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Errors in Altimeter
Position and Instrument Errors in Altimeter
- Position or Pressure error is caused due to location of pitot head
- Instrument Error is caused due to mechanical imperfections
- Position and Instrument error are corrected on ground
- Residual errors are listed on a correction card
Manoeuvre and Time lag Errors in Altimeter
- Manoeuvre Induced Error causes temporary fluctuations in attitude indications
- Time Lag Error is caused due to sluggish response of capsule to pressure
- Servo assisted altimeter avoids time lag error
Barometric Error
- Barometric error is caused due to change in MSL pressure
Effect of Incorrect QNH Setting
- If incorrect QNH set in sub-scale, indicated altitude would be in error from actual altitude
- If the sea level pressure reduces, the set datum would be lower than MSL
- Altimeter would over read
- If the sea level pressure increase, the set datum would be higher than MSL
- Altimeter would under read
Flight From High to Low Pressure Area
- During a flight from high pressure to low pressure area, the indicated altitude would be higher than true altitude
- True altitude is lower than that indicated by the altimeter
- Altimeter over reads, reducing terrain clearance which is potentially dangerous
Flight From Low to High Pressure Area
- During a flight from low pressure to high pressure area, the indicated altitude would be lower than true altitude
- True Altitude is higher that indicated by the altimeter
- Altimeter under reads, increasing terrain clearance
- Not so dangerous from terrain clearance point of view
Temperature Error – Cold Air
- Consider flight between two places with same Mean sea level pressure
- Colder air has higher lapse rate
- At a particular altitude, the observed pressure is lower
- Indicated altitude would be higher than True altitude
- Altimeter over read in a flight from high to lower temperature region
Temperature Error – Warm Air
- Consider flight between two places with same Mean sea level pressure
- Warmer air has lower lapse rate
- At a particular altitude, the observed pressure is higher
- Indicated altitude would be lower than True altitude
- Altimeter under reads in a flight from low to higher temperature region
Regional QNH
- Regional QNH
- Lowest forecast QNH in an Altimeter setting region
- Issued every one hour for use while flying close to ground
- Ensures minimum terrain clearance
Temperature Variation from ISA Temperature
- Effect of temperature variation from ISA
- For 1 deg colder from ISA – altimeter over reads by 4 ft / 1000 ft
- For 1 deg warmer from ISA – altimeter under reads by 4 ft / 1000 ft
Effect of Pressure and Temperature
- For both Temperature and Pressure
- High to Low – Altimeter Over reads
- Low to High – Altimeter Under reads
Alticor
- Alticor = indicated altitude – true altitude
- Add 30 ft for 1 hPa higher than MSL pressure
- Add 1 % of indicated altitude for ISA +3 conditions
- D value = True altitude – Indicated altitude
Blockage of Static Vent
- Static vent blockage would make the altimeter indicate the altitude at which the blockage occurred
- Under read during climb
- Over read in descent
Leak in Static Vent
- Leakage in static line outside pressurized compartment
- No problem, altimeter would indicate correctly
- Leak in static line inside pressurized compartment
- Altimeter would indicate cabin altitude instead of actual altitude
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