COCKPIT PREPARATION
COCKPIT PREPARATION CHECKLIST
BEFORE PUSHBACK/START CLEARANCE
LOADSHEET (PF-PM)
FUEL (PF-PM)
TAKEOFF DATA
SEATING POSITION
MCDU
AIR CONDITIONING UNITS
ELEC
AT PUSHBACK/START CLEARANCE
PUSHBACK/START CLEARANCE
EXTERIOR LIGHTS
ATC
WINDOWS AND DOORS
THRUST LEVERS
ACCU PRESSURE
PARKING BRAKE AND NOSEWHEEL STEERING
TAILWIND/ XWIND>20kts TAKEOFF Technique
TAKEOFF - ANNOUNCE
THRUST - 50% N1
SIDESTICK - FULL FORWARD
BRAKES - RELEASE
THRUST LEVERS - increase rapidly to 70% and then progressively to reach takeoff thrust by 40kts GS
At 80 kts - release sidestick gradually to be neutral at 100kts
Then, as normal takeoff
STABILIZATION HEIGHT
The stabilization HEIGHT is defined as one of the following:
STABILIZATION CRITERIA
In order for the approach to be stabilized, ALL of the following conditions must be satisfied before, or at the stabilization height:
Aircaft is on the CORRECT LATERAL and VERTICAL PATH;
+
Aircaft in the desired LANDING CONFIGURATION;
+
THRUST is stabilized, usually above idle, and the aircraft is at TARGET SPEED for approach;
+
Flight crew does NOT detect any EXCESSIVE flight parameter DEVIATION
If one of the above-mentioned conditions is not satisfied, the flight crew must initiate a go-around, unless they estimate that only small corrections are required to recover stabilized approach conditions.
EARLY STABILISED APPROACH
Under certain circumstances, the flight crew may decide to reduce the speed down to VAPP in the landing configuration at the FDP (i.e. approach via selected guidance, high glide path angle, low altitude intermediate approach, etc.)
-In order to obtain a valuable deceleration pseudo waypoint and to ensure a timely deceleration, set VAPP as a speed constraint at the FDP
CONFIGURATION SCHEDULE:
-Start configuring 7 NM Before FDP
DECELERATED APPROACH
Activate app phase 15 NM before TDZ;
CONFIGURATION SCHEDULE
-flap 1 3 NM Before FDP
-flaps 2 at 2000’ AGL
-GEAR DOWN in sequence
-flaps 3 in sequence
-flaps full in sequence
At 1000’ AGL MIN:
-VApp stable
-LDG Config
If speed selected:
To minimize flap wear, extend flaps when at Vfe-15 knots
What visual references are necessary at DH or MDH to land on a NPA, APV and ILS CAT 1 Operations?
At DH or MDH, at least one of the visual references specified below should be distinctly visible and identifiable to the pilot: A) elements of the approach lighting system B) the threshold C) the threshold markings D) the threshold lights E) the threshold identification lights F) the visual glide slope indicator G) the touchdown zone or touchdown zone markings H) the touchdown zone lights I) runway edge lights J) other visual references specified in the operations manual (AMC1 CAT.OP.MPA.305(e)) (LIDO 1.5.8.10.7)
ALTERNATE BRAKING SYSTEM CHECK
The purpose of this check is to verify the absence of “spongy pedals”
Y ELEC PUMP - check OFF
CHOCKS - IN PLACE
PARK BRK handle - OFF
BRAKE PEDALS - PRESS (max pressure)
(pressure must build up symmetrically. With full deflection, pressure must be within 2000 and 2700 PSI)
BRAKE PEDALS - RELEASE
PARK BRK - SET
On WET Runways (RWY surface condition GOOD), we may use IDLE REV IF:
-The landing performance calc was made with: MEDIUM TO POOR conditions; + NO REVERSER CREDIT
Preliminary cockpit preparation - Battery check (If aircraft has not been electrically supplied for 6 h or more)
If voltage AT OR BELOW 25.5V:
A charging cycle is required ( approx. 20’):
Check on ELEC SD page, that the battery contactor is closed and the batteries are charging.
After 20 minutes: