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时间:2011-10-13 19:42来源:蓝天飞行翻译 作者:航空
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Fuel system
Landing gear hydraulic system
Pitot and static systems
Brake system
Autopilot servo-actuator and aileron linkage (if installed)
219 Baggage compartment door Baggage compartment (from outside)
 
 
217R
 
Intrados voilure gauche
L.H. wing lower surface
14063000AAA BW Z4000 
 Intrados voilure droite
R.H. wing lower surface

Inspection doors - Area 210
Figure 2
 
ADAA
Validity : S / N 1 - 9999 Pre-MOD. 151
 
06-30 00Page 9
(EA) JUN 02
 
With battery at the front (Figure 2A)
Identification
No. DESCRIPTION AREA LOCATION
AND ACCESSIBLE ELEMENTS
211L L.H. inspection door (if installed) L.H. FWD table
L.H. instrument panel FWD section Console upper section
Vacuum system (if installed)
211 R R.H. inspection door (if installed) R.H. FWD table
R.H. instrument panel FWD section Console upper section
Battery
Voltage regulator
Radio console ventilator (if installed)
212L Inspection door on firewall Exterior light indicator printed circuit board Diode and fuse printed circuit board
Alternator output indicator printed circuit board
213L Inspection door (if installed) Vapor cycle cooling system connections (if installed)
213R Inspection door Vapor cycle cooling system connections (if installed)
Fuel system connection
Fuel flowmeter transmitter (if installed) Emergency vacuum system (if installed)
214 Inspection door Electric boost pump
Emergency vacuum system (if installed)
215 Inspection door Fuel selector / filter unit
216C Inspection door (if installed) Deicing fluid tank strainer and gage (if installed)
216L Inspection door (if installed) Ground power receptacle (if installed)
217L L.H. junction fairing L.H. wing FWD attachment to fuselage
217R R.H. junction fairing R.H. wing FWD attachment to fuselage
218A Aft cowling under hull Wing / fuselage central attachments Wing / fuselage aft attachments Landing gear hydraulic system Flaps relay and actuator
Lower section of cabin floor-panels
218F FWD cowling under hull Wing / fuselage central attachments
Lower section of cabin floor-panels
Fuel system
Landing gear hydraulic system
Pitot and static systems
Brake system
Autopilot servo-actuator and aileron linkage (if installed)
Emergency electromechanical vacuum pump (if installed)
219 Baggage compartment door Baggage compartment (from outside)

ADAA
Validity : S/ N 1 - 9999 Pre-MOD. 151 0V-30-00 (EA) Page 10
JUN 02
 
 
217R
 

 
Intrados voilure gauche
 
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