Document ID: chunk:federal_register_of_legislation:F2007L01110:body:0:p1
Version: federal_register_of_legislation:F2007L01110
Segment Type: other
Provision Reference: 
Character Range: 0–3206

AIRWORTHINESS DIRECTIVE
On the effective date specified below, and for the reasons set out in the background section, the CASA delegate whose signature appears below revokes Airworthiness Directive (AD) AD/CESSNA 206/62 and issues the following AD under subregulation 39.001(1) of CASR 1998.  The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.

Cessna 206 Series Aeroplanes
AD/CESSNA 206/62 Amdt 1  Flexible Fuel Hose End Fittings  6/2007 DM

Applicability:  Cessna Aircraft Model 206 with the following serial numbers (S/N) - all inclusive:

                   Model 206H S/N 20608231 through 20608285; and

                   Model T206H S/N T20608515 through T20608662, T20608664 through T20608697, T20608699 through T20608714, and T20608717.
Requirement:    Group 1 - Cessna 206 Aircraft - NOT equipped with the Garmin G1000 System:

                   1. Inspect the two end fittings on each of the following hoses in the engine compartment using the instructions of Cessna Service Bulletin (SB) No.
                   SB07-71-01, Revision 1, dated 16 March 2007 or later FAA approved revisions; and the procedures given in the appendix to this AD:

                     i) Fuel strainer to engine fuel pump.

                     ii) Engine fuel pump to fuel injector servo (except T206H).

                     iii) T206H only: Engine fuel pump to the union at the aft vertical cooling baffle.

                     iv) T206H only: Union at the aft vertical cooling baffle to the fuel injector servo.

                     v) Fuel injector servo to fuel manifold valve (except turbo models).

                     vi) Turbo models only: Fuel injector servo to fuel flow transducer.

                     vii) Turbo models only: Fuel flow transducer to fuel manifold valve.

                     vii) Fuel injector servo fuel return to firewall fitting.

                   2. If any incorrect torque values are found during the inspection in accordance with Requirement 1 of this AD, establish the correct torque values in accordance with the instructions of Cessna SB07-71-01, Revision 1 or later FAA approved revisions; and the procedures given in the appendix to this AD.

             Group 2 - Cessna 206 Aircraft - Equipped with the Garmin G1000 System:

                1. Inspect the two end fittings on each of the following hoses in the engine compartment using the instructions of Cessna Service Bulletin (SB) No.
                SB07-71-01, Revision 1, dated 16 March 2007 or later FAA approved revisions; and the procedures given in the appendix to this AD:

                  i) Fuel strainer to engine fuel pump.

                  ii) Engine fuel pump to fuel injector servo (except T206H).

                  iii) T206H only: Engine fuel pump to the union at