Altimeter Flashcards

1
Q

Altitude units

A

feet or meters

3.28ft= 1m

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2
Q

Height is…

A

height above ground

QFE used for height above aerodrome

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3
Q

Altitude is…

A

height above mean sea level

QNH used. may vary between regions with pressure and temperature

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4
Q

Pressure altitude is…

A

height above standard datum line (1013)

STD-flight levels

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5
Q

indicated altitude

A

reading on altimeter when set to local QNH

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6
Q

True altitude

A

actual elevation above MSL

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7
Q

How the altimeter works

A

purely on static pressure
partially evacuated aneroid capsule
measures change from set reference datum(pilot set QFE or QNH etc)
Calibrated to ISA

descent= more static= aneroid compress= indicate reduction in ALT

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8
Q

Altimeter construction

A
sealed tube 
static inlet
partially evacuated aneroid capsule
leaf spring
metal linkage 
scale
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9
Q

ISA model

A

Rate of change of pressure change feet per hPa in the atmosphere is non linear

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10
Q

density altitude

A

ISA altitude equivalent to pressure altitude

= pressure alt + (isa deviation x 120ft)

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11
Q

Simple altimeter

A
not used
1 needle
no pressure setting knob
single aneroid
basic adjustment to allow 0 feet to be set 
coarse scale- 0-10000ft range
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12
Q

sensitive altimeter

A
common in light 
larger range 
3 needles
pressure setting knob
aneroid stack
jewelled bearings 
vibrator (reduces lag)
digitiser (for mode C height encoding)
easier to read
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13
Q

Servo altimeter

A
more accurate
virtually no lag
aircraft with no ADC
E and I bars (magnets)
mechanical linkages removed 
3 needles 
pressure setting knob 
aneroid stack
stack connected to I bar
relies on electromagnet moving- based on equal gaps between E & I bars 
more accurate
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14
Q

servo altimeter operation- Climb

A

capsules expand
I moves closer to E at bottom
imbalance in gaps
current induced and voltage to servo motor(turns needles)
worm gear and follow up cam re position E bar to equal the air gaps again and stop current

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15
Q

GPS altitude

A

receivers generate gps derived alt value for the receiver based on trilateration of the received gps satellite signals
not affected by temp or pressure
does not provide same separation from aircraft
large aircraft do not display GPS alt

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16
Q

what Altitude errors are there?

A

IMP

Temperature- Actual temp dif to ISA. High to low look out below
barometric- actual pressure Dif from pressure set
time lag- due to friction in in gears and linkages. climb may under read, descent may over read

17
Q

altimeter blockages

A

freeze and not show anything
climb progressively under read
descent progressively over read
unblock using alternate static

18
Q

altimeter leak

A

fracture in static line inside pressure hull (pressurised aircraft) under read due to higher pressure
leak outside pressure hull- less accurate & over read
unpressurised aircraft- low press in cabin causes over read ‘cabin suction’