AIR FORCE MS23009 REV E-1987 ACCELEROMETER-AIRCRAFT INTEGRALLY LIGHTED ABU-4A A AND ABU-4B A《ABU-4A A 和 ABU-4B A型全面亮灯航空器加速计》.pdf

1、MS23009 REV E 66 9999932 0007246 9 E /=-/ -83 I 6610 DIAL AND POINTERS SHOWN FOR VIEW A (OPTIONAL) REFERENCE ONLY FOR DETAILS SEE PROCURENENT SPECIFICATION n 3.688 t.375 -m 3.093 i.375 (CASE LENGTH) SEE VIEW A CENTERED WITHIN i.093 .875 MAX A 2 INCH NOMINAL SIZE CASE IN-/ ACCORDANCE WITH MS33638 EXC

2、EPT AS SHOWN I- I / b+ ,562 i.125 SEE NOTE 6 FOR HS23009-4 REAR VIEW LWTE WITH MS3116-8-3s ELECTRICAL CONNECTOR CENTERLINE LOCATED WITFIIN DASHED LINE AREA 1 L- KEYWAY HATE WITH MS3116-8-3s- OPTIONAL CONNECTOR LOCATION FOR CASE LENGTHS NOT EXCEEDING 3.250 XEC DESIGN AFTER 9 APRIL 1969 USE MS23009-2

3、OB -3 FOR REPUCEMENT DEWTES CWGES t4vY-s INTER- NATIONAL ISAF - 99 INTEREST “* 1 SEE NOTE 5 ROCUREYENT SPECIFICATIOH MIL-A-25949 Mil IT ARY ST AN DARD TITLE ACCELEROMETER-AIRCRAFT INTEGRALLY LIGHTED AAS23009 ABU-4AIA AND dBU-4SIA OF i SVPERSEDES SHEET c b 10 -6 16 ENGIHEERING SPECIFICATIONS AND STAN

4、DARDS DEPARTMENT MX NAVAL AIR ENGINEERIHG CENTFR my LMEHURST. NEW JERSEY 08733 TYPED BY - CHECUD BY - ,1*411 Licensed by Information Handling ServicesProvided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MS23009 REV E 66 m 9999932 00072q7 O m FED. SUP CLAS

5、S 6610 REQUIREMENTS : 1. HTG HDW: THE CONTRACTOR SHALL FURNISH SUFFICIENT WUNTING SCREWS FOR INSTALLATION. HEAD BRASS HACHINE SCREWS. HAVING DURABLE DULL BLACK OXIDIZED OR BLACK NICKEL FINISH. SUFFICIENT FOR HOUNTING ON A PANEL ,188 THICK. THEY SHALL BE .13B-32NC-2 ROUND THE LENGTH SHALL BE 2. WEIGH

6、T:. NOT TO EXCEED 1.5 POUNDS. 3. XPPROCUREHENT SPEC MS23009-3 -ABU-4B/A, COVER GLASS COATED WITH REFLECTION REDUCING COATING, IN ACCORDANCE WITH MIL-C-14806. MS23009-4, COVER GLASS COATED WITH MULTILAYER ANTIREFLECTION COATING HIGH EFFICIENCY AND LIGHTED WITH NIGHT VISION HERMETICALLY SEALED, IHAGIN

7、G SYSTEM (NVIS) COMPATIBLE CLASS B NVIS GREEN A LIGHTING. NOTES : 1. DIMENSIONS ARE IN INCHES. 2. TOLERANCES: DECIHRL 2 .016, UNLESS OTHERWISE SPECIFIED, 3. REFERENCE DOCUMENTS SHALL BE OF THE ISSUE IN EFFECT ON DATE OF INVITATIONS FOR BIDS OR REQUEST FOR PROPOSAL, EXCEPT THAT REFERENCED ADOPTED IND

8、USTRY DOCUMENTS SHALL GIVE THE DATE OF THE ISSUE ADOPTED. 4. FOR DESIGN FEATURE PURPOSES, THIS STANDARD TAKES PRECEDENCE OVER PROCUREMENT DOCUMENTS REFERENCED HEREIN. 5. THE CONTENTS OF THIS STANDARD ARE THE SUBJECT OF INTERNATIONAL STANDARDIZATION AGREEMENTS ASCC 10/4 AND STANAG 3330. WHEN AHENDMEN

9、T, REVISION OR CANCELIATION OF THIS STANDARD IS PROPOSED. THE DEPARTMENTAL CUSTODIAN WILL INFORM RESPECTIVE DEPARTMENTAL STANDARDIZATION OFFICE FOR APPROPRIATE ACTION ON THE INTERNATIONAL AGREEMENTS CONCERNED, 9 6. WHEN CLASS B NVIS GREEN A LIGHTING IS SPECIFIED, IT SHALL BE POWERED BY PINS A ANO B.

10、 PIN C SHALL BE LEFT OPEN. M IL IT KST AN DA R MS 23009 A. AVY-AS INTCR- hn Curl jSAF - 9b ITLE NATIONAL ACCELERWETER-AIRCRAFT, INTEGR4LLY LIGHTED INTEREST SEE NOTE 5. ABU-4AIA AND ABU-4B/A 2 SHEET o KXXIREUENT SPECIFTATION WPERSEDES. MIL-A-25949 ENGINEERIYG SPCCIFICATIONS AND STANDARDS DEPARTMENT D

11、ITE NAVAL AIR ENGINEERING CFNTFR 1 I , , E . . ._ . . . _. ._ _. . . . . . . my LWEnURST, NEW JERSEK 00133 NOTLS TO PIhTLI REDUCE BOIDEI TO 0-17/3li9-3/4. RINT UP? TYIED QY .- - RINT BLlTlOY BOUDER LINEJ/I INCH -01 IOTTOU IDOL Or 8xIY-LO BOIDLI-LINE OWL INCH llW LE17 EDGE 01 1110-1/1 SHLLT. CHEelED DY SNf.11. SIGHATUIL IolU Wl TO BE IKLMLD ON 8i10-1/1 $=ET. -m iii47D ti Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-