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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
any malfunction below V1. I will
control the aircraft and extend the
speedbrakes and notify the tower.
Between 70 and V1 we will only
abort for red lights, loss of directional
control or loss of major dis-
CITATION MUSTANG OPERATING MANUAL
18-4 510OM-00
PHASE CONDITION CALLOUT
Takeoff All airspeed indicators moving “Airspeed alive”
All airspeed indicators indicating 70 KIAS “70 knots”
Airspeed indicators at computed V1 “V1”
Airspeed indicators at computed VR “Rotate”
Airspeed indicators at computed V2 “V2”
Departure/ Prior to intercepting an assigned course “Course alive”
Enroute/
Approach
Climb and descent Approaching transition altitude (IFR and VFR) “Transition altitude altimeters reset”
1,000 feet above/below assigned altitude (IFR) State altitude leaving and assigned
level-off altitude
Final At final approach fix (Fix) altimeters and instruments
check (NOTE 1)
500 feet above minimums “500 above minimums”
100 feet above minimums “100 above minimums”
Runway acquisition “Runway at (clock position)” or
“Approach lights at (clock position)”
(NOTE 2)
After pilot flying reports “visual,” pilot not “VREF ”
flying reverts to instruments and callouts
“Sink (rate of descent)”
“On,” “Above,” or “Below glide
slope,” if required
At decision altitude (DA) “Minimums, runway not in sight” or
“Minimums, runway at (clock
position)” or “Minimums, approach
lights, at (clock position)” (NOTE 2)
At minimum descent altitude (MDA) “Minimums” (NOTE 2)
At missed-approach point (MAP) “Missed-approach point, runway
not in sight” or “Missed-approach
point, runway at (clock position)”
or “missed-approach point, approach
lights, at (clock position)”
NOTES:
1. CHECK FOR APPEARANCE OF WARNING FLAGS AND GROSS INSTRUMENT DISCREPANCIES.
2. CARE MUST BE EXERCISED TO AVOID MAKING AMBIGUOUS CALLOUTS THAT COULD NEGATIVELY INFLUENCE THE PILOT
　
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