Consumables & expendables · Spec-Crosswalk

MIL-PRF-23699

MIL MIL-PRF-23699

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-PRF-23699

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

01599252 ASRC FEDERAL FACILITIES LOGISTICS,

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 9150-00-985-7099 →VISCOSITY AT RATED TEMP: 25.00 MINIMUM 100 DEG FAHRENHEIT AND 5.00 MINIMUM 210 DEG FAHRENHEIT AND 5.50 MAXIMUM 210 DEG F MINIMUM FLASH POINT AND TEST METHOD: 475.0 FAHRENHEIT CLEVELAND OPEN CUP

FLIS · DLA Logistics Information Services (FLIS)

102044 AEROSPHERES (UK) LTD

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 9150-00-985-7099 →VISCOSITY AT RATED TEMP: 25.00 MINIMUM 100 DEG FAHRENHEIT AND 5.00 MINIMUM 210 DEG FAHRENHEIT AND 5.50 MAXIMUM 210 DEG F MINIMUM FLASH POINT AND TEST METHOD: 475.0 FAHRENHEIT CLEVELAND OPEN CUP

FLIS · DLA Logistics Information Services (FLIS)

10333497 NIMIKKEISTOKESKUS NCB FINLAND

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 9150-01-439-0756 →VISCOSITY AT RATED TEMP: 25.00 MINIMUM 100 DEG FAHRENHEIT AND 5.00 MINIMUM 210 DEG FAHRENHEIT AND 5.50 MAXIMUM 210 DEG F MINIMUM FLASH POINT AND TEST METHOD: 475.0 FAHRENHEIT CLEVELAND OPEN CUP

FLIS · DLA Logistics Information Services (FLIS)

659352 BP AUSTRALIA PTY LTD

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 9150-00-985-7099 →VISCOSITY AT RATED TEMP: 25.00 MINIMUM 100 DEG FAHRENHEIT AND 5.00 MINIMUM 210 DEG FAHRENHEIT AND 5.50 MAXIMUM 210 DEG F MINIMUM FLASH POINT AND TEST METHOD: 475.0 FAHRENHEIT CLEVELAND OPEN CUP

FLIS · DLA Logistics Information Services (FLIS)

9150PL2194678 JEDNOLITY INDEKS MATERIALOWY -

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 9150-00-985-7099 →VISCOSITY AT RATED TEMP: 25.00 MINIMUM 100 DEG FAHRENHEIT AND 5.00 MINIMUM 210 DEG FAHRENHEIT AND 5.50 MAXIMUM 210 DEG F MINIMUM FLASH POINT AND TEST METHOD: 475.0 FAHRENHEIT CLEVELAND OPEN CUP

FLIS · DLA Logistics Information Services (FLIS)

AEROSHELL TURBINE OIL 500 1QT SHELL AVIATION LIMITED

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 9150-01-675-0213 →no stated characteristics

FLIS · DLA Logistics Information Services (FLIS)

EASTMAN TURBO OIL 2380 1QT EASTMAN CHEMICAL COMPANY

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 9150-01-675-0213 →no stated characteristics

FLIS · DLA Logistics Information Services (FLIS)

MIL-PRF-23699 LEONARDO SPA HELICOPTERS DIVISION -

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 9150-00-180-6266 →VISCOSITY AT RATED TEMP: 25.00 MINIMUM 100 DEG FAHRENHEIT AND 5.00 MINIMUM 210 DEG FAHRENHEIT AND 5.50 MAXIMUM 210 DEG F MINIMUM FLASH POINT AND TEST METHOD: 475.0 FAHRENHEIT CLEVELAND OPEN CUP

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

MIL-PRF-23699 HTS SOUTHERN CROSS LUBES SOUTHERN CROSS

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 9150-01-439-2070 →VISCOSITY AT RATED TEMP: 25.00 MINIMUM 100 DEG FAHRENHEIT AND 5.00 MINIMUM 210 DEG FAHRENHEIT AND 5.50 MAXIMUM 210 DEG F MINIMUM FLASH POINT AND TEST METHOD: 475.0 FAHRENHEIT CLEVELAND OPEN CUP

FLIS · DLA Logistics Information Services (FLIS)

MOBIL JET OIL II EXXON MOBIL CORPORATION

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 9150-00-985-7099 →VISCOSITY AT RATED TEMP: 25.00 MINIMUM 100 DEG FAHRENHEIT AND 5.00 MINIMUM 210 DEG FAHRENHEIT AND 5.50 MAXIMUM 210 DEG F MINIMUM FLASH POINT AND TEST METHOD: 475.0 FAHRENHEIT CLEVELAND OPEN CUP

FLIS · DLA Logistics Information Services (FLIS)

MOBIL JET OIL II 1QT EXXON MOBIL CORP

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 9150-01-675-0213 →no stated characteristics

FLIS · DLA Logistics Information Services (FLIS)

MOJO2001LT SIL-MID LIMITED

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 9150-00-985-7099 →VISCOSITY AT RATED TEMP: 25.00 MINIMUM 100 DEG FAHRENHEIT AND 5.00 MINIMUM 210 DEG FAHRENHEIT AND 5.50 MAXIMUM 210 DEG F MINIMUM FLASH POINT AND TEST METHOD: 475.0 FAHRENHEIT CLEVELAND OPEN CUP

FLIS · DLA Logistics Information Services (FLIS)

ROYCO 899 LANXESS CORPORATION

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 9150-00-985-7099 →VISCOSITY AT RATED TEMP: 25.00 MINIMUM 100 DEG FAHRENHEIT AND 5.00 MINIMUM 210 DEG FAHRENHEIT AND 5.50 MAXIMUM 210 DEG F MINIMUM FLASH POINT AND TEST METHOD: 475.0 FAHRENHEIT CLEVELAND OPEN CUP

FLIS · DLA Logistics Information Services (FLIS)

TURBONYCOIL 600 INTERCHEM PTY LTD

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 9150-00-985-7099 →VISCOSITY AT RATED TEMP: 25.00 MINIMUM 100 DEG FAHRENHEIT AND 5.00 MINIMUM 210 DEG FAHRENHEIT AND 5.50 MAXIMUM 210 DEG F MINIMUM FLASH POINT AND TEST METHOD: 475.0 FAHRENHEIT CLEVELAND OPEN CUP

FLIS · DLA Logistics Information Services (FLIS)

TURBONYCOIL 600 NYCO

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 9150-00-985-7099 →VISCOSITY AT RATED TEMP: 25.00 MINIMUM 100 DEG FAHRENHEIT AND 5.00 MINIMUM 210 DEG FAHRENHEIT AND 5.50 MAXIMUM 210 DEG F MINIMUM FLASH POINT AND TEST METHOD: 475.0 FAHRENHEIT CLEVELAND OPEN CUP

FLIS · DLA Logistics Information Services (FLIS)

TURBONYCOIL 600-1QT NYCO

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 9150-00-913-9717 →MINIMUM VISCOSITY INDEX: 134.6 MINIMUM FLASH POINT AND TEST METHOD: 425.0 FAHRENHEIT CLEVELAND OPEN CUP
NSN 9150-01-476-1074 →MINIMUM FLASH POINT AND TEST METHOD: 475.0 FAHRENHEIT CLEVELAND OPEN CUP

FLIS · DLA Logistics Information Services (FLIS)

V00000105 NYCO-IFI S.R.L.

CONFIRMED

Codified interchangeability (FLIS I&S)

NSN 9150-01-476-1074 →MINIMUM FLASH POINT AND TEST METHOD: 475.0 FAHRENHEIT CLEVELAND OPEN CUP

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).