AD 2008-16-15 Airworthiness Directives; Eclipse Aviation Corporation Model EA500 Airplanes

Models named: EA500. Read the applicability below — it usually turns on serial or part numbers too.

This AD affects Model EA500 airplanes, all serial numbers, that are certificated in any category.

To address this problem, you must do the following, unless already done:   Actions Compliance Procedures (1) Insert the following into the emergency and normal procedures sections of the applicable EA500 pilots operating handbook (POH) and airplane flight manual (AFM): (i) For POH/AFM part number (P/N) 06-122204: Temporary Revision No. 005 To EA500 POH and FAA-Approved Airplane Flight Manual, L & R ENG CONTROL FAIL, dated June 12, 2008; and Temporary Revision No. 006 To EA500 POH and FAA-Approved Airplane Flight Manual, THROTTLE STOPS, dated June 12, 2008. Before further flight after August 7, 2008 (the effective date of this AD). If you previously did this action per compliance with emergency AD 2008-13-51, then you may take “unless already done” credit for this portion of the AD. Under 14 CFR section 43.7 of the Federal Aviation Administration Regulations (14 CFR 43.7), the owner/operator holding at least a private pilot certificate is allowed to insert the AFM temporary revisions. Make an entry into the aircraft logbook showing compliance with this portion of the AD per compliance with section 43.9 of the Federal Aviation Regulations (14 CFR 43.9). (ii) For POH/AFM P/N 06-121654: Temporary Revision No. 007 To EA500 POH and FAA-Approved Airplane Flight Manual, L & R ENG CONTROL FAIL, dated June 12, 2008; and Temporary Revision No. 008 To EA500 POH and FAA-Approved Airplane Flight Manual, THROTTLE STOPS, dated June 12, 2008.     (iii) For POH/AFM P/N 06-100106: Temporary Revision No. 013 To EA500 POH and FAA-Approved Airplane Flight Manual, L & R ENG CONTROL FAIL, dated June 12, 2008; and Temporary Revision No. 014, To EA500 POH and FAA-Approved Airplane Flight Manual, THROTTLE STOPS, dated June 12, 2008.     (2) For POH/AFM P/N 06-122204, inserting Section 3, Emergency Procedures, Revision 1, dated June 25, 2008; and Section 4, Normal Procedures, Revision 1, dated June 25, 2008, satisfies the requirement specified in paragraph (e)(1)(i) of this AD. Before further flight after August 7, 2008 (the effective date of this AD). Under 14 CFR section 43.7 of the Federal Aviation Administration Regulations (14 CFR 43.7), the owner/operator holding at least a private pilot certificate is allowed to insert the AFM temporary revisions. Make an entry into the aircraft logbook showing compliance with this portion of the AD per compliance with section 43.9 of the Federal Aviation Regulations (14 CFR 43.9). (3) Inspect and modify (as applicable) the throttle quadrant assembly (TQA). (i) If you have done all the actions of emergency AD 2008-13-51 before August 7, 2008 (the effective date of this AD), an appropriately-licensed mechanic must do the inspection required by this AD at whichever of the following occurs first: Follow the instructions in Eclipse Aviation Alert Service Bulletin SB 500-76-001, REV B, dated July 22, 2008.   (A) No later than the next maintenance check; or     (B) Within the next 60 days after August 7, 2008 (the effective date of this AD).     (ii) If you have not done all of the actions of emergency AD 2008-13-51 as of August 7, 2008 (the effective date of this AD), an appropriately-licensed mechanic must do the inspection required by this AD before further flight after August 7, 2008 (the effective date of this AD). You may operate the airplane up to 10 hours time-in-service to reposition the airplane to the service center or maintenance facility doing the inspection provided the flight(s) occur(s) within 30 days after August 7, 2008 (the effective date of this AD).   (4) If any TQA fails the inspection required in paragraph (e)(3) of this AD, replace the TQA with a TQA that passes the test procedure set forth in Eclipse Aviation Alert Service Bulletin SB 500-76-001, REV B, dated July 22, 2008. Before further flight after the inspection where any TQA failed. Replace the TQA using FAA-approved procedures. Contact the FAA at the address in paragraph (f) of this AD for an FAA-approved procedure. Note: To get copies of the temporary revisions specified in this AD, contact Eclipse Aviation Corporation, 2503 Clark Carr Loop, SE., Albuquerque, NM 87105, fax: 505-241-8802; e-mail: customercare@eclipseaviation.com . Alternative Methods of

This AD is the result of the throttle position exceeding its maximum range. We are issuing this AD to reduce the likelihood of the throttle position signal exceeding its maximum range, which could cause loss of left and right engine control. This condition could result in the inability to maintain desired airspeed and/or altitude with consequent loss of control.