FSC 5342 Weapon System - Hardware: 5342-01-061-0694, 5342-01-061-1043, 5342-01-062-3040

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NSNMFG SKUItem NameDetailsManufacturer (CAGE)RFQ
5342-01-061-0694
5342010610694
951B065-1PLUGSundstrand Corp. (83843)
Hamilton Sundstrand Corporation (99167)

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5342-01-061-1043
5342010611043
160D960130-29Clip, SupportGeneral Characteristics Item Description: Cressh 301 1/2 hard, for engine drain line support
III End Item Identification: Aircraft model A-10A
Northrop Grumman Systems Corporation (26512)

Quote

5342-01-061-1044
5342010611044
160D960130-27Clip, SupportGeneral Characteristics Item Description: Cressh 301 1/2 hard, for engine drain line support
III End Item Identification: Aircraft model A-10A
Northrop Grumman Systems Corporation (26512)

Quote

5342-01-061-1045
5342010611045
160D960342-21Clip, SupportGeneral Characteristics Item Description: Cressh MIL-S-721, comp T or cb-ta
III End Item Identification: Aircraft model A-10A
Northrop Grumman Systems Corporation (26512)

Quote

5342-01-061-1641
5342010611641
281393 ITEM 18
169223
283854-0001 ITEM 25
CLIPGeneral Characteristics Item Description: Cres, astm A582
Marotta Controls Inc. (99657)

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5342-01-061-2165
5342010612165
ZP9183Bracket, Panel SupportGeneral Characteristics Item Description: Aluminum alloy 6063-T5, 2.000 in.lg
Zero Manufacturing Inc. (98376)

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5342-01-061-2610
5342010612610
407846SpringIII End Item Identification: Racine relief valve part no FEI-PBAK-TO6S used on magna 2 plate monocolor intaglio press serial no lg 11 (69)0545
Bosch Automation Technology (77521)

Quote

5342-01-061-3489
5342010613489
2L3994Bracket, SpecialGeneral Characteristics Item Description: Steel, corrosion resisting, comp 431; passivate; hardness rockwell C 39.0 to 48.0; arc shaped W/right angle cross section; first leg 0.415 in. lg by 0.060 in. w; second leg 0.468 in. lg by 0.090 in. min 0.095 in. max w; exterior arc surf. 2.375 in. r; interior arc surf. 1.960 in. r; exterior arc surf. 63.0 microinches both sides; arc ends 0.534 in. short of the diameter centerline and parallel W/the centerline; four 0.128 in. dia holes on 4.250 in. dia bolt circle W/100.0 deg by 0.230 in. dia countersink; holes spaced 11.5 deg about center and 71.5 deg about center
Dover Diversified DE Inc. (78062)
Rockwell Collins Electromechanical (86831)

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5342-01-061-4788
5342010614788
51716Clip, Throttle ShaftMcCulloch Corp. (81580)

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5342-01-061-6552
5342010616552
135656-0001Cap, Handle EndGeneral Characteristics Item Description: Aluminum alloy QQ-A-250/11, 6061-T6, finish per MIL-C-5541 class 1A, all surfaces 125 microinch, 0.885 in. lg W, 0.885 in. W, 0.250 in. thk, aperature 0.750 in. dia, outside corners 0.125 in. R, 2 holes drilled through to aperature 0.100 in. dia
BAE Systems Information and (19397)

Quote

5342-01-061-7086
5342010617086
23217-3
C9546-3
C9546-2
23217-3/04
23217-2
Mount, Resilient, Weapon SystemMaterial: Steel corrosion resisting core aluminum alloy or steel housing
(Non-Core Data) Resilient Member Material: Rubber, synthetic
Flange Length: 1.810 inches nominal
Lockheed Martin Corporation (81755)
Barry Wright Corporation (81860)

Quote

5342-01-061-8235
5342010618235
FC-3520-27Cap, Filler OpeningIII Fsc Application Data: Hydraulic reservoir, aircraft
System for Which Designed: Nonpressurized
Gripping Accommodation Type: Wing grip
Parker-Hannifin Corporation (99321)

Quote

5342-01-061-8316
5342010618316
629-3923-001Mounting kit, PreamplifierGeneral Characteristics Item Description: Mount, resilient 4; lead; electrical 4; screw 4; washer, flat 8; washer, lock 4
Rockwell Collins Inc. (13499)

Quote

5342-01-061-8319
5342010618319
461335-01Plate, RestrainerGeneral Characteristics Item Description: Aluminum alloy, QQ-A-250/11, 6061 T6; 1.95 in. lg; 0.38 in. w; 0.063 in. thk; 2 holes 0.130 in. dia located 0.600 in. from each end and 0.190 in. from side; pressure sensitive strip 0.420 in. lg and 0.380 in. W on each end
III End Item Identification: Aircraft F16
BAE Systems Controls Inc. (07690)

Quote

5342-01-061-8485
5342010618485
933207-A01Clamp, Shoulder ThreadedGeneral Characteristics Item Description: Aluminum QQ-A-250, 0.600 in. overall length, 0.280 overall width, finish hard anodize per MIL-A-3625 type 3, class 1; insert 6-32
Titan Corp., The (16224)
L-3 Services Inc. (63702)

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5342-01-061-9028
5342010619028
4N6910BraceGeneral Characteristics Item Description: Steel alloy
Caterpillar Inc. (11083)

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5342-01-062-1631
5342010621631
623-9912-001Cover AssemblyGeneral Characteristics Item Description: Aluminum alloy QQ-A-250/8 alloy 5052 temper H34, painted, black epoxy, 14.455 in. length, 7.590 in. width, 2.237 in. thk, retaining ring and turnlock stud included
Rockwell Collins Inc. (13499)

Quote

5342-01-062-1666
5342010621666
53-130-2
53-130
53-130-1
Clip, RotorGeneral Characteristics Item Description: 1.000 O/a lg, 0.180 in. W
III End Item Identification: F-14A aircraft
Goodrich Corporation (97153)

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5342-01-062-2229
5342010622229
C-14028 PT6
14028F131
F-19000 PIECE 16-8
RetainerGeneral Characteristics Item Description: Material steel
Teikoku USA Inc. (99827)

Quote

5342-01-062-3040
5342010623040
32-42000-28CLIPGeneral Characteristics Item Description: Aluminum alloy QQ-A-287 T6; 6.210 in. lg; 3.250 in. w; 0.040 in. H
Boeing Company, The (76301)

Quote

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