6746-5-1-20BLK ITT AEROSPACE CONTROLS LLC (73760)
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 number5970-00-329-9798
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.
04052573033738 AUTOFLUG GMBH DBA AUTOFLUG (D1131)
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.
6746-5-1-20BLK ITT AEROSPACE CONTROLS LLC
CONFIRMEDINSULATION SLEEVING,ELECTRICAL
NSN 5970-00-329-9798
OVERALL LENGTH: 1.200 INCHES NOMINAL WALL THICKNESS: 0.020 INCHES NOMINAL INSIDE DIAMETER: 0.186 INCHES NOMINAL COLOR: BLACK
FLEXITE HT-105C MARKEL CORP.
CONFIRMEDINSULATION SLEEVING,ELECTRICAL
NSN 5970-00-001-9373
WALL THICKNESS: 0.050 INCHES MINIMUM AND 0.070 INCHES MAXIMUM DIELECTRIC MATERIAL VOLTAGE RATING PER UNIT THICKNESS: 400.0 VOLTS PER MIL /0.001 INCH/ INSIDE DIAMETER: 2.000 INCHES MINIMUM AND 2.070 INCHES MAXIMUM COLOR: BLACK
Stated characteristics
The codification record's own dimensions and material statements — official, and public by nature.
WALL THICKNESS0.020 INCHES NOMINALFLIS characteristics (MRC)
RELIABILITY INDICATORNOT ESTABLISHEDFLIS characteristics (MRC)
INSIDE DIAMETER0.186 INCHES NOMINALFLIS characteristics (MRC)
OVERALL LENGTH1.200 INCHES NOMINALFLIS characteristics (MRC)
TEMP RATING105.0 CELSIUSFLIS characteristics (MRC)
COLORBLACKFLIS characteristics (MRC)
MATERIALPLASTICFLIS characteristics (MRC)
STYLE DESIGNATORNONSHRINKABLEFLIS 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) · 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).