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时间:2011-10-31 12:06来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

(3) If either rod end is corroded, prior to further flight replace the affected rod end with a serviceable part. 

(4) If the rudder trim mechanism is incorrectly installed, or if either rod end bearing is binding, prior to further flight replace the affected connecting rod and rod end assembly with


 CAD1996-MTRO-04 /39-1723
serviceable parts.
(5) If corrosion or binding is not found, reinstall the fairing strip and return the airplane to service. 
NOTE 1: Fairchild Aircraft Service Notes 26-SN-061, 226-SN-162, and 227-SN-074 pertain to the subject of this AD. 
NOTE 2: Although not required by this AD, the inspections specified in this AD should be included in the regular aircraft maintenance program.
(b) Airplanes may be flown in accordance to FAR 21.197 and 21.199 to a location where this AD may be accomplished. 

(c) An alternate method of compliance or adjustment of the compliance times that provides an equivalent level of safety may be approved by the Manager, Airplane Certification Office, Southwest Region, FAA, Fort Worth, Texas 76193-0150; Telephone


(817) 624-5150.
NOTE 3: The request should be forwarded through an FAA Maintenance Inspector, who may add comments and then send it to the Manager, Airplane Certification Office, Fort Worth, Texas 76193-0150.
This amendment (39-6837, AD 90-24-03) becomes effective on January 25, 1991, as to all persons except those persons to whom it was made immediately effective by priority letter AD 90-24-03, issued November 20, 1990, which contained this amendment. 
五. 生效日期:1996年 9月 25日
六. 颁发日期:1996年 9月 25日
 CAD1996-MTRO-04 /39-1723
七. 联系人:  祝海鹰               民航中南管理局适航处 02086122536
中国民用航空总局 CIVIL AVIATION
           ADMINISTRATION OF CHINA
C A A C

适航指令
           AIRWORTHINESS  DIRECTIVE

本指令根据中国民用航空规章《民用航空器适航指令规定》(CCAR-39)颁发,内容涉及飞行安全,是强制性措施。如不按规定完成,有关航空器将不再适航。
编号:CAD1996-340B-10 修正案号:39-1724
一. 标题:取消 CAD96-340B-01
二. 适用范围: SAAB 340和SAAB 2000飞机。
三. 参考文件:
1.SAD
NO 1-099 颁发日期 96年 8月 30日;

    2.CAD96-340B-01 修正案 39-1548;

 3.SAD
NO 1-083 修改 1。


四. 原因、措施和规定 本适航指令替代 CAD1996-340B-01,39-1548
    由于俯仰配平系统的功能检查间隔已写入SAAB 2000的MRB报告附录4和SAAB 340的MRB报告第F部分,决定取消CAD96-340B-01修正案39-1548。
五. 生效日期:1996年 9月 26日
六. 颁发日期:1996年 9月 26日
七. 联系人: 祝海鹰
 CAD1996-340B-10 /39-1724
              民航中南管理局适航处 02086122536
 
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本文链接地址:CAAC 适航指令 AIRWORTHINESS DIRECTIVE 16(10)