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18-8 Nonprecision Approach—Normal ....................................................................... 18-15
18-9 Nonprecision Approach—Single Engine............................................................. 18-16
18-10 Missed Approach—2 Engine (Precision/Nonprecision)...................................... 18-17
18-11 Missed Approach—Single Engine (Precision/Nonprecision) ............................. 18-18
18-12 Visual Approach................................................................................................... 18-19
18-13 Approach to Stall—Clean Configuration ............................................................ 18-20
18-14 Approach to Stall—Takeoff Configuration ......................................................... 18-21
18-15 Approach to Stall—Landing Configuration ........................................................ 18-22
18-16 Steep Turns .......................................................................................................... 18-23
TABLES
Table Title Page
18-1 Minimum Maneuvering Speeds ............................................................................. 18-2
18-2 Example Callouts (IFR and VFR).......................................................................... 18-4
CITATION MUSTANG OPERATING MANUAL
510OM-00 18-iii
CITATION MUSTANG OPERATING MANUAL
18-iv 510OM-00
INTENTIONALLY LEFT BLANK
INTRODUCTION
This chapter contains information and flight profiles likely to be encountered during most daily
flight operations. These procedures are consistent with the Cessna Model 510 Citation Mustang
Aircraft Flight Manual (AFM) and pilot abbreviated checklists.
CHAPTER 18
MANEUVERS AND PROCEDURES
CITATION MUSTANG OPERATING MANUAL
510OM-00 18-1
GENERAL
The flight profiles in this chapter show some
normal and emergency operating procedures.
Actual in-flight procedures may differ due
to aircraft configuration, weight, weather,
traffic, ATC instructions, etc. Procedures are
consistent with the AFM. If a conflict develops
between these procedures and the AFM,
then AFM procedures must be followed.
CITATION MUSTANG OPERATING MANUAL
18-2 510OM-00
PERFORMANCE
The Mustang performance is certified to Part
23 Normal Category with FAA Special
Conditions to meet Commuter Category
(14CFR Part 23) takeoff and landing performance
requirements. The following areas will
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
　
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