Yes, but you will have to call in your order to add length or shorten seat belts or harnesses.

Seat belts are measured from end to end laid out flat.

Individual Harnesses reach a maximum of 52’’ and a minimum of 26’’ end to end.

Yes, for instance you can order a bolt in seat belt with wrap around harness and bolt in sub belt.

This is also known as a Duck Bill Latch & Link. This has a pull down adjustment on the seat belts.
The Duck Bill Latch & Link has the adjuster built into the Latch & Link which makes it very short coupled.
Check photo on web page.

The Standard Latch & Link has 3-1/2" of webbing sewn between the Latch & Link and the adjusters.
Check photo on web page.

This means the seat belt adjustment pulls down away from the body.

This means the seat belt adjustment pulls up toward the body.

Kam Lock seat belts are normally Pull Down Adjustment but can be made Pull Up on request.
Special Lengths are also available.

Our Black Aluminum epoxy adjuster is spring loaded for a cleaner look on harnesses. 
To release, simply pull up on the tab. This is a very clean and modern adjuster.

With our Standard Adjuster, the webbing is woven through the adjuster with a standard roller style adjust.
(It is available in black epoxy and silver.)

Keeps your lap belts in place when you tighten your harnesses.

The 5 Point Anti Submarine belt should be anchored on or slightly behind the chest line.

The 6 Point Anti Submarine belt should be anchored at an angle of 20 degrees behind the chest line,
as measured from the intersection of the chestline and the lap belt buckle.

Eyebolts size: 7/16 X 20 with 1-1/2" long shank.
Eyebolts are furnished with all restraints that have floor mount ends.

SFI Tags are punched approximately 60 Days out.
Example: If it is June 15th the date punched would be August.

Watch this video to learn how to avoid frayed webbing caused by Velcrow.

Our suggestion is to check with the person doing your annual to see if they will sign off based on this regulation.

Here is a clip from the ASTM, 2245:

6.10.2 Occupant lap belts, harnesses, and baggage restraints, and their attachments to the structure shall be designed for the maximum load factors corresponding to the specified ground and flight conditions including the emergency landing conditions prescribed in 5.10 and the special factors of safety in 5.1.2.2. A straight pull test of each assembly (lap belt as one assembly and shoulder harness as a separate assembly, if not continuous) of at least 7600 N (1710 lbf) for at least 3 s without failure is considered sufficient for demonstrating compliance of the belt and harness materials and associated stitching to the requirements of 6.10.2. The use of any one of the following approved safety belts shall be acceptable without further testing: 6.10.2.1 Technical Standard Order TSO-C22f, Safety Belts. 6.10.2.2 Technical Standard Order TSO-C22g, Safety Belts. 6.10.2.3 SAE Aerospace Standards AS8043B, Restraint Systems for Civil Aircraft. 6.10.2.4 SAE Aerospace Standards AS8049, Performance Standards for Seats in Civil Rotorcraft, Transport Aircraft, and General Aviation Aircraft.

6.10.2.5 Safety belts that meet 49 CFR Part 571.209. 6.10.2.6 Technical Standard Order TSO-C114, Torso Restraint Systems.

9.1.6 Occupant Safety Restraint System—The occupant restraint system must have a permanent and legible marking stating compliance with ASTM F2245, the working load rating (see 6.10.2), and the date of manufacture. The use of approved safety belts listed in 6.10.2.1, 6.10.2.2, 6.10.2.3, 6.10.2.4, 6.10.2.5, or 6.10.2.6 shall be deemed acceptable.