(ii) Aeroplane able to land at an airport etc. suited to emergency landings even with two engines inoperative|Lifejackets or equivalent emergency equipment|Numbers equal to number of persons on board|(iii) First aid kits shall contain a full set of medical supplies.〔【出典】日本法令外国語訳データベースシステム 〕
(1) At least 15 hours of glide by solo flight and at least 20 times of landing with glide, and at least 25 hours of powered flight (including by an aircraft) by solo flight and at least 20 times of landing while an engine is on (including by an aeroplane). However, landing while an engine is on can be excluded for any landings that are not suitable for a landing with operating engine.〔【出典】日本法令外国語訳データベースシステム 〕
(i) Aeroplane able to fly and maintain the minimum safe altitude prescribed in the operating manual and to land at the destination airport etc. or the alternative airport etc., even with a critical engine inoperative|Waterproof Portable Light|1|(ii) Lifeboats shall be capable of accommodating all persons on board.〔【出典】日本法令外国語訳データベースシステム 〕
(1) Any operator of an aircraft with airworthiness certification may apply for spare part certification by the Minister of Land, Infrastructure, Transport and Tourism with regard to spare parts such as engines, propellers or other devices critical for aircraft performance and safety as may be specified by Ordinances of the Ministry of Land, Infrastructure, Transport and Tourism.〔【出典】日本法令外国語訳データベースシステム 〕
(2) A pilot in command shall, in the case of confirming the matters listed under item (i), conduct the inspection of aircraft logbook and other records on maintenance services, inspection of the exterior of aircraft and ground trial run of engines, and other elemental inspection of aircraft.〔【出典】日本法令外国語訳データベースシステム 〕
(3) The provisions of the preceding two paragraphs shall not apply to a person who serves on board an aircraft specified by Ordinances of the Ministry of Land, Infrastructure, Transport and Tourism to engage in pilotage (including handling airframe systems and engines on board an aircraft) or a person who is engaged in the on-board operations of aircraft for the purpose of test flights etc. under permission of the Minister of Land, Infrastructure, Transport and Tourism.〔【出典】日本法令外国語訳データベースシステム 〕
(3) Voice recording devices shall be operated continuously over the period from the commencement of engine operation for the purpose of flight to the cessation of engine operation.〔【出典】日本法令外国語訳データベースシステム 〕
On August 3rd, a group made up of people from Yamaha Motor Company succeeded in making a flight of 10.9 kilometers in a human-powered airplane."MB001835", "2419266"
W型発動機
W-type engine《機械》
このグループは1983年にヤマハ発動機の技術者たちによって結成されました。
The Yamaha Motors group was organized in 1983 by the company's engineers."MB001835", "2472886"
(h) Minimum flight altitude|Minimum flight altitude shall be specified such that an aircraft is able to maintain continuous radio contact with the ATC unit, taking into account the effects of navigational error and air turbulence, and in the case of a multi-engined aircraft, that it is able to land at any suitable aerodrome in case of the failure of one engine.〔【出典】日本法令外国語訳データベースシステム 〕
(i) Emergency procedures|Emergency procedures performed by flight crew, flight dispatcher, cabin crew and other staff in order to secure the safety of aircraft and passengers corresponding to each case of emergency such as engine failure, radio failure, interception, or emergency landing, and the location of emergency equipment on board aircraft, shall be clearly specified.〔【出典】日本法令外国語訳データベースシステム 〕
(ii) Types of aircraft other than listed under (i) and equipped with turbojet engines or turbofan engines|The flight time of a pilot having served as a pilot-in-command of aeroplane used for air transport services having a maximum take-off weight exceeding 5,700 kilograms shall be 1,000 hours or more and the flight time of said pilot as a pilot-in-chief of aeroplane in general shall be 2,000 hours or more.〔【出典】日本法令外国語訳データベースシステム 〕
(v) One (1) collision avoidance system in compliance with the standards laid down in Annex 10 Vol. 4 Amendment 77 of the Convention on International Civil Aviation (limited to aeroplane with more than nineteen passenger seats or maximum take-off weight exceeding 5,700 kilograms, and with turbine engines).〔【出典】日本法令外国語訳データベースシステム 〕
First of all, the participants visited the main plant of Yamaha Motor Co., which develops, manufactures, and sells the Yamaha motorbikes, motorboats, and so on that are popular around the world."IC017017", "2296601"
(iv) One (1) Ground Proximity Warning System which possesses the capabilities listed below (limited to aeroplane with more than nine passenger seats or maximum take-off weight exceeding 5,700 kilograms, and with turbine engines).〔【出典】日本法令外国語訳データベースシステム 〕
(iv)-2 One (1) Ground Proximity Warning System with the following capabilities (limited to aeroplane with more than nine passenger seats or maximum take-off weight exceeding 5,700 kilograms, and with piston engines).〔【出典】日本法令外国語訳データベースシステム 〕
A rating in connection with the rating of functions permitted pursuant to Article 25 paragraph (3) of the Act shall be granted separately for aircraft system structure, aircraft system equipment, piston engine, turbine engine, propellers, instruments, electronic equipment, electrical equipment, or radio communication equipment, based on the type of operation pertaining to the examinations.〔【出典】日本法令外国語訳データベースシステム 〕
The aircraft logbook which the user of an aircraft is required to keep under the provisions of Article 58 paragraph (1) of the Act are: for aircraft other than those listed under any of the items of Article 131 of the Act, a flight logbook, an engine logbook and a propeller logbook or glider logbook; and for aircraft listed under any of the items of Article 131 of the Act, a flight logbook.〔【出典】日本法令外国語訳データベースシステム 〕
The records that users of aircraft are required to keep, pursuant to the provisions of paragraph (2) of Article 61 of the Act, are Flight Data Recorder records related to the operations listed below (with the exception of periods when the engine(s) are stopped) (with the exception of records created more than 60 days previously).〔【出典】日本法令外国語訳データベースシステム 〕
Pursuant to the provisions of Article 60 of the Act, aeroplane used for purposes other than air transport services (limited to aeroplane with more than nine passenger seats or maximum take-off weight exceeding 5,700 kilograms, with the exception of aircraft used by the Self-Defense Forces) shall be equipped with Ground Proximity Warning System which possesses the capabilities listed below.〔【出典】日本法令外国語訳データベースシステム 〕
Aircrafts specified by Ordinances of the Ministry of Land, Infrastructure, Transport and Tourism set forth in item (ii), Article 15 of the Act shall be the aircrafts equipped with turbojet engine or turbofan engine not in conformity with the standards under paragraph (2) of Article 14 and shall exceed 34,000 kilograms of the maximum takeoff weight.〔【出典】日本法令外国語訳データベースシステム 〕
When aircraft learns that another aircraft is in emergency due to a failure of its engine, fuel shortage etc., it shall be navigated so as not to interfere with the emergency measure taken by the relevant aircraft regardless of the provisions in Articles 180 through 189.〔【出典】日本法令外国語訳データベースシステム 〕