曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

(8) Static dischargers (6) ......................................Condition
(9) Navigation and strobe lights ............................Condition
(10) Winglet ............................................................Condition
(11) Leading edge...................................................Condition
(12) Fuel vent valve .....................................................Check
(13) Fuel drains............................................................Check
(14) Lower wing surface .........................................Condition
(15) Wing anti-ice exhaust louvres ............................... Clear
(16) Upper wing surface .........................................Condition
(17) Engine intake......................................................... Clear
(18) Fuel filler cap .................................................... Secured
(19) Landing and taxi lights.....................................Condition
LEFT MAIN GEAR (Front)
(1) Area security ......................................................Verified
(2) Tires and wheels .............................................Condition
(3) Brakes and wear pins...........................................Check
(4) Gear door ......................................................... Secured
NOTE
If abnormal resistance is felt during pin extraction, do not remove pin.
Leave pin in place and request maintenance checkout.
(5) Downlock safety pin ......................................... Remove
(6) Downlock dust cover ........................................ Installed
LEFT UPPER FUSELAGE (Forward)
(1) Wing inspection lights......................................Condition
(2) Antennae ..............................................................Check VHF 1, ATC 1 and TCAS
(if installed).
BEFORE ENTERING AIRPLANE
(1) NLG door safety switch ........................................Check Set to FLT/CLOSE DOOR.
NORMAL PROCEDURES
Airplane Preparation
Vol. 1 04−04−19
REV 68, Apr 16/07
▼
CL−604 Operating Manual
PSP 604−6
1. AIRPLANE PREPARATION (CONT'D)
D. External Walkaround (Cont’d)
ENTERING AIRPLANE
(1) Door area security ..............................................Verified
(2) Pax door vent flap ............................................Checked 1
If door is closed and locked:
(a) Passenger door outer handle
trigger plate.....................................................Push and as the outer handle
comes out of the housing,
check that the vent flap
(flapper door) springs open.
If door is fully open:
(a) Passenger door vent flap
(flapper door) ................................................Check for spring tension by pulling
door vent flap outboard, to
verify that spring has not
disconnected.
(3) Stairs ................................................................Checked
(4) Gear and safety pins .......................................On board
E. Systems Check
During the systems check, the airplane systems and components are checked and configured
for the coming phases of flight.
The systems check will be performed by the flight crew, as applicable. Only the RH side
console and RH instrument panel items are checked by the copilot.
The external and internal pre-flight checks will be accomplished by the pilot and the co-pilot
prior to the start of this check.
COCKPIT
(1) Seat and harness .................................................Adjust Set seat to full aft position.
Fasten lap belt and shoulder
harness. Adjust height to
obtain optimum eye reference
position using indicator on
center windscreen post.
Check that seat position is not
restrictive when moving the
control column full forward and
full aft.
NOTE
The correct eye reference position is obtained by adjusting the seat so
that the white ball appears to cover the orange ball. The resulting eye
level should be approximately in the centre of the windshield (Refer to
FCOM Vol. 2, Chapter 1; AIRPLANE GENERAL – SEATS).
NORMAL PROCEDURES
Airplane Preparation
Vol. 1 04−04−20
REV 68, Apr 16/07
▼
CL−604 Operating Manual
PSP 604−6
1. AIRPLANE PREPARATION (CONT'D)
E. Systems Check (Cont’d)
(2) Rudder pedals ......................................................Adjust to allow full travel when the
knees are straightened.
When nosewheel area is confirmed clear:
(3) Hydraulic pump 3A ...............................................Select to ON.
(4) Nosewheel door ....................................................Close
SIDE CONSOLES
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：龐巴迪挑戰者604操作手冊 Operating Manual 1(74)