11732492-2 U S ARMY ARMAMENT RESEARCH &
CONFIRMEDCodified interchangeability (FLIS I&S)
FLIS · DLA Logistics Information Services (FLIS) · 2026-09
Consumables & expendables · Spec-Crosswalk
MIL-STD-670 Type T Grade TE-12
MIL MIL-STD-670 · T · TE-12
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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Other lines of MIL MIL-STD-670
The same document's other types, classes and grades — each its own crosswalk family.
- MIL-STD-670 Type T Grade TE12A4F3 9 qualified products
- MIL-STD-670 Grade SBE7 8 qualified products
- MIL-STD-670 Type S Class SC Grade SCE3 5 qualified products
- MIL-STD-670 Type S Class SC Grade SCE7 4 qualified products
- MIL-STD-670 Type S Class SC Grade SCO7 4 qualified products
- MIL-STD-670 3 qualified products
- MIL-STD-670 Type R Grade RE3LZ 3 qualified products
- MIL-STD-670 Type R Grade RO7 3 qualified products
- MIL-STD-670 Type S Class SC Grade SCE3F 3 qualified products
- MIL-STD-670 Grade RE3LK2 2 qualified products
- MIL-STD-670 Grade RO3 2 qualified products
- MIL-STD-670 Grade RO3F1L 2 qualified products
217-4642008IT6-13 NAVAL SHIP SYSTEMS COMMAND
CONFIRMEDCodified interchangeability (FLIS I&S)
| NSN 9320-00-003-5428 → | WIDTH: 36.000 INCHES NOMINAL LENGTH: 36.000 INCHES NOMINAL THICKNESS: 0.094 INCHES NOMINAL MATERIAL: RUBBER CHLOROPRENE CLASS CR LOCATION NOT OTHERWISE SPECIFIED |
|---|---|
| NSN 9320-00-003-5432 → | WIDTH: 36.000 INCHES NOMINAL LENGTH: 36.000 INCHES NOMINAL THICKNESS: 0.062 INCHES NOMINAL MATERIAL: RUBBER CHLOROPRENE CLASS CR LOCATION NOT OTHERWISE SPECIFIED |
| NSN 9320-00-007-1317 → | CROSS-SECTIONAL WIDTH: 0.062 INCHES NOMINAL LENGTH: 50.000 INCHES NOMINAL MATERIAL: RUBBER BUTADIENE-STYRENE CLASS SBR OR RUBBER POLYISOPRENE NATURAL CLASS NR MATERIAL DOCUMENT AND CLASSIFICATION: MIL-STD-670, TYPE R, STYLE E, GRADE RE3L MIL SPEC SINGLE MATERIAL RESPONSE |
| NSN 9320-00-009-0213 → | WIDTH: 36.000 INCHES NOMINAL LENGTH: 60.000 INCHES NOMINAL THICKNESS: 0.250 INCHES NOMINAL MATERIAL: RUBBER ISOBUTYLENE-ISOPRENE CLASS IIR |
| NSN 9320-00-010-3985 → | CROSS-SECTIONAL WIDTH: 0.219 INCHES MINIMUM AND 0.281 INCHES MAXIMUM LENGTH: 7.719 INCHES MINIMUM AND 7.781 INCHES MAXIMUM COLOR: BLACK BOTH SIDES MATERIAL: RUBBER SYNTHETIC STRENGTHENING FEATURE |
| NSN 9320-00-012-3481 → | WIDTH: 36.000 INCHES NOMINAL LENGTH: 72.000 INCHES NOMINAL THICKNESS: 0.060 INCHES NOMINAL MATERIAL: RUBBER ISOBUTYLENE-ISOPRENE CLASS IIR |
+594 more NSNs held — contact atas.aero for a breakdown
CAGE_MPN 81349 MILR3065 CAGE_MPN 81349 MILC3133 CAGE_MPN 19207 7739090 CAGE_MPN 81346 ASTM-D1056 CAGE_MPN 81349 MIL-R-6130 CAGE_MPN 81349 MIL-R-6855 +188 more held — contact atas.aero for a breakdown
FLIS · DLA Logistics Information Services (FLIS) · 2026-09
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).