Consumables & expendables · Spec-Crosswalk

MIL-I-22129

MIL MIL-I-22129

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

1A8082-1 GE AVIATION SYSTEMS LLC

CONFIRMED

Codified interchangeability (FLIS I&S)

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

3/16INSPIRAL CUT TFE TUBING NMC GROUP INC

CONFIRMED

Codified interchangeability (FLIS I&S)

FLIS · DLA Logistics Information Services (FLIS)

4-00124-002 ARMA DIV

CONFIRMED

Codified interchangeability (FLIS I&S)

FLIS · DLA Logistics Information Services (FLIS)

4-00124-009 ARMA DIV

CONFIRMED

Codified interchangeability (FLIS I&S)

FLIS · DLA Logistics Information Services (FLIS)

4-00124-110 ARMA DIV

CONFIRMED

Codified interchangeability (FLIS I&S)

FLIS · DLA Logistics Information Services (FLIS)

4-00124-310 ARMA DIV

CONFIRMED

Codified interchangeability (FLIS I&S)

FLIS · DLA Logistics Information Services (FLIS)

5M388T2 THE BOEING COMPANY

CONFIRMED

Codified interchangeability (FLIS I&S)

FLIS · DLA Logistics Information Services (FLIS)

5M388T8 THE BOEING COMPANY

CONFIRMED

Codified interchangeability (FLIS I&S)

FLIS · DLA Logistics Information Services (FLIS)

5M388T14 THE BOEING COMPANY

CONFIRMED

Codified interchangeability (FLIS I&S)

FLIS · DLA Logistics Information Services (FLIS)

5M388T15 THE BOEING COMPANY

CONFIRMED

Codified interchangeability (FLIS I&S)

FLIS · DLA Logistics Information Services (FLIS)

5M388T16 THE BOEING COMPANY

CONFIRMED

Codified interchangeability (FLIS I&S)

FLIS · DLA Logistics Information Services (FLIS)

5M388T18 THE BOEING COMPANY

CONFIRMED

Codified interchangeability (FLIS I&S)

FLIS · DLA Logistics Information Services (FLIS)

6L1115-269 LOCKHEED MARTIN CORPORATION

CONFIRMED

Codified interchangeability (FLIS I&S)

qualified at 2 sites: 60854 · 11530

NSN 5970-00-964-3457 →WALL THICKNESS: 0.007 INCHES MINIMUM AND 0.011 INCHES MAXIMUM INSIDE DIAMETER: 0.016 INCHES MINIMUM AND 0.022 INCHES MAXIMUM COLOR: WHITE

FLIS · DLA Logistics Information Services (FLIS)

6L1115-288 LOCKHEED MARTIN CORPORATION

CONFIRMED

Codified interchangeability (FLIS I&S)

qualified at 2 sites: LOCKHEED MARTIN CORPORATION · LOCKHEED MARTIN CORPORATION

FLIS · DLA Logistics Information Services (FLIS)

18 STANDARD PTI BLACK SAINT-GOBAIN PERFORMANCE PLASTICS

CONFIRMED

Codified interchangeability (FLIS I&S)

FLIS · DLA Logistics Information Services (FLIS)

18AWG042IDX012WALL SIGMA TEK, INC. DBA

CONFIRMED

Codified interchangeability (FLIS I&S)

FLIS · DLA Logistics Information Services (FLIS)

24 LWTFEBLACK ZEUS INDUSTRIAL PRODUCTS, INC

CONFIRMED

Codified interchangeability (FLIS I&S)

FLIS · DLA Logistics Information Services (FLIS)

45-033300-02 NORTHROP GRUMMAN SYSTEMS CORPORATIO

CONFIRMED

Codified interchangeability (FLIS I&S)

qualified at 2 sites: NORTHROP GRUMMAN SYSTEMS CORPORATIO · NORTHROP GRUMMAN SYSTEMS

FLIS · DLA Logistics Information Services (FLIS)

45-033300-05 NORTHROP GRUMMAN SYSTEMS CORPORATIO

CONFIRMED

Codified interchangeability (FLIS I&S)

qualified at 2 sites: 26916 · NORTHROP GRUMMAN SYSTEMS

FLIS · DLA Logistics Information Services (FLIS)

45-033300-07 NORTHROP GRUMMAN SYSTEMS

CONFIRMED

Codified interchangeability (FLIS I&S)

qualified at 2 sites: 15280 · NORTHROP GRUMMAN SYSTEMS CORPORATIO

NSN 5970-00-846-5906 →WALL THICKNESS: 0.016 INCHES NOMINAL INSIDE DIAMETER: 0.081 INCHES MINIMUM AND 0.091 INCHES MAXIMUM COLOR: NATURAL

FLIS · DLA Logistics Information Services (FLIS)

45-033300-08 NORTHROP GRUMMAN SYSTEMS

CONFIRMED

Codified interchangeability (FLIS I&S)

qualified at 2 sites: NORTHROP GRUMMAN SYSTEMS · NORTHROP GRUMMAN SYSTEMS CORPORATIO

NSN 5970-00-892-0967 →no stated characteristics

FLIS · DLA Logistics Information Services (FLIS)

45-033300-09 NORTHROP GRUMMAN SYSTEMS

CONFIRMED

Codified interchangeability (FLIS I&S)

qualified at 2 sites: NORTHROP GRUMMAN SYSTEMS · NORTHROP GRUMMAN SYSTEMS CORPORATIO

NSN 5970-00-837-0648 →WALL THICKNESS: 0.020 INCHES NOMINAL INSIDE DIAMETER: 0.129 INCHES MINIMUM AND 0.141 INCHES MAXIMUM COLOR: NATURAL

FLIS · DLA Logistics Information Services (FLIS)

77C717314-2 LOCKHEED MARTIN CORPORATION

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 5970-00-761-2953 →WALL THICKNESS: 0.009 INCHES NOMINAL INSIDE DIAMETER: 0.013 INCHES MINIMUM AND 0.019 INCHES MAXIMUM COLOR: NATURAL

FLIS · DLA Logistics Information Services (FLIS)

77C717314-6 LOCKHEED MARTIN CORPORATION

CONFIRMED

Codified interchangeability (FLIS I&S)

FLIS · DLA Logistics Information Services (FLIS)

limit reached — 385 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).

  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).