曝光臺 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

..................OFF
A/THR.............................................................................................................................
.................. OFF
Note: Check the actual slat/flap configuration on ECAM, since flap auto-retraction
may occur.
SLATS/FLAPS EXTENDED
Above 66 t 66 t-56 t Below 56 t
CONF Speed Pitch (°)/Thrust (% N1)
3 F 7.0/62.0 7.0/57.9 7.0/53.3
2 F 8.5/61.3 8.5/57.1 8.5/52.7
1 + F S 3.5/62.6 3.5/58.5 3.5/54.2
1 S 7.5/59.1 7.5/55.5 7.5/51.1
CLEAN
FL Speed Pitch (°)/Thrust (% N1)
Below FL 200 250 kt 3.5/62.4 3.0/60.3 2.0/58.8
FL 200 -FL 320 275 kt 2.5/74.3 2.0/72.7 1.5/71.4
Above FL 320 M 0.76 3.0/80.1 2.5/78.6 2.0/76.3
PITCH/THRUST FOR INITIAL LEVEL OFF
Flying technique to stabilize speed:
Adjust pitch in order to ‐ fly the required flight path.
‐ When target pitch is reached, flying intended flight path, adjust thrust to target:
• If the aircraft pitch tends to increase, aircraft is slow, then increase thrust;
• If the aircraft pitch tends to decrease, aircraft is fast, then decrease thrust.
To be continued on next page
ABN-34
7/10
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET , , , , , , , ,
, ,
UNRELIABLE SPEED INDICATION/ADR CHECK PROC - MEMORY
ITEMS (Cont'd)
WHEN FLIGHT PATH IS STABILIZED
PROBE/WINDOW
HEAT........................................................................................................................ ON
TECHNICAL RECOMMENDATIONS:
‐ Respect Stall Warning
‐ To monitor speed, refer to IRS Ground Speed, or GPS Ground Speed variations
�� If remaining altitude indication is unreliable:
‐ Do not use FPV and/or V/S, which are affected.
‐ ATC altitude is affected. Notify the ATC.
‐ Refer to GPS altitude: altitude variations may be used to control level flight, and is
an altitude
cue.R ‐ efer to Radio Altimeter.
CAUTION If the failure is due to radome destruction, the drag will increase and
therefore N1
must be increased by 5 %. Fuel flow will increase by about 27 %.
AFFECTED ADR IDENTIFICATION:
Crosscheck all speed indications and Refer to FPE-SPD Speeds
�� If at least one ADR is reliable:
Faulty
ADR(s).............................................................................................................................
OFF
REMAINING AIR
DATA.................................................................................................... CONFIRM
Alternate sources may be used to evaluate the air data:
‐ GPS altitude
‐ GPS and IRS Ground Speeds, taking into account altitude and wind effect.
�� If affected ADR(s) cannot be identified or all ADRs are affected:
ONE
ADR..........................................................................................................................
KEEP ON
Keep one ADR ON to maintain the STALL WARNING protection.
TWO
ADRs...............................................................................................................................
OFF
This prevents the flight control laws from using two coherent but unreliable ADR
data.
LDG CONF...................................................................................................................
USE FLAP 3
APP
SPD............................................................................................................................
VLS +10
LDG DIST
PROC...................................................................................................................
APPLY
Refer to ABN-80-B LDG CONF/APPR SPD/LDG DIST On Dry Runways Following
Failures - 34 -
NAV
�� To return to departure airport:
Keep takeoff configuration preferably.
Refer to ABN-34-C UNRELIABLE SPEED INDICATION/ADR CHECK PROC -
Approaches
(Pitch & Thrust Tables)
�� To accelerate and clean up after takeoff:
Accelerate and clean up the aircraft in level flight:
THRUST.........................................................................................................................
.... CLB
FLAPS.........................................................................................................................RE
TRACT
Retract from 3 or 2 to 1, once CLB thrust is set.
Retract from 1 to 0, when the aircraft pitch is lower than the pitch for S speed (Refer
to
ABN-34-C UNRELIABLE SPEED INDICATION/ADR CHECK PROC - Level-Off
(Pitch &
Thrust Table) )
Once in clean configuration, Refer to ABN-34-C UNRELIABLE SPEED
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A318/A319/A320/A321QRH快速檢查單QUICK REFERENCE HAND BOOK3(118)