USMC DRAWING PACKAGE.pdf

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— PUCT DAsanc CW13fI0 C

GENERAL NOTES

THIS DRAWING TAKES PRECEDENCE IN THE EVENT OF A REQUIREMENT

CONFLICT WITH THE SPECIFICAION.

2. DO NOT APPLY PRIMER OR TOPCOAT IN AREAS DESIGNATED AS BARE METAL

OR NO PAINT AREAS.

APPLY 1. 0’ WIDE STRIPE OF CLEAR ENAMEL CENTERED OVER LEADING EDGE

OF PAINT.

4. LETTERING TO BE PER MILITARY SPECIFICATION MIL—STD—2161(AS).

5. COLORS ARE IDENTIFIED BY THE FOLLOWING NUMBERS AND GOVERNED

BY THE INDICATED SPECIFICATIONS’

COLOR MIL—

NAVY #3 BLACK 37038 MIL—PRF—85285

LIGHT GRAY 16440 MIL—PRF—85285

STRIPE GRAY 36320 MIL—PRF—85285

MECHANIC GRAY 16187 MIL—PRF—85285

UNTINTED WHITE 17925 MIL—PRF—85285

OSHA BLACK 17038 MIL—PRF—85285

INSIGNIA RED 11136 MIL—PRF—85285

PRIMER MIL—PRF—23377

CLEAR MIL—PRF—85285

6. C—9 AIRCRAFT EMPLOY A COPPER BERYLLIUM ALLOY IN THE MAIN LANDING

GEAR DOORS SKIDS. THESE MAY BE SUBJECT TO SANDING IN PREPARATION

FOR PAINTING AND MAY CONSTITUTE A HEALTH RISK IF PROPER

PRECAUTIONS ARE NOT TAKEN. ENSURE PROPER PRECAUTIONS ARE TAKEN,

INCLUDING THE USE OF APPROVED PERSONAL PROTECTIVE EQUIPMENT, WHEN

SANDING THE DOOR SKIDS.

7. AREAS TO BE PAINTED SHALL BE PREPARED AND PAINTED PER APPROPRIATE

MILITARY SPEC DOCUMENTS.

APPLICATION AND REMOVAL OF TEMPORARY CORROSION PROTECTION SHALL

BE ACCOMPLISHED PER MILITARY SPEC DOCUMENTS.

9. SPLINE ALL CURVES APPROXIMATELY AS SHOWN.

0. ALL UNPAINTED AREA OF CLAD SKIN SHALL MEET THE REQUIREMENTS OF

APPROPRIATE DAC/BAC DOCUMENTS.

11. ALL EXPOSED PRIMED SURFACES SHALL RECEIVE COLOR #16440 LIGHT

GRAY, WITH THE EXCEPTION OF THE ANTI—GLARE AREA.

12. ALL DECALS SHALL BE APPLIED PER NA 01—C9B—2—11.

13. DIMENSIONING AND TOLERANCING PER ASME Y14, 5M—A994.

14. ALL DIMENSIONS ARE ALONG CONTOUR, EXCEPT AS NOTED.

15. ALL DIMENSIONS ARE IN INCHES EXCEPT AS NOTED.

16. DO NOT PAINT RUBBER, MYLAR, SILICONE RUBBER

SEALANT, OR RUBBER STRIPS.

17. ANTENNAS’ DO NOT PAINT BLADE OR FLUSH MOUNTED ANTENNAS.

INSPECT FOR COMPLIANCE TO THIS NOTE AFTER COMPLETION OF

AIRCRAFT PAINTING.

18 DO NOT PAINT RADOME.

1 DO NOT PAINT ANTI—CHAFE COATING ON ELEVATOR STABILIZER ROTATION

AREA.

MASK OVER CABIN PRESSURE SAFETY RELEASE VALVES PRIOR TO

PAINTING AIRCRAFT. AFTER PAINTING, ENSURE ALL MASKING

HAS BEEN REMOVED.

1 ALL FUSELAGE DRAIN VALVES ALONG UNDERSIDE MUST BE TEMPORARILY

PLUGGED PRIOR TO PAINTING. PAINT THE EXPOSED SURFACE OF THE

HOUSING UNLESS IT FALLS IN A BARE METAL AREA. INSPECT TO ENSURE

THAT PLUGS ARE REMOVED FROM ALL FUSELAGE DRAIN VALVES AFTER

COMPLETION OF AIRCRAFT PAINTING.

PASSENGER AND FLIGHT DECK WINDOW FRAMES ARE 0. 50’ BARE METAL

(ALL LOCATIONS).

APPLY TEFLON COATING TO LEADING EDGE OF WINGS BEHIND SLATS

AFTER PAINTING.

FORWARD FLAP HINGE COVERS SHALL REMAIN BARE METAL AND COVERED

IN MYLAR.

DISTRIBU11ON STATEMENT C:

DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES ONLY AND THEIR CONTRACTORS TO PROTECT PUBUCA11ONS REQUIRED FOR OFFiCIAL USE OR FOR ADMINISTRATIVE OR OPERATIONAL PURPOSES ONLY, DEIERMINED ON 1 JUNE 2010. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO

COMMANDING OmcER, NAVAL AJR SYSTEMS COMMAND (PMA 207/C—9 IPT). 46990 HINKLE CIRCLE, BUILDING 419, PATUXENT RIVER, MD 20670—1627.

DESTRUCTION NOTICE:

FOR UNCLASSIFiED, UMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT DISCLOSURE

OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.

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A3BREVIATIOMS lAW Y14. 38*4

ThIRD NO.1

PRD.CTI8**

THIS DRAWiNG HAS BEEN GENERATED AND IS MAJNTPJNED

BY A CAD SYSTEM. CHANGES SHALL BE INCORPORATED AS

DIRECTED BY THE DESIGN ACTIVITY.

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