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Maintenance Forms & RecordsAMT — General

Rebuilder Records and Zero-Time Engine Logbooks

When an FAA-certificated rebuilder restores an aircraft engine to zero-time status, specific logbook entries and paperwork are required — distinct from overhaul records — and understanding the difference is critical for AMT certification exams.

Reviewed & updated · Grounded in current FAA handbooks & the ACS

Aircraft engine logbooks are legal documents, and the entries inside them carry real consequences for airworthiness, resale value, and regulatory compliance. One of the most misunderstood entries an aviation maintenance technician (AMT) will encounter is the zero-time rebuilder entry — a notation that fundamentally resets an engine's recorded service life. Understanding exactly who may make this entry, what paperwork must accompany it, and how it differs from a simple overhaul record is not only a critical exam topic but an essential piece of professional knowledge every AMT must have in their toolkit.

This article walks through the regulatory framework governing rebuilt engine records, the specific logbook requirements, and the practical distinctions between a rebuilt engine and an overhauled engine — distinctions the FAA knowledge test will almost certainly exploit.

The Regulatory Foundation

The authority for rebuilt engine records flows directly from 14 CFR Part 91.421, which addresses rebuilt engine maintenance records. The rule establishes that the owner or operator of an aircraft with a rebuilt engine may use a new maintenance record — effectively a fresh logbook — without reference to previous operating history, provided the engine was rebuilt by the original equipment manufacturer (OEM) or by an agency approved by the manufacturer. This is a significant privilege: it legally severs the engine from all prior time and history, allowing it to begin life anew from zero hours.

It is important to recognize that 14 CFR Part 91.421 does not authorize just any shop or certificated repair station to issue a zero-time rebuilt engine record. The rule specifically limits this privilege to the engine manufacturer or an entity the manufacturer has approved in writing. A certificated repair station performing a routine overhaul — even to new limits — does not automatically earn the right to zero-time the engine. That distinction is central to the exam and to practical record-keeping.

Rebuilt vs. Overhauled: A Critical Distinction

The FAA makes a deliberate and important distinction between a rebuilt engine and an overhauled engine, and mixing up these terms is a common test trap.

An overhauled engine has been disassembled, cleaned, inspected, repaired as necessary, reassembled, tested, and approved for return to service in accordance with approved data (typically the manufacturer's overhaul manual). Overhauled engines are returned to service within serviceable limits, which may be either new limits or the manufacturer's approved wear limits. A certified repair station or an appropriately rated AMT can perform and sign off an overhaul. However, the engine's total time does not reset — the logbook continues from whatever hours were accumulated before the overhaul. The entry in the engine logbook must describe the work done, the date, and the signature and certificate number of the person approving the return to service.

A rebuilt engine, by contrast, has been disassembled, inspected, repaired as necessary, and reassembled by the manufacturer or an approved agency using new parts or used parts that meet new part tolerances and limits. This is a higher standard than a standard overhaul — rebuilt engines must meet new limits, not merely serviceable limits. Because of this elevated standard and the controlled rebuilding environment, the FAA allows the manufacturer (or approved rebuilder) to issue a zero-time record. The prior service history is legally irrelevant to the new owner and need not be maintained or referenced.

What Must Be in the New Logbook

When a certificated rebuilder returns a zero-timed engine to service, the new maintenance record — the fresh logbook — must contain a specific set of information to be legally valid. Drawing from 14 CFR Part 91.421 and the general records requirements of 14 CFR Part 43, the entry must include:

  • Date of rebuild: The calendar date the engine was approved for return to service after rebuilding.
  • Engine model and serial number: Positive identification of the specific engine so there is no ambiguity about which powerplant the record applies to.
  • New mandatory replacement parts installed: Any parts replaced as a matter of course or regulation during the rebuild process must be identified.
  • Current status of life-limited parts: Life-limited parts installed in the engine at the time of rebuild must be listed with their current accumulated cycles or hours and their published limit. This is non-negotiable — even in a zero-time rebuild, life-limited part history does not disappear. The FAA requires traceability for these components because running a life-limited part beyond its limit is a serious airworthiness and safety issue.
  • Time since overhaul (TSO) or time since new (TSN) for each major component: Where applicable, individual major components may carry their own service history that must be captured.
  • Identity of the rebuilder: The name and certificate number (or manufacturer's identity) of the person or organization that performed the rebuild and approved the engine for return to service.

Notice that even though the overall engine time resets to zero, life-limited parts retain their accumulated history. This is one of the most frequently tested nuances in this topic area. A turbine engine first-stage disk, for example, may have accumulated 2,000 cycles before being installed in a rebuilt engine — those 2,000 cycles are still counted against its life limit, regardless of what the engine logbook says about total time.

The Role of FAA Form 8130-3 and Airworthiness Approval Tags

When an approved rebuilder returns an engine to service, the transaction is typically documented with an FAA Form 8130-3 (Airworthiness Approval Tag), which accompanies the engine and serves as evidence of its airworthiness status at the time of release. The Form 8130-3 identifies the article, the certifying authority, and the basis of airworthiness approval. This tag does not replace the logbook entry but works alongside it as part of the complete documentation package. AMTs receiving a rebuilt engine should verify that the 8130-3 is present, legible, and consistent with the engine's logbook and nameplate data before installing or accepting the engine.

Practical Implications for the AMT

When an AMT encounters a rebuilt engine in the field, several practical verification steps are important. First, confirm that the entity that issued the zero-time record is actually the OEM or an OEM-approved rebuilder — not simply a repair station that performed an overhaul and informally called it a rebuild. Second, cross-check the life-limited parts listing in the logbook against actual hardware markings to ensure traceability. Third, verify that any applicable Airworthiness Directives (ADs) have been noted or complied with before the engine entered service — a rebuilt engine is not automatically AD-compliant simply because it carries a fresh logbook.

An owner or operator who discovers that a prior logbook was improperly zeroed out — perhaps by a shop that lacked manufacturer approval — faces a potentially serious regulatory and legal situation. The FAA's position is clear: only the manufacturer or an entity the manufacturer has specifically approved may issue a new maintenance record under Part 91.421. Records improperly created in violation of this section do not carry the legal weight the owner may believe they do, and the engine's true total time must be reconstructed to the extent possible.

Key Numbers and Rules

  • 14 CFR 91.421 — The governing regulation for rebuilt engine maintenance records and the zero-time privilege.
  • 14 CFR Part 43, Appendix B — Specifies what major alterations and repairs (including major overhauls) require as documentation and who may approve them.
  • Rebuilt = new limits only — All dimensions must meet new part tolerances, not merely serviceable wear limits.
  • Overhauled = serviceable limits acceptable — Parts may be within manufacturer's allowed wear range, not necessarily new specifications.
  • Life-limited part history never resets — Even in a zero-time rebuild, accumulated cycles or hours on life-limited parts must be carried forward in the new logbook.
  • Zero-time authority is limited — Only the OEM or an OEM-approved agency may legally issue a new (zero-time) maintenance record; a standard repair station overhaul does not qualify.

Common Test Traps

  • Confusing overhaul with rebuild: The FAA exam frequently uses both terms and expects you to know that only a rebuilt engine (by the OEM or approved agency) earns a fresh, zero-time logbook. An overhauled engine continues its existing record.
  • Assuming any certificated repair station can zero-time an engine: Even a fully certificated Part 145 repair station with an engine rating cannot unilaterally issue a new zero-time record unless it is specifically approved by the engine manufacturer to do so.
  • Forgetting life-limited part traceability: Examinees often assume a zero-time logbook means all component histories reset. Life-limited parts are the critical exception — their accumulated time or cycles always survive the rebuild entry.
  • Overlooking Form 8130-3 as part of the record: The 8130-3 is part of the rebuild documentation ecosystem. Knowing it accompanies (rather than replaces) the logbook is testable.
  • Mixing up new limits vs. serviceable limits: For a rebuild, new part tolerances are mandatory. For an overhaul, serviceable limits are acceptable. Swapping these on the exam — or in the shop — leads to errors with real airworthiness consequences.

See also

FAA source

Pilot's Handbook of Aeronautical Knowledge (FAA-H-8083-25), Chapter 9; Aviation Maintenance Handbook – General (FAA-H-8083-30), Chapter 2; 14 CFR Part 91.421; 14 CFR Part 43 and Appendix B.

This page is an original, plain-English summary grounded in the public-domain FAA handbook cited above. Click the citation to open the official FAA handbook PDF. It is a study aid, not a substitute for the official handbook or the regulations.

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