15. Warning Systems Flashcards
(47 cards)
PSEU Light
- Also illuminates for overwing exit flight lock fails to disengage when commanded,
- Inhibited from Thrust Lever advance for T/O until 30s after landing
- For some aircrafts acts also with “Simple Fault” logic,
- In this case illuminates after landing, extinguishes after Parking Brake SET or both engines shutdown
MACH AIRSPEED AND STALL WARNING TEST Switches Inhibit
While airborne
Landing Gear Warning Cutout Switch
Cannot be silenced with Flaps > 10
Current Altitude Alert
- White box shows around current altitude display becomes bold,
- Between 900-300FT before reaching the selected altitude,
- The box turns amber and flashes for 300-900FT deviation from the selected altitude
BELOW G/S P-INHIBIT Light
If pushed below 1000FT RA, inhibits Ground Proximity GLIDESLOPE alert
GRD PROX INOP Light
- GPWS computer malfunction or power loss,
- Invalid signals received from: RA, ADIRU, ILS, IRS, FMC, SMYD computers or EFIS panel
TERR INHIBIT Switch
Inhibits Look-Ahead terrain alerts and terrain display
RUNWAY INOP Light
- RAAS failure,
- GPS position accuracy is inadequate,
- The airport is not in the GPWS database,
- The airport is not in the RAAS RWY database
Terrain Display Color Codes
- Dotted Green: 2000FT below to 500Ft (250FT with gear down) below the aircraft,
- Dotted Amber: 500Ft (250FT with gear down) below to 2000FT above the aircraft,
- Dotted Magenta: No terrain data available,
- Solid Red: Look-Ahead warning is active,
- Solid Amber: Look-Ahead caution is active,
- Solid Green: Highest elevation
Terrain Inhibit Near Airport
Within 200/400FT of nearest airport RWY elevation does not show
Predictive Windshear Auto Pop-up
- Even neither pilot has WXR display selected,
- In Expanded Modes and Center Map Mode,
- If TERRAIN selected, WXR replaces it
Sound Alerts
- Clacker for airspeed,
- Warning tone for A/P disengagement,
- Intermittent horn for Takeoff Config and Cabin Altitude,
- Steady Horn for Landing Gear positions,
- Warning Bell for Fire
Warning Light Colors
- RED: Requires immediate attention,
- AMBER: Requires timely attention,
- BLUE: System information
Importance of MASTER CAUTION or FIRE RESET
Resets the system for future warnings
MASTER CAUTION Associated Area
Outside the normal field of vision of the flight crew
Simple Fault
- Single fault in certain redundant systems,
- Does not illuminate MASTER CAUTION,
- Stored in the system and illuinate during Recall, extinguishes after RESET
MASTER CAUTION Lights and Recall
All 12 lights must be illuminated
MASTER CAUTION OVERHEAD Unusual Lights
- EQUIP COOLING-OFF,
- EMER EXIT LIGHTS-NOT ARMED
Takeoff Configuration Warning
- Trailing Edge Flaps not in the range of 1-25,
- Trailing Edge Flaps are in Skew or Asymmetry or have Uncommanded Motion,
- Leading Edge Devices not configured for takeoff or have Uncommanded Motion,
- SPEED BRAKE Lever not in the DOWN position,
- Spoiler Control Valve is open, providing pressure to Ground Spoiler Interlock Valve,
- Parking Brake is SET,
- Stabilizer Trim not set in the takeoff range
Landing Gear Horn Activation
Flaps Up to Flaps 10:
- Below 800FT, either Thrust Levers between IDLE and 20 degrees,
- OEI Thrust Lever < 34 degrees,
- Can be silenced until 200FT RA
Flaps 15 to 25:
- Either Thrust Lever < 20 degrees (or 34 for OEI),
- Cannot be silenced
Flaps greater than 25:
- Regardless of Thrust Lever position,
- Cannot be silenced
PSEU System Monitors
Proximity Switch Electronic Unit monitors:
- Takeoff Configuration Warnings,
- Landing Configurations Warnings,
- Landing Gear,
- Air/Ground sensing
Stall Warning Purpose
- Natural Stall Warning (buffet) usually occurs at a speed prior to stall,
- In some configurations the margin between stall and natural stall warning is less than desired,
- Therefore an artificial Stall Warning Device, a Stick Shaker is used to provide the required warning
SMYD and Sources
Stall Management and Yaw Damper computers takes data from:
- Alpha Vane AoA outputs,
- ADIRU outputs,
- Anti-ice controls,
- Wing configurations,
- Air/Ground sensing,
- Thrust
SMYD Outputs
- Stick Shaker and Pitch Limit Indicator,
- Airspeed displays,
- GPWS Windshear detection and alert