Consumables & expendables · Spec-Crosswalk

ASTM B209

ASTM ASTM B209

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.

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001-000215-000 INSITU, INC.

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 9535-01-710-7311 →WIDTH: 1.38 INCHES NOMINAL LENGTH: 3.25 INCHES NOMINAL CROSS-SECTIONAL THICKNESS: 0.38 INCHES NOMINAL PERFORATION DIAMETER: 0.266 INCHES NOMINAL

FLIS · DLA Logistics Information Services (FLIS) · 2026-09

10164303 NIMIKKEISTOKESKUS NCB FINLAND

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 9535-00-232-0387 →WIDTH: 48.000 INCHES NOMINAL LENGTH: 12.000 FEET NOMINAL CROSS-SECTIONAL THICKNESS: 0.0630 INCHES NOMINAL MATERIAL: ALUMINUM ALLOY 6061

FLIS · DLA Logistics Information Services (FLIS)

AMS 4025, 0.063X48X144 DEFENSE LOGISTICS AGENCY DBA

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 9535-00-232-0387 →WIDTH: 48.000 INCHES NOMINAL LENGTH: 12.000 FEET NOMINAL CROSS-SECTIONAL THICKNESS: 0.0630 INCHES NOMINAL MATERIAL: ALUMINUM ALLOY 6061

FLIS · DLA Logistics Information Services (FLIS)

ASTM-B209, ALUM INUM ALLOY-5456 ZF INDUSTRIEANTRIEBE WITTEN GMBH

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 9535-01-352-8661 →WIDTH: 60.000 INCHES NOMINAL LENGTH: 10.000 FEET NOMINAL CROSS-SECTIONAL THICKNESS: 0.3750 INCHES NOMINAL MATERIAL: ALUMINUM ALLOY 5456

FLIS · DLA Logistics Information Services (FLIS)

ASTMB209, 0.063X48X144 DEFENSE LOGISTICS AGENCY DBA

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 9535-00-232-0387 →WIDTH: 48.000 INCHES NOMINAL LENGTH: 12.000 FEET NOMINAL CROSS-SECTIONAL THICKNESS: 0.0630 INCHES NOMINAL MATERIAL: ALUMINUM ALLOY 6061

FLIS · DLA Logistics Information Services (FLIS)

ASTMB209,6061-0 0.032X48X144 AMERICAN SOCIETY FOR TESTING AND

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 9535-01-670-1873 →WIDTH: 48.0 INCHES NOMINAL LENGTH: 144.0 INCHES NOMINAL MATERIAL: ALUMINUM ALLOY 6061

FLIS · DLA Logistics Information Services (FLIS) · 2026-09

QQ-A-250/1-H14,0.090X48X144 DEFENSE LOGISTICS AGENCY DBA

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 9535-00-167-2225 →WIDTH: 48.000 INCHES NOMINAL LENGTH: 12.000 FEET NOMINAL CROSS-SECTIONAL THICKNESS: 0.090 INCHES NOMINAL MATERIAL: ALUMINUM ALLOY 1100

FLIS · DLA Logistics Information Services (FLIS)

QQ-A-250/11-0, 0.063X48X144 DEFENSE LOGISTICS AGENCY DBA

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 9535-00-232-0387 →WIDTH: 48.000 INCHES NOMINAL LENGTH: 12.000 FEET NOMINAL CROSS-SECTIONAL THICKNESS: 0.0630 INCHES NOMINAL MATERIAL: ALUMINUM ALLOY 6061

FLIS · DLA Logistics Information Services (FLIS)

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).

  1. 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.
  2. 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.
  3. 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.
  4. 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.
  5. 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).
  6. 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).