時(shí)間：2015-01-22 15:18來(lái)源：藍(lán)天飛行翻譯公司 作者：民航翻譯 點(diǎn)擊：次
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To view this page ensure that Adobe Flash Player version 9.0.124 or greater is installed. *** This space is normally used to indicate the certification basis, i.e., certification code, with which the particular aircraft complies and/or its permitted operational category, e.g., commercial air transportation, aerial work, or private. **** This space shall be used either for periodic endorsement (giving date of expiry) or for a statement that the aircraft is being maintained under a system of continuous inspection. Annex 8: Part II, Chapter 3, Figure 1. IS: 5.3.1.6 ISSUANCE OF A SPECIAL CERTIFICATE OF AIRWORTHINESS (a) The Special Certificate of Airworthiness issued by the [Authority] shall be as follows. [STATE OF REGISTRY] [ISSUING AUTHORITY] SPECIAL AIRWORTHINESS CERTIFICATE A Category/Designation Purpose B Manufacturer Name Address C Flight From To D Registration No. Serial No. Builder Model E Date of Issuance Expiry Operating limitations date [dd/mm/yyyy] are part of this certificate Signature of CAA Representative Designation or office number Any alteration, reproduction, or misuse of this certificate may be punishable as specified in MCAR Part 1. This certificate must be displayed in the aircraft in accordance with MCAR 8 CAA Form No. [ ] See Reverse Side Front of form A This special airworthiness certificate is issued under the authority of the Model Law and MCAR Part 5. B This special airworthiness certificate authorised the manufacturer named on the reverse side to conduct production flight tests, and only production flight tests, of aircraft registered in his name. No person may conduct production flight tests (1) carrying persons or property for remuneration or hire and/or (2) carrying persons not essential for the purpose of the flight. C This special airworthiness certificate authorised the flight specified for the flight listed on the reverse side for the sole purpose shown in Block A. D This special airworthiness certifies that, as of the date of issuance, the aircraft to which issued has been inspected and found to meet the requirements of the applicable MCAR. The aircraft does not meet the requirements of the applicable and comprehensive detailed airworthiness code as provided by Annex 8 of the Convention on International Civil Aviation. No person may operate the aircraft described on the reverse side (1) except in accordance with the applicable MCAR and in accordance with conditions and limitations which may be prescribed by the Authority as part of this certificate, or (2) over any foreign country without the permission of that country E Unless sooner surrendered, suspended or revoked, this special airworthiness certificate is effective for the duration and under the conditions prescribed in the MCARs.. Back of form IS: 5.6.1.7 PERFORMANCE RULES: INSPECTIONS (a) Each person performing an annual or 100-hour inspection shall, before that inspection, thoroughly clean the aircraft and aircraft engine and remove or open all necessary inspection plates, access doors, fairings, and cowlings. (b) Each person performing an annual or 100-hour inspection shall inspect, where applicable, the following components— (1) Fuselage and hull group— (i) Fabric and skin - for deterioration, distortion, other evidence of failure, and defective or insecure attachment of fittings. (ii) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. (iii) The cabin and cockpit group. (iv) Generally - for uncleanness and loose equipment that might foul the controls. (v) Seats and safety belts - for poor condition and apparent defects. (vi) Windows and windshields - for deterioration and breakage. (vii) Instruments - for poor condition, mounting, marking, and (where practicable) for improper operation. (viii) Flight and engine controls - for improper installation and improper operation. (ix) Batteries - for improper installation and improper charge. (x) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. (2) Engine and nacelle group— (i) Engine section - for visual evidence of excessive oil, fuel, or hydraulic leaks, and sources of such leaks. (ii) Studs and nuts - for improper torquing and obvious defects. (iii) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. (iv) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. (v) Flexible vibration dampeners - for poor condition and deterioration. (vi) Engine controls - for defects, improper travel, and improper safetying. (vii) Lines, hoses, and clamps - for leaks, improper condition, and looseness. (viii) Exhaust stacks - for cracks, defects, and improper attachment. (ix) Accessories - for apparent defects in security of mounting. (x) All systems - for improper installation, poor general condition, defects, and insecure attachment. (xi) Cowling - for cracks and defects. (3) Landing gear group— (i) All units - for poor condition and insecurity of attachment. (ii) Shock absorbing devices - for improper oleo fluid level. (iii) Linkage, trusses, and members - for undue or excessive wear, fatigue, and distortion. (iv) Retracting and locking mechanism - for improper operation. (v) Hydraulic lines - for leakage. (vi) Electrical system - for chafing and improper operation of switches. (vii) Wheels - for cracks, defects, and condition of bearings. (viii) Tires - for wear and cuts. (ix) Brakes - for improper adjustment. (x) Floats and skis - for insecure attachment and obvious or apparent defects. (4) Wing and centre section assembly for— (i) Poor general condition, (ii) Fabric or skin deterioration, (iii) Distortion, (iv) Evidence of failure, and (v) Insecurity of attachment. (5) Complete empennage assembly for— (i) Poor general condition, (ii) Fabric or skin deterioration, (iii) Distortion, (iv) Evidence of failure, (v) Insecure attachment, (vi) Improper component installation, and (vii) Improper component operation. (6) Propeller group— (i) Propeller assembly - for cracks, nicks, binds, and oil leakage, (ii) Bolts - for improper torquing and lack of safety, (iii) Anti-icing devices - for improper operations and obvious defects, and (iv) Control mechanisms - for improper operation, insecure mounting, and restricted travel. (7) Avionics/instrument group— (i) Avionics/instruments equipment - for improper installation and insecure mounting. (ii) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. (iii) Bonding and shielding - for improper installation and poor condition. (iv) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. (8) Electronic/electrical group— (i) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. (ii) Bonding and shielding - for improper installation and poor condition. (iii) Each installed miscellaneous item that is not otherwise covered by this listing and/or has instructions for continued airworthiness - for improper installation and improper operation. 14 CFR: Part 43 Appendix D IS: 5.7.1.1 CONTENT, FORM AND DISPOSITION OF RECORDS FOR MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING AND MODIFICATION OF AIRCRAFT AND LIFE LIMITED PARTS IS: 5.7.1.1(B) RECORDING OF MAJOR REPAIRS AND MODIFICATIONS (a) Each person performing a major repair or major modification shall— (1) Execute the appropriate form prescribed by the Authority at least in duplicate; (2) Give a signed copy of that form to the aircraft owner/operator; and (3) Forward a copy of that form to the Authority, in accordance with Authority instructions, within 48 hours after the aeronautical product is approved for return to service. Note: Some CAA’s have an electronic system for recording major repairs and modifications. This IS is written presuming the [State] will use a hard copy form in duplicate. If an electronic system is used, the items here are recommended for inclusion in the system. (b) In place of the requirements of paragraph (a), major repairs made in accordance with a manual or specifications acceptable to the Authority, an AMO may— (1) Use the customer's work order upon which the repair is recorded; (2) Give the aircraft owner a signed copy of the work order and retain a duplicate copy for at least one year from the date of approval for return to service of the aeronautical product; (3) Give the aircraft owner a maintenance release signed by an authorised representative of the AMO and incorporating the following information— (i) Identity of the aeronautical product; (ii) If an aircraft, the make, model, serial number, nationality and registration marks, and location of the repaired area; (iii) If an aeronautical product, give the manufacturer's name, name of the part, model, and serial numbers (if any); and (4) Include the following or a similarly worded statement— The aeronautical product identified above was repaired, overhauled and inspected in accordance with currently effective, applicable instructions of the State of Design and regulatory requirements of the Authority, and is approved for return to service. Pertinent details of the repair are on file at this maintenance organisation. |
