BILL STACK'S
BEECHCRAFT KING AIR 350 REFERENCE TABLES
For Microsoft Flight Simulator®



 CAPACITY
Maximum Take-off Weight 14,992 LBS 6,800 KG
Fuel 539 USG 2,040 L
Useful Load 5,910 LBS 2,681 KG
Passengers 11

 PERFORMANCE
Cruise Climb Rate 1,800 FT/Min 549 M/Min
Range 1,765 NM 3,269 KM
Initial Climb Rate 2,844 FT/Min 867 M/Min
Cruise Climb Rate 1,800 FT/Min 549 M/Min
Cruise Speed 315 KIAS 583 KM
Ceiling, 2 Engines 35,000 FT 10,688 M
Ceiling, 1 Engine 21,500 FT 6,558 M
Fuel Flow Average (see notes) 18.1 USG/HR 68.52 L/HR
Take-off Distance, SL SA 4,192 FT 1,279 M/Min
Landing Distance 2,650 FT 808 M

 CRUISE CLIMB SPEEDS
Sea Level to 10,000 FT 170 KIAS
10,000 FT to 15,000 FT 160 KIAS
15,000 FT to 20,000 FT 150 KIAS
20,000 FT to 25,000 FT 140 KIAS
25,000 FT to 30,000 FT 130 KIAS
30,000 FT to 40,000 FT 120 KIAS

 V SPEEDS KIAS
V1 Take-off Decision <10,500 LBS 106
V1 Take-off Decision >10,500 LBS 108
V2 Take-off Safety <10,500 LBS 111
V2 Take-off Safety >10,500 LBS 117
VA Design Maneuvering 184
VB Turbulent Air Penetration 170
VFE Maximum Flaps Extended - Approach 202
VFE Maximum Gear Extended - Full Down 158
VLE Maximum Gear Extended 184
VLO Maximum Gear Operating - Extend 184
VLO Maximum Gear Operating - Retract 166
VMC Minimum Control 94
VMO Maximum Operating 263
VR Rotation <10,500 LBS 104
VR Rotation 111
VREF Approach Speeds - See VREF Table
VS1 Stall, Clean 96
VSSE Minimum Safe Single Engine 110
VSO Stall, Landing Configuration 81
VX Two-Engine Best Climb Angle 125
VXSE Single-Engine Best Climb Angle 125
VY Two-Engine Best Climb Rate 125
VYSESingle-Engine Best Climb Rate 125
Best Glide Speed, 0 Engines 135
MMOMaximum Mach (FL210 - FL350) 0.58

 MAXIMUM FLAPS SPEEDS
Position KIAS
Approach 202
Full Down 158

 VREF - LANDING APPROACH SPEEDS
Weight KIAS
15,000 (Fully Loaded) 109
14,000 105
13,000 102
12,000 100
11,000 100
10,000 100

 LEGEND
FT Feet
HR Hours
KG Kilograms
KIAS Knots Indicated Air Speed
KM Kilometers
L Liters
LBS Pounds
M Meter
Min Minutes
NM Nautical Mile
SA Standard Atmosphere
SL Sea Level
USG US Gallons

 NOTES
1. Data are collected from Microsoft Flight Simulator® primarily and from other reliable sources as needed.
2. Fuel-flow average is calculated from other performance data for estimating fuel needs. It is not true under all flight conditions.
3. This reference sheet is for personal use only. No commercial use or sale is permitted.
4. No changes to these reference sheets are permitted.
5. These reference tables are for home flight simulation only. They are not for real-world aviation. Neither Bill Stack nor TopSkills accept any blame or responsibility for any misuse.

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    Bill Stack & TopSkills
    Knoxville, Tennessee, USA
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