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-2006-11-014	2006/11/29	FAA	2006-24-05	This AD applies to Boeing Model 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, certificated in any category; as identified in Boeing Alert Service Bulletin 747-53A2675, dated October 12, 2006.
CAA-2006-06-001A(已有後續修訂版)	2006/11/29	EASA	2006-0153R1	AIRBUS A318, A319, A320 and A321 aircraft, all certified models, all serial numbers, except : - aircraft equipped with APIC APS 3200 APU, that have received AIRBUS modification (mod) 35803 in production or AIRBUS service bulletin (SB) A320-49-1070 in service. - aircraft equipped with Honeywell 131-9A APU, that have received Mod 35936 in production or SB A320-49-1075 in service.
CAA-2006-11-013(已有後續修訂版)	2006/11/28	Transport Canada Civil Aviation	CF-2006-23	Bell Helicopter Textron Canada (BHTC) Model 206 A helicopters, serial numbers 004 through 660; and 672 through 715; and Model 206 B helicopters, serial numbers 661 through 671 and 716 through 3216, having main rotor latch bolts, part numbers 206-010-169-001/-003 and 206-011-122-003.
CAA-2006-11-012A	2006/11/28	EASA	2006-0352-E	Model 228-212 aircraft, all serial numbers, if Carbon Brake Assemblies with Part Number (P/N) 5009850-1, 5009850-2, 5009850-3 or 5009850-4 are installed.
CAA-2006-10-011A	2006/11/28	EASA	2006-0315R1	AIRBUS A330 aircraft, models -201, -202, - 203, - 223, -243, -301, -321, - 322, -323, -341, -342 and -343, all serial numbers, except those on which AIRBUS modification 49202 has been embodied in production or AIRBUS Service Bulletin (SB) A330-57-3090 has been embodied in service. AIRBUS aircraft A340-200 and A340-300 series, all certified models, all serial numbers, except those on which AIRBUS modification 49202 has been embodied in production or AIRBUS Service Bulletin (SB) A340-57- 4098 has been embodied in service. This Airworthiness Directive (AD) is not applicable to A340 200/-300 aircraft repaired in accordance with Repair Drawing R57115053 or R57115051 or R57115047 (installation of Titanium Doubler) which are covered by EASA AD 2006-0314.
CAA-2006-11-012(已有後續修訂版)	2006/11/27	Germany LBA	D-2006-394	Dornier 228-212
CAA-2006-11-011	2006/11/27	FAA	2006-24-02	This AD applies to Boeing Model 747-100, 747-100B, 747-200B, 747-200C, 747-200F, 747SR, and 747SP series airplanes, certificated in any category; line numbers 001 through 430 inclusive.
CAA-2006-11-010(已有後續修訂版)	2006/11/24	EASA	2006-0350	Passenger Seats 12M( )( )-( )( )( )( )( )( ), all Part Numbers (P/N’s) as listed in Aviointeriors Service Bulletin 12M/F68-01 Revision 1 dated 2 October 2006. The affected seats are known to be installed on, but not limited to, the following aircraft: - ATR 42 series; - ATR 72 series.
CAA-2006-11-009(已有後續修訂版)	2006/11/24	ANAC	2006-09-04(BRASIL)	This Emergency Airworthiness Directive is applicable to all Embraer ERJ-190( ) aircraft models in operation.
CAA-2006-10-009A	2006/11/24	EASA	2006-0309R1	A340-211, A340-212, A340-311 and A340-312 aircraft, all serial numbers, except those on which AIRBUS modification 42445 has been embodied in production or AIRBUS Service Bulletin (SB) A340-78-4031 in service. This applicability is established considering that the aircraft have not been subject to any replacement of the thrust reverser since delivery or AIRBUS SB A340-78-4031 embodiment. It is the responsibility of the operator to check that its aircraft is in compliance with the present Airworthiness Directive (AD). Reason: During a shop inspection on thrust

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