Sharp AF-A18CE Manual do Utilizador Página 7

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NOTE:
UNLESS OTHER WISE INDICATED:
1.
DO NOT SCALE THIS DRAWING FOR DIMENSIONS.
2.
BREAK ALL SHARP EDGES .003-.015 AND REMOVE ALL BURRS AND SLIVERS.
3.
DIMENSIONS ARE IN INCHES AND TOLERANCES AS SHOWN BELOW.
TOLERANCES:
DECIMALS
.XXX +/- .005
.XX +/- .03
.X
+/- .1
ANGLES
+/- 1/2 IN.
4.
BOLT, SCREW, RIVET AND SPACER LENGTHS, AND CLAMP SIZES WITH ( ) OR
(XXX) ARE TO BE DETERMINED ON INSTALLATION. MAINTAIN 2D EDGE
DISTANCE AND 3D SPACING.
5.
MACHINED SURFACES TO BE 63 PER ANSI B46.1-1962.
6.
APPLY TWO COATS OF ZINC CHROMATE PRIMER PER FAA ADVISORY CIRCULAR
AC43.13-1A, CHAPTER 6, PARAGRAPHS 248 AND 250, TO ALL NEW AND
REWORKED METAL SURFACES.
7.
INSTALL ALL FASTENERS IN ACCORDANCE WITH STANDARD PRACTICES OF FAA
ADVISORY CIRCULAR AC43.13-1A, CHAPTER 2, PARAGRAPH 99F OF SECTION
3 AND CHAPTER 5, PARAGRAPHS 227B, 227E, 230A(1), 230A(2) AND 231A
OF SECTION 1.
8.
BOLT, SCREW AND RIVET HOLE SIZES SHALL BE THE NEXT NUMBERED OR
LETTERED DRILL SIZE LARGER THAN THE FASTENER DIAMETER.
9.
DRILLED HOLE TOLERANCES ARE PER AND10387.
10.
DRILL HOLES ON INSTALLATION TO MATCH HOLES IN MATING PARTS.
11.
ALL WIRE TO BE 12 AWG PER MIL-W-22759/16 OR MIL-W-81044/9. WHEN
SHIELDED, IT MUST BE SHIELDED AND JACKETED PER MIL-C-27500. THE
JACKET MATERIAL MUST MEET THE FLAMMABILITY REQUIREMENTS OF THE
WIRE BEING SHIELDED AND JACKETED. ROUTE WIRE WITH EXISITNG WIRE
BUNDLES WHERE POSSIBLE. ALL WIRING FABRICATION MUST BE
ACCOMPLISHED IN ACCORDANCE WITH FAA ADVISORY CIRCULAR AC43.13-1A,
CHAPTER 11, PARAGRAPHS 445 THRU 452 OF SECTION 2, PARAGRAPHS 482 &
483 OF SECTION 5 AND PARAGRAPHS 514 THRU 519 OF SECTION 7. USE
M535489 GROMMETS, MS21104 CLAMPS, AN743-13 BRACKETS, MS35207
SCREWS (#10), AN3 BOLTS, M521042 NUTS, AN960 WASHERS, AND NAS43DD3
SPACERS AS REQUIRED TO SECURE THE WIRING. DO NOT ATTACH CLAMPS NOR
BRACKETS TO "LIFE LIMITED" PARTS. (CONSULT THE DATA SHEET, MAINTEN-
ANCE MANUAL AND FLIGHT MANUAL FOR INFORMATION.) WIRE TERMINALS,
SPLICES AND CAPS MUST MEET THE REQUIREMENTS OF MS25036, MS25181
AND MS25274 RESPECTIVELY.
DATE: 11-15-83
VACUUM SYSTEM INSTALLATION
PAGE: 6 OF 8
AERO SAFE CORPORATION
DRAWN BY
D. SURSELY
DRAWING NUMBER
820501
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