DESCRIPTION |
FEATURES |
SPECIFICATIONS |
DOCUMENTS |
VIDEO |
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DESCRIPTION
The **Plane-Power TAL12-70** is a belt-driven generator-to-alternator conversion kit designed for eligible twin-engine aircraft powered by Lycoming engines.
The kit replaces two existing generator installations with two **10-1051 alternators**, each rated at 12 V and 70 A. It also includes the applicable Lycoming mounting components, solid-state Plane-Power voltage regulators, alternator-inoperative lamps and cockpit placards.
The TAL12-70 conversion is approved under **FAA Supplemental Type Certificate SA10682SC** and FAA-PMA Supplement 19.
*Images are representative and may not show the exact product for sale.*
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## Applications
- Eligible twin-engine aircraft
- Compatible Lycoming engine installations
- 12 V aircraft electrical systems
- Twin generator-to-alternator conversion applications
- Aircraft specifically approved for the TAL12-70 under STC SA10682SC
Always confirm the aircraft model, engine installation, existing generator configuration and approval requirements before ordering.
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## Why CJ Aerospace?
CJ Aerospace supplies a comprehensive range of **Plane-Power aircraft alternators, alternator kits, voltage regulators and associated components**.
Our team can assist with identifying the appropriate conversion kit based on the aircraft model, engine model, existing generator installation and electrical-system requirements.
- 🇦🇺 **Australian-owned and operated**
- 📦 **Extensive range of aircraft alternators and associated components**
- 🔧 **Technical assistance with product selection and compatibility**
- ✈️ **Reliable support for aircraft owners, operators and aviation professionals**
> ✉️ [Contact us at sales@cjaerospace.com.au](mailto:sales@cjaerospace.com.au)
> Need help identifying the correct Plane-Power generator-to-alternator conversion kit? Contact our team for assistance.
FEATURES
- Twin-engine generator-to-alternator conversion kit
- Two 12 V alternators
- 70 A rated output per alternator
- Belt-driven configuration
- Two Plane-Power 10-1051 alternator assemblies
- Two Lycoming engine mounting kits
- Two solid-state Plane-Power voltage regulators
- Alternator-inoperative warning lamps
- Left and right alternator cockpit placards
- STC/PMA approved
- Designed for eligible Lycoming-powered aircraft
SPECIFICATIONS
Package Dimensions
| Length | 27.9 cm |
| Height | 24.1 cm |
| Width | 28.6 cm |
| Weight | 7.67 kg |
Details
| **Specification** | **Details** |
|-------------------|-------------|
| **Part Number** | TAL12-70 |
| **Family** | AL Series |
| **Product Type** | Twin-Engine Generator-to-Alternator Conversion Kit |
| **Voltage** | 12 V |
| **Current Rating** | 2 × 70 A |
| **Drive** | Belt |
| **Alternator Assembly** | 2 × 10-1051 |
| **Mounting Kit** | 2 × 10-8099 |
| **Mounting Configuration** | Lycoming Engine Mount |
| **Voltage Regulator** | 2 × R1224S-12 |
| **Voltage Regulation** | External, Solid-State |
| **Compatible Engine Manufacturer** | Lycoming |
| **Helio Aircraft Applications** | Model 500 (Lycoming O-540-A2B or O-540-A2E)
|
| **KWAD Aircraft Applications** | Super-V (Lycoming O-360-A1A, O-360-A1C or O-360-A1D)
|
| **Piper PA-23 Applications** | PA-23 (Lycoming O-320-A1A, O-320-A1B, O-320-A3A or O-320-A3B); PA-23-160 (Lycoming O-320-B1A, O-320-B1B, O-320-B3A, O-320-B3B, O-320-C1A, O-320-C1B, O-320-C3A or O-320-C3B); PA-23-235 (Lycoming O-540-B1A5)
|
| **Piper PA-23-250 Applications** | PA-23-250, PA-23-250 Navy UO-1 and PA-E23-250 (Lycoming O-540-A1B5, O-540-A1D5, O-540-A3D5, IO-540-C1B5, IO-540-C4B5 or TIO-540-C1A)
|
| **Piper PA-30 Applications** | PA-30 (Lycoming IO-320-B1A) |
| **STC Number** | SA10682SC |
| **FAA-PMA Supplement** | 19 |
| **Approval** | STC/PMA |
| **Brand** | Plane-Power |
| **Manufacturer** | Hartzell Engine Tech LLC |
BROCHURES & DOCUMENTATIONS
List of Brochures
List of Documentation
VIDEO
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