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External Power..................................................................................... 1-10
Generator Limits.................................................................................. 1-10
Oxygen System .....................................................................................1-11
Rudder Boost.........................................................................................1-11
Spoilers/Autospoilers/Spoilerons ....................................................1-11
Starter .....................................................................................................1-11
Thrust Reversers.................................................................................. 1-12
Tires ....................................................................................................... 1-12
Powerplant Limits.................................................................................. 1-12
Engine Type.......................................................................................... 1-12
Engine Computer ................................................................................ 1-12
Engine Operating Limits (Figure 1-4)............................................... 1-13
Engine Transient Speed Limits.......................................................... 1-14
N1 Limits (Figure 1-5)...................................................................... 1-14
N2 Limits (Figure 1-5)...................................................................... 1-14
Engine Temperature Limits (ITT)...................................................... 1-15
Starting (Figure 1-6)......................................................................... 1-15
Except Starting (Figure 1-7) ............................................................ 1-16
Fuel Limits............................................................................................... 1-17
Fuel Load/Balance .............................................................................. 1-17
Approved Fuels ................................................................................... 1-17
Fuel Additives...................................................................................... 1-17
Anti-Icing Additive ......................................................................... 1-17
Biocide Additive .............................................................................. 1-17
Fueling .................................................................................................. 1-17
Hydraulic Fluid Limits ......................................................................... 1-17
Approved Hydraulic Fluids ............................................................. 1-17
Change
Limitation
FM 132 1 1
FAA Approved 9-24-2004
Change 2
GENERAL
TYPE OF OPERATION
This airplane is certificated in accordance with FAR 25 in the transport
category and is eligible for the following kinds of operations when the
appropriate instruments and equipment required by the airworthiness
and operating requirements are installed and approved and are in operable
condition.
This airplane is approved for:
- VFR (Visual)
- IFR (Instrument)
- Day
- Night
- Icing
Icing conditions exist when outside air temperature (OAT) on the
ground and for takeoff is 10°C (50°F) or below, or the static air temperature
(SAT) in flight is 10°C (50°F) to -40°C (-40°F), and visible moisture
in any form is present (such as clouds, fog with visibility of one mile or
less, rain, snow, sleet, or ice crystals).
Icing conditions also exist when the OAT on the ground and for takeoff
is 10°C (50°F) or below when operating on ramps, taxiways, or runways
where surface snow, ice, standing water, or slush may be ingested
by the engines, or freeze on engines, nacelles, or engine sensor probes.
When icing or frost conditions exist, this airplane must be inspected
and operated in accordance with the Cold Weather Operation procedures
of Section II. These procedures include the requirement to assure
that all critical surfaces of the airplane (wing, vertical and horizontal
stabilizers, flight control surfaces, spoilers and flaps) are free of frost,
ice and snow for takeoff. Conducting only a visual inspection may not
detect very small levels of contamination; therefore, a tactile (hand on
surface) check of the wing leading edge and adjacent wing upper surface
is required when the ambient temperature is less than 10°C (50°F).
This airplane is not certificated for ditching under FAR 25.801.
PERFORMANCE CONFIGURATION
The airplane configuration must be as presented under Standard Performance
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