Aircraft Weight and Balance Records Requirements: What the FAA Requires You to Keep
Last reviewed · By Chad Griffith
<p>Aircraft weight and balance records fall into two distinct types. The aircraft's <strong>master weight and balance record</strong> is the running document of empty weight and center of gravity, updated whenever equipment changes (14 CFR 43.9) and retained with the aircraft. The per-flight <strong>load manifest</strong> is a separate record that Part 135 multiengine operators must prepare for each takeoff and keep for at least 30 days (14 CFR 135.63(c)).</p>
What weight and balance records does the FAA require?
The FAA requires three layers of weight and balance documentation, and operators routinely confuse them. Knowing which record answers which rule is the difference between a clean inspection and a finding.
- The aircraft's master weight and balance record. Every aircraft has an established empty weight and center of gravity (CG). The original values come from the type certificate and Airplane Flight Manual (AFM); thereafter the record is amended whenever installed equipment changes. This record is retained with the aircraft's permanent records.
- The per-flight load manifest. Under 14 CFR 135.63(c), a Part 135 certificate holder must prepare a load manifest in duplicate before each takeoff in a multiengine aircraft. This is an operational record, prepared fresh for every flight, and retained for at least 30 days.
- The currency / reweigh record. Under 14 CFR 135.185(a), the current empty weight and CG of a multiengine Part 135 aircraft must be calculated from values established by actual weighing within the preceding 36 calendar months (with limited exceptions). The weighing record is the proof the master record is still current.
In plain terms: the master record says what the empty aircraft weighs, the reweigh record proves that figure is still valid, and the load manifest proves each individual flight was loaded within limits.
Where the weight and balance data must live: the aircraft and the AFM
Weight and balance limits are not optional reference material. They originate at type certification and must travel with the aircraft.
Under the airworthiness standards, the established weight and CG limits are furnished in the Airplane Flight Manual. For transport-category airplanes, 14 CFR 25.1583(c) states the weight and CG limitations must be furnished in the AFM (or in a separate weight and balance document incorporated by reference). For normal-category airplanes certificated under the part 23 performance-based rules, 14 CFR 23.2620 requires the AFM to contain operating limitations and loading information.
Once the aircraft is in service, 14 CFR 91.9(b) requires that a current, approved Airplane or Rotorcraft Flight Manual (and the approved manual material that carries the weight and balance data) be available in the aircraft. The takeaway: the W&B data the crew computes against must be the current, approved data, and it must be accessible during operations — not buried in a file at the operations base.
The Part 135 load manifest: contents, who carries it, and the 30-day rule
This is the record most often cited in a Part 135 records review, and it has the most specific requirements. Under 14 CFR 135.63(c), the certificate holder is responsible for preparing a load manifest in duplicate before each takeoff for multiengine aircraft. The manifest must contain:
- The number of passengers
- The total weight of the loaded aircraft
- The maximum allowable takeoff weight for that flight
- The center of gravity limits
- The center of gravity of the loaded aircraft (or a notation that it is within limits when determined by an approved method)
- The registration number of the aircraft or the flight number
- The origin and destination
- Identification of crew members and their crew position assignments
Who carries it: the pilot in command of an aircraft for which a load manifest must be prepared must carry a copy of the completed load manifest in the aircraft to its destination.
Retention: the certificate holder must keep copies of completed load manifests for at least 30 days at its principal operations base, or at another approved location.
The 30-day window is the trap. The load manifest is an everyday operational document, easy to generate and just as easy to misplace, so a records audit that pulls a flight from three weeks ago expects to find the matching completed manifest on file. A missing or incomplete manifest for a flight inside that window is a discrete, citable gap.
Empty weight currency: the 36-calendar-month reweigh rule (135.185)
An empty-weight figure does not stay valid forever. Under 14 CFR 135.185(a), no person may operate a multiengine aircraft under Part 135 unless the current empty weight and center of gravity are calculated from values established by actual weighing of the aircraft within the preceding 36 calendar months.
14 CFR 135.185(b) provides two exceptions. The reweigh requirement does not apply to: (1) an aircraft issued an original airworthiness certificate within the preceding 36 calendar months, or (2) an aircraft operated under a weight and balance system approved in the certificate holder's operations specifications (a fleet weight-control program).
For records purposes, the reweigh date is the anchor. If the aircraft is not on an approved fleet W&B program, the dated weighing record is what proves compliance, and it expires on a rolling 36-month clock. Treat it like any other expiring compliance artifact: know the date, know when it lapses, and have the next weighing scheduled before it does.
Recording weight and balance changes from equipment changes and alterations (43.9)
The master weight and balance record is only correct if every change that moves the empty weight or CG is captured. When equipment is installed, removed, or relocated, or when an alteration is performed, the work generates a maintenance record under 14 CFR 43.9(a), which requires an entry containing a description of (or reference to data for) the work performed, the date of completion, the name of the person performing the work, and the signature, certificate number, and kind of certificate held by the person approving the aircraft for return to service.
For major alterations, 14 CFR 43.9(d) directs that the work be recorded on the form and in the manner prescribed by the FAA (FAA Form 337, Major Repair and Alteration), which captures the resulting change to weight and balance. The revised empty weight, CG, and useful load are then carried forward into the aircraft's master weight and balance record. The chain only holds if the alteration record, the Form 337 where applicable, and the updated master W&B figures all agree — a reviewer cross-checks them against each other.
Keeping weight and balance records inspection-ready with FileFlo
FileFlo is a compliance document-intelligence platform — the records and proof layer, not a weight and balance calculator, a dispatch system, or a maintenance-tracking system. It does not compute your CG or build your load sheet. It makes sure the records that prove your compliance are classified, current, complete, and exportable on demand.
When you upload a document, FileFlo classifies it to its governing CFR citation — a completed load manifest, a weighing record, a Form 337, an AFM revision — and tracks the dates that matter. It flags the rolling 36-month reweigh window from 14 CFR 135.185 before it lapses, surfaces load manifests so you can confirm the 30-day file under 14 CFR 135.63 is intact, and flags records that are missing entirely. When an inspector or auditor asks, FileFlo exports an organized, inspection-ready audit binder with each document mapped to the rule it satisfies.
FileFlo is $89 or $299 per month with a 5-day free trial. (FileFlo is not SOC 2 certified.) The standard caveat applies: FileFlo organizes and surfaces your records — the operator remains responsible for the accuracy of every weight and balance computation and for actual regulatory compliance.
Master weight and balance record vs. load manifest: don't conflate them
These two records answer different questions and follow different rules. Mixing them up is the most common weight and balance recordkeeping error in Part 135 operations.
| Attribute | Master W&B record | Load manifest |
|---|---|---|
| Governing rule | 43.9; AFM under 23.2620 / 25.1583; 91.9(b); currency under 135.185 | 14 CFR 135.63(c) |
| What it documents | Empty weight & CG of the aircraft | The loaded weight & CG of one specific flight |
| How often it changes | When equipment changes or an alteration is performed; reweigh every 36 months | Prepared before every takeoff (multiengine) |
| Where it is kept | With the aircraft's permanent records | PIC carries a copy to destination; operator files copies |
| Retention | Retained with the aircraft (current record kept current) | At least 30 days at the principal operations base or approved location |
A clean records review confirms both: a current, properly amended master record backed by an in-date weighing, and a complete 30-day file of load manifests, each loaded within the limits the master record establishes.
Frequently Asked Questions
What weight and balance records are required for a Part 135 aircraft?
A Part 135 multiengine aircraft requires three things: a current master weight and balance record (empty weight and CG, kept current as equipment changes), proof that empty weight and CG were established by actual weighing within the preceding 36 calendar months under 14 CFR 135.185, and a completed load manifest for each takeoff under 14 CFR 135.63(c), retained for at least 30 days.
How long must a Part 135 load manifest be kept?
Under 14 CFR 135.63(c), the certificate holder must keep copies of completed load manifests for at least 30 days at its principal operations base, or at another location used by it and approved by the Administrator. Separately, the pilot in command must carry a copy of the completed load manifest in the aircraft to its destination.
What must a Part 135 load manifest contain?
Under 14 CFR 135.63(c), the load manifest must contain the number of passengers, the total weight of the loaded aircraft, the maximum allowable takeoff weight for that flight, the center of gravity limits, the center of gravity of the loaded aircraft (or a notation that it is within limits by an approved method), the aircraft registration number or flight number, the origin and destination, and identification of crew members and their crew position assignments.
How often does a Part 135 aircraft have to be weighed?
Under 14 CFR 135.185(a), a multiengine aircraft's current empty weight and center of gravity must be calculated from values established by actual weighing within the preceding 36 calendar months. This does not apply to an aircraft issued an original airworthiness certificate within the preceding 36 calendar months, or to an aircraft operated under a weight and balance system approved in the certificate holder's operations specifications.
What is the difference between the master weight and balance record and the load manifest?
The master weight and balance record documents the empty weight and center of gravity of the aircraft and is updated when equipment changes (14 CFR 43.9) and reweighed every 36 calendar months (14 CFR 135.185); it stays with the aircraft. The load manifest documents the loaded weight and balance of one specific flight, is prepared before every takeoff for multiengine aircraft, and is retained for at least 30 days (14 CFR 135.63(c)).
Where must the aircraft's weight and balance data be kept?
The established weight and center of gravity limits are furnished in the Airplane Flight Manual at type certification (14 CFR 25.1583(c) for transport-category airplanes; 14 CFR 23.2620 loading information for normal-category airplanes). Under 14 CFR 91.9(b), a current, approved Airplane or Rotorcraft Flight Manual and the approved manual material carrying that data must be available in the aircraft during operations.
Do weight and balance changes from an alteration have to be recorded?
Yes. Work that changes the aircraft's weight or center of gravity generates a maintenance record under 14 CFR 43.9(a) (description of work, date completed, person performing it, and the signature and certificate of the person approving return to service). Major alterations are recorded on FAA Form 337 under 14 CFR 43.9(d), and the revised empty weight and CG are carried forward into the aircraft's master weight and balance record.
Does FileFlo calculate weight and balance?
No. FileFlo is a compliance document-intelligence platform, not a weight and balance calculator, dispatch system, or maintenance-tracking system. It classifies your weight and balance records to their CFR citation, tracks the 36-month reweigh window and the 30-day load-manifest file, flags missing records, and exports an inspection-ready audit binder. The operator remains responsible for the accuracy of every W&B computation. FileFlo is $89 or $299 per month with a 5-day free trial and is not SOC 2 certified.
Authoritative sources
- 14 CFR 91.9 - Civil aircraft flight manual, marking, and placard requirements
- 14 CFR 135.63 - Recordkeeping requirements (load manifest)
- 14 CFR 135.185 - Empty weight and center of gravity: Currency requirement
- 14 CFR 43.9 - Content, form, and disposition of maintenance and alteration records
- 14 CFR 25.1583 - Operating limitations (transport-category AFM)
- 14 CFR 23.2620 - Airplane flight manual and other documents