ASAP Part Services, owned and operated by ASAP Semiconductor, has over 6 billion parts inventoried. This includes new, old, used, and obsolete parts, such as 11508656, 12276, 123-0934, 123-1467, 123-1467-01. As an ISO 9001:2015 certified and FAA AC 00-56B accredited company, we go to great lengths to ensure we are delivering quality parts. We partner exclusively with reliable manufacturers such as Abston Machine Shop Inc, Aerosonic Corporation, Aerocontrolex Group Inc, Allied Signal Inc, Aljers Llc. Our team provides superior quality assurance testing for and more. So if you are in need of Weight Counterbalance or any other NSN parts, submit an Instant RFQ and receive a quote in as little as 15 minutes.
Part No Part No
|
NSN NSN Parts
|
Details Item Name
|
QTY QTY
|
RFQ RFQ
|
---|---|---|---|---|
11508656 | 3040-01-016-5708 | Special Features: Moment Arm, Weight Simulator Assy 1, Pin, Straight, Dowel 3 | Avl | RFQ |
12276 | 3040-01-319-6905 | NA | Avl | RFQ |
123-0934 | 3040-01-668-2614 | NA | Avl | RFQ |
123-1467 | 3040-01-389-0544 | NA | Avl | RFQ |
123-1467-01 | 3040-01-389-0506 | NA | Avl | RFQ |
1282T100-20 | 3040-01-518-1110 | End Item Identification: L1011 Tristar Aircraft Part Name Assigned By Controlling Agency: Counter Balance Door Actuator | Avl | RFQ |
1548390-6 | 3040-00-509-1052 | Special Features: Material Tungsten Wire, Non/Magnetic Binder, Dia. 0.093 In., Length 0.547 In. End Item Identification: Rotor Generator P/N 28B26-3-1A | Avl | RFQ |
204670 | 3040-01-319-6906 | NA | Avl | RFQ |
204770 | 3040-01-339-1602 | Special Features: 0.246 In. Min, 0.254 In. Max Od;0.245 In. Min, 0.255 In. Max O/A Lg;0.120 In. Min, 0.130 In. Max Dia From Centerline To End;0.070 In. Dia Thru Tap No. 2-64 Unf-2B Thd | Avl | RFQ |
204770 | 3040-01-343-8523 | Special Features: 0.246 In. Min, 0.254 In. Max Od;0.245 In. Min, 0.255 In. Max O/A Lg;0.120 In. Min, 0.130 In. Max Dia From Centerline To End;0.070 In. Dia Thru Tap No. 2-64 Unf-2B Thd | Avl | RFQ |
204770-1 | 3040-01-339-1602 | Special Features: 0.246 In. Min, 0.254 In. Max Od;0.245 In. Min, 0.255 In. Max O/A Lg;0.120 In. Min, 0.130 In. Max Dia From Centerline To End;0.070 In. Dia Thru Tap No. 2-64 Unf-2B Thd | Avl | RFQ |
204770-2 | 3040-01-343-8523 | Special Features: Brass, Qq-B-626; 0.185 In. Lg; 0.185 In. Dia; 0.070 In. Bore Dia - 64 Unf - 2B | Avl | RFQ |
2650-3220-56 | 3040-01-407-0817 | Special Features: Fan Vanaxial | Avl | RFQ |
2650-3489-1 | 3040-01-407-0817 | Special Features: Fan Vanaxial | Avl | RFQ |
265348901 | 3040-01-407-0817 | Special Features: Fan Vanaxial | Avl | RFQ |
26535301 | 3040-01-381-0197 | NA | Avl | RFQ |
265353801 | 3040-01-381-0197 | NA | Avl | RFQ |
265353901 | 3040-01-381-0325 | NA | Avl | RFQ |
2670-3271-1.23 | 3040-01-407-0817 | Special Features: Fan Vanaxial | Avl | RFQ |
3022T01P02 | 3040-00-060-1354 | Special Features: 0.110 In.Thk Material: Steel Outside Diameter: 0.550 Inches Nominal | Avl | RFQ |
3323846-1 | 3040-01-007-2013 | Special Features: Sintered Tungsten Alloy, Per Mil-T-21014, Type Ii, Class 3; 1.350 In. Lg; 1.000 In. W; 0.060 In. To 0.065 In. Thick; Two Mounting Holes End Item Identification: Guided Missile Remote Control System | Avl | RFQ |
350A31-1861-20 | 3040-14-366-5639 | NA | Avl | RFQ |
355792-3 | 3040-01-414-4067 | Special Features: Uweight To Be .75 + .02/-.01 Lbs; O/A Height, 2.050 In. Nom; O/A Width, 0.200 In. Min 0.230 In. Max; Material, Lead Casting, Qq-L-171 Grade B; Hole Thru .60 In. From Each End .278 In. Dia; Hole Permitted At Center For Weight Control Overall Length: 4.650 Inches Nominal End Item Identification: Aircraft, Lockheed Aeronautical Corp, Model Hercules C-130 | Avl | RFQ |
355794 | 3040-01-414-4067 | Special Features: Uweight To Be .75 + .02/-.01 Lbs; O/A Height, 2.050 In. Nom; O/A Width, 0.200 In. Min 0.230 In. Max; Material, Lead Casting, Qq-L-171 Grade B; Hole Thru .60 In. From Each End .278 In. Dia; Hole Permitted At Center For Weight Control Overall Length: 4.650 Inches Nominal End Item Identification: Aircraft, Lockheed Aeronautical Corp, Model Hercules C-130 | Avl | RFQ |
355794-3 | 3040-01-414-4067 | Special Features: Uweight To Be .75 + .02/-.01 Lbs; O/A Height, 2.050 In. Nom; O/A Width, 0.200 In. Min 0.230 In. Max; Material, Lead Casting, Qq-L-171 Grade B; Hole Thru .60 In. From Each End .278 In. Dia; Hole Permitted At Center For Weight Control Overall Length: 4.650 Inches Nominal End Item Identification: Aircraft, Lockheed Aeronautical Corp, Model Hercules C-130 | Avl | RFQ |
35673 | 3040-01-375-8109 | Special Features: Brass; 1.125 In. Outside Dia; 0.399 In. Inside Dia; 0.188 In. W End Item Identification: 1730-01-266-4338 | Avl | RFQ |
35673-1 | 3040-01-375-8109 | Special Features: Brass; 1.125 In. Outside Dia; 0.399 In. Inside Dia; 0.188 In. W End Item Identification: 1730-01-266-4338 | Avl | RFQ |
357191-25 | 3040-00-774-9294 | NA | Avl | RFQ |
365A31-1889-01 | 3040-14-374-7285 | NA | Avl | RFQ |
365A31-2143-21 | 3040-14-387-9467 | NA | Avl | RFQ |
365A33-2124-35 | 3040-14-485-2097 | NA | Avl | RFQ |
365A33-2124-36 | 3040-14-485-2098 | NA | Avl | RFQ |
4014692CL4 | 3040-00-337-4214 | NA | Avl | RFQ |
40JA | 3040-01-250-2763 | Special Features: Cast Iron;24.000 In. Lg., 12.000 In. W, 8.500 Thk.;Painted Finish End Item Identification: Engine Model T700-Ge-401 | Avl | RFQ |
473718CL1 | 3040-00-966-5049 | NA | Avl | RFQ |
48864 | 3040-01-522-1762 | Special Features: Capscrew: 3/8 Nc X 4.50 Ss: Nut, Esna, 3/8 Nc Ss: Ear, 0.25Pl X 0.75 X 0.88 Overall Length: 4.000 Inches Nominal Outside Diameter: 5.000 Inches Nominal | Avl | RFQ |
500-1270 | 3040-00-719-5112 | NA | Avl | RFQ |
584943CL4 | 3040-01-216-0628 | NA | Avl | RFQ |
657800CL1 | 3040-01-322-9011 | NA | Avl | RFQ |
657800CL3 | 3040-01-323-6470 | NA | Avl | RFQ |
657800CL6 | 3040-01-323-2183 | NA | Avl | RFQ |
6786483 | 3040-00-652-6999 | End Item Identification: Acft Eng T56 | Avl | RFQ |
6793888 | 3040-00-877-0063 | End Item Identification: Acft Eng T56 | Avl | RFQ |
6819889 | 3040-00-924-7704 | NA | Avl | RFQ |
6844615 | 3040-00-015-2188 | End Item Identification: Balance Plate, Turbine Rotor, T-56 Engine Aircraft | Avl | RFQ |
6844615D | 3040-00-015-2188 | End Item Identification: Balance Plate, Turbine Rotor, T-56 Engine Aircraft | Avl | RFQ |
6860677-01 | 3040-00-858-0707 | End Item Identification: Acft Eng Tf41 | Avl | RFQ |
6860677-04 | 3040-00-858-0710 | End Item Identification: Acft Eng Tf41 | Avl | RFQ |
6860677-05 | 3040-00-858-0712 | End Item Identification: Acft Eng Tf41 | Avl | RFQ |
6860677-06 | 3040-00-858-0713 | End Item Identification: Acft Eng Tf41 | Avl | RFQ |
6860677-07 | 3040-00-858-0714 | End Item Identification: Acft Eng Tf41 | Avl | RFQ |
6863385 | 3040-00-871-6070 | End Item Identification: Acft Eng Tf41 | Avl | RFQ |
6863433 | 3040-00-872-0725 | NA | Avl | RFQ |
6863434 | 3040-00-872-0728 | NA | Avl | RFQ |
6863435 | 3040-00-872-0733 | NA | Avl | RFQ |
6863436 | 3040-00-872-0748 | End Item Identification: Acft Eng Tf41 | Avl | RFQ |
6863437 | 3040-00-872-0768 | NA | Avl | RFQ |
6863438 | 3040-00-872-0771 | End Item Identification: Acft Eng Tf41 | Avl | RFQ |
6868465-1 | 2840-00-150-7302 | End Item Identification: Acft Eng Tf41 | Avl | RFQ |
6868465-2 | 2840-00-150-7303 | End Item Identification: Acft Eng Tf41 | Avl | RFQ |
6868465-3 | 2840-00-150-7304 | End Item Identification: Acft Eng Tf41 | Avl | RFQ |
6868465-4 | 2840-00-150-7305 | End Item Identification: Acft Eng Tf41 | Avl | RFQ |
6868465-5 | 3040-00-150-7306 | End Item Identification: Acft Eng Tf41 | Avl | RFQ |
6868465-6 | 3040-00-150-7307 | End Item Identification: Acft Eng Tf41 | Avl | RFQ |
6868465-7 | 3040-00-150-7308 | End Item Identification: Acft Eng Tf41 | Avl | RFQ |
6868465-8 | 3040-00-150-7309 | End Item Identification: Acft Eng Tf41 | Avl | RFQ |
6869921-01 | 3040-00-323-8310 | Special Features: Steel, Ams5613, 0.642 In. Lg, 0.475 In. W, 0.428 In. Thk End Item Identification: Jet Engine, Tf41 | Avl | RFQ |
6869921-02 | 3040-00-323-8311 | Special Features: Steel, Ams5613, 0.766 In. Lg, 0.475 In. W, 0.428 In. Thk End Item Identification: Jet Engine, Tf41 | Avl | RFQ |
6869921-03 | 3040-00-322-1054 | Special Features: Steel, Ams5613, 0.890 In. Lg, 0.475 In. W, 0.428 In. Thk End Item Identification: Jet Engine, Tf41 | Avl | RFQ |
6869921-04 | 3040-00-322-1066 | Special Features: Item Has Hardness Rating Of Rc30-34;Has Second Unthreaded Hole 0.163 In. Dia.;Item Is 0.475 In. Wide, 0.428 In. Thk. Material: Steel Overall Length: 1.012 Inches Nominal | Avl | RFQ |
6869921-05 | 3040-00-322-1053 | Special Features: Steel, Ams5613, 1.136 In. Lg, 0.475 In. W, 0.428 In. Thk End Item Identification: Jet Engine, Tf41 | Avl | RFQ |
6869921-06 | 3040-00-322-1051 | Special Features: Steel, Ams5613, 1.258 In. Lg, 0.475 In. W, 0.428 In. Thk End Item Identification: Jet Engine, Tf41 | Avl | RFQ |
6869921-07 | 3040-00-322-1049 | Special Features: Steel, Ams5613, 1.380 In. Lg, 0.475 In. W, 0.428 In. Thk End Item Identification: Jet Engine, Tf41 | Avl | RFQ |
6869921-08 | 3040-00-322-0960 | Special Features: Steel, Ams5613, 1.500 In. Lg, 0.475 In. W, 0.428 In. Thk End Item Identification: Jet Engine, Tf41 | Avl | RFQ |
6869921-09 | 3040-00-322-1067 | Special Features: Steel, Ams5613, 1.620 In. Lg, 0.475 In. W, 0.428 In. Thk End Item Identification: Jet Engine, Tf41 | Avl | RFQ |
6869921-10 | 3040-00-322-0959 | Special Features: Steel, Ams5613, 1.740 In. Lg, 0.475 In. W, 0.428 In. Thk End Item Identification: Jet Engine, Tf41 | Avl | RFQ |
6887174 | 3040-00-467-0617 | End Item Identification: Engine, Turboprop, Model T56 | Avl | RFQ |
70128-301-1 | 1560-01-201-9668 | Special Features: Tungsten Alloy, Ams 725; 5.250 In. O/A Lg; 0.750 In. W; 0.750 In. Thk; Two Holes 0.166 In. Dia, 4.000 In. Distance Between Centerlines Of Holes; Paint, Mil-C-22750, Class 2, Color No. 26378 Per Fed-Std-595 | Avl | RFQ |
70128-301-1 | 3040-01-201-9668 | NA | Avl | RFQ |
717512348-001 | 3040-01-287-3440 | NA | Avl | RFQ |
74603 | 3040-00-772-9935 | NA | Avl | RFQ |
8925947 | 3040-01-246-5944 | NA | Avl | RFQ |
BR-1080 | 3040-01-455-3746 | NA | Avl | RFQ |
EU28457 | 3040-00-871-6070 | End Item Identification: Acft Eng Tf41 | Avl | RFQ |
EU37154 | 3040-00-872-0748 | End Item Identification: Acft Eng Tf41 | Avl | RFQ |
EU37156 | 3040-00-872-0771 | End Item Identification: Acft Eng Tf41 | Avl | RFQ |
EU52858 | 3040-00-858-0707 | End Item Identification: Acft Eng Tf41 | Avl | RFQ |
EU52861 | 3040-00-858-0710 | End Item Identification: Acft Eng Tf41 | Avl | RFQ |
EU52862 | 3040-00-858-0712 | End Item Identification: Acft Eng Tf41 | Avl | RFQ |
EU52863 | 3040-00-858-0713 | End Item Identification: Acft Eng Tf41 | Avl | RFQ |
EU52864 | 3040-00-858-0714 | End Item Identification: Acft Eng Tf41 | Avl | RFQ |
M11153 | 3040-00-057-5121 | NA | Avl | RFQ |
M1339 | 6610-00-406-8494 | End Item Identification: H-1 Iroquois Helicopter | Avl | RFQ |
M1339 | 3040-00-406-8494 | NA | Avl | RFQ |
ND2071 | 3040-01-363-2359 | NA | Avl | RFQ |
PL-1080-10 | 3040-01-455-3746 | NA | Avl | RFQ |
S8156B8-030C | 3040-00-637-2698 | Special Features: Round; 4130 Steel; Surface Treatment Qq-P-416, Ty1, Cl1 Cadmium; Hardness Rockwell C 28.0-36.0; Id O.255-0.260 In.; O/A Dia 0.410-0.430 In.; 0.030 In. Wd End Item Identification: Turbine Engine, General Electric, T700-Ge-700 | Avl | RFQ |
SM-D-657594 | 3040-01-215-9214 | NA | Avl | RFQ |
SM-D-657594-1 | 3040-01-215-9214 | NA | Avl | RFQ |
SM-D-657594-3 | 3040-01-189-0469 | NA | Avl | RFQ |
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