Page 568 - POH-SUPER KING AIR B200/B200C

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Super King Air B200/B200C

SECTION 5
PERFORMANCE
TABLE OF CONTENTS
SUBJECT PAGE

Introduction To Performance and Flight Planning . . . . . . . . . . . . . . . . . . . 5-5
Comments Pertinent to the Use of Performance Graphs . . . . . . . . . . . . 5-15
Graphs:
Airspeed Calibration - Normal System - Take-off Ground Roll . . . . . . . . . . . 5-19
Airspeed Calibration - Normal System. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-20
Airspeed Correction - Normal System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-21
Airspeed Calibration - Alternate System . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-22
Airspeed Correction - Alternate System. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-23
Indicated Outside Air Temperature Correction - ISA . . . . . . . . . . . . . . . . . . . 5-24
ISA Conversion . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-25
Fahrenheit to Celsius Temperature Conversion . . . . . . . . . . . . . . . . . . . . . . 5-26
Stall Speeds - Power Idle. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-27
Cabin Altitude for Various Airplane Altitudes . . . . . . . . . . . . . . . . . . . . . . . . . 5-28
Maximum Take-off Weight Permitted by Enroute Climb Requirement . . . . . 5-29
Take-off Weight to Achieve Positive One-Engine -Inoperative
Climb at Lift-off - Flaps 0%. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-30
Take-off Weight to Achieve Positive One-Engine -Inoperative
Climb at Lift-off - Flaps 40%. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-31
Maximum Enroute Weight (14 CFR Part 135 Operations). . . . . . . . . . . . . . . 5-32

Take-off Weight - Flaps 0% - To Meet 14 CFR Part 25 Take-off Climb
Requirements. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-34
Take-off Weight - Flaps 40% - To Meet 14 CFR Part 25 Take-off Climb
Requirements. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-35

Minimum Take-off Power at 2000 RPM With Ice Vanes
Retracted (65 Knots) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-36
Minimum Take-off Power With Ice Vanes Extended (65 Knots) . . . . . . . . . . 5-37
Take-off Flight Path . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-38
Wind Components . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-39
Take-off Distance - Flaps 0%. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-40
Accelerate-Stop - Flaps 0% . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-41
Accelerate -Go - Flaps 0%. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-42
Net Gradient of Climb - Flaps 0% . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-43
Take-off Distance - Flaps 40%. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-44
Accelerate-Stop - Flaps 40% . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-45
Accelerate-Go - Flaps 40% . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-46
Revised: April, 2007
P/N 101-590010-279 5-1