Mooney M20V Acclaim Ultra, Руководство по эксплуатации для пилотов

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MOONEY
M20V ACCLAIM ULTRA
SECTION VII
AIRPLANE AND SYSTEM DESCRIPTION
7 - 11
AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE - 03-16-2017
30. PROPELLER CONTROL
Push propeller control forward to increase engine RPM; pull control aft to decrease engine
RPM. Control is a vernier type and fine adjustments of RPM can be obtained by turning knob
clockwise to increase RPM and counter clockwise to decrease RPM. Knob should not be
turned IN any closer than .030” to .060” to panel nut face.
31. MIXTURE CONTROL
Mixture control allows pilot to adjust the fuel- air ratio (mixture) of the engine. Push control
forward to enrich mixture. Pull control full aft to close idle cut off, shutting down engine. Con-
trol is a vernier type and fine adjustments of mixture can be obtained by turning knob clock-
wise to enrich mixture and counterclockwise to lean. Knob should not be turned IN any closer
than .030” to .060” to panel nut face.
32. EMERGENCY LOCATOR TRANSMITTER (ELT) SWITCH
ELT is activated when the ON button is pushed. ELT returns to ’armed’ condition when the
RESET button is pushed. Refer to ELT description elsewhere in this section on proper and
lawful usage.
ARTEX ELT (optional): If the ELT switch is labeled ’ARTEX ELT’ then operation is different
from above. ELT is activated when the switch is in the ON position. ELT returns to ’armed’ the
switch is in the ARMED position.
33. GO AROUND SWITCH
GO AROUND switch is activated when the GA button is pushed. Reference G1000 Pilot’s
Guide for more detailed information on system functionality.
34. ALTERNATE STATIC SOURCE VALVE
Pull alternate static source valve full aft to change source of static air for the altimeter, air-
speed and vertical speed indicator from outside of aircraft to cabin interior. Air speed and al-
timeter readings are affected slightly when alternate static source is used (See Charts in
SECTION V).
35. PARKING BRAKE CONTROL
Depress brake pedals and pull parking brake control to set parking brake. Push parking
brake control in to release parking brake.
36. ALTERNATE AIR (ALT AIR)
The alternate air valve automatically opens when the primary induction air system becomes
blocked for any reason. The valve may be opened manually by pulling the ALT AIR knob aft.
An AMBER annunciation will illuminate when alternate air door is open.
37. CABIN HEAT CONTROL
Pull cabin heat control to turn cabin heat on. To lower cabin temperature, cabin heat control is
pushed forward toward the OFF position. Optimum use of cabin heat control is described in
the Cabin Environment Section.
38. DEFROST CONTROL
Pull defrost control to decrease air flow to lower cabin area and increase air flow to windshield
ducts in the front of glareshield area. Optimum use of the defrost control is described in the
Cabin Environment Section.
39. CABIN VENT CONTROL (Fresh Air)
Pull cabin vent control aft to open valve in mixing box connected to cabin air inlet vent located
on the right side of the airplane. Optimum use of cabin vent control is described in the Cabin
Environment Section.
40. ACCESSORY USB PORT
Universal Serial Bus: an external serial bus interface standard for charging peripheral per-
sonal devices; USB cable.
41. AIR CONDITIONING CONTROL (OPTIONAL)
See description in “Supplemental Section” in this POH/AFM.
42. TKS (OPTIONAL)
See description in “Supplemental Section” in this POH/AFM.