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Ground Proximity Warning System
Introduction to GPWS
- Ground proximity warning system prevents controlled flight into terrain
- Warns of proximity to the terrain which are potential threats to safety
- Operates in height band 50 to 2450 feet, which is same as radio altimeter
- Automatic selection of operation mode based on flight profile
- Radio altimeter, Mach meter, ADC and Glidepath provide inputs
- Undercarriage, Flaps and Navigation systems also provide inputs
Stages of GPWS Warnings
- GPWS warnings fall under two categories
- Alert is a caution which means advisory instructions.
- Warnings are commands which means obey the instructions.
Mode 1 – Excessive Barometric Descent Rate
- Mode 1 has two boundaries and is independent of aircraft configuration
- This mode activates below 2500 feet on radio altimeter.
- Penetration of the first boundary generates an voice alert of “SINK RATE”
- Audio warning repeats every 1.5 seconds.
- Penetrating the second boundary causes the repeated warnings
- Audio of “WHOOP, WHOOP PULL UP”
- Visual light indication of ‘PULL UP’
Mode 2 – Excessive Terrain Closure Rate
- Mode 2 monitors five parameters to set its boundaries
- Mach, radio altitude, rate of change, barometric altitude and configuration
- Mode 2 operates below 1500 feet at 0.35 mach
- Increase in mach number to 0.45 with gear up increases height to 2450 feet
- Flap override switch overrides the higher portion of envelope
- First boundary triggers an audio alert of “Terrain, Terrain” every 1.5 seconds.
- Second boundary generates audio warning of “WHOOP, WHOOP PULL UP”
- In landing configuration, only the repeating TERRAIN voice alert is heard.
Mode 3 – Descent after Take-off or Go-around
- Mode 3 alerts for descent is made during initial climb or go-around
- The audio alert of “DON’T SINK” is repeated each 1.5 seconds
- Operating height is between 50 and 700 feet of radio altitude.
- Alerts when aircraft descends more than 10 percent of barometric altitude.
- Mode 3 does trigger below 200 feet of radio altitude.
Mode 4A – Unsafe Terrain Clearance – Landing Gear Not down
- Mode 4A operates if aircraft descends below set height without landing gear.
- This mode operates below 500 feet of radio altitude
- Landing gear mode armed after aircraft climbs above 700 feet radio altitude.
- Upper limit increases from 500 feet to 1000 feet radio altitude.
- Below Mach 0.35, the aural alert “TOO LOW GEAR” is heard every 1.5 seconds
- Above Mach 0.35, voice alert “TOO LOW TERRAIN” is heard every 1.5 seconds
Mode 4B – Unsafe Terrain Clearance – Flaps Not in Landing Configuration
- Mode 4B alerts if landing gear is down without flaps below 300 feet.
- Below Mach 0.28, voice alert of “TOO LOW FLAPS” is heard every 1.5 seconds
- Above Mach 0.28, audio of “TOO LOW TERRAIN” is heard every 1.5 seconds
- Upper boundary increases to 1000 feet radio altitude.
- “TOO LOW GEAR” alert takes priority over the “TOO LOW FLAPS”.
- Mode 4B is inhibited by ‘FLAP OVRD’ switch
Mode 5 – Below Glide Slope Deviation Alert
- Mode 5 alerts descent of 1.3 dots below glide slope, below 1000 feet on ILS
- Operates when glide slope receiver is active and landing gear is down
- Hard alert sounds at full volume whereas Soft alert is at reduced volume
- Repetition rate increases with glide slope deviation and reducing in altitude
- Mode 5 is cancelled by pressing ‘BELOW G/S’ light
- Above 1000 feet radio altitude mode 5 will get re armed.
- Mode 1 to 4 audio alerts have priority over mode 5
- PULL UP and BELOW G/S lights could light up simultaneously
Mode 6A – Descent Below Selected Minimum Radio Altitude
- Mode 6A alerts on descent below the minimum decision altitude
- MDA is set using a cursor on captain’s radio altimeter.
- Mode 6A is active between 50 and 1000 feet of radio altitude.
- Audio alert consists of “MINIMUMS, MINIMUMS” sounded only once.
- The mode is re-armed when the radio altitude increases above the MDA.
Mode 6B – Altitude Call-outs and Bank Angle Alert
- Mode 6B calls out at altitudes at pre selected intervals and at minimums
- Normally, calls out at 200 ft and 100 ft to decision height
- Alternately absolute height call-outs from the radio altimeter.
- Mode 6B also calls out “BANK ANGLE” to alert for excessive roll angles.
- Bank angle limits reduce with proximity to the ground
Mode 7 – Wind Shear Alert
- Mode 7 provides visual and audio wind shear warnings based on calculations
- Pilot can initiate quicker wind shear go-around actions.
- Mode 7 warnings take priority over all other modes.
- GPWS calculates the initial conditions for entering an area of wind shear.
Mode 7 – Wind Shear Alert Calculation
- The calculations are based on five inputs
- Ground speed
- Air speed
- Barometric height
- Rate of descent
- Radio altitude
Enhanced Ground Proximity Warning System
- EGPWS provides warnings from rising terrain ahead using TAWS
- Terrain Awareness and Warning System is a world-wide terrain data base
- Terrain ahead is shown in shades of green, yellow and red on a display
- Display could be independent or of weather radar or navigation screen
- Audio warning may be of Caution Terrain Ahead or Whoop Whoop Pull Up
- Voice message in this mode depends on the type of danger
Action on GPWS Warning
- Pilots must take positive and immediate response to GPWS warnings
- Wings level and initiate a maximum gradient climb until minimum safe altitude
- Find the cause of the warning and verify the aircraft’s position.
Pilot Override on GPWS Warning
- Action can be deferred only under the following circumstances
- Positively identification of cause
- Warning has ceased
- During day
- Clear visual conditions
- Obviously not in any dangerous situation with regard to three factors
- Terrain clearance, Aircraft configuration or the Manoeuvre
Runway Awareness and Advisory System
- Runway Awareness and Advisory System increases situational awareness
- Reduce the likely-hood of runway incursions.
- Provides advisory during taxi, take off approach and landing
- RAAS uses Terrain Clearance Floor for its operation
- Terrain clearance floor is a height map in the vicinity of airfields
- Avoids premature descent on non-precision approaches
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