Page 1 Page 2 Page 3 Page 4 b) f) g) i) 2. 2, 2. a) b) C) 検査の結果
Contents
1. 4 5 5 5 6 2 2 4 2 7 3 5 6 2 2 2 10 a 5 0 9 12. 1 2
3. 2 2
4. 6 MS33588 MS20995 MS33540 10 1T 0 0 0 3 MS24665 1 NA 01 14 503 2
5. 1 12 C b e 5 6 2 2
6. c 5 6 2 2 1 0 1 2 1 9 NA 01 1A 17 7 2 7 2 1 7 2 2 a 1 0 1T 0002 1 0 1 0 0 0 8 15 b 2 a b 6 d f 16 3
7. 22
8. 4 6 0 M2S V 30021 1 1 MHP V 62010
9. oo OO AR Ww mm 20 SS ED SR A A 20 20 20 21 21 OS 21 21 22 19 20 1 1 1 1 2
10. 10 1 0005
11. i Tubing 1 NWN 1 3 1 4 1 5 1 0 1 0 0 0 3 NA 01 14 20 MIL STD 1247 NA 01 14 20 2 2 NA01 1A 17 3 k MTL W 5088 NA 01 1A 505 1
12. 1 3 a b ELECTRONTCS INSTALLATION INSTRUCTIONS c ELECTRONICS BENCH PRE FLIGHT FLIGHT TEST TNSTRUCTION 1 4 MHS J 30701 2 2 1 a 5 2 2 2 2 1 a 2 1 b 9
13. b 6 9 f g h i 2 3 2 4 2 5 a b o d 1 0
14. 2 2 2 a b 2 3 21 a CE C 5 6 2 2 b 2 3 a 1 2
15. R R C R T E C E C E C E 4 5 6 2 2 TE CE EO OE
16. 0 0 NY NN oo WM RR EE 10 1 5 6 2 2 2 2 a b e 2 1 1 3 3 1 5 6 2 2 1 0 1T 0 0 0 4 3 2
17. 1 2 DSP Z 9000 2 2 4 4 MHP V 51028 5 5 1 a 5 6 2 2 b 5 6 2 2 c x 1
18. 2 3 4 5 6 1 4 1 Fa SSD RN gt ee SS ooonnene see SS ar Ps 2 1 2 WT ON yy Sernen
19. 1 0 2T 6 4 7 3 3 5 0 9 4 5 5 1 5 2 8 b 9 6 a b e 9 e 6 2 7 1 Ths a 1 2 11
20. m 5 1 5 6 2 2 2 6 5 7 1 4 a 1 1 0 1 O 0 0 1 2 3 b 1 MIL S 5002 2
21. b 1 2 3 VSWR VOLTAGE STANDING WAVE RATIO e 1 2 2 4 2 4 1 a b 2 4 2 25 2 2 22 2 3 2 4 ELECTRONICS 1NSTALLATTON INSTRUCTION 2 6 e 8 b 6 9 2
22. 3 4 10 1T 000 2 1 0 1T0O0 3 1 2 14 h NM 01 1A 12
23. 5 6 2 2 TCR CR TR TCR x a b c d 17
24. MS33588 1 0 1T 0003 1 1 2 3 1 4 b d e f g 13 5 6 73
25. UR 7 1 2 a 1 2 b c MS33749 MS35333 MS35790 7 1 8 a
26. MHP V 51028 MHP V 62010 MHS J 30701 _ M2S Y 30021 4 4 50 9 27 1 1 9 37 12 24 7 3 42 12 12 5 6 2 2 10 12 8 5 0 9 13 3 30 1 4 8 14 3 29 4 5 5 13 1 6 4 6 0 13 1 6 1 0 17T O 0 0 1 57 11 9 1 0 1T 0002 57 11 9 1 0
27. 2 2 2 2 5 8 b 2 6 a b o 2 7 2 8 8 b 2 9 2 5 0 9 MHP V 62010
28. 1 0 1T 000 5 MIL C 81907 Scuff sand MTL C 81907 MIL F 7179 MIL C 18263 1 1 9 MTL C 8779 MIL F 7179 3 7 1 5 a 1 0 1 0003 b
29. 1 1 1 1 2 a b 1 3 8 b 1 4 MHS V 46008 17 PAR 1 4 a 1 MIL STD 1247 MARKINGS FUNCTIONS AND HAZARD DESIGNATOIN OF HOSE PIPE AND TUBE LINES FOR AIRCRAFT MISSILE AND SPACE MIL C 8779 MIL C 18263 MIL C 81907 MIL F 7179 MIL S 5002 COLOR INTERIOR AIRCRAFT REQUTREMENTS FOR COLORS EXTERTOR NAVAL ATRCRAFT REQIREMENTS FOR COATING SYSTEM POLYURETHANE ALTPHATIC WEATHER RESISTANT PROCESS FOR APPLICATION OF FINISHES COATING AND SEALANTS FOR THE PROTECTION OF AEROSPACE WEAPONS SYSTEMS SURFACE TREATMENTS AND INORGANIC COATINGS FOR METAL SURFACES OF WEAPONS OF WEAPONS SYSTEMS b c MTL W 5088 WTRTNG AEROSPACE VEHICLE DSP 2 9000
30. S a b 4 4 1 4 2 4 3 4 4 1 6 1 EE 15 1 i 5 1 KK 3 0 0 EL 5 1 5 D 1 5 6 2 2
31. 1T 0 0 0 8 59 5 21 1 0 17 2 1 9 50 8 20 1 0 17 0 0 05 10 3 31 1 0 2 6 4 7 10 9 30 1 0 1T 0O O 4 9 3 21 NA 01 1A 12 ATRCRAFT REPATR FABRICATTON MAINT AND REPATR OF TRANSPARENT HANDBOOK NA 01 1A 17 AVIATION HYDRAULICS MANUAL NA 01 14 20 AVIATION HOSE amp TUBE MANUAL ORGAN INTER amp DEPOT MAINT VARIOUS AIRCRAFT NA 01 1A 503 MAINT OF AERONAUTICAL ANTTFRICTION BEARTNGS NA 01 1A 505 ATRCRAFT ELECTRIC amp ELECTRONIC WIRTNG 1NSTALLATION PRACTICES b 1 5 a b e d 1 a b 2 2 MHP V 51030 MHP V 56016 3 1 10 12 2 8 9 10 12 8 9 1 10 12 8 9 2 10 12 8 9 3 10 12 8 PAR PROGRESSIVE AIRCRAFT REWORK
32. RE EE i 3 1 2 1 D lt 2 0 Ww 6 WW MW MRM NM OI Cn 1 2
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