Husky Instructions

and tighten. Mount to 90° oil filter mount plate (12) per assembly drawings using bolts (10), washers (11), and secure with .032 MS20995-C safety wire. ** SEE WARNING (B) BELOW ** 20. Install hose assy (22) connecting the “A” port on the adapter - engine to the “A” port on the filter base. routing over mounting tubes and oil cooler scat hose and torque to 270-350 in/ lbs.. 21. Install hose assy (21) from the “B” port on the adapter - engine to the “B” port on the filter base per installation drawing routing Fwd of breather tube and up between breather tube and vacuum hose (under vacuum hose, over breather) and torque to 270-350 in/ lbs. ** SEE WARNING (A) BELOW ** 22. Install oil filter (20), torque per instructions on oil filter and secure with .032 MS20995-C safety wire. 23. Secure hose assy’s (21) & (22) to engine mount tubes using adel clamps (24) & (25), screws (26), washers (27), and locknuts (23). 24. Run engine and check for leaks. 25. Reinstall and close upper cowl. 26. Determine weight and balance, initiate a 337 form, and update the equipment list. ***** WARNING (A) ***** NO ROUTING OF FLAMMABLE FLUID LINES ABOVE EXHAUST SYSTEM, UNLESS FIRESLEEVED. INSTALLER IS RESPONSIBLE FOR INTER-RELATIONSHIP BETWEEN THIS AND OTHER ENGINE CHANGES (INCLUDING ACCESSORIES) ***** WARNING (B) ***** USE LOCTITE® 567 PST TEFLON THREAD SEALANT BEFORE INSTALLATION OF FITTINGS. DO NOT ASSEMBLE FITTINGS INTO OIL FILTER BASE WITHOUT SEALANT OTHERWISE GALLING OF MATERIAL WILL RESULT. I n s t a l l a t i o n I n s t r u c t i o n s N o . A F C - K 0 0 5 - I I I n s t a l l a t i o n I n s t r u c t i o n s N o . A F C - K 0 0 5 - I I I n s t a l l a t i o n I n s t r u c t i o n s N o . A F C - K 0 0 5 - I I I n s t a l l a t i o n I n s t r u c t i o n s N o . A F C - K 0 0 5 - I I I n s t a l l a t i o n I n s t r u c t i o n s N o . A F C - K 0 0 5 - I I INSTRUCTIONS FOR CONTINUED AIRWORTHINESS A/C Make : Aviat Model: Husky S/N: ________________ Reg#: ___________________ Revision: Date: 01/08/2000 This sixteen item checklist are Instructions for Continued Airworthiness (ICA), to comply with FAA Handbook Bulletin for Airworthi- ness (HBAW-98-18 Dated October 7, 1998), are applicable to the aircraft above when the following equipment is installed: SYSTEM:Airwolf Remote Mount Oil Filter System. ITEM CHECKLIST INFORMATION 1. Introduction: This section briefly describes the aircraft, engine, propeller, or component that has been altered. Include and other information on the content, scope, purpose, arrangement, applicability, definitions, abbreviations, precautions, units of measure- ment, reverenced publications, and distribution of the ICA as applicable. Comment: ______Aviat Husky __________with Lycoming __O360 Series______ engine. Aircraft Model Engine Model 2. Description: Of the major alteration, it’s function including an explanation of it’s interface with other systems, if any. Comment: Installation of Airwolf Remote Mounted Oil Filter Kit P/N AFC-K005 3. Control: Operation information: Or special procedures if any. Comment: Pre-heating of both the engine and engine oil is recommended prior to starting the engine during periods of cold weather where the temperature is 30°F or below. 4. Servicing information: Such as types of fluids used, servicing points, and location of access panels, as appropriate. Comment: Oil System to be serviced in accordance withLycoming Service Bulletin 480C or higher. Oil should be changed at least once each 12 months. Cut the old filter open with Airwolf AFC-470 oil filter cutter at each oil change and inspect for metal contamination or any evidence that may indicate impending engine problems. 5. Maintenance Instructions: Such as recommended inspection/maintenance periods in which each of the major alteration compo- nents are inspected, cleaned, lubricated, adjusted, tested, including applicable wear tolerances and work recommended at each scheduled maintenance period. This section can refer to the manufactures instructions for the equipment installed where appropri- ate e.g. functional checks, repairs, inspections.) It should also include any special notes, cautions, or warnings as applicable. Comment: Inspect for security at each annual or 100 hr . inspection. After any oil change, always ground run the engine and check for leaks before flight. 6. Trouble shooting information: Information describing probably malfunctions, how to recognize those malfunctions, and the remedial actions to be taken. Comment:__N/A 7. Removal and replacement information: This section describes the order and method of removing and replacing products, parts, and any necessary precautions. This section should also describe or refer to the manufacture's instructions to make required tests, trim checks, alignment, calibrations, center of gravity changes, lifting or shoring, etc., if any. Comments:__N/A 8. Diagrams: Of access plates and information, if needed, to gain access for inspection. Comment:__N/A 9. Special inspection requirements: Such as X-ray, ultrasonic testing, or magnetic particle inspection, if required. Comment: __N/A 10. Application of protective treatments: To the affected area after inspection and/or maintenance, if any. Comment:__N/A Form AFC-K005-ICA Revised 10/01/00 Airwolf Filter Corp 15369 Madison Rd Middlefield, OH 44062 11. Data: Relative to structural fasteners such as type, torque, and installation requirements if any. Comment:__N/A 12. List of special tools: Special tools that are required, if any. Comment:__N/A 13. For commuter category aircraft: The following additional information must be furnished, as applicable: A. Electrical Loads B. Methods of balancing flight controls. C. Identification of primary and secondary structures> D. Special repair methods applicable to the airplane. Comment:__N/A 14. Recommended overhaul periods: Are required to be noted on the ICA when an overhaul period has been set by the manufac- turer of a component, or equipment. If there is no overhaul period, the ICA should state for item 14: “No additional overhaul time limitations.” Comment:__N/A 15. Airworthiness Limitation Section: Include any “approved” airworthiness limitations identified by the manufacturer of FAA type Certificate Holding Office (e.g., An STC incorporated in a larger field approved major alteration may have an airworthiness limita- tion.) The FAA inspector should not establish, alter, or cancel airworthiness limitations without coordinating with the appropriate FAA type Certificate Holding Office. If there are no changes to the airworthiness limitations, the ICA should state for item 15: “No additional airworthiness limitations” or “ Not Applicable.” Comment:__N/A 16. Revision: This section should include information on how to revise the ICA. For example, a letter will be submitted to the local FSDO with a copy of the revised FAA Form 337 and revised ICA. The FAA inspection accepts the change by signing Block 3 and including the following statement: “The attached revised/new Instructions for Continued Airworthiness (date_______) for the above aircraft or component major alteration have been accepted by the FAA, superseding the Instructions for Continued Airworthiness (date_______).” Once the revision has been accepted, a maintenance record entry will be made, identifying the revision, its location, date of the Form 337. Comment:__ A letter will be submitted to the local FSDO with a copy of the revised FAA Form 337 and revised ICA. The FAA inspector accepts the change by signing Block 3 and including the following statement: “The attached revised/new Instructions for Continued Airworthiness (date_______) for the above aircraft or component major alteration have been accepted by the FAA, superseding the Instructions for Continued Airworthiness (date_______).” Once the revision has been accepted, a maintenance record entry will be made, identifying the revision, its location, date of the Form 337. NOTE: Implementation and Record Keeping: For major alterations performed in accordance with FAA Field Approval policy, the owner operator operating under part 91 is responsible for ensuring that the ICA is made part of the applicable section 92.409 inspection program for their aircraft. This is accomplished when a maintenance entry is made in the aircraft’s maintenance record in accordance with section 43.9. This entry recorded the major alteration and identifies the original ICA location (e.g., Block 8 of FAA Form 337, dated 5/28/98) along with a statement that the ICA is now part of the aircraft’s inspection/maintenance requirements. For major alterations performed in accordance with field approval on air carrier aircraft, the air carrier operator is responsible for ensuring that the ICA is made part of the applicable inspection/maintenance program for their aircraft. If a procedure is not currently included in the operator’s manual to incorporate ICA, this process will need to be appropriately addressed (i.e. the operator submits a revision to its maintenance program to the applicable certificate-holding district office (CHDO). For aircraft inspected under an Approved Aircraft Inspection Program (AAIP), the operator will submit a change to the CHDO in accordance with section 135.419b). For air carrier aircraft inspected using an annual/100 hour inspection program, a reference to the new ICA will be made in the aircraft’s maintenance record in accordance with section 43.9. This entry records the major alteration and identifies the original ICA location (e.g., ICA are located/attached to Block 8 of FAA Form 337, dated 5/28/98). In addition, the operator will request a revision to the operator’s Operations Specifications, additional maintenance requirements, which incorporates the ICA into the inspection program. INSTRUCTIONS FOR CONTINUED AIRWORTHINESS Form AFC-K005-ICA Revised 10/01/00 EQUIPMENT - ITEM LBS. LONG LONG REMOTE OIL FILTER 4.75 36.0 171.0 SURPLUS EQUIPMENT WEIGHT ARM-INCHES MOMENT - IN/LBS. WEIGHT AND BALANCE REPORT AVIAT HUSKY A-1 Airwolf Filter Corp. Revisions 03/30/93 Dwg# AFC-D-0014 John P. Kochy ASSEMBLY DRAWING# AFC-D-0014 MATERIAL LIST Index Part Number Description Qty 01. LYC-10 Adapter - Engine, Full Flow (1) 02. 61173 Adapter Base Gasket (1) 03. AN833-8D Bulkhead Fitting, 90° (1) 04. AN815-8D Union, Flaired Tube (1) 05. AN6289-8D Bulkead Nut (1) 06. MS35769-11 Gasket, Oil Temp. Sensor (1) 07. MS35769-21 Gasket, Thermostatic Valve (1) 08. MS28773-08 Boss Gasket (1) 09. MS9387-08 "O" Ring (2) Assembly Drawing. LYC-10 Adapter - Engine, Full Flow 03. 05. 04. 09. 01. 07. 06. 09. 08. Locate fitting towards bottom LH mounting hole. Airwolf Filter Corp. Revisions 03/30/93 Dwg# AFC-D-0015 John P. Kochy ASSEMBLY DRAWING# AFC-D-0015 Assembly Drawing. OFB-10 Oil Filter Base Husky A-1 MATERIAL LIST Index Part Number Description Qty 10. AN4H-4A Bolt, Drilled Head (4) 11. AN960-416 Flat Washers (16) 12. OFM-11 Oil Filter Mount Plate - 90° (1) 13. DBL-10 Doubler Plate (1) 14. AN4-5A Bolt (6) 15. MS20365-428A Locknut (6) 16. OFB-10 Oil Filter Base (1) 17. AN816-8D Fitting (1) 18. MS20823-8D Fitting, 45° (1) 19. OFS-10 Oil Filter Stud (1) 20. AFC-500 Oil Filter (1) 10. 16. 18. 19. 20. 15. 13. 14. 17. 11. 12. 11. Revisions 03/30/93 Dwg# AFC-D-0016 John P. Kochy Installation Drawing. Hose Assy's. Husky A-1 LH Side Airwolf Filter Corp. MATERIAL LIST Index Part Number Description Qty 21. F1300008-0236 Hose Assy w/Firesleeving TSO'D (1) 23. MS20365-1032 Locknut (1) 24. MS21919WDG-16 Adel Clamp (1) 25. MS21919WDG-12 Adel Clamp (1) 26. AN3-4A Bolt (1) 27. AN960-10 Flat Washer (1) INSTALLATION DRAWING# AFC-D-0016 24. 25. 23, 26, 27 21. Revisions 03/30/93 Dwg# AFC-D-0017 John P. Kochy Installation Drawing. Hose Assembly. Husky A-1 RH Side Airwolf Filter Corp. MATERIAL LIST Index Part Number Description Qty 22. F13000208-0344 Hose Assy w/Firesleeving TSO'D (1) 23. MS20365-1032 Locknut (1) 24. MS21919WDG-16 Adel Clamp (1) 25. MS21919WDG-12 Adel Clamp (1) 26. AN3-4A Bolt (1) 27. AN960-10 Flat Washer (1) INSTALLATION DRAWING# AFC-D-0017 24. 25. 23, 26, 27 22. Revisions 03/30/93 Dwg# AFC-D-0018 John P. Kochy Airwolf Filter Corp. MATERIAL LIST Index Part Number Description Qty 12. OFM-11 Oil Filter Mount Plate (1) 13. DBL-10 Doubler Plate (1) 16. OFB-10 Oil Filter Base (1) 20. AFC-500 Oil Filter (1) Installation Drawing. OFM-11 Oil Filter Mount Plate, DBL-10 Doubler Plate, & OFB-10 Oil Filter Base 1/4" INSTALLATION DRAWING# AFC-D-0018 13. Locate Doubler Plate (13) 1/4"Down from top of Firewall, & 1/4" Left of Voltage Regulator, LONG SIDE UP