P5382-2-0 LOCKHEED MARTIN CORPORATION (81755)
CONFIRMEDINSULATION SLEEVING,ELECTRICAL
design-control reference — the reference that controls this item of supply (RNCC 3 · RNVC 2)
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 number2 approved sources
You are here · Stock number5970-00-812-2974
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.
MS63-84 3/32IN BLACK TE CONNECTIVITY CORPORATION (06090)
POSSIBLEINSULATION SLEEVING,ELECTRICAL
secondary reference — also codified against this stock number, as a secondary reference (RNCC 5)
Substitutes — other stock numbers
Codified interchangeability across stock numbers (FLIS I&S), with the catalogue's order of use where it states one.
956001032 INDRA SISTEMAS, SOCIEDAD ANONIMA
CONFIRMEDINSULATION SLEEVING,ELECTRICAL
NSN 5970-00-812-2974
MS63-84 3/32IN BLACK TE CONNECTIVITY CORPORATION
CONFIRMEDINSULATION SLEEVING,ELECTRICAL
NSN 5970-01-183-8045
OVERALL LENGTH: 200.000 FEET MINIMUM RECOVERED WALL THICKNESS: 0.020 INCHES NOMINAL DIELECTRIC MATERIAL VOLTAGE RATING PER UNIT THICKNESS: 500.0 VOLTS PER MIL /0.001 INCH/ EXPANDED INSIDE DIAMETER: 0.093 INCHES NOMINAL
Stated characteristics
The codification record's own dimensions and material statements — official, and public by nature.
OVERALL LENGTH200.000 FEET MINIMUMFLIS characteristics (MRC)
TEMP RATING-55.0 CELSIUS AND 135.0 CELSIUSFLIS characteristics (MRC)
EXPANDED INSIDE DIAMETER0.093 INCHES NOMINALFLIS characteristics (MRC)
RECOVERED INSIDE DIAMETER0.046 INCHES NOMINALFLIS characteristics (MRC)
RECOVERED WALL THICKNESS0.020 INCHES NOMINALFLIS characteristics (MRC)
HEAT SHRINKAGE RATING IN PERCENT50.0FLIS characteristics (MRC)
MINIMUM TENSILE STRENGTH1500 POUNDS PER SQUARE INCHFLIS characteristics (MRC)
FLEXIBILITYFLEXIBLEFLIS characteristics (MRC)
COLORBLACKFLIS characteristics (MRC)
MATERIALPLASTIC POLYOLEFINFLIS characteristics (MRC)
STYLE DESIGNATORSHRINKABLEFLIS characteristics (MRC)
DIELECTRIC MATERIAL VOLTAGE RATING PER UNIT THICKNESS500.0 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).