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A reads text to speech;
190 Cards in this Set
- Front
- Back
- 3rd side (hint)
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CCAS T/O inhibited alerts |
Oil/Smoke All cautions except Efis Comp, eng (ADC switch fault), Flt Ctl if TLU or ail lock or pitch disconnect, GPWS Fault, parking brake, maint pnl |
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T/o Inhibition canceled by |
- LDG rétraction - Pressing RCL |
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What is the purpose of CLR Pb |
Clear all CAP amber lights except : prkg brake, gpws, maint panel When corrective action done but malfunction remain push the clr to allow the CCAS to detect another failure |
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Emergency audio cancel switch |
Cancels all aural alert for the entire flight exept : - ldg - vmo, vfe, vle - stall - pitch trim whooler - AP OFF Réactivation : - next a/c energized - MFC 1B/2N reset - pressing rcl - pressing t/o pb |
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Emergency audio cancel switch canceled |
A/c energized again MFC 1B/2B reset RCL pb T/O inhibited pb pressed |
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Stick shaker/pusher inhibited |
On ground 10s after lift off When descending below RA 500ft |
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Can CC access the cockpit when door selected off? |
Yes via emergency |
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How to cancel emergency entry in cockpit |
Deny within 30s after CC push Emergency |
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Deny inhibit entry and alert for ? |
3min |
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MFC primary and alternate supply |
MFC 1A : dc ess/dc emer 1B : bus 1 / main 2A : dc emer/ main 2B : Bus 2/ emer Primary -> alter < 19V altern >22V Altern -> primary => prim > 22v |
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Precautions when testing weather radar or in other position than stby |
- security sector of 3m/130deg - not during refuel of a/c or other a/c <30m - not toward any large size metal object < 30m radius |
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Mrw |
22970 |
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Mrw |
22970 |
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Mtow |
22800kg |
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Mlw |
22 350 kg |
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MZFW |
20 800 kg |
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Alt and T for t/o and land |
-1000ft to 8500ft - 35C to 50C |
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TCAS RA CLIMB or increase climb inhibition |
Flaps 15 at TO AND FLAPS 30 : increase climb In icing : Flaps 0 z> 20 000ft RA climb Flaps 30 climb All increase inhibited
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TCAS ground operation |
Taxi : STBY T/O : xpdr alt + tcas Auto |
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All TCAS RA inhibition => TA only |
Climbing 1100ft Descending 900ft |
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TA only |
Engine out Stick pusher/shaker failure Flight with landing gear down |
Prevent to much AOA in case of RA |
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Max pressure refueling |
50 Psi |
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Each electric pump is able to supply how many engine ? |
Only 1 |
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Max TQ feather operation |
66,6% |
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Max TQ feather operation |
66,6% |
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Min NP in Icing condition |
82% |
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Fuel T starting and operating |
- 38 starting - 48 operation |
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Feed lo pressure |
4 Psi |
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Jet pump low pressure threshold and alert? |
5psi No alert only Run on electrical pump |
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Propeller anti-icing inhibited |
63% NP |
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Fuel governing mode inhibition |
EEC off or fault PEC Off |
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ACW frequency |
341 Hz to 488Hz |
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ACW frequency |
341 Hz to 488Hz 115VAC |
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ACW engagement Np |
Np 70,8% |
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Single DCgen opération limit |
Isa + 25 20 000 ft max |
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Dc Gen max load |
400 A none 600 A 2min 800 A 8sec |
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Max load TRU |
60A none 90A 5min |
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Max load ACW |
20 KVA none 30 KVA 5min 40 KVA 5s |
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Max load inv |
500Va none 575 VA 30min 750 VA 5min |
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Parameters RTO |
5min Tq 100% np 100% ITT 800c NH 103% OIL P 55-65 and T 0 to 125deg |
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Paramet T/O |
TQ 90% NP 100% ITT 740-765 NH 101% Oil 55-65 T 0 125 |
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MCT PARAM |
TQ 90,9% (100% 42) NP 100% ITT 800 |
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MCT PARAM |
TQ 90,9% (100% 42) NP 100% ITT 800 |
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CLB param |
TQ 97% (109% 42) NP 82% |
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ITT starting |
840 for 20s 950 for 5s |
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ATPCS arming condition (5) |
A/C on ground or in flight Pwr mgt set to T/O Pla > 49deg TQ > 46% ATPCS Pb on |
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White bug |
Vfto Vx VmLB0 Single engine climb speed |
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White bug + 10 |
Vy VmHB0 |
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TLU Auto mode HO and LO |
Accélération 185kt Décélération 180 |
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Xwind limit without TLU |
15kt x1,5 LDR |
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Bleed Xfeed valve open ? |
On ground with Eng 2 un hôtel mode |
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Bleed Xfeed valve open ? |
On ground with Eng 2 un hôtel mode |
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Bleed valve closes when (6) |
OVHT LEAK FIRE HANDLE ATPCS Starting sequence PROP BREAK SELECTED ON FOR LEFT BLEED VALVE |
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Bleed duct leak |
> 153deg BLEED VALVE, HP Pack valve, Pack valve close |
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Bleed duct leak + consequence |
> 153deg BLEED VALVE, HP Pack valve, Pack valve close |
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Bleed duct ovht |
> 274 deg Can be reset |
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Pack valve OVHT protection |
Close if T> 204deg downstream pack compressor => fault on pack pb T> 88deg downstream of mixing chamber => temperature control valve closes to reduce hot air flow T>92deg in duct after Mixing C => pack valve DOES NOT close + OVHT + MC |
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Cabin depressi rate after landing |
550fpm |
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Cabin ROD norm and high |
Normal -400fpm High -500fpm |
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Cabin depressi rate after landing |
550fpm |
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Cabin ROD norm and high |
Normal -400fpm High -500fpm |
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Turbofan (pack) activation |
Always on ground IAS< 150kt with LDG down or up but less than 10min Engine low oil pressure + IAS< 150kt |
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How to engage YD |
Depressing AP DEpressing only YD |
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Does AP disengage when YD is disengaged? |
Yes |
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AP automatic disengagement (4) |
- one engagement condition is no longer meet - stall warning - Disagreement between 2AHRS or 2 ADC - mismatch between 2 pitch trim |
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AP manual disengagement |
- AP Pb - YD pb - AP quick disconnect pb - action on pitch trim - GA pb - force > 30N on Rudder - force > 20N on pitch |
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Failure which Use of AP prohibited |
Pitch mistrim Pitch trim fail |
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Dashes on ADU = |
Loss of ASBC bus |
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Normal voltage reading for battery |
23-28V with load 25-28V without load |
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Weak battery consequences |
Automatic protection : - shedding of DC SVCE + Utility Bus - BTC open => loss of DC Bus 1 - GCU disconnect GEN 2 => loss of DC Bus 2 |
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Main Battzry charge pb function and désactivation (3) |
Close contact or between main battery and DC Bus Automatic off when : - thermal RWY (fault + MC) - under voltage detected - battery toglle switch on OVRD |
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Dc SVCE bus and utility bus loss |
- BPCU detect abnormal operation of the bus or overload - bus pb on FAP on shed (not visible from cockpit - bus pb on cockpit (shed on FAP) |
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Reset SVCE bus |
1- pb on FAP on 2- reset BTC 3- reset bus in cockpit |
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Fire handle pulled consequences |
- feather - engine fuel LP valve close - engine bleed valve close - Bleed HP valve - de ice and isolation valve close - désactivation of DC and AC Gen - activation and illumination of squib |
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Lavatory automatic fire extinguisher trigger |
78-80c |
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Halon and water extinguisher capacity |
Halon 1kg 13s Water 2L 40s |
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PAX O2 |
30min |
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Pitch trim fail and AP? |
Should disconnect and not réengage |
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Roll trim on which aileron ? |
LH |
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How many pitch trim tab? Supply ? Principle? |
2 pitch trim on each aileron Electrical actuator Connected via flexible shaft |
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O2 Pressure before flight 02 Lo pr |
1400psi 50psi |
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Ra fail |
- dash on EADI - GPWS Fault + other system using RA - TCAS on STBY |
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Ra fail (3) indication and action |
- dash on EADI - GPWS Fault + other system using RA - TCAS on STBY |
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RA range |
-20 to 2500ft |
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Ra transmit info to |
CCAS GPWS FDAU AP SGU |
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Ra indication |
White box = 100ft above Dh un white bow = RA < DH |
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Deceleration height high speed app |
IAS x 10 = ft |
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RWY width certification |
> 30m If 14m Vmcg + 5kt |
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System that cannot be reset |
EEC Pec Cab press mode sel Bat chg Bleed valve in case of bleed leaks Dc Gen in case of bus failure |
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AHRS Accuracy |
ATT +-1,4 HDG +-2 |
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DGR on EHSI |
Unable RNP |
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Pitch roll att disagreement trigger |
> 6 |
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CVR + DFDR activation |
Auto energized with DC GEN on Stop 10min after engine shut off |
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Hydraulic OVHT Trigger |
121 |
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Engine de ice fault triggered by |
T> 230 P < 14 psi Inflation sequencing incorrect No Pressure detected but valve open Pressure detected but valve closed |
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Engine de ice fault |
T> 230 P < 14 psi Inflation sequencing incorrect No Pressure detected but valve open Pressure detected but valve closed |
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Airframe de icing fault |
Pressure detected but distribution valve closes No pressure but distribution valve open |
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Normal mode of de icing : fast or slow ? |
Fast => 60s pb released 0 |
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WX Range |
300nm 45deg on each side 15deg tilt up and down |
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WX Range |
300nm 45deg on each side 15deg tilt up and down |
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Color scale in gmap mode and source of info |
Black, pale blue, yellow and magenta Use map of egpws (TAD) |
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When TERR pb should be released |
Inhib enhanced mode Take off or approach to airport without EGPWS data base |
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Vmo wipers |
160kt |
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Max xwind dry |
35kt |
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Max xwind dry |
35kt |
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Max Xwind braking action 5 |
28kt |
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Max xwind dry |
35kt |
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Max Xwind braking action 5 |
28kt |
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Max Xwind braking action 4 |
22kt |
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Max xwind dry |
35kt |
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Max Xwind braking action 5 |
28kt |
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Max Xwind braking action 4 |
22kt |
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Max Xwind braking action 3 |
16kt |
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Max xwind dry |
35kt |
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Max Xwind braking action 5 |
28kt |
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Max Xwind braking action 4 |
22kt |
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Max Xwind braking action 3 |
16kt |
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Max Xwind braking action 2 |
16kt |
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Max xwind dry |
35kt |
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Max Xwind braking action 5 |
28kt |
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Max Xwind braking action 4 |
22kt |
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Max Xwind braking action 3 |
16kt |
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Max Xwind braking action 2 |
16kt |
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Max Xwind braking action 1 |
10kt |
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Va |
175kt |
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Vmcl |
98kt |
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Vra (maximum rough air) |
180kt |
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Speed of extract fan |
Dépend on flight deck temperature Minimum if T<20 Maximum if T > 52 |
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When extract fan stop |
OVBD pb released => OVBD val le partially open in flight During 120s during engine start |
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When OVBD CLOSES AUTO |
On ground with engine 1 running In flight |
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Bank pb on ADU |
Hi bank = max 27 Lo bank = max 15 |
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A/erect pb illuminated amber when |
Tas most from both ADC |
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Ap engaged and coupled with SGU failure |
Both CRT on one side are lost Upper mode lost (all mode with SGU computation ) Select valid SGU and AP Recovers |
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Consequence of ADC 1 failure |
- Ap loss upper modes but ca be réengaged - GPWS Inop -Lansing élévation in pressure altitude - incorrect torque bug pointer (show 23%) - TAT/SAT Loss |
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Roll aileron trim |
Electrical tab on LH aileron |
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How control forces is reduced on each control surfaces? |
Spring tab |
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Pressurisation of the hydraulic system |
2 Electric pump energized by ACW power 1 electric pump powered by DC Power |
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Hydraulic tank |
Non pressurised 9,6L but low level alert on each section <2,5L |
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Hrydaulic system low level alert |
<2,5L on each section Xfeed valve inhibited Check lost equipment |
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Hydraulic OVHT |
>121 in pump drain line |
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Antiskid breaking action inhibited at touchdown |
Wheel spin up speed > 35kts or 5s |
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Antiskid touch down protection |
Inhibit anti skid until wheel speed > 35kt or until 5s after touchdown |
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Block wheel protection action |
Speed > 23kts + 50% of difference speed between a wheels |
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Anti skid locked wheel protection |
Available with a speed > 23kt If wheel speed difference > 50% activation of this protection => brake on slower wheel is released |
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Anti skid availability |
LDG down and locked Speed > 10kts But can test even in flight |
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Conditions for thé APM to perform calculation |
APM Pb on SAT < 10c 2 engines on LDG Up Flaps 0 Ice accretion detected or at Icing AOA on or Aiframe pb de icing on |
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Increase speed |
IAS < icing bug + 10kt in climb add the loss of ROC |
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Increase speed |
IAS < icing bug + 10kt in climb add the loss of ROC = severe drag |
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Degraded perf |
Significant decrease of IAS or ROC => recommanded to accelerate to icing bug + 30 or at least +10 And if not possible reduce to low bank |
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Break temperature Hot |
150 |
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LDG not safe CCAS alert |
Any gear not down and locked Flaps 30 RA < 500ft |
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Engine oil lo pr |
40PSI |
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Yellow bug for approach |
VGA = 1,1 VMCA |
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Fuel clog light on / fuel bypass |
Light on > 25psi Bypass > 45psi |
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EEC Function |
- Ensure minimum prop speed control on ground and at low power - automatic up trim - controls opening of HBV |
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Fast/Slow indicator |
+-5,5 to 11 25< deviation < 15 index half visible >25 no visible < -11 deviation remain visible |
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Flaps asymmetry |
> 6,7 |
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Blue ext flag on flaps indicators |
= flap valve is hydraulically commanding flap extension If flaps already extends with this flag = hydraulic leak |
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Flaps unlock |
Spurious recreation > 4deg |
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Nac OVHT |
170 |
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Pack valve function |
- pack shutoff - flow control |
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Pack valve function |
- pack shutoff - flow control |
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Packs function |
Regulate - air flow - temperature (+ removed moisture and pressurize bleed air ) |
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AP Engagement without FD mode or using TCS |
Maintien pitch if +-15 or return to max 15 pitch BA < 6 wing level + Maintain heading 6< BA < 35 maintain BA BA >35 Return to 35 |
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Loc and GS scales flash |
Excessive deviation |
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Stall alert |
Cricket |
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Stall alert |
Cricket |
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Overspeed aural alert |
Clacker |
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Ap disconnect aural warning |
Cavalry |
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Function of emer audio pb |
Cancel specific aural alert in case of false system indication |
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In case of MFC 1B and 2B |
All level 2 + level 3 alerts : config + eng oil + prop brk » are not processed All other level 3 processed but NO MW and CRC AND not displayed on CAP |
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CLR Pb |
Clear only caution alert |
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Zone 3 Amber lights |
Prkg brake / GPWS fault / maint pnl Can be relive only by corrective action |
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Climb speed with icing With ice accretion |
Icing = red bug Ice accretion = red bug + 10 |
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Prop Anti icing model pb modes |
Released = norm = 0< T < -10 = 50s cycle Fast = - 10 < T < -30 = 80s |
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Prop Anti icing model pb modes |
Released = norm = 0< T < -10 = 50s cycle Fast = - 10 < T < -30 = 80s |
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De icing mode sel Pb |
Released = fast = T > -20 = 60s Pb in = slow = T < -20 = 180s |
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De icing ovrd pb function and fault |
Fault : MFC modules for air intake boots control fail OVRD : emergency de icing activation (sequence 60s) |
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Mode sel auto pb function and fault |
Fault = MFC and/or ADC fails FAST mode automatic activated Function = manage boots cycle with ADC and MFC |
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ACW GEN on line And give power |
66% NP on line 70,8% available |
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Max cabin differential pressure |
6,35 to -0.5 |
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AP Pitch Actuator |
RH Column |
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ITT Max to abort t/o |
765 |
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How jet pump motive flow valve closed? |
By pump pb off |
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Does electrical pump goes on if fuel lo lvl ? |
Yes pumps run of fuel lo lvl |
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In case of one loop off does engine fire is triggered ? |
Yes because they are in parallèle Engine fire : - both loop detect fire - only one loop |
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Pack valve delay ? |
Left no delay Right : 6s delay for max confort |
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Operations with CCAS Failure |
MFC 1B 2B fail : - MC on but do not flash - MFC Amber light on CAP - MFC 1B 2B fault light => level 2 alert + config + oil + prop brake level 3 alerts not processed All other level 3 processed but without LW and CRC |
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Yaw trim ? Electrical or mechanical ? |
Electrically controlled and actuated Yaw trim motor |
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Évitement d’orage en zone terminale |
3Nm |
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