Document ID: chunk:federal_register_of_legislation:F2006B09442:body:0:p1
Version: federal_register_of_legislation:F2006B09442
Segment Type: other
Provision Reference: 
Character Range: 4–3379

Electrical Equipment

    AD/ELECT/67 Aerospace Lighting Corporation Cabin
                     Fluorescent Lighting System Components

    3/96

               Applicability: This Directive is applicable to the following Aerospace Lighting Corporation (ALC) products:

                 Lamp Connectors part number (P/N) 31.85.1.A; Series 66 fluorescent lamps;
                 Power Units P/N TR-991, TR-992, AL-0546 and AL-0514; and Power Supplies P/N 18-95D and AL-0598.
               Note 1: These products are utilised in cabin fluorescent lighting systems and are known to be installed on, but not limited to, the following aircraft series:

                 Airbus Industrie A310

                 Avion Marcel Dassault Aviation Falcon 10

                 Boeing 727, 737, 747 and 757
                 Raytheon Corporate Jets (formerly BAe) HS 125-600, -700, -800 and -1000 Bombardier Canadair               CL-600-1A11, -2A12, -2B16, -2B19,
                                           CL-601, CL-601-3A and -3R

                 Cessna 550 and 560

                 Dassault Aviation Mystere-Falcon 20 and 50

                 Embraer EMB-120

                 Gulfstream G-159, G-1159, G-1159A and G-IV

                 Israel Aircraft Industries 1124 and 1125

                 Jetstream 3100

                 Learjet 35 and 36

                 Saab SF 340A

                 Sikorsky S-76A
 COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 107 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

           Note 2: The following information is provided as an aid to the identification of fluorescent lighting system components manufactured by ALC. Components manufactured by ALC and those manufactured by SELA Laboratoire Abadie (SELA) are very similar in size, shape, colour and part number, however they may be identified by trademark. The ALC power unit can be identified by a stylised ALC logo with `Aerospace Lighting Corp' in smaller print beneath the logo while the SELA power unit can be identified by a starburst pattern incorporating the text `laboratoire, abadie, France'. The ALC lamp connector has ALC moulded into the body of the conical piece of the connector while the SELA lamp connector is only stamped in yellow ink. The ALC lamp can be positively identified by the presence of a small hole in the locking channel of each blue plastic end piece.

             Requirement: 1. Inspect the cabin fluorescent lighting system in accordance with ALC Information Bulletin IB 90-001 dated 15 August 1992 Part IV `Fluorescent Lighting System Components Identification and Inspection Procedures' sub-paragraphs B.1, 2, 3, 5, 6 and 7.

             2.    Remove and replace, in accordance with the procedures in Part IV sub-paragraphs B.4, 8 and 9 of IB 90-001 dated 15 August 1992, any part or parts found to be damaged or improperly configured.

           Note: FAA AD 95-22-01 Amdt 39-9408 refers.

           Compliance: For Requirement 1 - If not previously accomplished in accordance with AD/ELECT/56, then prior to 29 April 1996.

           For Requirement 2 - Before further flight, if any part or parts are found to be damaged or improperly configured during the Requirement 1 inspection or within five flights or 10 hours time in service, whichever occurs first, of a cabin fluorescent lighting