交通部民用航空局

發布日期

2010/01/27

適用性說明

This AD applies to the oxygen cylinder assemblies, approved under United States Department of Transportation Regulations for Type 3HT cylinders, identified in Table 1 of this AD. These oxygen cylinder assemblies may be installed on various transport airplanes, certificated in any category, identified in but not limited to the airplanes included in Table 2 of this AD. Table 1--Affected Oxygen Cylinder Assembly Part Numbers Manufacturer Part Numbers AVOX Systems *6350A34 series 800112-03 800112-10 800112-13 801293-03 801307-00 801307-01 801307-02 801307-03 801307-07 801307-09 801307-23 801307-24 801365-04 801365-14 801375-00 801977-05 *8915 series (*For example, 6350A34-X-X or 8915XX-XX, where “X” denotes a part number digit) B/E Aerospace 176018-115 176112-115 176177-115 176181-115 176529-97 Table 2--Affected Airplanes Manufacturer Model Airbus A300 B4-620, B4-622, B4-605R, and F4-605R airplanes A310-203, -204, -221, -222, -304, and -324 airplanes A318-111 and -112 airplanes A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes A320-111, -211, -212, -214, -231, -232, and -233 airplanes A321-111, -112, -131, -211, and -231 airplanes A330-301, -321, and -322 airplanes A340-211 and -212 airplanes A340-311 and -312 airplanes The Boeing Company 707-100 long body, -200, -100B long body, and -100B short body series airplanes; and 707-300, -300B, -300C, and -400 series airplanes 727, 727C, 727-100, 727-100C, 727-200, and 727-200F series airplanes 737-100, -200, -200C, -300, -400, -500, -600, -700, -700C, -800, -900, and -900ER series airplanes 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747SR, and 747SP series airplanes 757-200, -200PF, -200CB, and -300 series airplanes 767-200, -300, -300F, and -400ER series airplanes 777-200, -200LR, -300, -300ER, and 777F series airplanes Gulfstream Aerospace Corporation G-IV airplanes McDonnell Douglas Corporation DC-8-11, DC-8-12, DC-8-21, DC-8-31, DC-8-32, DC-8-33, DC-8-41, DC-8-42, DC-8-43, DC-8-51, DC-8-52, DC-8-53, and DC-8-55 airplanes DC-9-11, DC-9-12, DC-9-13, DC-9-14, DC-9-15, DC-9-15F, DC-9-21, DC-9-31, DC-9-32, DC-9-32 (VC-9C), DC-9-32F, DC-9-32F (C-9A, C-9B), DC-9-33F, DC-9-34, DC-9-34F, DC-9-41, DC-9-51, DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), and DC-9-87 (MD-87) airplanes DC-10-10, DC-10-10F, DC-10-15, DC-10-30, DC-10-30F (KC-10A and KDC-10), and DC-10-40 airplanes MD-10-10F and MD-10-30F airplanes MD-11 and MD-11F airplanes MD-88 airplanes MD-90-30 airplanes Short Brothers PLC SD3-30, SD3-SHERPA, and SD3-60 SHERPA airplanes

型別

AVOX Systems and B/E Aerospace Oxygen Cylinder Assemblies, as Installed on Various Transport Airplanes

民航局AD編號

CAA-2009-12-003A

原發布國

FAA

原AD編號

2009-21-10R1

生效日期

2010/02/04

主旨摘要

To prevent an oxygen cylinder from rupturing, which, depending on the location, could result in structural damage and rapid decompression of the airplane, damage to adjacent essential flight equipment, deprivation of the necessary oxygen supply for the flightcrew, and injury to cabin occupants or maintenance or other support personnel.

參考資訊（版本/ATA/SB）

This AD revises AD 2009-21-10(CAA-2009-12-003). Ref. Air Transport Association (ATA) of America Code 35: Oxygen.

存檔序號

99-01-013

專業分項

Systems

產品類別

Application

備註

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