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AVIA 110 - Lab Exercise# 10
1) How does ca
uretor ice form, how is the pilot made aware of it (fixed pitch prop, and
how is it removed. How is the ca
uretor heat system tested?
2) With regard to ca
uretor ice, what advantage does a fuel injection system have?
3) What are five dangers of structural ice?
4) With regards to ground icing (dew-frozen, frost, or snow), which needs to be completely
emoved before flight?
5) Describe rime ice with regards to:
a. Appearance
. Temperature of formation
c. Speed of building
d. Effect on airfoil aerodynamics, aircraft weight, or both
e. Ease of removal in flight
f. Recommendation for flight changes if encountered
6) Describe clear ice with regards to:
a. Appearance
. Temperature of formation
c. Speed of building
d. Effect on airfoil aerodynamics, aircraft weight, or both
e. Ease of removal in flight
f. Recommendation for flight changes if encountered
7) List two ways that large Liquid Water Content (LWC) and Supercooled Large Droplets
(SLD) produce the most dangerous icing conditions.
8) What is meant by runback icing and what is its danger?
9) How is freezing rain produced and how should the flight be altered if it is encountered?
10) How are the following PIREP's interpreted:
a. . ......... / IC SVR RIME XXXXXXXXXXDURD
. . ......... ./ IC MOD MIXED 090 IN CLOUDS
c. . .......... / IC LGT RIME XXXXXXXXXXDURD ON FINAL RWY 6
11) What are three ADDS weather products that would help you understand the icing
hazard on a certain flight?
12) List three "types" of visibility observations obtained on the ground.
13)Give the basic definition of the term "ceiling" and the limitations of AWOS and ASOS
automated stations in their reporting of this value.
14)Give the fixed standard definition of VFR, MVFR, IFR and LIFR
1 S)Who is the final authority as to the ceiling and visibility for a given flight?
16)With regards to lowering ceilings and visibilities, what is the biggest cause of serious
weather related accidents for VFR pilots? What type of weather system (warm, cold,
occluded, stationary) is primarily responsible for generating these dangerous
conditions?
17)What is the visibility difference between Fog (FG) and Mist (BR)?
18)With the Temp/Dew Point spread as follows and a cooling trend is in place, how soon
may fog be expected to occur:
a. 2 Deg: F:
. 5 Deg. F:
c. 12 Deg. F:
19)What is the shorthand aviation designation for these visibility limiters:
a. Ice Fog:
. Shallow Fog:
C. Drizzle:
d. Light Rain:
e. Blowing Snow:
f. Smoke:
g. Haze:
h. Dust:
i. Blowing Dust:
20)List three weather products (ADDS and/or LEIDOS) that depict CURRENT VMC/IMC
weather conditions
21) List three weather products (ADDS and/or LEI DOS) that depict FORECAST VMC/IMC
weather conditions
Answered 3 days After Apr 11, 2023

Solution

Dr Shweta answered on Apr 15 2023
42 Votes
Ans 1. When the humidity is high and the air temperature is low, ca
uretor ice forms. After enough gasoline has evaporated to cool the ca
uretor and cause water to condense from the intake air, ice begins to develop in the ca
uretor's key sections. Reduced power and a rough-running engine are the typical signs of ca
ice. The first sign in an aircraft with fixed pitch propellers is often a little reduction in engine rpm. Most of the time, pilots can remove ca
uretor ice build-ups by applying ca
heat. Following the mag check, during the run-up, is a good opportunity to check the ca
uretor's heat. On an aircraft with fixed pitch propellers, a modest decrease in RPM is seen.
Ans 2. Fuel injection has the advantages of cleaner, more efficient combustion, sharper, quicker throttle response, and better fuel economy or mileage. FI systems are less prone to damage and need little maintenance as compared to ca
uretors. In a typical ca
uretor system, the temperature decrease that occurs when fuel is put into the air might cause ice issues. A fuel-injected engine's cylinder experiences this mixing, which reduces the likelihood of ice.
Ans 3. The following are the five risks of structural icing: Airflow around the aircraft is disrupted by structural ice accumulation, which has a negative impact on performance. Ice building on the wings adds weight and lowers lift, and icing on the aircraft's propeller causes increased drag and decreased power.
Ans 4. Hoar frost is a thin, homogeneous layer of ice that has a fine, crystalline structure and is white in colour. Prior to take-off, it must be removed since it won't regenerate.
Ans 5. Rime ice, also known as opaque or milky white deposits of ice, develops when an aircraft is travelling over filmy or striatal clouds. It is reliant on a negligibly high rate of capture of tiny supercooled water droplets. It builds up on antennae, pilot heads, the front edges of wings, etc. A white ice called hard rime that often occurs in conditions of high wind speeds and air temperatures between 2 and 8 °C (28 and 18 °. It is very challenging to remove hard rime forms. They resemble combs, in contrast to clear ice, which seems uniform and translucent, and soft rime, which has a feathery or spiky appearance. It occurs when there isn't any fog, but there is a lot of relative humidity in the air (over 90%), and the temperature is below 8 °C (18 °F). Soft rime formations seem like scales and needles of white ice; they are delicate and readily shaken off of things. Soft rime ice is not very tightly connected to the aircraft surfaces and can therefore easily
eak off, hence flight not recommended for cancellation.
Ans 6. When flying through regions with a high concentration of big, supercooled water droplets, such as cumuliform clouds and freezing rain, clear ice, also known as glazing ice, develops as a thick...
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