Document ID: chunk:federal_register_of_legislation:F2008L00386:body:0:p1
Version: federal_register_of_legislation:F2008L00386
Segment Type: other
Provision Reference: 
Character Range: 0–5942

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/J4100/1 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.

BAe Systems (Operations) Jetstream 4100 Series Aeroplanes
AD/J4100/1 Amdt 1  State of Design ADs  4/2008 DM

Applicability:  Jetstream 4100 model aircraft, as identified in the individual Airworthiness Directive (AD) listed in Table 1 and 2.
Requirement:       1. Unless previously accomplished in accordance with the original issue of this Directive, determine the applicability of the ADs issued by the Civil Aviation Authority of the United Kingdom - CAA(UK), listed in Table 1 or the AD issued by the European Aviation Safety Agency - EASA, listed in Table 2.
                   2. If it is determined that an AD listed in Table 1 or 2 is applicable and has not been previously accomplished, perform the actions required by that AD.
                Table 1
                CAA(UK) AD                                                                                                                                                                                                                                                                                                         Effective Date                                                                              Title
010-03-93       16 March 1993                                                                                                                                                                                                                                                                                                      Fire Protection - Tests to detect defective joints in the fire extinguisher control system
006-04-93       6 April 1993                                                                                                                                                                                                                                                                                                       MLG Aft Doors Hinge Bracket
007-04-93       9 April 1993                                                                                                                                                                                                                                                                                                       Elevator Fasteners
013-05-93       19 May 1993                                                                                                                                                                                                                                                                                                        Main Baggage Bay Door Pressure Seal
005-06-93       10 June 1993                                                                                                                                                                                                                                                                                                       Bulkhead Assembly De-compression Vent at STN 510
013-08-93       13 August 1993                                                                                                                                                                                                                                                                                                     Flight Controls - Aileron Tab - Positive locking of hinge wire
014-08-93       24 August 1993                                                                                                                                                                                                                                                                                                     Doors - Passenger/Crew - Inspection of the electrical loom of the main entrance door
001-09-93       8 September 1993                                                                                                                                                                                                                                                                                                   Electrical Power - DC Generation - Earth post failure

           003-10-93          7 October 1993                                                                                                                                                     Rear Cabin Attendant Seat Debris Guard
010-10-93  13 October 1993    Electrical Power - Wing Rear Spar Harness - Introduction of additional clipping point
011-10-93  15 October 1993    Aileron Drive Quadrant Support Structure
007-11-93  30 November 1993   Rear Pressure Bulkhead Elevator Controls Mounting Structure
002-01-94  12 January 1994    Elevator Decouple Control Handle Placard
002-02-94  7 February 1994    Main Landing Gear Crashworthy Trunnion Pins
012-03-94  15 March 1994      Decompression Vents in Forward Stowages
003-06-94  9 June 1994        Flight Controls - Spoiler System - Inspection of spoiler activators and introduction of revised system flushing and bleeding system
004-06-94  13 June 1994       Main Door Handrail Assembly
007-08-94  12 August 1994     Hydraulic Power - Hydraulic Case