Noise abatement procedures shall be executed by all aircraft.
Air Ground communication shall be reduced to absolute minimum
during approach and initial departure phase.
Arrivals
Approach Phase:
Runways 25L/R are noise preferential and shall be used to the
greatest extent possible. If special meteorological conditions
are present in arrival and approach sectors, ATS unit may at its
own discretion or by a pilot-in-command's request, deviate from
the provisions given below, if it is necessary for safety reasons.
Restrictions:
The required noise abatement procedures shall not be observed
over the overflow areas in the following cases:
- if there is ice, slush, water, mud, rubber, oil etc on the
runway and friction coefficient is 0.4 or less
- when cloud ceiling is less than 150m or horizontal visibility
is less than 1800m
- when a crosswind component on the runway (including gusts)
exceeds 15kt
- when a tail wind component on the runway exceeds 5kt
- when wind shear is forecasted or reported or it is expected
that unfavorable weather conditions may influence aircraft approach
or landing.
During instrument as well as visual approach, it is not allowed
to fly below ILS GS angle. No noise abatement procedures shall
envisage the increasing of indicated air speed of descent.
A displacement threshold shall not be used as a noise abatement
measure.
Landing of aircraft with tail wind component up to 5m/sec is allowed
under the following conditions:
- Runway is dry or damp
- friction coefficient if 0.5 or more
- crosswind component is not more than 5m/sec
Runways 07L/R Approach
When reaching 13.5 NM from threshold, pilots shall conduct the
flight at 3590' (2960m) maintaining 210 KT and flight direction
enabling to intercept ILS LOC operational area providing runways
07L/R approach to land.
At a distance of 11.9 NM the aircraft shall reach a rate of 180kt
+/- 10kt to intercept ILS LOC at 7.6 NM from threshold descending
to 2600' (1970m).
Intercept glide slope at 2280' (1650m). Pilots shall continue
to reduce speed in order to reach 4.3 NM from threshold at 2110'
(1480m) and at a rate of 155 kt.
Thereafter speed shall be maintained as per Airplane Flight Manual
Departures
Take-off and Climbing Phase
Noise abatement procedures shall not be executed at the expense
of reduction of flight safety and in case of engine failure during
take-off
Runways 07L/R are noise preferential and shall be used to the
greatest extent possible.
Restrictions
Take0off with tail wind component up to 5 m/sec is allowed under
the following conditions:
- Runway is dry or dam;
- friction coefficient is 0.5 or more
- crosswind component is not more than 5m/sec
During take-off from runway 25L/R on take-off heading and maximum
possible climb gradient aircraft shall proceed to a distance of
MR 1.1 DME then turn right immediately on 340 degrees track for
SIDs AR 25D, BP 25E (it is strictly prohibited to reduce 340 degrees
track until intersecting 229 degrees bearing from UM or reaching
a distance of MR 3.2 DME unless it is required for further flight
safety)/28 degrees bearing to KN for SID KN 25D/ intercept 200
degrees bearing to KS for SID KS 25D/intercept 116 degrees bearing
to BP for SID BP 25D/intercept 028 bearing to KN for SID KN 25D.
During take-off from runway 07L/R on take-off heading and maximum
possible climb gradient aircraft shall proceed not further than
MM (distance of MR 3.9 DME) then turn left immediately on 045
degrees track.
Changing of flight course after take-off is permitted only after
reaching 1030' (400m).
During take-off from runway 25L/R it is prohibited to make a left
turn to proceed to KS.
The minimum indicated air speed during steady climb shall not
be less than V2+10kt or less than prescribed in the Airplane Flight
Manual if it has greater value.
Maintaining the minimum indicated air speed of climb is not required
if it brings to exceeding the minimum permissible angle of attack.
The reduction of power shall not be applied until:
- reaching 1420' (790m)
- the established standard power mode enables with maximum certified
take-off mass to maintain the established climb gradient of
not less than 4% at the above specified speed
- take-off flight path provides overflying of all obstacles
located under the flight path with sufficient clearance when
all engines are operating normally and also taking into account
possible engine failure and time period necessary for the rest
engines to develop full power.
Climbing Phase
Pilots shall apply two noise abatement procedures during climbing
phase:
- noise abatement departure near airport (NADP1)
- noise abatement procedure far from airport (NADP2)
The pilot-in-command may use any of them for reaching necessary
effect (ICAO Doc 8168, Volume 1, Part V, Chapter 3).
Reverse Thrust
Reverse thrust power with the exception reverse idle thrust is
used only for safety reasons. |