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- Area 130 : Lower section of power plant
B. Area 200
This area is composed of the fuselage section located behind the firewall, including the tail cone.
It is subdivided into five secondary areas :
- Area 210 : FWD fuselage - external area between the firewall and frame C6
- Area 220 : Rear fuselage - from frame C6, including tail cone
- Area 230 : Cockpit - internal area between the firewall and the back of the rear seat except for control station
- Area 240 : Upper duct and baggage compartment - internal upper duct area and internal area between the back of rear seat and the AFT baggage compartment bulkhead (frame C6)
- Area 250 : Control station - internal area comprising instrument panel and upper surface of pedestal
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C. Area 300
This area is composed of the horizontal and vertical stabilizers.
It is subdivided into three secondary areas :
- Area 310 : Fixed vertical stabilizer
- Area 320 : Rudder
- Area 330 : Stabilator
D. Area 500
This area is composed of the L.H. wing.
It is subdivided into three secondary areas :
- Area 510 : Wing lower surface
- Area 520 : Wing upper surface
- Area 530 : Wing interior
E. Area 600
Similar to area 500, this area is composed of the R.H. wing.
It is subdivided into two secondary areas :
- Area 610 : Wing lower surface
- Area 620 : Wing upper surface
F. Area 700
This area consists of the landing gear assembly. It is subdivided into three secondary areas :
- Area 710 : Nose landing gear
- Area 730 : L.H. main landing gear
- Area 740 : R.H. main landing gear
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Z740
 
 
 

 
Z500
 
Z330
 
Z510
 

 
Location of areas
Figure 1
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Location of fuselage frames
Figure 2
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EMPLANTURE
WING ROOT
 

 
Location of wing ribs
Figure 3
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INSPECTION DOORS
DESCRIPTION AND OPERATION
1. GENERAL
The inspection or service doors generally include all openings which facilitate maintenance practices or which allow access to certain components.
　
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