Kt 70 Installation Manual Free -
Approximately 3.1 lbs (1.41 kg) with the installation tray. Mounting Rules
This has covered everything from pinouts and wiring to advanced torque sensor calibration. A properly installed Kt 70 transforms a generic e-bike kit into a responsive, informative riding experience.
200 Watts minimum pulse power at the antenna. TSO Compliance: TSO C112 (Class 2A). Weight: 3.1 lbs (1.41 kg) with mounting rack. Required Tools and Equipment
| Parameter | Function | Recommended Setting | |-----------|----------|----------------------| | P1 | Motor pole pairs × reduction ratio | (Number of magnets ÷ 2) × gear ratio. For direct drive: poles/2. Common: 46, 100 | | P2 | Wheel speed sensor magnets | 1 (for external sensor), 6 (for internal DD hub) | | P3 | Battery voltage (1=36V, 2=48V, 3=24V, 4=36/48 auto) | Match your pack | | P4 | Throttle type (0=voltage, 1=current) | 0 for most KT controllers | | P5 | Assist sensor type (0=PAS, 1=T_Sensor) | for torque simulation, 0 for basic PAS | | P6 | Wheel diameter (inches) | 16, 20, 26, 27.5, 700c, 29 | Kt 70 Installation Manual
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Use a certified transponder ramp test set to verify: Mode A: Correct squawk code transmission.
To ensure your installation complies with all regulatory standards and safety guidelines, always keep a verified, physical or digital copy of the official on your workbench during the project. Approximately 3
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Route these wires as a bundled harness away from high-power strobe or ignition wires to avoid signal corruption.
The hexadecimal code is programmed via a dedicated external configuration module or hardwired strapping pins on the rear harness assembly, depending on the specific mod status of the KT 70 chassis. 200 Watts minimum pulse power at the antenna
Verify that the liquid crystal display illuminates and all segments show up correctly during the self-test initialization phase.
Once the physical installation and wiring are complete, a formal test sequence must be performed before the unit is certified for flight. Ground Bench Test
The KT 70 uses a rear-mounted connector assembly. Wiring must be executed using MIL-W-22759 spec wire, and RF cables must meet low-loss attenuation requirements. Primary Pin Allocations (Molex/Edge Connector) Pin Number Wire Gauge (AWG) Aircraft Power (+14VDC or +28VDC) 2 Power Ground A Gillham Altitude Digit A1 B Gillham Altitude Digit A2 C Gillham Altitude Digit A4 D Gillham Altitude Digit B1 E Gillham Altitude Digit B2 F Gillham Altitude Digit B4 H Gillham Altitude Digit C1 J Gillham Altitude Digit C2 K Gillham Altitude Digit C4 L Gillham Altitude Digit D4 15 External Suppressor Pulse Input/Output 22 AWG (Shielded) 17 Lighting Bus (14V or 28V) Antenna RF Cable Guidelines
Total RF loss between the transponder and the antenna must not exceed at 1090 MHz. 4. Altitude Encoder Integration