Trail

Consumables & expendables · Spec-Crosswalk

INSULATOR,STANDOFF

Stock number · interchangeable / substitutable per the NSN catalogue (FLIS I&S) — every member CONFIRMED

← Search another part, spec or stock number

Purchasable unitnone derived yet
Part number2 approved sources
You are here · Stock number5970-00-117-5353
Specificationnone cited

Approved sources and substitutes

Every maker's item codified on this stock number, with the catalogue's order of use.

61300 NAVAL SHIP SYSTEMS COMMAND

CONFIRMED

INSULATOR,STANDOFF

NSN 5970-00-117-5353

OVERALL WIDTH: 0.719 INCHES NOMINAL OVERALL LENGTH: 0.719 INCHES NOMINAL SCREW THREAD DIAMETER AND LOCATION: 0.190 ELECTRICAL TERMINATION INCHES NOMINAL AND 0.190 MOUNTING FACILITY INCHES NOMINAL OVERALL HEIGHT: 1.000 INCHES NOMINAL

MIL-I-23264/2 MILITARY SPECIFICATIONS

CONFIRMED

INSULATOR,STANDOFF

NSN 5970-00-076-1599

OVERALL WIDTH: 0.500 INCHES NOMINAL THREAD LENGTH: 0.375 INCHES NOMINAL OVERALL LENGTH: 0.500 INCHES NOMINAL DIELECTRIC MATERIAL VOLTAGE RATING PER UNIT THICKNESS: 249.0 VOLTS PER MIL /0.001 INCH/

Stated characteristics

The codification record's own dimensions and material statements — official, and public by nature.

IDENTIFICATION CODE COLORWHITEFLIS characteristics (MRC)
OVERALL LENGTH0.719 INCHES NOMINALFLIS characteristics (MRC)
OVERALL HEIGHT1.000 INCHES NOMINALFLIS characteristics (MRC)
OVERALL WIDTH0.719 INCHES NOMINALFLIS 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)
DISTANCE FROM CENTER TO EDGE0.360 INCHES NOMINAL SECOND · 0.360 INCHES NOMINAL FIRSTFLIS characteristics (MRC)
MATERIALPORCELAIN OVERALL · PORCELAIN MOUNTING BASEFLIS characteristics (MRC)
STYLE DESIGNATORPILLARFLIS characteristics (MRC)

Take the family with you

The whole group as CSV — members, makers, stock numbers and order of use.

Export paused

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.

Request a Stage 1(a) dossierTriage the whole list free
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).

  1. 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.
  2. 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.
  3. 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.
  4. 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.
  5. 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).
  6. 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).