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Consumables & expendables · Spec-Crosswalk

HYDRAULIC FLUID,PETROLEUM BASE

Stock number · one item of supply — the parts codified against it, and the stock numbers it substitutes for

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Purchasable unitnone derived yet
Part numbernone recorded
You are here · Stock number9150-00-261-8318
Specificationnone cited

Approved sources

Every maker's reference the catalogue files against this item of supply — the parts someone holding this number can use. The design-control reference is the one that controls the item; a secondary reference is a real codified fact and a weaker one.

R0YC0717 LANXESS CORPORATION (07950)

POSSIBLE

HYDRAULIC FLUID,PETROLEUM BASE

secondary reference — also codified against this stock number, as a secondary reference (RNCC 5)

BRAYC0717 CASTROL INDUSTRIAL NORTH AMERICA (98308)

POSSIBLE

HYDRAULIC FLUID,PETROLEUM BASE

codified reference — recorded against this stock number; the catalogue grade is not held

What defines this item

Specifications and drawings the catalogue records against this number. These are what the parts above are made to — never alternatives to them.

Historical & informational references

Numbers the catalogue records against this item but marks as not for procurement — withdrawn entries, information-only listings, drawings, and references that need more than the number to identify the item. If you arrived holding one of these, this is the item it points to; the sources above are what can actually be used.

H-575 BUREAU MILITAIRE DE (I9001)

WITHDRAWN

HYDRAULIC FLUID,PETROLEUM BASE

no longer valid — this reference was withdrawn from the catalogue record (RNVC 9) — the history trail: hold it, do not buy to it

Stated characteristics

The codification record's own dimensions and material statements — official, and public by nature.

BASIC INGREDIENTADDITIVES AND MINERAL OIL AND TRICRESYL PHOSPHATEFLIS characteristics (MRC)
SERVICE CHARACTERISTICSCORROSION RESISTIVE AND ANTIWEAR AND OXIDATION RESISTANTFLIS characteristics (MRC)
QUANTITY WITHIN EACH UNIT PACKAGE55.000 GALLONSFLIS characteristics (MRC)
VISCOSITY AT RATED TEMP1000.0 MAXIMUM NEG 35 DEG CELSIUS AND 500.0 MAXIMUM -20 DEG CELSIUS AND 25.0 MINIMUM 40 DEG CELSIUS AND 8.0 MINIMUM 100 FLIS characteristics (MRC)
MAXIMUM POUR POINT-40.0 CELSIUSFLIS characteristics (MRC)
MINIMUM FLASH POINT AND TEST METHOD104.0 CELSIUS CLEVELAND OPEN CUPFLIS characteristics (MRC)
SPECIAL FEATURESMINIMUM FIRE POINT AND TEST METHD: 235 DEG FAHRENHEIT CLEVELAND OPEN CUP; HUES IAW ASTM D1500,MAXIMUM 2FLIS characteristics (MRC)

Take the family with you

The whole group as CSV — members, makers, stock numbers and order of use.

Export paused

The monthly allowance for this address is used — the pattern reads as catalogue work, not a line to settle.

Whole-catalogue work is what Stage 1(a) is for: every line human-checked against the cited evidence, discrepancies annotated, back inside 24 hours. Free searching stays free — this gate only catches bulk pulls.

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.

Source: DLA Logistics Information Services (FLIS) · official codification

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).