INSTRUCTION – HEATER INSTALLATION

perimeter of strip, gently rock controller in place w/ down force pressure of 5 to 10-lbs then w/ pressure applied hold for 15-30 seconds, this pressure and time activates adessive properties of strip. 4.5 Cable/wire Heater cable supplied in two parts: Cable Kit, w/ circuit protection device (CPD) p/n: TC03164 and Control Cable Assembly p/n: TC03246-A. Three Cable-tie Anchor’s p/n: TU02782 and Adhesive Mix Kit p/n: CB92 are supplied for use as needed. For heater circuit diagram and cable routing refer to Figures 6.5, 6.6 and 6.7. a) Cable Kit: Terminate short lead off CPD in rear of engine preheat power plug. b) Route lead aft w/ existing wiring to engine firewall. Using cable-ties and/or clamps secure CPD and cable along the way. Compensate for engine movement w/ service loop/slack between engine and mount. Note: Cable Kit supplied w/ connectors that may be used at the installers discretion for engine disconnect, refer to Figures 6.5 and 6.6. c) Select existing firewall passthrough (mixture cable or other) or install new passthrough using supplied parts, refer to Figures 6.8 and 6.9. d) Route lead through passthrough into cabin. e) Once lead is in cabin cut to length and terminate w/ Socket Connector Kit p/n: TCS2598 for connecting w/ Control Cable Assembly. Before cutting verify Control Cable routing. f) Control Cable Assembly: Route and connect leads as labeled, and secure w/ exiting wiring and lines. g) Seal firewall passthrough w/ DC 736, refer to Figure 6.8. h) Reinstall kick plate accessed in § 4.3. 4.6 Completion 1. Inspect: Visually inspect and verify components are connected and installed in accordance with this instruction. 2. Check: Connect power to heater circuit. Cool thermostat below set point and verify operation, listen for audible fan and check for warm air circulation. 3. Record: Pursuant 14 CFR part 43.9(a), and/or other procedures set in place, record installation. a) Wt & Bl and equipment list, amend as required under aircraft type certificate. b) Record and Retain Data as indicated in ICA: TCA1000 and Operating Guide: TPG1000. c) Complete Registration/Warranty Card, go to: https://www.tanisaircraft.com/warranty-card- registration Instruction –Heater Installation TNF3165 Rev. C OCT-22-2021 Tanis Aircraft Products Data – Subject to warning on cover page. Page 4 of 11 MAINTENANCE AND SERVICE Do Not open-up or modify heater or controller. There are no authorized repair procedures. Should a malfunction be detected, disconnect from power, and refer to Tanis ICA: TCA1000 and/or contact Tanis engineering.  Keep dry and free from Foreign Objects and Debris (FOD).  Annually inspect security of attachment, air intake and outlet ports for FOD and obstructions, and verify operation.  For additional specifications and supplement component information refer to AV/Cabin Heater Instruction: TN03094, and Thermal Control Instruction: TN03251. Instruction –Heater Installation TNF3165 Rev. C OCT-22-2021 Tanis Aircraft Products Data – Subject to warning on cover page. Page 5 of 11 FIGURES Examples in section are for reference. Actual configuration and installations may vary by application and/or kit specific instruction. Additional installation information may be referenced through Cirrus SR series IPC, AMM, and SB2X-71-34. Figure 6.1. Heater is located on left lower kick plate. Figure 6.2. Cirrus AV/Cabin Heat Kit p/n: TSF3165, refer to TLD: 03165 for parts and document listings. Approximate installed weight: 2.0 lbs (0.68 Kg). For CG calculations use FS 102.5. Instruction –Heater Installation TNF3165 Rev. C OCT-22-2021 Tanis Aircraft Products Data – Subject to warning on cover page. Page 6 of 11 Figure 6.3. Example of Heater and bracket on kick plate. Using bracket as template, align right front hole of bracket as shown and match drill plate. Deburr and protect holes. Using supplied hardware mount heater and bracket on kick plate. Be careful not to distort the bracket when tightening the two long front screws. Located controller aft of heater outflow, behind or beside heater as shown or locate in serviceable area above left quarter panel, refer to Figure 6.10. Do Not locate in front of heater outflow. Final location TBD by installing technician based on serviceability and heater outflow. Instruction –Heater Installation TNF3165 Rev. C OCT-22-2021 Tanis Aircraft Products Data – Subject to warning on cover page. Page 7 of 11 Figure 6.4. Verify ducting clearances. To avoid warm air standstill and overheating maintain ducting clearances. Figure 6.5. Heater circuit diagram. Cable Kit p/n: TC03164, w/ CPD and connector kits supplied for use as needed, refer to Figure 6.6 for suggested routing. Control Cable p/n: TC03246-A, refer to Figure 6.7 for suggested routing. Instruction –Heater Installation TNF3165 Rev. C OCT-22-2021 Tanis Aircraft Products Data – Subject to warning on cover page. Page 8 of 11 Figure 6.6. Cable Kit p/n: TC03164. Route from engine preheat plug below baffle to firewall passthrough. Secure CPD and cabling w/ existing wiring using cable-ties and/or cushioned clamps. Connector kits supplied for use as needed for engine disconnect or other, optional TBD by installer. Note: Passthrough shown as example location may vary by installation, refer to Figure 6.8. Instruction –Heater Installation TNF3165 Rev. C OCT-22-2021 Tanis Aircraft Products Data – Subject to warning on cover page. Page 9 of 11 Figure 6.7. Heater kit parts explosion behind avionics panel. Cabling routed from engine mounted plug through firewall. Note: Firewall passthrough location may differ from location shown, refer to Figure 6.8. Instruction –Heater Installation TNF3165 Rev. C OCT-22-2021 Tanis Aircraft Products Data – Subject to warning on cover page. Page 10 of 11 Figure 6.8. Cable routed through existing firewall passthrough (mixture cable or other) into cabin, suggested passthrough locations shown. Both sides of passthrough are resealed with High-temp silicone sealant: DC 736, reference Cirrus AMM. Note: If new passthrough is required, configure as shown using suppled parts or refer to TNG1000 for approved alternates and Cirrus AMM or SB2X-71.34 as needed. Figure 6.9. Examples of firewall passthroughs. Additional details available in Cirrus AMM or SB2X-71.34. Instruction –Heater Installation TNF3165 Rev. C OCT-22-2021 Tanis Aircraft Products Data – Subject to warning on cover page. Page 11 of 11 Figure 6.10. Thermal Control p/n: TN03251. Suggested location is above left-side kick plate directly on aircraft skin. Controller may be located on kick plate behind or beside heater. Do Not locate in front of heater outflow. Final location TBD by installing technician based on space availability and heater outflow. Alternate adjustable controller (supplied separately): Thermostat p/n: TLP3235, refer to Instruction: TN03235. ***** NOTHING FOLLOWS *****