MOONEY
M20V ACCLAIM ULTRA
SECTION II
LIMITATIONS
2 - 8
AIRPLANE FLIGHT MANUAL
FAA APPROVED
ORIGINAL ISSUE - 03-16-2017
FUEL LIMITATIONS
Takeoff maneuvers when the selected fuel tank contains less than 12 gallons
(45.4 liters) of fuel have not been demonstrated.
-WARNING-
-NOTE-
Each fuel quantity gauge is calibrated to read zero only in coordinated level flight
when remaining quantity of fuel can no longer be safely used.
-NOTE-
An optional visual fuel quantity gauge is installed on top of each tank and is to be
used as a reference for refueling tanks only.
Standard Tanks (2)
47.5 U.S. Gal. each (179.8 liters)
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Total Fuel Capacity - Standard (see Chapter XI for Optional)
95 U.S. Gal. (359.6 liters)
. . . .
Usable Fuel
89 U.S. Gal. (336.9 liters)
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Unusable Fuel:
6 U.S. Gal. (22.7 liters)
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Fuel Grade (and color):
100LL (low lead) (blue) or 100 octane (green) is approved
. . . . . . . .
Ethylene glycol monomethyl ether (EGME) or other additives are not recommended
due to potential deteriorating effects within the fuel system. Under certain condi-
tions of temperature and humidity, water can be present in fuel in sufficient quanti-
ties to create ice formations within the fuel system. To prevent this, add Anhydrous
ISOPROPYL Alcohol to the fuel supply in quantities not to exceed 3% of total fuel
volume per tank.
-CAUTION-
WEIGHT LIMITS
Maximum Weight - Takeoff
3368 lb. (1528 Kg.)
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Maximum Weight - Landing
3200 lb. (1452 Kg)
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Maximum Weight in Baggage Compartment
120 lb.
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
(54.4 Kg.) @ Fus. Sta. 101.5 (253.7 cm.)
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Maximum Weight in Rear Storage Area
10 lb.
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
(4.54 Kg.) @ Fus. Sta. 131.0 (297.5 cm.)
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Maximum Weight in Cargo Area (Rear seats folded down)
340 lbs.
. . . . . . . . . . . . . . . . . . . . . . .
(154.2 KG) @ Fus. Sta. 70.7 (176.8 cm.)
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
CENTER OF GRAVITY LIMITS (GEAR DOWN)
Most Forward
Fus. Sta. 41.0 IN. (104.1 cm.) @ 2430 lb. (1102 Kg)
. . . . . . . . . . . . . . . . . . . . . . .
16.79% MAC
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Intermediate Forward
Fus. Sta. 44 IN. (111.7 cm.) @ 3300 lb. (1497 Kg)
. . . . . . . . . . . . . . . . . .
21.7% MAC
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Forward Gross
Fus. Sta. 46.0 IN. (116.8 cm.) @ 3368 lb. (1528 Kg)
. . . . . . . . . . . . . . . . . . . . . .
24.98% MAC
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Aft Gross
Fus. Sta. 51.0 IN. (129.5 cm.) @ 3368 lb. (1528 Kg)
. . . . . . . . . . . . . . . . . . . . . . . . . . .
33.18% MAC
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
MAC (at Wing Sta. 94.85)(241 cm.)
61.00 In.
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Datum (station zero) is 13 inches (32.5 cm.) aft of the centerline of the nose gear trunnion attach/
pivot bolts.
MANEUVER LIMITS
This airplane must be operated as a Normal Category airplane. Aerobatic maneuvers, including
spins, are prohibited.
