CIRRUS AIRPLANE MAINTENANCE MANUAL
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1 PROPELLER ASSEMBLY 1. DESCRIPTION The propeller assembly consists of a hollow aluminum hub which supports the propeller blades and also houses the pitch changing mechanism. Movement of propeller blades is controlled by a hydraulic piston/ cylinder combination mounted on the front of the hub. The linear motion of the hydraulic piston is transmitted to each blade through a pitch change rod and fork. A pitch change knob at the base of each blade intersects with the fork. Blade pitch is controlled by the governor. The governor supplies oil to the propeller hub to move the blades toward high pitch position (decreased RPM). Conversely, the propeller blades move toward low pitch position (increase RPM) as the governor drains oil away from the propeller hub. A mechanical spring is installed within the propeller to assist movement of the blades to a lower pitch position as RPM decays since blade centrifugal twisting moment is only present when the propeller is rotating. The mechanical spring will ensure that blade angle will reach the low pitch stop when the propeller is static. If oil pressure is lost at any time, the propeller will move to low pitch. The propeller assembly employes high-strength, aluminum blades. It is essential that the propeller assembly be maintained in accordance with Hartzell Propeller recommended service procedures. Refer to the manufacturer s approved Instructions For Continued Airworthiness. Page 1
2 2. MAINTENANCE PRACTICES A. Propeller (See Figure 1) The following maintenance practices apply to both the standard two blade propeller and optional three blade propeller as the maintenance practices do not differ. The propeller hub mounting flange has six, half inch diameter studs configured in a four inch circle. Two half inch diameter dowel pins are also provided to transfer torque and index the propeller with respect to the engine crankshaft. WARNING: Ensure master and magneto switches are off, and ignition key is removed. (1) Removal - Propeller (a) Acquire necessary tools, equipment, and supplies. Description P/N or Spec. Supplier Purpose Hoist - Any Source Hoist propeller. Sling - Any Source Secure propeller to hoist. Drain Pan - Any Source Receive waste lubricant. (b) Remove key from ignition. (c) Set BAT 1, BAT 2, and AVIONICS switches to OFF positions. (d) Move fuel selector to OFF position. (e) Place mixture control in idle cut-off. (f) Remove engine cowling. (Refer to 71-10) To ensure spinner dome is reinstalled in same clocked position, draw a reference line across spinner dome and spinner bulkhead. (g) Remove screws and washers securing spinner dome to spinner bulkhead. (h) Remove spinner dome from airplane. (i) Remove alternator belt. (Refer to 24-30) (j) Position hoist and lifting sling forward of airplane and attach sling to propeller. (k) Place a drain pan beneath propeller to catch any spilled lubricant. (l) Loosen and remove nuts and washers securing propeller to engine flange. Note orientation of propeller blades to engine to ensure propeller is reinstalled in correct clock position. Remove propeller from engine flange with care to prevent damaging the propeller mounting studs. (m) Remove propeller from airplane. To ensure spinner bulkhead is reinstalled in same clocked position, draw a reference line across spinner bulkhead and propeller hub. (n) Remove bolts, spacers, washers, and nuts securing spinner bulkhead to propeller hub. (o) Remove O-ring from groove inside hub at flange mounting and discard. (p) Remove drain pan and discard spilled lubricant. (2) Installation - Propeller Page 2
3 (a) Acquire necessary tools, equipment, and supplies. Description P/N or Spec. Supplier Purpose Hoist - Any Source Hoist propeller. Sling - Any Source Secure propeller to hoist. Degreaser - Any Source Degrease components. O-Ring C Hartzell Propellers Inc. Piqua, Ohio Sealing component. (b) Apply a light coat of engine oil to new O-ring and bore surfaces of propeller. Insert O-ring into groove inside hub at flange mounting. Verify spinner bulkhead is in same clocked position as originally installed. (c) Position spinner bulkhead to propeller hub and secure with bolts, spacers, washers, and nuts. Torque nuts to 22 ft-lb (30 Nm). Do not add nut run on drag to torque values. (d) Clean the engine shaft, propeller flange, and engine flange. (e) Assemble alternator backing plates, and sheave around engine flange and loosely tighten nuts, washers, and bolts. (f) Place alternator belt around sheave. (Refer to 24-30) Verify propeller is in same clocked position as originally installed. Care must be taken to avoid damaging hub or O-ring when installing propeller. Do not attempt to forcefully draw propeller onto engine flange with nuts. (g) (h) Using hoist and sling, align dowel pins in propeller flange with corresponding holes in engine mounting flange. Install washers and nuts securing propeller assembly to engine flange. Tighten nuts evenly to avoid hub damage. (i) Through a system of gentle rocking, hoisting, and maneuvering, systematically tighten backing plates, sheave, and propeller to engine flange. (j) Torque nuts securing propeller to engine flange ft-lb ( Nm). Do not add nut run on drag to torque values. (k) Install bolts securing backing plates and sheave to engine flange. (l) Adjust alternator belt tension. (Refer to 24-30) Verify spinner dome is in same clocked position as originally installed. (m) Position spinner dome to front of propeller hub and secure to spinner bulkhead with screws and washers. (n) Install engine cowling. (Refer to 71-10) Page 3 01 May 2012
4 LEGEND 1. Spinner 2. Sheave 3. Washer 4. Nut 5. Bolt 6. Propeller Stud 7. Dowel Pin 8. O-ring 9. Engine Prop Flange 10. Backing Plate 11. Spinner Backing Plate 12. Screw 13. Spacer 14. Propeller 15. Alternator Belt 16. Alternator Pulley (Ref) SR20_MM61_1061A Page 4 Figure 1 Propeller Installation
5 B. Adjustment/Test - Dynamic Balance Dynamic balancing reduces vibration produced by the propeller and powerplant. Small balance weights are added to the propeller/crankshaft assembly to correct for errors in mass distribution so vibration is reduced. Refer to the manufacturer's Instructions for Continued Airworthiness for pertinent information regarding dynamic balancing. C. Inspection/Check - Blade Track Blade track is the way one rotating blade tip follows the other in almost the same plane. Excessive difference in blade track may be an indication of bent blades or improper propeller installation. Refer to the manufacturer's Instructions for Continued Airworthiness for pertinent information regarding blade track. D. Inspection/Check - Loose Blades Although blades should be tight in the propeller, slight movement is acceptable if blade returns to original position when released. Blades with excessive movement, or that do not return to original position when released may indicate internal wear or damage. Refer to the manufacturer's Instructions for Continued Airworthiness for pertinent information regarding loose blades. E. Cleaning/Painting Propeller blades are painted with a durable specialized coating that is resistant to abrasion. If this coating becomes eroded, it is necessary to re-paint the blades to provide proper corrosion and erosion protection. Refer to the manufacturer's Instructions for Continued Airworthiness for pertinent information regarding painting. F. Repairs Nicks, gouges, and scratches on blade surfaces or on leading or trailing edges must be removed prior to flight. Refer to the manufacturer's Instructions for Continued Airworthiness for pertinent information regarding repairs. Page 5
6 Intentionally Left Blank Page 6
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