19. The Fifth Schedule to the principal Order is amended —(a) | by deleting the words “and H” under the heading “Scale of equipment required” in item 2(c) and (d) (page 87) of paragraph 4 and substituting in each case the words “, H and S(i)”; | (b) | by deleting sub-paragraph (e) of item 2 (page 88) in paragraph 4 and substituting the following sub-paragraph: “(e) | when flying over water — |
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| (i) | in the case of an aeroplane having such a weight and performance that with any one of its power units inoperative and the remaining power unit or units 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 Minister, it is capable of a gradient of climb of at least 1 in 200 at an altitude of 5,000 feet in the International Standard Atmosphere specified in or ascertainable by reference to the Certificate of Airworthiness in force in respect of that aeroplane, when — |
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| (aa) | more than 50, but not exceeding 400, nautical miles from the nearest aerodrome at which an emergency landing can be made |
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| . . . A, B, D, F(i) only and H. |
| (bb) | more than 400 nautical miles from the nearest aerodrome at which an emergency landing can be made |
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| . . . A, B, D, F(i) only, H and J. |
| (ii) | in the case of all other flying machines, when more than 100 nautical miles or 30 minutes flying time*, whichever is the lesser, from such aerodrome |
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| . . . A, B, D, F(i) only, H and J.”; |
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| (c) | by inserting, immediately after “5,700 kg.,” in the 6th line of item 6 (page 91) in paragraph 4, the word “and”; | (d) | by deleting the words “, and are certificated to carry more than 9 passengers” in the penultimate and last lines of item 6 (page 91) in paragraph 4; | (e) | by deleting items 7 and 8 (page 91) of paragraph 4 and substituting the following items:“7. | All helicopters for which an individual Certificate of Airworthiness was first issued (whether in Singapore or elsewhere) on or after 1st January 1989 and which have a maximum total weight authorised exceeding 2,700 kg. |
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| | 8. | All aeroplanes exceeding 5,700 kg. Maximum total weight authorised or authorised to carry more than 9 passengers |
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| (f) | by deleting paragraphs (i) and (ii) (page 92) under Scale B of paragraph 5 and substituting the following paragraphs:(i) | First aid equipment of good quality, sufficient in quantity, having regard to the number of persons on board the aircraft, including the following: |
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| (a) | a handbook on first aid; |
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| (b) | ground-air visual signal code for use by survivors; |
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| (c) | materials for treating injuries such as roller bandages, triangular bandages, absorbent gauze, adhesive plaster, white absorbent lint, cotton wool (or wound dressing in place of the lint and cotton wool), burn dressings, safety pins; |
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| (d) | haemostatic bandages or tourniquet; |
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| | | (g) | a decongestant nasal spray; |
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| | | | (k) | water-miscible antiseptic/skin cleanser; |
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| (l) | materials for treatment of extensive burns; |
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| (m) | oral drugs as follows: analgesic, antispasmodic, central nervous system stimulant, circulatory stimulant, coronary vasodilator, antidiarrhoeic and motion sickness medications; and |
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| (n) | an artificial plastic airway and splints. |
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| (ii) | In the case of flying machines with a maximum total weight authorised exceeding 5,700 kg. used for the public transport of passengers, in addition to paragraph (i), a medical kit for the use of medical doctors or other qualified persons in treating in-flight medical emergencies with the following supplies: |
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| (a) | sterile surgical gloves; |
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| | | | | (f) | haemostatic bandages or tourniquet; |
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| (g) | sterile equipment for suturing wounds; |
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| (h) | disposable syringes and needles; |
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| (i) | disposable scalpel handle and blade; |
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| (j) | coronary vasodilators; |
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| | | | | | | (q) | oral or injectable drugs as follows: analgesic, antihistamine, coronary stimulant, cortico-steroid, intravenous infusion fluid, sedative and tranquilliser, uterine stimulant and vasopresser agent; and |
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| (r) | injectable broncho dilator.”; |
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| (g) | by deleting paragraph (vi) (page 93) under Scale B in paragraph 5 and substituting the following paragraph:“(vi) | A forward or rearward facing (within 15º of the longitudinal axis of the aircraft) seat, fitted with a safety harness for the use of each cabin crew member specified in paragraph 18(8) of the Order, which shall be located near floor level and emergency exits.”; |
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| (h) | by deleting paragraphs (iv) and (v) (page 94) under Scale E in paragraph 5 and substituting the following paragraphs:“(iv) | Two sensitive pressure altimeters with counter drum-pointer or equivalent presentation but not including any three-pointer or drum-pointer altimeter. |
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| (v) | An emergency power supply, independent of the main electrical generating system, capable of operating and illuminating an attitude indicating instrument (which shall be clearly visible to the pilot-in-command) for a minimum period of 30 minutes after the total failure of the main electrical generating system, in respect of — |
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| (a) | aircraft, for which a Certificate of Airworthiness was first issued on or after 1st January 1975 (whether in Singapore or elsewhere), fitted with electrical attitude indicating instruments, of which the maximum total weight authorised exceeds 5,700 kg. issued with a Singapore Certificate of Airworthiness in the Transport Category; |
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| (b) | aircraft, fitted with electrical attitude indicating instruments, certified in the Transport Category for the carriage of more than 19 persons over the age of 3 years; and |
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| (c) | aircraft, fitted with electrical attitude indicating instruments, with a maximum total weight authorised exceeding 15,900 kg., |
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| | which shall be automatically operative after the total failure of the main electrical generating system and clear indication shall be given that each attitude indicator is being operated by emergency power.”; |
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| (i) | by deleting the words “one liferaft radio transmitter” in paragraph (ii) (page 97) of Scale J in paragraph 5 and substituting the words “one survival ELT”; | (j) | by deleting the 1st paragraph (page 100) under Scale K2 in paragraph 5 and substituting the following paragraphs:“(i) | A supply of oxygen and the associated equipment to meet the requirements set out in Parts I and II of this Scale. The duration for the purposes of this Scale shall be — |
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| (a) | that calculated in accordance with the operations manual prior to the commencement of the flight, being the period or periods which it is reasonably anticipated that the aircraft will be flown in the circumstances of the intended flight at a height where such requirements apply and in calculating the duration account shall be taken of — |
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| (A) | in the case of pressurised aircraft, the possibility of depressurisation when flying above flight level 100; |
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| (B) | the possibility of failure of one or more of the aircraft engines; |
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| (C) | restrictions due to required minimum safe altitude; |
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| | (E) | the performance of the aircraft; or |
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| (b) | the period or periods during which the aircraft is intended to be flown in the circumstances specified in Parts I and II, |
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| | whichever is the greater. |
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| (ii) | If an aircraft is not capable, at the time when a failure to maintain cabin pressurisation occurs, of descending from flight level 250 or above in accordance with the emergency descent procedure specified in the relevant flight manual and without flying below the minimum altitudes for safe flight specified in the operations manual relating to the aircraft, to flight level 130 within 4 minutes and of continuing at or below that flight level to its place of intended destination or any other place at which a safe landing can be made, the aircraft shall be equipped with automatically deployable oxygen equipment and the number of oxygen dispensing units shall exceed the number of passenger and cabin crew member seats by at least 10 per cent.”; |
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| (k) | by deleting the last paragraph (page 102) of Scale K2 in paragraph 5 and substituting the following paragraph:“A | The flying machine is capable, at the time when a failure to maintain cabin pressurisation occurs, of descending in accordance with the emergency descent procedure specified in the relevant flight manual and without flying below the minimum altitudes for safe flight specified in the operations manual relating to the aircraft, to flight level 130 within 4 minutes and of continuing at or below that flight level to its place of intended destination or any other place at which a safe landing can be made.”; |
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| (l) | by deleting Scale P (pages 103 to 106) in paragraph 5 and substituting the following Scale: | | A flight data recorder and a cockpit voice recorder which shall satisfy the requirements specified in the Singapore Airworthiness Requirements (SAR) in the following aspects: |
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| (a) | capability of recording, by reference to a timescale, and retaining data; |
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| (b) | parameters or information to be recorded; |
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| (c) | type, construction, location and installation on aircraft; |
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| (d) | duration of the recording; and |
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| (e) | inspection requirements.”; |
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| (m) | by deleting paragraph (i) (page 107) under Scale S in paragraph 5 and substituting the following paragraph:“(i) | At least two survival ELTs, on long-range over-water flights and at least one survival ELT, on flights over designated land areas.”; |
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| (n) | by deleting paragraph (i) (page 107) under Scale T in paragraph 5 and substituting the following paragraph: | (o) | by renumbering the existing paragraph under Scale U (page 107) in paragraph 5 as paragraph (i) of that Scale, and by inserting immediately thereafter the following paragraph:“(ii) | The ground proximity warning system referred to in sub‑paragraph (i) shall provide, as a minimum, warnings of the following circumstances: |
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| (a) | excessive descent rate; |
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| (b) | excessive terrain closure rate; |
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| (c) | excessive altitude loss after take-off or go-around; |
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| (d) | unsafe terrain clearance while not in landing configuration — |
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| (i) | gear not locked down; or |
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| (ii) | flaps not in a landing position; and |
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| (e) | excessive descent below the instrument glide path.”; |
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| (p) | by deleting paragraph (i) (page 108) under Scale W in paragraph 5 and substituting the following paragraph: | (q) | by deleting Scales Z and AA (pages 108 to 111) in paragraph 5 and substituting the following Scales: | | A flight data recorder and a cockpit voice recorder which shall satisfy the requirements specified in the Singapore Airworthiness Requirements (SAR) in the following aspects: |
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| (a) | capability of recording, by reference to a timescale, and retaining data; |
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| (b) | parameters or information to be recorded; |
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| (c) | type, construction, location and installation on aircraft; |
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| (d) | duration of the recording; and |
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| (e) | inspection requirements. |
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| | | A flight data recorder and a cockpit voice recorder which shall satisfy the requirements specified in the Singapore Airworthiness Requirements (SAR) in the following aspects: |
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| (a) | capability of recording, by reference to a timescale, and retaining data; |
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| (b) | parameters or information to be recorded; |
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| (c) | type, construction, location and installation on aircraft; |
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| (d) | duration of the recording; and |
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| (e) | inspection requirements.”; |
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| (r) | by deleting the words “cabin attendant” in the 6th line of paragraph (i)(a) (page 106) under Scale R in paragraph 5 and substituting the words “cabin crew member”; | (s) | by deleting the words “cabin attendants” in the following provisions in paragraph 5 and substituting in each case the words “cabin crew members”:(i) | Scale G — paragraph (iii)(b)(B)(ii) (page 95); |
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| (ii) | Scale R — paragraph (ii)(a) (page 106); and |
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| (iii) | Scale V — paragraph (iv)(b) (page 108); and |
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| (t) | by deleting the words “Cabin attendants” in the following provisions in paragraph 5 and substituting in each case the words “Cabin crew members”:(i) | Scale K2 – paragraph (ii)(b) (page 100) under the heading “Supply for” in Part I; |
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| (ii) | Scale K2 – paragraph (iii)(b) (page 101) under the heading “Supply for” in Part I; |
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| (iii) | Scale K2 – paragraph (ii)(b) (page 101) under the heading “Supply for” in Part II; |
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| (iv) | Scale K2 – paragraph (ii)(c) (page 101) under the heading “Supply for” in Part II; and |
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| (v) | Scale K2 – paragraph (iii)(b) (page 102) under the heading “Supply for” in Part II. |
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