時(shí)間：2015-01-22 15:21來(lái)源：藍(lán)天飛行翻譯公司 作者：民航翻譯 點(diǎn)擊：次
|
To view this page ensure that Adobe Flash Player version 9.0.124 or greater is installed. 14 CFR 133.25 11.3.2.8 AVAILABILITY, TRANSFER, AND SURRENDER OF CERTIFICATE (a) Each person conducting a rotorcraft external-load operation shall carry a facsimile of the Rotorcraft External-Load Operator Certificate in each rotorcraft used in the operation. (b) A certificate holder shall return its certificate to the Authority— (1) If the Authority suspends or revokes its Rotorcraft External-Load Operator Certificate, or (2) If the certificate holder discontinues operations and does not resume operations within two years. 14 CFR 133.27 11.3.3 OPERATING RULES AND RELATED REQUIREMENTS 11.3.3.1 OPERATING RULES (a) No person may conduct a rotorcraft external load operation without, or contrary to, the Rotorcraft/Load Combination Flight Manual prescribed in 11.3.4.4. (b) No person may conduct a rotorcraft external load operation unless— (1) The rotorcraft complies with 11.3.2.6, and (2) The rotorcraft and rotorcraft/load combination is authorised under the Rotorcraft External Load Operator Certificate. (c) Before a person may operate a rotorcraft with an external load configuration that differs substantially from any that person has previously carried with that type of rotorcraft (whether or not the rotorcraft/load combination is of the same class), that person shall conduct, in a manner that will not endanger persons or property on the surface, such of the following flight operational checks as the Authority determines are appropriate to the rotorcraft/load combination: (1) A determination that the weight of the rotorcraft/load combination and the location of its centre of gravity are within approved limits, that the external load is securely fastened, and that the external load does not interfere with devices provided for its emergency release. (2) Make an initial liftoff and verify that controllability is satisfactory. (3) While hovering, verify that directional control is adequate. (4) Accelerate into forward flight to verify that no attitude (whether of the rotorcraft or of the external load) is encountered in which the rotorcraft is uncontrollable or which is otherwise hazardous. (5) In forward flight, check for hazardous oscillations of the external load, but if the external load is not visible to the pilot, other crewmembers or ground personnel may make this check and signal the pilot. (6) Increase the forward airspeed and determine an operational airspeed at which no hazardous oscillation or hazardous aerodynamic turbulence is encountered. (d) Notwithstanding the provisions of Part 8, the holder of a Rotorcraft External Load Operator Certificate may conduct rotorcraft external load operations over congested areas if those operations are conducted without hazard to persons or property on the surface and comply with the following: (1) The operator shall develop a plan for each complete operation and obtain approval for the operation from the Authority. Note: The plan must include an agreement with the appropriate political subdivision that local officials will exclude unauthorised persons from the area in which the operation will be conducted, coordination with air traffic control, if necessary, and a detailed chart depicting the flight routes and altitudes. (2) Each flight shall be conducted at an altitude, and on a route, that will allow a jettisonable external load to be released, and the rotorcraft landed, in an emergency without hazard to persons or property on the surface. (e) Notwithstanding the provisions of Part 8, and except as provided in 11.3.4.3(a)(4), the holder of a Rotorcraft External Load Operator Certificate may conduct external load operations, including approaches, departures, and load positioning manoeuvres necessary for the operation, below 500 feet above the surface and closer than 500 feet to persons, vessels, vehicles, and structures, if the operations are conducted without creating a hazard to persons or property on the surface. (f) No person may conduct rotorcraft external load operations under IFR unless specifically approved by the Authority. 14 CFR: 133.33 11.3.3.2 CARRIAGE OF PERSONS (a) No AOC holder may allow a person to be carried during rotorcraft external load operations unless that person— (1) Is a flight crewmember, (2) Is a flight crewmember trainee, (3) Performs an essential function in connection with the external load operation, or (4) Is necessary to accomplish the work activity directly associated with that operation. (b) The PIC shall ensure that all persons are briefed before takeoff on all pertinent procedures to be followed (including normal, abnormal, and emergency procedures) and equipment to be used during the external load operation. 14 CFR: 133.35 11.3.3.3 CREWMEMBER TRAINING, CURRENCY, AND TESTING REQUIREMENTS (a) No certificate holder may use, nor may any person serve, as a pilot in rotorcraft external load operations unless that person— (1) Has successfully demonstrated to the Authority the knowledge and skill with respect to the rotorcraft/load combination, and (2) Has in his or her personal possession a letter of competency or an appropriate logbook entry indicating compliance with paragraph (a)(1) of this section. (b) No AOC holder may use, nor may any person serve as, a crewmember or other operations personnel in Class D operations unless, within the preceding 12 calendar months, that person has successfully completed either an approved initial or a recurrent training programme. (c) Notwithstanding the provisions of paragraph (b) of this section, a person who has performed a rotorcraft external load operation of the same class and in an aircraft of the same type within the past 12 calendar months need not undergo recurrent training. 14 CFR: 133.37 11.3.4 AIRWORTHINESS REQUIREMENTS 11.3.4.1 FLIGHT CHARACTERISTICS REQUIREMENTS (a) The applicant must demonstrate to the Authority, by performing the following operational flight checks, that the rotorcraft-load combination has satisfactory flight characteristics, unless these operational flight checks have been demonstrated previously and the rotorcraft-load combination flight characteristics were satisfactory. For the purposes of this demonstration, the external-load weight (including the external-load attaching means) is the maximum weight for which authorisation is requested. (b) Class A rotorcraft-load combinations: The operational flight check must consist of at least the following manoeuvres: (1) Take off and landing. (2) Demonstration of adequate directional control while hovering. (3) Acceleration from a hover. (4) Horizontal flight at airspeeds up to the maximum airspeed for which authorisation is requested. (c) Class B and D rotorcraft-load combinations: The operational flight check must consist of at least the following manoeuvres: (1) Pickup of the external load. (2) Demonstration of adequate directional control while hovering. (3) Acceleration from a hover. (4) Horizontal flight at airspeeds up to the maximum airspeed for which authorisation is requested. (5) Demonstrating appropriate lifting device operation. (6) Manoeuvring of the external load into release position and its release, under probable flight operation conditions, by means of each of the quick-release controls installed on the rotorcraft. (d) Class C rotorcraft-load combinations: For Class C rotorcraft-load combinations used in wire-stringing, cable-laying, or similar operations, the operational flight check must consist of the manoeuvres, as applicable, prescribed in paragraph (c) of this section. 14 CFR: 133.41 11.3.4.2 STRUCTURES AND DESIGN (a) External-load attaching means. Each external-load attaching means shall be approved by the Authority. (b) Quick release devices. Each quick release device means shall be approved by the Authority. (c) Weight and centre of gravity: (d) Weight. The total weight of the rotorcraft-load combination must not exceed the total weight approved for the rotorcraft during its type certification. (e) Centre of gravity. The location of the centre of gravity must, for all loading conditions, be within the range established for the rotorcraft during its type certification. For Class C rotorcraft-load combinations, the magnitude and direction of the loading force must be established at those values for which the effective location of the centre of gravity remains within its established range. 14 CFR: 133.43 11.3.4.3 OPERATING LIMITATIONS (a) In addition to the operating limitations set forth in the approved Rotorcraft Flight Manual, and to any other limitations the Authority may prescribe, the operator shall establish at least the following limitations and set them forth in the Rotorcraft-Load Combination Flight Manual for rotorcraft-load combination operations: (1) The rotorcraft-load combination may be operated only within the weight and centre of gravity limitations established in accordance with this subpart. (2) The rotorcraft-load combination may not be operated with an external load weight exceeding that used in showing compliance with this subpart. (3) The rotorcraft-load combination may not be operated at airspeeds greater than those established in accordance with this subpart. (4) No person may conduct an external-load operation under Part 11 with a rotorcraft type certified in the restricted category over a densely populated area, in a congested airway, or near a busy airport where passenger transport operations are conducted. (5) The rotorcraft-load combination of Class D may be conducted only in accordance with the following: (b) The rotorcraft to be used must have been type certified under transport Category A for the operating weight and provide hover capability with one engine inoperative at that operating weight and altitude. |
上一篇：民航規(guī)章 CIVIL AVIATION REGULATIONS 2
下一篇：沒(méi)有了
2002-2021 www.jdhsafaris.com 北京藍(lán)天飛行翻譯公司版權(quán)所有 北京藍(lán)天飛行翻譯公司版權(quán)聲明
