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external walkaround and the systems check (if required).
The normal power-up check and the systems check are required:
• Before the airplane’s first flight of the day, or
• After a crew change, or
• After any related non-routine maintenance action, or
• If the airplane was left unattended by qualified personnel, or
• If the pilot-in-command has any doubt about the airplane status.
B. External Safety Inspection (First Flight of the Day)
This procedure must be performed before entering an airplane which has been left
unattended, or which is taken over from maintenance responsibility. This procedure must be
followed to ascertain that no obvious unsafe conditions exist prior to applying power (AC or
DC, pneumatic or hydraulic) to the airplane. All panels, not required for the safety inspection,
will be understood as closed and secured.
These procedures should be performed on through flights if there is any doubt that all safety
aspects of the prevailing situation can be covered.
During cold weather operations, the flight crew must ensure that the airplane fuselage, wings
and tail surfaces are free from ice, snow or frost (Refer to Chapter 6; SUPPLEMENTARY
PROCEDURES – COLD WEATHER OPERATION).
Start the inspection at the top of the boarding stairs, proceed in the direction indicated in
Figure 04−04−1 and terminate at the bottom of the passenger stair unit.
NORMAL PROCEDURES
Airplane Preparation
Vol. 1 04−04−1
REV 66, Feb 01/07
▼
CL−604 Operating Manual
PSP 604−6
1. AIRPLANE PREPARATION (CONT'D)
B. External Safety Inspection (First Flight of the Day) (Cont’d)
NORMAL PROCEDURES
Airplane Preparation
Vol. 1 04−04−2
REV 66, Feb 01/07
External Safety Inspection
Figure 04−04−1
CL−604 Operating Manual
PSP 604−6
1. AIRPLANE PREPARATION (CONT'D)
B. External Safety Inspection (First Flight of the Day) (Cont’d)
AIRPLANE DOCUMENTATION
(1) Maintenance status ..............................................Check Ensure that airplane
maintenance status is in
accordance with Minimum
Equipment List (MEL) and
Configuration Deviation List
(CDL) requirements.
LEFT FORWARD FUSELAGE
(1) Probe covers .................................................. Removed
NOSEWHEEL AND GEAR
(1) Chocks ............................................................. Installed
(2) Towbar ........................................................ As required
(3) ADG safety pin ................................................. Installed
(4) Nose door safety pin (if
applicable) ........................................................ Installed
(5) Downlock safety pin ......................................... Installed
(6) Brake accumulator gauges (2) .............................Check
(7) Position of nosewheel ..........................................Check Ensure steering angle is within
nominal operating range of
±55°.
(8) Fluid leaks ............................................................Check
(9) Covers/mooring lines...................................... Removed
RIGHT FORWARD FUSELAGE
(1) Probe covers .................................................. Removed
(2) Oxygen blowout plug............................................. Intact
RIGHT MAIN GEAR
(1) Chocks ........................................................ As required
(2) Wheel covers.................................................. Removed
(3) Fluid leaks ............................................................Check
(4) Downlock safety pin ......................................... Installed
RIGHT WING
(1) Flight control area and surfaces ............................ Clear Ensure proper clearance of all
flight control surfaces from all
ground equipment or other
obstructions. Ensure surfaces
clear of dirt, sand, ice, snow or
frost.
(2) Flap position ........................................................... Note
NORMAL PROCEDURES
Airplane Preparation
Vol. 1 04−04−3
REV 66, Feb 01/07
▼
CL−604 Operating Manual
PSP 604−6
1. AIRPLANE PREPARATION (CONT'D)
B. External Safety Inspection (First Flight of the Day) (Cont’d)
(3) Static wicks........................................Condition/secured
(4) Fluid leaks ............................................................Check
(5) Picket/mooring lines ....................................... Removed
(6) Fuel NACA vent cover.................................... Removed Ensure vent is clear of any
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庞巴迪挑战者604操作手册 Operating Manual 1(67)
