ALB3 SDB CONSULTANTS, LTD. (0PGK2)
CONFIRMEDLUBRICATING OIL,GEAR
design-control reference — the reference that controls this item of supply (RNCC 3 · RNVC 2)
Consumables & expendables · Spec-Crosswalk
LUBRICATING OIL,GEAR
Stock number · one item of supply — the parts codified against it, and the stock numbers it substitutes for
← Search another part, spec or stock number
Purchasable unitnone derived yet
Part number2 approved sources
You are here · Stock number9150-01-600-3318
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.
MOBIL AGL EXXON MOBIL CORP (0TS34)
CONFIRMEDLUBRICATING OIL,GEAR
design-control reference — the reference that controls this item of supply (RNCC 3 · RNVC 2)
ALB3 1QT SDB CONSULTANTS, LTD. (0PGK2)
POSSIBLELUBRICATING OIL,GEAR
secondary reference — also codified against this stock number, as a secondary reference (RNCC 5)
MOBIL AGL 1QT EXXON MOBIL CORP (0TS34)
POSSIBLELUBRICATING OIL,GEAR
secondary reference — also codified against this stock number, as a secondary reference (RNCC 5)
HMS20-1267/2417 THE BOEING COMPANY (8V613)
POSSIBLELUBRICATING OIL,GEAR
codified reference — recorded against this stock number; the catalogue grade is not held
Substitutes — other stock numbers
Codified interchangeability across stock numbers (FLIS I&S), with the catalogue's order of use where it states one.
ALB3 SDB CONSULTANTS, LTD.
CONFIRMEDLUBRICATING OIL,GEAR
NSN 9150-01-600-3318
FATTY MATERIAL TYPE: SYNTHETIC OIL VISCOSITY AT RATED TEMP: 68.0 MINIMUM 40 DEG CELSIUS AND 10.9 MAXIMUM 100 DEG FAHRENHEIT
MOBIL AGL EXXON MOBIL CORP
CONFIRMEDLUBRICATING OIL,GEAR
NSN 9150-01-600-3318
FATTY MATERIAL TYPE: SYNTHETIC OIL VISCOSITY AT RATED TEMP: 68.0 MINIMUM 40 DEG CELSIUS AND 10.9 MAXIMUM 100 DEG FAHRENHEIT
Stated characteristics
The codification record's own dimensions and material statements — official, and public by nature.
END ITEM IDENTIFICATIONAPACHE BLK IIIFLIS characteristics (MRC)
FATTY MATERIAL TYPESYNTHETIC OILFLIS characteristics (MRC)
LUBRICANT TYPEANY ACCEPTABLEFLIS characteristics (MRC)
QUANTITY WITHIN EACH UNIT PACKAGE1.0 QUARTSFLIS characteristics (MRC)
VISCOSITY AT RATED TEMP68.0 MINIMUM 40 DEG CELSIUS AND 10.9 MAXIMUM 100 DEG FAHRENHEITFLIS characteristics (MRC)
MAXIMUM POUR POINT45.0 CELSIUSFLIS characteristics (MRC)
VAPOR PRESSURE MAXIMUM TEMP RATING20.0 CELSIUSFLIS characteristics (MRC)
PART NAME ASSIGNED BY CONTROLLING AGENCYMOBIL AGL-SYNTHETICFLIS characteristics (MRC)
SPECIAL FEATURESLIQUID; ORANGE; ODOR IS CHARACTERISTIC; BOILING BOILING PT/RANGE >260 DEGREES CELSIUS (500 DEGREES FAHRENHEIT); SOLUBILIFLIS 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).
- 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.
Source: DLA Logistics Information Services (FLIS) · cycle 2026-07 · 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).