Commission Regulation (EU) 2017/363Dangos y teitl llawn

ANNEX U.K.

Annexes II, III, IV and V to Regulation (EU) No 965/2012 are amended as follows:

(1)

in Annex II (Part-ARO), Appendix II is replaced by the following:

‘Appendix II

’ ;”

(2)

Annex III (Part-ORO) is amended as follows:

(a)

in point ORO.GEN.110, points (j) and (k) are replaced by the following:

‘(j)

The operator shall establish and maintain dangerous goods training programmes for personnel as required by the technical instructions. Such training programmes shall be commensurate with the responsibilities of personnel. Training programmes of operators performing CAT, whether they transport dangerous goods or not, and of operators conducting operations other than CAT referred to in points (b), (c) and (d) of point ORO.GEN.005 that transport dangerous goods shall be subject to review and approval by the competent authority.

(k)

Notwithstanding point (j), operators conducting commercial operations with the following aircraft shall ensure that the flight crew has received an appropriate dangerous goods training or briefing, to enable them to recognise undeclared dangerous goods brought on-board by passengers or as cargo:

(1)

a sailplane;

(2)

a balloon;

(3)

a single-engined propeller-driven aeroplane having a maximum certified take-off mass of 5 700 kg or less and a MOPSC of 5 or less operated in a flight taking off and landing at the same aerodrome or operating site, under VFR by day; or

(4)

an other-than complex motor-powered helicopter, single-engined, with a MOPSC of 5 or less operated in a flight taking off and landing at the same aerodrome or operating site, under VFR by day.’;

(b)

in point ORO.FC.A.250, point (a) is replaced by the following:

‘(a) The holder of a CPL(A) (aeroplane) shall only act as commander in commercial air transport on a single-pilot aeroplane if either of the following conditions is met:

(1)

when carrying passengers under VFR outside a radius of 50 NM (90 km) from an aerodrome of departure, he/she has a minimum of 500 hours of flight time on aeroplanes or holds a valid instrument rating;

(2)

when operating on a multi-engine type under IFR, he/she has a minimum of 700 hours of flight time on aeroplanes, including 400 hours as pilot-in-command. These hours shall include 100 hours under IFR and 40 hours in multi-engine operations. The 400 hours as pilot-in-command may be substituted by hours operating as co-pilot within an established multi-pilot crew system prescribed in the operations manual, on the basis of two hours of flight time as co-pilot for one hour of flight time as pilot-in command;

(3)

when operating on a single-engined aeroplane under IFR, he/she has a minimum of 700 hours of flight time on aeroplanes, including 400 hours as pilot-in-command. Those hours shall include 100 hours under IFR. The 400 hours as pilot-in-command may be substituted by hours operating as co-pilot within an established multi-pilot crew system prescribed in the operations manual, on the basis of two hours of flight time as co-pilot for one hour of flight time as pilot-in command.’;

(3)

Annex IV (Part-CAT) is amended as follows:

(a)

point CAT.OP.MPA.136 is replaced by the following:

‘CAT.OP.MPA.136 Routes and areas of operation — single-engined aeroplanes

Unless approved by the competent authority in accordance with Annex V (Part-SPA), Subpart L — SINGLE-ENGINED TURBINE AEROPLANE OPERATIONS AT NIGHT OR IN IMC (SET-IMC), the operator shall ensure that operations of single-engined aeroplanes are only conducted along routes, or within areas, where surfaces are available that permit a safe forced landing to be executed.’;

(b)

in point CAT.OP.MPA.180, point (a) is replaced by the following:

‘(a) Where it is not possible to use the departure aerodrome as a take-off alternate aerodrome due to meteorological or performance reasons, the operator shall select another adequate take-off alternate aerodrome that is no further from the departure aerodrome than:

(1)

for two-engined aeroplanes:

(i)

one hour flying time at an OEI cruising speed according to the AFM in still air standard conditions based on the actual take-off mass; or

(ii)

the ETOPS diversion time approved in accordance with Annex V (Part-SPA), Subpart F, subject to any MEL restriction, up to a maximum of two hours, at the OEI cruising speed according to the AFM in still air standard conditions based on the actual take-off mass;

(2)

for three and four-engined aeroplanes, two hours flying time at the OEI cruising speed according to the AFM in still air standard conditions based on the actual take-off mass;

(3)

for operations approved in accordance with Annex V (Part-SPA), Subpart L — SINGLE-ENGINED TURBINE AEROPLANE OPERATIONS AT NIGHT OR IN IMC (SET-IMC), 30 minutes flying time at normal cruising speed in still air conditions, based on the actual take-off mass.

In the case of multi-engined aeroplanes, if the AFM does not contain an OEI cruising speed, the speed to be used for calculation shall be that which is achieved with the remaining engine(s) set at maximum continuous power.’;

(c)

in point CAT.POL.A.300, point (a) is replaced by the following:

‘(a) Unless approved by the competent authority in accordance with Annex V (Part-SPA), Subpart L — SINGLE-ENGINED TURBINE AEROPLANE OPERATIONS AT NIGHT OR IN IMC (SET-IMC), the operator shall not operate a single-engined aeroplane:

(1)

at night; or

(2)

in IMC, except under special VFR.’;

(d)

point CAT.POL.A.320 is replaced by the following:

‘CAT.POL.A.320 En-route — single-engined aeroplanes

(a)

In the meteorological conditions expected for the flight, and in the event of engine failure, the aeroplane shall be capable of reaching a place at which a safe forced landing can be made, unless the operator is approved by the competent authority in accordance with Annex V (Part-SPA), Subpart L — SINGLE-ENGINED TURBINE AEROPLANE OPERATIONS AT NIGHT OR IN IMC (SET-IMC) and makes use of a risk period.

(b)

For the purposes of point (a), it shall be assumed that, at the point of engine failure:

(1)

the aeroplane is not flying at an altitude exceeding that at which the rate of climb equals 300 ft per minute, with the engine operating within the maximum continuous power conditions specified; and

(2)

the en-route gradient is the gross gradient of descent increased by a gradient of 0,5 %.’;

(4)

in Annex V (Part-SPA), the following Subpart L is added:

‘SUBPART L SINGLE-ENGINED TURBINE AEROPLANE OPERATIONS AT NIGHT OR IN INSTRUMENT METEOROLOGICAL CONDITIONS (SET-IMC)

SPA.SET-IMC.100 SET-IMC operations

In commercial air transport (CAT) operations, single-engined turbine aeroplanes shall only be operated at night or in IMC if the operator has been granted a SET-IMC approval by the competent authority.

SPA.SET-IMC.105 SET-IMC operations approval

To obtain a SET-IMC approval by the competent authority, the operator shall provide evidence that all the following conditions have been complied with:

(a)

an acceptable level of turbine engine reliability is achieved in service by the world fleet for the particular airframe-engine combination;

(b)

specific maintenance instructions and procedures to ensure the intended levels of continued airworthiness and reliability of the aeroplane and its propulsion system have been established and included in the operator's aircraft maintenance programme in accordance with Annex I to Regulation (EU) No 1321/2014 (Part-M), including all the following:

(1)

an engine trend monitoring programme, except for aeroplanes first issued with an individual certificate of airworthiness after 31 December 2004 that shall have an automatic trend monitoring system;

(2)

a propulsion and associated systems' reliability programme;

(c)

flight crew composition and a training/checking programme for the flight crew members involved in these operations have been established;

(d)

operating procedures have been established specifying all the following:

(1)

the equipment to be carried, including its operating limitations and appropriate entries in the MEL;

(2)

the flight planning;

(3)

the normal procedures;

(4)

the contingency procedures, including procedures following a propulsion system failure, as well as forced landing procedures in all weather conditions;

(5)

the monitoring and incident reporting.

(e)

a safety risk assessment has been performed, including the determination of an acceptable risk period if an operator intends to make use of it.

SPA.SET-IMC.110 Equipment requirements for SET-IMC operations

Aeroplanes used for SET-IMC operations shall be equipped with all the following equipment:

(a)

two separate electrical generating systems, each one capable of supplying adequate power to all essential flight instruments, navigation systems and aeroplane systems required for continued flight to the destination or alternate aerodrome;

(b)

two attitude indicators, powered from independent sources;

(c)

for passenger operations, a shoulder harness or a safety belt with a diagonal shoulder strap for each passenger seat;

(d)

airborne weather-detecting equipment;

(e)

in a pressurised aeroplane, sufficient supplemental oxygen for all occupants to allow descent, following engine failure at the maximum certificated cruising altitude, at the best range gliding speed and in the best gliding configuration, assuming the maximum cabin leak rate, until sustained cabin altitudes below 13 000 ft are reached;

(f)

an area navigation system capable of being programmed with the positions of landing sites and providing lateral guidance to the flight crew to reach those sites;

(g)

a radio altimeter;

(h)

a landing light, capable of illuminating the touchdown point on the power-off glide path from 200 ft away;

(i)

an emergency electrical supply system of sufficient capacity and endurance capable of providing power, following the failure of all generated power, to additional loads necessary for all of the following:

(1)

the essential flight and area navigation instruments during descent from maximum operating altitude after engine failure;

(2)

the means to provide for one attempt to restart the engine;

(3)

if appropriate, the extension of landing gear and flaps;

(4)

the use of the radio altimeter throughout the landing approach;

(5)

the landing light;

(6)

one pitot heater;

(7)

if installed, the electrical means to give sufficient protection against impairment of the pilot's vision for landing;

(j)

an ignition system that activates automatically, or is capable of being operated manually, for take-off, landing, and during flight, in visible moisture;

(k)

a means of continuously monitoring the power train lubrication system to detect the presence of debris associated with the imminent failure of a drivetrain component, including a flight crew compartment caution indication;

(l)

an emergency engine power control device that permits continuing operation of the engine at a sufficient power range to safely complete the flight in the event of any reasonably probable failure of the fuel control unit.’.