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Consumables & expendables · Spec-Crosswalk

INSULATOR,STRAIN

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

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Part number5 approved sources
You are here · Stock number5970-00-117-4988
Specificationnone cited

Approved sources and substitutes

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

61088 NAVAL SHIP SYSTEMS COMMAND

CONFIRMED

INSULATOR,STRAIN

NSN 5970-00-117-4988

OVERALL LENGTH: 4.000 INCHES NOMINAL OUTSIDE DIAMETER: 0.750 INCHES NOMINAL WIRE HOLE DIAMETER: 0.188 INCHES NOMINAL IDENTIFICATION CODE COLOR: WHITE

8A1222 NORTHROP GRUMMAN SYSTEMS CORPORATIO

CONFIRMED

INSULATOR,STRAIN

NSN 5970-00-405-8971

OVERALL LENGTH: 4.000 INCHES NOMINAL OUTSIDE DIAMETER: 0.750 INCHES NOMINAL WIRE HOLE DIAMETER: 0.188 INCHES NOMINAL IDENTIFICATION CODE COLOR: BROWN

JANI8 JOINT ARMY-NAVY SPECIFICATIONS

CONFIRMED

INSULATOR,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

JANI8TYPENS3B5016 JOINT ELECTRONICS TYPE DESIGNATION

CONFIRMED

INSULATOR,STRAIN

NSN 5970-00-280-4944

OVERALL LENGTH: 2.750 INCHES NOMINAL OUTSIDE DIAMETER: 0.500 INCHES NOMINAL WIRE HOLE DIAMETER: 0.125 INCHES NOMINAL IDENTIFICATION CODE COLOR: BROWN

MIL-I-23264/20 MILITARY SPECIFICATIONS

CONFIRMED

INSULATOR,STRAIN

NSN 5970-00-178-1150

OVERALL LENGTH: 4.000 INCHES NOMINAL OUTSIDE DIAMETER: 0.750 INCHES NOMINAL WIRE HOLE DIAMETER: 0.188 INCHES NOMINAL IDENTIFICATION CODE COLOR: BROWN

Stated characteristics

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

IDENTIFICATION CODE COLORBROWNFLIS characteristics (MRC)
OVERALL LENGTH4.000 INCHES NOMINALFLIS characteristics (MRC)
OUTSIDE DIAMETER0.750 INCHES NOMINALFLIS characteristics (MRC)
FIRST CORNER RADIUS0.188 INCHES NOMINALFLIS characteristics (MRC)
SECOND CORNER RADIUS0.062 INCHES NOMINALFLIS characteristics (MRC)
CONDUCTOR SEPARATION DISTANCE3.000 INCHES NOMINALFLIS characteristics (MRC)
WIRE HOLE DIAMETER0.188 INCHES NOMINALFLIS characteristics (MRC)
FIRST DISTANCE FROM CONDUCTOR HOLE TO INSULATOR END0.500 INCHES NOMINALFLIS characteristics (MRC)
STYLE DESIGNATORDOUBLE, BALL ENDFLIS 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).

  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).