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March 2003 or appropriate later revision), must be immediately available
to the flight crew.
ENGINE SYNCHRONIZER
ENG SYNC must be OFF for takeoff, landing, and single-engine
operation.
EXTERNAL POWER
The maximum amperage from an external power source must be limited
to 1500 amps.
GENERATOR LIMITS
Generator output is limited as follows:
Ground or Flight Operations
- Continuous — 300 amps.
If more electrical load is applied than can be supplied
by the generators, the current will be drawn
from the aircraft batteries and will not be shown on
the DC amps display. If this occurs, DC voltage will
be reduced.
- Transient — Higher transient loads for cross-starts and battery
charging are authorized.
NOTE
Limitations
FM-132 1-11
FAA Approved 9-24-2004
SYSTEM LIMITS (Cont)
OXYGEN SYSTEM
The following aircraft certification requirements are in addition to the
requirements of applicable operating rules. The most restrictive requirements
(certification or operating) must be observed.
Hats and “ear-muff” type headsets must be removed
prior to donning crew oxygen masks.
Crew and passenger oxygen masks are not approved for use above
40,000 feet cabin altitude. Prolonged operation of passenger masks
above 25,000 feet cabin altitude is not recommended.
Passenger masks are intended for use during an
emergency descent to an altitude not requiring supplemental
oxygen.
RUDDER BOOST
Rudder boost must be on for takeoff.
SPOILERS/AUTOSPOILERS/SPOILERONS
Spoilers:
Do not extend spoilers with flaps extended while airborne, except as
specified in EMERGENCY and/or ABNORMAL PROCEDURES in
Section III and Section IV, this manual.
Autospoilers:
Autospoilers must be armed for takeoff and landing, except, do not
arm autospoilers for training maneuvers where engine failure will be
simulated above V1 speed or for touch-and-go landings.
STARTER
The following cooling periods must be observed between consecutive
uses of the starter:
After Start Attempt Wait
1 1 minute
2 2 minutes
3 30 minutes
NOTE
WARNING
Limitations
1-12 FM-132
FAA Approved 9-24-2004
Change 1
SYSTEM LIMITS (Cont)
THRUST REVERSERS
Thrust reverser system use is limited to ground operations on paved
surfaces and attempts to deploy shall not be made in flight.
Thrust reversers must not be used to back up the aircraft.
Thrust reverser circuit breakers must not be intentionally pulled while
in flight, except as specified in EMERGENCY and/or ABNORMAL
PROCEDURES in Section III and Section IV of this manual.
Thrust reversers must not be used for touch-and-go landings.
Maximum reverse thrust is usable at speeds down to 40 KIAS.
Thrust reversers must be limited to idle reverse when the engines are
operating in MANual mode.
TIRES
Tire Limiting Speed (Ground Speed) ......................................... 165 knots
The takeoff and landing speeds presented in this
manual will not exceed this limit.
POWERPLANT LIMITS
ENGINE TYPE
On aircraft 45-2001 & subsequent not modified by SB 40-72-01, Honeywell
TFE731-20AR-1B turbofan propulsion engines.
On aircraft 45-2001 & subsequent modified by SB 40-72-01, Honeywell
TFE731-20BR-1B turbofan propulsion engines.
ENGINE COMPUTER
The engines must be operated at all times with the ENG CMPTR
switches in the ON position, except as specified in NORMAL,
EMERGENCY and ABNORMAL PROCEDURES in Sections II, III and
IV, this manual.
NOTE
Limitations
FM-132 1-13
FAA Approved 9-24-2004
Change 1
ENGINE OPERATING LIMITS

Maximum oil pressure may be exceeded for cold temperature starts for short
durations.
 Engine preheat is recommended at temperatures below -28°C.
 Allow oil temperature to increase to 30°C prior to increasing thrust above idle. If cold
ambient conditions prevent oil temperature from obtaining 30°C, idle thrust may be
exceeded as required.
 If altitude is greater than 30,000 feet: Oil Temperature — 140°C.
If altitude is 30,000 feet or less: Oil Temperature — 127°C.
 Manual Mode or RMU — 917°C (amber), Limit — 942°C (red).
 The thrust setting tables, in Section V, may be more limiting than the values listed
here.
 Anti-ice ON limit.
Figure 1-4
Operating Condition Operating Limits
Thrust
Setting
Time Limit
Minutes
N1
%

Max
ITT °C
N2
%
Oil Press
psi
Oil Temp
　
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