Cessna 208B Grand Caravan EX. Airplane Flight Manual (2012) - page 4
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-2
FAA APPROVED
5-14
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
PRESSURE CONVERSION
Example:
Pressure = 29.55 inches of mercury
Pressure = 1000.6 millibars.
Figure 5-3
FAA APPROVED
208BPHCUS-00
U.S.
5-15
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
TEMPERATURE CONVERSION CHART
Figure 5-4
FAA APPROVED
5-16
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
ISA CONVERSION
AND OPERATING TEMPERATURE LIMITS
CAUTION
Do not operate in shaded area of chart.
Figure 5-5
FAA APPROVED
208BPHCUS-00
U.S.
5-17
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-6
FAA APPROVED
5-18
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
WIND COMPONENTS
NOTE
Maximum demonstrated crosswind velocity is 20 knots (not
a limitation).
Figure 5-7
FAA APPROVED
208BPHCUS-00
U.S.
5-19
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
MAXIMUM ENGINE TORQUE FOR TAKEOFF
CONDITIONS:
1900 RPM
60 KIAS
INERTIAL SEPARATOR - NORMAL
Figure 5-8 (Sheet 1 of 2)
FAA APPROVED
5-20
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
MAXIMUM ENGINE TORQUE FOR TAKEOFF
NOTE
1. Torque increases approximately 30 FT-LB from 0 to 60 KIAS.
2. Torque on this chart shall be achieved without exceeding
850°C ITT or 103.7 percent Ng. When the ITT exceeds 825°C,
this power setting is time limited to 5 minutes.
3. With the inertial separator in BYPASS, where altitude and
temperature do not permit 2397 FT-LB for takeoff, decrease
torque setting by 85 FT-LB.
4. With the cabin heater ON, where altitude and temperature do
not permit 2397 FT-LB for takeoff, decrease torque setting by
75 FT-LB.
Figure 5-8 (Sheet 2
FAA APPROVED
208BPHCUS-00
U.S.
5-21
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
MAXIMUM ENGINE TORQUE FOR CLIMB
CONDITIONS:
1900 RPM
Vy KIAS
INERTIAL SEPARATOR NORMAL
Figure 5-9 (Sheet 1 of 2)
FAA APPROVED
5-22
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
MAXIMUM ENGINE TORQUE FOR CLIMB
NOTE
1. Torque on this chart shall be achieved without exceeding
825°C ITT or 103.7 percent Ng.
2. With the inertial separator in BYPASS, decrease torque setting
by 115 FT-LB.
3. With the cabin heater ON, decrease torque setting by 85 FT-
LB.
Figure 5-9 Sheet 2
FAA APPROVED
208BPHCUS-00
U.S.
5-23
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-10 (Sheet 1 of 5)
FAA APPROVED
5-24
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-10 (Sheet 2)
FAA APPROVED
208BPHCUS-00
U.S.
5-25
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-10 (Sheet 3)
FAA APPROVED
5-26
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-10 (Sheet 4)
FAA APPROVED
208BPHCUS-00
U.S.
5-27
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-10 (Sheet 5)
FAA APPROVED
5-28
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-11 (Sheet 1 of 3)
FAA APPROVED
208BPHCUS-00
U.S.
5-29
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-11 (Sheet 2)
FAA APPROVED
5-30
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-11 (Sheet 3)
FAA APPROVED
208BPHCUS-00
U.S.
5-31
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-12
FAA APPROVED
5-32
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-13
FAA APPROVED
208BPHCUS-00
U.S.
5-33
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-14
FAA APPROVED
5-34
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-15
FAA APPROVED
208BPHCUS-00
U.S.
5-35
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-16
FAA APPROVED
5-36
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-17
FAA APPROVED
208BPHCUS-00
U.S.
5-37
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
This Page Intentionally Left Blank
FAA APPROVED
5-38
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-18 (Sheet 1 of 2)
208BPHCUS-00
U.S.
5-39
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-18 (Sheet 2)
5-40
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-19 (Sheet 1 of 11)
208BPHCUS-00
U.S.
5-41
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-19 (Sheet 2)
5-42
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-19 (Sheet 3)
208BPHCUS-00
U.S.
5-43
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-19 (Sheet 4)
5-44
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-19 (Sheet 5)
208BPHCUS-00
U.S.
5-45
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-19 (Sheet 6)
5-46
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-19 (Sheet 7)
208BPHCUS-00
U.S.
5-47
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-19 (Sheet 8)
5-48
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-19 (Sheet 9)
208BPHCUS-00
U.S.
5-49
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-19 (Sheet 10)
5-50
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-19 (Sheet 11)
208BPHCUS-00
U.S.
5-51
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-20 (Sheet 1 of 7)
5-52
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-20 (Sheet 2)
208BPHCUS-00
U.S.
5-53
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-20 (Sheet 3)
5-54
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-20 (Sheet 4)
208BPHCUS-00
U.S.
5-55
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-20 (Sheet 5)
5-56
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-20 (Sheet 6)
208BPHCUS-00
U.S.
5-57
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-20 (Sheet 7)
5-58
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
NOTE
1. Fuel required includes the fuel used for engine start, taxi, takeoff,
maximum climb from sea level, descent to sea level and 45
minutes reserve. Time required includes the time during a
maximum climb and descent.
2. With INERTIAL SEPARATOR in BYPASS, increase time by 8%
or CABIN HEAT ON, increase time by 4%.
Figure 5-21 (Sheet 1 of 2)
208BPHCUS-00
U.S.
5-59
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
NOTE
1. Fuel required includes the fuel used for engine start, taxi, takeoff,
maximum climb from sea level, descent to sea level and 45
minutes reserve. Time required includes the time during a
maximum climb and descent.
2. With INERTIAL SEPARATOR in BYPASS, increase time by 11%
and fuel by 4%, or CABIN HEAT ON, increase time by 8% and
fuel by 4%.
Figure 5-21 (Sheet 2)
5-60
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
NOTE
1. Fuel required includes the fuel used for engine start, taxi, takeoff,
maximum climb from sea level, descent to sea level and 45
minutes reserve. Time required includes the time during a
maximum climb and descent.
2. With INERTIAL SEPARATOR in BYPASS, increase time by 5%
and fuel by 2%, or CABIN HEAT ON, increase time by 5% and
fuel by 2%.
Figure 5-22 (Sheet 1 of 2)
208BPHCUS-00
U.S.
5-61
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
NOTE
1. Fuel required includes the fuel used for engine start, taxi, takeoff,
maximum climb from sea level, descent to sea level and 45
minutes reserve. Time required includes the time during a
maximum climb and descent.
2. With INERTIAL SEPARATOR in BYPASS, increase time by 3%
and fuel by 4%, or CABIN HEAT ON, increase time by 2% and
fuel by 3%.
Figure 5-22 (Sheet 2)
5-62
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-23
208BPHCUS-00
U.S.
5-63
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-24
5-64
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-25
208BPHCUS-00
U.S.
5-65
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
The Page Intentionally Left Blank
5-66
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-26 (Sheet 1 of 5)
FAA APPROVED
208BPHCUS-00
U.S.
5-67
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-26 (Sheet 2)
FAA APPROVED
5-68
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-26 (Sheet 3)
FAA APPROVED
208BPHCUS-00
U.S.
5-69
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-26 (Sheet 4)
FAA APPROVED
5-70
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-26 (Sheet 5)
FAA APPROVED
208BPHCUS-00
U.S.
5-71
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-27 (Sheet 1 of 5)
NOTE
Figures 5-27 thru 5-43 apply to airplanes configured
WITHOUT a cargo pod.
FAA APPROVED
5-72
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-27 (Sheet 2)
FAA APPROVED
208BPHCUS-00
U.S.
5-73
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-27 (Sheet 3)
FAA APPROVED
5-74
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-27 (Sheet 4)
FAA APPROVED
208BPHCUS-00
U.S.
5-75
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-27 (Sheet 5)
FAA APPROVED
5-76
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-28 (Sheet 1 of 3)
FAA APPROVED
208BPHCUS-00
U.S.
5-77
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-28 (Sheet 2)
FAA APPROVED
5-78
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-28 (Sheet 3)
FAA APPROVED
208BPHCUS-00
U.S.
5-79
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-29
FAA APPROVED
5-80
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-30
FAA APPROVED
208BPHCUS-00
U.S.
5-81
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-31
FAA APPROVED
5-82
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-32
FAA APPROVED
208BPHCUS-00
U.S.
5-83
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-33
FAA APPROVED
5-84
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-34
FAA APPROVED
208BPHCUS-00
U.S.
5-85
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
This Page Intentionally Left Blank
FAA APPROVED
5-86
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-35 (Sheet 1 of 2)
208BPHCUS-00
U.S.
5-87
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-35 (Sheet 2)
5-88
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-36 (Sheet 1 of 12)
208BPHCUS-00
U.S.
5-89
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-36 (Sheet 2)
5-90
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-36 (Sheet 3)
208BPHCUS-00
U.S.
5-91
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-36 (Sheet 4)
5-92
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-36 (Sheet 5)
208BPHCUS-00
U.S.
5-93
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-36 (Sheet 6)
5-94
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-36 (Sheet 7)
208BPHCUS-00
U.S.
5-95
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-36 (Sheet 8)
5-96
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-36 (Sheet 9)
208BPHCUS-00
U.S.
5-97
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-36 (Sheet 10)
5-98
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-36 (Sheet 11)
208BPHCUS-00
U.S.
5-99
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-36 (Sheet 12)
5-100
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-37 (Sheet 1 of 7)
208BPHCUS-00
U.S.
5-101
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-37 (Sheet 2)
5-102
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-37 (Sheet 3)
208BPHCUS-00
U.S.
5-103
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-37 (Sheet 4)
5-104
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-37 (Sheet 5)
208BPHCUS-00
U.S.
5-105
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-37 (Sheet 6)
5-106
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-37 (Sheet 7)
208BPHCUS-00
U.S.
5-107
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
NOTE
1. Fuel required includes the fuel used for engine start, taxi, takeoff,
maximum climb from sea level, descent to sea level and 45
minutes reserve. Time required includes the time during a
maximum climb and descent.
2. With INERTIAL SEPARATOR in BYPASS, increase time by 9%
or CABIN HEAT ON, increase time by 6%.
Figure 5-38 (Sheet 1 of 2)
5-108
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
NOTE
1. Fuel required includes the fuel used for engine start, taxi, takeoff,
maximum climb from sea level, descent to sea level and 45
minutes reserve. Time required includes the time during a
maximum climb and descent.
2. With INERTIAL SEPARATOR in BYPASS, increase time by 11%
and fuel by 4%, or CABIN HEAT ON, increase time by 7% and
fuel by 3%.
Figure 5-38 (Sheet 2)
208BPHCUS-00
U.S.
5-109
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
NOTE
1. Fuel required includes the fuel used for engine start, taxi, takeoff,
maximum climb from sea level, descent to sea level and 45
minutes reserve. Time required includes the time during a
maximum climb and descent.
2. With INERTIAL SEPARATOR in BYPASS, increase time by 5%
and fuel by 2%, or CABIN HEAT ON, increase time by 5% and
fuel by 2%.
Figure 5-39 (Sheet 1 of 2)
5-110
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
NOTE
1. Fuel required includes the fuel used for engine start, taxi, takeoff,
maximum climb from sea level, descent to sea level and 45
minutes reserve. Time required includes the time during a
maximum climb and descent.
2. With INERTIAL SEPARATOR in BYPASS, increase time by 2%
and fuel by 5%, or CABIN HEAT ON, increase time by 2% and
fuel by 3%.
Figure 5-39 (Sheet 2)
208BPHCUS-00
U.S.
5-111
SECTION 5
CESSNA
PERFORMANCE
MODEL 208B 867 SHP
GARMIN G1000
Figure 5-40
5-112
U.S.
208BPHCUS-00
CESSNA
SECTION 5
MODEL 208B 867 SHP
PERFORMANCE
GARMIN G1000
Figure 5-41
208BPHCUS-00
U.S.
5-113