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Consumables & expendables · Spec-Crosswalk

SHIM STOCK,LAMINATED

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 number2 approved sources
You are here · Stock number9535-00-807-0468
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.

BAC1534-62 THE BOEING COMPANY (81205)

CONFIRMED

OEM source-control number — the OEM’s own reference for this item; the sources beneath answer it. All of this OEM’s references →

SHIM STOCK,LAMINATED

design-control reference — the reference that controls this item of supply (RNCC 3 · RNVC 2)

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.

Substitutes — other stock numbers

Codified interchangeability across stock numbers (FLIS I&S), with the catalogue's order of use where it states one.

BAC1534-62 THE BOEING COMPANY

CONFIRMED

OEM source-control number — the OEM’s own reference for this item; the other members are its approved sources per codification. All of this OEM’s references →

SHIM STOCK,LAMINATED

NSN 9535-00-807-0468

CROSS-SECTIONAL WIDTH: 24.000 INCHES NOMINAL LENGTH: 4.000 FEET NOMINAL CROSS-SECTIONAL THICKNESS: 0.0630 INCHES NOMINAL LAMINATION THICKNESS: 0.003 INCHES NOMINAL

09A063FA SPIROL INTERNATIONAL CORPORATION

CONFIRMED

SHIM STOCK,LAMINATED

NSN 9535-00-610-7277

WIDTH: 24.000 INCHES NOMINAL LENGTH: 48.000 INCHES NOMINAL CROSS-SECTIONAL THICKNESS: 0.0650 INCHES NOMINAL LAMINATION THICKNESS: 0.003 INCHES NOMINAL AND 0.032 INCHES NOMINAL

Stated characteristics

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

LENGTH4.000 FEET NOMINALFLIS characteristics (MRC)
CROSS-SECTIONAL THICKNESS0.0630 INCHES NOMINALFLIS characteristics (MRC)
CROSS-SECTIONAL WIDTH24.000 INCHES NOMINALFLIS characteristics (MRC)
BASIC SHAPE STYLEROUNDFLIS characteristics (MRC)
LAMINATION CONSTRUCTION IN PERCENT50.0FLIS characteristics (MRC)
LAMINATION QUANTITY10FLIS characteristics (MRC)
LAMINATION THICKNESS0.003 INCHES NOMINALFLIS characteristics (MRC)
WEIGHT PER UNIT MEASURE0.907 POUNDS PER SQUARE FOOTFLIS characteristics (MRC)
NONDEFINITIVE SPEC/STD DATA1 COMPOSITION AND 2 TYPE AND 2 CLASSFLIS 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.

Request a Stage 1(a) dossierTriage the whole list free
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) · 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).