No qualified-products (QPL / ASSIST) export loaded for this specification yet — members below come from codification and manufacturer sources; QPL membership lands with the data cycle.
WALL THICKNESS: 0.017 INCHES MINIMUM AND 0.023 INCHES MAXIMUMDIELECTRIC MATERIAL VOLTAGE RATING PER UNIT THICKNESS: 200.0 VOLTS PER MIL /0.001 INCH/INSIDE DIAMETER: 0.182 INCHES MINIMUM AND 0.198 INCHES MAXIMUMCOLOR: CLEAR
WALL THICKNESS: 0.017 INCHES MINIMUM AND 0.023 INCHES MAXIMUMDIELECTRIC MATERIAL VOLTAGE RATING PER UNIT THICKNESS: 200.0 VOLTS PER MIL /0.001 INCH/INSIDE DIAMETER: 0.258 INCHES MINIMUM AND 0.275 INCHES MAXIMUMCOLOR: BLACK
WALL THICKNESS: 0.017 INCHES MINIMUM AND 0.023 INCHES MAXIMUMDIELECTRIC MATERIAL VOLTAGE RATING PER UNIT THICKNESS: 200.0 VOLTS PER MIL /0.001 INCH/INSIDE DIAMETER: 0.182 INCHES MINIMUM AND 0.198 INCHES MAXIMUMCOLOR: CLEAR
OVERALL LENGTH: 48.000 INCHES NOMINALRECOVERED WALL THICKNESS: 0.034 INCHES MINIMUM AND 0.046 INCHES MAXIMUMDIELECTRIC MATERIAL VOLTAGE RATING PER UNIT THICKNESS: 500.0 VOLTS PER MIL /0.001 INCH/EXPANDED INSIDE DIAMETER: 1.500 INCHES MINIMUM
OVERALL LENGTH: 100.000 FEET MINIMUMWALL THICKNESS: 0.017 INCHES MINIMUM AND 0.023 INCHES MAXIMUMDIELECTRIC MATERIAL VOLTAGE RATING PER UNIT THICKNESS: 200.0 VOLTS PER MIL /0.001 INCH/INSIDE DIAMETER: 0.289 INCHES MINIMUM AND 0.311 INCHES MAXIMUM
WALL THICKNESS: 0.017 INCHES MINIMUM AND 0.023 INCHES MAXIMUMDIELECTRIC MATERIAL VOLTAGE RATING PER UNIT THICKNESS: 200.0 VOLTS PER MIL /0.001 INCH/INSIDE DIAMETER: 0.258 INCHES MINIMUM AND 0.275 INCHES MAXIMUMCOLOR: BLACK
WALL THICKNESS: 0.060 INCHES MINIMUM AND 0.080 INCHES MAXIMUMDIELECTRIC MATERIAL VOLTAGE RATING PER UNIT THICKNESS: 200.0 VOLTS PER MIL /0.001 INCH/INSIDE DIAMETER: 2.500 INCHES MINIMUM AND 2.590 INCHES MAXIMUMCOLOR: BLACK
WALL THICKNESS: 0.022 INCHES MINIMUM AND 0.028 INCHES MAXIMUMDIELECTRIC MATERIAL VOLTAGE RATING PER UNIT THICKNESS: 200.0 VOLTS PER MIL /0.001 INCH/INSIDE DIAMETER: 0.500 INCHES MINIMUM AND 0.524 INCHES MAXIMUMCOLOR: BLACK
WALL THICKNESS: 0.017 INCHES MINIMUM AND 0.023 INCHES MAXIMUMDIELECTRIC MATERIAL VOLTAGE RATING PER UNIT THICKNESS: 200.0 VOLTS PER MIL /0.001 INCH/INSIDE DIAMETER: 0.258 INCHES MINIMUM AND 0.275 INCHES MAXIMUMCOLOR: BLACK
OVERALL LENGTH: 100.000 FEET MINIMUMWALL THICKNESS: 0.017 INCHES MINIMUM AND 0.023 INCHES MAXIMUMDIELECTRIC MATERIAL VOLTAGE RATING PER UNIT THICKNESS: 200.0 VOLTS PER MIL /0.001 INCH/INSIDE DIAMETER: 0.289 INCHES MINIMUM AND 0.311 INCHES MAXIMUM
OVERALL LENGTH: 100.000 FEET MINIMUMWALL THICKNESS: 0.017 INCHES MINIMUM AND 0.023 INCHES MAXIMUMDIELECTRIC MATERIAL VOLTAGE RATING PER UNIT THICKNESS: 200.0 VOLTS PER MIL /0.001 INCH/INSIDE DIAMETER: 0.289 INCHES MINIMUM AND 0.311 INCHES MAXIMUM
WALL THICKNESS: 0.017 INCHES MINIMUM AND 0.023 INCHES MAXIMUMDIELECTRIC MATERIAL VOLTAGE RATING PER UNIT THICKNESS: 200.0 VOLTS PER MIL /0.001 INCH/INSIDE DIAMETER: 0.114 INCHES MINIMUM AND 0.124 INCHES MAXIMUMCOLOR: BLACK
OVERALL LENGTH: 100.000 FEET MINIMUMWALL THICKNESS: 0.013 INCHES MINIMUM AND 0.019 INCHES MAXIMUMDIELECTRIC MATERIAL VOLTAGE RATING PER UNIT THICKNESS: 200.0 VOLTS PER MIL /0.001 INCH/INSIDE DIAMETER: 0.057 INCHES MINIMUM AND 0.067 INCHES MAXIMUM
WALL THICKNESS: 0.017 INCHES MINIMUM AND 0.023 INCHES MAXIMUMDIELECTRIC MATERIAL VOLTAGE RATING PER UNIT THICKNESS: 200.0 VOLTS PER MIL /0.001 INCH/INSIDE DIAMETER: 0.258 INCHES MINIMUM AND 0.275 INCHES MAXIMUMCOLOR: BLACK
OVERALL LENGTH: 48.000 INCHES NOMINALRECOVERED WALL THICKNESS: 0.034 INCHES MINIMUM AND 0.046 INCHES MAXIMUMDIELECTRIC MATERIAL VOLTAGE RATING PER UNIT THICKNESS: 500.0 VOLTS PER MIL /0.001 INCH/EXPANDED INSIDE DIAMETER: 1.500 INCHES MINIMUM
OVERALL LENGTH: 100.000 FEET MINIMUMWALL THICKNESS: 0.013 INCHES MINIMUM AND 0.019 INCHES MAXIMUMDIELECTRIC MATERIAL VOLTAGE RATING PER UNIT THICKNESS: 200.0 VOLTS PER MIL /0.001 INCH/INSIDE DIAMETER: 0.057 INCHES MINIMUM AND 0.067 INCHES MAXIMUM
OVERALL LENGTH: 100.000 FEET MINIMUMWALL THICKNESS: 0.013 INCHES MINIMUM AND 0.019 INCHES MAXIMUMDIELECTRIC MATERIAL VOLTAGE RATING PER UNIT THICKNESS: 200.0 VOLTS PER MIL /0.001 INCH/INSIDE DIAMETER: 0.057 INCHES MINIMUM AND 0.067 INCHES MAXIMUM
FLIS · DLA Logistics Information Services (FLIS)
limit reached — 29 more held · contact atas.aero for a breakdown
Watch this family.
We’ll alert you when its restriction status changes or a new qualified alternative lands.
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.
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).