Hawker Beechcraft Hawker 800XP, Руководство по эксплуатации для пилотов

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Pilot’s Operating Manual
P/N 140-590032-0007
Revision A4: Sep, 2010
Page 1-7
Section V Sub-section 1
NORMAL HANDLING
WHEEL BRAKES
The normal wheel brake system incorporates Maxaret anti-skid units which automatically reduce the
brake pressure should a wheel tend to skid.
NOTE: The Maxaret unit does not operate until the wheel is revolving, therefore the brakes must not
be applied before touchdown.
It should be noted that the emergency braking system by-passes the anti-skid units, therefore care
should be exercised when using this system.
If any of the wheels' fusible plugs blow, the brakes must be inspected and certified serviceable before
the next takeoff.
The brakes are of adequate capacity to bring the airplane to a stop under all circumstances, including
a rejected takeoff from V
1
, provided the brake procedures in the AFM Section 5.05 are complied with.
Repeated Wheel Brake Usage
If repeated braked landings are made for crew training or any other reason, the brakes and tires may
not have time to cool between runs and their temperatures may rise to an undesirable level. The
following restrictions should therefore be observed:
• Heavy braking should not be used more than necessary for the purpose of the exercise, and the
landing gear should be extended as long as possible - never less than five minutes in each circuit.
• Landings with light braking may be repeated at intervals of not less than fifteen minutes. After a
landing with heavy braking, one or more touch and go circuits should be done, and a time of 30
minutes should elapse before the next braked landing.
For established cooling times, refer to the table in the Airplane Flight Manual Section 2 - LIMITATIONS.
TAKEOFF
Refer to the following paragraphs and referenced figures for recommended takeoff sequences and
procedures.
ICE PROTECTION - BEFORE TAKEOFF
Prime the airframe ice protection system by setting the WING/TAIL ANTICE time switch to run the pump
for two minutes. Check that priming is complete before start of takeoff.
If the outside air temperature is 10° C or below and is associated with conditions of high humidity, i.e.,
mist or fog reducing visibility to approximately 1 mile (1,600 meters), or with a wet runway surface, set
ENG ANTICE 1 and 2 and ENG IGNITION 1 and 2 to ON.
NOTE: ENG ANTICE 1 and 2 should be selected ON before setting take-off thrust.
When takeoff is made with ENG ANTICE 1 and 2 selected ON, ITT must be monitored during takeoff
and initial climb.
Allowance must be made for the use of ENG ANTICE on performance by reference to the appropriate
figures in the Airplane Flight Manual Sub-section 5.05.
If necessary, the airframe WING/TAIL ANTICE switch may also be selected on for takeoff. Switch ENG
ANTICE 1 and 2 to OFF and the ENG IGNITION 1 and 2 to off when conditions permit.