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True Track Angle Available
Ground Speed Available
Selected Altitude Available
True Airspeed Available
510FM-07 AI 2-31.1
SECTION II - OPERATING LIMITATIONS MODEL 510
FAA APPROVED
U.S. Configuration
STANDBY INSTRUMENTS
The standby flight instruments (including ATT, ALT and ASI) must successfully complete the preflight
test defined in the Normal Procedures section and be functioning prior to takeoff.
AHRS AREAS OF OPERATION
Navigation using the G1000 is not authorized north of 70° North latitude or south of 70° South
Latitude due to unsuitability of the magnetic fields near the Earth’s poles. In addition, operations are
not authorized in the following two regions:
1. North of 65° North latitude between longitude 75° W and 120° W (Northern Canada).
2. South of 55° South latitude between longitude 120° E and 165° E (region south of Australia
and New Zealand).
Dispatch is prohibited with the GEO LIMITS Garmin System message displayed.
ICE AND RAIN PROTECTION
In icing conditions, the airplane must be operated, and its ice protection systems must be used, as
described in Section III, Normal Procedures, ICE PROTECTION SYSTEMS. Specific operational
speeds and performance information must be used where established for such conditions.
The ENGINE and WINDSHIELD ANTI-ICE switches must be selected ON at a RAT of +10°C (50°F)
or colder when in visible moisture.
WING/STAB deice must be selected to AUTO at the first sign of ice accretion anywhere on the
airplane.
Except for the ground preflight check, maximum RAT for operation of engine anti-ice with the
throttles above idle is +20°C (+68°F).
Limit the ground operation of the pitot-static heat to 2 minutes to preclude damage to the pitot tubes
and stall warning vane.
The airplane must be free of ice prior to takeoff. Anti-ice systems must not be used to deice engine
inlets prior to takeoff. Dispatch with polished frost is prohibited.
CAUTION
To prevent possible engine damage from ingestion of ice, do not chip or
scrape ice or snow from the engine air inlet. Deice these areas prior to start.
Minimum airspeed for sustained flight in icing conditions (except takeoff, approach and landing) is
160 KIAS.
In icing conditions, operation at other than flaps UP and landing gear retracted is prohibited except
during approach and landing.
The use of wing or tail deice boots is prohibited below -30°C RAT.
2-32 AA 510FM-07
MODEL 510 SECTION II - OPERATING LIMITATIONS
FAA APPROVED
Configuration U.S.
OPERATIONS IN SEVERE ICING CONDITIONS
WARNING
Severe icing may result from environmental conditions outside of those
for which the airplane is certified. Flight in freezing rain, freezing drizzle,
or mixed icing conditions (supercooled liquid water and ice crystals)
may result in ice build-up on protected surfaces exceeding the capability
of the ice protection system, or may result in ice forming aft of the
protected surfaces. This ice may not be shed when using the ice
protection systems, and may seriously degrade the performance and
controllability of the airplane.
During flight, severe icing conditions shall be determined by the following visual cues:
1. Unusually extensive ice accumulation on the airframe and windshield in areas not normally
observed to collect ice.
2. Accumulation of ice on the upper surface of the wing aft of the edge of the boot.
If one or more of these visual cues exist:
1. Use of the autopilot is prohibited.
2. Immediately request priority handling from Air Traffic Control to facilitate a route or altitude
change to exit the icing conditions.
3. Leave flaps in current position, do not extend or retract.
4. Avoid abrupt and excessive maneuvering that may exacerbate control difficulties.
5. If unusual or uncommanded roll control movement is observed, reduce angle of attack.
Since the autopilot, when installed and operating, can mask tactile cues that indicate adverse
changes in handling characteristics, use of the autopilot is prohibited when:
1. Unusual lateral trim is required while the airplane is in icing conditions.
2. Autopilot trim warnings are encountered while the airplane is in icing conditions.
510FM-07 AA 2-33
SECTION II - OPERATING LIMITATIONS MODEL 510
FAA APPROVED
U.S. Configuration
KINDS OF OPERATIONS EQUIPMENT LIST
This airplane may be operated in day or night VFR or IFR and flight into known icing conditions when
the appropriate equipment is installed.
The following equipment list identifies the systems and equipment upon which type certification for
each kind of operation was predicated. The systems and items of equipment listed must be installed
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Citation Mustang airplane flight manual 1(21)
