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Tachometer - 700 - 2800 RPM - 2801 RPM
Oil Temperature Indicator 75o F 170 - 220o F 75 - 170o F 220 - 240o F 240o F
Cylinder Head Temperature Indicator - 360 - 420o F 240 - 360o F 420 - 460o F 460o F
Oil Pressure Indicator 10 psi 30 - 60 psi RPM > 2100 10 - 30 psi 60 - 100 psi 100 psi
Fuel Pressure Indicator 3.5 psi - - 16.5 psi
3.5 psi - - Top of Red Line (See Note) *
Note: The allowable operating fuel pressure is greater than 32.5 psi. Operation to the top of the Red Line is permitted. This change is temporary pending installation of modified fuel pressure gauge.
Powerplant instrument markings for instruments delivered after July 1999.
Instrument Red Line/ Lower Limit Green Arc/ Normal Operating Range Yellow Arc/ Caution Range Red Line/ Upper Limit
Oil Temperature Indicator 75o F 170 - 220o F - 240° F
Cylinder Head Temperature Indicator - 300 - 420o F 420 - 460o F 460° F
Oil Pressure Indicator 10 psi 30 - 60 psi - 100 psi
2.6. MISCELLANEOUS INSTRUMENT MARKINGS
Instrument Red Arc = Lower Limit Green Arc = Normal Operating Range Yellow Arc = Caution Range Red Line = Upper Limit
Voltmeter 8 - 11 Volts 12.5 - 16 Volts 11 - 12.5 Volts 16.1 Volts
Doc # DA202-C1 April 06, 2010 Page 2 - 5
Rev 25 DOT Approved
2.7. WEIGHT
Maximum Ramp Weight Maximum Take-Off Weight Maximum Landing Weight Maximum permissible weight in the baggage compartment : 1660 (753 kg) : 1653 lbs (750 kg) : 1653 lbs (750 kg) : 44 lbs (20 kg) only permissible with baggage harness
WARNING
EXCEEDING WEIGHT LIMITATIONS MAY LEAD TO OVERLOADING OF THE AIRPLANE AND CAUSE LOSS OF CONTROL OF THE AIRPLANE AND/OR STRUCTURAL DAMAGE.
2.8. CENTER OF GRAVITY
The reference datum (RD) for the center of gravity (CG) calculation is tangent to the leading edge of the wing at the root rib. This plane is vertical when the fuselage is horizontal. Procedures for horizontal alignment, as well as particulars with regard to the empty weight center of gravity, refer to Chapter 6.
Most forward CG (all weights) : 7.96 in (202 mm) aft of RD. Most rearward CG (all weights) : 12.49 in (317 mm) aft of RD.
WARNING
EXCEEDING THE CENTER OF GRAVITY LIMITATIONS REDUCES THE MANEUVERABILITY AND STABILITY OF THE AIRPLANE.
The procedure used to determine the center of gravity is described in Chapter 6.
2.9. APPROVED MANEUVERS
This airplane is certified in the UTILITY Category in accordance with Canadian Airworthiness Manual Chapter 523-VLA.
Permissible Utility Category Maneuvers:
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