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РПП Часть В |
Стандартные эксплуатационные процедуры |
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Издание: 05 |
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Airbus-319/320/321 |
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Standard operating procedures(SOP) |
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Изменение: 00 |
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SUMMARY FOR EACH PHASE |
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BEFORE ENGINE START/PUSH BACK |
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EVENT |
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CM1 |
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CM2 |
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Before start up clearance |
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BEFORE START C/L |
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received |
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DOWN TO THE LINE |
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After start up clearance |
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BELOW THE LINE |
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received |
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BEFORE START C/L COMPLETE |
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TO REMOVE GROUND SUPPLY |
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EVENT |
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CM1 |
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GND Mech |
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Initial ground contact |
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GROUND (from) COCKPIT |
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COCKPIT (from) GROUND |
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External disconnection |
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REMOVE EXTERNAL |
EXTERNAL REMOVED |
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PUSH BACK/ENGINE START |
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When ready for pushback, |
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GROUND (from) COCKPIT, |
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and pushback startup |
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CLEARED FOR PUSH |
COCKPIT (from) GROUND, |
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clearance received from ATC |
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RELEASE BRAKES |
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Start of push |
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BRAKES RELEASED |
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READY TO PUSH |
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When ready to start engines |
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CLEAR TO START? |
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STARTING ENG 2(1) |
CLEAR TO START |
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When push back completed |
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BRAKES SET |
SET BRAKES |
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When ready to disconnect |
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CLEAR TO DISCONNECT |
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(after engine started, and |
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(hand signals on left/right) |
DISCONNECTING |
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parameters are stabilized) |
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(hand signals on left/right) |
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AFTER ENGINE START |
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EVENT |
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CM1 |
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CM2 |
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ENG mode selector norm. |
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AFTER START PROCEDURE |
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Flight control check in |
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FLIGHT CONTROLS |
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Note :* The CM2 should follow |
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following sequence |
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CHECK |
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pedal movement with his/her feet |
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1. Elevators |
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FULL UP, FULL DOWN, |
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NEUTRAL |
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2. Ailerons/Spoilers |
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FULL LEFT, FULL RIGHT, |
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NEUTRAL |
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3. Rudder* |
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RUDDER |
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FULL LEFT, FULL RIGHT, |
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NEUTRAL |
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All engines started and |
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AFTER START C/L |
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AFTER START C/L |
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GND is disconnected |
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COMPLETE |
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cтр. 108 |
СТАНДАРТНЫЕ ФРАЗЫ |
Дата 01.02.2013 |
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РПП Часть В |
Стандартные эксплуатационные процедуры |
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Издание: 05 |
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Airbus-319/320/321 |
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Standard operating procedures(SOP) |
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Изменение: 00 |
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TAXI |
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EVENT |
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CM1 |
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CM2 |
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When taxi clearance |
CLEAR LEFT SIDE |
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obtained |
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CLEAR RIGHT SIDE |
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Brake transfer check |
BRAKE CHECK |
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PRESSURE ZERO |
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During taxi |
BEFORE TAKEOFF C/L |
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DOWN TO THE LINE |
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Lining up on the runway |
BELOW THE LINE |
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BEFORE TAKEOFF C/L |
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COMPLETE |
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TAKEOFF |
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CM1 |
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CM2 |
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Setting thrust levers to initial |
TAKEOFF |
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stabilization value |
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Upon aligned RWY |
YOU HAVE CONTROL |
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centerline |
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I HAVE CONTROL |
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EVENT |
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PF |
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PNF |
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When thrust levers set to |
ANNOUNCE FMA |
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FLEX/TOGA |
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CHECKED |
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Before passing 80 kts |
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THRUST SET |
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At 100 kts |
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HUNDRED KNOTS |
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CHECKED |
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At V1 |
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V1 |
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At VR |
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ROTATE |
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Gear retraction (when |
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POSITIVE CLIMB |
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positive increase of V/S, |
GEAR UP |
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BARO ALT, RA) |
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GEAR UP |
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If AP is engaged by PNF |
AP1 (2) ON |
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If AP is engaged by PF |
AP1 (2) |
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CHECKED |
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After takeoff check |
AFTER TAKEOFF C/L |
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(not normally requested upon |
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flap retraction completed) |
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DOWN TO THE LINE |
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After crossing transition |
BELOW THE LINE |
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altitude and altimeter setting |
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AFTER TAKEOFF C/L |
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(in climb) |
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COMPLETE |
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At 10000 ft oR FL 100 |
FL ONE HUNDRED |
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PROCEDURE |
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Дата 01.02.2013 |
СТАНДАРТНЫЕ ФРАЗЫ |
cтр. 109 |
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РПП Часть В |
Стандартные эксплуатационные процедуры |
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Издание: 05 |
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Airbus-319/320/321 |
Standard operating procedures(SOP) |
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Изменение: 00 |
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APPROACH AND LANDING |
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EVENT |
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PF |
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PNF |
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At 10000 ft of FL 100 |
FL ONE HUNDRED |
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PROCEDURE |
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After altimeter setting |
APPROACH C/L |
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APPROACH C/L COMPLETE |
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Activation of approach Phase |
ACTIVATE APPROACH |
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(approx 10 nm from FAF |
PHASE |
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APPROACH PHASE |
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or automatic in NAV mode) |
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ACTIVATED |
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RA alive |
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RADIO ALTIMETER ALIVE |
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CHECKED |
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(see Note 1 and 2 below) |
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“GS*” |
GA ALTITUDE ___ FT SET |
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Or below GO-AROUND ALTfor NPA |
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CHECKED |
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At FAF |
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PASSING |
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(Fix Name), |
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CHECKED |
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When landing flaps set, and |
LANDING C/L |
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green landing memo on ECAM |
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LANDING C/L COMPLETE |
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1000 feet or 500 feet |
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ONE THOUSAND |
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(FIVE HUNDRED) STABILIZED |
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CHECKED |
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or NOT STABILIZED (Note 2) |
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FMA “LAND” green |
LAND |
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CHECKED |
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100 feet above MDA/DH |
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HUNDRED ABOVE (Note 2) |
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CHECKED |
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MDA/DH visual reference |
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MINIMUM (Note 2) |
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СONTINUE |
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MDA/DH no visual reference |
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MINIMUM (Note 2) |
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GO AROUND - FLAPS |
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After touchdown: |
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- Ground spoilers extended |
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SPOILERS(Note 3), |
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- REV green on EWD |
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REVERSE GREEN (Note 4) |
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Deceleration |
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DECEL (See Note 5 below) |
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At 70 knots |
CHECKED |
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SEVENTY KNOTS |
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Note 1: Crew awareness, crew should now keep RA in scan to landing.
Note 2: PNF monitors pin-programmed auto callout, or announces if inoperative. Note 3: If the spoilers are not extended, call NO SPOILERS.
Note 4: If no reverse deployment, call NO REVERSE ENGINE_ or NO REVERSE, as appropriate. Note 5: DECEL callout means that the deceleration is felt by the crew and confirmed by the speed trend on the PFD. It can also be confirmed by the “DECEL” light when auto brake is used.
If no positive deceleration, call NO DECEL. * NO REVERSE ENGINE or NO REVERSE
cтр. 110 |
СТАНДАРТНЫЕ ФРАЗЫ |
Дата 01.02.2013 |
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РПП Часть В |
Стандартные эксплуатационные процедуры |
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Издание: 05 |
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Airbus-319/320/321 |
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Standard operating procedures(SOP) |
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Изменение: 00 |
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ALTIMETER SETTING CHANGES TO / FROM QNH / STD |
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EVENT |
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PF |
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PNF |
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While crossing transition |
SET STANDARD |
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altitude (transition level) |
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(SETQNH) |
STANDARD (QNH) |
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Barometric setting change |
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CROSS-CHECKED |
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and subsequent altimeter |
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PASSING FL___ (___ FT) NOW |
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cross-check |
CHECKED |
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GO AROUND |
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GO AROUND decision |
GO AROUND - FLAPS |
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Flaps retraction |
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FLAPS |
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Gear retraction |
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POSITIVE CLIMB |
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GEAR UP |
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GEAR UP |
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After takeoff check |
AFTER TAKEOFF C/L |
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(not normally requested upon |
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flap retraction completed) |
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DOWN TO THE LINE |
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After crossing transition |
BELOW THE LINE |
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altitude and altimeter |
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AFTER TAKEOFF C/L |
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setting (in climb) |
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COMPLETE |
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AFTER LANDING |
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EVENT |
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CM1 |
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CM2 |
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When clear of the runway |
AFTER LANDING C/L |
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AFTER LANDING C/L |
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COMPLETE |
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PARKING |
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Upon parking stand |
PARKING C/L |
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PARKING C/L COMPLETE |
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SECURING THE AIRCRAFT |
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EVENT |
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CM1 |
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CM2 |
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Upon last passenger has left |
SECURING THE |
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aircraft |
AIRCRAFT C/L |
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SECURING THE AIRCRAFT C/L |
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COMPLETE |
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MALFUNCTION BEFORE V1 AT TAKEOFF |
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EVENT |
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CM1 |
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CM2 |
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If GO decision |
GO |
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If RTO decision |
STOP |
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- REV green on EWD |
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REVERSE GREEN* |
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- Deceleration |
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DECEL (Note 5) |
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Дата 01.02.2013 |
СТАНДАРТНЫЕ ФРАЗЫ |
cтр. 111 |