Parts Catalog for Cessna 208 Caravan

5. Insert the supplied POH/AFM Supplement in the airplane's POH/AFM. 6. Update the airplane's weight and balance records and equipment list. 7. Complete FAA form 337 stating the Propeller has been installed in accordance with this STC. 8. Make appropriate logbook entries. | B. Installation Instructions for replacement of existing McCAULEY propeller with a propeller having no ice protection or an ELECTRIC de-ice system: 1. Remove the existing McCauley propeller from the airplane. Refer to chapter 61 of the Cessna 208 Maintenance Manual for removal procedures. 2. (For electric de-ice equipped airplanes only) Refer to BFGoodrich drawing number 5E2715 and installation instructions for installation details of airframe-side (non-rotating) kit 5E2715-3. Replace existing airframe-side de-ice system components: brush block, brush HARTZELL PROPELLER INC ONE PROPELLER PLACE PIQUA, OH 45356 Document No. 208-3BP-IM Rev 3, March 31, 2016 Page 3 of 6 block bracket, shim and brush attachment hardware with new components. Re-use remaining components (Timer, ammeter, shunt, switch, etc.). NOTE: ASSURE THAT BRUSHES ARE ADJUSTED TO THE AFT MOST POSITION OR INSTALL AFTER INSTALLATION OF PROPELLER TO AVOID DAMAGE TO BRUSHES AS THE PROPELLER IS BEING INSTALLED. • Refer to BFGoodrich drawing number 5E2715 and installation instructions for installation of components included with BFGoodrich propeller-side de-ice kit 5E2715-1. 3. Install new Hartzell 3-blade propeller on airplane. • • Refer to chapter 61 of the Cessna 208 Maintenance Manual and to the Propeller Owner's Manual for installation procedures. The latter will supersede the former regarding details specific to this propeller model. Some re-rigging of the reversing lever and controls will be required - follow the procedures outlined in chapters 61 and 76 of the Cessna 208 Maintenance Manual and perform the following checks: Reverse Power test/adjustment (Ch. 76) Maximum Propeller RPM test/adjustment (Ch. 76) Beta Switch adjustment (Ch. 61) 4. (For electric de-ice equipped airplanes only) Test the operation of the propeller de-icers: CAUTION TO PREVENT OVERHEATING, DO NOT LEAVE THE DE-ICERS ON FOR MORE THAN 1 CYCLE (3 MINUTES). AN ASSISTANT MUST BE POSITIONED AT THE PROPELLER, MUST CONTINUALLY ROTATE THE PROP TO PREVENT SLIP RING DAMAGE, AND TO CHECK FOR HEATING OF ALL THREE BLADES. • • • With the battery switch on and the prop anti-ice circuit breakers pushed in, temporarily place a jumper between terminals “1” and “3” at the pressure switch to test the "AUTO" function of the propeller de-icers. The propeller de-icers should cycle, 90 seconds on and 90 seconds off, and each blade de-ice boot must get warm. The anti-ice ammeter must read in the green arc during the on portion of the cycle. After the propeller de-icers have cooled, place the "DEICE/ANTI-ICE PROP" switch to the "MANUAL" position and the anti-ice ammeter must read in the green arc. Do not use the propeller anti-ice for the initial 30 minutes of flight after installation to allow the brushes to seat properly on the slip ring. 5. Insert the supplied POH/AFM Supplement in the airplane's POH/AFM. 6. Update the airplane's weight and balance records and equipment list. 7. Complete FAA form 337 stating the Propeller has been installed in accordance with this STC. 8. Make appropriate logbook entries. C. Installation Instructions for replacement of an existing propeller with a propeller having fluid (TKS) anti-ice system: 1. Remove the existing propeller from the airplane. . Refer to chapter 61 of the Cessna 208 Maintenance Manual for removal procedures. | | HARTZELL PROPELLER INC ONE PROPELLER PLACE PIQUA, OH 45356 2. Install new Hartzell 3-blade propeller on airplane. • . Document No. 208-3BP-IM Rev 3, March 31, 2016 Page 4 of 6 Refer to chapter 61 of the Cessna 208 Maintenance Manual and to the Propeller Owner's Manual for installation procedures. The latter will supersede the former regarding details specific to this propeller model. Some re-rigging of the reversing lever and controls may be required - follow the procedures outlined in chapters 30, 61, and 76 of the Cessna 208 Maintenance Manual and perform the following checks: Installation and Adjustment of Fluid Anti-Ice System Propeller Components (Ch. 30) Reverse Power test/adjustment (Ch. 76) Maximum Propeller RPM test/adjustment (Ch. 76) ° о Beta Switch adjustment (Ch. 61) 3. Insert the supplied POH/AFM Supplement in the airplane's POH/AFM. 4. Update the airplane's weight and balance records and equipment list. 5. Complete FAA form 337 stating the Propeller has been installed in accordance with this STC. 6. Make appropriate logbook entries. Table 2. Parts List for Aircraft Without De-ice Equipment; Without Start-locks Qty Part Number 1 8 8 HC-B3TN-3AF/ T10890CN-2 B-3339 A-2048-2 1 C-3317-230 1 D-4897(P) 1 208-3BP-IM 1 SA02181AK 208-3BP-AFMS Item Description Propeller Assembly Bolt, Double Hexagon Washer O-Ring Spinner Assembly Installation Instructions STC Document Airplane Flight Manual Supplement Table 3. Parts List for Aircraft Without De-ice Equipment; With Start-Locks Part Number HC-B3TN-3AFY/ T10890CN-2 B-3339 Qty 1 8 8 A-2048-2 1 C-3317-230 1 D-4897(P) 1 208-3BP-IM 1 SA02181AK 1 208-3BP-AFMS Item Description Propeller Assembly Bolt, Double Hexagon Washer O-Ring Spinner Assembly Installation Instructions STC Document Airplane Flight Manual Supplement | HARTZELL PROPELLER INC ONE PROPELLER PLACE PIQUA, OH 45356 Document No. 208-3BP-IM Rev 3, March 31, 2016 Page 5 of 6 Table 4. Parts List for Aircraft with ELECTRIC De-ice Equipment; Without Start-Locks Qty Part Number HC-B3TN-3AF/ T10890CNK-2 Item Description Propeller Assembly | 8 B-3339 8 A-2048-2 1 C-3317-230 D-4897(P) 5E2715-1 1 1 1 208-3BP-IM SA02181AK 208-3BP-AFMS Bolt, Double Hexagon Washer O-Ring Spinner Assembly De-Ice Kit for Propeller (BFGoodrich) Installation Instructions STC Document Airplane Flight Manual Supplement Table 5. Parts List for Aircraft with ELECTRIC De-ice Equipment; With Start-Locks Part Number HC-B3TN-3AFY/ Item Description Propeller Assembly Qty 1 T10890CNK-2 8 B-3339 8 A-2048-2 1 C-3317-230 1 1 1 D-4897(P) 5E2715-1 208-3BP-IM SA02181AK 208-3BP-AFMS Bolt, Double Hexagon Washer O-Ring Spinner Assembly De-Ice Kit for Propeller (BFGoodrich) Installation Instructions STC Document Airplane Flight Manual Supplement Table 6. Additional Airframe Parts required for installations with ELECTRIC de-ice equipment Item Description Qty Part Number A/R 5E2715-2 De-ice Kit for Airframe (BFGoodrich) Hartzell Propeller Replacement 1 5E2715-3 De-ice Kit for Airframe (BFGoodrich) McCauley Propeller Replacement HARTZELL PROPELLER INC ONE PROPELLER PLACE PIQUA, OH 45356 Document No. 208-3BP-IM Rev 3, March 31, 2016 Page 6 of 6 Table 7. Parts List for Aircraft with FLUID Anti-ice Equipment; Without Start-Locks Qty 1 Part Number HC-B3TN-3AF/ T10890CNB-2 B-3339 8 8 A-2048-2 1 1 1 C-3317-230 D-4897-2(P) 105014 1 208-3BP-IM 1 SA02181AK 208-3BP-AFMS Item Description Propeller Assembly Bolt, Double Hexagon Washer O-Ring Spinner Assembly Propeller Anti-Ice Kit Installation Instructions STC Document Airplane Flight Manual Supplement Table 8. Parts List for Aircraft with FLUID Anti-ice Equipment; With Start-Locks Qty Part Number 1 8 HC-B3TN-3AFY/ T10890CNB-2 B-3339 8 A-2048-2 1 C-3317-230 1 1 D-4897-2(P) 105014 1 208-3BP-IM 1 SA02181AK 1 208-3BP-AFMS Item Description Propeller Assembly Bolt, Double Hexagon Washer O-Ring Spinner Assembly Propeller Anti-Ice Kit Installation Instructions STC Document Airplane Flight Manual Supplement END