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DRIFTDOWN………………………………………………………………………. 45
DESCENT………………………………………………………………………….. 47
HOLDING…………………………………………………………………………… 51
CITATION MUSTANG OPERATING MANUAL
510OM-00 1
DEFINITIONS
Altitude: All altitudes used in this manual are pressure altitudes unless
otherwise stated
Anti-Ice systems: The engine anti-ice system is the only anti-ice system that affects
performance in this section. Performance, when referred to ANTI-ICE
ON, is based on the above system being operated.
Additionally, windshield, pitot-static and angle-of-attack anti-ice
systems are anti-ice systems which do not affect performance.
Deice Systems: The wing, horizontal stabilizer, and tail deice system comprise the
deice system.
FAA: Federal Aviation Administration
Hr: Hour
Ind Mach: The displayed Mach number value that includes position error. Zero
instrument error is assumed.
ISA: International Standard Atmosphere in which:
a. The air is a dry perfect gas;
b. The temperature at sea level is 15°C;
c. The pressure at sea level (standard datum plane) is 29.92
inches mercury;
d. The temperature gradient from sea level to the altitude at
which the temperature is –56.6°C will be –1.98°C per 100
feet.
KIAS: Airspeed indicator reading (knots) that includes position error. Zero
instrument error is assumed.
KTAS: True airspeed expressed in knots
Lb: Pound
Lb/hr: Pounds-per-hour
M or Mach: Mach number. The ratio of true airspeed to the speed of sound.
N1 Low pressure turbine speed. The fan is attached to the low pressure
turbine.
CITATION MUSTANG OPERATING MANUAL
2 510OM-00
TEMP Ambient air temperature. The free air static temperature, obtained
either from the ground meteorological sources or from in-flight
temperature indications adjusted for instrument error and ram air
temperature rise.
Position Correction: A correction applied to indicated airspeed or altitude to eliminate the
effect of the location of the static pressure source on instrument
reading.
RAT Ram air temperature. RAT is displayed on each PFD. RAT is ambient
air temperature increased by ram rise due to Mach Number. On the
ground with engine(s) operating, RAT is ambient temperature.
RPM Revolutions-per-minute.
True Airspeed (KTAS) The airspeed (knots) of an airplane relative to undisturbed air.
CITATION MUSTANG OPERATING MANUAL
510OM-00 3
CLIMB
Climb performance for the multi-engine climb schedule is presented in tabular form on the
following pages.
This performance is based on maximum continuous climb thrust setting on both engines, gear and
flaps up, speed brakes retracted, and anti-ice systems OFF. The performance is also presented
for anti-ice systems ON.
The time, distance, fuel and rate-of-climb used to any given altitude is based on the climb starting
at sea level. If the climb is initiated at some other altitude, it is necessary to go into the data twice,
once at the initial altitude and once at the final altitude. The difference in time, distance, and fuel
between these two altitudes provides the proper values for the climb. The data allows for fuel
burnoff in the climb; therefore, the weight presented is at the start of the climb.
The climb data for the conditions requiring a step climb are based on climbing direct to the highest
attainable altitude as shown in the step climb weight table, cruising at the altitude until the desired
weight is achieved, and then climbing to the desired altitude or the next step altitude per the step
climb weight table.
Consult the buffet onset chart in Section IV, Performance, Standard Charts, of the FAA Approved
Airplane Flight Manual to ensure adequate maneuver margin during the climb phase of flight.
CITATION MUSTANG OPERATING MANUAL
4 510OM-00
CRUISE CLIMB
170 KIAS/0.44 INDICATED MACH
TIME, DISTANCE, FUEL, AND RATE OF CLIMB ANTI-ICE SYSTEMS OFF
T.O.
WEIGHT 8645 8000 7500 7000 6500 8645 8000 7500 7000 6500 8645 8000 7500 7000 6500
PRESSURE 5000 FEET 10000 FEET 15000 FEET
ALTITUDE ISA = 5°C = 41°F ISA = -5°C = 23°F ISA = -15°C = 6°F
　
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