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TR > 15 Warning Systems > Flashcards

15 Warning Systems Flashcards

1
Q

🛑 TAKEOFF CONFIG

A

on ground when throttles advanced if aircraft not correct T/O config. WITH aural warning

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2
Q

🛑 CABIN ALTITUDE

A

cabin altitude ABOVE 10.000 feet, extinguished below. WITH aural warning

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3
Q

STALL warning test
MACH warning test

A

S - on ground with AC power available
M - prohibited in air

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4
Q

Landing Gear warning cutout switch, when pushed:

A

Silences LG configuration warning at flaps up - flaps 10 and above 200 feet RA

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5
Q

Selected altitude alert
Current altitude alert

A

selected: white box around selected altitude, BOLD box around current altitude: between 900’-200’ before reaching selected altitude

Current: amber blinking box around current altitude until 200 feet deviation. The flashing continues when: between 900’-200’ before reaching selected altitude or selecting a new altitude

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6
Q

BELOW GS light, when pushed:
🟧 INOP, illuminated:

A

Inhibits ground proximity Glideslope alert when below 1000’ RA
🟧: GPWS computer malfunction OR power is lost: has inputs from ILS, IRS, Stall management computer, ADIRU, EFIC control panel, radio altimeter, FMC

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7
Q

GROUND PROXIMITY SYSTEM TEST
- push
- in flight

A

On ground:
- lights: below GS, GPWS INOP
- ND: TERR FAIL, TERR TEST, TERRAIN (caution)
- aural sounds: “Glideslope, PULL UP, WINDSHEAR, TERRAIN TERRAIN PULL UP, OBSTACLE OBSTACLE PULL UP, AIRSPEED LOW”
- alerts: PULL UP + WINDSHEAR
Followed by:
- alerts: radio altimeter based, bank angle, wind shear, look ahead terrain,
- callouts: appraoch

PROHIBITED in flight

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8
Q

Terrain Display
- armed
- aircraft 500’ or more above highest terrain in selected range

A

A - when in: PLN, CTR VOR, CTR APP

  • Solid 🟩: highest elevation terrain
  • High-density dotted 🟩: intermediate elevation terrain
  • Low-density dotted 🟩: lowest elevation terrain
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9
Q

Terrain Display
- when aircraft less than 500’ above highest terrain in selected range
- exception
- when does it automatically show

A
  • Solid 🛑: look ahead terrain warning active
  • Solid 🟧: look ahead terrain caution active
  • Dotted 🛑: terrain > 2000’ above aircraft altitude
  • Dotted 🟧: terrain 500’ below- 2000’ above aircraft altitude
  • Dotted 🟩: terrain 2000’ below - 500’ below aircraft altitude
  • Dotted 🟪: no terrain data available
  • Exception: terrain within 200’ of nearest airport RUNWAY elevation does not show

Auto show:
- neither pilot has terrain display selected, and
- Look-ahead terrain alert occurs, and
- EXP MAP, VOR, APP, center MAP

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10
Q

Predictive wind shear
- automatically on ND when

A
  • predictive wind shear alert occurs
  • neither pilot has WXR radar display selected
  • in EXP MAP, VOR, APP, CTR MAP
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11
Q

TCAS CONTROL
- transponder mode selecter

A

A - sets TCAS display at UPPER elevation limits
B - sets TCAS display at LOWER elevation limits

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12
Q

TAKEOFF CONFIG WARNING

A
  • TE flaps not F1-F25 and/or uncommanded position
  • LE devices not TO position or uncommanded position
  • speed brake lever NOT down
  • HYD fluid to ground spoilers interlock valve
  • STAB trim not in (green) TO range
  • parking brake set
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13
Q

LANDING GEAR LEVER HORN
- F UP- F10
- F15 - F25
- F30 - F40

A

WHEN LG NOT DOWN AND LOCKED

F UP - F10
- alt< 800’ RA, either thrust lever set between IDLE - 20 DEG thrust lever angle or OIE and operative thrust lever < 34 DEG thrust lever angle
- landing gear warning horn can be silenced until descending below 200’ RA

F 15 - F 25
- either thrust lever between IDLE - 20 DEG thrust lever angle or OEI and operative engine thrust lever below 34 DEG
- Landing gear warning horn CAN NOT be silenced

F 30 - F 40
- Regardless of thrust lever position
- Landing gear warning horn CAN NOT be silenced

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14
Q

PSEU monitors:

  • pseu light illuminate for single warning:
    – when extinguished
  • pseu light inhibited
A

T/O + LDG config warnings, landing gear warnings, air/ground sensing

P - ONLY after landing
W – when parking brake is set or both engines turned off
P - in flight, thrust levers advanced for TO power until 30 seconds after landing

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15
Q

Stick shaker
- where and when

A

One on each control column vibrate and are always armed except on the ground

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16
Q

SMYD computers determine when stall warning is required upon:
- sends signals to

A
  • Alpha Vane AoA outputs
  • ADIRU outputs
  • air/ground sensing
  • FMC outputs
  • anti-ice controls
  • wing configurations
  • thrust

S - PLI

17
Q

Altitude alerting
- inhibited

A

I - when trailing edge flaps are extended to F25 or greater OR when G/S is captured

18
Q

GPWS
- provides alerts based on
- alerts are for:
- Windshear warning priority over

A

P - Radio altitude and combination of: altitude, airspeed, glide slope deviation, and airplane configuration

Alerts are for:
- excessive descent rate
- excessive terrain closure rate
- altitude loss after Takeoff or Go-around
- unsafe terrain clearance when not in landing configuration
- excessive deviation below the ILS or GLS glide slope or the FMC generated flight path angle
- excessive deviation below glide path

W - over look-ahead terrain alert and radio altitude based alerts

19
Q

Look-ahead terrain alerting
- based on:

A

Based: on airplane’s position, barometric altitude, vertical flight path, and ground speed

20
Q

Look-ahead terrain alerting
- TERRAIN TERRAIN, PULL UP
- CAUTION TERRAIN
- TOO LOW, TERRAIN

A

T - 20-30 seconds from impact with terrain shown 🟥 on NAV display: PULL UP on both attitude indicators
C - 40-60 seconds from impact with terrain shown 🟧 on NAV display
T - Descent below unsafe radio altitude: PULL UP on both attitude indicators

21
Q

Radio altitude based alerts
- PULL UP
- TERRAIN
- DON’T SINK
- GLIDESLOPE
- SINK RATE
- TOO LOW, FLAPS
- TOO LOW, GEAR
- TOO LOW, TERRAIN

A

ON ALL PULL UP ON BOTH ATTITUDE INDICATORS

PULL - follows SINK RATE alert if excessive descent rate continues, follows radio altitude based TERRAIN alert if excessive terrain closure continues
TERRAIN - Excessive terrain closure
DON’T SINK - Excessive altitude loss after takeoff or go-around
GLIDESLOPE - deviation below GS or GP, ground proximity light cancels or inhibits below 1000’RA when pushed
SINK RATE - excessive descent rate
TOO LOW, FLAPS - unsafe terrain clearance at low airspeed with flaps not in normal landing position. Push flap inhibit, inhibits the alert
TOO LOW, GEAR - unsafe terrain clearance at low airspeed with LG not down. Push gear inhibit inhibits the alert
TOO LOW, TERRAIN - unsafe terrain clearance at high airspeed with either LG not down or flaps not in LDG position. Follows DON’T SINK if another descent is initiated after initial alert

22
Q

Obstacle alerts
- OBSTACLE OBSTACLE, PULL UP
- CAUTION OBSTACLE

A

O - PULL UP on both attitude indicators, 20 - 30 sec from impact 🟥 on ND
C - 40 - 60 sec from project impact 🟧 on ND

23
Q

Windshear alert
- detected by
- enabled when
- when does detection begin
- when does WX radar begins scanning:

A

D - GPWS
E - below 1500’ RA
W - windshear detection begins at rotation
When
- thrust levers set for takeoff, even if engine is off or IRS not aligned, or
- in flight below 2300’ RA (predictive wind shear alert issued below 1200’ RA)

24
Q

Windshear
- WINDSHEAR AHEAD
- GO AROUND, WINDSHEAR AHEAD
- MONITOR RADAR DISPLAY

A

Predictive wind shear symbol on ND display shows its position on all 3 types.

  • WINDSHEAR: 🟥 Symbol on both attitude indicators, 🟥 wind shear symbol + message on NAV display. wind shear close and ahead of airplane. Enabled during takeoff below 1200’ RA
  • GO AROUND, WINDSHEAR: 🟥 Symbol on both attitude indicators, 🟥 wind shear symbol + message on NAV display. wind shear within 1.5 miles and directly ahead of airplane. Enabled during approach below 1200’ RA
  • MONITOR RADAR DISPLAY: 🟥 Symbol on both attitude indicators, 🟥 wind shear symbol + message on NAV display. wind shear symbol on ND, 🟧 wind shear message on ND. wind shear within 3 miles and ahead of airplane, enable during takeoff and approach below 1200’
25
Q

Windshear
- when alert available
- predictive wind shear alert area:
- when new predictive wind shear caution alerts are inhibited

A

W - approximately 12 seconds after WX radar begins scanning for wind shear. predictive wind shear alerts can be enabled prior to TO by pushing EFIS control panel WXR switch

predictive wind shear alert area
- On GND: .5 nm(side) - 3nm(ahead), 30 DEG L and 30 DEG right
- in FLT: .5nm (side) - 1.5nm(ahead), 30 DEG L and 30 DEG R up to 3NM

When: during takeoff and landing are inhibited between 80 KTS and 400 feet RA. A new warning alert between 100 KTS and 50 feet RA. these inhibits do not remove existing predictive wind shear alerts.

26
Q

Bank angle alert
- what alert and when provided, and what inputs

A

W - provided by GPWS when there is excessive roll of airplane. Silent until system is reset at 30 DEG bank. Inputs from radio altitude and bank angle
- from 3 - 30 feet AGL: alert sounds when the bank angle exceeds 10 DEG
- from 30 - 130 feet AGL: alert sounds linearly from bank angle 10 DEG at 30 feet AGL - bank angle 35 DEG at 130 feet AGL
- above 130 feet AGL, alert sounds when the bank angle exceeds 35, 40 or 45 degrees

27
Q

IAN Autopilot alert
- when

A

Autopilot engaged below 100 feet RA with either FAC or G/P engaged

28
Q

TCAS
- TA , RA
- proximate traffic
- TCAS auto show on ND

A

TA 40 sec, RA 25 sec
Prox - within 6 miles and 1200 feet vertically but NOT expected to cause TA/RA
AUTO - when:
- transponder mode selecter in TA ONLY or TA/RA, and
- a TCAS TA or RA occurs, and
- neither pilot has the TCAS display selected, and
- in CTR MAP, EXP MAP, VOR, APP

29
Q

TCAS Inhibits
- INCREASE DESCENT RA
- DESCENT RA
- RA
- ALL TCAS
- ALL TCAS

A

INC - inhibited below 1500 feet RA
DES - inhibited below 1100 feet RA
RA - inhibited below 1000 feet RA, below 1000 feet RA when TA/RA mode selected on transponder panel, TA only mode is enable automatically and TCAS message. TA ONLY displays on ND
ALL TCAS - voice annunciations are inhibited below 500 feet RA
ALL TCAS - inhibited by GPWS and wind shear warnings

30
Q
A

TR (18 decks)

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