Consumables & expendables · Spec-Crosswalk

MIL-I-7444

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-I-7444

The same document's other types, classes and grades — each its own crosswalk family.

MIL-I-7444 Type 1 Class 1 3 qualified products
MIL-I-7444 Type 11 1 qualified product
MIL-I-7444 Type I Class 1 no members yet

277 members, grouped by the makers' own part-number structure — open a family to see its graded, cited rows.

5M388A12 THE BOEING COMPANY

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 5970-00-542-7120 →	WALL THICKNESS: 0.013 INCHES MINIMUM AND 0.019 INCHES MAXIMUM DIELECTRIC MATERIAL VOLTAGE RATING PER UNIT THICKNESS: 750.0 VOLTS PER MIL /0.001 INCH/ INSIDE DIAMETER: 0.064 INCHES MINIMUM AND 0.072 INCHES MAXIMUM COLOR: CLEAR

FLIS · DLA Logistics Information Services (FLIS)

17 I1725-96 U S ARMY TANK AUTOMOTIVE COMMAND

CONFIRMED

Codified interchangeability (FLIS I&S)

FLIS · DLA Logistics Information Services (FLIS)

17-I-1725-56 U S ARMY TANK AUTOMOTIVE COMMAND

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 5970-00-296-6078 →	WALL THICKNESS: 0.017 INCHES MINIMUM AND 0.023 INCHES MAXIMUM DIELECTRIC MATERIAL VOLTAGE RATING PER UNIT THICKNESS: 650.0 VOLTS PER MIL /0.001 INCH/ INSIDE DIAMETER: 0.144 INCHES MINIMUM AND 0.158 INCHES MAXIMUM COLOR: CLEAR

FLIS · DLA Logistics Information Services (FLIS)

17-I-1726-76 U S ARMY TANK AUTOMOTIVE COMMAND

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 5970-00-577-1629 →	WALL THICKNESS: 0.017 INCHES MINIMUM AND 0.023 INCHES MAXIMUM DIELECTRIC MATERIAL VOLTAGE RATING PER UNIT THICKNESS: 650.0 VOLTS PER MIL /0.001 INCH/ INSIDE DIAMETER: 0.258 INCHES MINIMUM AND 0.278 INCHES MAXIMUM COLOR: CLEAR

FLIS · DLA Logistics Information Services (FLIS)

17-I-1728-131 U S ARMY TANK AUTOMOTIVE COMMAND

CONFIRMED

Codified interchangeability (FLIS I&S)

FLIS · DLA Logistics Information Services (FLIS)

19-266197-3-05-4 GENERAL DYNAMICS MISSION SYSTEMS, I

CONFIRMED

Codified interchangeability (FLIS I&S)

FLIS · DLA Logistics Information Services (FLIS)

71+452792+10S AMPHENOL CORP

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 5970-00-729-2507 →	WALL THICKNESS: 0.017 INCHES MINIMUM AND 0.023 INCHES MAXIMUM DIELECTRIC MATERIAL VOLTAGE RATING PER UNIT THICKNESS: 200.0 VOLTS PER MIL /0.001 INCH/ INSIDE DIAMETER: 0.229 INCHES MINIMUM AND 0.249 INCHES MAXIMUM COLOR: BLACK

FLIS · DLA Logistics Information Services (FLIS)

85T4-5 BELL TEXTRON INC

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 5970-00-263-1325 →	no stated characteristics

FLIS · DLA Logistics Information Services (FLIS)

91+538139+46T AMPHENOL CORP

CONFIRMED

Codified interchangeability (FLIS I&S)

FLIS · DLA Logistics Information Services (FLIS)

152-1757-00 ROCKWELL COLLINS, INC.

CONFIRMED

Codified interchangeability (FLIS I&S)

FLIS · DLA Logistics Information Services (FLIS)

152-4188-000 ROCKWELL COLLINS, INC.

CONFIRMED

Codified interchangeability (FLIS I&S)

FLIS · DLA Logistics Information Services (FLIS)

152-4204-000 ROCKWELL COLLINS, INC.

CONFIRMED

Codified interchangeability (FLIS I&S)

FLIS · DLA Logistics Information Services (FLIS)

152-41990-00 ROCKWELL COLLINS, INC.

CONFIRMED

Codified interchangeability (FLIS I&S)

FLIS · DLA Logistics Information Services (FLIS)

204-41636-2 THE BOEING COMPANY

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 5970-00-729-5381 →	WALL THICKNESS: 0.017 INCHES MINIMUM AND 0.023 INCHES MAXIMUM DIELECTRIC MATERIAL VOLTAGE RATING PER UNIT THICKNESS: 200.0 VOLTS PER MIL /0.001 INCH/ INSIDE DIAMETER: 0.258 INCHES MINIMUM AND 0.275 INCHES MAXIMUM COLOR: BLACK

FLIS · DLA Logistics Information Services (FLIS)

206-1-G HELLERMANNTYTON LTD

CONFIRMED

Codified interchangeability (FLIS I&S)

qualified at 2 sites: HELLERMANNTYTON LTD · HELLERMANNTYTON LIMITED

NSN 5970-01-173-1846 →	no stated characteristics

FLIS · DLA Logistics Information Services (FLIS) · 2026-08

218-1426 RS COMPONENTS SAS

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 5970-01-173-1846 →	no stated characteristics

FLIS · DLA Logistics Information Services (FLIS) · 2026-08

222K152-25 — 3 members

222K152-25 TE CONNECTIVITY CORPORATION

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 5970-01-173-1845 →	no stated characteristics

FLIS · DLA Logistics Information Services (FLIS) · 2026-08

222K152-25 TYCO ELECTRONICS FRANCE SAS

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 5970-01-173-1845 →	no stated characteristics

FLIS · DLA Logistics Information Services (FLIS) · 2026-08

222K152-25 RAYCHEM SA

CONFIRMED

Codified interchangeability (FLIS I&S)

FLIS · DLA Logistics Information Services (FLIS) · 2026-08

267-10006P11 RAYTHEON COMPANY

CONFIRMED

Codified interchangeability (FLIS I&S)

qualified at 2 sites: RAYTHEON COMPANY · RAYTHEON COMPANY

FLIS · DLA Logistics Information Services (FLIS)

382A012-25 TE CONNECTIVITY CORPORATION

CONFIRMED

Codified interchangeability (FLIS I&S)

FLIS · DLA Logistics Information Services (FLIS) · 2026-08

382A012-25-0 TYCO ELECTRONICS FRANCE SAS

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 5970-01-173-1846 →	no stated characteristics

FLIS · DLA Logistics Information Services (FLIS) · 2026-08

382A012-25-0 RAYCHEM SA

CONFIRMED

Codified interchangeability (FLIS I&S)

FLIS · DLA Logistics Information Services (FLIS) · 2026-08

493H123-7 3M CO ADMININISTRATIVE ELECTRONIC &

CONFIRMED

Codified interchangeability (FLIS I&S)

FLIS · DLA Logistics Information Services (FLIS) · 2026-08

1103-4G2 HELLERMANNTYTON

CONFIRMED

Codified interchangeability (FLIS I&S)

FLIS · DLA Logistics Information Services (FLIS) · 2026-08

1156-4-B7 HELLERMANNTYTON

CONFIRMED

Codified interchangeability (FLIS I&S)

FLIS · DLA Logistics Information Services (FLIS) · 2026-08

2219 THE BOEING COMPANY

CONFIRMED

Codified interchangeability (FLIS I&S)

FLIS · DLA Logistics Information Services (FLIS)

limit reached — 209 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).