PRECISION APPROACH PNF

Transcription

1 NON PF PRECISION (MANAGED) Initial APP Interm. APP Final APP IAF FAF D MDA/H FLYING REF : TRACK/FPA (FPD) - Version 02a

2 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 approach Different approach strategies : 3 CONDITIONS FOR MANAGED :

3 When cleared for approach : 1.b. INITIAL APPR PB..ARM TRK/FPA SET Approx 15 NM from touchdown APPR PHASE ACTIVATION CHECK POSITIONING.MONITOR MANAGED SPEED CHECK SPEEDBRAKES.AS RQRD ND MODE/RANGE.AS RQRD ND MODE/RANGE AS RQRD TRK FPA D AUTOMATIC APPR APPR phase PHASE For Lateral positioning properly monitor F-PLN sequencing For Vertical positioning use V/DEV information

4 2. INTERMEDIATE A330 /A RADAR TILT ADJUST At green dot speed : 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 ECAM WHEEL PAGE...CHECK GROUND SPOILERS.ARM AUTO BRAKE CONFIRM When FLAPS 3, below VFE next : FLAPS FULL DECEL TOWARDS VAPP CHECK

5 3.a. FINAL After the FAF : Check FINAL APP green ANNOUNCE SET GA ALT xx FT GO AROUND ALT..SET ANNOUNCE.. GA ALT xx FT SET A/THR.. CHECK SPEED MODE POSITION/FLIGHT PATH MONITOR

6 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

7 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 AP off LANDING FDs off Set Runway Track MDA/MDH At MDA/MDH 50 ft AP automatic disconnection

8 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 LS P/B is OFF except for LOC only approaches. Different approach strategies : If check is negative use Selected guidance 4 CONDITIONS FOR MANAGED : for ILS interception NOTE : 1) Approach is in the database If the FMGS detects low NAV ACCURACY, then the 2) GPS PRIMARY or NAV ACCURACY hasenhanced been modes V/S-FPA of theknob EGPWS are automatically checked deactivated 3) Approach is validated by the airline for use of FINAL APP mode and not modified by the crew 4) All engines operative BARO REF : QNH C/L NAV ACCURACY MONITOR Use raw data to check NAV ACCURACY VAPP SPEED CSTR AT FAF..INSERT In managed mode, reversion to selected mode is available by PULLING HDG/TRK or + PROG

9 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 D NAV ACCURACY MONITOR VAPP SPEED CSTR AT FAF..INSERT LS P/B is OFF except for LOC only approaches. 4 CONDITIONS FOR MANAGED page : 1) Approach is in the database F-PLAN F-PLN A page 2) GPS PRIMARY or NAV ACCURACY has been checked 3) Approach is validated by the airline for use of FINAL APP mode and not modified by the crew 4) All engines operative ND Different approach strategies : NOTE : In managed mode, reversion to selected mode is available by PULLING HDG/TRK or V/S-FPA knob

10 STRATEGIES 1.a. INITIAL SEAT BELTS ON/AUTO Lateral and vertical selected guidance : ENG MODE sel AS RQRD NAV ACCURACY MONITOR When cleared to an altitude : DESCENT INITIATE Lateral managed guidance and vertical selected guidance : LS P/B is OFF except for LOC only approaches. 4 CONDITIONS FOR MANAGED : Whatever the strategy, the Final approach must be monitored laterally and vertically, using In managed mode, reversion to selected 1) Approach is in the database adequate raw data (altimeter, reference navaid) 2) GPS PRIMARY or NAV ACCURACY has been checked HDG TRK V/S FPA 3) Approach is validated by the airline Lateral, for vertical use of Note FINAL : APP mode andpull not modified selected by the crew guidance 4) All engines operative BARO REF : QNH C/L This type of guidance can be used provided the approach is stored in the navigation data base Lateral and vertical managed guidance : VAPP SPEED CSTR AT FAF..INSERT Different approach strategies : NOTE : mode is available by PULLING HDG/TRK or V/S-FPA knob PULL Vertical selected guidance

11 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 approach 3 CONDITIONS FOR MANAGED : Different approach strategies : 1) Approach is in the database 2) GPS PRIMARY or NAV ACCURACY has been checked NOTE : In managed mode, reversion to selected mode is available by PULLING HDG/TRK or V/S-FPA knob 3) Approach is validated by the airline for use of FINAL APP mode and not modified by the crew

12 When cleared for approach : 1.b. INITIAL BOTH PILOTS APPR PB..ARM ARC, or.. GS TAS / TRK/FPA SET Approx 15 NM from touchdown GS TAS APPR PHASE ACTIVATION CHECK / POSITIONING.MONITOR MANAGED SPEED CHECK SPEEDBRAKES.AS NM RQRD NM ND MODE/RANGE.AS RQRD NM : ROSE VOR, or NM : ROSE NAV ND MODE/RANGE AS RQRD TRK FPA NM NM D AUTOMATIC APPR APPR phase PHASE For Lateral positioning properly monitor F-PLN sequencing with navaid raw data For Vertical positioning use V/DEV information

13 If phase is active : V/DEV V/DEV PFD V/DEV scale max deviation : +/-200 ft V/DEV Intercept point symbol on ND «Brick» symbol FMS computed flight path +/- if GPS PRIMARY is not available, V/DEV information is reliable only when the NAV ACCY ckeck is positive

14 F-PLN SEQUENCING If the sequencing is not correct APPR NAV engagement is not possible C FAF B A GO AROUND mode : TOGA SEQUENCING NO SEQUENCING FAF C FAF B A NAV mode No NAV mode F-PLAN is automatically sequenced in case of radial inbound INTCP QFU C IN BND FAF

15 2. INTERMEDIATE A330 /A RADAR TILT ADJUST At green dot speed : 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 ECAM WHEEL PAGE...CHECK GROUND SPOILERS.ARM AUTO BRAKE CONFIRM When FLAPS 3, below VFE next : FLAPS FULL It is recommended to select FLAPS FULL at VFE next - 15 knots to minimize flaps wear. DECEL TOWARDS VAPP CHECK

16 GO AROUND ALTITUDE 3.a. FINAL After the FAF : Check FINAL APP green 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 ALT......SET GO AROUND ALT..SET ANNOUNCE.. GA Delay it ALT xx FT SET G/A ALT POSITION/FLIGHT PATH MONITOR A/THR.. CHECK SPEED MODE GO AROUND ALT......SET

17 3.a. FINAL After the FAF : Check FINAL APP green ANNOUNCE SET GA ALT xx FT GO AROUND ALT..SET ANNOUNCE.. GA ALT xx FT SET A/THR.. CHECK SPEED MODE POSITION/FLIGHT PATH MONITOR Monitor the engagement of FINAL APP mode using the raw data info If FINAL APP does not engage, revert to selected approach : Select FPA convergent to the Final Descent Path so as to fly with VDEV=0 Do not try to rearm APPR Xchecks Altitudes and Distances with Landing charts

18 FLT PARAMETERS SLIDING TABLE STOW 3.b. FINAL A340 / A330 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