6747002 SYSTEMS PROTECTION GROUP US LLC (81851)
CONFIRMEDSLEEVING,TEXTILE,ELECTRICAL
design-control reference — the reference that controls this item of supply (RNCC 3 · RNVC 2)
Consumables & expendables · Spec-Crosswalk
SLEEVING,TEXTILE,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 number5970-01-446-1510
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.
Stated characteristics
The codification record's own dimensions and material statements — official, and public by nature.
WALL THICKNESS0.015 INCHES NOMINALFLIS characteristics (MRC)
INSIDE DIAMETER0.125 INCHES NOMINALFLIS characteristics (MRC)
OVERALL LENGTH2000.000 FEET NOMINALFLIS characteristics (MRC)
TEMP RATING150.0 CELSIUSFLIS characteristics (MRC)
ENVIRONMENTAL PROTECTIONMILDEW RESISTANT AND WATER RESISTANT AND OIL RESISTANT AND FLAME RESISTANT AND CORROSION RESISTANTFLIS characteristics (MRC)
END ITEM IDENTIFICATIONCOAST GUARD HH65A HELICOPTERSFLIS characteristics (MRC)
MINIMUM TENSILE STRENGTH38000 POUNDS PER SQUARE INCHFLIS characteristics (MRC)
SPECIAL FEATURESTHIS ITEM IS A LIGHTWEIGHT, SELF-FITTING SLEEVING THAT ADDS TOUGH PHYSICAL PROTECTION OVER WIRES,CABLES, AND HARNESSESFLIS characteristics (MRC)
FLEXIBILITYFLEXIBLEFLIS characteristics (MRC)
COLORBLACKFLIS characteristics (MRC)
MATERIALRUBBER CHLOROPRENE CLASS CR LOCATION NOT OTHERWISE SPECIFIEDFLIS characteristics (MRC)
MATERIAL DOCUMENT AND CLASSIFICATIONMIL-I-23053, CLASS 1 MIL SPEC SINGLE MATERIAL RESPONSEFLIS characteristics (MRC)
STYLE DESIGNATORNONSHRINKABLEFLIS characteristics (MRC)
SUPPLEMENTARY FEATURESBULK PACKAGED IN 2000 FOOT ROLLSFLIS 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) · 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).