Document ID: chunk:federal_register_of_legislation:F2006B09445:body:0:p2
Version: federal_register_of_legislation:F2006B09445
Segment Type: other
Provision Reference: 
Character Range: 3051–6695

50, B50, C50, D50, D50A, D50B, D50C,
                      D50E, D50E-5990, E50, F50, G50, H50, and J50

            SA4282WE Raytheon (Beech) Models 35, A35, B35, C35, D35, E35, F35, G35,
                      and 35R

                      SA4178WE  Mooney Models M20, M20A, M20C, M20D, M20E, M20F, M20G, M20J, and M20K

                      SA4234WE  The New Piper Aircraft, Inc. (Piper) Models PA-34-200, PA-34- 200T, and PA-34-220T

            SA4179WE Piper Models PA-24, PA-24-250, PA-24-260, and PA-24-400 SA4235WE Piper Models PA-44-180 and PA-44-180T
                      SA4236WE  Piper Models PA-28-140, PA-28-150, PA-28-160, PA-28-180, PA- 28-235, PA-28-151, PA-28-181, PA-28-161, PA-28-236, PA-28-
                      201T, PA-285-160, PA-28S-160, PA-28S-180, PA-28R-180, PA-
                      28R-200, PA-28R-201, PA-28R-201T, PA-28RT-201, and PA-
                      28RT-201T

                      SA4237WE  Piper Models PA-23, PA-23-160, PA-23-235, PA-23-250, and PA- E23-250

            SA4238WE Piper Models PA-30, PA-39, and PA-40

               SA4385WP Piper Models PA-31, PA-31-300, PA-31-325, and PA-31-350

                          SA4288WE  Piper Models PA-32-260, PA-32-300, PA-32S-300, PA-32-301, PA-32-301T, PA-32R-300, PA-32R-301, PA-32R-301T, PA-32RT- 300, and PA-32RT-300T

               SA2511NM Bellanca Models 17-30, 17-31, and 17-31TC SA2510NM  Bellanca Models 17-30A, 17-31A, and 17-31ATC SA4316WE               Wing Aircraft Company Model D-1
                 Requirement: 1. Unless already accomplished in accordance with previous issues of this Directive, deactivate the electric door seal inflation system by accomplishing the following:

                   1. Disconnect the battery.

b.    Locate the air pump and identify the power wire to the air pump.

c.    Trace the power wire to its connection to the aircraft's original electrical power system. Disconnect the power wire at its attachment to the aircraft's electrical power system and stow the wire end.

d.    Reconnect the battery before returning the aircraft to service.

                 2.    For non-pressurised aircraft or for aircraft that have an operating manual door seal inflation system, unless already accomplished in accordance with previous issues of this Directive:

                   1. Fabricate a placard that incorporates the following words utilising letters that are at least 2.5mm (0.1 inches) in height and install the placard on the instrument panel within the pilot's clear view:

                    "ELECTRIC DOOR SEAL INFLATION SYSTEM INOPERATIVE"

b.    Add the following statement to the Limitations section of the Flight Manual:

                    "ELECTRIC DOOR SEAL INFLATION SYSTEM INOPERATIVE"

                   This task may be accomplished by inserting a copy of this Airworthiness Directive into the Limitations section of the Flight Manual.

                 3.    For pressurised aircraft or for aircraft that do not have an operating manual door seal inflation system unless already accomplished in accordance with previous issues of this Directive:

                1. Fabricate a placard that incorporates the following words utilising letters that are at least 2.5mm (0.1 inches) in height and install the placard on the instrument panel within the pilot's clear view:

"ELECTRIC DOOR SEAL INFLATION SYSTEM INOPERATIVE THIS AIRCRAFT CAN ONLY BE OPERATED IN UNPRESSURISED FLIGHT"

                 b.    Add the following statement to the Limitations section of the Flight Manual:

"ELECTRIC DOOR SEAL INFLATION SYSTEM INOPERATIVE THIS AIRCRAFT CAN ONLY BE OPERATED IN