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FCOM LIM-11 |
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WEIGHT LIMITATIONS (kg) |
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A/C |
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MTOW |
|
MLW |
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MZFW |
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MAX TAXI |
MIN WEIGHT |
||||||
A319(MSN 1884-1901, 3385-3388) |
|
75500 |
|
62500 |
58500 |
|
75900 |
35400 |
|||||||||
|
A319(MSN 3834) |
|
|
|
75500 |
|
61000 |
57000 |
|
75900 |
35400 |
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A320(MSN 0140-0157) |
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77000 |
|
64500 |
60500 |
|
77400 |
37230 |
|||||||
A320(MSN 0735, 1063-1152, 1484, 1751, |
|
77000 |
|
64500 |
61000 |
|
77400 |
37230 |
|||||||||
2166, 2278, 2349, 2998-3107) |
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A320(MSN 1777, 2175-2187, 2327, 3189, |
|
77000 |
|
66000 |
62500 |
|
77400 |
37230 |
|||||||||
3433, 3472) |
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A321(MSN 0775-1012, 1199, 1905-2117) |
|
89000 |
|
75500 |
71500 |
|
89400 |
47500 |
|||||||||
A321(MSN 1720, 2707) |
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|
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93000 |
|
77800 |
73800 |
|
93400 |
47500 |
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MAXIMUM DIFFERENCES BETWEEN ALTITUDE INDICATIONS |
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||||||||||||||
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(msn 0140-0775, 1012-1484) |
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FCOM PRO-SUP-34 |
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FL/SPEED |
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ALTITUDE (ft) COMPARISON BETWEEN |
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|||||||||
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ADR1 and ADR2 |
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ADR3 and ADR1 or |
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STBY ALTI and any |
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||||||||
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(on PFD) |
|
ADR3 and ADR2 on PFD |
|
ADR1 or 2 or 3 |
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|||||||
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GND CHECK |
20 (6 m) |
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|
|
20 (6 m) |
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*** |
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FL50/250 KT |
50 (15 m) |
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80 (24 m) |
|
130 (40m) |
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FL100/250 KT |
55 (17 m) |
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80 (24 m) |
|
185 (56 m) |
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||||||
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FL200/300 KT |
90 (27 m) |
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145 (44 m) |
|
295 (90 m) |
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||||||
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FL300/.78 |
130 (40 m) |
|
|
355 (108m) |
|
390 (119 m) |
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||||||
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FL390/.78 |
130 (40 m) |
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365 (111m) |
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445 (136 m) |
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|
||||||
|
(msn 0815-0991, 1720-1905, 2175-2187, 2327, 2707-3099, 3189) |
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|
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|||||||||
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FL/SPEED |
|
|
ALTITUDE (ft) COMPARISON BETWEEN |
|
|
|
|||||||||
|
|
ADR1 and ADR2 |
|
ADR3 and ADR1 or |
|
STBY ALTI and any |
|
|
|
||||||||
|
|
|
(on PFD) |
|
ADR3 and ADR2 on PFD |
|
ADR1 or 2 or 3 |
|
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|
|||||||
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GND CHECK |
20 (6 m) |
|
|
|
20 (6 m) |
|
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*** |
|
|
|
|
|||
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FL50/250 KT |
50 (15 m) |
|
|
65 (20 m) |
|
130 (40m) |
|
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|
||||||
|
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FL100/250 KT |
55 (17 m) |
|
|
80 (24 m) |
|
185 (56 m) |
|
|
|
||||||
|
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FL200/300 KT |
90 (27 m) |
|
|
135 (41 m) |
|
295 (90 m) |
|
|
|
||||||
|
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FL300/.78 |
130 (40 m) |
|
|
195 (59 m) |
|
390 (119 m) |
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|
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FL390/.78 |
130 (40 m) |
|
|
195 (59 m) |
|
445 (136 m) |
|
|
|
||||||
*** On ground, the check is meaningless because the standby altimeter’s vibrator is off.
(msn 2117-2166, 2278, 2349, 3107, 3385-3834)
FL/SPEED |
|
ALTITUDE (ft) COMPARISON BETWEEN |
|||
ADR1 and ADR2 |
ADR3 and ADR1 or |
ISIS and any ADR1 |
|||
|
(on PFD) |
ADR3 and ADR2 on PFD |
or 2 or 3 |
||
GND CHECK |
20 |
(6 m) |
20 |
(6 m) |
100(30m) |
FL50/250 KT |
50 (15 m) |
65 (20 m) |
130 (40m) |
||
FL100/250 KT |
55 (17 m) |
80 (24 m) |
185 (56 m) |
||
FL200/300 KT |
90 (27 m) |
135 |
(41 m) |
295 (90 m) |
|
FL300/.78 |
130 |
(40 m) |
195 |
(59 m) |
390 (119 m) |
FL390/.78 |
130 |
(40 m) |
195 |
(59 m) |
445 (136 m) |
|
FCOM LIM-12 |
MAXIMUM WIND CONDITION |
- Wind for take off and landing:
Ограничение AFM: Maximum tailwind for takeoff and landing для всего парка А319/320/321 –10kt
msn 0140-0157, 735-1152, 1484, 1751, 1884-1905, 2175-2187, 2327, 2707, 3107,3433-3834
Maximum tailwind for take off |
10 kt |
Maximum tailwind for landing |
10 kt |
|
|
msn 1199, 2117, 2166, 2278, 2349 |
|
Maximum tailwind for take off |
15 kt |
Maximum tailwind for landing |
10 kt |
Только для 2166, 2278, 2349. Примечание: Максимальная попутная составляющая для Landing & Rollout 10kt. Посадка с попутной составляющей 15kt разрешается только с закрылками FULL ??
msn 1720, 1777, 2998-3099, 3189-3388
Maximum tailwind for take off |
15 kt |
Maximum tailwind for landing |
15 kt |
Примечание: Максимальная попутная составляющая для Landing & Rollout 10kt. Посадка с попутной составляющей 15kt разрешается только с закрылками FULL.
-Maximum crosswind under different runway conditions:
*Runway covered with a layer of 1/2 in (12.7 mm) of water, slush, or wet snow
…………………………………………………….………………………..10kt (5 m/s)
Wind for passenger/cargo door operation:
•Maximum wind for passenger door operation………………………………………65 kt
•Maximum wind for cargo door opening ……………………………………………..40 kt
(or 50 kt, if the aircraft nose oriented into the wind, or the cargo door is on the leeward side)
• The cargo door must be closed, before the wind speed exceeds………………..65 kt
FCOM LIM-22-20
msn 775-1012,1199,1720,1905-2117,2707
MAXIMUM WIND CONDITIONS FOR CAT II AUTOMATIC APPROACH WITHOUT AUTOLAND
Head wind ………………………………40 kt Tail wind …………………………...........10 kt
Cross wind ………………………………25 kt
msn 775-1012,1199,1720,1905-2117,2707
MAXIMUM WIND CONDITIONS FOR CAT III AUTOMATIC APPROACH OR AUTOMATIC LANDING AND AUTOMATIC ROLL OUT
Head wind ………………………………30 kt
Tail wind …………………………...........10 kt Cross wind ………………………………20 kt
Note: Wind limitation is based on the surface wind reported by ATC. If the wind displayed on ND exceeds the above-noted autoland limitations, but the tower reports a surface wind within the limitations, then the autopilot can remain engaged. If the tower reports a surface wind that exceeds the limitations, only CAT II automatic approach without autoland can be performed provided wind conditions are wiyhin the limitations quoted on Refer to LIM-22-20 ILS Category
II (see above). Otherwise, only CAT I automatic approach without autoland can be performed.
FCOM LIM-22-20
msn 140-735,1063-1152,1484,1751-1901,2166-2349,2998-3834
MAXIMUM WIND CONDITIONS FOR CAT II OR CAT III AUTOMATIC APPROACH LANDING AND ROLL OUT
Head wind ………………………………30 kt
Tail wind …………………………...........10 kt Cross wind ………………………………20 kt
Note: Wind limitation is based on the surface wind reported by ATC. If the wind displayed on ND exceeds the above-noted autoland limitations, but the tower reports a surface wind within the limitations, then the autopilot can remain engaged. If the tower reports a surface wind beyond limitations, only CAT I automatic approach without autoland can be performed.
ILS AUTOMATIC LANDING IN CAT I OR BETTER WEATHER CONDITIONS
Applicable to: ALL
The automatic landing system’s performance has been demonstrated on runways equipped with CAT II or CAT III ILS approaches. However, automatic landing in CAT I or better weather conditions is possible on CAT I ground installations or when ILS sensitive areas are not protected, if thefollowing precautions are taken:
The airline has checked that the ILS beam quality and the effect of terrain profile before the runway have no adverse effect on AP/FD guidance. In particular, the effect of terraindiscontinuities within 300 m before runway threshold must be evaluated.
The crew is aware that LOC or GS beam fluctuations, independent of the aircraft systems, may occur and the PF is prepared to immediately disconnect the AP and take appropriate action,should unsatisfactory guidance occur.
At least CAT2 capability is displayed on the FMA, and CAT II/III procedures are used. Visual references are obtained at an altitude appropriate to the performed CAT I approach,
otherwise go–around is initiated.
AUTOMATIC LANDING
Applicable to: ALL
CAT II and CAT III autoland are approved in CONF 3 and CONF FULL.Automatic landing is demonstrated:
With CAT II and CAT III ILS beam
With slope angle within (-2.5 °, -3.15 °) rangeFor airport elevation at or below 2 500 ft
At or below the maximum landing weight
Automatic rollout performance has been approved on dry and wet runways, but performance on snow-covered or icy runways has not been demonstrated.
|
|
Особенности по парку |
|
|
|
MSN 0140-0735, 1063, 1484 |
|
At approach speed (VAPP) = VLS + 5 kt + wind correction. |
|
|
|
MSN 1152, 1751-1777, 2166-2349 |
|
At approach speed (VAPP) = VLS + wind correction. |
|
Minimum wind correction 5 kt ; maximum windcorrection15 kt |
|
MSN 0775-1012, 1199 |
|
At approach speed (VAPP) = VLS + wind correction |
|
Minimum wind correction 5 kt ; maximum wind correction 15 kt. |
|
|
During automatic rollout with one engine inoperative or one thrust reverser |
|
|
inoperative, the use of the |
|
|
thrust reverser is limited to IDLE reverse with a maximum crosswind component |
|
|
of 15 kt |
|
MSN 1884-1901 |
|
For airport elevation at or below 9 200 ft |
|
|
At approach speed (VAPP) = VLS + wind correction |
|
Minimum wind correction 5 kt, maximum wind correction 15 kt. |
|
|
|
|
|
Note: Depending on the situation (e.g. emergency or other) and provided that the |
|
|
runway isapproved for automatic landing, the flight crew can decide to perform |
|
|
an autoland up to 69 t(152 117 lb) |
|
MSN 2998-3099, 3189 |
|
At approach speed (VAPP) = VLS + 5 kt + wind correction. |
|
Automatic landing is not allowed below -1 000 ft pressure altitude. |
|
|
|
|
MSN 1720, 1905-2117 |
|
For airport elevation at or below 5 750 ft |
|
|
At approach speed (VAPP) = VLS + wind correction |
|
Minimum wind correction 5 kt, maximum wind correction 15 kt. |
|
|
|
|
|
During automatic rollout with one engine inoperative or one thrust reverser |
|
|
inoperative, the flight crew |
|
|
can use the remaining thrust reverser, provided that: |
|
|
|
Only IDLE reverse thrust is used |
|
The crosswind does not exceed 15 kt |
|
MSN 3107, 3433, 3472 |
|
At approach speed (VAPP) = VLS + wind correction. |
|
||
|
Minimum wind correction 5 kt; maximum 15 kt. |
|
|
Automatic landing is not allowed below -1 000 ft pressure altitude. |
|
MSN 2707 |
|
For airport elevation at or below 5 750 ft |
|
|
At approach speed (VAPP) = VLS + wind correction |
|
Minimum wind correction 5 kt, maximum wind correction 15 kt. |
|
|
|
|
|
Automatic landing is not allowed below-1 000 ft pressure altitude. |
|
|
During automatic rollout with one engine inoperative or one thrust reverser |
|
|
inoperative, the flight crew |
|
|
can use the remaining thrust reverser, provided that: |
|
|
|
Only IDLE reverse thrust is used |
|
The crosswind does not exceed 15 kt. |
|
MSN 3385-3834 |
|
For airport elevation at or below 9 200 ft |
|
||
|
|
At approach speed (VAPP) = VLS + wind correction |
|
Minimum wind correction 5 kt, maximum wind correction 15 kt. |
|
|
|
|
|
Automatic landing is not allowed below-1 000 ft pressure altitude. |
|
|
Note: Depending on the situation (e.g. emergency or other) and provided that the |
|
|
runway isapproved for automatic landing, the flight crew can decide to perform |
|
|
an autoland up to 69 t(152 117 lb) |
|
Allowable runway conditions: |
FCOM LIM-12 |
•Runway paved and hard surfaced.
•Runway covered with a layer of water, slush, or wet snow, no greater than 1/2 in (12.7 mm).
•Runway covered with a layer of dry snow no greater than 2 in (50 mm)
Maximum crosswind under different runway conditions:
• Runway covered with a layer of 1/2 in (12.7 mm) of water, slush, or wet snow..............10 kt (5 m/s)
Расчет взлетно-посадочных характеристик в разделе Performance – RWy FCOM PER contamination выполнен для двух категорий определенных толщиной осадков. Для каждой
категории ниже приведены условия эквивалентности. |
|
Для взлета |
Для посадки |
EQUIVALENT of WET RUNWAY (RWY covered with or less than)
-3 mm (0,12 inch) slush
-3 mm (0,12 inch) water
-3 mm (0,12 inch) wet snow
-3 mm (0,12 inch) dry snow
CONTAMINATED RUNWAY
An equivalence between depth of slush and snow:
-12,7 mm (1/2 inch) wet snow = 6,3 (1/4 inch) slush
-50,8 mm (2 inch) dry snow = 6,3 mm (1/4 inch) slush
-25.4 mm (1 in) wet snow = 12.7 mm (1/2 in) slush
-101.6 mm (4 in) dry snow = 12.7 mm (1/2 in) slush
NOTE: 1. It is not recommended to take off from a runway covered with more than 4 inch of dry snow or 1 inch of wet snow.
EQUIVALENT of WET RUNWAY (RWY covered with or less than)
-3 mm (0,12 inch) slush
-3 mm (0,12 inch) water
-3 mm (0,12 inch) wet snow
-3 mm (0,12 inch) dry snow
CONTAMINATED RUNWAY
An equivalence between depth of slush and snow:
-up to 30 mm (1.18 in) wet snow = slush
-up to 130 mm (5.12 in) dry snow = slush
|
|
|
Maximum crosswind for different RWy conditions |
FCOM LIM-12 |
|||||
|
|
|
|
(ALL) |
|
|
|
|
|
|
OTHER AIRPORTS (except CIS) |
|
|
|
|
||||
|
Код |
|
|
|
Измеренный |
Боковой ветер |
Эквивалентное |
||
|
Код |
Эффективность |
(расчётный) |
(узлы/ м/с) |
состояние |
||||
снежного |
|||||||||
ICAO |
торможения |
коэффициент |
|
|
полосы ** |
||||
|
|
||||||||
NOTAM |
взлёт |
посадка |
|||||||
|
|
|
|
|
сцепления |
|
|
|
|
5 |
95 |
Good |
0,4 и выше |
29/14.9 * |
33/17 * |
1 |
|||
4 |
94 |
Good/medium |
039-0,36 |
29/14.9 |
29/14.9 |
1 |
|||
3 |
93 |
Medium |
0,35-0,30 |
25/12.9 |
2/3 |
||||
2 |
92 |
Medium/poor |
0,29-0,26 |
20/10.3 |
2/3 |
||||
1 |
91 |
Poor |
0,25 и ниже |
15/7.7 |
3/4 |
||||
0 |
99 |
Ненадёжная |
|
5 узлов |
4/5 |
||||
*: The maximum crosswind demonstrated for dry and wet runways.
**: Equivalent runway conditions (only valid for maximum crosswind determination): 1. Dry, damp or wet runway (less than 3 mm water depth)
2.Runway covered with slush
3.Runway covered with dry snow
4.Runway covered with standing water, or with risk of hydroplaning, or with wet snow
5.Icy runway, or high risk of hydroplaning
CIS AIRPORTS
Reported |
Нормативный |
Боковой ветер (узлы/ м/с) |
||
braking action |
коэффициент сцепления |
|
|
|
взлёт |
|
посадка |
||
|
|
|
||
Good |
0,50 и выше |
29/14.9 * |
|
33/17 * |
Good/medium |
0,49-0,45 |
29/14.9 |
|
29/14.9 |
Medium |
0,44-0,40 |
|
25/12.9 |
|
Medium/poor |
0,39-0,35 |
|
20/10.3 |
|
Poor |
0,34-0,30 |
|
15/7.7 |
|
It is not permitted to operate on runways covered with ice, or with
a friction coefficient of µ < 0,3
NOTE: 1.In the case of a loss of 3 spoilers, or of a flaps or slats jam/fault, the cross wind limit is 15 knots. 2.Landing conditions, in the case of a dual G+Y hydraulic system failure:
-Runway condition………………………………………………………..… Dry
-Crosswind…………………………No more than 10 knots (5 meter/second)
|
QRH IN FLT |
Maximum Crosswind on Contaminated Runways |
Таблица синусов
|
0 |
1 |
2 |
3 |
4 |
5 |
6 |
7 |
8 |
9 |
0 |
0 |
0,02 |
0,03 |
0,05 |
0,07 |
0,09 |
0,1 |
0,12 |
0,14 |
0,16 |
10 |
0,17 |
0,19 |
0,21 |
0,22 |
0,24 |
0,26 |
0,28 |
0,29 |
0,31 |
0,33 |
20 |
0,34 |
0,36 |
0,37 |
0,39 |
0,41 |
0,42 |
0,44 |
0,45 |
0,47 |
0,48 |
30 |
0,5 |
0,52 |
0,53 |
0,54 |
0,56 |
0,57 |
0,59 |
0,6 |
0,62 |
0,63 |
40 |
0,64 |
0,66 |
0,67 |
0,68 |
0,69 |
0,71 |
0,72 |
0,73 |
0,74 |
0,75 |
50 |
0,77 |
0,78 |
0,79 |
0,8 |
0,81 |
0,82 |
0,83 |
0,84 |
0,85 |
0,86 |
60 |
0,87 |
0,87 |
0,88 |
0,89 |
0,9 |
0,91 |
0,91 |
0,92 |
0,93 |
0,93 |
70 |
0,94 |
0,95 |
0,95 |
0,96 |
0,96 |
0,97 |
0,97 |
0,97 |
0,98 |
0,98 |
80 |
0,98 |
0,99 |
0,99 |
0,99 |
0,99 |
1 |
1 |
1 |
1 |
1 |