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Consumables & expendables · Spec-Crosswalk

INSULATION SLEEVING,ELECTRICAL

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 numbernone recorded
You are here · Stock number5970-00-761-2953
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.

5M388T2 THE BOEING COMPANY (76301)

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

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

558011-15 ELDEC AEROSPACE CORP (08748)

POSSIBLE

INSULATION SLEEVING,ELECTRICAL

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

596C28-1002 CARDWELL CONDENSER CORP (94033)

POSSIBLE

INSULATION SLEEVING,ELECTRICAL

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

6L1115-288 LOCKHEED MARTIN CORPORATION (60854)

POSSIBLE

INSULATION SLEEVING,ELECTRICAL

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

77C717314-2 LOCKHEED MARTIN CORPORATION (03538)

POSSIBLE

INSULATION SLEEVING,ELECTRICAL

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

691C731P21 BAE SYSTEMS CONTROLS INC. (89954)

POSSIBLE

INSULATION SLEEVING,ELECTRICAL

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

C101108201 KEARFOTT CORPORATION (88818)

POSSIBLE

INSULATION SLEEVING,ELECTRICAL

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

FLXTETW28-10 MARKEL CORP. (03890)

POSSIBLE

INSULATION SLEEVING,ELECTRICAL

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

PF28LWNAT SAINT-GOBAIN PERFORMANCE PLASTICS (09795)

POSSIBLE

INSULATION SLEEVING,ELECTRICAL

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

S12573-28 TRELLEBORG SEALING SOLUTIONS US, IN (09257)

POSSIBLE

INSULATION SLEEVING,ELECTRICAL

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

TU-150 GRIMES AEROSPACE COMPANY (72914)

POSSIBLE

INSULATION SLEEVING,ELECTRICAL

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.

  • M22129-28-N — Military Specifications (specification · not yet a document in the graph)
  • MIL-I-22129 — Military Specifications

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.

6L1115-288 LOCKHEED MARTIN CORPORATION (11530)

WITHDRAWN

INSULATION SLEEVING,ELECTRICAL

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

Y00030-002 BAE SYSTEMS INFORMATION AND ELECTRO (12436)

WITHDRAWN

INSULATION SLEEVING,ELECTRICAL

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

Stated characteristics

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

WALL THICKNESS0.009 INCHES NOMINALFLIS characteristics (MRC)
DIELECTRIC WITHSTANDING VOLTAGE IN VOLTS11500.0FLIS characteristics (MRC)
RELIABILITY INDICATORNOT ESTABLISHEDFLIS characteristics (MRC)
INSIDE DIAMETER0.013 INCHES MINIMUM AND 0.019 INCHES MAXIMUMFLIS characteristics (MRC)
TEMP RATING275.0 CELSIUSFLIS characteristics (MRC)
FLEXIBILITYFLEXIBLEFLIS characteristics (MRC)
COLORNATURALFLIS characteristics (MRC)
STYLE DESIGNATORNONSHRINKABLEFLIS characteristics (MRC)
NONDEFINITIVE SPEC/STD DATA28AWG SIZEFLIS 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.

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) · 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).