CAE SimuFlite Citation Bravo, Pilot Training Manual

Page: 344 / 718

4-92
Developed for Training Purposes
Citation Bravo
September 2005
CAE SimuFlite
Example
The following example exhibits the technique for determining takeoff
and landing distances (
Table 4-C
) for a runway covered with 0.8 inches
of loose, dry snow using the corrections factors discussed.
Table 4-C: Takeoff and Landing Distances
1. Consider both operations occurring on a dry, hard surface runway.
Using
Figures 4-48
and
4-49
,
the following apply
.
n
From
Figure 4-48,
V1 is 108 KIAS.
n
From
Figure 4-48
, takeoff field length is 3,420 ft.
n
From
Figure 4-49
, landing distance is 2,980 ft.
2. On a runway contaminated with 0.8 inches of snow, the follow-
ing apply.
n
V
1
is 108 KIAS.
n
Takeoff field length is 3,420 ft multiplied by 2.8, or 9,576 ft.
n
Landing distance is 2,980 ft multiplied by 2.4, or 7,152 ft.
Landing Weight Limitation
Weight – 13,500 lbs
Landing weight is limited by the
most restrictive of:
n
maximum certified landing
weight
n
maximum landing weight
permitted by climb require-
ments or brake energy limit
n
landing distance.
Flaps T.O. & APPR LAND
Ambient Temperature 0°C 0°C
Pressure Altitude 2,000 ft 2,000 ft
Weight 14,800 lbs 13,500 lbs
Wind 10 kts headwind 10 kts headwind
Runway Gradient 0% 0%
Anti-Ice Systems OFF OFF
Conditions Takeoff Landing
Landing Distance – Feet
Flaps – FULL/2000 FT
CONDITIONS
Anti-ice – ON or OFF Airspeed – VREF AT 50 FT
Landing Gear – DOWN Thrust – IDLE
WINDMILLING AFTER V1
Speedbrakes – EXTEND AFTER TOUCHDOWN
(1) Some conditions do not meet climb requirements. Obtain allowable weight form maximum takeoff weight tables.
(2) To obtain landing distance with negative (downhill) runway gradient, refer to landing procedures.
(3) * For use in an emergency that requires a landing a landing at weight in excess of the maximum design landing
weight of 13,500 lbs.
4-49
Takeoff Field Length – Feet
Flaps – 15°2000 FT
CONDITIONS
Anti-ice – OFF Runway Gradient – ZERO
Landing Gear – DOWN Inoperative Engine – WINDMILLING AFTER V1
Speedbrakes – RETRACTED Operative Engine – TAKEOFF THRUST
Some conditions do not meet climb requirements. Obtain allowable weight form maximum takeoff weight tables.
4-48