Document ID: chunk:federal_register_of_legislation:F2008L00386:body:0:p3
Version: federal_register_of_legislation:F2008L00386
Segment Type: other
Provision Reference: 
Character Range: 8730–13055

22 August 1996     Stringer Joint Piece Part Number 14153014 at Station 130
001-12-96  13 December 1996   Fire Protection - Engine and Nacelle Fire - Extinguisher System - To find and replace defective hoses in the system
006-12-96  4 December 1996    Flight Controls - Aileron Control - Incorrect heat treatment chain links installed in the control column
004-07-97  8 July 1997        Electrical Power - Introduction of improved sealing to electrical connectors on rear pressure bulkhead area
009-07-97  25 July 1997       Additional Side Plates to Up-lock Attachments
004-08-97  9 August 1997      Main Baggage Compartment Reduced Loading Limitations
001-09-97  12 September 1997  Passenger Door Increased Diameter 'G' Lock Rollers
015-11-97  10 November 1997   Rear Baggage Bay Fire Extinguisher Placard
007-08-98  20 August 1998     Front Row Passenger Seats

             006-09-98          11 September 1998                                                                                                       Elevator and Rudder Controls at Rear Pressure Bulkhead
005-04-99    5 April  1999      Fuel - Distribution - Protection of the cable assembly to the fuel standby (boost) pump (left and right)
004-05-99    11 May 1999        Temporary Placard to Prohibit Aircraft Pushback with Engines Running
007-09-99    17 September 1999  Landing Gear - Inspection and rectification of main landing gear retract actuator ramrod piston retraining nut
002-03-2000  10 March 2000      Flight Controls - Rudder Pedals - Elimination of potential restricted movement of the rudder pedals
003-03-2000  15 March 200       Hydraulic Hand Pump Mounting Brackets
006-05-2000  31 May 2000        Flying Controls - Introduction of an elevator cable tension regulator incorporating secondary locking of the regulator
001-07-2001  3 July 2001        Nose Landing Gear Life limits
001-11-2001  5 November 2001    Propeller - Reduced performance due to loss of propeller efficiency
006-11-2001  7 November 2001    Flight Controls - Trim Screw Jack Chain Replacement
007-01-2002  24 January 2002    Main Landing Gear Door Drive Trunnion Pins
006-08-2002  6 August 2002      Landing Gear - Introduction of overhaul lives for auxiliary components installed on the main and nose gear
006-06-2003  27 June 2003       Aileron Rear Spar
G-2005-0006  8 February 2005    ATA 24 - Electrical System - Modification

              Table 2
                 EASA AD                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 Effective Date                                                    Title
   2007-0268  22 October 2007                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         Placards & Marking - Propeller Limitations Placard - Replacement
              Note 1:  CAA(UK) and EASA ADs issued after28 September 2003 may be accessed via the internet at the following URL:

               http://ad.easa.europa.eu/
              Note 2:  CAA(UK) ADs issued before 28 September 2003 are listed in CAA(UK)
              CAP 476 which may be accessed via the internet, by following the links at the following URL:

               http://www.caa.co.uk/default.aspx?catid=1443&pagetype=90
              Note 3:  Australian ADs previously issued in the CAO 105 AD/J41 series are no longer effective.  However these ADs will be reviewed and, if necessary, will be reissued in this series.
Compliance:   For Requirements 1 and 2 - Within 30 days after the effective date of this Directive or prior to the issue of