交通部民用航空局

依據民用航空法規，航空器所有人或使用人除應遵守本國民航局所發布適航指令，亦應遵守航空器設計國之民航主管機關所通告之適航指令。

備註：點選「+」圖示，展開瀏覽「適用性說明」；點選「民航局AD編號」瀏覽更多資訊。

民航局AD編號	發布日期	原發布國	原AD編號	適用性說明	檔案下載
CAA-2006-11-015修訂	2007/01/24	EASA	2006-0354 Correction	AIRBUS aircraft A330-200, A330-300, A340-200, A340-300, A340-500 and A340-600 series, all certified models, all serial numbers, equipped with GOODRICH slide rafts on Type A doors with the following Part Numbers (PN): Doors 1 and 4, LH and RH: PN’s 7A1508-003/-005/-007/-023/-025/-027/-029/-033/-035/-037/-115/- 119/-121 Doors 2, LH: PN’s 7A1539-003/-005/-007/-023/-025/-027/-029/-033/-035/-037/-115/- 119/-121 Doors 2, RH: PN’s 7A1539-004/-006/-008/-024/-026/-028/-030/-034/-036/-038/-116/- 120/-122 Doors 3, LH: PN’s 7A1510-003/-005/-007/-023/-025/-027/-029/-033/-035/-037/-115/- 119/-121 Doors 3, RH: PN’s 7A1510-004/-006/-008/-024/-026/-028/-/030/-034/-036/-038-116/- 120/-122 2/4 Doors 3, LH: PN’s 4A3934-1/-001/-5/-7 Doors 3, RH: PN’s 4A3934-2/-002/-6/-8 The following aircraft on which no slide raft has been replaced since aircraft delivery are not affected by this Airworthiness Directive (AD): • A330, A340-200 and A340-300 aircraft with modification 40161 (i.e. with optional Type A door 3) having received the four AIRBUS modifications 50806 and 50807 and 55071 and 55072 in production, • A330, A340-200 and A340-300 aircraft without modification 40161 (i.e. with basic Type 1 door 3) having received AIRBUS modifications 50806 and 55071 in production, • A340-500 series having received the three AIRBUS modifications 50806 and 50807 and 55071 in production, • A340-500 series having received the two AIRBUS modifications 50806 and 55071 in production, • A340-600 series having received the four AIRBUS modifications 50806 and 50808 and 55071 and 55073 in production. The following aircraft on which no slide raft has been replaced since SBs embodiment are not affected by this AD: 􀁹 A330 aircraft having received AIRBUS SB A330-25-3173 Revision 01 and AIRBUS SB A330-25-3301, 􀁹 A340-200 and A340-300 series having received AIRBUS SB A340-25- 4191 Revision 01 and AIRBUS SB A340-25-4273, 􀁹 A340-500 and A340-600 series having received AIRBUS SB A340-25- 5004 Revision 01 and AIRBUS SB A340-25-5110. Reminder: It is the operator’s responsibility to ensure that any slide raft held as spare part that could be installed on the aircraft does not invalidate the compliance of the aircraft with this AD.
CAA-2004-01-016A	2007/01/24	FAA	2007-01-02	This AD applies to McDonnell Douglas Model MD-11 and -11F airplanes, as identified in Boeing Alert Service Bulletin MD11- 54A011, Revision 3, dated November 9, 2005; certificated in any category.
CAA-2004-07-015B	2007/01/22	EASA	2007-0009	AIRBUS aircraft A330-200, A330-300, A340-200 and A340-300 series, all certified models and all serial numbers. The requirements of paragraphs 1, 2 and 4 of this Airworthiness Directive (AD) are not applicable to Airbus A330-200 aircraft on which AIRBUS modification 53969 or 54833 has been embodied in production or AIRBUS Service Bulletin (SB) A330-27-3134 or SB A330-27-3136 has been embodied in service. Reminder: It is the responsibility of the operator to ensure that any spare part that has been or could be installed on the aircraft does not invalidate the compliance of the aircraft with the requirements of this AD.
CAA-2005-10-001A	2007/01/19	EASA	2007-0008	AIRBUS A330-200, A330-300, A340-200 and A340-300 aircraft, all certified models, all serial numbers, except those on which AIRBUS modification 54833 has been embodied in production or AIRBUS Service Bulletin (SB) A330-27-3136 or SB A340-27-4135 has been embodied in service. Reminder: It is the responsibility of the operator to ensure that any spare part that has been or could be installed on the aircraft does not invalidate the compliance of the aircraft with the requirements of this AD.
CAA-2003-09-027B	2007/01/19	EASA	2007-0011	AIRBUS aircraft A330-200, A330-300, A340-200 and A340-300 series, all certified models and all serial numbers except those on which AIRBUS modification 50394 or 52195 or 53969 or 54833 has been embodied in production or AIRBUS Service Bulletin (SB) A330-27-3128 or SB A340-27- 4129 or Goodrich VSB 4800-27-16 Revision 03 or SB A330-27-3136 or SB A340-27-4135 has been embodied in service.
CAA-2007-01-002	2007/01/15	EASA	2007-0005	- AIRBUS A300 MSN 0202, 0205, 0225, 0299, and 0302 aircraft in Forward Facing Crew Cockpit (FFCC) configuration except aircraft which have received in service application of AIRBUS Service Bulletin (SB) A300-21-0132, - AIRBUS A310 aircraft, all certified models, all serial numbers, except aircraft which have received in service application of SB A310-21-2062, - AIRBUS A300-600 aircraft, all certified models, all serial numbers, on which AIRBUS modification No. 03881 is embodied, except aircraft which have received either incorporation of AIRBUS modification No. 12942 during production, or application of AIRBUS Service Bulletin (SB) A300-21-6049 in service.
CAA-2007-01-001	2007/01/15	FAA	2006-26-13	Boeing Model 707-100 Long Body, -100B Long Body, -100B Short Body, -E3F, -300, -300B, and -300C Series Airplanes; Model 727-100 and -200 Series Airplanes; Model 737-200, -200C, -300, -400, and -500 Series Airplanes; Model 747-100B, 747-200B, 747- 200C, 747-200F, 747-300, 747-400, 747-400D, 747SR, and 747SP Series Airplanes; Model 757- 200 and 757-200PF Series Airplanes; and Model 767-200 and -300 Series Airplanes; Equipped With Observer or Attendant Seats
CAA-2006-07-001A	2007/01/11	EASA	2006-0178R1	- AIRBUS A300 and A300-600 aircraft, all certified models and all serial numbers, except aircraft on which AIRBUS modification No. 12994 has been embodied in production, or Airbus Service Bulletin (SB) A300-32-0448 or SB A300-32-6094 embodied in service; and - A300-600ST aircraft, all certified models and all serial numbers, except aircraft on which SB A300-32-9011 has been embodied in service (AIRBUS modification No. 19579).
CAA-2006-04-002B	2007/01/11	EASA	2006-0075R2	AIRBUS A300, A300-600 and A300-600ST aircraft, all certified models and all serial numbers, on which the main landing gear retraction actuators are equipped with sliding rods with P/N C69029-2 or C69029-3.
CAA-2006-11-005修訂	2007/01/02	FAA	2006-23-02 Correction	Raytheon Aircraft Company Models C90A, B200, B200C, B300, and B300C Airplanes

1.本局早期(2012年前)所發布AD目前未提供檔案下載服務。如欲查詢，請自行連結原發布國民航主管機關網頁，再依”原AD編號”查詢。

2.我國目前所引進航空產品原發布國民航主管機關網頁聯結如下：
Canada、EASA、FAA、Israel、JapanCAB、UK、Brazil、CAA-CZ