Fig Main landing gear Wheels are cantilevered on gear struts and feature hydraulically actuated disc brakes see fig.
Main gear wheels mount Air-Trac type 5. Hydraulic circuit shut-off valve 2 is positioned between seats. With circuit shut off, pulling emergency brake lever activates parking brake function. Control lever 1 activates master cylinder 3 that features built-in brake-fluid reservoir 4. The brake system is equipped with a non-return valve 5 , which insures that braking action is always effective even if parking brake circuit should accidentally be closed.
The brake system see Figure E-8 consists of a brake fluid reservoir 1 , a master cylinder 2 and two disc brakes assemblies 3 ; an intercept valve activates parking brake 4. Braking action is through a lever 5 located on cabin tunnel between seats. The reservoir 4 is directly connected to the brake master cylinders 3 , as shown in the figure E Oil Oil normal operating temperature approx.
For your information only Bar is a unit of measure.
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The word comes from the Greek word baros, "weighty. One bar is just a bit less than the average pressure of the Earth's atmosphere, which is In practice, meteorologists generally record atmospheric pressure in millibars mb. In English-speaking countries, barometric pressure is also expressed as the height, in inches, of a column of mercury supported by the pressure of the atmosphere. In this unit, one bar equals It is therefore suggested to avoid using this type of fuel unless strictly necessary.
Hg 2. See the FARs for more information. This will reduce the amount of math you need. Get moments from loading charts 2. Obtain the empty weight and moment from the most recent weight and balance 3. Insert the weights and the moments for fuel, occupants and baggage from the previous chart 4. Total the weight and the moment columns 5.
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Divide the total moment by the total weight to get the arm 6. Check that the total weight does not exceed maximum gross weight of pounds 7. Check that the arm falls within the C. Baggage must be secured using a tie-down net to prevent any baggage movement during maneuvers. Some of the equipment may not be installed in your airplane. Equipment list Ref.
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D Fuel Quantity Ind. Mitchell Aircraft Inst. Given information is sufficient to plan journey with required precision and safety. Additional information is provided for each table or graph. Indicated Airspeed 43 Doc. Crosswind chart 46 Doc. Emergencies caused by a malfunction of the aircraft or engine are extremely rare if appropriate maintenance and pre-flight inspections are carried out. In case of emergency, suggestions of the present section should be considered and applied as necessary to correct the problem.
Before operating the aircraft, the pilot should become thoroughly familiar with the present manual and, in particular, with the present section. Further, a continued and appropriate training program should be provided. IDLE Brakes OFF Master switch OFF When the airplane is under control Fuel selector valves OFF Electric fuel pump OFF 5. OFF Fuel selector valves ON Electric fuel pump ON If the engine continues to run irregularly: Fuel selector valve ASAP 5.
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ON If the engine continues to run irregularly: Fuel selector valves LAND as soon as possible If increasing LAND as soon as possible and be alert for impending engine failure 5. Preferably below ft Carburetor heat ON Fuel selector valves ON Master Switch OFF In-flight engine restart OFF Ignition Switches OFF Parking brake SET Escape rapidly from the aircraft 5. OFF Cabin heating SET Escape rapidly from the aircraft 55 Doc.
OFF Throttle OFF Do not attempt an in-flight restart Procedure for a forced landing APPLY 5. OFF Cabin vents OPEN Canopy OPEN, if necessary Master switch OFF Try to choke the fire. Direct the fire extinguisher towards flame base Procedure for a forced landing OFF Safety belts OFF Touchdown Speed FULL Note Align the airplane on the opposite side of runway to the side with the defective tire to compensate for change in direction, which is to be expected during final rolling.
IDLE Ailerons PARE is a convenient memory aid that points the way to spin recovery. The PARE format mimics the most docile spin configuration possible, affording the greatest response to recovery inputs. Errant control inputs that may aggravate the spin are avoided in the process. As a mental checklist, it forces you to focus on the appropriate recovery actions.
Calling each item out loud also tends to reinforce the physical inputs. Carburetor heat ON Increase rpm to avoid ice formation on propeller blades.
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Cabin heat Causes for malfunctions are hard to establish but, in any case, problems of this nature must be dealt with immediately. The following may occur: 5. Adjust speed to control aircraft without excessive stick force Land aircraft as soon as possible 58 Doc. ON or chocks installed Fuel selector valves Reinstall the four screws. Verify tab is below latch upon closing. Pull out the first hinge pin positioned on the side of the firewall, then, while holding cowling, pull out second hinge pin; remove cowling with downward motion.
For installation follow reverse procedure 59 Doc.
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SET Friction lock ON Generator light ON Aux. Alternator switch if installed ON Alternator light ON Fuel pump ON Check for audible sound and operation of fuel pressure indicator Fuel pump OFF Flaps For flight safety, pilot should verify actual fuel quantity visually in tanks before takeoff. Visual inspection is defined as follows: check for defects, cracks, detachments, excessive play, and unsafe or improper installation as well as for general condition.
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