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68 Cards in this Set
- Front
- Back
At whitch altitude Automatic changeover between indicated and Mach occurs |
Approximately what FL 260 |
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What is the symbol for under speed limit |
Flashing "A" |
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What symbol is showing for over speed |
Flashing "8" |
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What are the A/T modes annunciation during VNAV (4) |
FMC SPD N1 ARM RETARD
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What hapen to VNAV ALT airplane while reaching altitude constraints |
VNAV ALT Annunciation reaching MCP altitude. VNAVPATH Annunciation reaching FMC altitude |
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What is the range of the Altlitude Display |
0 to 50,000 by 100 ft Incrememts |
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What is the range of the Vertical speed display |
-7,900 to +6,000 fpm 50 fpm when <1,000fpm 100 fpm when > 1,000 fpm |
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A/T and Pitch modes in LVL CHG |
Climb: N1 and MCP SPD Descent: Retard then Arm and MCP SPD |
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What is the Bank Angle limit when LNAV < 200ft |
8° |
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What is the Bank Angle Limit LNAV > 200ft |
30° |
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How Far fr an LNAV route can you intercepted if not within 90° |
Within 3NM of an Active Route |
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MCP CRS Selector vs VHF |
Capt CRS With VHF1 Autopilot A FO CRS with VHF2 Autopilot B |
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Minimum Altitude for dual chanel ILS |
Prior 800 RA |
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When CWS engages (3) |
Pitch or Roll not Selected Pitch or Roll de selected Pitch or Roll manually Overridden |
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What Happen when approaching a selected Altitude in CWS P Mode |
Pitch Mode Engages ALT ACQ Then ALT HOLD |
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What Hapen when approaching a selected Radio Course with VOR/LOC or APP Armed in CWS R Mode |
VOR/LOC Engages |
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FMA (A/T) Modes (7) |
N1 THR HLD GA MCP SPD FMC SPD ARM (white) Retard |
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Roll Modes (3) |
HDG SEL VOR/LOC LNAV |
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Pitch Modes (9) |
TO/GA V/S MCP SPD VNAV PATH VNAV SPEED ALT/ACQ ALT HOLD G/S FLARE |
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What is the AFS |
Automatic flight system which is autopilot flight director (AFDS)and Auto throttle (A/T) |
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What information the A/T receives from the FMC |
N1 Limits Target N1 Command Airspeed |
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What controls the AFDS |
1 MCP 2 FMC |
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AFDS Consists of |
1 MCP + 2 FMC + 2 FCC ( A & B) |
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What FCCs are doing |
Take info fr MCP and FMC Send control commands to their respective pitch and Roll Hydraulic servos trough 2 hydraulic system in AP Mode. or Position the command bars on FD mode. |
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MCP functions |
Select desire command Mode to AFDS & A/T |
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What can prevent auto pilot or CWS to be engaged |
No force applied on the control wheel STAB TRIM AUTOPILOT cutout SW is at NORMAL |
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Only time when both autopilot can be engaged |
APP Mode |
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Autopilot disengagment |
1 pushing autopilot disengage switch 2 pushing the illuminated autopilot engage switch 3 pushing the autopilot disengage bar down 4 Activating either pilot's control trim Switch 5 moving Stab Trim Autopilot Cutout Switch to CUTOUT 6 Pressing TO/GA SW Single chanel - < 2000ft or - > 2000ft with flaps not up or GS Engaged. 7 - IRS Fail or Fault light illuminated 8 - Loss of Power 9 - Loss of respective hydraulic 10 - Failure of one Radio Altimeter will disengage AP 2sec > LOC and GS Capture 11 - Loss of an Engine 12 - Heavy demand or Loss of Engine driven Hydraulic pump system A may disengage the AP.
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Dual channel autopilot operation is possible only when 2 |
Generators are powering the buses |
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Is Take Off mode FD Mode or AP mode |
It's a FD mode Only |
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Is FD having flare capability |
NO bars retract arround 50 RA on an ILS approach |
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How it is indicated the master FCC |
Illumination of the respective master FD indicator light |
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N1 Autothrottle Mode |
Maintain Trust at selected N1 and maintain N1 Limit |
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Autothrottle Mode in GA |
Maintain Trust at reduced Go Arround setting |
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Autothrottle Mode "RETARD" |
When Trust levers move to aft stop . Followed by ARM Mode |
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FMC SPD Autothrottle Mode |
Maintain Speed command by FMC with N1 limits |
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MCP SPD Autothrottle Mode |
Maintain IAS/Mach set in the MCP with limit N1 |
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THR HLD Autothrottle Mode |
AT servos inhibited and levers can be adjusted manually |
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Autothrottle Mode "ARM" |
No AT Mode Engaged Servos inhibited Can be manually moved |
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TO/GA Pitch Mode Take Off |
On the Ground Both FD Swv must be on 10° nose down to 60kt 15° nose up > 60kt 15° nose up > lift off until sufficient climb rate then MCP speed plus 20kt. TOGA can be engaged with FD sw off if Pushed > 80kt and < 2000RA + prior150 sec |
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Go-around Pitch Mode |
Engage in GA if button pushed And - < 2000ft RA inflight - > 2000ft RA in flight ( flaps not up or GS captured ) Either FD On or Off Ground Track + 15° Nose Up After reaching g a programmed rate of climb FD targets pitch for each Flaps Setting @ Max Gross Weight |
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When is FLARE ( armed ) Displayed (3) |
Dual AP app > LOC and GS Capture < 1500 RA |
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When is FLARE ( Engaged ) |
Dual AP ILS app At 50 RA |
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When LNAV engage on Take off |
At 50 RA |
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AT disengagement |
AT armed SW to OFF AT Disengage SW AT system fault 2 sec after touchdown Trust levers separated > 10° in very Specifics Conditions |
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What are the Automatic Flight Operations (4) |
Take Off and Climb Enroute Approach and Landing Go-Around |
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On Take OFF the pitch is 15° what is the pitch if loosing an Engine. |
Pitch V2 if below V2 V2- V2+20 if between V2 and V2+20 V2+20 if above V2+20
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When THR HLD on |
84kt to 800 RA then ARM and reduction can be made by pressing N1 |
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With Airplane without Trust Auto Réduction Altitude selection when it is reducing trust automatically |
When VNAV, ALT ACQ and ALT HLD |
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What terminates T-OFF Mode |
Engaging CMD mode Giving MCP SPD if no VNAV armed on the ground |
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At what altitude VNAV and LNAV engage on T-Off |
LNAV @ 50 RA VNAV @ 400 RA |
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On a Dual Chanel approach when is the 2nd AP Engages |
After LOC and GS Captures and < 1500 RA |
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How many dots the LOC is Captured |
No later than 1/2 Dot |
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On dual Chanel Fail Operational What is the system doing @ 1500 RA
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2nd AP Engage Test of the ILS Test of AP Ruder Servo FLARE armed AP GO Around Mode armed (but not annunciated) (Single CH changes for ROLLOUT Armed in some airplanes) |
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What verify @ 500 RA on Dual Ch Fail Operational Aurplanane |
LAND 2 or LAND 3 Annunciated |
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On Fail Operational when and Where is ROLLOUT Annunciated |
2 RA Roll Mode replacing VOR/LOC |
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Difference between Engaging CWS And Deselect roll or pitch to go CWS |
CWS selected is a FD Mode When de selecting pitch or Roll independently CMD remains engaged and ALT ACQ or LOC cap works |
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How to exit APP MODE After LOC + GS are Captured (3) |
Pushing TOGA SW Disengage AP and FD SW off Retuning à VHF NAV Freq |
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What is the max Side Slip Angle in Autoland |
5° |
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Is a single engine Approach < 50ft authorized. APU Provinding second source of électronique for dual APP |
No APP < 50ft and Autoland single engine |
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Can you engage second AP in single engine ILS |
Yes to use the AP GO Arround Mode + Rudder Auto Compensation IF APU use as second power source And Do not continu < 50ft |
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On Fail Operational When is the RWY alignement Starts |
@ 450ft |
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When AT Go Arround Mode Armed ? |
< 2000 RA > 2000 RA if flaps not up or GS capt With or without AFDS Engaged |
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When is AP GO Arround Mode Armed ? |
When Flare Armed Annunciated up to AP sensing Touchdown And DUAL AP Engaged |
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In Auto GO Arround Mode AT gives ? Roll is ? And Pitch is ? |
AT Gives reduced GA Thrust N1 for 1000-2000ft/min
Roll is ground Track and some airplanes Ground track up to 400 RA then LNAV.
Pitch Gives 15° up to programmed Rate of Climb then Target airspeed for each Flaps setting |
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Single Engine FD Go Arround |
The same as automatic GA Except: FD Indication Only In some airplane Roll Mode changes from Ground Track to LNAV @ 50ft (vs 400 in Auto GO Arround) The pitch is 13° then Target airspeed dépending when the failure has occured but never less than V2 except in WS.
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FD Go Arround |
Same as Auto but FD Indications only |
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Auto GO Arround Mode When pitch is ALT ACQ What is the AT Mode annunciated |
MCP SPD The Speed window will open. |