172 Folder

1).oil pressure should register in cold weather in 60 seconds. 2) In the event of alternate static door open ASI will give an error of 4kts &altimeter error will be +/-30¢in closed window condition. 3) propeller ground clearance is 11.25 or 11 ¢¢¼ . 4) minimum turning radius of a/c is 27¢ 5.5¢¢. 5) abrupt use of controls is prohibited beyond a speed of 99kts . 6) yellow arc of ASI is from 129 to 163 kts . 7) minimum oil pressure of a/c is 20 psi . 8) annunciator does not activate activate on low fuel flow . 9) alternator should be switched off in the event of ammeter reading of 31.5V. 10) compass upto 25deg may come in the event of alternator switched off . 11) to get get maximum maximum cabin heating =Heat knob should be fully out & cabin cabin air fully in . 12) DGI has to be aligned regularly on long flight for precession . 13) audible stall warning will be heard 5 to 10 kts above stalling speed . 14) attitude indicator bank marking is at an increment of 10 deg . 15) avionics cooling fan switches on automatically when avionics master switch is on . 16) maximum window open speed is 163 kts . 17) maximum oil pressure is 115 psi . 18) unusable fuel quantity is 1.5 gallons in each tank . 19) maximum ramp weight is 2457 lbs 20) maximum slip duration with one fuel tank dry is 30 sec. 21) colour of 100LL fuel is Blue . 22) minimum oil oil quantity for extended extended flight is None . 23) concentration of DIEGME 0.1.0per to 0.15 per to be added to fuel quantity . 24) MIL-L-22851 oil is to be used after 50 hours of engine running or when composition is stabilised . 25) maximum deflection of nose wheel by the use of rudder on ground is 10 to either  side . 26) mechanical stops on flaps are at 10°20°30°. 27) shock absorption is accomplished accomplished by Air/Oil struct on nose wheel & tubular spring steel on main wheel 28) best rate of climb speed at sea level is 79 kts . 29) in the event of engine flooding . 30) standard temperature lapse rate is 2°C /1000 feet . 31 ) starter cycle for the engine is 10 sec on 20 sec off for three times and then  10min gap for cooling is to given . 32) enroute climb speed is 5 to 10 kts above best rate of flying speed for best visibility.

33) until 50 hours has been accumulated engine should run at 80% power on crusing . 34) open alternate door will result in an approximately 10% loss of power at full trottle . 35) carburetor icing is indicated by loss of RPM in fixed pitch propeller and loss of manifold pressure in constant speed propeller . 36) OAT / voltmeter guage select switch may be tested by putting the select button down for 3 sec to start . 37) if the PTT of microphone is pressed for more more than 33sec in continuation then the transmitter will stop transmitting . 38) in the event of static blockage ASI reads error . 39) to permit heavy cabin loading fuel load can be reduced to 17.5 gallons usable in each tank . 40) in a voltmeter/OAT /clock ,pushing upper control button will charge the display on OAT /Voltmeter window to E.F.C.E . 41) stall warning placement Left leading edge . 42) Ignition placement R ,L, BOTH . 43) at the time of start up if black smoke comes Spark plug fowling . 44 ) in cold weather start the engine by manually prim . 45) if pitot & static source is blocked all instrument VSI, ASI & altimeter give error.