Trail

Part number family

MIL-I-23264/16

MILITARY SPECIFICATIONS · INSULATOR,BUSHING

One manufacturer designation, every identity it carries: 12 stock numbers.

Purchasable unitnone recorded
You are here · Part numberMIL-I-23264/16
Stock number →5970-00-054-8897
Specificationnone recorded

Codified — the stock numbers

The codification catalogue keys on the item of supply — each stock number opens the catalogue's own family, with approved sources and order of use.

NSN5970-00-054-8897FLIS
NSN5970-00-054-8911FLIS
NSN5970-00-158-6854FLIS
NSN5970-00-159-1400FLIS
NSN5970-00-235-5090FLIS
NSN5970-00-280-9427FLIS
NSN5970-00-283-9970FLIS
NSN5970-00-284-8430FLIS
NSN5970-00-538-2939FLIS
NSN5970-00-552-9845FLIS
NSN5970-00-577-0948FLIS
NSN5970-00-752-5720FLIS

Approved alternates — codified interchangeability (FLIS I&S)

Order of use is the catalogue's, not ours. Every member opens its own part-number family.

INSULATOR,BUSHING

group family page →

NSN 5970-00-774-6477 190-1123-00 ROCKWELL COLLINS, INC. · OEM source-control reference

NSN 5970-00-157-0730 39-46 BARKER & WILLIAMSON

NSN 5970-00-117-5046 6-1BALT1PC64 THE DEWEY ELECTRONICS CORPORATION

NSN 5970-00-027-8617 JANI8 JOINT ARMY-NAVY SPECIFICATIONS

NSN 5970-00-280-8309 K32102 BETA LABS INC A-B AND MILLEN MFG DIV

NSN 5970-00-054-8897 MIL-I-23264/16 MILITARY SPECIFICATIONS

NSN 5970-00-158-6861 MILI23264-16 MILITARY SPECIFICATIONS

Graded alternates — other manufacturers on the same lines

Products the evidence places against this one, each naming the line that vouches for it. CONFIRMED means every claim cites a source; POSSIBLE is a lead to verify, not a match.

No other maker holds a published citation on these lines yet — coverage grows with each qualified-products cycle.

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).