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Dispatch with an engine FADEC fault (ENG CTRL SYS L or R message displayed) is prohibited.
ENGINE FAN INSPECTION
Prior to engine start, the Engine Fan Duct and Fan inspection in Section III, Normal Procedures,
must be satisfactorily completed.
510FM-07 AA 2-11
SECTION II - OPERATING LIMITATIONS MODEL 510
FAA APPROVED
U.S. Configuration
ENGINE START LIMITATIONS (AIR)
Inter-Turbine Temperature (ITT) Limits . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Refer to Figure 2-3
Airspeed/Altitude Limits . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Refer to Figure 3-1
Minimum Temperature for Windmill Start . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . -10°C RAT
STARTER CYCLE LIMITATIONS
Starter Cycle Limitation. . . . . . . . . . . .Three engine starts per 30 minutes. Three cycles of operation
with a 60-second rest period between cycles is permitted.
NOTE
This limitation is independent of starter power source (i.e., battery, generator-assisted
cross start, or ground power unit) and applies to both starting and dry motoring of the
engine.
GROUND POWER UNIT LIMITATIONS FOR STARTING
Minimum/Maximum Current . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 800/1100 Amps
Maximum Voltage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 29 VDC
CAUTION
Normal starter current draw is approximately 1000 amps peak. Ground power
units with variable maximum current shutoff should be set to 1100 amps. Use
of a ground power source with voltage in excess of 29 VDC or current in
excess of 1100 amps may damage the starter.
BATTERY LIMITATIONS
Battery Start Limitation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Three engine starts per hour
Minimum Voltage for Start. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 24 Volts
CAUTION
Battery starts are prohibited at airport elevations above 10,000 feet. Above
10,000 feet, engines must be started using a ground power unit or using a
generator assisted cross start.
NOTE
• If battery limitation is exceeded, ground maintenance procedures are required.
Refer to Chapter 24 of the Maintenance Manual for procedure.
• Three generator-assisted cross starts are equal to one battery start.
• If a ground power unit is used for start, no battery cycle is counted.
2-12.1 AC 510FM-07
MODEL 510 SECTION II - OPERATING LIMITATIONS
FAA APPROVED
Configuration U.S.
ELECTRICAL POWER SYSTEM
Generator limits are as listed in Figure 2-8.
Figure 2-8
NOTE
The above limits are steady state limits. Following an engine battery start, generator
current may exceed 150 amps at ground idle for up to 5 minutes while the battery is
recharging. Above idle or during flight, transients up to 450 amps are permitted for up
to 2 minutes.
HYDRAULIC POWER SYSTEM
The only approved hydraulic fluid for the hydraulic power system is MIL-PRF-87257.
LANDING GEAR AND TIRE LIMITATIONS
The only approved hydraulic fluid for the landing gear struts is MIL-PRF-87257.
The tires listed in Figure 2-9 are the only tires approved. Tires must be inflated to the pressure
shown.
NOTE
If the ground operating temperature is expected to drop more than 28°C (50°F) or the
arrival airfield is expected to be more than 28°C (50°F) colder than the departure
airfield, refer to the Airplane Maintenance Manual for tire servicing.
Figure 2-9
STATUS LIMIT
On Ground, Idle 150 Amps
On Ground, Above Idle 300 Amps
Air < 30,000 Feet 300 Amps
Air > 30,000 Feet 280 Amps
POSITION VENDOR PART NUMBER UNLOADED
PRESSURE
LOADED
PRESSURE
Nose Tire Michelin 079-606-0 120 ± 5 PSIG 125 ± 5 PSIG
Dunlop DR17026T 120 ± 5 PSIG 125 ± 5 PSIG
Main Tires Michelin 021-523-0 85 ± 5 PSIG 88 ± 5 PSIG
Dunlop DR25526T 85 ± 5 PSIG 88 ± 5 PSIG
510FM-07 AA 2-13
SECTION II - OPERATING LIMITATIONS MODEL 510
FAA APPROVED
U.S. Configuration
GROUND OPERATION
Continuous engine ground static operation up to and including 5 minutes at takeoff thrust is limited to
ambient temperatures defined in Figure 2-13.
Limit ground operation of pitot-static heat to 2 minutes to preclude damage to the pitot tubes and stall
warning vane.
Movement of the flaps is prohibited at temperatures colder than -40°C.
FUEL LIMITATIONS
The corresponding electric fuel boost pump must be turned ON when the FUEL LO L-R CAS
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Citation Mustang airplane flight manual 1(10)
