NOTES UNLESS OTHERWISE SPECIFIED:
1. MATERIAL PROCESS AND METHODS AS PER AMM AND SRM OR OTHERWISE AS PER THE PERTINENT
SECTION OF FAA AC NO. 43.13-1B (CHANGE 1, CHAPTER 11). REFERENCE ENGINEERING ORDER
2305-AVI-EO-11 FOR INSTALLATION. REFERENCE WIRING DIAGRAM 2305-AVI-311 AND WIRE KIT
2305-AVI-WK-K11 FOR WIRE CONNECTION DETAILS. TERMINATE WIRING IN ACCORDANCE WITH
IPC/WHMA-A-620 CLASS 3. ELECTRICAL BONDING AND SHIELDING REQUIREMENTS IN ACCORDANCE
WITH EMBRAER SWPM-2430.
2. CONSISTENT WITH THE EMBRAER S.A. STANDARD PRACTICE MANUAL, ADVISORY CIRCULARS 25-10,
25-16 AND 43.13-1B THE PHILOSOPHY FOR WIRE ROUTING DESIGN IS AS FOLLOWS (SEE DETAIL):
1. NEW WIRE BUNDLES ARE TO BE ROUTED SEPARATELY FROM EXISTING WIRE
BUNDLES.
2. MINIMUM BEND RADII FOR ALL NEW WIRE BUNDLES MUST NOT BE LESS THAN TEN
TIMES THE OUTSIDE DIAMETER OF THE LARGEST WIRE IN THAT WIRE BUNDLE. A
NEW BEND RADII OF SIX TIMES MAY BE USED AT BUNDLE BREAKOUTS.
3. IN THE EVENT OF SPACE LIMITATIONS, IT IS PERMISSIBLE TO ROUTE NEW WIRING
WITH OTHER CONCURRENTLY INSTALLED WIRING BY WRAPPING NEW WIRING
WITH ITEM 6, ROUNDIT 2000NX 13-5 OR EQUIVALENT TO PROVIDE LAYER OF
SEPARATION. THE SIGNALS IN THE WIRING FROM EACH OF THESE SYSTEMS MUST
BE EVALUATED AND DETERMINED TO BE LOW LEVEL POWER OF LITTLE
ELECTROMAGNETIC INTERFERENCE RISK, AND CONSISTENT WITH THE WIRE
TYPES CONTAINED IN THE WIRING. RESULTANT WIRE BUNDLES ARE TO BE
CLAMPED AND SECURED CONSISTENT WITH THE STANDARDS SET FORTH HEREIN.
4. ALL SERVICE LOOPS SHALL MAINTAIN AT LEAST A MINIMUM BEND RADIUS OF
THREE TIMES THE DIAMETERS OF THE ENTIRE WIRE HARNESS.
5. WIRING SHOULD BE INSTALLED WITH SUFFICIENT SLACK SO THAT BUNDLES AND
INDIVIDUAL WIRES ARE NOT UNDER TENSION. NORMALLY, WIRE BUNDLES SHOULD
NOT EXCEED 1/2" DEFLECTION BETWEEN SUPPORT POINTS. THIS MEASUREMENT
MAY BE EXCEEDED PROVIDED THERE IS NO POSSIBILITY OF THE WIRE BUNDLE
TOUCHING A SURFACE THAT MAY CAUSE ABRASION.
6. IN ADDITION TO THE SEPARATION AND ROUTING REQUIREMENTS CONTAINED
HEREIN, CAREFUL CONSIDERATION MUST ALSO BE MADE TO THE WIRE ROUTING
REQUIREMENTS CONTAINED IN THE EMBRAER WIRING MANUALS.
7. ROUTE HARNESS ASSEMBLY AS SHOWN. IN AREAS WHERE THE NEW WIRING IS
ROUTED WITH OR IN PLACE OF EXISTING WIRING, THERE MAY BE SOME VARIANCE
A/R 20 CM-SCE-TP-1/2-4H-4 HL TIE-ON CABLE MARKER TAGS AMP/TYCO
BETWEEN AIRCRAFT BASED ON SPACE LIMITATIONS. ANY DIFFERENCES TO WIRE
A/R 19 CM-SCE-1/4-4H-4 HL TIE-ON CABLE MARKER TAGS AMP/TYCO
ROUTING SHOWN MUST BE ROUTED IN ACCORDANCE WITH AC43.13-1B.
A/R 18 M23053/5-104-9 WHITE 1/8 INCH HEAT SHRINKABLE TUBING QPL
1 17 2305-AVI-WK-K11 WIRE KIT, EO AVIATEK
A/R 16 P-212 GLASS CLOTH TAPE NITTO
3. ROUTE ELECTRICAL WIRES AND CABLES ABOVE FLUID LINES AND PROVIDE 6" SEPARATION FROM
A/R 15 DP805 SCOTCH WELD ADHESIVE 3M
ANY FLAMMABLE LIQUID, FUEL OR OXYGEN LINE, FUEL TANK WALL, AND ANY OTHER LOW VOLTAGE A/R 14 CB9120V5 CABLE TIE MOUNT CLICK BOND
WIRING THAT ENTERS A FUEL TANK AND REQUIRES ELECTRICAL ISOLATION TO PREVENT AN A/R 13 NAS1149C0332R WASHER, FLAT QPL
IGNITION HAZARD. WRAP WIRING WITH ITEM 6, ROUNDIT 2000NX 13-5 OR EQUIVALENT TO PROTECT A/R 12 NAS43DD3-40N SPACER, SLEEVE-SCREW AND BOLT QPL
HARNESS AND PROVIDE LAYER OF SEPARATION IN THESE AREAS. A/R 11 MS21044N3 NUT QPL
A/R 10 MS35207-271 SCREW, MACHINE, PAN, #10-32, 2" QPL
MS21919WDG(X) QPL
4 USE STANDOFFS, ITEM 1, FOR SEPARATION FROM EXISTING WIRE BUNDLES (SEE WIRE ROUTING 10 11 A/R
A/R
9
8 608036-1
ADEL CLAMPS
FIRE RETARDANT TAPE QPL
DETAIL). A/R 7 RT-1162 HELICAL CONOLEX TE
11 12 A/R 6 ROUNDIT 2000 NX X-X EXPANDABLE SLEEVING BENTLY HARRIS
5 TECHNICIAN TO USE STRING TIE AS REQUIRED (SEE WIRE ROUTING DETAIL). A/R 5 TYPE HP (MIL-Y-1140) VARGLAS SLEEVING VARGLAS CORP.
A/R 4 MS3367-4-9 CABLE TIES QPL
A/R 3 MS3367-2-9 CABLE TIES QPL
6 WRAP CABLES WITH ITEM 16, P-212 SILICONE GLASS CLOTH TAPE OR EQUIVALENT AT EACH
A/R 2 MIL-T-43435B WAXED STRING QPL
TIEDOWN POINT. MINIMUM WRAP: 2 LAYERS WRAP MUST EXTEND A MINIMUM OF .25" FROM CABLE
A/R 1 CR4H-M STANDOFFS PANDUIT
TIE EDGE. QTY MANUFACTURER/
ITEM PART NUMBER DESCRIPTION
-01 SPECIFICATION
7 PART NUMBER DEFINITION IS SHOWN BELOW: PARTS LIST
MS3367-4-9
PROJECT:
COLOR DASH NUMBER
SIZE DASH NUMBER INSTALLATION ELECTRO OPTICAL
BASIC PART NUMBER
SYSTEM ON AIRCRAFT EMB-145
8 TORQUE FASTENERS TO 40±5 IN LBS.
ACCEPTABLE TO CHANGE CLAMP SIZE, STANDOFF AND SCREW LENGTH AS
TITLE: WIRE ROUTING ELECTRO OPTICAL
9
NECESSARY TO MEET ROUTING REQUIREMENTS. 18" MAXIMUM SPACING BETWEEN
CLAMP POINTS.
SCALE ORIG DATE DWG. No.
NTS A4 03/29/2024 2305-AVI-211
CODE CAGE: - SHT: 1 OF 9 REV: 2
La información contenida en este documento hace parte de los derechos de propiedad intelectual de AVIATEK. Esta información no puede ser reproducida o divulgada a terceros, ya sea en parte o en su
totalidad sin autorización de AVIATEK.
