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°C
Min Max Min Max
APR 5 100.0 963 101.0 50 100 30 127
T/O 5 100.0
941
963
100.0 50 100 30 127
MCT Continuous 100.0
916
941
100.0 50 100 30
140 %
30,000 ft.
127 &
MCR Continuous 100.0 900 100.0 50 100 30
140 %
30,000 ft.
127 &
Ground
Idle
Continuous - - - 50 100 30 127
Flight
Idle
Continuous - - - 50 100 30 127
Starting 1 100.0 941
Immediate
Rotation
-
125
-28
127
EFFECTIVITY
Aircraft 45-2001 & Subsequent
not modified by SB 40-72-01
Limitations
1-14 FM-132
FAA Approved 9-24-2004
ENGINE TRANSIENT SPEED LIMITS
N1 LIMITS
N2 LIMITS
Reduce applicable N1 or N2 below limit.
Reduce applicable N1 or N2 below limit. Record maximum N1 or N2, and time
above limit in engine log book. Refer to Honeywell Engine Light Maintenance Manual
for control check and performance calibration.
Reduce applicable N1 or N2 below limit. Record maximum N1 or N2, and time
above limit in engine log book. Refer to Honeywell Engine Light Maintenance Manual
for overspeed inspection.
N2 may operate for 5 minutes in APR.
NOTE: There may be a momentary N1 red EI illumination which is allowable.
Figure 1-5
100
101
102
103
0
TIME ~ SECONDS
N 1 PERCENT (PHYSICAL)
10
100.5
2 3
1
Limitations
FM-132 1-15
FAA Approved 9-24-2004
Change 1
ENGINE TEMPERATURE LIMITS (ITT)
STARTING
Abort start. Record maximum ITT and time in excess of 941°C in engine log book.
Determine cause and correct prior to next start.
Abort start. Record maximum ITT and time in excess of 941°C in engine log book.
Refer to Honeywell Engine Light Maintenance Manual for static takeoff power check.
Abort start. Record maximum ITT and time in excess of 941°C in engine log book.
Refer to Honeywell Engine Light Maintenance Manual for hot section inspection.
Figure 1-6
EFFECTIVITY
Aircraft 45-2001 & Subsequent
not modified by SB 40-72-01
0 10
940
TIME-SECONDS
950
960
970
980
3
1 2
981°C
941°C
INTERSTAGE TURBINE TEMPERATURE (ITT) ~ °C
Limitations
1-16 FM-132
FAA Approved 9-24-2004
Change 1
ENGINE TEMPERATURE LIMITS (ITT) (Cont)
EXCEPT STARTING
Reduce thrust below limit (Anti-ice Off).
Record APR cycle in engine log book per Honeywell Engine Light Maintenance Manual.
Reduce thrust below limit. Record maximum ITT and time in excess of 963°C in
engine log book. Refer to Honeywell Engine Light Maintenance Manual.
Reduce thrust below limit. Record maximum ITT and time in excess of 941°C in
engine log book. Refer to Honeywell Engine Light Maintenance Manual for hot section
inspection.
Figure 1-7
EFFECTIVITY
Aircraft 45-2001 & Subsequent
not modified by SB 40-72-01
0 5
900
TIME-MINUTES
910
920
930
940
INTERSTAGE TURBINE TEMPERATURE (ITT) ~ °C
950
960
970
980
1
2
3
900°C (MCR)
916°C (MCT Anti-ice Off)
941°C (T/O Anti-ice Off)
963°C (T/O Anti-ice ON)
963°C (APR) 4
981°C
941°C (MCT Anti-ice ON) ( )
Limitations
FM-132 1-17
FAA Approved 9-24-2004
Change 1
FUEL LIMITS
FUEL LOAD/BALANCE
Do not takeoff or land with wing fuel imbalance greater than 200
pounds (91 kg).
During flight, wing fuel balance must be maintained within 200
pounds (91 kg).
APPROVED FUELS
The mixing of fuel types is allowed.
JP-5, JP-8, Jet A and Jet A-1 fuels are approved. Refer to Addendum I —
FUEL SERVICING for a listing of approved fuels.
FUEL ADDITIVES
ANTI-ICING ADDITIVE
Anti-icing additive is not a requirement. Refer to Addendum I — FUEL
SERVICING for additional information.
BIOCIDE ADDITIVE
Biocide additive is not a requirement. However, Biobor JF is approved
for use as a biocide additive when premixed with fuel in the fuel supply
facility. Blending of Biobor JF and fuel using the gravity fill method of
refueling is not approved. Additive concentration is not to exceed 270
ppm. Refer to Addendum I — FUEL SERVICING for additional
information.
FUELING
Single-point pressure refueling is limited to 55 psig (3792 hPa) and defueling
is limited to -10 psig (-690 hPa).
HYDRAULIC FLUID LIMITS
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