PROPELLER ASSEMBLY
CIRRUSAIRPLANE MAINTENANCE MANUALMODEL SR22PROPELLER ASSEMBLY1. DESCRIPTIONThe propeller assembly consists of a hollow aluminum hub which supports the propeller blades and alsohouses the pitch changing mechanism. Movement of propeller blades is controlled by a hydraulic piston/cylinder combination mounted on the front of the hub.Serials 0002 & subs w/ Hartzell propeller: The linear motion of the hydraulic piston is transmitted to eachblade through a pitch change rod and fork. A pitch change knob at the base of each blade intersects withthe fork.Serials 0687 & subs w/ optional McCauley propeller: The linear motion of the hydraulic piston is transmitted to each blade through a piston rod, linkage assembly, and actuating pin. The actuating pin assembly issecured to the base of each blade with screws.Blade pitch is controlled by the governor. The governor supplies oil to the propeller hub to move the bladestoward 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 isinstalled within the propeller to assist movement of the blades to a lower pitch position as RPM decayssince blade centrifugal twisting moment is only present when the propeller is rotating. The mechanicalspring will ensure that blade angle will reach the low pitch stop when the propeller is static. If oil pressure islost at any time, the propeller will move to low pitch.The propeller assembly employs high-strength, aluminum or composite blades. It is essential that the propeller assembly be maintained in accordance with vendor recommended service procedures. Refer to themanufacturer’s approved Instructions For Continued Airworthiness and/or other service instructions.EFFECTIVITY:All61-10Page 115 Apr 2007
CIRRUSAIRPLANE MAINTENANCE MANUALMODEL SR222. MAINTENANCE PRACTICESA. Propeller - Serials 0002 & subs w/ Hartzell Propeller (See Figure 61-101)WARNING:(1)Ensure master and magneto switches are off, and ignition key is removed.Removal - Propeller(a)Acquire necessary tools, equipment, and oseHoist-Any SourceHoist propeller.Sling-Any SourceSecure propeller to hoist.Drain Pan-Any SourceReceive waste lubricant.Remove key from ignition.Set BAT 1, BAT 2, and AVIONICS switches to OFF positions.Move fuel selector to OFF position.Place mixture control in idle cut-off.Remove engine cowling. (Refer to 71-10)CAUTION:(g)(h)(i)(j)(k)P/N or Spec.To ensure spinner dome is reinstalled in same clocked position, draw a reference line across spinner dome and spinner bulkhead.Remove screws and washers securing spinner dome to spinner bulkhead.Remove spinner dome from airplane.Position hoist and lifting sling forward of airplane and attach sling to propeller.Place a drain pan beneath propeller to catch any spilled lubricant.Serials 0334 & subs w/ optional Ice Protection System: Remove bolt, washer, clamp, andnut securing slinger ring feed tube to bracket on engine baffle and remove feed tube nozzle from inside of slinger ring.Loosen and remove nuts and washers securing propeller to engine flange.CAUTION: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 thepropeller mounting studs.(m)(n)(o)Remove propeller from airplane.Serials 0334 thru 0365 w/ optional Ice Protection System: Remove safety wire securingfeed tube mounting hose.Serials 0366 & subs w/ optional Ice Protection System: Remove bolts, p-clips, washers,and nuts securing feed tubes to propeller hub.CAUTION:(p)(q)(r)61-10Page 215 Apr 2007To ensure spinner bulkhead is reinstalled in same clocked position, draw areference line across spinner bulkhead and propeller hub.Remove bolts, spacers, washers, and nuts securing spinner bulkhead to propeller hub.Remove O-ring from groove inside hub at flange mounting and discard.Remove drain pan and discard spilled lubricant.EFFECTIVITY:Serials 0002 & subs w/ Hartzell Propeller
CIRRUS(2)AIRPLANE MAINTENANCE MANUALMODEL SR22Installation - Propeller(a)Acquire necessary tools, equipment, and st-Any SourceHoist propeller.Sling-Any SourceSecure propeller tohoist.Degreaser-Any SourceDegrease components.O-RingC-3317-228Hartzell Propellers Inc. Sealing compoPiqua, Ohionent for Hartzell937-778-4200propeller.Apply a light coat of engine oil to new O-ring and bore surfaces of propeller. Insert O-ringinto groove inside hub at flange mounting.CAUTION:(c)P/N or Spec.Verify spinner bulkhead is in same clocked position as originally installed.Position spinner bulkhead to propeller hub and secure with bolts, spacers, washers, andnuts. Torque nuts to 22 ft-lb (30 Nm).Serials 0334 thru 0365 w/ optional Ice Protection System: Insert feed tube into mountinghose and secure with safety wire.Serials 0366 & subs w/ optional Ice Protection System: Install bolts, p-clips, washers, andnuts securing blade feed tubes to propeller hub.Clean the engine shaft, propeller flange, and engine flange.CAUTION: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)Using hoist and sling, align dowel pins in propeller flange with corresponding holes inengine mounting flange.CAUTION:(h)(i)Install washers and nuts securing propeller to engine flange. Torque nuts to 70 - 80 ft-lb(94.9 - 108.5 Nm).Serials 0366 & subs w/ optional Ice Protection System: Position slinger ring feed tube toengine baffling bracket and to inside of slinger ring. Install bolt, washer, clamp, and nutsecuring feed tube to engine baffling.CAUTION:(j)(k)Tighten nuts evenly to avoid hub damage.Verify spinner dome is in same clocked position as originally installed.Position spinner dome to front of propeller hub and secure to spinner bulkhead withscrews and washers.Serials 0334 thru 0366 w/ optional Ice Protection System: Check feed tube alignment.1Perform Inspection/Check - Blade Feed Tube Orientation. (Refer to 30-60)2Perform Inspection/Check - Slinger Ring Feed Tube Orientation. (Refer to 30-60)Serials 0366 & subs w/ optional Ice Protection System: Check feed tube alignment.(l)EFFECTIVITY:Serials 0002 & subs w/ Hartzell Propeller61-10Page 315 Apr 2007
CIRRUS(m)61-10Page 415 Apr 2007AIRPLANE MAINTENANCE MANUALMODEL SR221Perform Inspection/Check - Blade Feed Tube Orientation. (Refer to 30-60)2Perform Inspection/Check - Slinger Ring Feed Tube Orientation. (Refer to 30-60)Install engine cowling. (Refer to 71-10)EFFECTIVITY:Serials 0002 & subs w/ Hartzell Propeller
CIRRUSAIRPLANE MAINTENANCE MANUALMODEL SR2227ENGINE 110LEGEND1. Spinner2. Washer3. Screw4. Propeller Stud5. O-ring6. Spinner Bulkhead7. Nut8. Spacer9. Propeller10. Bolt11. Feed Tube12. P-Clip13. Sealing Ring14. Standoff15. Slinger Ring16. Bonded Seal17. Propeller Boot, De-Ice101NOTETorque nuts to 22 ft-lb. (30 Nm).Torque nuts to 50 -70 in-lb. (5.6 - 7.9 Nm).Torque nuts to 70 -80 ft-lb. (94.9 - 108.5 Nm).SR22 MM61 1430AFigure 61-101Propeller Installation - Serials 0002 & subs w/ Hartzell PropellerEFFECTIVITY:Serials 0002 & subs w/ Hartzell Propeller61-10Page 515 Apr 2007
CIRRUSAIRPLANE MAINTENANCE MANUALMODEL SR22B. Propeller - Serials 0687 & subs w/ optional McCauley Propeller (See Figure 61-102)WARNING:(1)Ensure master and magneto switches are off, and ignition key is removed.Removal - Propeller(a)Acquire necessary tools, equipment, and oseHoist-Any SourceHoist propeller.Sling-Any SourceSecure propeller to hoist.Drain Pan-Any SourceReceive waste lubricant.Remove key from ignition.Set BAT 1, BAT 2, and AVIONICS switches to OFF positions.Move fuel selector to OFF position.Place mixture control in idle cut-off.Remove engine cowling. (Refer to 71-10)CAUTION:(g)(h)(i)(j)(k)(l)P/N or Spec.To ensure spinner dome is reinstalled in same clocked position, draw a reference line across spinner dome and spinner bulkhead.Remove screws and washers securing spinner dome to spinner bulkhead.Remove spinner dome from airplane.Remove spinner support and shim(s) from front of propeller hub.Position hoist and lifting sling forward of airplane and attach sling to propeller.Place a drain pan beneath propeller to catch any spilled lubricant.Serials 0687 & subs w/ optional Ice Protection System: Remove bolt, washer, clamp, andnut securing slinger ring feed tube to bracket on engine baffle and remove feed tube nozzle from inside of slinger ring.Loosen and remove nuts securing propeller to engine flange.CAUTION: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 thepropeller mounting studs.(n)(o)Remove propeller from airplane.Serials 0687 & subs w/ optional Ice Protection System: Remove screws, washers, clamps,and nuts securing blade feed tubes to feed tube brackets.CAUTION:(2)61-10Page 615 Apr 2007To ensure spinner bulkhead assembly is reinstalled in same clocked position, draw a reference line across spinner bulkhead assembly and propellerhub.(p) Remove screws and washers securing spinner bulkhead assembly to propeller hub.(q) Remove O-ring from groove inside hub at flange mounting and discard.(r)Remove drain pan and discard spilled lubricant.Installation - PropellerEFFECTIVITY:Serials 0687 & subs w/ optional McCauley Propeller
CIRRUS(a)AIRPLANE MAINTENANCE MANUALAcquire necessary tools, equipment, and supplies.Description(b)(d)(e)P/N or Spec.SupplierPurposeHoist-Any SourceHoist propeller.Sling-Any SourceSecure propeller tohoist.Degreaser-Any SourceDegrease components.O-RingA-1633-3McCauley Propeller Systems Sealing componentVandalia, Ohiofor McCauley propel937-890-5246ler.LubricantMIL-T-83483Any SourceLubricate mountingstuds and nuts onMcCauley propeller.Apply a light coat of engine oil to new O-ring and bore surfaces of propeller. Insert O-ringinto groove inside hub at flange mounting.CAUTION:(c)MODEL SR22Verify spinner bulkhead assembly is in same clocked position as originallyinstalled.Position spinner bulkhead to propeller hub and secure with screws and washers. Torquescrews to 75 - 85 in-lb (0.53 - 0.60 Nm). Safety wire screws in pairs.Serials 0687 & subs w/ optional Ice Protection System: Install screws, washers, clamps,and nuts securing feed tubes to feed tube brackets.Clean the engine shaft, propeller flange, and engine flange.CAUTION: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.(f)Using hoist and sling, align dowel pins in propeller flange with corresponding holes inengine mounting flange.CAUTION:(g)Liberally apply lubricant to threads of studs and threads and faces of nuts. Install nutssecuring propeller assembly to engine flange.CAUTION:(h)(i)Never use oil as a substitute for approved lubricant. Substitution of theapproved grease with an unapproved lubricant (or no lubricant) could resultin undertorquing or severe overtorquing of propeller attaching parts.Tighten nuts evenly to avoid hub damage.Secure propeller to engine flange and torque nuts to 45 - 50 ft-lb (61.0 - 67.7 Nm).Serials 0687 & subs w/ optional Ice Protection System: Position slinger ring feed tube toengine baffling bracket and to inside of slinger ring. Install bolt, washer, clamp, and nutsecuring feed tube to engine baffling.CAUTION:Verify spinner dome is in same clocked position as originally installed.EFFECTIVITY:Serials 0687 & subs w/ optional McCauley Propeller61-10Page 715 Apr 2007
CIRRUS(j)AIRPLANE MAINTENANCE MANUALPosition spinner support and shim(s) to front of propeller hub.Note:(k)(l)(m)(n)61-10Page 815 Apr 2007MODEL SR22Spinner installation holes should be approximately 0.05 inch (1.27 mm)from true alignment when shims are correctly adjusted.Lightly press spinner shell snug against support and check alignment of holes in bulkhead.Pushing hard on shell, align installation holes with bulkhead. Secure spinner shell to spinner bulkhead with four equally spaced screws and washers. Relax force against shell andinstall remaining screws and washers.Serials 0687 & subs w/ optional Ice Protection System: Check feed tube alignment.1Perform Inspection/Check - Blade Feed Tube Orientation. (Refer to 30-60)2Perform Inspection/Check - Slinger Ring Feed Tube Orientation. (Refer to 30-60)Install engine cowling. (Refer to 71-10)EFFECTIVITY:Serials 0687 & subs w/ optional McCauley Propeller
CIRRUSAIRPLANE MAINTENANCE MANUALMODEL SR227177 294161252332151110ENGINE PROPFLANGE(REF)6117182313141LEGEND1. Spinner2. Washer3. Screw4. Propeller Stud5. O-ring6. Spinner Bulkhead7. Nut8. Spacer9. Propeller10. Bolt11. Feed Tube12. Slinger Ring13. Propeller Boot, De-Ice14. Support15. Shim16. Adapter17. Backing Plate18. BracketNOTEApply lubricant to threads of studs and threads and faces of nuts.Torque nuts to 45 - 50 ft-lb (61.0 - 67.8 Nm).Torque screws to 75 - 80 in-lb (8.47 - 9.04 Nm).Torque nuts to 30 - 36 in-lb (3.4 - 4.0 Nm).SR22 MM61 1759Figure 61-102Propeller Installation - Serials 0687 & subs w/ optional McCauley PropellerEFFECTIVITY:Serials 0687 & subs w/ optional McCauley Propeller61-10Page 915 Apr 2007
CIRRUSAIRPLANE MAINTENANCE MANUALMODEL SR22C. Adjustment/Test - Dynamic BalanceDynamic balancing reduces vibration produced by the propeller and powerplant. Small balanceweights are added to the propeller/crankshaft assembly to correct for errors in mass distribution sovibration is reduced. Refer to the manufacturer's Instructions for Continued Airworthiness for pertinentinformation regarding dynamic balancing.D. Inspection/Check - Blade TrackBlade 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 tothe manufacturer's Instructions for Continued Airworthiness for pertinent information regarding bladetrack.E. Inspection/Check - Loose BladesAlthough 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 positionwhen released may indicate internal wear or damage. Refer to the manufacturer's Instructions for Continued Airworthiness for pertinent information regarding loose blades.F.Cleaning/PaintingPropeller 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 informationregarding painting.G. RepairsNicks, gouges, and scratches on blade surfaces or on leading or trailing edges must be removed priorto flight. Refer to the manufacturer's Instructions for Continued Airworthiness for pertinent informationregarding repairs.61-10Page 1015 Apr 2007EFFECTIVITY:All
61-10 Page 6 Serials 0687 & subs w/ optional McCauley Propeller EFFECTIVITY: CIRRUS AIRPLANE MAINTENANCE MANUAL MODEL SR22 15 Apr 2007 B. Propeller - Serials 0687 & subs w/ optional McCauley Propeller (See Figure 61-102) WARNING: Ensure master and magneto switches are off, and ignition key is removed.
the propeller, pressure developed by the propeller, stresses, deformations and strains developed within the propeller when subjected to a thrust. The modifications made to the propeller in terms of material, number of blades and rake angles suggested which variant of the propeller is best suited for different requirements of the Ship.
Aircraft propeller is sometimes colloquially known as an air screw propeller The present work is directed towards the study of composite aircraft propeller working and its terminology, simulation and flow simulation of composite aircraft propeller has been performed. To analyze the composi
Removal and Installation 0 Put match marks on flanges and separate propeller shaft from differential carrier. SPD103 0 Draw out propeller shaft from transmission and plug up rear end of transmission rear extension housing. Transmission 7 SPD359 Inspection Inspect propeller shaft runout. If runout exceeds specifications, replace propeller shaft .
Hartzell Propeller Inc. Service Bulletin No. HC-SB-61-272, “PROPELLER - PROPELLER INSTALLATION”, Issued: January 17/05 or subsequent revision; Hartzell Propeller Inc. Service Letter No. HC-SL-61-239, “PROPELLER - SLIP RING SPLIT MOUNTING PLATE INSPECTION A
EWD (Extruded Aluminum Propeller, Direct Drive) 16 EWB (Extruded Aluminum Propeller, Belt Drive) 17 EPD (Packaged, Extruded Aluminum Propeller, Direct Drive) 18 EPB (Packaged, Extruded Aluminum Propeller, Belt Drive) 19 Typical Installations 20 Options & Accessori
the propeller if the prop bolts get loose on the flange, at which point the side loads will rapidly lead to cracks in the propeller hub and/or failure of the propeller bolts. It is recommended to install the W69EK7 series propeller on the DA20-C1 using MS21044N7 self locking nuts. It is also allowable to use AN310-7 castellated nuts with cotter .
ical power produced by a propeller with its diameter and rotation velocity as C P P shaft ˆN3D5: (6) Yet, another parameter that is important is the propeller e ciency . Since the propeller was pre-tended to be optimized to reduce the electrical power of the system motor propeller, this parame-ter was de ned as the ratio between the power that
The “Agile Software Development Manifesto” was developed in February 2001, by representatives from many of the fledgling “agile” processes such as Scrum, DSDM, and XP. The manifesto is a set of 4 values and 12 principles that describe “What is meant by Agile". THE AGILE VALUES 1. Individuals and interactions over processes and tools 2. Working software over comprehensive .
