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ICA 

1500-SERIES-ICA-1

 

Revision A - 01/22/2009

 

Page 

10

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15

 

Instructions for  
Continued Airworthiness 

4.4  Inspection of Element (Severe Conditions) 

In these conditions it may be necessary clean and inspect the elements more 
frequently than recommended in Section 3.  Elements used in such conditions should 
be replaced if element filter media or fine mesh screen is severely degraded.  They 
may be cleaned and serviced as many times as required during the element life.  
Regardless of the actual time in service of the elements, the physical condition of the 
element, when exposed to these harsh conditions, must remain the most important 
factor used to determine the serviceability of the element. 

At each cleaning carefully inspect the elements as follows: 

a) 

Inspect the fine mesh on the forward surface of the element pleats.  Complete 
erosion of more than .50 in. is cause for element rejection. 

b) 

Inspect the course mesh on the aft surface of the element.  Any evidence of 
mesh wire wear or general signs of mesh breakage or deterioration are cause for 
element rejection. 

c) 

After cleaning and before re-oiling, hold the element up to a light and check for 
holes in the element material greater than .020 (it is normal to observe pinholes 
in the filter media particularly at the pleat folds.  These pinholes will not allow the 
passage of dirt once the element is oiled).  Close the holes if present using a fine 
pick to reposition the media material to cover the hole.  Numerous holes in the 
media greater than 0.030 will reduce the filtration efficiency and are cause for 
element rejection. 

d) 

Check the condition of the element assembly: 

  Frames for security 

  Aft element latch brackets for wear and loose rivets 

  Forward element Camloc receptacles for security and loose rivets. 

Defects found are to be rectified.  Consult FDC Engineering in the event any 
repair cannot be performed using standard practices.  

When operating in the most severe conditions it is highly recommended that an 
additional serviceable, pre-oiled element be available.  This will allow continued 
service while the dirty element is being cleaned, inspected and re-oiled. 

4.5  Inspection of Element (Normal Conditions) 

At each 100 ±10 hours of operation or upon activation of the low inlet pressure warning 
light: 

  Remove the elements and inspect in accordance with paragraphs 

4.4 a, b, c & d

  Elements should be replaced after 1500 hours in service.  Service life may be 

extended upon consultation with and approval of FDC Engineering. 

Summary of Contents for aerofilter 1500 Series

Page 1: ...AIRWORTHINESS 1500EFS ENGINE INLET BARRIER FILTER SYSTEM MDHI HUGHES OH 6 A C CAYUSE This document provides information necessary for the maintenance of the 1500EFS Engine Inlet Barrier Filter System...

Page 2: ...customers with the best possible support and assistance with our products Please contact us using the information below to get the latest version of this and other documents FDC aerofilter 8 Digital D...

Page 3: ...Table 3 1 Recommended Service Intervals 7 4 0 Filter Element Servicing 8 4 1 General Information 8 4 2 Removal and Reinstallation 8 Figure 4 1 Filter Element 8 4 3 Filter Element Cleaning 9 4 4 Inspec...

Page 4: ...ely affected prior to the next scheduled servicing The pilot actuated alternate air system is provided to bypass the filter elements in the event that engine performance is degraded due to filter bloc...

Page 5: ...contained in this ICA Although best efforts will be made to distribute revisions and updates to the registered owner of the product it is ultimately the responsibility of the current user to ensure he...

Page 6: ...ss 2 0 Airworthiness Limitations The Airworthiness Limitations section specifies inspections and other maintenance required under 43 16 and 91 403 of the Federal Aviation Regulations unless an alterna...

Page 7: ...triction However large obvious debris such as leaves brush litter etc should be removed prior to flight Good judgment and practice will ensure safe operation as well as long filter life Inspections sc...

Page 8: ...as when removing and replacing the element from the duct The pleated material s fragile wire mesh is easily damaged or deformed when allowed to scrape against other components Careful attention to the...

Page 9: ...tively soak element in a shallow pan of filter cleaner and allow cleaner to permeate for ten minutes NOTE DO NOT use any other solvents or materials to clean filter element DO NOT use Gasoline DO NOT...

Page 10: ...check for holes in the element material greater than 020 it is normal to observe pinholes in the filter media particularly at the pleat folds These pinholes will not allow the passage of dirt once the...

Page 11: ...use Transmission Oil DO NOT use Hydraulic Fluid DO NOT use Lightweight Oils WD 40 LPS etc a Fill sprayer with recommended quantity of FDC aerofilter Oil 15 Fluid Ounces b Charge sprayer with compress...

Page 12: ...actuator on to mount bracket stud and secure with washer nut and cotter pin Note nut to be finger tight then backed off to next slot for pin installation b Position lug end of actuator between spring...

Page 13: ...ve forward inlet fairing b Disconnect DPS harness c Disconnect DPS pressure line d Remove side cover of aft inlet fairing e Remove 4 screws nuts and washers attaching DPS to rear of housing assembly R...

Page 14: ...essure port c Apply suction to test port and check that cockpit annunciator light comes on at 9 ins H2O 1 in H2O d Replace DPS if out of limits e Remove test equipment and replace pressure tube assemb...

Page 15: ...R to OPEN if TOT is within limits Annunciator light on at all power settings Filter element is dirty Select ALT AIR to OPEN only if TOT for power required exceeds limits while still in harsh environme...

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