Hawker Beechcraft Hawker 800XP, Руководство по эксплуатации для пилотов, Страница: 847 / 923

Page 2-18
Pilot’s Operating Manual
Revision A2: Nov, 2004
Sub-section 2
GROUND SERVICING
Hawker 800XP Pro Line 21
Section VI - GROUND OPERATIONS
Test Refuel Control System Before Refuel (continued)
(c) Push the RIGHT OVER FLOW PRESS TO TEST and check:
• OVER FLOW is indicated.
• MASTER VALVE indicates SHUT.
• All three REFUEL VALVES indicate SHUT.
(d) Release the RIGHT OVER FLOW PRESS TO TEST and check all indications are
the same as those at the end of step (2).
(e) Push the VENTRAL P TO T and check:
• FULL is indicated.
• VALVE indication changes from OPEN to SHUT.
(f) Release the VENTRAL P TO T and check that all indications are the same as those
at the end of step (2).
(g) Push the L WING PRESS TO TEST and check:
• FULL is indicated.
• VALVE indication changes from OPEN to SHUT.
(h) Push the R WING PRESS TO TEST and check:
• FULL is indicated.
• VALVE indication changes from OPEN to SHUT.
(5) Select the VENTRAL and L & R WING tank REFUEL switches OFF and check:
• All VALVE indications revert to SHUT.
(6) Push the OVER PRESS PRESS TO TEST for more than 1 second, then release and
check:
• OVER PRESS is indicated.
• MASTER VALVE indicates SHUT and remains SHUT.
(7) Select the refuel MASTER switch OFF, then after approximately 2 seconds, select ON
and check the MASTER VALVE reopens.
Airworthiness Requirements
The previous Test Refuel Control System Before Refuel, Step (4) sub-steps (a) thru (h) is given to show
compliance with United States F.A.R. Part 25.979.