*Do Not Use This Information For Flight Planning
Powerplant
| Engine Make Engine Model Power Propeller Make |
Lycoming O-320-E2D 150hp@2700rpm McCauley |
Oil Quantity Oil Type (>16°C) (-18°C-21°C) RPM Limit |
6qt.-8qt. SAE50 SAE10W30 2700rmp |
Engine Type: Four cylinders, direct drive, horizontally opposed, air cooled, carburetor-equipped.
Propeller Type: two blades, fixed pitch.
Fuel System
| Total Capacity Total Usable |
42gal. 28gal. |
Each Tank Approved Grades |
21gal. 100LL, 100 |
System Description: The airplane is equipped with a standard fuel system consisting of two vented fuel tanks, a fuel tank selector valve, fuel strainer, manual primer, and carburetor. Fuel flows by gravity from one or both tanks to the fuel selector, through a fuel strainer to the carburetor. From the carburetor, the fuel/air mixture flows to the cylinders. The fuel selector should be in the BOTH position for takeoff, climb, descent, landing, and maneuvers that involve prolonged slips or skids. Operation from either the LEFT or RIGHT position is reserved for level cruising flight only
Weight Limites
Open Weight and Balance Calculator
|
Ramp Weight Takeoff Weight Landing Weight Baggage Weight Area 1 Area 2 |
Normal 2307 lbs. 2300 lbs. 2300 lbs. 120 lbs. 120 lbs. 50 lbs. |
Utility 2007 lbs. 2000 lbs. 2000 lbs. none none none |
Electrical System
| Alternator | 14 vlot, 60 amp | Battery | 12 volt, 25 amp hour |
System Description: Power is supplied to most general electrical items through the primary bus. All avionics are powered by the avionics bus. The two busses are tied together through the avionics power switch, which also functions as a circuit breaker for the avionics bus. The avionics power switch should be turned off prior to starting the engine to prevent harmful transient voltages from damaging the avionics equipment. The ammeter shows a charge or discharge on the battery and should remain at or near the zero indication after a brief charging period.
Tire Inflation
| Main Tires | 29 psi. | Nose Tire | 31 psi. |
Airspeed Limitations
| Never Exceed Speed Max. Structural Cruising Speed Maneuvering Speed 2300 lbs. 1600 lbs. Max. Flaps extended Speed |
VNE VNO VA VFE |
160 KIAS 128 KIAS 97 KIAS |
| BEST GLIDE SPEED Stalling Speed, Flaps Up Stalling Speed, Landing Configuration Best Angle-of-Climb Speed, Sea Level Best Rate-of-Climb Speed, Sea Level Rotate Speed Enroute Climb Normal Approach, Flaps Up Normal Approach, Flaps 40° Soft Field Approach, Flaps 40° Max. Demonstrated Crosswind Component |
VG VS VS0 VX VY VR |
65 KIAS 47 KIAS 41 KIAS 64 KIAS 78 KIAS 55 KIAS 80-90 KIAS 60-70 KIAS 55-65 KIAS 60 KIAS 15 KNOTS |