INITIAL APPR PHASE...ACTIVATE POSITIONING...MONITOR SEQUENCING MANAGED SPEED CHECK SPEEDBRAKES.AS RQRD FAF NO SEQUENCING C FAF Manual Approach phase activation on the PERF page NAV mode APPR PHASE B A DECEL Nopseudo NAV mode waypoint symbol is white ( 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
RADAR TILT.........ADJUST When cleared for approach : TRK/FPA SET At green dot speed below VFE next : 2. INTERMEDIATE A330/340-300 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
GO AROUND ALTITUDE 0.3 NM before the FAF : FPA TO FINAL PATH...SET AND PULL 3.a. FINAL 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 theg/adescent ALT path : Slope gradient (θ) calculation : Bird below the horizon Consistent V/S GO AROUND ALT......SET θ( ) = θ(%) x 0.6 Xcheck Altitudes and Distances with If the GO AROUND setting is not done correctly LandingALT charts * will engage
FLT PARAMETERS SLIDING TABLE STOW 3.b. FINAL A330/340-300 Announce any deviation in excess of FLT PARAMETERS : WING A. ICE (if not required)..off BANK EXTERIOR 7 LIGHTS SET COURSE 10 10 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 10 10 +10 LANDING C/L PITCH SINK RATE 10 FLT10 PARAMETERS...CHECK 0 10 1000 ft/min OBSERVE ECAM MEMO _ FT HIGH or LOW At altitude check points