MILR6855 CL1 GR 40 .665THK ZF INDUSTRIEANTRIEBE WITTEN GMBH
CONFIRMEDCodified interchangeability (FLIS I&S)
| NSN 9320-00-395-2914 → | no stated characteristics |
|---|
FLIS · DLA Logistics Information Services (FLIS) · 2026-07
Consumables & expendables · Spec-Crosswalk
MIL-S-6855 Class 1 Grade 40-CANCELED
MIL MIL-S-6855 · 1 · 40-CANCELED
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-S-6855
The same document's other types, classes and grades — each its own crosswalk family.
- MIL-S-6855 24 qualified products
- MIL-S-6855 Class 2 Grade 60-CANCELED 12 qualified products
- MIL-S-6855 Class 2 Grade 40-CANCELED 11 qualified products
- MIL-S-6855 Class 1 Grade 60-CANCELED 4 qualified products
- MIL-S-6855 Class 3 Grade 60-CANCELED 3 qualified products
- MIL-S-6855 Class 2 Grade 80-CANCELED 2 qualified products
- MIL-S-6855 Class 1 Grade 80-CANCELED 1 qualified product
- MIL-S-6855 Class 4 Grade 60-CANCELED 1 qualified product
- MIL-S-6855 Class 5 Grade 40-CANCELED 1 qualified product
NA2-4043 THE BOEING COMPANY
CONFIRMEDCodified 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 +188 more held — contact atas.aero for a breakdown
FLIS · DLA Logistics Information Services (FLIS) · 2026-08
Manufacturer variant families
The maker's own range around this line's members — qualification marked per variant from recorded edges. A different variant is not a substitute unless your specification allows it; "family only" means the designation grammar places it, and no qualification is recorded or implied.
MILR 6855 ZF INDUSTRIEANTRIEBE WITTEN GMBH
MILR6855CL2GR60 → MIL-R-6855 · MILR6855CL2GR40 TYA1-32THK → MIL-S-6855 Class 2 Grade 40-CANCELED · MILR6855 → MIL-R-6855 · MILR6855CL2TYAG R40 1-2IN → MIL-R-6855 Type A Class 2 Grade 40 · MILR6855CL2GR40 -1-2THK → MIL-R-6855 Type A Class 2 Grade 40 · MILR6855 CL1 GR 40 .665THK ✓ this line · MILR6855CL2TYAG R60 → MIL-R-6855 Type A Class 2 Grade 60 Form SHEET · MILR6855CL2TYAG R60-48X36X1 1-4 family only · MILR6855CL2GR30 TYA 24X24X.125T → AMS-R-6855 · MILR6855CL1GR60 -1.50THKX36X36 → MIL-R-6855 Class 1 Grade 60 Form SHEET · MILR6855CL1GR60 -1.75THK36X36 → MIL-R-6855 Class 1 Grade 60 Form SHEET
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).