CAE SimuFlite Citation Bravo, Pilot Training Manual

Page: 334 / 718

4-82
Developed for Training Purposes
Citation Bravo
September 2005
CAE SimuFlite
Landing Distance and Approach Speeds
Use the Landing Field Length table (
Figure 4-44
) to determine VREF,
VAPP, and runway length required by weight and ambient conditions.
With a landing weight of 12,313 lbs, use the chart for 12,500 lbs.
1. Enter the block for the appropriate altitude ( 1,000 ft ) and weight
( 12,500 lbs ) from the left at the correct ambient temperature ( 25°C ).
2. Move to the right until the applicable wind component is reached
( 19 kts ).
Use the distance under 10kts for added safety.
3. Read the landing distance; interpolate if nece.ssary
The landing distance is 2,760 ft.
4. To meet FAR 135 requirements or for an additional margin of safety,
divide the runway length by 0.6
.
5.
From the top of the block, just below the weight, read V
REF
and
V
APP
speeds. Interpolate as necessary.
V
REF
is 107 KIAS and V
APP
is 113 KIAS.
6.
The formula for V
AP
, the approach target speed, is: V
REF
+ 10
KIAS + 1/2 the headwind com all of the gust factor.
The total adjustment may not exceed V
REF
+ 20 KIAS.
107 + 10 + 10 + 0 = 127 KIAS
7.
Find V
ZF
by adding 30 kts to V
REF
.
107 + 30 = 137
8. Enter this information on the TOLD card.
where:
L= Landing Distance
0.6 = FAR 135 Factor
R= Required Landing Distance
L
0.6
-------
R =
ATIS
GROSS WEIGHT
FLAPS
V
REF
V
AP
GO AROUND
PWR
APPROACH CITATION
V
ZF
89.8%
NOTES:
R
W
Y
R
Q
D
V
APP
FT.
12,500
FULL
107
127
137
4,600
113
2 760ft ,
0.6
--------------------
4 600ft , =