1955-HKRS30-8-45_Part05 — Page 19

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inspected in accordance with the approved maintenance schedules and that adjustments and rectifications found necessary have been made and inspected to my satisfaction.

Signed

Dated at

Aircraft Maintenance Engineer: Licence No.

Time of Issue

This

day of

Period of validity

days from the time of issue or upon completion by the aircraft of

.......... flying hours whichever is the shorter period.

*NOTE: Thig certificate includes the attachment of the radio apparatus to the aircraft structure, and the condition of the earth system of the aircraft, including the bonding and screening to ensure suppression of high frequency clectrical interference. It does not include the radio apparatus.

(4) In the case of a glider-

CERTIFICATION OF MAINTENANCE.”

Glider Type

Nationality and Registration Marks

1 HEREBY certify that the above aircraft (including its prescribed instruments and equipment and also its towing gear) has been maintained and inspected in accordance with the approved maintenance schedules and that adjustments and rectifications found necessary have been made and inspected to my satisfaction.

Dated at

Signed

Aircraft Maintenance Engineer: Licence No.

Time of Issue

this

Period of validity

day of

days from the time of issue flying hours

or upon completion by the aircraft of whichever is the shorter period.

• NOTE: This certificate includes the attachment of the radio apparatus to the aircraft structure, and the condition of the earth systema of the aircraft, including the bonding and screening to ensure suppression of high frequency electrical interference. It does not include the radio apparatus.

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32. Every certificate of maintenance required by Article rô of the Order shall be prepared in ink or indelible pencil.

Requirements as to the Weight and Performance of Public Trans- port Aeroplanes having no Performance Group Classification in their Certificates of Airworthiness.

33. With reference to Article 17 of the Order a public transport acroplance having no performance group classification in the certificate of airworthiness relating to the aeroplane issued or rendered valid by the Director shall not fly or attempt to fly unless the following conditions are satisfied-

(1) The weight and performance of the aeroplane at the commencemeat of the take-off run are such that either-

(a) the wing loading of the acroplane does not exceul 20 lb.

per square foot; or

(b) the stafling speed of the seroplane in the landing con-

figuration does not exceed 60 knots; or

(c) the aeroplane, with any one of its engines inoperative and the remaining engine or engines operating within the maximum continuous power conditions specified in the certificate of airworthiness, performance schedule or flight manual relating to the aeroplane issued or rendered valid by the Director, shall be capable of a gradient of climb of at least in 200, at an altitude of 5,000 feet above mican sea level in air having a temperature of 5.1* centigrade and a pressure of 843 millibars.

(2) The weight of the neroplane at the commencement of the take-off run does not exceed any of the following weights-

(a) the weight, if any, specified in the performance schedule or flight manual relating to the aeroplane issued or rendered valid by the Director as being the maximum take-off weight appropriate either to the height above mean sea level of and the air temperature at the aero- drome at which the take-off is to be made, or to the height above mean sea level of such aerodrome;

(b) the weight at which the aeroplane, with all engines operating within the maximum take-off power conditions specified in the certificate of airworthiness, performance