222K152-25 TE CONNECTIVITY CORPORATION (06090)
CONFIRMEDINSULATION SLEEVING,ELECTRICAL,S
design-control reference — the reference that controls this item of supply (RNCC 3 · RNVC 2)
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 numbernone recorded
You are here · Stock number5970-01-173-1845
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.
1103-4G2 HELLERMANNTYTON (F3341)
POSSIBLEINSULATION SLEEVING,ELECTRICAL,S
secondary reference — also codified against this stock number, as a secondary reference (RNCC 5)
1156-4-B7 HELLERMANNTYTON (F3341)
POSSIBLEINSULATION SLEEVING,ELECTRICAL,S
secondary reference — also codified against this stock number, as a secondary reference (RNCC 5)
222K152-25 TYCO ELECTRONICS FRANCE SAS (F0286)
POSSIBLEINSULATION SLEEVING,ELECTRICAL,S
secondary reference — also codified against this stock number, as a secondary reference (RNCC 5)
72392 GDI SIMULATION (F2181)
POSSIBLEINSULATION SLEEVING,ELECTRICAL,S
secondary reference — also codified against this stock number, as a secondary reference (RNCC 5)
ME2005599 ALFARIVER DEFENSE S.L (9331B)
POSSIBLEINSULATION SLEEVING,ELECTRICAL,S
secondary reference — also codified against this stock number, as a secondary reference (RNCC 5)
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Numbers the catalogue records against this item but marks as not for procurement — withdrawn entries, information-only listings, drawings, and references that need more than the number to identify the item.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.
222K152-25 RAYCHEM SA (F6220)
WITHDRAWNINSULATION 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no longer valid — this reference was withdrawn from the catalogue record (RNVC 9) — the history trail: hold it, do not buy to it
Stated characteristics
The codification record's own dimensions and material statements — official, and public by nature.
TEMP RATING125.0 CELSIUSFLIS characteristics (MRC)
ENVIRONMENTAL PROTECTIONCORROSION RESISTANT AND MILDEW RESISTANT AND OIL RESISTANT AND WATER RESISTANTFLIS characteristics (MRC)
LARGE END WALL THICKNESS OF MAIN BODY0.070 INCHES NOMINAL AFTER UNRESTRICTED RECOVERYFLIS characteristics (MRC)
SMALL END WALL THICKNESS OF MAIN BODY0.040 INCHES NOMINAL AFTER UNRESTRICTED RECOVERYFLIS characteristics (MRC)
DISTANCE FROM INTERSECTING CENTERLINES TO EDGE OF SMALL END1.810 INCHES NOMINAL AFTER UNRESTRICTED RECOVERYFLIS characteristics (MRC)
DISTANCE FROM CENTERLINE OF SMALL END TO EDGE OF LARGE END1.020 INCHES NOMINAL AFTER UNRESTRICTED RECOVERYFLIS characteristics (MRC)
MAIN BODY SMALL END INSIDE DIAMETER1.420 INCHES MINIMUM AS SUPPLIED · 0.330 INCHES MAXIMUM AFTER UNRESTRICTED RECOVERYFLIS characteristics (MRC)
MAIN BODY LARGE END INSIDE DIAMETER0.880 INCHES MAXIMUM AFTER UNRESTRICTED RECOVERY · 1.420 INCHES MINIMUM AS SUPPLIEDFLIS characteristics (MRC)
DISTANCE FROM TOP OF SHOULDER TO SMALL END OF MAIN BODY0.590 INCHES NOMINAL AFTER UNRESTRICTED RECOVERYFLIS characteristics (MRC)
ANGLE BETWEEN LARGE END AND SMALL END CENTERLINES IN DEG90.0 NOMINAL AFTER UNRESTRICTED RECOVERYFLIS characteristics (MRC)
MINIMUM TENSILE STRENGTH2800 POUNDS PER SQUARE INCHFLIS characteristics (MRC)
FLEXIBILITYFLEXIBLEFLIS characteristics (MRC)
HEIGHT1.500 INCHES NOMINAL AFTER UNRESTRICTED RECOVERYFLIS characteristics (MRC)
COLORBLACKFLIS characteristics (MRC)
MATERIALPLASTIC POLYVINYL CHLORIDE (PVC) OR PLASTIC POLYVINYL CHLORIDE-ACETATE LOCATION NOT OTHERWISE SPECIFIEDFLIS characteristics (MRC)
MATERIAL DOCUMENT AND CLASSIFICATIONMIL-I-7444 MIL SPEC ALL MATERIAL RESPONSES LOCATION NOT OTHERWISE SPECIFIEDFLIS characteristics (MRC)
STYLE DESIGNATORBOOT-90 DEGREESFLIS characteristics (MRC)
DIELECTRIC MATERIAL VOLTAGE RATING PER UNIT THICKNESS220.0 VOLTS PER MIL /0.001 INCH/FLIS characteristics (MRC)
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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).