Position and secure the aircraft according to maintenance procedures before beginning cable inspection.
Identify the approved cable measurement location and choose a straight accessible section.
Confirm temperature conditions and account for any required correction guidance.
Place the aircraft cable tension meter correctly and obtain a stable reading.
Document the measured cable tension and verify measurement consistency.
Compare results with approved aircraft specifications and adjust if required.
Aircraft cable tension specifications vary by manufacturer, aircraft model, control system, cable size, and temperature. Use the model-specific pages below as starting points for organizing approved rigging references and aircraft maintenance documentation.
| Aircraft Category | Common Use | What to Verify | Subpage |
|---|---|---|---|
|
Cessna
Single-engine and light aircraft
|
Common reference for aileron, elevator, rudder, and trim cable rigging checks. | Confirm model-specific tension range, cable size, control position, and temperature correction. | View Cessna Specs → |
|
Piper
Training and general aviation aircraft
|
Used for checking control cable systems across common Piper airframes and maintenance workflows. | Verify the approved maintenance manual, allowable range, ambient temperature, and measurement location. | View Piper Specs → |
|
Beechcraft
Personal, business, and utility aircraft
|
Supports cable tension reference pages for aircraft requiring precise rigging and repeatable inspections. | Check aircraft-specific procedures, cable routing, control surface condition, and required tension window. | View Beechcraft Specs → |
|
Experimental Aircraft
Kit-built and custom aircraft
|
Helpful for organizing builder documentation, inspection notes, and cable tension measurement practices. | Reference builder guidance, component manufacturer limits, cable diameter, and final rigging documentation. | View Experimental Specs → |
Note: Always confirm cable tension values against the approved aircraft maintenance manual, service information, and applicable inspection requirements for the specific aircraft model.