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.
MMS455 THE BOEING COMPANY (76301)
POSSIBLE
OEM source-control number — the OEM’s own reference for this item; the sources beneath answer it. All of this OEM’s references →
PAINT,HEAT RESISTING
secondary reference — also codified against this stock number, as a secondary reference (RNCC 5)
PAINT,HEAT RESISTING
design-control reference — the reference that controls this item of supply (RNCC 3 · RNVC 2)
821405 AVIOCOM B.V. (H1Z16)
POSSIBLE
PAINT,HEAT RESISTING
secondary reference — also codified against this stock number, as a secondary reference (RNCC 5)
PAINT,HEAT RESISTING
secondary reference — also codified against this stock number, as a secondary reference (RNCC 5)
KOROTHERM Courtaulds Aerospace (83574)
POSSIBLE
PAINT,HEAT RESISTING
secondary reference — also codified against this stock number, as a secondary reference (RNCC 5)
PAINT,HEAT RESISTING
codified reference — recorded against this stock number; the catalogue grade is not held
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Numbers the catalogue records against this item but marks as not for procurement — withdrawn entries, information-only listings, drawings, and references that need more than the number to identify the item.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.
PAINT,HEAT RESISTING
no longer valid — this reference was withdrawn from the catalogue record (RNVC 9) — the history trail: hold it, do not buy to it
PAINT,HEAT RESISTING
no longer valid — this reference was withdrawn from the catalogue record (RNVC 9) — the history trail: hold it, do not buy to it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.
SPECIFIC USEAIRCRAFTFLIS characteristics (MRC)
APPLICATION METHODSPRAYING AS ISFLIS characteristics (MRC)
QUANTITY WITHIN EACH UNIT PACKAGE2.500 OUNCESFLIS characteristics (MRC)
CONTENT WITHIN EACH UNIT PACKAGECONSISTS OF 2 OUNCES OF COMPONENT A (BASE) AND 1/2 OUNCE OF COMPONENT B (ACTIVATOR) TO EQUAL 2-1/2 OUNCESFLIS characteristics (MRC)
TEMP RATING2000.0 FAHRENHEIT MAXIMUMFLIS characteristics (MRC)
FEATURES PROVIDEDCHROMATE FREEFLIS characteristics (MRC)
VEHICLE MATERIAL TYPEPOLYURETHANEFLIS characteristics (MRC)
RATED DRYING TIME60.000 MINUTES MINIMUM AND 80.000 MINUTES MAXIMUMFLIS characteristics (MRC)
COLOR CHIP NUMBER27769FLIS characteristics (MRC)
VOLATILE ORGANIC COMPOUND IN GRAMS PER LITER76.0FLIS characteristics (MRC)
SPECIAL FEATURESFOR USE AS AIRCRAFT INTERNAL FIRE AND THERMAL BARRIER COATING; APPROXIMATE COLOR MATCH TO FED STD 595 COLOR NO. 27769 TEFLIS characteristics (MRC)
COLORBEIGEFLIS 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.