通航信息_通航_通用航空_General Aviation

ABAA
Validity : S / N 1 - 9999 56-TCPage 1
(CA) SEP 04
 
SUBJECT CHAPTER PAGE
REAR TRANSPARENT PANEL 56-20-00 (BA) 1
DESCRIPTION AND OPERATION 1
1. GENERAL 1
2. LOCATION 1 VALIDITY
1 - 9999

REAR TRANSPARENT PANEL 56-20-00 (BA) 401 1 - 9999
REMOVAL / INSTALLATION 401 Post MOD. 151
1. REMOVAL OF THE REAR TRANSPARENT PANEL 401
A. Tools and consumable materials 401
B. Procedure 401
2. INSTALLATION OF THE REAR TRANSPARENT PANEL 401
A. Tools and consumable materials 401
B. Procedure 402
DOOR TRANSPARENT PANEL 56-30-00 (BA) 1 1 - 9999
DESCRIPTION AND OPERATION 1
1. GENERAL 1
2. LOCATION 1
DOOR TRANSPARENT PANEL 56-30-00 (DA) 401 1 - 9999
REMOVAL / INSTALLATION 401 Pre-MOD. 151
1. REMOVAL OF THE DOOR TRANSPARENT PANEL 401
A. Tools and consumable materials 401
B. Procedure 401
2. INSTALLATION OF THE DOOR TRANSPARENT PANEL 401
A. Tools and consumable materials 401
B. Procedure 402
DOOR TRANSPARENT PANEL 56-30-00 (EA) 401 1 - 9999
REMOVAL / INSTALLATION 401 Post-MOD. 151
1. REMOVAL OF THE DOOR TRANSPARENT PANEL 401
A. Tools and consumable materials 401
B. Procedure 401
2. INSTALLATION OF THE DOOR TRANSPARENT PANEL 401
A. Tools and consumable materials 401
B. Procedure 402
ABAA
Validity : S / N 1 - 9999 56 TC (CA) Page 2 SEP 04
 
WINDOWS
DESCRIPTION AND OPERATION
1. GENERAL
The windows are used for pilot and passengers visibility.
Visibility is ensured by an assembly of elements in plexiglas formed to the profile of the fuselage. The main elements are :
- the windshield,
- the rear transparent panels,
- the door transparent panels.
2. LOCATION (Figure 1)
COMPONENT QTY AREA ACCESS DOOR REFERENCE
Windshield 1 210 / 56-10-00
Rear transparent panel 2 210 / 56-20-00
　
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