7606246 U S ARMY ARMAMENT RESEARCH & (19200)
POSSIBLEINSULATOR,STANDOFF
codified reference — recorded against this stock number; the catalogue grade is not held
Consumables & expendables · Spec-Crosswalk
INSULATOR,STANDOFF
Stock number · one item of supply — the parts codified against it, and the stock numbers it substitutes for
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Purchasable unitnone derived yet
Part number9 approved sources
You are here · Stock number5970-00-284-7930
Specificationnone cited
Approved sources
Every maker's reference the catalogue files against this item of supply — the parts someone holding this number can use. The design-control reference is the one that controls the item; a secondary reference is a real codified fact and a weaker one.
BL713988 LUCENT TECHNOLOGIES INC CORPORATE (3B4M0)
POSSIBLEINSULATOR,STANDOFF
codified reference — recorded against this stock number; the catalogue grade is not held
What defines this item
Specifications and drawings the catalogue records against this number. These are what the parts above are made to — never alternatives to them.
- MIL-I-23264/3 — Military Specifications (specification · not yet a document in the graph)
- NL522W20-016 — Military Specifications (specification · not yet a document in the graph)
Substitutes — other stock numbers
Codified interchangeability across stock numbers (FLIS I&S), with the catalogue's order of use where it states one.
135-0503-001 VIKING TECHNOLOGIES, LTD. DBA
CONFIRMEDINSULATOR,STANDOFF
NSN 5970-00-284-7930
OUTSIDE DIAMETER: 1.125 INCHES NOMINAL SCREW THREAD DIAMETER AND LOCATION: 0.190 ELECTRICAL TERMINATION INCHES NOMINAL AND 0.190 MOUNTING FACILITY INCHES NOMINAL OVERALL HEIGHT: 2.063 INCHES NOMINAL IDENTIFICATION CODE COLOR: WHITE
135-0504-001 VIKING TECHNOLOGIES, LTD.
CONFIRMEDINSULATOR,STANDOFF
NSN 5970-00-535-2681
DIELECTRIC MATERIAL VOLTAGE RATING PER UNIT THICKNESS: 249.0 VOLTS PER MIL /0.001 INCH/ OUTSIDE DIAMETER: 1.500 INCHES NOMINAL TOP DIAMETER: 0.750 INCHES NOMINAL SCREW THREAD DIAMETER AND LOCATION: 0.190 ELECTRICAL TERMINATION INCHES NOMINAL AND 0.190 MOUNTING FACILITY INCHES NOMINAL
25279 LAPP INSULATOR COMPANY LLC
CONFIRMEDINSULATOR,STANDOFF
NSN 5970-00-644-3047
FLANGE THICKNESS: 0.250 INCHES NOMINAL OUTSIDE DIAMETER: 2.125 INCHES NOMINAL MOUNTING HOLE DIAMETER: 0.188 INCHES NOMINAL MOUNTING BOLT CIRCLE DIAMETER: 1.688 INCHES NOMINAL
6465 CARBORUNDUM CO THE REFRACTORIES AND
CONFIRMEDINSULATOR,STANDOFF
NSN 5970-00-235-6633
OUTSIDE DIAMETER: 1.125 INCHES NOMINAL SCREW THREAD DIAMETER AND LOCATION: 0.190 MOUNTING FACILITY INCHES NOMINAL AND 0.190 ELECTRICAL TERMINATION INCHES NOMINAL OVERALL HEIGHT: 2.000 INCHES NOMINAL IDENTIFICATION CODE COLOR: WHITE
7106960PT4 LOCKHEED MARTIN CORPORATION
CONFIRMEDINSULATOR,STANDOFF
NSN 5970-00-931-1115
THREAD LENGTH: 0.375 INCHES NOMINAL DIELECTRIC MATERIAL VOLTAGE RATING PER UNIT THICKNESS: 299.0 VOLTS PER MIL /0.001 INCH/ OUTSIDE DIAMETER: 0.500 INCHES NOMINAL SCREW THREAD DIAMETER AND LOCATION: 0.164 ELECTRICAL TERMINATION INCHES NOMINAL AND 0.164 MOUNTING FACILITY INCHES NOMINAL
7602239P3 WESTINGHOUSE ELECTRIC CORP
CONFIRMEDINSULATOR,STANDOFF
NSN 5970-00-156-6143
OUTSIDE DIAMETER: 1.500 INCHES NOMINAL TOP DIAMETER: 0.750 INCHES NOMINAL SCREW THREAD DIAMETER AND LOCATION: 0.190 ELECTRICAL TERMINATION INCHES NOMINAL AND 0.190 MOUNTING FACILITY INCHES NOMINAL OVERALL HEIGHT: 3.000 INCHES NOMINAL
7606246 U S ARMY ARMAMENT RESEARCH &
CONFIRMEDINSULATOR,STANDOFF
NSN 5970-00-117-4954
THREAD LENGTH: 0.375 INCHES NOMINAL DIELECTRIC MATERIAL VOLTAGE RATING PER UNIT THICKNESS: 249.0 VOLTS PER MIL /0.001 INCH/ OUTSIDE DIAMETER: 1.125 INCHES NOMINAL TOP DIAMETER: 0.625 INCHES NOMINAL
JANI8 JOINT ARMY-NAVY SPECIFICATIONS
CONFIRMEDINSULATOR,STANDOFF
NSN 5970-00-027-8617
OUTSIDE DIAMETER: 0.750 INCHES NOMINAL SCREW THREAD DIAMETER AND LOCATION: 0.190 ELECTRICAL TERMINATION INCHES NOMINAL AND 0.190 MOUNTING FACILITY INCHES NOMINAL OVERALL HEIGHT: 3.000 INCHES NOMINAL IDENTIFICATION CODE COLOR: WHITE
MIL-I-23264/3 MILITARY SPECIFICATIONS
CONFIRMEDINSULATOR,STANDOFF
NSN 5970-00-117-4954
THREAD LENGTH: 0.375 INCHES NOMINAL DIELECTRIC MATERIAL VOLTAGE RATING PER UNIT THICKNESS: 249.0 VOLTS PER MIL /0.001 INCH/ OUTSIDE DIAMETER: 1.125 INCHES NOMINAL TOP DIAMETER: 0.625 INCHES NOMINAL
Stated characteristics
The codification record's own dimensions and material statements — official, and public by nature.
IDENTIFICATION CODE COLORWHITEFLIS characteristics (MRC)
THREAD LENGTH0.375 INCHES NOMINALFLIS characteristics (MRC)
OUTSIDE DIAMETER1.125 INCHES NOMINALFLIS characteristics (MRC)
OVERALL HEIGHT2.000 INCHES NOMINALFLIS characteristics (MRC)
TOP DIAMETER0.625 INCHES NOMINALFLIS characteristics (MRC)
THREAD LOCATIONMOUNTING FACILITY AND ELECTRICAL TERMINATIONFLIS characteristics (MRC)
MOUNTING FACILITY TYPE AND QUANTITY1 THREADED HOLE(S)FLIS characteristics (MRC)
SCREW THREAD QUANTITY PER INCH AND LOCATION32 ELECTRICAL TERMINATION AND 32 MOUNTING FACILITYFLIS characteristics (MRC)
SCREW THREAD DIAMETER AND LOCATION0.190 ELECTRICAL TERMINATION INCHES NOMINAL AND 0.190 MOUNTING FACILITY INCHES NOMINALFLIS characteristics (MRC)
THREAD CLASS AND LOCATION2B ELECTRICAL TERMINATION AND 2B MOUNTING FACILITYFLIS characteristics (MRC)
STYLE DESIGNATORPILLARFLIS characteristics (MRC)
DIELECTRIC MATERIAL VOLTAGE RATING PER UNIT THICKNESS249.0 VOLTS PER MIL /0.001 INCH/FLIS characteristics (MRC)
Take the family with you
The whole group as CSV — members, makers, stock numbers and order of use.
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The monthly allowance for this address is used — the pattern reads as catalogue work, not a line to settle.
Whole-catalogue work is what Stage 1(a) is for: every line human-checked against the cited evidence, discrepancies annotated, back inside 24 hours. Free searching stays free — this gate only catches bulk pulls.
Staying inside the regulation — routes from candidate to approved
Codification and qualification say who vouches for a part — they are not installation eligibility. Under EASA Part-21, eligibility flows from the approved design (type design / IPC) or an approved change; under Part-145, acceptance needs an EASA Form 1 or, for genuine standard parts, conformity traceable to the officially recognised standard (145.A.42).
- Classify the part. Is it a GENUINE standard part? If the IPC/CMM references only a public specification (AN/MS/NAS/SAE-AS/ISO/EN) with no OEM source-control drawing, buy at source with conformity traceable to that standard.
- Check for an approved alternate. The IPC/CMM/vendor list may already carry an alternate part number or vendor code — an already-approved alternate needs no new approval.
- Ask the design approval holder. Request the source-control data, written equivalence, or addition of the alternative source to the approved data. Document a refusal.
- Raise a design change. Via a Part-21J DOA (or EASA/ADOA): a 21.A.95 minor change adding the alternate to the approved data, backed by an identicality/equivalence file — dimensions, material, class, load rating, lubricant/seal, corrosion protection, acceptance criteria. Critical applications escalate to major change/STC.
- FAA-PMA / BASA path. Where the product is also FAA-certificated: PMA parts reach EASA aircraft under the BASA/TIP (non-critical directly; critical via EASA-validated STC).
- Production, release, traceability. Approved parts are produced under a POA, released on an EASA Form 1 (marked EPA where applicable), with EN/AS 9120-grade traceability into Part-145/CAMO acceptance.
Stage 1(a): we assemble the equivalence/identicality starter file — the cited evidence this graph holds, shaped for your DOA or compliance department to take forward. See pricing.
Regulatory explainer, not legal advice: paragraph numbers, derogations and the BASA/TIP revision change — verify against the current consolidated Regulation (EU) 748/2012, the EASA Easy Access Rules and the current TIP, and engage your DOA and competent authority early.
Source: DLA Logistics Information Services (FLIS) · cycle 2026-0 · official codification
This crosswalk identifies candidate equivalents with cited evidence. It is not an airworthiness approval. Substitution decisions remain subject to your organisation’s procurement and engineering approval process and the governing maintenance data (AMM/CMM/SRM/CML/OMAT).