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Consumables & expendables · Spec-Crosswalk

INSULATION SLEEVING,ELECTRICAL,S

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 number3 approved sources
You are here · Stock number5970-00-122-5429
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.

SS7073-0204 SIKORSKY AIRCRAFT CORPORATION (78286)

POSSIBLE

OEM source-control number — the OEM’s own reference for this item; the sources beneath answer it. All of this OEM’s references →

INSULATION SLEEVING,ELECTRICAL,S

secondary reference — also codified against this stock number, as a secondary reference (RNCC 5)

LS9747-9 LOCKHEED MARTIN CORP (98897)

POSSIBLE

OEM source-control number — the OEM’s own reference for this item; the sources beneath answer it. All of this OEM’s references →

INSULATION SLEEVING,ELECTRICAL,S

codified reference — recorded against this stock number; the catalogue grade is not held

C2023-1-4 LOCKHEED MARTIN CORPORATION (81755)

CONFIRMED

INSULATION SLEEVING,ELECTRICAL,S

design-control reference — the reference that controls this item of supply (RNCC 3 · RNVC 2)

102-1-B7 HELLERMANNTYTON LTD (K0720)

POSSIBLE

INSULATION SLEEVING,ELECTRICAL,S

secondary reference — also codified against this stock number, as a secondary reference (RNCC 5)

11153149-4 US ARMY AVIATION AND MISSILE COMMAND (18876)

POSSIBLE

INSULATION SLEEVING,ELECTRICAL,S

secondary reference — also codified against this stock number, as a secondary reference (RNCC 5)

202A153-3 TYCO ELECTRONICS FRANCE SAS (F0286)

POSSIBLE

INSULATION SLEEVING,ELECTRICAL,S

secondary reference — also codified against this stock number, as a secondary reference (RNCC 5)

Also filed by the same company as 202A153-3 (D1973) — one product, several catalogue rows.

202A153-3-0 TE CONNECTIVITY CORPORATION (06090)

POSSIBLE

INSULATION SLEEVING,ELECTRICAL,S

secondary reference — also codified against this stock number, as a secondary reference (RNCC 5)

10163801-2 US ARMY AVIATION AND MISSILE COMMAND (18876)

POSSIBLE

INSULATION SLEEVING,ELECTRICAL,S

codified reference — recorded against this stock number; the catalogue grade is not held

3068462-10-3 HONEYWELL INTERNATIONAL INC. (59364)

POSSIBLE

INSULATION SLEEVING,ELECTRICAL,S

codified reference — recorded against this stock number; the catalogue grade is not held

313H264-1 3M COMPANY (53387)

POSSIBLE

INSULATION SLEEVING,ELECTRICAL,S

codified reference — recorded against this stock number; the catalogue grade is not held

347C733H06 NORTHROP GRUMMAN SYSTEMS CORPORATIO (97942)

POSSIBLE

INSULATION SLEEVING,ELECTRICAL,S

codified reference — recorded against this stock number; the catalogue grade is not held

704AS6303-2 NAVAL AIR SYSTEMS COMMAND MANAGED (30003)

POSSIBLE

INSULATION SLEEVING,ELECTRICAL,S

codified reference — recorded against this stock number; the catalogue grade is not held

C085101-004 GYRODYNE CO OF AMERICA INC (10618)

POSSIBLE

INSULATION SLEEVING,ELECTRICAL,S

codified reference — recorded against this stock number; the catalogue grade is not held

HS1-202D153-4 NATIONAL STARCH AND CHEMICAL CO (04552)

POSSIBLE

INSULATION SLEEVING,ELECTRICAL,S

codified reference — recorded against this stock number; the catalogue grade is not held

MP263-4 RAYTHEON TECHNICAL SERVICES COMPANY (36378)

POSSIBLE

INSULATION SLEEVING,ELECTRICAL,S

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.

  • SM-C-679703 — US Army CECOM (SM- / SC- / A3 drawings) (specification · not yet a document in the graph)
  • SM-C-679703-9 — US Army CECOM (SM- / SC- / A3 drawings) (specification · not yet a document in the graph)

Historical & informational references

Numbers the catalogue records against this item but marks as not for procurement — withdrawn entries, information-only listings, drawings, and references that need more than the number to identify the item. If you arrived holding one of these, this is the item it points to; the sources above are what can actually be used.

202A153-3 TE CONNECTIVITY CORPORATION (06090)

WITHDRAWN

INSULATION SLEEVING,ELECTRICAL,S

no longer valid — this reference was withdrawn from the catalogue record (RNVC 9) — the history trail: hold it, do not buy to it

313H264-1 3M CO ADMININISTRATIVE ELECTRONIC & (20999)

WITHDRAWN

INSULATION SLEEVING,ELECTRICAL,S

no longer valid — this reference was withdrawn from the catalogue record (RNVC 9) — the history trail: hold it, do not buy to it

SC5975-0024-5 DRS ICAS, LLC DBA (12115)

WITHDRAWN

INSULATION SLEEVING,ELECTRICAL,S

no longer valid — this reference was withdrawn from the catalogue record (RNVC 9) — the history trail: hold it, do not buy to it

Substitutes — other stock numbers

Codified interchangeability across stock numbers (FLIS I&S), with the catalogue's order of use where it states one.

114E3040-5 THE BOEING COMPANY

CONFIRMED

OEM source-control number — the OEM’s own reference for this item; the other members are its approved sources per codification. All of this OEM’s references →

INSULATION SLEEVING,ELECTRICAL,S

NSN 5970-00-122-5429

MAIN BODY OVERALL LENGTH: 1.750 INCHES MINIMUM AS SUPPLIED MAIN BODY LARGE END INSIDE DIAMETER: 1.500 INCHES MINIMUM AS SUPPLIED

202K153-3-01 TE CONNECTIVITY CORPORATION

CONFIRMED

INSULATION SLEEVING,ELECTRICAL,S

NSN 5970-01-086-6575

MAIN BODY OVERALL LENGTH: 3.140 INCHES NOMINAL AFTER UNRESTRICTED RECOVERY MAIN BODY WALL THICKNESS: 0.080 INCHES NOMINAL AFTER UNRESTRICTED RECOVERY MAIN BODY SMALL END INSIDE DIAMETER: 1.420 INCHES MINIMUM AS SUPPLIED · 0.330 INCHES MAXIMUM AFTER UNRESTRICTED RECOVERY MAIN BODY LARGE END INSIDE DIAMETER: 1.420 INCHES MINIMUM AS SUPPLIED · 0.880 INCHES MAXIMUM AFTER UNRESTRICTED RECOVERY

HS1-202D153-4 NATIONAL STARCH AND CHEMICAL CO

CONFIRMED

INSULATION SLEEVING,ELECTRICAL,S

NSN 5970-00-828-3452

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.

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).