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01-E2AAA-2-2.2
WP 096 00 (Deicing System)
Question | Answer |
---|---|
The deicing system is ____ operated and ____ controlled. | Pneumatically, electrically |
Where is the two-position WING TAIL toggle switch located? | on the ANTI-ICE, DE-ICING, and DE-FOG control panel in the the cockpit |
The three distributor valves apply what pressure to inflate the boots? | 18 psi |
The three distributor valves apply what suction to deflate the boots? | 6 in. Hg |
What are the main components of the deicing system? | electronic timer, distributor valves, pressure regulator and relief valve, ejector, suction relief valve, deicer boots, pressure gage, suction gage |
How many distributor valves are there? | 3 |
Where is the electronic timer located? | shelf section forward of the main power distribution box |
What does the electronic timer contain? | electronic timing circuit, a transistor, relay, and rotary switch |
On the distributor valve in each outer panel of each wing, to what wing boots are port a and b connected to respectively? | inboard wing boot, outboard wing boot |
Distributor valve in the tail section controls ____. | stabilizer and fin boots |
On the distributor valve in the tail section, to what are port a and b connected to respectively? | outboard stabilizer and fin boots; inboard stabilizer and fin boots |
What does the distributor valve contain? | pressure inlet port, suction outlet port, two ports (A and B) to deicer boots, port piped overboard to a low-pressure area, and two solenoids (A and B) |
Approximately ____ suction is always available, due to the suction port being connected to the main suction line. | 4 in. Hg |
The electronic timer is powered by what? | 28 V dc |
What is the inflation sequence of the groups of boots? | inboard wing boots, outboard wing boots, outboard stabilizer and outboard fin boots, and inboard stabilizer and inboard fin boots. |
Each group of boots is inflated for how long? | 5 seconds |
The succeeding group of boots starts to inflate when? | 10 seconds after deflation of the previous group of boots |
What is the total time of the inflation cycle for all four groups of boots? | 60 seconds |
After the solenoid is deenergized and the airflow is cutoff through the distributor valve, the air discharged out of the boots until the pressure reaches approximately ____. | 1 in. Hg |
On what aircraft ____, the ____ are inserted in the left and right engine supply. | 163029 and subsequent, de-ice bleed air check valve |
Where are the deice bleed air check valves located? | in-line to the pressure regulator and relief valve in the left and right engine supply |
Where is the pressure regulator and relief valve located? | on the wing rear beam to the left of the aircraft centerline |
The pressure regulator and relief valve consists of what? | two bodies brazed together |
What are the respective functions of the 2 bodies of the pressure regulator and relief valve? | One body regulates pressure, while the other is a relief valve to prevent excessive pressure buildup |
Where is the ejector located? | to the left of the pressure regulator and relief valve |
What does ejector consist of? | venturi, pressure port, suction port, and overboard port |
Where is the suction relief valve located? | in the tail section |
The suction relief valve has ____ ports, which are connected to what? | 2, one is connected to the distributor valves while the other to the ejector suction line |
When suction becomes excessive , the suction relief valve opens o permit compartment air to enter the suction manifold to reduce the suction to ____. | 62 in. Hg |
On aircraft ____ trough ____ and ____ through ____, the boots are made of ____. | 158638-163848; 163850-165647; soft pliable rubber |
On aircraft ____, ____ and subsequent, the boots are made of ____. | 163849, 165648; polyurethane (have a veneer on outer surface to protect from sunlight, oil, ozone, and heat. |
The wing boots are ____ boots. | single-manifold, simultaneous-inflation, chord wise tube |
The stabilizer and fin boots are ____ boots. | single-manifold, simultaneous-inflation- span wise tube |
Where is the pressure gage located? | on the right overhead console in the cockpit |
How is the pressure gage calibrated? | from 0 to 20 psi, in increments of 1 psi |
What is pressure source for the pressure gage? | pressure manifold |
A non-operation condition on the pressure gage is indicated by what? | steady reading of 18 psi on the gage |
Where is the suction gage located? | on the left overhead console in the cockpit |
The suction gage is graduated from ____. | 0 to 10 in. Hg, in major increments of 1 in. and in minor increments of .2 in |
What is the source of the suction gauge? | suction manifold |
A non-operation condition on the suction gage is indicated by what? | steady reading of 6 in. Hg |
What indicates system operation on the pressure and suction gages? | pointer fluctuations |