Consumables & expendables · Spec-Crosswalk

ASTM D2000

ASTM ASTM D2000

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.

0011830 LAKE SHORE SYSTEMS, INC.

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 8040-01-656-7830 →COLOR: BLACK MATERIAL: RUBBER STYRENE MATERIAL DOCUMENT AND CLASSIFICATION: ASTM-D-2000 ASSN STD SINGLE MATERIAL RESPONSE MINIMUM FLASH POINT: -14.0 DEG FAHRENHEIT

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

10900472 U S ARMY TANK AUTOMOTIVE COMMAND

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 9390-00-166-0254 →OVERALL WIDTH: 0.500 INCHES NOMINAL LENGTH: 34.000 INCHES NOMINAL LEFT SIDE FLANGE THICKNESS: 0.125 INCHES NOMINAL RIGHT SIDE FLANGE THICKNESS: 0.125 INCHES NOMINAL

FLIS · DLA Logistics Information Services (FLIS)

114S6901-23 THE BOEING COMPANY

CONFIRMED

Codified interchangeability (FLIS I&S)

qualified at 2 sites: THE BOEING COMPANY · 81205

NSN 9390-00-763-6908 →no stated characteristics

FLIS · DLA Logistics Information Services (FLIS)

3011526 GARWOOD/FELLER INC GARWOOD WINCH DIV

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 9390-00-166-0254 →OVERALL WIDTH: 0.500 INCHES NOMINAL LENGTH: 34.000 INCHES NOMINAL LEFT SIDE FLANGE THICKNESS: 0.125 INCHES NOMINAL RIGHT SIDE FLANGE THICKNESS: 0.125 INCHES NOMINAL

FLIS · DLA Logistics Information Services (FLIS)

4799 3M COMPANY

CONFIRMED

Codified interchangeability (FLIS I&S)

qualified at 2 sites: 1A9T3 · 76381

NSN 8040-01-656-7830 →COLOR: BLACK MATERIAL: RUBBER STYRENE MATERIAL DOCUMENT AND CLASSIFICATION: ASTM-D-2000 ASSN STD SINGLE MATERIAL RESPONSE MINIMUM FLASH POINT: -14.0 DEG FAHRENHEIT

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

7000000926 3M COMPANY

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 8040-01-656-7830 →COLOR: BLACK MATERIAL: RUBBER STYRENE MATERIAL DOCUMENT AND CLASSIFICATION: ASTM-D-2000 ASSN STD SINGLE MATERIAL RESPONSE MINIMUM FLASH POINT: -14.0 DEG FAHRENHEIT

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

7181003 MB DYNAMICS, INC.

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 9320-01-117-1803 →no stated characteristics

FLIS · DLA Logistics Information Services (FLIS)

728951 L3HARRIS CINCINNATI ELECTRONICS

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 9390-00-515-3337 →no stated characteristics

FLIS · DLA Logistics Information Services (FLIS)

8610K93 MCMASTER-CARR SUPPLY CO

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 9320-01-659-2980 →WIDTH: 12.0 INCHES NOMINAL LENGTH: 12.0 INCHES NOMINAL THICKNESS: 0.125 INCHES NOMINAL MATERIAL: NEOPRENE LOCATION NOT OTHERWISE SPECIFIED

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

ASTM-D2000 ZF INDUSTRIEANTRIEBE WITTEN GMBH

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 9320-00-551-3141 →WIDTH: 12.000 INCHES NOMINAL LENGTH: 12.000 INCHES NOMINAL THICKNESS: 1.000 INCHES NOMINAL COLOR: BLACK BOTH SIDES

FLIS · DLA Logistics Information Services (FLIS) · 2026-07

BAC1521-73 THE BOEING COMPANY

CONFIRMED

Codified interchangeability (FLIS I&S)

qualified at 2 sites: 82918 · THE BOEING COMPANY

NSN 9390-00-250-0804 →OVERALL WIDTH: 0.630 INCHES NOMINAL APERTURE WIDTH: 0.240 INCHES NOMINAL BASE FLANGE THICKNESS: 0.050 INCHES NOMINAL OVERALL HEIGHT: 0.280 INCHES NOMINAL

FLIS · DLA Logistics Information Services (FLIS)

F050212 REV C ITEM NO 7 LAKE SHORE SYSTEMS, INC.

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 8040-01-656-7830 →COLOR: BLACK MATERIAL: RUBBER STYRENE MATERIAL DOCUMENT AND CLASSIFICATION: ASTM-D-2000 ASSN STD SINGLE MATERIAL RESPONSE MINIMUM FLASH POINT: -14.0 DEG FAHRENHEIT

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

MILC3432 ZF INDUSTRIEANTRIEBE WITTEN GMBH

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 9390-00-515-3337 →no stated characteristics

FLIS · DLA Logistics Information Services (FLIS)

NA2-4043 THE BOEING COMPANY

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 9320-00-202-1631 →WIDTH: 36.000 INCHES NOMINAL LENGTH: 36.000 INCHES NOMINAL THICKNESS: 0.031 INCHES NOMINAL MATERIAL: RUBBER LOCATION NOT OTHERWISE SPECIFIED
NSN 9330-01-361-7458 →WIDTH: 2.000 INCHES NOMINAL LENGTH: 12.000 INCHES NOMINAL THICKNESS: 0.0025 INCHES MINIMUM AND 0.0035 INCHES MAXIMUM COLOR: BLACK BOTH SIDES
NSN 9330-01-397-2802 →WIDTH: 1.300 INCHES NOMINAL LENGTH: 3.300 INCHES NOMINAL THICKNESS: 0.005 INCHES NOMINAL COLOR: WHITE, FED STD 595, 17875
NSN 9330-01-397-2803 →WIDTH: 1.300 INCHES NOMINAL LENGTH: 3.300 INCHES NOMINAL THICKNESS: 0.005 INCHES NOMINAL COLOR: YELLOW, FED STD 595, 13538
NSN 9330-01-422-9101 →WIDTH: 36.000 INCHES NOMINAL LENGTH: 36.000 INCHES NOMINAL THICKNESS: 0.003 INCHES NOMINAL COLOR: ALUMINUM
NSN 9330-01-422-9104 →WIDTH: 36.000 INCHES NOMINAL LENGTH: 36.000 INCHES NOMINAL THICKNESS: 0.003 INCHES NOMINAL COLOR: WHITE, FED STD 595, 17875

+375 more NSNs held — contact atas.aero for a breakdown

CAGE_MPN 81349 ASTMD2000 CAGE_MPN 82918 3293 CAGE_MPN 81349 MIL-P-38477 CAGE_MPN 14153 P00345NRP CAGE_MPN 81343 AMS-R-6130A CAGE_MPN 81349 MILR6130TY1GRBSOFT2-500 CAGE_MPN 81349 MILR6130TY2GRCSOFT +159 more held — contact atas.aero for a breakdown

FLIS · DLA Logistics Information Services (FLIS)

VS80538-1 THE BOEING COMPANY

CONFIRMED

Codified interchangeability (FLIS I&S)

qualified at 2 sites: 81205 · THE BOEING COMPANY

NSN 9390-00-763-6908 →no stated characteristics

FLIS · DLA Logistics Information Services (FLIS)

X-102 ZF INDUSTRIEANTRIEBE WITTEN GMBH

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 9390-00-515-3337 →no stated characteristics

FLIS · DLA Logistics Information Services (FLIS)

X102 ATLANTIC INDIA RUBBER CO, INC

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 9390-00-515-3337 →no stated characteristics
NSN 9390-00-640-9580 →no stated characteristics

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).