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help to familiarize the pilot with terms in the
AFM and to help the pilot understand the capabilities
of the aircraft.
TAKEOFF AND LANDING
SPEEDS
Refer to the FAA-approved Cessna Model 510
Citation Mustang pilot abbreviated checklists
or AFM for takeoff and landing speeds.
V1 (takeoff decision speed)—The distance to
continue the takeoff to 35 feet will not exceed
the scheduled takeoff field length if recognition
occurred at V1 (accelerate-go). The distance
to bring the aircraft to a full stop
(accelerate-stop) will not exceed the scheduled
takeoff field length provided that the brakes
are applied at V1.
VR (rotation speed)—The speed at which rotation
is initiated during takeoff to attain the
V2 climb speed at or before a height of 35 feet
above runway surface has been reached.
V2 (takeoff safety speed)—This climb speed is
the actual speed at 35 feet above the runway surface
as demonstrated in flight during takeoff with
one engine inoperative.
VENR (enroute climb speed)—Single-engine
enroute climb speed.
VREF (minimum final approach speed)—The
airspeed equal to the landing 50-foot point speed
with flaps LAND (anti-ice OFF) or with flaps
15 (anti-ice ON) and landing gear extended.
For emergency and abnormal procedures, the airspeed
equal to the 50-foot point speed with
flaps in landing position as defined and landing
gear extended.
VAPP (missed approach climb speed)—The
landing approach climb speed (1.3 VS1) with
15 flap position, landing gear up.
Speeds are posted on the airspeed tape for reference
during takeoff, approach, and landing.
The V-speed flags on the G-1000 may be selected
ON or OFF at the discretion of the pilot.
Minimum maneuvering speeds provide a safety
margin above stall speed (for current flap setting
and weight) when maneuvering prior to
establishing a stabilized final approach.
Table 18-1 lists minimum maneuvering speed.
WEIGHTS
Maximum takeoff weight is limited by the
most restrictive of:
1. Maximum certified takeoff weight
(Flaps—TAKEOFF/APPROACH) 8,645
pounds
2. Maximum weight permitted by climb
requirements
3. Maximum weight permitted by takeoff
field length
Takeoff weight may be further limited by obstacle
clearance requirements of a departure
runway or procedure, or by the landing weight
restrictions at destination.
Table 18-1. MINIMUM MANEUVERING
SPEEDS
FLAP CITATION
CONFIGURATION CE-510
UP VREF + 30
TO/APR VREF + 20
LAND VREF + 10
Maximum landing weight is limited by the
most restrictive of:
1. Maximum certified landing weight—
8,000 pounds
2. Maximum weight permitted by climb requirements
or brake energy limits
3. Maximum weight permitted by landing
distance
Landing weight may be further limited by obstacle
clearance requirements of a missed approach
procedure.
Some flight departments use preprinted cards
for computations,ATIS and clearances. Sample
takeoff and landing data (TOLD) cards are
shown in Figure 18-1.
FLIGHT OPERATIONS
Sample flight profiles are shown in Figures 18-
2 through 18-17.
PREFLIGHT AND TAXI
If flying as a crew, the pilot-in-command ensures
that the copilot understands the normal and
emergency procedures to be used for that takeoff.
This includes verbal callouts during takeoff
roll and initial climb (refer to Table 18-2).
CITATION MUSTANG OPERATING MANUAL
510OM-00 18-3
TAKE OFF DATA
CITATION
T/O N1 CLB N1
V1 VR V2
V2 + 10 VENR FLAPS
CLEARANCE
ARPT_____________ ELEV ______RWY ______
ATIS______ WIND _____ VIS________________
CIG _________________ TEMP/DP_____ / ____
ALT ___________RMKS ____________________
RWY LENGTH__________ RWY REQ’D ________
ZFW_______________ T.O. WT._______________
EMERGENCY RETURN
VREF___________VAPP _______ MSA _________
LANDING DATA
CITATION
VREF VAPP
GA N1 RWY REQ’D
CLEARANCE
ARPT_____________ ELEV ______RWY ______
ATIS______ WIND _____ VIS________________
CIG _________________ TEMP/DP_____ / ____
ALT ___________RMKS ____________________
ZFW_______________ T.O. WT._______________
Figure 18-1. Takeoff and Landing Data Card
Sample Takeoff Briefing
“This will be a static (or rolling)
takeoff with flaps at TO/APR. Check
takeoff power and call “speed alive,
70 knots, V1 and rotate.” I will call
for gear up, flaps, and yaw damper.
The departure is _____. Call abort for
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