the Authority The equipment referred to in Scale A (ii):
(b> First aid equipment and handbook, referred to in Scale A;
(c)
Time-pieces, referred to in Scale F:
(di Torches, referred to in Scales. G.H.K. and Z:
(e)
Whistles, referred to in Scale H;
(f)
Sea anchors, referred to in Scales H. J and K:
(y)
Rocket signals, referred to in Scale J:
Ihi Equipment for mooring, anchoring or maneuvring aircraft on the water referred to in Scale J:
(i)
Puddles, referred to in Scale K:
(j)
Food and water, referred to in Scales K. U. and V;
(k)
Stoves cooking utensils, snow shovels, ice sa^s. sleeping bags and Arctic suits, referred to in Scale V;
(m)
Megaphones, referred to in Scales Yl and Y2 and V ice saws, in Scale "V. k TABLE
Description of Aircraft' Circumstances of Flight Scale of Equipment required
(1)
Gliders (a) flying for purposes A (ii) other than public transport or aerial work; and when living by night.
(b)
Hying for the A. B (i) and (ii). D and F purposes of public (i) transport and aerial work; and
(i)
When Hying by night C and G
(ii)
When carrying out B (iii) an aerobatic maneuvers.
(2)
Aeroplanes (a) Hying for purposes A (i) and and B (i; other than public transport; and
(i)
when Hying by night C and D (ii; v.hen Hying under Instrument Flight rulcs- (a;i) outside controlled D airspace. (hh; wilhin controlled E v-ith duplicated airspace and F (iii; when carrying out B • :ii) aerobatic manoeuvres. lb) Hying lor the A.B.li) and (ii). D and F purpose of public (i> transport ; and
(i)
when Hying under E with E t:\) duplicated Instrument Flight Rules and F except flights Outside controlled airspace by Aeroplanes having a maximum total weight authorised not exceeding' 1150ks.
(ii)
when Hying by C and G E with E (iv) night; and in case duplicated and F aeroplanes of which the maximum total weight authorised exceeds 1150kg. i'iii) when Hying over H water bevond eliding distance from land.
(iv)
on al! Hights on H which in the case of any emergency occurring during take-off or during the landing at the intended destination or anv likclv alternate destination it is reasonably possible that the aeroplane would be forced to land onto water. tvi when flying over A.B. I.) and D and I' <i' water- < aaj in case of an aeroplane taaa,1 classified in its ccriit'icaie of airworthiness as being of perlon nance group A. C <-r X. or
(bhb)
having no iH. J <k K performance group classification in iis certificate of airworthiness and of such a weight and performance that with any 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. pcrl'onnancc schedule or flight manual relating to the aeroplane issued or rendered valid by the Authority it is capable of a gradient ofclimb of at least I in 200 at an altitude of 5000ft in the International Standard Atmosphere specified in or ascertainable by reference to the ; certificate of airworthiness in force in | respect of that aircraft I w hen either more than | 400 nautical miles or I more than 90 minutes | l i\ inc time: I ' i (ccc) tor the purpose ot • I thi< Table. Hying time I ; shall be calculated on I the assumption that the I aircraft is tlvinc in still air at the *pceu • I xpcjil'ied in the relevant ; j ccriiheaie ol i i airv.orihinc>s as the | speed for compliance with regulations governing Hights over water, from the nearest aerodrome at which an emergency landing can be made. Circumstance of flight Scale of Equipment required
(bh)
in the case of all H and K other aeroplanes, when more than 30 minutes flying time from such an aerodrome-
(iv)
on all flights which H.J&K involve manoeuvers on water.
(vii)
when Hying at a height of 10.000 ft or . more above man sea level.
(aa)
having a certificate LI or 1.2 of airworthiness first 1 issued (whether in Uganda or elsew here) before 1st January 1 i 1989.
(bb)
having a certificate \ L2 of airworthiness first i I issued (whether in i Uganda or elsewhere) i» on or after 1 st January i 1 1989 11
(viii > on Hight when (he weather report or forecasts available al lhe I aerodrome at the lime of | departure indicate that I lhe conditions favouring ice formation arc likely to be met.
(ix)
when carrying out acrobatic manoeuvres. tx) on all flights (in which the aircraft carries a Hight crew of more than one person I I !»\i i on all i'light> lor i (he purpo>e of lhe i public transport of I pu^cneeisi i i aa > before l>( January. q Y: [1990 i
; hoi on or after i Q M Y2 hi: and c.ii; January. 1990
(xiij on all Hights by a R1 I pressurised aircraft- I
Haai before 1st January. R2 I 1990. I i ■ (bbi on or after 1st •January I WO. i
■ ixin.' v.hen flying over suh'tjniially • uninhabited land area' • v. here, in the case of ' any emergency landing: to p:..d c.'t\!ili<ins arc like!-, (o be met.
txiv) when living over i\ substantially uninhabited land areas 1 where, in case of anv i emergency landing: ! polar conditions are ' likely to he met.
(xv)
when Hying at an iw altitude of more than 49.000ft.
(?) Turbine-jet when tlvinu lor lhe 0 aeroplanes having a purpose of public maximum total weight transport. authorised exceeding 5700kg or pressurised aircraft having a maximum total weight authorised exceeding 11400kg.
(4)
Turbine-engined aeroplanes having a maximum total weight authorised exceeding 5700kg. And pistonengined aeroplanes having a maximum total weight _ ethorised 1 exceeding 2"-'^)kg- i i ia) which arc perated When fl v inu on anv ;p by an air Iran-port flight undcnukimi u'.der a ccruhcaie of airworthiness r: lhe Transport calc>»ry < passenger) or he i Transport Car-.: >ry l 1 i C argo): or
(b)
in respect of which When Hying on any application has been Hight made and not withdrawn or refused for such a certificate and which fly under a certificate of airworthiness in the Special Category. except that this paragraph shall not apply to aeroplanes falling within paragraphs (5) or (6i of this Table.
(5)
Aeroplanes in respect of which there is in force a certificate of airworthiness in the Transport Category (Cargo) and aeroplanes in respcc' uf which application has been made, and not withdrawn or refused for such a certificate of airworthiness and which fly under 'A conditions' or in respect of which there is in force a certificate of airworthiness in the Special Category.
(a)
which conform to a When Hying on any type first issued with a Hight. certificate (whether in Uganda or elsew here1 on or after I st
April.1971 and which 1 1 have a maximum total weight authorised 1 exceeding 5700kg but 1 1 not exceeding 11400kg. 1
(b)
which conform to a when living on anv S tiO type first issued with a Hight. type certificate (whether in Uganda or elsewhere) on or after 1st April 1971 and which have a maximum total weight authorised exceedins 11400kg but not exceeding 27000kg;
(c)
which conform to a when living on anv S- iii> type first issued with a flight. i type certificate (whether in Uganda or i elsewhere) on or after 1 i 1st January 1 971 and 1 which have a maximum Ii total weight authorised 1 exceeding 230000kg;
(d)
which conform to a when Hying on any •Siv) type first issued with a (light. type certificate in Uganda on or after 1 January 19":; and which have a maximum total weight authorised exceeding *2. 'X)00kg. expect that tn.ts paragraph s.'.JI not apply to aer planes falling with:.'; paragraph (6j of this tame.
(6)
Aeroplanes in respect of which there is in force a certificate of airworthiness in the Transport Category (Passenger) or Transport Category (Cargo) and aeroplanes in respect of which application has been made and not withdrawn or refused for such a certificate of airworthiness and which fly under eA Conditions!' or in respect of which there is in force a certificate of airworthiness in the Special Category.
(a)
for which an when living on anv S(iv) individual certificate of Hight. airworthiness was first issued (whether in Uganda or elsewhere i on or after I June 1990 and which have a maximum total weight authorised not exceeding 5700kg arc powered by 2 or more turbine engines and are certified to carry more than 9 passenger; or
(b)
for which an when living on anv individual certificate ■'.( Riehl. airworthiness was first H'.ued (whether in Uganda or ebewhere on ;>r after 1 June I ) and which ha-- e a maximum total weigh; authorised exceeding 5700kg but not exceeding 27000kg: or 1
<c) lor which an S-.vi! individual certificate of airworthiness was first issued (whether in Uganda or elsewhere) on or after 1st June 1990 and which have a maximum total weight authorised exceeding 27000kg:
(7)
Aeroplanes in Siix > respect of which there is in force a certificate of airworthiness in the Aerial Work or Private Category and for which an individual certificate of airworthiness wa< first issued (whether in Uganda or clsew here) on or after 1st June. 1990 and which have a maximum total v-.eiuht authorised exceeding 27000kg.
(Si Aeroplanes: when living on anv T Hight. <a> which conform to a type first issued with a T type certificate tn When fly ing on any Uganda on or after 1st Hight. January. 1970 and which have a maximum total weight u. autr.'-.'ised T
exceeding 230000kg. .And tn respect of w Inch there i> in force such airworthiness in the Transport Category (Passenger) or the 'Transport Category tCargoi.
ibi which conform to a When IK me on anv t\pe 1'ii'sl issued w iih a t\pc ^eriilicaie in Uganda on or al ter 1st 1970 and which have a maximum total weight authorised exceeding 23O.(XX)kg and in respect of which there r in force such a certificate of airworthiness.
<c> having a maximum ! When flying on any total weight authorised ! niuiit exceeding 27.000ke which conform to a type hr>l issued with a lxpe certificate on or alter 1 .April. 197 I (or I >t January I S70 m the case of an aeroplane ha\ ing a maximum total weight authorised exceeding 230.000kg) in respect of which an I II application has been I made, and not I I w itlidraw n or re!used I I lor 'uch a ven i Create or anW'•r.hincss and I i which iix under die '.A I ] *.••ndition or in respect : a which there h in l ' i.. a certificate ol *. a:iPithiness m the
t9) Aeroplane which On all Hights for the have a maximum total purpose of public weight authorised transport. exceeding 15000kg or which in accordance with the certificate of airworthiness in force in respect of it may carry more than 30 passengers.
(10)
Aeroplanes: When flviim • bv* niuht -* for the purpose of the public transport of passengers. ta) which are a turbo jet and which have a maximum total weight authorised exceeding 22.700kg: or tb) having a maximum When flying by night weight authorised for the purpose of the exceeding 5.700kg. public transport of And which conform to passengers. a type for which a certificate of airworthiness was first applied for whether in Uganda or elsewhere) after 30th April 19"2 but not including any aeroplane which in the opinion of the Authority is identical in ail matters affecting the provision of etr.er-.'cncv i I evacuation facihiic-' to an aeroplane lUr which I a certificate of I airworthiness was first applied for bcf. re 'hut Jute: or
(e)
which in accordance When Hying by night Zoo an J Hii' w iih (he certificate in for the purpose of the levee in respect of it public transport of may carry more (han 19 passengers. passengers: or
(c)
which arc a turbo When Hying for the Z iii jet and which have a purpose of the public maximum total weight transport of passengers. authorised exceeding 22.700km * or
(f)
first issued with a When Hying on any Ztiiii type certificate whether flight on or after 1 st in Uganda or April. 1989. elsewhere! on or alter 1 1st January 1958 and i i which in accordance 1 ii i wiih the certificate of i airworthiness in force i 1 i in respeci therelore | may carry more than 19 i 1 1 passengers 1 fill Aeroplanes When 11} ing on am. AA Hight on or after 1 st i;u powered by one or April. I9S9. r*e m» turbine jets ami InM issued w :ih a ccriilkaic of airv.urihincss in i Uganda prior :o 1 April 19-9. [
(hi powered hy one or When 11\ing on an} i■ more turbine ids and Hight "fi or alter 1 st i I Hist issued w iih a .April '990. i 1 cert ilk-ale of 1t •i airworthiness in L'gaiiJa prior t I .April 19S9.
(12)
Aeroplanes on all flights for the Y 2tiv> (a) which conform to a purpose ol the public | type first issued with a transport of passengers. type certificate (whether in Uganda or elsewhere) on or after 1 st April 1978 and in respect of which there is in force a certificate airworthiness in the Transport Catenors (Passenger).
(bi which conform to a On all Hights for the Y2'iv: type issued with a type purpose of the public certificate (whether in transport of passengers. Uganda or elsewhere) on or after 1 si April 1968) and before 1 April 1978 and in respect of which there is in force a certificate •1 of airworthiness in the Transport Category. i Passengern
(ci which conform to a on all Hights for the Y2(iv; type first issued with a purpose of the public type certificate transport of passengers (w hether in Uganda or on or after 1 st April e 1 ss h e re be I o re 1 > 1993. April 1968 and in respect of which there is in force a certillcute of airworthiness in me Transport Category 1 Pj"Cngcr):
i a; fly ing for purpose' . . 11 : ■ a:sd Bi 11 Um Helicopt. r> an..:
(iy roplancs other than public *ptran «»rr. and
(i)
when Hying by day D under visual Hight rules with visual ground reference.
(ii)
when Hying by day under Instrument Flight rules or without visual ground reference.
(aa)
outside controlled E with (II) duplicated E airspace with Etii) and E(iv) duplicated & F with F(iv) for al! weights. (hb) within controlled airspace (iii) when Hying at night.
(aa)
with visual ground C.E.G(ii) and G (v) reference. (bb) without visual I• around reference j (aaa) outside controlled C.E with E (ii) : airspace. duplicated. G (iii) and i i Gi vj I i ' (bbb) within control C. E with both E (ii) and airspace) iE (;■■) duplicated F with ■ <iv> for all weights. • (G< -ii) and Div).
' ib) fl} ing for the . A.E 1 i i and i ii). F(i) and purpose of public : F i : • i for ad weights. I
; (i) when flying by day D ■ under \isual flight rules i with Huai ground reference.
(ii)
when Hying by E uith both E (iit and night with visual Elio duplicated F(ii). ground reference. F(ni> and F(v).
(aa)
in (he case of a C.E and G helicopter or gyroplane having a maximum total weight authorised not exceeding 2OOOkg. i bb) in the case of a C.E with E(ii) helicopter or gyroplane duplicated and either having a maximum Ei.»v > duplicated and total weight authorised either E-iv duplicated exceeding 2()()()ku. or radio altimeter. Ftii). Ft iii '. F' \ > and G. (iv) when Hying by night without visual ground reference.
(\) when Hying over C.E 'a.th both E (ii) and water. E (iv duplicated. F tii) 11 \)and G
(aa)
in the case of a E and H helicopter or gy roplane classified in its certificate of airworthiness as being of performance group A2 or B when beyond 1 autorotational gliding 1 distance from kind i if suitable for an emergency landing. ii • (bb) on all Hights on H i u huh in case of any I c11 urgency <ucurri ng during the take off or 1 1 during the landing at i the intended destination or anv likclv alternate destination it is reasonably possible that the helicopter or gyroplane would be forced to land onto water.
(cc)
in the case ot E.H.K and T helicopter or gyroplane classified in its certificate of airworthiness as being of performance group A2 when beyond 10 minutes Hying time from land
(dd)
for more than a total of 3 minutes in any Hight.
(ee)
in the case of a 1 helicopter or a gyroplane classified in its certificate of airworthiness as being of performance group A?, which is intended to Hy beyond 10 minutes Hying time form land which actually Hies beyond I'1 minutes flying lime from land, on a flight 'Uppori of or in connection with the oil 'fore e.'.phiitation er exploration ol mincra1' resources (including t i 7 hen ihu weal he: i report nr IbrccaMs : u-.uilahlc to the 1 j commander <>l lhe 1 aircraft indicate that the sea temperature will he less thanlOoC during the lliuhi or when any part of the Hight.is at night. (vii) when Hying at a being of 10.OOOft or more above man sea level: (aa) having a certificate LI or L2 of airworthiness first issued (whether in Uganda or elsewhere) before 1st January 1989.
(bb)
having a certificate L2 of airworthiness first issued (whether in Uganda or elsewhere) on or after I st January 1989.
(viii)
on Hights when the weather reports or forecasts available at the aerodrome at the lime of departure indicate that conditions fax curing ice formation are likely to be met
(ixi on all Hights on #X%' which the aircraft carries a Hitthl crew of more than one person. (x> on all Hights for the purpose of the public transport of passengers.
i *(aa, before Im January i
(hb)
on or after 1st Y2 ii). m' <-< (iii) January. 1990. (xi) when Hying mer (U) substantially uninhabited land areas where, in the event of an emergency landing, tropical condi tions are likely to be met. (xii) when Hying over (V) substantially uninha bited land or other areas where, in the event of an emer-gency landing. polar conditions arc likely to be met. i i4) Helicopters and Gy cop lanes: ia) having a maximum When * llvineW bv* niyht Z(i) and (ii> total weight authorised for the purpose of the exceeding 57(X) ky and public transport of which conform to a type for which a certificate of passengers. airworth i-ncss was first applied for whether in Uganda or elsewhere after 30 April 1972 hut not including any helicopter of gyroplane which in the opinion i-f the Authority r identical in al! matter' affecting the provision <>t emergency c'.-cuation laciiities ;• a helicopter or gyroplane lor uhich a certificate of airworthi ness was 1'irst applied h;r before that date: or (hi uhich in accordan.v When fly ing by night Z(i 'a uh. the certificate of for the purpose of the airworthiness in force public transport of in respect the rent may passengers. 1 carry more than 19 i passengers: or i ic) which have a When Hying on any certificate of flight before I st airworthiness issued in February. 1991 the Transport Category iPassenger or Cargo) and which have either a maximum total weight authorised exceeding 2730kg or which may carry more than 9 passengers; or (di which have a certificate of airworthiness issued in the Transport Category (Passenger or Cargo) and helicopters and gyroplanes in respect of which application had been made and not withdrawn or refused for such a certificate of airworthiness and which fly under the "A". conditions or which have a ccrtiiuaie of airworthiness in the special categ- ry and (i) which have a When flying on any i■ :n i; maximum t< tai weight Hight on or after I st authorised exceeding 2730kg but n- t February. 1991 exceeding ?! - >Okg or which in acc 'dance with the cci rtt'icate or airworthinc" m force in respect o: tt may carry more than 9 passengers. : both i tiii which h_ -c a | When living on any r •: i i i; • maximum t al weight [Hight on or alter 1st authorised e ■ .ceding I February. 1991 7000kg. i
-• 1 ne scale of equipment indicated in the Table set out in paragraph 4 shall be as follows-
Scale A (i) Spare fuses for all electrical circuits the fuses of which can be replaced in flight consisting of 10 percent of the number of each rating, whichever is the greater. (ii) maps, charts, codes and other documents and navigational equipment necessary, in addition to any other equipment required under these regulations, for the intended flight of the aircraft including any diversion which may reasonably be expected. (iii) First aid equipment of good quality, sufficient in quantity, having regard to the number of persons on board the craft, and including the following- Roller bandaged, triangular bandages, adhesive plaster, absorbent gauze, cotton wool (or wound dressing in place of absorbent gauze and cotton wool); bum dressing, safety pins; Homeostatic bandages or tournicuets. scissors. antiseptic, analgesic and stimulant drugs, splints, in the ca^e of aeroplanes the maximum total weight authorised of which exceeds 5700kg. A handbook on first aid: (iv) In the case of a flying machine used for the public transport of passengers in which, while the flying machine is at rest on the ground, the sill of any external door intended for the disembarkation of passenger, whether normally or in an emergency; (a) is more than 1.82 metres from the ground when the undercarriage of the machine is in the normal position for taxing; or (I)) would be more than 1.82 metres from the ground if the undercarriage or any par. of it should collapse. break or fail to function; apparatus * readily available for use at each such door consisting of a device or devices which will enable passengers to
reach (he eround sal'clv in an emergence while the flvine machine is on the ground, and can be readily fixed in position for use. Scale AA An altitude alerting system capable of alerting the pilot upon approaching a preselected altitude in either ascent or descent, by a sequence of visual and aural signals in sufficient time to establish level flight at that preselected altitude, and when deviating above or below that preselected altitude, by a visual and an aural signal: except that if the system becomes unserviceable, the aircraft may fly or continue to fly, until it first lands at a place at which it is reasonably practicable for the system to be repaired or replaced.
Scale B (i) (a) If the maximum total weight authorised of the aircraft is 2730 kg or less, for every pilots seat and for any scat situated alongside a pilot's seat, a safety belt with one diagonal shoulder strap or a safety harness:
except that the Authority may penr.it a safety bell without diasonal shoulder strap A to be fitted if it is satisfied that it is not reasonably practicable to fit a safety belt with one diagonal shoulder strap or a safety harness:
(bi If the maximum total weight authorised of the aircraft exceeds 2730kg a safety harness foremens pilot's seat and for any seat situated alongside a pilot's scat, in place of the safety belt with one diagonal shoulder strap referred to under sub-paragraph (ar. except that the Authority may permit a safety belt with one diagonal shoulder strap to be fitted it is satisfied that it is not reasonably practicable to fit fora safety harness.
(( ' I or every seat in use (not being a seat referred to in sub paragraph (a). (b) (e) and if/ a safety belt v. ith or without one diagonal shoulder strap or a safety harness.
(d)
In addition and for attachment to the equipment required in sub-paragraph (c) above, a child restraint device tor every child under the age of 2 years on board. (e) On all flights for the public..transport of passengers by aircraft, for each seat for use by cabin attendants who are required to be carried under these Regulations, a safety harness. (f) On all flights in aeroplanes the maximum total weight authorised of which does not exceed 5700kg which in accordance with the certificate of airworthiness in force for it is not capable of seating more than 9 passengers (otherwise than in seats referred to under sub-paragraphs (a) and (b), a safety belt with one diagonal shoulder strap or a safety'harness for each seat intended for use by a passenger. (g) The provisions of sub-paragraph (f) shall not apply to aeroplanes in respect of which a certificate of airworthiness was first issued (whether in Uganda or elsewhere) before 1 February, 1989; (ii) If the commander cannot, from his or her own seat, see all the passengers' seats in the aircraft, a means of indicating to the passengers that seat belts should be fastened. (iii) A safety harness for every seat in use expect that in the case of an aircraft carrying out aerobatic maneuvres consisting only of erect spinning, the Authority may permit a safety belt with one diagonal shoulder strap to be fitted if it is satisfied that such restraint is sufficient for the carrying out of erect spinning in that aircraft and that it is not reasonably practicable to fit a safety harness in that aircraft.
Scale C (i) Equipment for displaying the lights required b> (he Rules of the Air and Air Traffic Control:
(ii)
Electrical equipment supplied from the main source of supply in the aircraft, to provide sufficient illumination to enable the flight crew properly to carry out their duties during flight.
(iii)
Unless the aircraft is equipped with radio, devices for making the visual signal specified in the Rules of the Air and Air Traffic Control as indicating a request for permission to land.
Scale D (i) (a) In the case of a helicopter or gyroplane, a slip indicator,
(b)
In the case of any other flying machine either;
(aa)
a turn indicator and a slip indicator; or
(bb)
a gyroscopic bank and pitch indicator and a gyroscopic direction indicator, (ii) A sensitive pressure altimeter adjustable for any sea level barometric pressure which the weather report or forecasts available to the commander of the aircraft indicate is likely to be encountered during the intended flight.
Scale E (i) (a) In the case of a helicopter or gyroplane, a slip indicator;
(b)
In the case of any other flying machine, a turn indicator and a slip indicator; '
(ii)
A gyroscopic bank and pitch indicator;
(iii)
A gyroscopic direction indicator;
(iv)
A sensitive pressure altimeter adjustable for any sea level barometric pressure which the weather report or forecasts available to the commander of the aircraft indicate is likely to be encountered during the intended flight.
(c)
Any aircraft may, at the option of the operator be equipped with an additional gyroscopic bank and pitch indicator in lieu of the turn indicator referred to in (i) of this scale. Scale EE A radio altimeter with an audio voice warning operating below; and pre-set height and a visual warning capable of operating at a height selectable by the pilot.
Scale F (i) A timepiece indicating the time in hours, minutes and seconds; (ii) A means of indicating whether the power supply to the gyroscopic instrument is adequate;
(iii)
A rate of climb and descent indicator;
(iv)
If the maximum total weight authorised of the aircraft exceeds 5700kg a means of indicating outside air temperature;
(v)
If the maximum total weight authorised of the aircraft exceeds 5700kg two air speed indicators.
Scale G (i) In the case of an aircraft other than a helicopter or gyroplane landing lights consisting of 2 single filament lamps, or one dual filament lamp with separately energised filaments;
(ii)
An electrical lighting system to provide illumination in every passenger compartment;
(iii)
(a) One electric torch for each member of the crew of the a'rcraft; or
(b)
(aa) one electric torch for each member of the flight crew of the aircraft: and
(bb)
at least one electric torch affixed adjacent to each floor level exit intended for the disembarkation of passengers whether normally or in on emergency except that such torches shall- (aaa) be readily accessible for use by the crew of the aircraft at all times; and (bbb) number in total not less than die minimum number of cabin attendants required to be carried with a full passenger complement; (iv) In the case of an aircraft other than a helicopter or gyroplane of which the maximum total weight authorised exceeds 5700kg, means of observing the existence and build up of ice on the aircraft; (v) (a) In the case of a helicopter or gyroplane in respect of which there is in force a certificate of airworthiness designating the helicopter or gyroplane as being of performance group A, either: (aa) 2 landing lights both of which are adjustable so as to illuminate the ground in front of and below the helicopter or gyroplane and one of which is adjustable so as to illuminate the ground on either side of the helicopter or gyroplane; or
(bb)
one landing light or, if the maximum total weight authorised of the helicopter or gyroplane exceeds 5700kg. one dual filament landing light with separately energized filaments, or 2 single filament lights, each of which is adjustable so as to illuminate the ground in from of and below the helicopter of gyroplane, and 2 parachute flares;
(b)
In the case of a helicopter or gyroplane in respect ot which there is in force a certificate of airworthiness designating the helicopter or gyroplane as being of performance group B. either:
(cici)
one landing light and 2 parachute flares; or (l^b) if the maximum total weight authorised of the helicopter or gyroplane exceeds 5700kg, either one dual filament landing light with separately energized filaments or 2 single filament landing lights, and 2 parachute llatev Scale H (a) For each person on board, a lifejacket equipped with a whistle and water proof torch:
(b)
Lifejackets constructed and carried solely for use by children under three years of age need not be equipped with a whistle.
Scale I A survival suit for each member of the crew.
Scale J (i) Additional flotation equipment, capable of supporting one-fifth of the number of persons on board, and provided in a place of stowage accessible form outside the fl vine machine:
(ii)
Parachute distress rocket signals capable of making, from the surface of the water, the pyrotechnical signal of distress specified in the Rules of the Air Traffic Control.
(iii)
A sea anchor and other equipment necessary -o facilitate mooring. anchoring or maneuvering the flying machine on water, appropriate to its size, '.'.eight and handling characteristics.
Scale K (i) (a) In the case of a flying machine, other than a helicopter or gyroplane carrying 20 or more persons, aircrafts sufficient to accommodate all persons on board;
(b)
in the case of a hejicopter or gy roplane carrying 20 or more persons, a minimum of 2 liferafts sufficient together to accommodate all persons on board; Each life raft shall contain the following equipment- (a) means for maintaining buoyancy;
<c) life-lines, and means of attaching one-aircraft to another; (cl) paddles or other means of propulsion:
(e)
means of protecting the occupants from the elements; (f) a waterproof torch; tg) marine type pyrotechnica! distress signals;
<h) means of making sea water drinkable, unless the full quantity of fresh water is carried as specified in sub-paragraph (i);
(i)
for each 4 or proportion of 4 persons the aircraft is designed to cam': 100 grammes of glucose toffee tablets; '/-> litre of fresh water in durable containers.
(c)
In any case in which it is not reasonably practicable to carry the quantity of water specified as large, a quantity of fresh water as is reasonably practicable in the circumstances mav be substituted. In no case however shall the quantity of water carried be less ■.han is sufficient, when added to the amount of fresh water capable of being produced b> means of (he equipment specified in sub-paragraph (h) to provide 1/2 litre of water each 4 or proportion of 4 persons the aircraft is designed to carry. (j) first aid equipment;
Item (f) or'(j) inclusive shall be contained in a pack. (ii) The number of survival beacon radio apparatus carried when the aircraft is carrying the number of aircrafts specified in column I of (he following Table shall be not less than the number specified in or calculated in accordance with column 2.
Not more than 8 liferafts. 2 survival beacon radio apparatus. For every additional 4 or 1 additional >ur\hai beacon radion proportion of 4 liferafts. apparatus.
(iii)
In the case of a helicopter or gyroplane, an emergency beacon which is automatically ** * w deployed and activated in the event of a cash.
Scale LI Part I (i) In every flying machine which is provided with means for maintaining a pressure greater then 700 millibars throughout the flight in the flight crew compartment and in the compartments in which the passengers are earned:
(a)
a 'Upply of o.xygen sufficient, in case of failure to maintain such pressure, occurring in the circumstances specified in columns land 2 of the Table set out in Part II of this Scale for continuous use. during the periods specified in column 3 of that Table, by the persons for whom oxygen is to be p'ovided in accordance with column 4 of this Table; and
(b)
in addition, in every case v here the Hying machine flies above Hight level 350. a supply of oxygen in a portable container sufficient for the simultaneous first aid treatment of 2 passengers: together wit!', suitable and sufficient apparatus to enable .-'.'.ch persons to use the oxygen.
(ii)
In anv other flvine machine:
(a)
a supply of oxygen sufficient for continuous use by all the crew other than the flight crew, and if passengers are carried, 10% of the number of passengers, for any period exceeding 30 minutes durine which the Ovine machine flies above flight level 130 and the flight crew shall be supplied with oxygen sufficient for continuous use for any period during which the flvine machine flies above flich: level 100; and
(b)
a supply of oxygen sufficient for continuous use by all persons on board for the whole time during which the flying machine flies above flight level 130.
Together with suitable and sufficient apparatus to enable such persons to use the oxygen.
(iii)
The quantity of oxygen required for the purpose of complying with paragraphs (ij and (ii- of this Pan of this scale shall be computed in accordance vuth the information and instructions relating :? it specified in the operations manual relating to the aircraft under t Item (vi; and Part A of Schedule 11 of these Regulations.