MSFS 2024 · General Aviation
Beechcraft Bonanza G36 Quick Reference
V-SPEEDS
| Speed | Value | Description |
|---|---|---|
| Vr (Flaps UP) | 73 KIAS | Rotation at 3,650 lb (50-ft 84 kts) |
| Vr (Flaps APPR) | 67 KIAS | Flaps 12 deg (50-ft 77 kts) |
| Vx | 84 KIAS | Best angle climb |
| Vy | 100 KIAS | Best rate climb |
| Cruise Climb | 110 KIAS | 2,500 RPM |
| Vg | 110 KIAS | Max range glide, 1.7 NM/1,000 ft |
| Va | 141 KIAS | Maneuvering (also turbulent air penetration) |
| Vfe (Approach 12 deg) | 154 KIAS | Max approach flap |
| Vfe (Full 30 deg) | 124 KIAS | Max full flap |
| Vle / Vlo | 154 KIAS | Max gear extended / operating |
| Vno | 167 KIAS | Max structural cruise |
| Vne | 205 KIAS | Never exceed |
| Vs0 | 61 KIAS | Stall, flaps down, max weight |
| Vs1 | 68 KIAS | Stall, flaps up, max weight |
| Vref | 79 KIAS | Approach flaps DOWN (90 kts flaps UP) |
POWER SETTINGS
| Phase | Setting |
|---|---|
| Takeoff | Full throttle, 2,700 RPM (300 HP) |
| Taxi / After Start | 1,000-1,200 RPM |
| Run-Up | 1,700 RPM |
| MCP Climb | Full throttle / 2,700 RPM at 100 kts |
| Cruise Climb | Full throttle / 2,500 RPM at 110 kts |
| Cruise | Per Section 5 cruise tables, lean using EGT |
| Balked Landing | Throttle and propeller FULL FORWARD, 80 kts |
FLAP SCHEDULE
| Setting | Max Speed | Use |
|---|---|---|
| UP (0 deg) | Any | Cruise / normal takeoff |
| APPROACH (12 deg) | <= 154 KIAS | Short field takeoff / approach |
| DOWN (30 deg) | <= 124 KIAS | Normal landing |
ENGINE LIMITS
| Parameter | Value |
|---|---|
| Engine | Continental IO-550-B, 300 HP |
| Takeoff / Max Continuous | Full throttle, 2,700 RPM |
| Max Cylinder Head Temp | 238 degC (460 degF) |
| Oil Temp | 24 degC min for takeoff / 116 degC max |
| Oil Pressure | 10 psi min (idle) / 100 psi max |
| Oil Quantity | 10 qt minimum (preflight) |
| Max Fuel Flow | 27.4 GPH |
| Starter Duty Cycle | 30 sec max in any 4-minute period |
KEY NUMBERS
| Parameter | Value |
|---|---|
| Max Ramp Weight | 3,663 lbs |
| Max Takeoff / Landing Weight | 3,650 lbs (1,655 kg) |
| Max Zero Fuel Weight | No structural limitation |
| Fuel Capacity | 80 gal total / 74 gal usable |
| Min Fuel for Takeoff | 13 gal in each tank (not in yellow band) |
| Max Fuel Imbalance (AP on) | 15 gal (approx 90 lbs) |
| Max Slip Duration | 30 seconds |
| Max Demonstrated Crosswind | 17 kts |
| Glide Ratio | 1.7 NM / 1,000 ft (2 sm / 1,000 ft) |
| Magneto Drop Limit | 150 RPM max / 50 RPM variance |
| Prop Exercise Drop | 200-300 RPM |
| Takeoff Trim | 3 deg nose up (6 deg front seats only) |