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.
OEM source-control number — the OEM’s own reference for this item; the sources beneath answer it. All of this OEM’s references →
SHEET,METAL
codified reference — recorded against this stock number; the catalogue grade is not held
3M269AD4-24 BLAKE RIVET CO DIV OF LIBERTY (06606)
POSSIBLE
SHEET,METAL
codified reference — recorded against this stock number; the catalogue grade is not held
3M269AD4-24 ALLFAST FASTENING SYSTEMS, LLC (53551)
POSSIBLE
SHEET,METAL
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.
- AMS-QQ-A-250/1 — SAE (AS / AMS) (specification · not yet a document in the graph)
- ASTM B209 — ASTM
- QQ-A-250/1 — Federal Specifications (specification · not yet a document in the graph)
- QQ-A-561 — Federal Specifications
Stated characteristics
The codification record's own dimensions and material statements — official, and public by nature.
FABRICATION METHODROLLEDFLIS characteristics (MRC)
WIDTH36.000 INCHES NOMINALFLIS characteristics (MRC)
LENGTH12.000 FEET NOMINALFLIS characteristics (MRC)
CROSS-SECTIONAL THICKNESS0.025 INCHES NOMINALFLIS characteristics (MRC)
BASIC SHAPE STYLESOLIDFLIS characteristics (MRC)
WEIGHT PER UNIT MEASURE2.840 POUNDS PER SQUARE FOOTFLIS characteristics (MRC)
MINIMUM TENSILE STRENGTH16000 POUNDS PER SQUARE INCHFLIS characteristics (MRC)
MINIMUM YIELD STRENGTH14000 POUNDS PER SQUARE INCHFLIS characteristics (MRC)
HEAT TREATMENTH-14 STRAIN HARDENED, 1/2 HARDFLIS characteristics (MRC)
MATERIALALUMINUM ALLOY 1100FLIS characteristics (MRC)
MATERIAL DOCUMENT AND CLASSIFICATIONAMS-QQ-A-250/1 FED SPEC SINGLE MATERIAL RESPONSEFLIS characteristics (MRC)
NONDEFINITIVE SPEC/STD DATAH14 TEMPERFLIS 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.