Maximum Ramp Weight: 2658
Maximum Takeoff Weight: 2650 lbs.
Maximum Landing Weight: 2650 lbs.
Maximum Weight in Baggage Compartment:
Baggage Area 1 - Station 82 to 108: 200 lbs. See note below.
Baggage Area 2 - Station 108 to 124: 50 lbs. See note below.
The maximum combined weight capacity for baggage areas 1 and 2 is 200 lbs.NOTE
CENTER OF GRAVITY LIMITS
Center of Gravity Range:
This airplane is certificated in the normal category. The normal category is applicable to aircraft intended for non-aerobatic operations. These include any maneuvers incidental to normal flying, stalls (except whip stalls), lazy eights, chandelles, and steep turns in which the angle of bank is not more than 60 deg.
Aerobatic maneuvers, including spins, are not approved.
FLIGHT LOAD FACTOR LIMITS
*Flaps Up: +3.8 g -1.52g
*Flaps Down: +2.0 g
*The design load factors are
150% of the above, and in all cases, the structure meets or exceeds design
KINDS OF OPERATION LIMITS
The airplane is equipped for day VFR and may be equipped for night VFR and/or IFR operations. FAR Part 91 establishes the minimum required instrumentation and equipment for these operations. The refer ence to types of flight operations on the operating limitations placard reflects equipment installed at the time of Airworthiness Certificate issuance.
Flight into known icing
conditions is prohibited.
2 Standard Tanks: 33 U.S.
Total Fuel: 66 U.S. gallons
Usable Fuel (all flight conditions): 62 U.S. gallons.
Unusable Fuel: 4.0 U.S. gallons.
Operation on either left or right tank is limited to level flight only.
With 1/4 tank or less, prolonged uncoordinated flight is prohibited when operating on either left or right tank in level flight.
Fuel remaining in the tank after the fuel quantity indicator reads empty (red line) cannot be safely used in flight.
Approved Fuel Grades (and Colors):
100 LL Grade Aviation Fuel (Blue).OTHER LIMITATIONS
100 (Formerly 100/ 130) Grade Aviation Fuel (Green).
Approved Takeoff Range:
Approved Landing Range: 0 deg to 30 deg.