DESCRIPTION |
FEATURES |
SPECIFICATIONS |
DOCUMENTS |
VIDEO |
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DESCRIPTION
The **Plane-Power SAL12-70C** is a belt-driven generator-to-alternator conversion kit for approved single-engine aircraft powered by compatible Continental engines.
Designed for nominal 12 V aircraft electrical systems, the kit provides a 70 A alternator output with typical 14 V regulated system operation.
The kit includes Plane-Power alternator assembly **10-1050C**, Continental mounting kit **10-9099**, solid-state voltage regulator **R1224** and a 14 V alternator-inoperative warning lamp.
*Images are representative and may not show the exact product for sale.*
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## Applications
- Approved single-engine aircraft with compatible Continental engines
- Nominal 12 V aircraft electrical systems
- Belt-driven generator-to-alternator conversion applications
- Aircraft approved under STC SA10682SC
- Installations requiring a 70 A alternator output
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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
- Belt-driven generator-to-alternator conversion
- 12 V alternator configuration
- Typical 14 V regulated system operation
- 70 A rated output
- Designed for compatible Continental-powered aircraft
- Alternator assembly 10-1050C
- Continental mounting kit 10-9099
- Solid-state Plane-Power R1224 voltage regulator
- Alternator-inoperative warning lamp
- STC/PMA approved
SPECIFICATIONS
Package Dimensions
| Length | 27.9 cm |
| Height | 24.1 cm |
| Width | 28.6 cm |
| Weight | 7.67 kg |
Details
| **Specification** | **Details** |
|-------------------|-------------|
| **Part Number** | SAL12-70C |
| **Family** | AL Series |
| **Product Type** | Generator-to-Alternator Conversion Kit |
| **Alternator Voltage** | 12 V |
| **Typical Regulated System Voltage** | 14 V |
| **Current Rating** | 70 A |
| **Drive** | Belt |
| **Pulley** | 3-inch Diameter, 3/8-inch V-Belt Pulley |
| **Alternator Assembly** | 10-1050C |
| **Mounting Kit** | 10-9099 |
| **Voltage Regulator** | R1224 |
| **Voltage Regulation** | External, Solid-State |
| **Warning Lamp** | 14-1010 Alternator-Inoperative Lamp |
| **Placards** | ALP-1001 ALT FIELD and ALP-1006 ALT INOP |
| **Installation Instructions** | 14-6001 |
| **Compatible Engine Manufacturer** | Continental |
| **Alexandria Aircraft Applications** | 14-19-2 (Continental O-470-K); 14-19-3 and 14-19-3A (Continental IO-470-F) with STC SA10682SC installed
|
| **Interceptor Aviation Applications** | 200, 200A, 200B, 200C and 200D with STC SA10682SC installed; the 200D application uses the Continental IO-520-A
|
| **Lockheed Aircraft Applications** | 402-2 with Continental IO-470-R or TSIO-470-B and STC SA10682SC installed
|
| **Sierra Hotel Aero Applications** | Navion D, E, F, G and H; Navion L-17A; Navion A in L-17B and L-17C configurations; and Navion B modified by an approved STC conversion to a Continental O-470 or IO-470 engine, with STC SA10682SC installed
|
| **Textron Aviation – Beechcraft 35-Series Applications** | 35, A35, B35, C35, D35, E35, F35, G35 and 35R modified by an approved STC conversion to a Continental O-470 or IO-470 engine, with STC SA10682SC installed
|
| **Other Textron Aviation – Beechcraft Applications** | 35-33 and 35-A33 (Continental IO-470-J or IO-470-K); 35-B33 and 35-C33 (Continental IO-470-K); H35, J35, K35 and M35 (Continental IO-470-C); N35 and P35 (Continental IO-470-N). Applicable aircraft must have the original generator installation and STC SA10682SC installed
|
| **Textron Aviation – Cessna 180 Applications** | 180 (Continental O-470-A, O-470-J or O-470-K); 180A and 180B (Continental O-470-K); 180C, 180D, 180E, 180F and 180G (Continental O-470-L or O-470-R) with the original generator and STC SA10682SC installed
|
| **Textron Aviation – Cessna 182 Applications** | 182, 182A, 182B, 182C, 182D, 182E, 182F, 182G and 182H with the original generator and STC SA10682SC installed
|
| **Textron Aviation – Cessna 185 Applications** | 185, 185A, 185B, 185C and 185D with Continental IO-470-F, original generator and STC SA10682SC installed
|
| **Textron Aviation – Cessna 206 Applications** | 206 with Continental IO-520-F and P206 with Continental IO-520-A, original generator and STC SA10682SC installed
|
| **Textron Aviation – Cessna 205 and 210 Applications** | 210 and 210A with Continental IO-470-E; 210-5 (205) and 210-5A (205A) with Continental IO-470-S, original generator and STC SA10682SC installed |
| **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
Service Bulletin No. 209
VIDEO
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