Document ID: chunk:federal_register_of_legislation:F2009L00178:body:0:p1
Version: federal_register_of_legislation:F2009L00178
Segment Type: other
Provision Reference: 
Character Range: 0–3265

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/ERJ-190/13 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.

Embraer ERJ-190 Series Aeroplanes
AD/ERJ-190/13 Amdt 1  Cargo Doors  2/2009

Applicability:  Embraer aircraft models ERJ 190-100 LR, ERJ 190-100 STD, ERJ 190-100 IGW, ERJ 190-200 LR, ERJ 190-200 STD and ERJ 190-200 IGW.
Requirement:       1. Remove and discard the cover plate from the door surround trim lining in accordance with Embraer Alert Service Bulletin (ASB) No. 190-52-A018.

                     a. Perform a detailed inspection (DET) for signs of interference of the door lock handle with the aft edge liner assembly.

                     b. Rework the aft edge liner assembly according to Embraer Service Bulletin (SB) No. 190-50-0006.

                   2. Remove the aft surround trim lining to perform a detailed inspection (DET) for signs of damage of the lateral roller fitting on the forward and aft cargo door frames at the fuselage in accordance with Embraer ASB No. 190-52-A018.

                     a. If no damage is found, no immediate corrective action is required.

                     b. If any damage is found, replace the lateral roller fitting with another one bearing the same part number.

                   3. Repeat the requirements detailed in Requirement 2 of this AD.

                   4. Perform the following actions on the fore and aft cargo doors:

                     a. Relocate the cargo door closed indication sensor in accordance with Embraer SB No. 190-52-0023 original issue.

                     b. Modify the cargo door lock handle mechanism and replace cargo door roller fittings P/N 170-92569-401 and P/N 170-85452-401 by new ones, according to Embraer SB No. 190-52-0027 original issue.

                5. Revise the Airplane Maintenance Program to include the operational (OPC) and functional (FNC) checks, of the fore and aft cargo doors, in accordance with the Airplane Maintenance Manual (AMM) tasks 52-31-20-720-801-A/500,
                52-31-00-710-801-A/500, 52-32-20-720-801-A/500 and
                52-32-00-710-801-A/500, dated 15 July 2008, at repetitive intervals that do not exceed 6000 flight hours.

             The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

                Definitions:

             For the purpose of this AD:

             A detailed inspection (DET) is: "An intensive examination of a specific item, installation or assembly to detect damage, failure or irregularity.  Available lighting is normally supplemented with a