Part Number Education

Understanding Alternate, Superseded, and Revised Aircraft Part Numbers

Aircraft parts can change numbers over time because of drawing revisions, new materials, manufacturing changes, standard transfers, product improvements, or administrative renumbering. This guide explains what alternate and superseding numbers mean, why a zero or suffix may appear after a dash, and why matching specifications do not automatically make two parts interchangeable.

What Is an Alternate Part Number?

An alternate part number is another identifier that may be associated with the same application, a related design, an approved replacement, a manufacturer equivalent, or a part that has been cross-referenced for purchasing or maintenance review.

The word “alternate” does not always mean “freely interchangeable.” It may mean that the number is worth researching, that it is approved only for certain aircraft or serial numbers, or that it may replace the original only when specific installation, modification, documentation, or effectivity requirements are met.

Alternate Part Number Superseded Part Number Interchangeability Revision Control

A Cross-Reference Is a Research Lead—not Automatic Approval

A seller catalog, inventory system, interchange list, or search result may show two numbers together. That connection can be useful, but final eligibility should come from approved aircraft data, the controlling standard, a manufacturer document, a parts catalog, an engineering authorization, or another accepted technical source.

  • Confirm whether the relationship is one-way or two-way.
  • Check aircraft model, serial number, effectivity, and installation location.
  • Determine whether additional parts or modifications are required.
  • Do not install a part solely because two numbers appear in the same online listing.

Why Part Numbers Change

A manufacturer or standards organization may revise or replace a number for technical, manufacturing, regulatory, or administrative reasons.

Design Revision

A dimension, material, tolerance, feature, finish, strength, or manufacturing requirement may change.

Improved Product

A newer design may correct a service issue, improve durability, simplify production, or support a broader application.

Standard Transfer

An AN or MS document may move to NAS, NASM, SAE AS, or another standards system while retaining similar technical requirements.

Administrative Renumbering

A company merger, drawing-system change, supplier transition, or catalog cleanup may create a new number without a major physical change.

How Revisions Appear in Part Numbers

There is no universal revision format. Different manufacturers and standard families may use dash numbers, suffix letters, revision letters, added zeros, new base numbers, or separate drawing-revision fields.

Suffix Letter A letter may identify material, finish, drilling, revision, configuration, or another family-defined option.
Added Dash Number A new dash item may identify a new size, assembly option, configuration, or revised design.
Added Zero A “0” after a dash may represent the basic configuration, a length or size code, an administrative renumbering, or a new drawing item.
New Base Number A substantial change or new document-control system may result in an entirely different part number.
PART-1 → PART-01

This change does not automatically mean “revision 01” or “the same part with a zero added.” In one numbering system it may identify a longer part, a different configuration, or a separate drawing item. In another system it may be an administrative successor. The applicable drawing or parts catalog must explain the relationship.

Superseded Part Number

A superseded number has been replaced in the manufacturer’s or standards organization’s records by another number.

  • The newer part may replace the older part.
  • The replacement may be one-way only.
  • The old part may remain usable in existing installations.
  • Additional hardware, modification, or documentation may be required.
  • Effectivity and approved data must be checked.

Revised Part Number

A revised number may identify a changed version within the same design family, but the change can be minor, major, or purely administrative.

  • Do not assume every revision is backward compatible.
  • Do not assume the newest number fits every older installation.
  • Check whether the change affects form, fit, function, or installation.
  • Review service bulletins, drawing notes, and effectivity.

Common Interchangeability Relationships

The direction of the relationship matters. “A replaces B” does not always mean “B replaces A.”

Relationship General Meaning Typical Risk What to Verify
Fully Interchangeable Either number may replace the other within the approved application. Catalog errors or unlisted effectivity limitations. Approved cross-reference, dimensions, configuration, and aircraft eligibility.
One-Way Interchangeable The newer part may replace the older part, but the older part may not replace the newer one. Installing an older configuration where the improved part is required. Direction of supersession and service-instruction requirements.
Conditional Alternate The alternate may be used only with certain aircraft, serial numbers, modifications, or supporting parts. Missing brackets, spacers, software, wiring, hardware, or modification steps. Effectivity, installation kit, service bulletin, and configuration.
Procurement Equivalent The items may satisfy the same purchasing description or standard but may not be approved for every installation. Assuming common specifications equal installation approval. Aircraft data, qualification source, material, finish, and exact configuration.
Form-Fit-Function Similar The item may appear and operate similarly while differing in approval basis, life limit, material, software, or qualification. Hidden differences not visible during receiving inspection. Design approval, eligibility, limitations, and documentation.

How an AN and NAS Part Can Be Interchangeable

Some AN hardware families were later replaced, supplemented, or cross-referenced by NAS, MS, NASM, or SAE AS standards. When the controlling documents establish an approved relationship, an AN part and a NAS part may be interchangeable for a particular application.

That relationship may exist because the newer standard preserves the same critical dimensions and performance, or because the aircraft manufacturer approved the newer part as a replacement. However, the prefixes alone do not prove interchangeability.

  • The NAS part may have tighter tolerances or a different strength level.
  • The head style, grip length, thread length, drilling, material, or finish may differ.
  • The replacement may be approved in one direction only.
  • The aircraft parts catalog may approve the alternate only for certain effectivity.

Matching Specifications Do Not Always Mean Interchangeable

Two parts can share a diameter, thread, length, material, finish, and even a general performance specification without being approved substitutes for each other.

  • One part may have a different grip-to-thread relationship.
  • One may have tighter dimensional tolerances or fatigue requirements.
  • One may be qualified for a different temperature, load, vibration, or corrosion environment.
  • One may have a different approval, marking, inspection, or trace requirement.
  • The aircraft design data may call for one exact standard or source.

Why “Same Specs” Can Still Be Different

A short catalog description cannot capture every engineering and approval requirement.

Different Tolerances

Nominal dimensions may match while allowable variation, concentricity, surface finish, or fit class differs.

Different Qualification

One part may have passed fatigue, vibration, fire, environmental, electrical, or pressure testing that the other has not.

Different Approval Basis

One item may be approved under the aircraft type design, PMA, TSO, standard-part criteria, or another accepted basis.

Different Manufacturing Controls

Heat treatment, raw-material controls, special processing, inspection, and lot acceptance may differ.

Different Life or Limits

Parts that fit the same location may have different life limits, inspection intervals, torque values, or reuse restrictions.

Different Configuration

Marking, keying, software, electrical pinout, seal compound, drilling, or installation hardware may differ.

Good Evidence of Interchangeability

  • Aircraft illustrated parts catalog showing both numbers
  • Manufacturer supersession or interchange document
  • Approved service bulletin or engineering instruction
  • Current standard showing a formal superseding relationship
  • FAA-approved PMA eligibility or approved design data
  • Authorized technical publication with effectivity

Weak Evidence by Itself

  • Same dimensions in a seller catalog
  • Same generic description or material
  • Similar appearance in a photograph
  • Unverified internet cross-reference
  • Supplier statement without supporting technical data
  • “It fits” without approval or eligibility review

What to Check Before Ordering an Alternate

  • Original number: Confirm the exact part number currently required by the aircraft or assembly data.
  • Alternate number: Verify every dash, suffix, revision, and manufacturer identifier.
  • Relationship direction: Determine whether interchangeability is full, one-way, or conditional.
  • Effectivity: Check aircraft model, serial number, modification status, engine, component, and installation position.
  • Technical differences: Review dimensions, tolerances, material, finish, strength, configuration, and performance.
  • Supporting requirements: Check whether additional hardware, software, modification instructions, or records are needed.
  • Documentation: Confirm CoC, manufacturer paperwork, trace, FAA Form 8130-3, PMA marking, or other required evidence.
  • Approval: Confirm that the part is eligible for the intended installation using accepted technical data.

Need Help Reviewing an Alternate Part Number?

Send AVBOX US the original number, proposed alternate, aircraft model, serial number, installation location, photos, and documentation requirement. We can help review the available information, but final installation eligibility must come from the appropriate approved data and authorized decision-maker.