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when the outside air temperature is less than 10°C (50°F) or if it cannot be determined that
the wing fuel temperature is above 0°C (32°F) and:
a. There is visible moisture present (rain, drizzle, sleet, snow, fog, etc.); or
b. Water is present on the wing upper surface; or
c. The difference between the dew point and the outside temperature is 3°C (5°F) or less;
or
d. The atmospheric conditions have been conducive to frost formation.
ENROUTE OPERATIONAL LIMITS
GENERAL
Maximum Operating Altitude. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 41,000 Feet
Maximum Ambient Temperature . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Refer to Figure 2-13
Minimum Ambient Temperature . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Refer to Figure 2-13
Maximum Altitude for Extension of Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18,000 Feet
Minimum Temperature for Operation of Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . -40°C RAT
Yaw Damper must be engaged above FL300.
510FM-07 AA 2-19
SECTION II - OPERATING LIMITATIONS MODEL 510
FAA APPROVED
U.S. Configuration
TAKEOFF / LANDING / ENROUTE TEMPERATURE
LIMITS
Figure 2-13
NOTE
• Ambient air temperature is ISA temperature corrected for indicated ISA deviation
(reference Figures 4-2 and 4-3).
• For operations below -10°C (+14°F), refer to Section III, Normal Procedures,
COLD WEATHER OPERATIONS.
• Long term operation (>30 minutes) is limited to a maximum of ISA + 31°C if the air
conditioner is inoperative or turned OFF.
2-20 AA 510FM-07
MODEL 510 SECTION II - OPERATING LIMITATIONS
FAA APPROVED
Configuration U.S.
ENROUTE OPERATIONAL LIMITS (Continued)
RVSM OPERATIONS
Minimum Speed in RVSM Airspace . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 110 KIAS
Minimum Weight in RVSM Airspace . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6300 Pounds
The following equipment must be installed and operating normally upon entering RVSM airspace:
• Pilot and copilot primary altimeters
• Autopilot
• Altitude Alerter
• ATCRBS Transponder
NOTE
• Any changes to the pitot-static, air data computer, autopilot, altitude alerting and/
or transponder systems, or other changes that affect operation of these systems
must be evaluated for impact on the RVSM approval.
• The standby altimeter is not approved for RVSM operations.
Each operator must ensure compliance with required crew training and operating practices and
procedures. Individual airplane and operational approval must be obtained in accordance with
applicable operating rules.
MINIMUM CREW
Except where otherwise prescribed by applicable operating limitations,
Minimum Crew for all operations:
One pilot, provided:
• The pilot holds a CE510(S), single-pilot type rating
• The airplane is equipped for single-pilot operation as specified in the Kinds of Operations
Equipment List
• The pilot must occupy the left pilot’s seat
Or
One pilot and one copilot provided:
• The pilot holds a CE510(S) or CE510 (second-in-command required) pilot type rating
LOAD FACTOR
Flaps - UP (0º) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . -1.44 to +3.6G at 8645 pounds
Flaps - TAKEOFF / APPROACH or LAND (15º or 30º). . . . . . . . . . . . . .0.0 to +2.0G at 8645 pounds
NOTE
These accelerations limit the angle-of-bank in turns and limit the severity of pull-up
maneuvers.
(Continued Next Page)
510FM-07 AA 2-21
SECTION II - OPERATING LIMITATIONS MODEL 510
FAA APPROVED
U.S. Configuration
CABIN PRESSURIZATION LIMITATIONS
Normal Cabin Pressurization Limitations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 0.0 to 8.5 (+0.1) PSID
MANEUVER LIMITATIONS
Acrobatic maneuvers, including spins, are prohibited.
Intentional stalls are prohibited above 18,000 feet.
Refer to Figure 2-12 for maximum maneuvering speeds.
PASSENGER COMPARTMENT
For taxi, takeoff, and landing, adjustable passenger seats must be positioned with seatbacks upright.
Passenger seat belts must be properly fastened.
The maximum passenger seating, not including 2 crew seats, is four.
The use of the lavatory is prohibited for taxi, takeoff, and landing and is limited to one occupant in
flight.
BAGGAGE COMPARTMENTS
Nose Baggage Compartment (L-R) . . . . . . . . . . . . . . . . . . . . . . . 320 pounds maximum (combined)
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Citation Mustang airplane flight manual 1(13)
