Originally posted by RB
to Irinel
На счет радиополукомпаса ничего не говорится Есть инструкции только к радио оборудование как таковому

coolant temperature gage
carburetor ait temperature
manifold pressure
engine gauge unit
oxyhen pressure and flow indicator
gear box pressure gauge


11. GENERAL FLYING CHARACTERISTICS.
a. Fuel selection was noted "reserve tank" for "take-off." After take-off proceed as follows:
(1) After about 20 minutes switch to belly tank
("AUX") and run it dry.
(2) Run "right tank" dry.
(3) Run "left tank" dry.
(4) Switch to "reserve."
NOTE
"Left tank" will partially refill in flight due to

b. In cruising flight, the following gages and their respective readings give the most satisfactory indication of the engine's performance:
.
RPM
Oil Inlet Temperature
Oil Pressure (Pounds Per Square Inch)
Coolant Outlet Temperature

1600 to 2400
60°C (140°F) to 80°C (176°F) 60 to 70
100°C (212°F) to 120°C (248°F)


8. CARBURETOR AIR FILTER AND HEATER.
a_. Two controls for operation of the filter and heater (figure 8) are located in the cockpit at the left of the pilot's seat on the turn-over beam. These controls operate dampers in the air ducts. The first control selects the desired amount of cold rammed un-filtered air which is led directly to the carburetor through a duct leading from the air scoop located on the top cowling directly over the carburetor. The second control permits the selection of hot unfiltered or cold filtered air to the carburetor.
b_. It is recommended that under extreme frigid conditions, and when the airplane is kept in outside air, that a cover be placed over the carburetor air scoop to prevent snow or ice from forming on the scoop or entering the carburetor. In case a cover is not placed over the air scoop, it is necessary to thaw out the carburetor and scoop preflight. The heat of the engine alone should not be relied upon to thaw out these units because the extreme warm-up that would be required would overheat the engine.
c_. A carburetor air thermometer is installed on the main instrument panel in the cockpit to calibrate the temperature of carburetor air at all times.
d. Carburetor icing usually occurs with carburetor air temperatures below 50°F (10°C) in high humidity air. It is evidenced by roughness or loss

2. FUEL, OIL, AND COOLANT.
Fuel Specification No. AN-W-F-781
Octane 100
Oil Specification No. AN-W-O-446
Normal Temperature Grade 1120 (SAE No. 60)
Low Temperature Grade 1100 (SAE No. 50)
А перевести?
Вообщем -то в основном меня интересует показания приборов контроля температуры охдадителя и масла..