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 01003, 01008, 01010, 1035, 14-01162. 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 Triumph Aerostructures Llc, Ndt Engineering Corporation, Olympus Scientific Solutions, Morehouse Instrument Company, Aurora Flight Sciences Of West. Our team provides superior quality assurance testing for and more. So if you are in need of Reference Standard Physical Prop 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
|
---|---|---|---|---|
01003 | 9535-01-585-4706 | NA | Avl | RFQ |
01008 | 9535-01-585-4709 | NA | Avl | RFQ |
01010 | 9535-01-585-4713 | NA | Avl | RFQ |
1035 | 9535-01-585-4718 | NA | Avl | RFQ |
14-01162 | 6635-01-495-9789 | Part Name Assigned By Controlling Agency: F-5E Dorsal Longeron Ndi Ref Standard Overall Length: 17.580 Inches Nominal Functional Description: Used To Validate Opperation Of Ndi Equipment (Eddy Current) | Avl | RFQ |
14-01162 | 6635-01-495-9789 | Part Name Assigned By Controlling Agency: F-5E Dorsal Longeron Ndi Ref Standard Overall Length: 17.580 Inches Nominal Functional Description: Used To Validate Opperation Of Ndi Equipment (Eddy Current) | Avl | RFQ |
14-01162-1 | 6635-01-495-9789 | Part Name Assigned By Controlling Agency: F-5E Dorsal Longeron Ndi Ref Standard Overall Length: 17.580 Inches Nominal Functional Description: Used To Validate Opperation Of Ndi Equipment (Eddy Current) | Avl | RFQ |
14-01162-1 | 6635-01-495-9789 | Part Name Assigned By Controlling Agency: F-5E Dorsal Longeron Ndi Ref Standard Overall Length: 17.580 Inches Nominal Functional Description: Used To Validate Opperation Of Ndi Equipment (Eddy Current) | Avl | RFQ |
1877AS162-1 | 6635-01-378-8444 | End Item Identification: Special Acft And Engine Tool And Support Equipment And Parts | Avl | RFQ |
1877AS163-1 | 6635-01-378-4943 | End Item Identification: Special Acft And Engine Tools, Support Equipment And Parts | Avl | RFQ |
1877AS164-1 | 6635-01-378-6685 | End Item Identification: Special Acft And Engine Tools, Support Equipment And Parts | Avl | RFQ |
1916451 | 6635-01-378-8444 | End Item Identification: Special Acft And Engine Tool And Support Equipment And Parts | Avl | RFQ |
1916452 | 6635-01-378-4943 | End Item Identification: Special Acft And Engine Tools, Support Equipment And Parts | Avl | RFQ |
1916453 | 6635-01-378-6685 | End Item Identification: Special Acft And Engine Tools, Support Equipment And Parts | Avl | RFQ |
200-10K | 6635-01-494-4903 | Special Features: 10, 000 Lb Capacity; Tension & Compression Type General Characteristics Item Description: 200 Division Dial; Adjustable Vernier Index; Scale Reading To 1/10 A Division & Interpolation To 1/20 Per Division; Zero Reading On No-Load; Part Name Assigned By Controlling Agency: Proving Ring | Avl | RFQ |
200-1K | 6635-01-494-4913 | Special Features: 1, 000 Lb Capacity General Characteristics Item Description: 200 Division Dial; Adjustable Vernier Index; Scale Reading To 1/10 A Division & Interpolation To 1/20 Per Division; Zero Reading On No-Load; Part Name Assigned By Controlling Agency: Proving Ring | Avl | RFQ |
200-30K | 6635-01-494-4923 | Special Features: 30, 000 Lb Capacity General Characteristics Item Description: 200 Division Dial; Adjustable Vernier Index; Scale Reading To 1/10 A Division & Interpolation To 1/20 Per Division; Zero Reading On No-Load; Part Name Assigned By Controlling Agency: Proving Ring | Avl | RFQ |
200-3K | 6635-01-494-4928 | Special Features: 3, 000 Lb Capacity General Characteristics Item Description: 200 Division Dial; Adjustable Vernier Index; Scale Reading To 1/10 A Division & Interpolation To 1/20 Per Division; Zero Reading On No-Load; Part Name Assigned By Controlling Agency: Proving Ring | Avl | RFQ |
2562-1 | 9535-01-585-4721 | NA | Avl | RFQ |
2563-1 | 9535-01-585-4722 | NA | Avl | RFQ |
3673310M01044-1 | 9535-01-582-3877 | NA | Avl | RFQ |
3673310M01046-1 | 6635-01-582-3878 | End Item Identification: Rq-4A Part Name Assigned By Controlling Agency: Ndi Standard | Avl | RFQ |
3673310M01050-1 | 6635-01-582-3892 | End Item Identification: Rq-4A Drone | Avl | RFQ |
3673310M01051-1 | 6635-01-582-3881 | End Item Identification: Rq-4A Part Name Assigned By Controlling Agency: Reference Standard | Avl | RFQ |
3673310M01054-1 | 6635-01-582-3890 | End Item Identification: Rq-4A Drone | Avl | RFQ |
3673310M01055-1 | 6635-01-582-3882 | End Item Identification: Rq-4A Part Name Assigned By Controlling Agency: Ndi Standard | Avl | RFQ |
3673310M01056-1 | 9535-01-582-3885 | NA | Avl | RFQ |
3673310M01061-1 | 6635-01-583-4267 | End Item Identification: Rq-4A Part Name Assigned By Controlling Agency: Ndi Standard | Avl | RFQ |
3673310M01071-1 | 6635-01-582-3883 | End Item Identification: Rq-4A Part Name Assigned By Controlling Agency: Ndi Standard | Avl | RFQ |
3673310M01072-1 | 6635-01-583-0872 | End Item Identification: Rq-4A Drone | Avl | RFQ |
507851 | 6635-00-415-9225 | General Characteristics Item Description: Matl: 1018 Steel, Nickel Plated; Calibrates Distance And Determines The Angle Of Sound Beam Propagation From Search Units; Reference Holes Added To Permit Sensitivity Level Setting | Avl | RFQ |
54352 | 6635-01-419-6234 | Special Features: This Gage Is Designed To Fit On The Disk Adapter Of The Eeeeeeeeeeeeee/C Test Stand P/N 5Wa54233. End Item Identification: F100 Pw220 | Avl | RFQ |
57A-4244-19 | 6635-00-415-9225 | General Characteristics Item Description: Matl: 1018 Steel, Nickel Plated; Calibrates Distance And Determines The Angle Of Sound Beam Propagation From Search Units; Reference Holes Added To Permit Sensitivity Level Setting | Avl | RFQ |
601-1016TYPE2 | 6635-00-415-9225 | General Characteristics Item Description: Matl: 1018 Steel, Nickel Plated; Calibrates Distance And Determines The Angle Of Sound Beam Propagation From Search Units; Reference Holes Added To Permit Sensitivity Level Setting | Avl | RFQ |
7947479 | 6635-01-092-5129 | Special Features: Consists Of Compsite Plate With 20 Holes From 5/32 To 3/4 In 1/32 Increments. 5 Notches And A Radius. Holes, Notches And Radius Area All Have Known Defects/Flaws Part Name Assigned By Controlling Agency: Dwg: Plate Assembly, Eddy Current; Prvious Item Name: Standard, Universal, Eddy Current Overall Length: 6.995 Inches Minimum And 7.005 Inches Maximum | Avl | RFQ |
7947479-10 | 6635-01-092-5129 | Special Features: Consists Of Compsite Plate With 20 Holes From 5/32 To 3/4 In 1/32 Increments. 5 Notches And A Radius. Holes, Notches And Radius Area All Have Known Defects/Flaws Part Name Assigned By Controlling Agency: Dwg: Plate Assembly, Eddy Current; Prvious Item Name: Standard, Universal, Eddy Current Overall Length: 6.995 Inches Minimum And 7.005 Inches Maximum | Avl | RFQ |
901-220-950-101 | 6635-01-454-8913 | End Item Identification: V-22 Acft Overall Length: 8.000 Inches Nominal Overall Width: 6.000 Inches Nominal | Avl | RFQ |
93720 | 6635-01-352-0357 | End Item Identification: 6635-01-290-2927 General Characteristics Item Description: Honeycomb Aluminum; O/A Dim. 5.000 In. Lg; 5.000 In. W; 4.000 In. H, Flaw Sample | Avl | RFQ |
96652SS | 6635-01-567-7267 | NA | Avl | RFQ |
99073 | 6635-01-609-4427 | NA | Avl | RFQ |
99120 | 6635-01-561-0156 | End Item Identification: F-22 Aircraft Engine Thrust Mount Kit 6635-01-560-8721 Part Name Assigned By Controlling Agency: Reference Standard, Engine Side | Avl | RFQ |
99121 | 6635-01-561-0159 | End Item Identification: F-22 Aircraft Engine Thrust Mount Kit 6635-01-560-8721 Part Name Assigned By Controlling Agency: Reference Standard, Airframe Side | Avl | RFQ |
99834 | 6635-01-609-4450 | NA | Avl | RFQ |
99891 | 6635-01-609-4456 | NA | Avl | RFQ |
99917 | 6635-01-609-4444 | NA | Avl | RFQ |
99918 | 6635-01-609-4514 | NA | Avl | RFQ |
C12-DEL-3C1N | 6635-01-527-0445 | Special Features: Gr/Ep Skin Hc Core Disbond Reference Defect End Item Identification: Boeing Aircraft | Avl | RFQ |
C12-DIS-3C1N | 6635-01-611-5932 | NA | Avl | RFQ |
C12-POT-3C1N | 6635-01-527-0446 | End Item Identification: Boeing Generic Part Name Assigned By Controlling Agency: Cr/Ep Skin/Hc Core Disbond Reference Defect | Avl | RFQ |
DAA7257G818-001 | 6635-01-399-5955 | General Characteristics Item Description: The Upper Facesheet Has 7 Piles Of 207-7-500 Tp 1 Woven Gr/Ep Fabric Plus 1 Upper Ply Of 207-7-505 Tp1 Gr/Ep Mat, 207-8-434, C12, Gr15 Film Adhesive; 3.0 In. Thick With Bottom Facesheet 7 Plies Of 207-7-500, Tp1 Woven Gr/Ep Fabric; Divided In To 3 Blocks, 1-Solid Phenolic Block, 1-Honeycomb Core 8.0 Lbs., 1-Honeycomb Core 5.5 Lbs.; Additional Buildu On Solid Side Of 6 Plies Of 207-7-500, Tp1 Woven Gr/Ep Fabric Overall Length: 13.000 Inches Nominal Overall Width: 6.000 Inches Nominal | Avl | RFQ |
DAA7257G820-001 | 6635-01-399-5957 | End Item Identification: Pacer Special General Characteristics Item Description: Conssits Of 2 Layers-1 First Layup, 2-Second Layup; 2 Polytetrafluoroethylene Inserts 1 From The Right Edge In On The Centerline 1.75 In. Center Of The Hole, 1-1.75In From Left Edge On Centerline Overall Length: 6.000 Inches Nominal | Avl | RFQ |
ECRS-161C TI | 6635-01-611-5675 | End Item Identification: F-22A Support Equipment Part Name Assigned By Controlling Agency: Reference Standard | Avl | RFQ |
F16A-7-LB-S1 | 6635-01-342-7692 | NA | Avl | RFQ |
F16A-7-LB-S1 | 6635-01-342-7692 | NA | Avl | RFQ |
F16A-7-LG-S1 | 6635-01-342-7692 | NA | Avl | RFQ |
F16A-7-LG-S1 | 6635-01-342-7692 | NA | Avl | RFQ |
F16A-LG-S1 | 6635-01-342-7692 | NA | Avl | RFQ |
F16A-LG-S1 | 6635-01-342-7692 | NA | Avl | RFQ |
NDT 1033-10 | 6635-01-527-0451 | End Item Identification: Boeing Generic | Avl | RFQ |
NEC6120 | 6635-01-495-8409 | Special Features: Aluminum 7075T6; Used To Set Up Inspection Instruments Looking For Defects In Aircraft Structure Material: Aluminum | Avl | RFQ |
PDSANE471 | 6635-00-415-9225 | General Characteristics Item Description: Matl: 1018 Steel, Nickel Plated; Calibrates Distance And Determines The Angle Of Sound Beam Propagation From Search Units; Reference Holes Added To Permit Sensitivity Level Setting | Avl | RFQ |
PWA43232 | 6635-01-310-2492 | NA | Avl | RFQ |
PWA43235 | 6635-01-310-2493 | NA | Avl | RFQ |
PWA54297 | 6635-01-239-9948 | General Characteristics Item Description: 4.500 In. W, 5.500 In. L, 2.500 In. H; 2 Lb; Matl:Boltaron/Waspaloy; Probe Dia: 0.398 And 0.630 In.; Used In Eddy Current Inspection To Detect Flaws In The 7Th, 9Th, 11Th, & 13Th Compressor Disk Holes; Maufactures Suggested Name Gage Standard, Probe Calibration | Avl | RFQ |
PWA54298 | 6635-01-239-9949 | General Characteristics Item Description: 4.500 In. W, 3.500 In. L, 1.500 In. H; 2 Lb; Matl: Boltaron/Waspaloy; Probe Dia: 0.456, 0.471, 0.390 In.; Used In Eddy Current Inspection To Detect Flaws In The 8Th, 10Th, 12Th, And 13Th Compressor Disk Holes; Manufactures Suggested Name Gage Standard, Probe Caibration | Avl | RFQ |
PWA54347 | 6635-01-419-4935 | Special Features: This Gage Is Used To Set Up And Calibrate The Sensitivity Of The Eddy Current Instrument Prior To And After Performing The Eddy Current Test On The Balance Weight Flange Scallop Of The 1St. Compressor Disk.Thiss Gage Is Designed To Fit On The Disk Adapter Of The Eddy Current Test Stand P/N Pwa54233. End Item Identification: Engine Aircraft, F100-Pw220 | Avl | RFQ |
PWA54348 | 6635-01-419-4937 | Special Features: This Gage Is Used To Set Up And Calibrate The Eddy Current Instrument Prior To And After Performing The Eddy Current Inspection Of The Broach Slot Of The Engine Disk. It Is Designed To Fit Disk Adapter Of The E/C Test Stand P/N Pwa54300. End Item Identification: Engine Aircrtaft, F100-Pw220 (F-15C/D/E). | Avl | RFQ |
PWA71302 | 6635-01-448-0984 | NA | Avl | RFQ |
ST8870-1 | 6635-01-527-0441 | Special Features: Gr/Ep Skin/Nomex Core Disbond Reference Defect End Item Identification: Boeing 757 | Avl | RFQ |
ST8870-4 | 6635-01-527-0443 | Special Features: Gr/Ep Skin/Nomex Core Disbond Reference Defect End Item Identification: Boeing 757 | Avl | RFQ |
ST8870-7 | 6635-01-527-0452 | End Item Identification: Boeing 757 Part Name Assigned By Controlling Agency: Gr/Ep Laminate Step Thickness Standard | Avl | RFQ |
ST8870-8 | 6635-01-527-0455 | End Item Identification: Boeing 757 Part Name Assigned By Controlling Agency: Gr/Ep Laminate Step Thickness Standard | Avl | RFQ |
ST8870-9 | 6635-01-527-0458 | End Item Identification: Boeing 757 Part Name Assigned By Controlling Agency: Gr/Ep Laminate Step Thickness Standard | Avl | RFQ |
STD-1008 | 6635-01-577-0853 | Special Features: 0.980In Through Hole In Two Layer (0.25 And 0.30In Thk) Iconel 718. Edm Notch 0.30 X 0.30In In 0.30In Thk Layer; Part Of Side Of Body Pin Bore Inspection Kit 9231862 End Item Identification: F-22 Raptor Part Name Assigned By Controlling Agency: Eddy Current Reference Standard | Avl | RFQ |
TB5939-1 | 6635-00-415-9225 | General Characteristics Item Description: Matl: 1018 Steel, Nickel Plated; Calibrates Distance And Determines The Angle Of Sound Beam Propagation From Search Units; Reference Holes Added To Permit Sensitivity Level Setting | Avl | RFQ |
TSD2052 | 6635-01-596-3286 | NA | Avl | RFQ |
UT 10 | 6635-01-582-3878 | End Item Identification: Rq-4A Part Name Assigned By Controlling Agency: Ndi Standard | Avl | RFQ |
UT 1099 | 6635-01-561-0545 | Part Name Assigned By Controlling Agency: Test Block Functional Description: Used With Ut 1096 To Measure The Thickness Of A Case Supplementary Features: Materail Is Inco 718 | Avl | RFQ |
UT 16 | 6635-01-582-3892 | End Item Identification: Rq-4A Drone | Avl | RFQ |
UT 17 | 6635-01-582-3881 | End Item Identification: Rq-4A Part Name Assigned By Controlling Agency: Reference Standard | Avl | RFQ |
UT 18 | 6635-01-582-3883 | End Item Identification: Rq-4A Part Name Assigned By Controlling Agency: Ndi Standard | Avl | RFQ |
UT 19 | 6635-01-583-0872 | End Item Identification: Rq-4A Drone | Avl | RFQ |
UT 20 | 6635-01-582-3890 | End Item Identification: Rq-4A Drone | Avl | RFQ |
UT 21 | 6635-01-582-3882 | End Item Identification: Rq-4A Part Name Assigned By Controlling Agency: Ndi Standard | Avl | RFQ |
UT 22 | 9535-01-582-3885 | NA | Avl | RFQ |
UT 28 | 6635-01-583-4267 | End Item Identification: Rq-4A Part Name Assigned By Controlling Agency: Ndi Standard | Avl | RFQ |
UT11 | 6635-01-585-4712 | End Item Identification: Rq-4A | Avl | RFQ |
UT13 | 6635-01-585-4716 | End Item Identification: Rq-4A Part Name Assigned By Controlling Agency: Ndi Standard | Avl | RFQ |
UT15 | 6635-01-585-4717 | End Item Identification: Rq-4A | Avl | RFQ |
UT23 | 9535-01-585-4720 | NA | Avl | RFQ |
UT25 | 9535-01-585-4723 | NA | Avl | RFQ |
UT26 | 6635-01-585-4724 | End Item Identification: Rq-4A | Avl | RFQ |
UT27 | 6635-01-585-4725 | End Item Identification: Rq-4A Part Name Assigned By Controlling Agency: Ndi Standard | Avl | RFQ |
VM.30889-C1A | 6635-01-092-5129 | Special Features: Consists Of Compsite Plate With 20 Holes From 5/32 To 3/4 In 1/32 Increments. 5 Notches And A Radius. Holes, Notches And Radius Area All Have Known Defects/Flaws Part Name Assigned By Controlling Agency: Dwg: Plate Assembly, Eddy Current; Prvious Item Name: Standard, Universal, Eddy Current Overall Length: 6.995 Inches Minimum And 7.005 Inches Maximum | Avl | RFQ |
VM.30889-C1A | 6635-01-092-5129 | Special Features: Consists Of Compsite Plate With 20 Holes From 5/32 To 3/4 In 1/32 Increments. 5 Notches And A Radius. Holes, Notches And Radius Area All Have Known Defects/Flaws Part Name Assigned By Controlling Agency: Dwg: Plate Assembly, Eddy Current; Prvious Item Name: Standard, Universal, Eddy Current Overall Length: 6.995 Inches Minimum And 7.005 Inches Maximum | Avl | RFQ |
VM30889-C1A AF | 6635-01-092-5129 | Special Features: Consists Of Compsite Plate With 20 Holes From 5/32 To 3/4 In 1/32 Increments. 5 Notches And A Radius. Holes, Notches And Radius Area All Have Known Defects/Flaws Part Name Assigned By Controlling Agency: Dwg: Plate Assembly, Eddy Current; Prvious Item Name: Standard, Universal, Eddy Current Overall Length: 6.995 Inches Minimum And 7.005 Inches Maximum | Avl | RFQ |
VM30889-C1I | 6635-01-512-4953 | Special Features: Consists Of A Composit Plate With 20 Holes From 5/32 To 3/4 In 1/32 Increments; 9 Notches And A Radius; Holes, Notches And Radius Areaall Have Known Defects End Item Identification: F/A-22 Raptor Part Name Assigned By Controlling Agency: Reference Standard, Physical Properties | Avl | RFQ |
VM30889-C1S | 6635-01-512-4952 | Special Features: Consists Of A Composite Plate With 20 Holes From 5/32 To 3/4 In 1/32 Increments; 9 Notches And A Radius; Holes, Notches And Radium Area All Have Known Defects; Material 4000 Series Steel (4340 Or 4130) End Item Identification: F/A 22 Raptor Aircraft Overall Length: 7.000 Inches Nominal | Avl | RFQ |
VM30889-C1SS | 6635-01-548-6559 | Part Name Assigned By Controlling Agency: Universal Eddy Current Refernce Material: Steel Corrosion Resisting | Avl | RFQ |
VM30889-C1T | 6635-01-390-1768 | Special Features: Dconsists Of A Composite Plate With 20 Holes From 5/32 To 3/4 In 1/32 Increments. 9 Notches And A Radius. Holes, Notches And Radius Area All Have Known Defects. Material Is Titanium Alloy 6Al-4V. Part Name Assigned By Controlling Agency: Eddy Current Reference Standard Overall Length: 7.000 Inches Nominal | Avl | RFQ |
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