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THRUST SETTING TIME LIMIT
(MINUTES)
ITT
TEMPERATURE °C N2% N1% OIL PRESSURE
PSI
OIL TEMPERATURE
°C
START --- 862
SEE FIGURE 2-3 --- --- 0 TO 250
(NOTE 5) -40 MINIMUM
GND IDLE CONTINUOUS --- 48.6 --- 24 MINIMUM -40 TO 135
(NOTE 3)
FLT IDLE CONTINUOUS --- 56.8 (MINIMUM)
(NOTE 4) --- SEE FIGURE 2-7 22 TO 135
TAKEOFF
(TO DETENT)
5
(NOTE 1) 830 100.0 100.0
(NOTE 1) SEE FIGURE 2-7 22 TO 135
(NOTE 3)
MAXIMUM
CONTINUOUS
(CLB DETENT)
CONTINUOUS 830 100.0 100.0
(NOTE 2) SEE FIGURE 2-7 22 TO 135
MAXIMUM CRUISE
(CRU DETENT) CONTINUOUS 830 100.0 100.0 SEE FIGURE 2-7 22 TO 135
TRANSIENT
20 SECONDS 862
SEE FIGURE 2-4
102.0
SEE FIGURE 2-5
101.0
SEE FIGURE 2-6 --- ---
90 SECONDS --- --- --- SEE FIGURE 2-7 135 TO 141
15 / 500 SECONDS --- --- --- SEE FIGURE 2-7 ---
2-6 AA 510FM-07
MODEL 510 SECTION II - OPERATING LIMITATIONS
FAA APPROVED
Configuration U.S.
OVERTEMPERATURE LIMITS - STARTING
Figure 2-3
510FM-07 AA 2-7
SECTION II - OPERATING LIMITATIONS MODEL 510
FAA APPROVED
U.S. Configuration
OVERTEMPERATURE LIMITS - EXCEPT STARTING
Figure 2-4
2-8 AA 510FM-07
MODEL 510 SECTION II - OPERATING LIMITATIONS
FAA APPROVED
Configuration U.S.
N2 ENGINE OVERSPEED LIMITS
Figure 2-5*
510FM-02 AA 2-9
SECTION II - OPERATING LIMITATIONS MODEL 510
FAA APPROVED
U.S. Configuration
N1 ENGINE OVERSPEED LIMITS
Figure 2-6*
2-10 AA 510FM-02
MODEL 510 SECTION II - OPERATING LIMITATIONS
FAA APPROVED
Configuration U.S.
ENGINE OIL PRESSURE LIMITS
Figure 2-7
FADEC (FULL AUTHORITY DIGITAL ENGINE CONTROL)
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. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 22 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.
If the BATTERY O’TEMP message displays during ground operations, dispatch is prohibited until
after the proper maintenance procedures have been accomplished.
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 AB 510FM-07
MODEL 510 SECTION II - OPERATING LIMITATIONS
FAA APPROVED
Configuration U.S.
ENGINE OIL PRESSURE LIMITS
Figure 2-7
FADEC (FULL AUTHORITY DIGITAL ENGINE CONTROL)
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Citation Mustang airplane flight manual 1(9)
