Aircraft Flight Operation Regulations Article 300
Except for compliance with those requirements prescribed in paragraph 5 to 7 of this article, no person may operate a civil aircraft unless it is equipped with approved automatic type ELT.Each ELT required in the preceding paragraph must be attached to the aircraft in such a manner that the probability of damage to the transmitter in the event of crash impact is minimized. Fixed and deployable automatic type transmitters must be attached to the aircraft as far aft as practicable.The battery of ELT shall be replaced or charged when:1. When the transmitter has been in use for more than 1 cumulative hour; or2. When 50 percent of their useful life (or, for rechargeable batteries, 50 percent of their useful life of charge) has expired, as established by the transmitter manufacturer under its approval.The new expiration date for replacing (or recharging) the battery must be legibly marked on the outside of the transmitter and entered in the aircraft maintenance record. Subparagraph 2 of preceding paragraph of this article does not apply to batteries that are essentially unaffected during probable storage intervals.Each ELT required in paragraph 1 of this article must be inspected within 12 calendar months after the last inspection for:1. Proper installation;2. Battery corrosion;3. Operation of the controls and crash sensor; and4. The presence of a sufficient signal radiated from its antenna.No person other than required crew members may be carried aboard an aircraft being ferried in the condition mentioned below:1. Ferry a newly acquired aircraft from the place where possession of it was taken to a place where the ELT is to be installed; and2. Ferry an aircraft with an inoperative ELT from a place where repairs or replacements cannot be made to a place where they can be made.Paragraph 1 of this article shall not apply to:1. For turbojet-powered aircraft which first time airworthiness before January 1, 2004; or2. Aircraft while engaged in training operations conducted entirely within a 50-nautical mile radius of the airport from which such local flight operations began; or3. Aircraft while engaged in flight operations incident to design and testing; or4. New aircraft while engaged in flight operations incident to their manufacture, preparation, and delivery; or5 Aircraft certificated for research and development purposes; or6. Aircraft while used for showing compliance with pertinent airworthiness regulatory requirements, crew training, exhibition, air racing, or market surveys; or7. Aircraft equipped to carry not more than one person; or8. Free balloon.9. An aircraft during any period for which the transmitter has been temporarily removed for inspection, repair, modification, or replacement.Subparagraph 9 of preceding paragraph shall comply with the following:1. No person may operate the aircraft unless the aircraft records contain an entry which includes the date of initial removal, the make, model, serial number, and reason for removing the transmitter, and a placard located in view of the pilot to show “ELT not installed”; and2. No person may operate the aircraft more than 90 days after the ELT is initially removed from the aircraft.
中文原文 航空器飛航作業管理規則第300條
航空器應裝置自動方式發射之緊急定位發報機，並保持作用正常，始得飛航。
但符合第六項之情形者，不在此限。
依前項所安裝之緊急定位發報機，應裝置於航空器遭受撞擊時受損最小之部位。
但自動固定式及自動施放式之緊急定位發報機應儘可能裝置於航空器之最尾端。
緊急定位發報機之電池，有下列情形之一時，應予更換或充電：
一、使用累積超過一小時。
二、使用壽命超過原製造廠核准壽命百分之五十或充電電池超過充電壽命百分之五十。
緊急定位發報機之電池更換後之最新有效日期應標示於緊急定位發報機明顯處，並記載於維護紀錄內。
保存期限內電力不會衰退之電池不受前項第二款之限制。
依第一項所裝置之緊急定位發報機，應於每十二個月內執行下列檢查：
一、正確裝置檢查。
二、電池腐蝕檢查。
三、控制器及撞擊作用感應器之操作檢查。
四、天線發射足夠信號強度檢查。
航空器有下列情形，除必要之組員外，不得搭載其他人員飛航：
一、新購之航空器運渡至裝置緊急定位發報機安裝地點之飛航。
二、緊急定位發報機失效需運渡至有能力修理或更換緊急定位發報機地點之飛航。
有下列情形之一者，不適用第一項規定：
一、中華民國九十三年一月一日前首次適航之渦輪噴射發動機之航空器。
二、航空器於起飛機場半徑五十浬以內從事本場訓練。
三、航空器從事設計及測試之飛航作業。
四、新航空器之製造、準備及交機飛航作業。
五、檢定為研究及發展用途之航空器。
六、航空器從事證明符合適航規定、試飛組員訓練、展示、空中競賽及市場調查。
七、單座之航空器。
八、自由氣球。
九、緊急定位發報機自航空器暫時移出執行檢查、修理、改裝或更換。
前項第九款應符合下列規定：
一、航空器之維護紀錄簿已記載緊急定位發報機移出日期、原製造廠、型式、序號及移出原因，並於駕駛員易見之處標示緊急定位發報機暫時移出。
二、緊急定位發報機自航空器移出後之飛航不得超過九十日。
但符合第六項之情形者，不在此限。
依前項所安裝之緊急定位發報機，應裝置於航空器遭受撞擊時受損最小之部位。
但自動固定式及自動施放式之緊急定位發報機應儘可能裝置於航空器之最尾端。
緊急定位發報機之電池，有下列情形之一時，應予更換或充電：
一、使用累積超過一小時。
二、使用壽命超過原製造廠核准壽命百分之五十或充電電池超過充電壽命百分之五十。
緊急定位發報機之電池更換後之最新有效日期應標示於緊急定位發報機明顯處，並記載於維護紀錄內。
保存期限內電力不會衰退之電池不受前項第二款之限制。
依第一項所裝置之緊急定位發報機，應於每十二個月內執行下列檢查：
一、正確裝置檢查。
二、電池腐蝕檢查。
三、控制器及撞擊作用感應器之操作檢查。
四、天線發射足夠信號強度檢查。
航空器有下列情形，除必要之組員外，不得搭載其他人員飛航：
一、新購之航空器運渡至裝置緊急定位發報機安裝地點之飛航。
二、緊急定位發報機失效需運渡至有能力修理或更換緊急定位發報機地點之飛航。
有下列情形之一者，不適用第一項規定：
一、中華民國九十三年一月一日前首次適航之渦輪噴射發動機之航空器。
二、航空器於起飛機場半徑五十浬以內從事本場訓練。
三、航空器從事設計及測試之飛航作業。
四、新航空器之製造、準備及交機飛航作業。
五、檢定為研究及發展用途之航空器。
六、航空器從事證明符合適航規定、試飛組員訓練、展示、空中競賽及市場調查。
七、單座之航空器。
八、自由氣球。
九、緊急定位發報機自航空器暫時移出執行檢查、修理、改裝或更換。
前項第九款應符合下列規定：
一、航空器之維護紀錄簿已記載緊急定位發報機移出日期、原製造廠、型式、序號及移出原因，並於駕駛員易見之處標示緊急定位發報機暫時移出。
二、緊急定位發報機自航空器移出後之飛航不得超過九十日。