Document ID: chunk:federal_register_of_legislation:F2006L01697:body:0:p2
Version: federal_register_of_legislation:F2006L01697
Segment Type: other
Provision Reference: 
Character Range: 2954–5941

as daylight, hangar lighting, flashlight, or droplight and may require removal or opening of access panels or doors. Stands, ladders, or platforms may be required to gain proximity to the area being checked."

        (b) If a crew alert system message of "L FUEL FILTER, R FUEL FILTER, LR FUEL FILTER, L FUEL PRESS LOW, R FUEL PRESS LOW, or LR FUEL PRESS LOW" occurs during flight or on the ground, do the actions required by requirements 2(a) of this AD.

      3. Corrective Actions

        (a) If any tape or adhesive tape residue is found during the general visual inspection required by requirement 1 or 2 of this AD, do the actions specified in paragraphs 3(a)(i) and 3(a)(ii) of this AD.

           (i) Clean the wing fuel tank in accordance with Chapter 20-71-00 of the Bombardier Learjet 45 M45 Maintenance Manual.

           (ii) Service the affected engine fuel filter and return any engine fuel control subjected to contaminated fuel for servicing to Honeywell Engines.

        (b) If any damage is found during the general visual inspection required by paragraph 2(a)(ii) of this AD do the applicable action specified in requirements 3(b)(i) or 3(b)(ii) of this AD in accordance with Chapter
        28-20-15 of the Bombardier Learjet 45 M45 Maintenance Manual.

           (i) For damage that is repairable: Repair damaged filter.

           (ii) For damage beyond repair: Replace the damaged filter with a new filter.

      4. Reporting Requirement

      Submit a report of the applicable review and inspection results to CASA via the SDR system.  The report must include the following, as applicable:

        (a) The aeroplane serial number;

        (b) The number of flight hours on the aeroplane;

                  (c) The applicable review and inspection results (both positive and negative findings), including a description, pictures, and pertinent information for any tape or adhesive tape residue found in the wing tank(s); and

                  (d) Date of inspection of the wing tank(s);

                  (e) The number of this AD.

             Note 2:  FAA AD 2006-10-15 Amdt 39-14599 dated 9 May 2006 refers.
Compliance:     1. Within 50 flight hours or 30 days after the effective date of this AD, whichever occurs first.

                  2. (a) Within 50 flight hours or 30 days after the effective date of this AD, whichever occurs first

                  2. (b) Before further flight, after the effective date of this AD unless the actions detailed in requirement 2(a) have already been done.

                3. Before further flight, after the effective date of this AD.

                4. Within 10 days after accomplishing the review required by requirement 1 of this AD or the general visual inspection required by requirement 2 of this AD if done.
             This Airworthiness Directive becomes effective on 5 June 2006.
Background:  This AD results from reports of tape found in the wing fuel tanks.  The