_____________________
6.
List of Manufacturers -------------------------------------------| MANUFACTURER | P/N | -------------------------------------------
| CONRAC WMM | 502 |
| KINGSLEY | KVE-7BL |
| KINGSLEY | KVE-751 |
| KINGSLEY AUTOWIRE | 10 |
| TAB | 67501 |
| AUTO TAB | 77610-02 |
-------------------------------------------
20-25-62 Page 5
______________________________________________________________
STANDARD RULES AND RECOMMENDATIONS - DESCRIPTION AND OPERATION
_______
1.
General The chapters that follow give the general design description and requirements related to the electrical installations on aircraft.
_________________________
2.
Structure of the Chapters
A. Specific areas (Ref. 20-31-XX)
B. Identification and Marking (Ref. 20-32-XX) R C. Wire harness (Ref. 20-33-XX)
20-30-00 Page 1
__________________________________________
SPECIFIC AREAS - DESCRIPTION AND OPERATION
________
1.
General: The chapters that follow give the general design description and requirements related to the specific areas.
__________________________
2.
Structure of the chapters:
A. Specific areas location (Ref. 20-31-30).
20-31-00 Page 1
___________________________________________________
SPECIFIC AREAS LOCATION - DESCRIPTION AND OPERATION
_______
1.
General This chapter gives the location of the specific areas on the aircraft.
________________________
2.
Structure of the chapter
A. Pressurized Areas (Ref. 20-31-31)
B. Skydrol Areas (Ref. 20-31-32)
C. Vibration Areas (Ref. 20-31-33)
D. Hot Areas (Ref. 20-31-34)
E. SWAMP Areas (Ref. 20-31-35)
F. Fuel Areas and Fuel Vapor Areas (Ref. 20-31-36)
G. Fire Areas (Ref. 20-31-37)
20-31-30 Page 1
_____________________________________________
PRESSURIZED AREAS - DESCRIPTION AND OPERATION
_______
1. General
This chapter gives the location of the pressurized areas on the aircraft.
________________________________________
2. A300 - A310 - A300/600 Pressurized Areas (Ref. Fig. 001)
---------------------------------------------------------------------| AREAS | DESIGNATION | |---------|---------------------------------------------------------| | 121 | Avionics Compartment | | 122 | | |---------|---------------------------------------------------------| | 131 | FWD Cargo Compartment | | 132 | | |---------|---------------------------------------------------------| | 133 | FWD Bay Under FWD Cargo Compartment Floor | | 134 | | |---------|---------------------------------------------------------| | 135 | AFT Bay Under FWD Cargo Compartment Floor | | 136 | | |---------|---------------------------------------------------------| | 137 | Bay between AFT Bulkhead of FWD Cargo Compartment | | 138 | and FWD Pressure Bulkhead of Wing Center Box | |---------|---------------------------------------------------------| | 145 | Pressurized Zone Between Wing Center Box/Main Landing | | 146 | Gear Well and Cabin Floor | |---------|---------------------------------------------------------| | 151 | AFT Cargo Compartment | | 152 | | |---------|---------------------------------------------------------| | 153 | Bay Under AFT Cargo Compartment Floor | | 154 | | |---------|---------------------------------------------------------| | 161 | Bulk Cargo Compartment | | 162 | | |---------|---------------------------------------------------------| | 163 | Bay Under Bulk Cargo Compartment Floor | | 164 | | |---------|---------------------------------------------------------| | 171 | AFT Cabin Underfloor Compartment | | 172 | | |---------|---------------------------------------------------------| | 200 | Upper Half of Fuselage | ---------------------------------------------------------------------
20-31-31 Page 1
Specific Areas - Pressurized Areas
For A300 - A310 - A300/600
Figure 001
20-31-31 Page 2
____________________________________
---------------------------------------------------------------------| AREAS | DESIGNATION | |---------|---------------------------------------------------------| | 121 | FWD Avionics Compartment | | 122 | | |---------|---------------------------------------------------------| | 125 | Lateral Avionics Compartment | | 126 | | |---------|---------------------------------------------------------| | 127 | AFT Avionics Compartment | | 128 | | |---------|---------------------------------------------------------| | 129 | Stair Bay | |---------|---------------------------------------------------------| | 131 | FWD Cargo Compartment | | 132 | | |---------|---------------------------------------------------------| | 133 | Bay Under Forward Cargo Compartment Floor | | 134 | | |---------|---------------------------------------------------------| | 137 | Bay between AFT Bulkhead of Forward Cargo Compartment | | 138 | and Forward Pressure Bulkhead of Wing Center Box | |---------|---------------------------------------------------------| | 145 | Pressurized Zone Between Wing Center Box/Main Landing | | 146 | Gear Well and Cabin Floor | |---------|---------------------------------------------------------| | 151 | AFT Cargo Compartment | | 152 | | |---------|---------------------------------------------------------| | 153 | Bay Undes AFT Cargo Compartment Floor | | 154 | | |---------|---------------------------------------------------------| | 161 | AFT Cargo Compartment | | 162 | | |---------|---------------------------------------------------------| | 163 | Bay Under AFT Cargo Compartment Floor | | 164 | | |---------|---------------------------------------------------------| | 171 | AFT Cabin Underfloor Compartment | | 172 | | |---------|---------------------------------------------------------| | 200 | Upper Half of Fuselage | ---------------------------------------------------------------------
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320 ESPM Electrical Standard Practices Manual 2(17)
