Whirlwind GA-UL260-2B Installation And Operation Instructions Manual Download Page 10

of 12

8

GA-UL260-2B

For   UL  Engines 

Inspections

6. 

Remove Mounting Bolts and dimensionally 
check against one another. Any bolts that 
exhibit stretching, corrosion or damage such 
as cracks or nicks are to be replaced.

7. 

Remove the Hub Mount Half . Inspect both 
hub halves for corrosion.

8. 

Remove the rear spinner bulkhead and 
examine for missing fasteners, damage, 
and cracks. If damaged, replace the spinner 
bulkhead.

9. 

REPLACE the special Wedge-lock washers.

10. 

Reinstall the assembly per the above 
installation instructions.

2000-Hour Major Periodic Inspection 

Must be accomplished by an A&P or IA.

1. 

Remove Spinner Dome and examine it for 
damage, and cracks. If necessary, replace the 
spinner dome.

2. 

Remove Clamping Bolts and washers and 
retire both sets from service.

3. 

Remove the Hub Clamp Half and set aside.

4. 

Remove Mounting Bolts and washers and 
retire both sets from service.

5. 

Remove the Hub Mount Half . 

6. 

Remove the rear spinner bulkhead and 
examine for missing fasteners, damage, 
and cracks. If damaged, replace the spinner 
bulkhead.

7. 

Send both hub half’s and both blades to an 

Approved Propeller Repair Center

 for the 

remaining 2000 hour inspection.

d

b

NOTE

: These blades do not have life 

limitation.  There is no specified over haul 
time. The propeller parts are removed from 
service when they can no longer meet the 
Continued Airworthiness Requirements

Suspected Impact

Propellers that have been involved in a known or 
suspected static or rotating impact with relatively 
solid objects (e.g., ground, maintenance stands, 
runway lights, birds, etc.) or relatively yielding 
objects (e.g., snow banks, puddles of water, heavy 
accumulation of slush, etc.) should be inspected for 
damage before further flight.
If the inspection reveals one or more of the 
following listed indications, the propeller should 
be removed and sent to Whirl Wind Propellers for 
evaluation.

d

l

A blade that tracks out of limits or out of edge 
alignment.

d

l

Loose blades in the hub.

d

l

Any diameter reduction (tip damage).

d

l

Visible major damage to the hub that cannot 
meet the Minor Hub Repairs criteria.

d

l

Visible major damage to a blade that cannot 
meet the Minor Blade Repairs criteria.

d

l

Operating changes, such as vibration or 
abnormal RPM.

d

b

IMPORTANT

:

 After any propeller strike the 

bolts should be replaced.

Lighting Strike

Any Whirl Wind composite blade suspected of 
lightning strike should be inspected and may 
require repair or replacement.
Lightning strikes usually enter a composite blade 
through the metal erosion shield. If a lightning 
strike is present, a darkened area and possible 
pitting, usually in the proximity of the tip, will be 
noticeable.
If a lightning strike is suspected or detected, 
consider the blade unairworthy. Return the blade 
to the factory or an approved propeller repair 
center for further examination.

Summary of Contents for GA-UL260-2B

Page 1: ...GA UL260 2B 64 66 Installation and Operation Instructions 9 11 3 Spinners For UL260 Engines ...

Page 2: ...GA UL260 2B For UL Engines of ii ii ...

Page 3: ...ected Impact 8 Lighting Strike 8 Paint Wear On Blade 9 Continued Airworthiness Requirements 10 Limited Warranty 12 Propeller Models These instructions apply to the following propellers Models Diameter s GA UL260 2B 64 66 Torque Values 5 16 Bolts 15 ft lbs 170 in lbs Packing List GA UL260 2B Non Threaded Flange Part Qty Blades 2 Hub forward aft halves 1 Mounting Bolts Long 5 16 x 4 4 Mounting Bolts...

Page 4: ...nes Read and follow these guidelines to ensure a safe successful propeller installation CAUTION Failure to follow these instructions will void all warranties expressed and implied Mounting difficulties and increased vibration will result with improper assembly of the propeller blades and hub parts 1 Verify the magneto ignition switch is OFF and that both magnetos are grounded 2 Chock the aircraft ...

Page 5: ...ed vertically l l Place the top blade in first with one hand and hold it in place using the forward hub half with the other hand l l Now angle the hub half so that it holds the top blade but provides a large enough gap to insert the bottom blade and forward hub half l l Once both blade are in lightly secure the propeller assembly with the mounting and clamping bolts Installation Instructions l l M...

Page 6: ...b half to prevent a change in pitch angle b b NOTE after all mounting and clamping bolts have been properly tightened Check the blade angles again to make sure they have not changed b b IMPORTANT After the first 5 hours of operation or any blade angle pitch change re check all hub mounting bolts and blade clamping bolts torque values b b NOTE To lower RPM increase the blade pitch To increase RPM d...

Page 7: ...MUM RPM RATING FOR YOUR ENGINE If you are not seeing your correct static RPM be certain the tachometer was properly calibrated 2 After the desired static RPM is achieved re check all bolt torque values The ideal pitch setting will allow the propeller to reach with out exceeding maximum RPM at full throttle in level flight d d WARNING Do not operate your propeller above the recommended engine RPM I...

Page 8: ...mped sides facing each other AN 365 524 locknuts Engine Flange UL260 Drivelug 5 16 Wedge Lock Washers Qty 4 AN5 15A Short Mounting Bolts Qty 4 AN 960 516 5 16 Flat Washers Qty 12 Torque Values 5 16 Bolts 15 ft lbs Hub Bolt Type Size Socket GA UL260 2B Clamping 5 16 1 2 Mounting 5 16 1 2 Aft Hub 5 16 4 Long Mounting Bolts Qty 4 Forward Hub Aft Spinner Back Plate ...

Page 9: ... will cover hole l l Any crack deeper than 025 l l Any solid tip damage that can t be trimmed off completely Tachometer Inspection An improperly operating tachometer can lead to propeller failure excessive vibration or cause an engine to exceed maximum RPM limits established by manufacturers Proper tachometer operation and accuracy should always be checked using the manufacturer s pro cedure if av...

Page 10: ...o longer meet the Continued Airworthiness Requirements Suspected Impact Propellers that have been involved in a known or suspected static or rotating impact with relatively solid objects e g ground maintenance stands runway lights birds etc or relatively yielding objects e g snow banks puddles of water heavy accumulation of slush etc should be inspected for damage before further flight If the insp...

Page 11: ...e depends on several factors including high operating RPM s in rain or sandy areas FOD on taxiways and runways etc Propeller Removal 1 Safe engine ignition system for maintenance by disconnecting the aircraft battery 2 Perform installation procedure as illustrated on page 5 in reverse order of operation Inspections ...

Page 12: ...int over areas of corrosion on hub parts l l Do not operate any aircraft after a propeller has been subjected to an impact without a thorough inspection Refer to the Inspection After Suspected Impact section for details l l Do not use the propeller as a tow bar to move your aircraft l l Apply a good quality automotive paste wax to the blades at least once a year l l Avoid running up in areas conta...

Page 13: ... pitches will provide 4 6 mph higher airspeeds at cruise power rpm s maximum level flight speeds are no better than climb or standard pitches and the take off and climb performance will noticeably suffer CLIMB PITCH HIGH ALTITUDE OPERATION For improved take off and climb performance use a climb pitch propeller that will turn 100 to 200 engine rpm more than a standard pitch propeller Refer to your ...

Page 14: ...terations improper installation improper maintenance or repair or improper packaging for shipment and it does not pertain to damage due to object strike or excessive blade wear due to operation Overspeed of any kind or use on or with engines or equipment not approved by Whirl Wind Propellers Corporation automatically voids this warranty This limited warranty is the only warranty provided with resp...

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