Hawker 750/800XP/850XP/900XP
Ground Handling Checklist
Part I - Pre-Flight Checks
Table of Contents
Page
Pre-Flight Checks ........................................................................................5
Preamble ........................................................................................................5
A. General......................................................................................................5
B. Left Nose and Fuselage...........................................................................5
C. Nose Landing Gear and Bay ...................................................................6
D. Right Nose and Fuselage ........................................................................6
E. Right Wing ................................................................................................6
F. Right Main Landing Gear.........................................................................7
G. Right Engine and Nacelle ........................................................................7
H. Aft Fuselage — Right Side ......................................................................8
I. Empennage (Tail Section) .......................................................................8
J. Aft Fuselage — Left Side.........................................................................8
K. Rear Equipment Bay ................................................................................9
L. Left Engine and Nacelle...........................................................................9
M. Left Main Landing Gear and Center Keel.............................................10
N. Left Wing.................................................................................................10
O. Flight Compartment ...............................................................................11
P. Vestibule, Passenger Cabin and Toilet Compartment........................11
Q. Final Items ..............................................................................................12
List of Illustrations
General
Figure 1 - Recommended Walk-Around Sequence
Airplanes Without Winglets ....................................................2
Figure 2 - Recommended Walk-Around Sequence
Airplanes With Winglets .........................................................4
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C
A GENERAL D RIGHT NOSE AND FUSELAGE
B LEFT NOSE AND FUSELAGE D E RIGHT WING
C NOSE LANDING GEAR AND BAY B O
START
A
N LEFT WING P
Q
O FLIGHT COMPARTMENT
P VESTIBULE, PASSENGER CABIN AND TOILET
Q FINAL ITEMS
N E
M F
H
K
L G
J AFT FUSELAGE - LEFT SIDE F RIGHT MAIN LANDING GEAR
K REAR EQUIPMENT BAY J G RIGHT ENGINE AND NACELLE
L LEFT ENGINE AND NACELLE I H AFT FUSELAGE - RIGHT SIDE
M LEFT MAIN LANDING GEAR I EMPENNAGE (TAIL SECTION)
AND CENTER KEEL
WALK-AROUND DIRECTION
BELOW AIRCRAFT
HA00C
071500AA.AI
INSIDE AIRCRAFT
Figure 1
Recommended Walk-Around Sequence
Airplanes Without Winglets
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Ground Handling Checklist
Intentionally left blank
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C
A GENERAL D RIGHT NOSE AND FUSELAGE
B LEFT NOSE AND FUSELAGE E RIGHT WING AND WINGLET
D
C NOSE LANDING GEAR AND BAY
O F RIGHT MAIN LANDING GEAR
B
START
A
N LEFT WING AND WINGLET P
Q
O FLIGHT COMPARTMENT
P VESTIBULE, PASSENGER CABIN AND TOILET
Q FINAL ITEMS
N E
M F
H
K
L G
J AFT FUSELAGE - LEFT SIDE
K REAR EQUIPMENT BAY
J G RIGHT ENGINE AND NACELLE
I
L LEFT ENGINE AND NACELLE H AFT FUSELAGE - RIGHT SIDE
M LEFT MAIN LANDING GEAR I EMPENNAGE (TAIL SECTION)
AND CENTER KEEL
WALK-AROUND DIRECTION
BELOW AIRCRAFT
HA00C
071501AA.AI
INSIDE AIRCRAFT
Figure 2
Recommended Walk-Around Sequence
Airplanes With Winglets
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Hawker 750/800XP/850XP/900XP
Ground Handling Checklist
Part I
PRE-FLIGHT CHECKS
Before proceeding with these checks, make sure that you have read and understood the Preamble and
the notes that follow the Preamble.
Preamble
The PRE-FLIGHT CHECKS supersede and replace the PRE-FLIGHT INSPECTION which was previously listed
in the Hawker 800XP AIRCRAFT FLEXIBLE MAINTENANCE SCHEDULE.
It is the responsibility of the Flight Crew and Pilot-in-Command to ensure the items contained within are
accomplished before flight. The Flight Crew or appropriately rated maintenance personnel may accomplish all
items. It is recommended that these pages be photocopied and used as a check-off sheet prior to each flight.
NOTE: Requirements marked with 4 (preceding the check) need only be completed once daily, before the
first flight.
NOTE: These checks should be done prior to and in conjunction with the External Checks and Internal
Checks listed in the Normal Procedures section of the FAA Approved Airplane Flight Manual.
NOTE: Refer to Figure 1 or Figure 2 (as applicable) — Recommended Walk-Around Sequence.
Check Box when
A. General Complete
(1) Make sure that any defects reported in the technical log or Pilot’s Report have been
cleared or cleared for flight in accordance with the Minimum Equipment List.
(2) Assure that Post Flight Checks have been accomplished.
NOTE: Do not remove gear pins.
(3) Remove external covers, plugs, guards, internal control locks (if installed) and stow
correctly (Part III, Para. C).
B. Left Nose and Fuselage
(1) Make sure the stall detector vane moves freely through the full range of travel. Vane
movement must be smooth and damped.
4 (2) Check pitot tube condition, cover removed and hole clear.
(3) Check static plate and static ports for condition; free from dents, corrosion, contaminants
and obstructions.
(4) Check OAT sensor probe for condition.
(5) Check ice detector for condition and rotor movement.
(6) Check external fuselage and flight compartment windows for damage.
(7) Check nose skin, forward of static plate, free from dents, paint bubbles and sealant
bulges.
(8) Make sure avionics access door (if installed) is correctly seated and secure.
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(9) Check radome for condition and security.
(10) Check condition of nose taxi light lens and bulbs (L and R).
C. Nose Landing Gear and Bay
(1) Make sure the nose landing gear ground lock is installed in the nose landing gear and
is secure.
(2) Make sure there is no visible damage to doors, nose gear assembly or wheels.
(3) Check the nose gear bay to make sure there is no fluid leakage.
(4) Check condition of wiring and hoses.
4 (5) Make sure that the auxiliary hydraulic system reservoir has been checked.
(6) Check nose landing gear doors are closed and manual release is secure.
4 (7) Visually check the strut for normal condition.
4 (8) Check tires for condition.
D. Right Nose and Fuselage
(1) Check radome for condition and security.
(2) Make sure avionics access door (if installed) is correctly seated and secure.
(3) Check nose skin, forward of static plate, free from dents, paint bubbles and sealant
bulges.
(4) Check static plate and static ports for condition; free from dents, corrosion,
contaminants and obstructions.
(5) Check external fuselage and flight compartment windows for damage.
4 (6) Check pitot tube condition, cover removed and hole clear.
(7) Make sure the stall detector vane moves freely through the full range of travel. Vane
movement must be smooth and damped.
(8) Make sure venturi outlet is clear.
(9) Check SAT sensor for condition.
(10) Check external fuselage and windows for damage; overwing emergency exit closed
and flush with fuselage and dorsal air intake cover removed and intake clear.
E. Right Wing
(1) Make sure that all water has been drained from the center section fuel tank sumps
(Part III, Para. D).
(2) Check condition of the wing ice light lens and bulb.
(3) Check condition of overwing fillet fairing.
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(4) Check the condition of the external structure of the wing to make sure it is clean and
undamaged; upper and lower surface (no fuel leaks), leading edge, stall strip, landing
and taxi lights (condition of lens and bulbs) and vortilon.
(5) Make sure the vortex generators are secure and not deformed.
(6) Check the overwing fuel cap for security.
(7) Make sure the stall warning system vent (if installed) is clear.
(8) Make sure the NACA vent is clear.
(9) Check drain vent surge tank drain.
(10) Check condition of strobe and navigation light lens and bulbs/LEDs (if installed).
(11) Check condition of wing tip. Check winglet (if installed).
(12) Check condition of aileron and aileron trim tab.
(13) Make sure there are no foreign objects or debris in the aileron shrouds.
(14) Make sure the aileron moves freely through the full range of travel.
(15) Check condition of flap and air brakes.
(16) Check for damaged or missing static wicks.
F. Right Main Landing Gear
(1) Make sure main landing gear ground lock is installed in the main landing gear and is
secure.
(2) Visually inspect the side stay components and attach points for security and make
sure there is no visible damage.
4 (3) Visually check the strut for normal condition.
4 (4) Check tires for condition.
(5) Make sure there is no visible damage to the fairing and main landing gear doors.
(6) Check the main gear and inside the main gear bay to make sure there is no fluid
leakage.
(7) Check condition of wiring and hoses.
G. Right Engine and Nacelle
(1) Check right engine, remove engine cover and make sure there are no visible oil leaks
in the engine intake and cowling and free from foreign objects.
WARNING: DO NOT ATTEMPT TO STOP THE FAN BY HOLDING THE BLADES IF THE FAN IS
WINDMILLING. THE BLADES ARE SHARP. STOP THE FAN BY PUSHING ON THE
SPINNER.
(2) Make sure there is no damage to the fan blades when viewed through the engine
intake.
(3) Check P2T2 sensor clean, undamaged and secure.
(4) Make sure the starter generator cooling intake and outlet are unobstructed.
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(5) Check general condition of cowling and latches for damage, vents and drain holes
should be clear.
(6) Check engine oil tank quantity (Part III, Para. L) and engine oil filter bypass pin (if
installed).
(7) Make sure there is no damage to the turbine blades when viewed through the
exhaust.
(8) Make sure there are no visible oil leaks in the engine cowling and engine exhaust
areas.
(9) Check engine exhaust drain mast clear, no leaks.
4 (10) Make sure the pin is removed from the thrust reverser and the TR is stowed and is
secure.
H. Aft Fuselage — Right Side
4 (1) Check the APU (if installed) exhaust is unobstructed/undamaged.
(2) Check condition of pressure refuelling cap and make sure it is secure. Make sure the
pressure refuelling door is closed and secured.
(3) Make sure the ground power unit access door is secure.
(4) Make sure the oxygen charging port access panel is secure.
I. Empennage (Tail Section)
(1) Check condition of tailcone and make sure it is secured and locked and the vents are
unobstructed.
(2) Check condition of tailcone strobe and navigation light lenses and bulbs.
(3) Make sure there is no visible damage to the vertical stabilizer and rudder.
(4) Make sure there is no visible damage to the horizontal stabilizer and elevator.
(5) Visually check that vortex generators are present and undamaged (airplanes with
winglets only).
(6) Check condition of the upper anti-collision light.
(7) Check condition of static wicks, present and undamaged.
J. Aft Fuselage — Left Side
(1) Check ventral tank (if installed) filler cap for security and make sure the ventral tank
access door is closed and secure.
(2) Check ventral tank (if installed) fairing installed and secure.
(3) Make sure the fire extinguisher pressure relief indication disc for each engine is intact
and the APU (if installed) fire extinguisher pressure relief indication disc is intact (for
Hawker 800XP airplanes only).
(4) Make sure the APU (if installed) inlet is clear and unobstructed.
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(5) Check the External Baggage Compartment (EBC) fire bottle for the correct pressure for
the existing temperature, which is found on the attached placard (Hawker 750 only).
(6) Check that the EBC forward and aft fire detectors are not damaged (Hawker 750 only).
(7) Make sure the EBC and baggage compartment door are undamaged and latched
(Hawker 750 only).
K. Rear Equipment Bay
(1) Open hatch to rear equipment bay and check condition of hatch.
(2) Open upper hatch and check condition of upper hatch (Hawker 750 only).
(3) Check general condition of rear equipment bay.
(4) Check the maintenance panel (if installed), located next to the hydraulic accumulators.
(5) Assure that hydraulic accumulator pressures have been checked. Check for minimum
pressure.
(6) Assure that the main hydraulic reservoir contents (dependant on accumulator pressure)
have been checked and there are no leaks.
(7) Check battery connectors for security.
(8) Check computers, connected and secure.
(9) Check APU (if installed) general condition, no leaks.
(10) Make sure the fire extinguisher pressure relief indication disc, located in the rear bay
adjacent to the APU (if installed) is intact (Hawker 750, 850XP and 900XP airplanes
only).
(11) Check stick pusher assembly, general condition/no leaks.
(12) Make sure equipment bay light is off and the hatch is closed and latched securely.
(13) Make sure the lower hatch is closed and latched securely (Hawker 750 only).
L. Left Engine and Nacelle
(1) Remove engine cover and check exhaust and make sure it is free from foreign objects.
(2) Make sure there is no damage to the turbine blades when viewed through the
exhaust.
(3) Make sure there are no visible oil leaks in the engine cowling and engine exhaust
areas.
4 (4) Make sure the pin is removed from the thrust reverser and the TR is stowed and
secure.
(5) Check general condition of cowling and latches for damage, vents and drain holes
should be clear.
(6) Check engine oil tank quantity (Part III, Para. L) and engine oil filter bypass pin (if
installed).
(7) Check engine exhaust drain mast clear, no leaks.
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(8) Make sure there are no visible oil leaks in the engine intake and cowling.
WARNING: DO NOT ATTEMPT TO STOP THE FAN BY HOLDING THE BLADES IF THE FAN IS
WINDMILLING. THE BLADES ARE SHARP. STOP THE FAN BY PUSHING ON THE
SPINNER.
(9) Make sure there is no damage to the fan blades when viewed through the engine intake.
(10) Check P2T2 sensor clean, undamaged and secure.
(11) Make sure the starter generator cooling intake and outlet are unobstructed.
M. Left Main Landing Gear and Center Keel
(1) Make sure the main landing gear ground lock is installed in the main landing gear and
is secure.
(2) Visually inspect the side stay components and attach points for security and make
sure there is no visible damage.
4 (3) Visually check the strut for normal condition.
4 (4) Check tires for condition.
(5) Make sure there is no visible damage to the main landing gear doors and fairing.
(6) Check the main gear and inside the main gear bay to make sure there is no fluid
leakage.
(7) Check condition of wiring and hoses.
(8) Check condition of anticollision light lens and bulb, located on the center keel.
(9) Check all antennas attached to keel are secure and undamaged.
(10) Make sure that all water has been drained from ventral fuel tank (if installed; Part III,
Para. D).
N. Left Wing
(1) Check condition of flap and air brakes.
(2) Check for damaged or missing static wicks.
(3) Check condition of aileron and aileron trim tab.
(4) Make sure there are no foreign objects or debris in the aileron shrouds.
(5) Make sure the aileron moves freely through the full range of travel.
(6) Check condition of wing tip. Check condition of winglet (if installed).
(7) Check condition of strobe and navigation light lens and bulbs/LEDs (if installed).
(8) Check drain vent surge tank drain.
(9) Make sure the NACA vent is clear.
(10) Make sure the vortex generators are secure and not deformed.
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Ground Handling Checklist
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(11) Check the overwing fuel cap for security.
(12) Make sure the stall warning system vent (if installed) is clear.
(13) Check the condition of the external structure of the wing to make sure it is clean and
undamaged; upper and lower surface (no fuel leaks), leading edge, stall strip, landing
and taxi lights (condition of lens and bulbs) and vortilon.
(14) Check condition of wing ice light lens and bulb.
(15) Check condition of overwing fillet fairing seal.
(16) Check condition of the boarding light lens and bulb.
(17) Check condition of the main entry door seal/frame, external fuselage and windows.
(18) Make sure that all water has been drained from the center section fuel tank sumps
(Part III, Para. D).
O. Flight Compartment
(1) Make sure all flashlights function correctly.
(2) Make sure the auxiliary hydraulic system handpump handle/rudder gust lock is
properly stowed.
(3) Make sure the dump valve lever is set to SHUT.
(4) Make sure there is full and free movement of the aileron, elevator and rudder primary
controls.
(5) Make sure the oxygen system contents are adequate and the valves are ON
(Part III, Para H).
4 (6) With the landing gear ground locks installed, make sure that the emergency
dump valve is properly exercised by operating the auxiliary hydraulic system
selector handle several times. Investigate any undue stiffness in operation. On
completion of the check, make sure the selector handle is reset to the fully-in position.
(7) Check protective breathing equipment and portable breathing equipment (if installed).
(8) Check the airframe anti-icing system tank contents.
(9) Check the fuel tanks for required fuel quantities.
NOTE: If the airplane will be operated in an area where microbiological contamination of
fuel is likely to exist, it is strongly recommended that regular use is made of fuel
treated with an approved biocidal additive. Refer to Section 2 (Limitations) in the
FAA Approved Airplane Flight Manual.
P. Vestibule, Passenger Cabin and Toilet Compartment
(1) Make sure all emergency equipment is on board and properly stowed.
(2) Make sure the emergency exit door is secure.
(3) Remove the emergency exit internal locking pin (if installed) and stow securely.
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Ground Handling Checklist
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Q. Final Items
(1) Make sure that all access doors and servicing panels are secure.
(2) Make sure that any frost, snow or ice is removed, refer to AFM Section 2 for
limitations. Make sure that any accumulation of snow or ice is removed from the air
conditioning system cooling turbine exhaust duct before starting the APU or the main
engines.
(3) Make sure steering disconnect pin, located between the nose gear torque link sleeve
and the steering sleeve, is secured in place with the quick-release pin locked. Quick-
release pin is locked when indicator groove is exposed and level with the head.
(4) Remove the gear pins and stow (Part III, Para C).
Completion Record
Airplane Registration:...............................................................................................................................
Time completed at:.................................................. Date:...................................................................
Completed by:.........................................................................................................................................
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