natgillin/translations-raw huggingface dataset:
Operations without an assured safe forced landing capability
Operacije brez zagotovljenih zmogljivosti za varen pristanek v sili
Operations without an assured safe forced landing capability during the take-off and landing phases shall only be conducted if the operator has been granted an approval by the competent authority.
Operacije brez zagotovljenih zmogljivosti za varen pristanek v sili med fazo vzeta in pristajanja se izvajajo samo, če je pristojni organ izdal odobritev operatorju.
To obtain and maintain such approval the operator shall:
Operator za pridobitev in ohranitev take odobritve:
conduct a risk assessment, specifying:
izvede oceno tveganja ter v njej navede:
the type of helicopter; and
tip helikopterja in
the type of operations;
vrsto operacij;
implement the following set of conditions:
uresniči naslednji sklop pogojev:
attain and maintain the helicopter/engine modification standard defined by the manufacturer;
pridobi in vzdržuje standard za spremembe helikopterja/motorja, ki ga določi proizvajalec;
conduct the preventive maintenance actions recommended by the helicopter or engine manufacturer;
izvaja preventivne vzdrževalne ukrepe, ki jih priporoča proizvajalec helikopterja ali motorja;
include take-off and landing procedures in the operations manual, where they do not already exist in the AFM;
vključi postopke vzleta in pristanka v operativni priročnik, če še niso vključeni v letalski priročnik helikopterja;
specify training for flight crew; and
določi usposabljanje za letalsko posadko in
provide a system for reporting to the manufacturer loss of power, engine shutdown or engine failure events;
zagotovi sistem za obveščanje proizvajalca o izgubi moči, zaustavitvah motorja in okvarah motorja
implement a usage monitoring system (UMS).
izvaja sistem spremljanja uporabe (UMS).
The take-off mass shall not exceed the maximum mass specified for a rate of climb of 150 ft/min at 300 m (1000 ft) above the level of the aerodrome or operating site with the critical engine inoperative and the remaining engine(s) operating at an appropriate power rating.
Vzletna masa ne presega največje mase, navedene za hitrost vzpenjanja 150 ft/min na višini 300 m (1000 ft) nad nivojem letališča ali območja delovanja, z nedelujočim ključnim motorjem in drugimi motorji, ki delujejo z ustrezno imensko močjo.
For operations other than those specified in CAT.POL.H.305, the take-off shall be conducted such that a safe forced landing can be executed until the point where safe continuation of the flight is possible.
Pri drugih operacijah, ki niso določene v CAT.POL.H.305, se izvede takšen vzlet, da je varen pristanek v sili mogoč do točke, na kateri se lahko let varno nadaljuje.
For operations in accordance with CAT.POL.H.305, in addition to the requirements of (a):
Pri operacijah v skladu s CAT.POL.H.305 poleg zahtev iz odstavka (a):
the take-off mass shall not exceed the maximum mass specified in the AFM for an all engines operative out of ground effect (AEO OGE) hover in still air with all engines operating at an appropriate power rating; or
vzletna masa ne presega največje vzletne mase, določene v letalskem priročniku helikopterja za lebdenje z vsemi delujočimi motorji brez učinka tal (AEO OGE) v brezvetrju in vsemi motorji, ki delujejo z ustrezno imensko močjo, ali
for operations from a helideck:
se pri operacijah s heliportov na vodnih ploščadih s:
with a helicopter that has an MOPSC of more than 19; or
s helikopterjem z največjim operativnim številom potniških sedežev (MOPSC) nad 19 ali
any helicopter operated from a helideck located in a hostile environment,
katerim koli helikopterjem, ki izvaja operacije s heliporta na vodni ploščadi v neprijaznem okolju,
the take-off mass shall take into account: the procedure; deck-edge miss and drop down appropriate to the height of the helideck with the critical engine(s) inoperative and the remaining engines operating at an appropriate power rating.
pri vzletni masi upoštevajo: postopek, zgrešitev roba ploščadi in spust, ki ustrezajo višini ploščadi – z enim ali več nedelujočimi motorji in drugimi motorji, ki delujejo z ustrezno imensko močjo.
When showing compliance with (a) to (c), account shall be taken of the appropriate parameters of CAT.POL.H.105(c) at the point of departure.
Pri dokazovanju skladnosti z odstavki (a) do (c) se upoštevajo ustrezni parametri iz CAT.POL.H.105(c) na odhodni točki.
That part of the take-off before the requirement of CAT.POL.H.315 is met shall be conducted in sight of the surface.
Del vzleta, ki poteka pred izpolnitvijo zahteve iz CAT.POL.H.315, se izvede v vidnem dosegu površine.
From the defined point after take-off (DPATO) or, as an alternative, no later than 200 ft above the take-off surface, with the critical engine inoperative, the requirements of CAT.POL.H.210(a)(1), (a)(2) and (b) shall be complied with.
Po določeni točki po vzletu (DPATO) ali – kot druga možnost – najpozneje 200 ft nad vzletno površino z nedelujočim ključnim motorjem so izpolnjene zahteve iz CAT.POL.H.210(a)(1), (a)(2) in (b).
The requirement of CAT.POL.H.215 shall be complied with.
Izpolnjena je zahteva iz CAT.POL.H.215.
The landing mass at the estimated time of landing shall not exceed the maximum mass specified for a rate of climb of 150 ft/min at 300 m (1000 ft) above the level of the aerodrome or operating site with the critical engine inoperative and the remaining engine(s) operating at an appropriate power rating.
Pristajalna masa ob predvidenem času pristanka ne presega največje mase, določene za hitrost vzpenjanja 150 ft/min na višini 300 m (1000 ft) nad nivojem letališča ali območja delovanja z nedelujočim ključnim motorjem in drugimi motorji, ki delujejo z ustrezno imensko močjo.
If the critical engine fails at any point in the approach path:
Če ključni motor na kateri koli točki priletne poti odpove:
a balked landing can be carried out meeting the requirement of CAT.POL.H.315; or
se lahko izvede zaustavljeni pristanek v skladu z zahtevo iz CAT.POL.H.315 ali
for operations other than those specified in CAT.POL.H.305, the helicopter can perform a safe forced landing.
pri operacijah, ki niso določene v CAT.POL.H.305, lahko helikopter izvede varen pristanek v sili.
the landing mass shall not exceed the maximum mass specified in the AFM for an AEO OGE hover in still air with all engines operating at an appropriate power rating; or
pristajalna masa ne presega največje mase, določene v letalskem priročniku helikopterja za lebdenje z vsemi delujočimi motorji brez učinka tal (AEO OGE) v brezvetrju in z vsemi motorji, ki delujejo z ustrezno imensko močjo, ali
for operations to a helideck:
se pri operacijah do heliportov na vodnih ploščadih:
any helicopter operated to a helideck located in a hostile environment,
katerim koli helikopterjem, ki se uporablja do heliporta na vodni ploščadi v neprijaznem okolju,
the landing mass shall take into account the procedure and drop down appropriate to the height of the helideck with the critical engine inoperative and the remaining engine(s) operating at an appropriate power rating.
pri pristajalni masi upoštevata postopek in spust, ki ustrezata višini ploščadi, z enim nedelujočim motorjem in drugim motorjem ali motorji, ki delujejo z ustrezno imensko močjo.
When showing compliance with (a) to (c), account shall be taken of the appropriate parameters of CAT.POL.H.105(c) at the destination aerodrome or any alternate, if required.
Pri dokazovanju skladnosti z odstavki (a) do (c) se upoštevajo ustrezni parametri iz CAT.POL.H.105(c) na namembnem letališču ali katerih koli drugih nadomestnih letališčih, če je to potrebno.
That part of the landing after which the requirement of (b)(1) cannot be met shall be conducted in sight of the surface.
Del pristanka, po katerem zahteve iz pododstavka (b)(1) ni mogoče izpolniti, se izvede v vidnem dosegu površine.
Performance class 3
Razred zmogljivosti 3
Helicopters operated in performance class 3 shall be certified in category A or equivalent as determined by the Agency, or category B.
Helikopterji, ki se uporabljajo za operacije razreda zmogljivosti 3, so certificirani v kategoriji A ali enakovredni kategoriji, kakršno določi agencija, ali v kategoriji B.
Operations shall only be conducted in a non-hostile environment, except:
Operacije se izvajajo samo v neneprijaznem okolju, razen:
when operating in accordance with CAT.POL.H.420; or
operacij v skladu s CAT.POL.H.420 ali
for the take-off and landing phase, when operating in accordance with (c).
operacij v skladu z odstavkom (c) v zvezi s fazami vzleta in pristanka.
Provided the operator is approved in accordance with CAT.POL.H.305, operations may be conducted to/from an aerodrome or operating site located outside a congested hostile environment without an assured safe forced landing capability:
Če je operator odobren v skladu s CAT.POL.H.305, se lahko operacije izvajajo na poti do tistih letališč ali območij delovanja ali s takih letališč ali območij, ki so zunaj neprijaznega gosto naseljenega območja in nimajo zagotovljene zmogljivosti za varen pristanek v sili:
during take-off, before reaching Vy (speed for best rate of climb) or 200 ft above the take-off surface; or
med vzletom, preden helikopter doseže Vy (hitrost za najboljšo hitrost vzpenjanja) ali 200 ft nad vzletno površino ali
during landing, below 200 ft above the landing surface.
med pristankom manj kot 200 ft nad pristajalno površino.
Operations shall not be conducted:
Operacije se ne izvajajo:
out of sight of the surface;
zunaj vidnega dosega tal;
at night;
ponoči;
when the ceiling is less than 600 ft; or
kadar je baza oblakov nižja od 600 ft ali
when the visibility is less than 800 m.
pri vidljivosti, slabši od 800 m.
The take-off mass shall be the lower of:
Vzletna masa je manjša od spodnjih mas:
the MCTOM; or
največja potrjena vzletna masa (MCTOM) ali
the maximum take-off mass specified for a hover in ground effect with all engines operating at take-off power, or if conditions are such that a hover in ground effect is not likely to be established, the take-off mass specified for a hover out of ground effect with all engines operating at take-off power.
največja vzletna masa, navedena za lebdenje v talnem učinku z vsemi motorji, delujočimi pri vzletni moči, ali če so razmere take, da lebdenja pri talnem učinku verjetno ne bo mogoče vzpostaviti, vzletna masa, navedena za lebdenje brez talnega učinka z vsemi motorji, delujočimi z vzletno močjo.
Except as provided in CAT.POL.H.400(b), in the event of an engine failure the helicopter shall be able to perform a safe forced landing.
V primeru odpovedi motorja helikopter lahko izvede varen pristanek v sili, razen kot je določeno v CAT.POL.H.400(b).
En-route
Na zračni poti
The helicopter shall be able, with all engines operating within the maximum continuous power conditions, to continue along its intended route or to a planned diversion without flying at any point below the appropriate minimum flight altitude.
Helikopter lahko z vsemi motorji, delujočimi v razmerah največje stalne moči, let nadaljuje po načrtovani zračni poti ali do načrtovane preusmeritve, ne da bi pri tem kadar koli letel pod ustrezno najmanjšo višino letenja.
Except as provided in CAT.POL.H.420, in the event of an engine failure the helicopter shall be able to perform a safe forced landing.
Helikopter lahko v primeru odpovedi motorja izvede varen pristanek v sili, razen kot je določeno v CAT.POL.H.420.
The landing mass of the helicopter at the estimated time of landing shall be the lower of:
Pristajalna masa helikopterja ob predvidenem času pristanka je manjša od spodnjih mas:
the maximum certified landing mass; or
največja certificirana pristajalna masa ali
the maximum landing mass specified for a hover in ground effect, with all engines operating at take-off power, or if conditions are such that a hover in ground effect is not likely to be established, the landing mass for a hover out of ground effect with all engines operating at take-off power.
največja pristajalna masa, navedena za lebdenje v talnem učinku, z vsemi motorji, delujočimi pri vzletni moči, ali če so razmere take, da lebdenja v talnem učinku verjetno ne bo mogoče vzpostaviti, pristajalna masa za lebdenje brez talnega učinka z vsemi motorji, delujočimi z vzletno močjo.
Except as provided in CAT.POL.H.400(b), in the event of an engine failure, the helicopter shall be able to perform a safe forced landing.
Helikopter lahko v primeru odpovedi motorja izvede varen pristanek v sili, razen kot je določeno v CAT.POL.H.400(b).
Helicopter operations over a hostile environment located outside a congested area
Helikopterske operacije nad neprijaznim okoljem zunaj gosto naseljenega območja
Operations over a non-congested hostile environment without a safe forced landing capability with turbine-powered helicopters with an MOPSC of six or less shall only be conducted if the operator has been granted an approval by the competent authority, following a safety risk assessment performed by the operator.
Operacije nad neprijaznim okoljem zunaj gosto naseljenega območja brez zmogljivosti za varen pristanek v sili s turbinskimi helikopterji z največjim operativnim številom potniških sedežev (MOPSC) šest ali manj se izvajajo le, če ima operator odobritev pristojnega organa, izdano na podlagi ocene varnostnih tveganj, ki jo je izvršil operator.
only conduct these operations in the areas and under the conditions specified in the approval;
izvaja te operacije le na tistih območjih in pod tistimi pogoji, ki so določeni v odobritvi;
not conduct these operations under a HEMS approval;
ne izvaja teh operacij na podlagi odobritve HNMP;
substantiate that helicopter limitations, or other justifiable considerations, preclude the use of the appropriate performance criteria; and
utemelji, da omejitve helikopterja ali drugi upravičeni premisleki onemogočajo uporabo ustreznih meril zmogljivosti, in
be approved in accordance with CAT.POL.H.305(b).
so odobreni v skladu s CAT.POL.H.305(b).
Notwithstanding CAT.IDE.H.240, such operations may be conducted without supplemental oxygen equipment, provided the cabin altitude does not exceed 10000 ft for a period in excess of 30 minutes and never exceeds 13000 ft pressure altitude.
Ne glede na CAT.IDE.H.240 se take operacije lahko izvajajo brez dodatne kisikove opreme, če višina kabine ne preseže 10000 ft za več kot 30 minut in nikoli ne preseže 13000 ft tlačne višine.
Mass and balance, loading
Masa in ravnotežje, obremenitev
During any phase of operation, the loading, mass and centre of gravity (CG) of the aircraft shall comply with the limitations specified in the AFM, or the operations manual if more restrictive.
V kateri koli fazi operacije so obremenitev, masa in masno središče zrakoplova v skladu z omejitvami iz letalskega priročnika zrakoplova ali iz operativnega priročnika, če je strožji.
The operator shall establish the mass and the CG of any aircraft by actual weighing prior to initial entry into service and thereafter at intervals of four years if individual aircraft masses are used, or nine years if fleet masses are used.
Operator določi maso in masno središče vsakega zrakoplova z dejanskim tehtanjem pred začetkom njegove uporabe in nato vsaka štiri leta, če se uporabljajo individualne mase zrakoplovov, in vsakih devet let, če se uporabljajo mase flot.
The accumulated effects of modifications and repairs on the mass and balance shall be accounted for and properly documented.
Upoštevajo in ustrezno dokumentirajo se skupni učinki predelav in popravil na maso in ravnotežje.
Aircraft shall be reweighed if the effect of modifications on the mass and balance is not accurately known.
Zrakoplovi se znova stehtajo, če učinek predelav na maso in ravnotežje ni točno znan.
The weighing shall be accomplished by the manufacturer of the aircraft or by an approved maintenance organisation.
Tehtanje izvede proizvajalec zrakoplova ali potrjena organizacija za vzdrževanje.
The operator shall determine the mass of all operating items and crew members included in the aircraft dry operating mass by weighing or by using standard masses.
Operator s tehtanjem ali na podlagi standardnih mas določi maso vseh operativnih delov in članov posadke, vključeno v suho operativno maso zrakoplova.
The influence of their position on the aircraft’s CG shall be determined.
Določi se vpliv njihovega položaja na masno središče zrakoplova.
The operator shall establish the mass of the traffic load, including any ballast, by actual weighing or by determining the mass of the traffic load in accordance with standard passenger and baggage masses.
Operator določi maso prometnega tovora, vključno z balastom, z dejanskim tehtanjem ali v skladu s standardnimi masami potnikov in prtljage.
In addition to standard masses for passengers and checked baggage, the operator can use standard masses for other load items, if it demonstrates to the competent authority that these items have the same mass or that their masses are within specified tolerances.
Operator lahko poleg standardnih mas za potnike in prijavljeno prtljago uporabi tudi standardne mase za druge natovorjene predmete, če pristojnemu organu dokaže, da imajo ti predmeti enako maso ali da je njihova masa v okviru določenih dovoljenih odstopanj.
The operator shall determine the mass of the fuel load by using the actual density or, if not known, the density calculated in accordance with a method specified in the operations manual.
Operator določi maso napolnjenega goriva na podlagi dejanske gostote, če ta ni znana, pa na podlagi gostote, ki se izračuna po postopku iz operativnega priročnika.
The operator shall ensure that the loading of:
Operator zagotovi, da natovarjanje:
its aircraft is performed under the supervision of qualified personnel; and
njegovih zrakoplovov poteka pod nadzorom usposobljenega osebja in
traffic load is consistent with the data used for the calculation of the aircraft mass and balance.
prometnega tovora poteka v skladu s podatki, uporabljenimi pri izračunu mase in ravnotežja zrakoplova.
The operator shall comply with additional structural limits such as the floor strength limitations, the maximum load per running metre, the maximum mass per cargo compartment and the maximum seating limit.
Operator upošteva dodatne konstrukcijske omejitve, kot so omejitve glede trdnosti tal, največja obremenitev na tekoči meter, največja masa na prostor za tovor in omejitve največjega števila sedežev.
For helicopters, in addition, the operator shall take account of in-flight changes in loading.
Poleg tega za helikopterje upošteva spreminjanje obremenitve med letom.
The operator shall specify, in the operations manual, the principles and methods involved in the loading and in the mass and balance system that meet the requirements contained in (a) to (i).
Operator v operativnem priročniku navede načela in postopke, ki se nanašajo na nakladanje ter sistem mase in ravnotežja, ki izpolnjuje zahteve iz odstavkov (a) do (i).
This system shall cover all types of intended operations.
Ta sistem zajema vse vrste predvidenih operacij.
Mass and balance data and documentation
Podatki in dokumentacija o masi in ravnotežju
The operator shall establish mass and balance data and produce mass and balance documentation prior to each flight specifying the load and its distribution.
Operator pred vsakim letom določi podatke o masi in ravnotežju ter pripravi dokumentacijo o masi in ravnotežju, v kateri sta navedena tovor in njegova porazdelitev.
The mass and balance documentation shall enable the commander to determine that the load and its distribution is such that the mass and balance limits of the aircraft are not exceeded.
Dokumentacija o masi in ravnotežju vodji zrakoplova omogoča opredelitev, ali sta tovor in njegova porazdelitev takšna, da omejitve zrakoplova za maso in ravnotežje niso presežene.
The mass and balance documentation shall contain the following information:
Dokumentacija o masi in ravnotežju vsebuje naslednje informacije:
Aircraft registration and type;
registracijo in tip zrakoplova;
Flight identification, number and date;
identifikacijsko številko in datum leta;
Name of the commander;
ime vodje zrakoplova;
Name of the person who prepared the document;
ime osebe, ki je pripravila dokument;
Dry operating mass and the corresponding CG of the aircraft:
suho operativno maso in ustrezno masno središče zrakoplova;
for performance class B aeroplanes and for helicopters the CG position may not need to be on the mass and balance documentation if, for example, the load distribution is in accordance with a pre-calculated balance table or if it can be shown that for the planned operations a correct balance can be ensured, whatever the real load is;
pri letalih razreda zmogljivosti B in helikopterjih lege masnega središča morda ni treba navesti v dokumentaciji o masi in ravnotežju, če je na primer porazdelitev tovora v skladu z vnaprej izračunano preglednico o ravnotežju ali če je mogoče dokazati, da je za načrtovane operacije mogoče zagotoviti ustrezno ravnotežje, ne glede na dejanski tovor;
Mass of the fuel at take-off and the mass of trip fuel;
maso goriva ob vzletu in maso goriva za potovanje;
Mass of consumables other than fuel, if applicable;
maso drugega potrošnega materiala razen goriva, če je ustrezno;
Load components including passengers, baggage, freight and ballast;
sestavne dele tovora, vključno s potniki, prtljago, tovorom in balastom;
Take-off mass, landing mass and zero fuel mass;
vzletno in pristajalno maso ter maso zrakoplova brez goriva;
Applicable aircraft CG positions; and
lege masnega središča zrakoplova, ki se uporabljajo, ter
The limiting mass and CG values.
mejne vrednosti mase in masnega središča.
The information above shall be available in flight planning documents or mass and balance systems.
Zgornje informacije so na voljo v dokumentih za načrtovanje letov ali sistemih mase in ravnotežja.
Some of this information may be contained in other documents readily available for use.
Nekatere od teh informacij so lahko v drugih dokumentih, ki so takoj na voljo za uporabo.
Where mass and balance data and documentation is generated by a computerised mass and balance system, the operator shall verify the integrity of the output data.
Če se dokumentacija o masi in ravnotežju pripravlja z računalniško podprtimi sistemi za maso in ravnotežje, operator preveri celovitost izhodnih podatkov.
The person supervising the loading of the aircraft shall confirm by hand signature or equivalent that the load and its distribution are in accordance with the mass and balance documentation given to the commander.
Oseba, ki nadzira natovarjanje letala, z lastnoročnim podpisom ali na enakovreden način potrdi, da sta tovor in njegova porazdelitev v skladu z dokumentacijo o masi in ravnotežju, predloženo vodji zrakoplova.
The commander shall indicate his/her acceptance by hand signature or equivalent.
Vodja zrakoplova z lastnoročnim podpisom ali na enakovreden način potrdi prejem.
The operator shall specify procedures for last minute changes to the load to ensure that:
Operator določi postopke za spremembo tovora v zadnjem trenutku za zagotovitev, da:
any last minute change after the completion of the mass and balance documentation is brought to the attention of the commander and entered in the flight planning documents containing the mass and balance documentation;
je vodja zrakoplova opozorjen na vse spremembe v zadnjem trenutku po izpolnitvi dokumentacije o masi in ravnotežju in so vnesene v dokumente za načrtovanje leta, ki vključujejo dokumentacijo o masi in ravnotežju;
the maximum last minute change allowed in passenger numbers or hold load is specified; and
je opredeljena največja dovoljena sprememba števila potnikov ali tovora v zadnjem trenutku in
new mass and balance documentation is prepared if this maximum number is exceeded.
da se pripravi nova dokumentacija o masi in ravnotežju, če je to največje število preseženo.
The operator shall obtain approval by the competent authority if he/she wishes to use an onboard integrated mass and balance computer system or a stand-alone computerised mass and balance system as a primary source for dispatch.
Operator pridobi odobritev pristojnega organa, če želi na zrakoplovu kot glavni vir za odpošiljanje uporabljati celovit računalniški sistem za maso in ravnotežje ali samostojen računalniško podprt sistem za maso in ravnotežje.