Auto flight, Navigation, Flight Instruments Flashcards

1
Q

What components make the EFIS?

A

SHEA

  • 3 Symbol Generators
  • 2 HSIs
  • 2 EFIS Control Panels
  • 2 ADIs
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2
Q

How do you know a Symbol Generator has failed?

A

Both HSI and ADI Screens Blank. (If one blanks, its a CRT Failure)

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3
Q

Where does the Symbol Generator get information?

A

FIFA

  • FCCs
  • IRSs
  • FMCs
  • ADCs, A/Ps, Auto Nav Tuning
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4
Q

What does the ALTN EFI Switch do?

A

SIR EFI

  • Selects ALTN / Center
  • Symbol Generator,
  • ILS receiver, and
  • RA.
  • If both CA and FO use the ALTN / C SG, the Left EFIS Control Panel will control both.
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5
Q

What does the FLT DIR Switch do on the INST SOURCE SEL Panel?

A
  • Selects which FCC (L,C, or R) commands the respective FD.
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6
Q

What does the NAV source select switch do on the INST SOURCE SEL Panel?

A
  • Selects which FMC is used by the L/R Symbol Generator and FCC.
  • In ALTN config., you use the opposite side.
  • CDU R/L is used to provide information to the SG during ALTN NAV.
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7
Q

Describe the Alternate Navigation System.

A
  • Used in case of Dual FMC Failure.
  • Two Pages left: IRS LEGS and IRS PROG
  • No LNAV, VNAV, efficiency information…
  • Must go to Perf. Inflight Chapter for V speeds / Power
  • Only Position relative to Existing Waypoints, and IRS (LAT/LONG) information.
  • Conditional waypoints, offsets, and holds are dropped.
  • Old waypoints can still be referenced by their IDs, new waypoints must be entered as LAT/LONG.
  • Existing/CDU Stored course is great circle; new courses are direct.
  • CDUs operate independently, but can be X-displayed.
  • Uses IRS data for navigation.
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8
Q

When is the FD automatically displayed?

A
  • Go Around
  • A/S greater than 80
  • Flaps Not Retracted.
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9
Q

Which buttons on the MCP will command a thrust modes?

A
  1. THR
  2. SPD (when pitch mode is ALT HOLD, V/S, or G/S)
  3. VNAV
  4. FLCH
  5. GA
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10
Q

Describe the Auto Thrust Modes

A
  1. N1 - trying to maintain N1
  2. THR HLD - Servos discon., holds whatever you set.
  3. SPD - Maintains commanded speed on FMA or in FMC
  4. FLCH - 2 Minute rule
  5. GA - goes for 2000fpm.
  6. IDLE - Thrust reduced to idle, as in VNAV descent, or with pitch mode FLARE.
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11
Q

Describe the Pitch Modes.

A
  1. TO - On TO, commands greater of V2+15 / Liftoff+15.
  2. SPD - commanded from FMC or SPD Intervene.
  3. V/S - NO STALL PROTECTION.
  4. VNAV PTH - AFDS will pitch to maintain VNAV profile
  5. VNAV SPD - maintains speed to climb to selected ALT.
  6. VNAV ALT - when FMC and MCP disagree.
  7. ALT CAP
  8. ALT HOLD - it will take snapshot and return to ALT where selected. Also activated when ALT reached as commanded by FLCH or V/S
  9. G/S
  10. FLARE - at 50’
  11. GA - pitch to MCP / Current Speed (whichever is higher).
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12
Q

Describe the Roll Modes.

A
  1. TO - activates at liftoff, to track flight path (extended CL)
  2. LNAV - Activates when in position to turn onto active leg, within 2.5 miles.
  3. HDG HOLD - holds present heading, or rollout heading if pressed while in a bank.
  4. HDG SEL - holds selected heading.
  5. ATT - Default mode. Holds bank.
  6. LOC - will capture within 120degrees of course
  7. ROLLOUT - arms below 1500’ and activates below 5’
  8. GA - no annunciation when active; commands flight path when selected.
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13
Q

What happens during active operations if an autopilot fails.

A
  1. Attitude Stabilizing Mode
  2. Amber line is drawn through the affected mode.
  3. AUTO PILOT LIGHT
  4. EICAS
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14
Q

Walk through a normal AFDS TO and CLMB Profile

A
B4 80kts - N1/TO/TO/FD
at  80kts - THR HLD/TO/TO/FD
at Rotation - thrust for greater of V2+15 or Current +15
at LNAV Selection - THR HLD/TO/LNAV/FD
at FRA - SPD, VNAV SPD, LNAV, CMD
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15
Q

Automatic Flight Windshear Recovery

A
  • Normal GA pitch and roll modes.

- pitch ~15 or slightly below limit, whichever lower.

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16
Q

What does arming APP do?

A
  1. Arm LOC/GS
  2. Arms all three A/Ps
  3. Isolates Power Distribution (C A/P to HOT BATT BUS)
17
Q

Describe ASA (Autoland Status Anuciator) Display

A
  • Displays below 1500’
  • LAND 3 - Fail Operational - 3 A/Ps
  • LAND 2 - Fail Passive - Redundancy Reduced
  • NO LAND 3 - Results in ^^ / Inhibited < 200’
  • NO AUTOLAND - Go-Around, AUTOLAND unable.
18
Q

Describe GA Mode.

A
  • Armed (not displayed) with Flaps Ext. / G/S Cap.
  • Annuciated in FMA when Engaged.
  • Maintains higher of Current A/S or MCP Speed
  • Maintains 2000 fpm
  • Maintains ground track.
  • From Arming to GA & 400’, cannot get rid of it = turn off both FDs and A/P.
19
Q

What is a key difference of the ILS / VOR Modes (on the HSI)?

A

It is heading up, not TRACK UP.

20
Q

Describe the FMS.

A
  • 2 CDUs
  • 2 FMCs
  • Cross Communicate
  • L FMC Primary / Actually provides NAV
21
Q

Describe an FMC Failure

A
  • Respective CDU Blanks
  • EICAS Message
  • MAP and VTK Flags on HSI (no course info)
  • R FMC automatically takes over if L fails.
  • Requires QRH (New YORK New York NO)
  • Selecting Other FMC will bring back CDU
22
Q

Describe the Inertial Reference System

A
  • 60S to 73N, some 82S to 82N
  • 3 IRUs - L,C,R
  • 1 IRS Panel
  • Provides HDG/ATT, PPOS, TK/GS, Wind info.
  • Normally A/C Power, HOT BATT BUS / DC Backup
23
Q

Describe the IRS Alignment Process

A
  • Full Alignment takes about 10 minutes.
  • Must align every 18 hours.
  • To align, select ALIGN;
  • ON DC flash to test, ALIGN light steady illuminated
  • ALIGN Flashing = “NO BAD MOVE”
  • NO PPOS info, BAD PPOS info, A/C MOVEd
24
Q

What are the different PPOS you can give the IRSs, in order of priority?

A
  1. GPS postion.
  2. Last Position
  3. Airport Coordinates
  4. Gate Coordinates