Aircraft Flight Operation Regulations Article 342
No person may take off any transport category airplane which is not driven by turbine-powered engine unless:1. The take-off weight does not exceed the authorized maximum take-off weight for the elevation of the airport of take-off;2. The elevation of the airport of take-off is within the altitude range for which maximum take-off weights have been determined;3. Normal consumption of fuel in flight to the airport of intended landing will leave a weight on arrival not in excess of the authorized maximum landing weight for the elevation of that airport; and4. The elevations of the airport of intended landing and of all specified alternate airports are within the altitude range for which the maximum landing weights have been determined.No person may take off a transport category airplane which driven by turbine-powered engine unless:1. The take-off weight does not exceed the take-off weight specified in the Airplane Flight Manual for the elevation of the airport and for the ambient temperature existing at the time of take-off;2. Normal consumption of fuel in flight to the airport of intended landing and to the alternate airports will leave a weight on arrival not in excess of the landing weight specified in the Airplane Flight Manual for the elevation of each of the airports involved and for the ambient temperatures expected at the time of landing;3. The take-off weight does not exceed the weight shown in the Airplane Flight Manual to correspond with the minimum distances required for take-off, considering the elevation of the airport, the runway to be used, the effective runway gradient, the ambient temperature and wind component at the time of take-off, and, if operating limitations exist for the minimum distances required for take-off from wet runways, the runway surface condition (dry or wet). Wet runway distances associated with grooved or porous friction course runways, if provided in the Airplane Flight Manual, may be used only for runways that are grooved or treated with a porous friction course (PFC) overlay, and that the operator determines are designed, constructed, and maintained in a manner acceptable to CAA.4. Where the take-off distance includes a clearway, the clearway distance is not greater than one-half of take-off run distance.5. The accelerate-stop distance is no greater than the length of the runway plus the length of the stopway (if present); and6. The take-off distance is no greater than the length of the runway plus the length of the clearway (if present); and7. The take-off run distance is no greater than the length of the runway.
中文原文 航空器飛航作業管理規則第342條
運輸類非渦輪發動機之飛機應符合下列條件，始得起飛：
一、起飛重量不超過該飛機於起飛機場標高之最大起飛重量。
二、起飛機場標高於最大起飛重量高度範圍內。
三、於到達預定降落之機場時，其重量不超過機場標高允許之最大落地重量。
四、預定降落之機場及所有備用機場標高，均在最大落地重量之高度範圍內。
運輸類渦輪發動機之飛機應符合下列條件，始得起飛：
一、起飛重量不超過飛航手冊所規定之機場標高及起飛時外界溫度條件下之重量。
二、落地重量不超過飛航手冊所規定之機場標高及預計落地時外界溫度條件下之重量。
三、起飛重量應考量機場標高、使用跑道、跑道有效梯度、起飛溫度、風分量及乾、溼跑道情況之最短起飛距離操作限制。
如飛航手冊提供有關溝漕式或多孔摩擦力之溼跑道起飛距離，航空器所有人或使用人應確認該跑道之設計、施工及維護為合格後，始得使用溼跑道起飛距離。
四、起飛距離得包括清除區，該清除區長度不得超過該飛機型別檢定所需起飛滾行距離之一半。
五、起飛及放棄起飛距離不超過跑道長度加停止區長度。
六、起飛距離不超過跑道長度加清除區長度。
七、起飛滾行距離不超過跑道長度。
一、起飛重量不超過該飛機於起飛機場標高之最大起飛重量。
二、起飛機場標高於最大起飛重量高度範圍內。
三、於到達預定降落之機場時，其重量不超過機場標高允許之最大落地重量。
四、預定降落之機場及所有備用機場標高，均在最大落地重量之高度範圍內。
運輸類渦輪發動機之飛機應符合下列條件，始得起飛：
一、起飛重量不超過飛航手冊所規定之機場標高及起飛時外界溫度條件下之重量。
二、落地重量不超過飛航手冊所規定之機場標高及預計落地時外界溫度條件下之重量。
三、起飛重量應考量機場標高、使用跑道、跑道有效梯度、起飛溫度、風分量及乾、溼跑道情況之最短起飛距離操作限制。
如飛航手冊提供有關溝漕式或多孔摩擦力之溼跑道起飛距離，航空器所有人或使用人應確認該跑道之設計、施工及維護為合格後，始得使用溼跑道起飛距離。
四、起飛距離得包括清除區，該清除區長度不得超過該飛機型別檢定所需起飛滾行距離之一半。
五、起飛及放棄起飛距離不超過跑道長度加停止區長度。
六、起飛距離不超過跑道長度加清除區長度。
七、起飛滾行距離不超過跑道長度。