Atlas Avioane de Linie

8/13/2019 Atlas Avioane de Linie

1/177

PPEERRFFOORRMMAANNTTEEssii

CCAARRAACCTTEERRIISSTTIICCIIAAEERROONNAAVVEE

CCAATTAALLOOGGDDEEPPRREEZZEENNTTAARREE

VVOOLLUUMMUULL11

ROMATSA


2/177

ROMATSA - DMTA PERFORMANTE si CARACTERISTICI AERONAVE

DO ACH/ODF MAN0001 ACFT 1

DATA: iulie 2001, editia 1.0I

PERFORMANTE siCARACTERISTICI AERONAVE

CATALOG DE PREZENTARE

VOLUMUL 1


Editia : 1.0

Data editiei : 10.07.2001

Statut : Document propus

Clasificare : Document ROMATSA


3/177



DATA: iulie 2001, editia 1.0II

DESCRIEREA DOCUMENTULUI

Titlul:

PERFORMANTE si CARACTERISTICI AERONAVE

CATALOG DE PREZENTARE, VOLUMUL 1

REFERINTE ROMATSAPENTRU CONTROLUL DOCUMENTULUI:

COD DE IDENTIFICARE: DO ACH/ODF MAN0001 ACFT 1

EDITIA: 1.0

INDEX PROIECT: DATA: Iulie 2001

SUMAR:Prezinta performantele si caracteristicile a 144 de tipuri de aeronave care opereaza

frecvent in spatiul aerian al Romaniei

Cuvinte cheie:

aeronave, producatori, ICAO, caracteristici, performante, schite, grafice, poze

Persoane de contact: Gheorghe MANEA Telefon:230 3007 ext. 128, ACH

Radu CHIVU Telefon:230 3007 ext. 529, ODF

Virginia COMAN Telefon:230 3007 ext. 542, ACH

Elisabeta PLAMADEALA Telefon:230 3007 ext. 514, ACH

STATUTUL SI TIPUL DOCUMENTULUI

STATUTUL CATEGORIA CLASIFICAREA

Ciorna

Document propus

Document aprobat

Management

Specialist

Alte categorii

Public

ROMATSA

Confidential

REFERINTA ELECTRONICA

Nume fisier: Caracteristici_si_performante_aeronave.pdfEditor : Adobe Acrobat 4.0

FISA de IDENTIFICARE a DOCUMENTULUI


4/177



DATA: iulie 2001, editia 1.0III

Pagina de semnaturi

Nivel Functie/nume Semnatura Data

Aprobat Director General Marin VOICU

Director DMTA Dan ESTER

Director DMRT Mihai BRANISTE

Director DMRE Aurica COJOC

Avizat

Director DMSC Bogdan DONCIU

VerificatSef Serviciu ACH Ioan DELIANIS

Sef Serviciu ODF Stefan CUCU

ElaboratExpert ACH Gheorghe MANEA

Referent ODF Radu CHIVU

Referent ODF Virginia COMAN

Referent ODF Elisabeta PLAMADEALA

Consultant ACH Vasile POPA


5/177



DATA: iulie 2001, editia 1.0IV

Fisa de nregistrare a editiilor si amendamentelor

Nr.Editie

Nr.Amd.

Data Continut pe scurt Data si semnaturade introducere

Paginiafectate

1.0 - Iulie 2001 Document propus toate


6/177



DATA: iulie 2001, editia 1.0V

Lista paginilor efective

Cod document: DO ACH/ODF MAN0001 ACFT 1

Nr. Pag. Data

Nr.

Amendament Nr. Pag. Data

Nr.

Amendament


7/177



DATA: iulie 2001, editia 1.01

CUPRINS

Inroducere___________________________________________________________

BIBLIOGRAFIE_______________________________________________________

CAPITOLUL I Definitii________________________________________________

CAPITOLUL II Performante si Caracteristici Aeronave_______________________

3

1

16

149


8/177



Introducere 1/3 DATA: iulie 2001, editia 1.0

Introducere

Scopul lucrarii

Prezentul document sintetizeaza, ordoneaza si prezinta, intr-un prim volum,

performantele si caracteristicile a 144 de aeronave care opereaza frecvent in spatiul aerianal Romaniei.Necesitatea compilarii acestor date intr-o baza de date coerenta rezulta din cerintele

functionarii in bune conditii atat a sistemului IDS cat si a sistemului FDP/RDP, pentrupredictia traiectoriei unui zbor cu suficienta acuratete si, in consecinta, pentru calculareadiferitelor momente ale evenimentelor in zbor, in vederea fluidizarii optime si asigurariisigurantei zborurilor.

Domeniul de aplicare

Pentru ntocmirea bazei de date de performante si caracteristici aeronave si, inconsecinta pentru elaborarea prezentului document s-a pornit de la:

- analiza datelor existente;- consultarea urmatorilor beneficiari: controlori de trafic aerian, piloti, experti.

In acest sens, au fost identificate informatiile necesare personalului operativ dedirijare/informare pentru desfasurarea activitatii lor in trafic real in conditii de siguranta atraficului aerian, datele necesare pentru realizarea aplicatiilor tehnice de simulator si adatelor necesare functionarii sistemului FDP/RDP.

Documentul ar trebui distribuit tuturor subunitatilor operationale ROMATSA, pentru aservi ca material de referinta in activitatea curenta a personalului operativ dedirijare/informare a traficului.

De asemenea, consideram ca lucrarea de fata este o colectie cuprinzatoare de date,care poate fi asimilata cu o sursa utilade informatii pentru personalul operativ.

Referinte

Pentru intocmirea acestui document, s-au folosit numeroase documente, publicatii si altesurse de referinta, ca de exemplu:- Janes All the Worlds Aircraft;- Aircraft 2ndedition;- Aircraft Type Designators;- Companii aeriene ca TAROM, DACAIR, etc.

Structura documentuluiDocumentul este structurat in doua capitole:

- Capitolul 1: Definitii, inglobeaza definitiile termenilor folositi pe parcursul lucrarii;- Capitolul 2: Performante si caracteristici aeronave, sintetizeaza, ordoneaza si prezintaperformantele si caracteristicile a 144 de aeronave care opereaza frecvent in spatiulaerian al Romaniei.

Fiecare aeronava este prezentata pe o pagina, intr-o macheta care sintetizeazaprincipalele performante si caracteristici ale acesteia. Macheta contine de asemenea, opoza color a aeronavei, schita acesteia si graficul profilului de urcare.

Precizam ca graficul profilului de urcare a fost obtinut folosindu-se valori ale vitezei

verticale de urcare corespunzatoare pentru 75% din MTOW(Maximum TakeOff Weight).Spre comparatie, datele prezentate in blocul Operational Data - Climb corespund valoriiMTOW. Mentionam de asemenea ca, pentru unele aeronave nu a fost posibila (din lipsadatelor) prezentarea pozei color a aeronavei, schitei, sau a graficului profilului de urcare.


9/177




Pentru fiecare aeronava se pot urmari 6 blocuri distincte de date, dupa cum urmeaza*:

- Basic Data:ICAO Flight Plan Designator (campul 7 Aircraft Identification)Type of aircraft (campul 9 - Type of aircraft)

WTC (Wake Turbulence Category) (campul 9 - WTC)ManufacturerGeneral presentation of the aircraft

- Technical Data:Engines (Number and type of engines)Approach CategoryRange (NM) range with maximum capacityFuel capacity (ltr) (campul 19 Endurance, exprimat in ore si minute)Weights (Kg): MTOW (Maximum Take Off Weight)

MLW (Maximum Landing Weight)Dimensions (m): Wing Span

LengthHeight

ToD(Take-off distance)LD (Landingdistance)Exits (Number of emergency exits)PassengersCrew

(campul 19 Persons on Board)

SIWL (Single Wheel Load)LCN (Load Classification Number) valoarea lui se determina dintr-un grafic, in functie de

SIWL (Single Wheel Load, valoare extrasa din Aicraft Operations Manual) si de presiuneadin cauciucuri

- Operational Data Climb (date corespunzatoare MTOW)

RoC (Rate of Climb) up to FL 100 (fpm)RoC FL 100 up to FL 200 (fpm)RoC FL 200 up to FL 300 (fpm)RoC above FL 300 (fpm)Initial cruising altitudeIAS (Indicated Air Speed) up to FL 100 (fpm)

IAS FL 100 up to FL 200 (kts)IAS FL 200 up to FL 300 (kts)Mach number above FL 300

- Operational Data - Cruise

Absolute ceilingService ceiling (campul 19 - Level)Optimum ceilingService ceiling/OEIM/IAS optimum at optimum cruising level (M/kts)

*s-a optat pentru prezentarea terminologiei in limba engleza, asa cum apare in literatura de specialitate; deasemenea, s-au prezentat intre paranteze pozitiile respectivelor date in ICAO Flight Plan


10/177




True Air Speed (kts) (campul 15 Cruising Speed)Turbulence Penetration Speed (kts/M)M/IAS at optimum cruising level (M/kts)M/IAS at maximum certificated altitude (M/kts)

- Operational Data DescentRoD (Rate of Descent) from FL max to FL 310 (fpm)RoD from FL 310 to FL 160 (fpm)RoD below FL 160 (fpm)Maximum speed for RoD from FL max to FL 310 (M)Maximum speed for RoD from FL 310 to FL 160 (kts)Maximum speed for RoD below FL 160 (kts)Maximum rate of descent in emergency descent situation from FL max to safety level

- Operational Data for Approach

Minimum Clean speed (kts)Final Approach Speed (kts)

Documentul a fost compilat in ordinea alfabetica a codurilor ICAO ale aeronavelor.Pentru a facilita cautarea unei aeronave, documentul contine lista codurilor ICAO, cucorespondenta paginilor.

Pentru vizualizarea pe computer a documentatiei, s-a optat pentru prezentarealucrarii si pe suport magnetic.

Grupul de lucru care a intocmit prezentul volum va continua completarea acesteilucrari, care se va concretiza prin lansarea unei editii revizuite a volumului 1 si a volumului 2al Catalogului de Prezentare a Performantelor si Caracteristicilor Aeronavelor.

Autorii acestei editii vor aprecia orice comentariu sau idee constructiva pentruimbunatatirea acestui catalog.


11/177



Bibliografie 1/1 DATA: iulie 2001, editia 1.0

BIBLIOGRAFIE

Aircraft 2ndedition, DFS Deutsche Flugsicherung (1996)

Aircraft Type designators, 28th edition, International Civil Aviation Organization, Doc.8643/28 (November 2000)

ICAO Doc. 8168, VOL. II, Third and Fourth Editions Aircraft Operations Holding Speeds

Janes All the Worlds Aircraft 1995 1996, 1996 1997, 1997 1998, edited by PaulJackson MRAeS

Procedures for Air Navigation Services Rules of the Air and Air Traffic Services, 13thedition, International Civil Aviation Organization, Doc. 4444-RAC/501 (1996)

International Standards Rules of the Air - Annex 2 to The Convention on International CivilAviation, 9th edition,International Civil Aviation Organization (July 1990)

International Standards and Recommended Practices Air Traffic Services: Air TrafficControl Service, Flight Information Service, Alerting Service Annex 11 to The Conventionon International Civil Aviation, 12th edition , International Civil Aviation Organization(July 1998)

International Standards and Recommended Practices Operation of Aircraft Annex 6 toThe Convention on International Civil Aviation, Part I: International Commercial Air

Transport Aeroplanes, 6th edition of Part I, International Civil Aviation Organization(July 1995)

International Standards and Recommended Practices Operation of Aircraft Annex 6 toThe Convention on International Civil Aviation, Part II: International General Aviation Aeroplanes, 6th edition of Part II, International Civil Aviation Organization (July 1998)


12/177

CAPITOLUL I - DEFINITII


13/177



CAPITOLUL I - Definitii 2/16 DATA: iulie 2001, editia 1.0

A

Absolute ceilingGreatest altitude attainable by aircraft in unaccelerated flight.

AeroplaneA power driven heavier-than-air aircraft, deriving its lift in flight chiefly from aerodynamicreactions on surfaces which remain fixed under given conditions of flight.

AccommodationMaximum seating capacity for all economy configuration with maximum number of seatsabreast and minimum pitch. This layout may differ in accordance with airlines operationalrequirements.

Aircraft

Any machine that can derive support in the atmosphere from the reactions of the air againstthe earths surface.

AerodromeA defined area on land or water (including any buildings, installations and equipment)intended to be used either wholly or in part for the arrival, departure and surface movementof aircraft.

Alternate aerodromeAn aerodrome to which an aircraft may proceed when it becomes either impossible or

inadvisable to proceed to or to land at the aerodrome of intended landing. Alternateaerodromes include the following:

Take-off alternateAn alternate aerodrome at which an aircraft can land should become necessaryshortly after take-off and it is not possible to use the aerodrome of departure.

En-route alternateAn aerodrome at which an aircraft would be able to land after experiencing anabnormal or emergency condition while en route.

Destination alternateAn alternate aerodrome to which an aircraft may proceed should it become either

impossible or inadvisable to land at the aerodrome of intending landing.

AilavatorControl surface functioning as aileron and elevator.

AirstairRetractable stairway built into aircraft.

ICAO Approach categoriesThe following ICAO table indicates the specified range of handling speeds (KIAS) for each

category of aircraft to perform the manoeuvres specified. These speed ranges have beenassumed for use in calculating airspace and obstacle clearance requirements for eachprocedure.


14/177




Table 1: ICAO Approach categories

MAX SPEEDS forMissed Approach

Aircraftcategory

Vat

Range ofSpeeds for

Initial

Approach

Range ofFinal

Approach

Speeds

MAXSPEEDS for

VisualManoeuvring

(Circling) Intermediate FinalA < 91 90 / 150

(110 *)70 /100 100 100 110

B 91 / 120 120 / 180(140 *)

85 / 130 135 130 150

C 121 / 140 160 / 240 115 / 160 180 160 240

D 141 / 165 185 / 250 130 / 185 205 185 265

E 166/ 210 185 / 250 155 / 230 240 230 275

Vat - speed at threshold based on 1.3 times stall speed in the landing configuration at

maximum certified landing mass.* - maximum speed for reversal and racetrack procedures.Category E contains only certain Military Aircraft and is not included on Jeppesen ApproachCharts.

Approach noiseMeasured 1 NM from downwind end of runway with aircraft passing overhead at 113 m(370ft).

AnhedralDownward slope of wing from root to tip.

Angle of attackAngle at which airstream meets airfoil (angle between mean chord and free streamdirection);*not to be confused with angle of incidence

AerofoilAny solid body so shaped that as a fluid medium (air or hot gas) moves past it, isexperiencing a useful force perpendicular to the direction of relative motion; thus a winggenerate lift, while a turbine blade generates torque on a shaft.

Angle of incidenceStrictly, the angle at which the wing is set in relation to the zone / aft axis. Wrongly used tomean angle of attack.

AntegyroRotary wing aircraft propelled by a propeller (or other thrusting device) and lifted by a freelyrunning autorotating rotor.

Avionics

Aviation electronics


15/177




B

BarISA pressure at S/L is 1013.2 mb or just over 1 bar. ICAO has standardised hectopascal foratmospheric pressure, in which ISA S/L pressure is 1013.2 hPa.

Bleed airHot high-pressure air extracted from gas turbineengine compressor or combuster and takenthrough valves and pipes to perform useful work such as pressurisation driving machinery oranti icing by heating surfaces.

C

Cabin altitude

Height above S / L at which ambient pressure is the same as inside the cabin.

CanardsForeplanes, fixed or controllable aerodynamic surfaces ahead of centre of gravity (CG).

ChaffThin slivers of radar reflective material cut to length appropriate to wavelengths of hostileradars and scattered in bundles to protect friendly aircraft.

Cabin attendant

A crew member who performs, in the interest of safety of passengers duties assigned by theoperator or the pilot in command of the aircraft, but who shall not act as a flight crewmember.

Commercial air transport operationAn aircraft operation involving the transport of passengers, cargo or mail for remuneration orhire.

Crew memberA person assigned by an operator to duty on an aircraft during flight time.

Cruising levelA level maintained during a significant portion of a flight. Necessary for ACC controllers.

CleanIn flight confirmation with landing gear, flaps, slots and so on retracted.

ContrarotatingPropellers on same axis turning in opposite direction.

ConvertibleTransport aircraft able to be equipped to carry passengers or cargo.


16/177




D

Dangerous goodsArticles or substances which are capable of poising significant risk to health, safety orproperty when transported by air.

DeratedEngine restricted to power less than potential maximum (usually such an engine is flatrated).

DihedralUpward slope of wing from root to tip.

Disposable loadSum of masses that can be loaded or unloaded, including payload, crew, usable fuel and so

on.

DopplerShort for Doppler radar radar using fact that received frequency is a function of relativevelocity between transmitter or reflecting surface and receiver; used for measuring speedover ground or for detecting aircraft or moving vehicles against static ground or sea.

E

Emergency locator transmitter (ELT)A generic term describing equipment which broadcast distinctive signals on designatedfrequencies and, depending on application, may be automatically activated by impact or bemanually activated. An ELT may be any of the following:

Automatic fixed ELT (ELT(AF))An automatically activated ELT which is permanently attached to an aircraft.

Automatic portable (ELT(AP))An automatically activated ELT which is rigidly attached to an aircraft but readily

removable from the aircraft.

Automatic deployable ELT (ELT(AD))An ELT which is rigidly attached to an aircraft and which is automatically deployedand activated by impact and, in some cases, also by hidrostatic sensors. Manuallydeployment is also provided.

Survival ELT (ELT (S))An ELT which is removable from an aircraft, stowed so as to facilitate its ready use inan emergency and manually activated by survivors.

ElevonWing trailing-edge control surface combining functions of aileronsand elevators.


17/177




F

FarFederal Aviation Regulation

Far Pt 23Defines the airworthiness of private and air taxi aeroplanes of 5670 Kg (12500 lb.) MTOWand below;

Far Pt 25Defines the airworthiness of public transport aeroplanes exceeding 5670 kg (12500 lb.)MTOW.

Far field lengthDefines the length measured on the runway necessary for take off and landing of the

aircraft, at MTOW, S/L, ISA +15C, dry RWY, zero slope.

Take off field length at S/L, ISA+15CDefines the length, measured on the runway, from break release to 15m up in the airnecessary for take off of the aircraft.

Landing field length at S/L, MLW, ISA+15CDefines the length, measured on the runway, from 15m up in the airto full stop of theaircraft.

Flight crew memberA licensed crew member charged with duties essential to the operation of an aircraft duringflight time.

Flight planSpecified information provided to air traffic services units, relative to an intended flight orportion of a flight of an aircraft.

FactoredMultiplied by an agreed number to take account of extreme adverse conditions, errors,design deficiencies other inaccuracies.

Fail operationalSystem which continues to function after any single fault has occurred.

Fail safeStructure or system which survives to a failure (in case of system may no longerfunction normally).

Feathering

Setting propeller or similar blades at pitch aligned with slipstream to give resultant torque(not tending to turn shaft) and thus minimum drag;


18/177




Final Approach SpeedTypical speed for the final approach segment.

FinesseThe ratio L / D (lift-to-drag) ratio is sometimes called glide-number or glide ratio or

finesse.

Table 2shows a summary of aerodynamic efficiency L / D. Some data are estimated.

Table 2: Summary of Lift- to- Drag Ratio

Aircraft (year) (L / D) max

Boeing Boeing 707 - 320 19.4

Douglas DC-8 17.9

Airbus A 320 17

Boeing 767- 200 19Boeing 747-100 17.7

Douglas DC-10 17.7

Lockheed Tristar L1011 17.0

Douglas DC-9 (1966) 16

Boeing B727-200 16.4

Fokker 50 (1966) 16.5

Flight recorderAny type of recorder installed in the aircraft for the purpose of complementing accident /incident investigation.

Flight timeThe total time from the moment an aircraft first moves under its own power for the purposeof taking off until the moment it comes to rest at the end of the flight.

Note: - flight time as here defined is synonymous with the term block to block time orchock to chock time in general usage which is measured from the time an aircraft movesfrom the loading point until it stops at the unloading point.

ForeplanesPivoted canard surfaces forming part of the primary flight control system with authority inpitch and possibly also in roll.See also canards.

FlapA surface carried on the leading or trailing edge of a wing and able to move relative to it.


19/177




FlaperonWing trailing edge surface combining functions of flap and aileron.

Flight data recorder

Crash protected recorder of dynamic / static pressure, air temperature, control - surfaceand slat / flap positions, 3-axis accelerations, engine parameters and possibly othervariables;

Free turbineTurbine mechanically independent of engine upstream, other than being connected byrotating bearings.

Fuel (capacity)Maximum internal fuel capacity of the aircraft.

G

Green aircraftAircraft flyable but unpainted, unfurnished and basically equipped;

Glide slopeElement giving vertical (height) guidance in ILS;

Gunship

Aircraft designed for battlefield attack; helicopter gunship normally with slim body carryingpilot and weapon operator only.

H

HandedRotating in opposite directions.

Hardened

Protected as far as possible against nuclear explosion.

Holding procedureA predetermined manoeuvre which keeps an aircraft within a specified airspace whileawaiting further clearance.

Holding speedSpeed maintained by aircraft during holding procedure.

Table 3shows a summary of the aircraft operations holding speeds.


20/177




Table 3: Holding speedsICAO Doc. 8168, VOL. II, Third and Fourth Editions Aircraft Operations Holding Speeds

Levels(1) Normal conditions Turbulence conditions

up to 4250 m inclusive14000 ft

425 km/h(2)

(230 kts)

315 km/h(4)

(170 kts)

520 km/h(3)

(280 kts)

315 km/h(4)

(170 kts)

above 4250 m to 6100 m inclusive14000 ft to 20000 ft

445 km/h(5)

(240 kts)

above 6100 m to 10350 m inclusive20000 ft to 34000 ft

490 km/h(5)

(265 kts)

520 km/h (280 kts)or 0.8 Mach,whichever is less(3)

Above 10350 m34000 ft

0.83 Mach 0.83 Mach

(1)The levels tabulated represents altitudes or corresponding fight levels depending upon

the altimeter setting in use.(2) When the holding procedure is followed by the initial segment of an instrumentapproach procedure promulgated at a speed higher than 425 km/h (230kts), the holdingshould also be promulgated at this higher speed whenever possible.(3)The speed of 520 km/h (280kts) (0.8Mach) reserved for turbulence conditions shall beused for holding only after prior clearance with ATC, unless the relevant publicationsindicate that the holding area can accommodate aircraft flying at these high holdingspeeds.(4)For holdings limited to CAT A and B aircraft only.(5) Wherever possible, 520 km/h (280 kts) should be used for holding proceduresassociated with airway route structures.

Hovering ceilingCeiling of helicopter (corresponding to air density at which maximum rate of climb is zero).

I

Inertial navigationMeasuring all accelerations imparted to a vehicle and, by integrating these with respect totime calculating speed at every instant (in all them planes) and by integrating a second timecalculating total charge of portion in relation to starting point.

Instrument meteorological conditions (IMC)Meteorological conditions expressed in terms of visibility, distance from cloud and ceilingless than minimum specified for visual meteorological conditions.

Instrument approach and landing operationsInstrument approach and landing operations using instrument approach procedures are classified as follows:

Non-precision approach and landing operationsAn instrument approach and landing which does not utilise electronic glide pathguidance;


21/177




Precision approach and landing operationsAn instrument approach and landing using precision azimuth and glide path guidancewith minimum as determined by the category of operation.

Categories of precision approach and landing operations( JAR - OPS ):

Category I (CAT I) operationA precision instrument approach and landing with a decision height lower than 60m(200 ft) and with either a visibility not less than 800 m or a runway visual range notless than 550m.

Category II (CATII) operationA precision instrument approach and landing with a decision height lower than 60 m(200 ft), but not lower than 30m (100 ft) and a runway visual range not less than 300m.

Category III A (CAT III A) operationA precision instrument approach and landing with:

decision height lower than 30 m (100 ft) or no decision height; anda runway visual range not less than 200m.

Category III B (CAT III B) operationA precision instrument approach and landing with:

a) decision height lower than 15 m (50 ft) or no decision height; andb) a runway visual range less than 200 m but not less than 75m.

Category III C (CAT III C) operationA precision instrument approach and landing with no decision height and no runwayvisual range limitations.

Note where decision height (DH) and runway visual range (RVR) fall into differentcategories of operation, the instrument approach and landing operations would beconducted in accordance with the requirements of the most demanding category (e.g. anoperation with a DH in the range of CAT III A, but with an RVR in the range of CAT III Bwould be considered a CAT III B operation or an operation with a DH in the range of CAT II,but an RVR in the range of CAT I would be considered a CAT II operation).

J

Joined wingTandem wing layout in which forward and aft wings are swept so that the outer sectionsmeet.

L

Load factorDesign factor (g limit) for airframe of the aircraft.


22/177




Load Classification Number (LCN)Defines the bearing strength of runway pavement.

LocaliserElement giving steering guidance in ILS.

Long-range/ normalcruisingspeed / Mach numberTypical speed range for normal cruise and long-range economical cruisein kts and machnumber. The comparison between kts and Mach number will vary in accordance withthe aircrafts` altitude or flight level.

Large aeroplaneAn aeroplane of a maximum certified take-off mass of over 5700 kg.

M

Maximum massMaximum certified take-off mass;

Maximum cruising speed/ Mach numberTypical speed for maximum cruise. Data concerning military high performance jet aircraftare referred to aircraft in clean configuration, without external loads and armament, toillustrate the highest possible performance.

Medevac

Medical evacuation.

Minimum clean speedLowest speed range for aircraft in clean configuration, without usage of speed brakes,spoilers, etc.

Minimum equipment list (MEL)A list which provides for the operation of aircraft subject to specified conditions withparticular equipment inoperative, prepared by an operator in conformity with, or morerestrictive than the MMEL (master minimum equipment list) established for the aircraft type.

Minimum descent altitude (MDA) or minimum descend height (MDH)A specified altitude or height in a non-precision approach or circling approach below whichdescend must not be made without the required visual reference.

N

NightThe hours between the end of evening civil twilight and the beginning of morning civil twilight

or such other period between sunset or sunrise, as may be prescribed by the appropriateauthority.


23/177




Note civil twilight ends in the evening when the centre of the suns` disc is 6degrees belowthe horizon and begins in the morning when the centre of the suns` disc is 6 degrees belowthe horizon.

O

Operational controlThe exercise of authority over the initiation, continuation, divertion or termination of a flight inthe interest of the safety of the aircraft and the regularity and efficiency of the flight.

Operational flight planThe operators` plan for the safe conduct of the flight based on considerations of aeroplaneperformance, other operating limitations and relevant expected conditions on the route to befollowed and at the aerodromes concerned.

Operational manualA manual containing procedures, instructions and guidance for use by operational personnelin the execution of their duties.

OperatorA person, organisation or enterprise engaged in or offering to engage in an aircraftoperation;

OptimumThe best that is possible;

Optimum speedThe speed of an aircraft to obtain maximum range with minimum flight time with minimumfuel consumption.

Optimum levelA level of aircraft in normal operation to maintain optimum speed.

P

PayloadDisposable load generating revenue (passengers, cargo, mail and other paid items 0; inmilitary aircraft, loosely used to mean total load carried of weapons, cargo or other missionequipment;

PlaneA lifting surface (for example wing, tailplane).

Pilot-in-command

The pilot responsible for the operation and safety of the aircraft during flight time.


24/177




Primary-flight controlsThose used to control trajectory of aircraft (thus, not trimmers, tabs, flaps, slats, airbrakes orlift dumps and so on).

Primary-flight displays

Single screen bearing all data for aircraft flight path control.

ProfanA family of new technology propellers characterised by multiple scimitar shaped blades withthin sharp-edged profile. Single and contrarotating examples promise to extend propellerefficiency up to an aircraft mach number of about 0.8.

Pressure-altitudeAn atmospheric pressure expressed in terms of altitude which corresponds to that pressurein the Standard Atmosphere.

PortLeft sideof the aircraft, looking forward.

Psychoactive substancesAlcohol, opioids, cannabinoids, sedatives and hypnoties, cocaine, other psychostimulants,hallucinogens and volatile solvents, whereas coffee and tobacco are excluded.

R

Radiusof actionIn terms of performance, the distance an aircraft can fly from base and return withoutintermediate landing.

Rate of climbVertical distance flown by an aircraft in a unit of time, during climb given in feet / min underISA conditions with maximum take-off weight (MTOW). These data depend on manyexternal influences and differ in daily operations.

Rate of descend

Vertical distance flown by an aircraft in a unit of time, during descend, given in feet / minunder ISA conditions with maximum landing weight (MLW). These data depend on manyexternal influences and differ in daily operations.

RangeThe distance an aircraft can fly with specified load and usually while making allowance forspecified additional manoeuvres (directions, stand off, go-around and so on).

Runway visual range - (RVR)The range over which the pilot of an aircraft on the centre line of a runway can see therunway surface markings or the lights delineating the runway or identifying its centre line.

RuddervatorsFlying control surface.


25/177




RedundantProvided with spare capacity or data channels and thus made to survive failures.

Required navigation performance (RNP)

A statement of the navigation performance necessary for operation within a definedairspace.

RNP typeA containment value expressed as a distance in nautical miles from the intended positionwithin which flights will be for at least 95 per cent of the total flying time.

S

Safe-life

A term denoting that a component has proved by testing that it can be expected to continueto function safely for a precisely defined period before replacement.

Sensitive altimeterAltitude indicator of mechanical type, having acute sensitivity.

Service ceilingUsually height equivalent to air at which maximum attainable rate of climb is 100 ft / min.

Sideline noise

EPNDB measure of aircraft landing and taking off at point 0,25 NM (two or three engined) or0,35 NM (four engined) from runway center line.

SlatAuxiliary curved or mini-aerofoil surface designed to prevent flow breakaway from a wing ortail. On a tail leading edge it may be fixed, leaving a narrow slot. On a wing it is alwaysretractable, normally flush with the wing profile, but extended (under power or byaerodynamic lift) to leave a narrow slot for take off, low speed loiter or landing.

Sidestick

Control column in the form of a short handgrip beside the pilot.

State of registryThe state on whose register the aircraft is entered.

Stalling speedAirspeed at which aircraft stalls at 1g, that wing lift suddenly collapses.

Standard DayISA temperature and pressure;

StarboardRight sideof the aircraft, looking forward.


26/177




StealthLow-observable (materials and structures designed to reduce aircraft signatures of allkinds).

Specific fuel consumption

Rate at which fuel is consumed divided by power or thrust developed and thus a measure ofengine efficiency.

Stick shakerStall-warning device that noisily shakes pilots` control column as stalling angle of attack isneared.

T

Taileron

Left and right tail planes used as primary control surfaces.

TailplaneMain horizontal tail surface, originally fixed and carrying hinged elevator(s) but today oftensingle slab serving as control surface.

TransponderRadio transmitter triggered automatically by a particular received signal as in civil secondarysurveillance radar (SSR).

TurbofanGas turbine jet engine generating most thrust by a large-diameter cowled fan, with smallpart added by jet from core.

TurbojetSimplest form of gas turbine comprising compressor, combustion chamber, turbine andpropulsive nozzle.

TurbopropGas turbine in which as such energy as possible it from gas jet and used to drive reduction

gearbox and propeller.

U

Usable fuelTotal mass of fuel consumable in flight, usually 95 to 98 per cent of system capacity.

Useful loadUsable fuel plus payload.

UnfactoredPerformance level expected of average pilot, in average aircraft, without additional safetyfactors.


27/177




W

WetHousing fuel; wet wing often has extra connotations of integral tankage;

WheelbaseMinimum distance from nosewheel or tailwheel (centre of contact area) to live joiningmainwheels (center of contact area).

WidebodyPassenger aircraft with cabin wide enough to have two longitudinal aisles between seats.

WingletSmall auxiliary aerofoil, usually sharply upturned and often swept back, at tip of wing.

Y

Yoke

Pilots` flight control interface for pitch and roll axes in the form of a stick (control column) tothe top of which is laterally pivoted a pair of handgripes in the form of Y.


28/177

CAPITOLUL II - PERFORMANTE si

CARACTERISTICI AERONAVE


29/177

PAGEICAO TYPE MANUFACTURER

1A306 A-300-600 AIRBUS INDUSTRIES

2A30B A-300-B2/4 AIRBUS INDUSTRIES



5A318 A-318 AIRBUS INDUSTRIES












17A748 BAe-748 BRITISH AEROSPACE

18AT43 ATR-42-300 AEROSPATIALE/ALENIA

19AT45 ATR-42-500 AEROSPATIALE/ALENIA

20AT72 ATR-72 AEROSPATIALE/ALENIA

21ATP ATP JETSTREAM 61 BRITISH AEROSPACE

22B190 BEECH 1900 D BEECHCRAFT

23B350 BEECH Super King Air 350 BEECHCRAFT

24B461 BAe-146-100 BRITISH AEROSPACE



27B703 B707-300 BOEING

28B712 B717-200 BOEING

29B721 B727-100 BOEING


30/177


30B722 B727-200 BOEING

31B732 B737-200 BOEING

32B733 B737-300 BOEING

33B734 B737-400 BOEING

34B735 B737-500 BOEING

35B736 B737-600 BOEING

36B737 B737-700 BOEING

37B738 B737-800 BOEING

38B739 B737-900 BOEING

39B741 B747-100 BOEING

40B742 B474-200 BOEING

41B743 B747-300 BOEING

42B744 B747-400 BOEING

43B74S B747SP BOEING

44B752 B757-200 BOEING

45B762 B767-200 BOEING

46B763 B767-300 BOEING

47B772 B777-200 BOEING

48B773 B777-300 BOEING

49BA11 BAC 1-11-500 BRITISH AEROSPACE/Rombac

50BE10 BEECH 100 King Air BEECHCRAFT

51BE20 BEECH 200, Super King Air BEECHCRAFT

52BE30 BEECH Super King Air 300 BEECHCRAFT

53BE40 Beechjet 400 A BEECHCRAFT

54BE58 BEECH 58 Baron BEECHCRAFT

55BE60 BEECH 60 Duke BEECHCRAFT

56BE65 BEECH 65 Queen Air BEECHCRAFT

57BE76 BEECH 76 BEECHCRAFT

58BE99 BEECH 99 BEECHCRAFT


31/177


59BE9L BEECH 90 BEECHCRAFT

60C130 C-130 LOCKHEED

61C135 Stratolifter BOEING

62C160 TRANSALL AEROSPATIALE

63C17 C-17 Globemaster 3 MCDONNELL DOUGLAS

64C210 CESSNA 210,T210 Centurion CESSNA

65C212 CASA C-212 Aviocar CASA

66C303 CESSNA T303 Crusader CESSNA

67C310 CESSNA 310 CESSNA

68C337 CESSNA 337, (Turbo)Super Sky CESSNA


70C402 CESSNA 401,402 Businessliner CESSNA


72C421 Golden Eagle CESSNA

73C425 Corsair CESSNA

74C441 CESSNA 441 Conquest CESSNA

75C500 Citation 1 CESSNA

76C501 Citation 1SP CESSNA

77C525 CitationJet CESSNA

78C560 Citation 5/5 Ultra CESSNA

79C650 Citation VI CESSNA

80C750 Citation X CESSNA

81CN35 CASA CN-235, Persuader CASA

82CONC Concorde AEROSPATIALE/BA

83CRJ1 RJ-100 CANADAIR



86D228 DORNIER 228 DORNIER

87D328 DORNIER 328 DORNIER


32/177


88DC10 DC-10 MCDONNELL DOUGLAS

89DC87 DOUGLAS DC-8-73 MCDONNELL DOUGLAS

90DH8A DASH8-100 DE HAVILLAND

91DH8B DASH8-200 DE HAVILLAND

92DH8C DASH8-300 DE HAVILLAND

93DH8D DASH8-400 DE HAVILLAND

94E110 EMBRAER EMB-110 EMBRAER


96E121 EMB-121 Xingu EMBRAER

97E135 ERJ-135 EMBRAER


99F100 FOKKER 100 FOKKER

100F27 FOKKER F-27 FOKKER

101F28 FOKKER F-28 FOKKER




105G159 Gulfstream 1 GRUMMAN

106GLF2 GULFSTREAM 2/2B/2SP GRUMMAN

107GLF3 Gulfstream 3/SMA GULFSTREAM AEROSPACE

108GLF4 Gulfstream 4/4SP/SRA-4 GULFSTREAM AEROSPACE

109GLF5 Gulfstream 5 GULFSTREAM AEROSPACE

110JS31 Jetstream 31 BRITISH AEROSPACE

111JS32 Jetstream Super 31 BRITISH AEROSPACE

112JS41 Jetstream 41 BRITISH AEROSPACE

113L101 L-1011 TriStar LOCKHEED

114L188 L-188 Electra LOCKHEED

115L29A L-1329 LOCKHEED

116L29B L-1329 LOCKHEED


33/177


117L410 LET L-410/420 LET

118L610 LET L-610 LET

119LJ23 LEAR JET 23 GATES LEARJET



122LJ28 LEARJET 28 GATES LEARJET






128MD11 MD-11 MCDONNELL DOUGLAS






134N262 N-262, FrTgate AEROSPATIALE

135S601 SN-601, Corvette AEROSPATIALE

136SB20 SAAB 2000 SAAB

137SC7 Skyvan SHORTS

138SF34 SAAB 340 SAAB

139SH33 SHORT 330 / Sherpa SHORTS

140SH36 SHORT 360 SHORTS

141STAR BEECH 2000 Starship BEECHCRAFT

142T134 TUPOLEV 134 TUPOLEV




34/177

Passengers transport aircraft, low wing monoplan, all-weather operation, two jet engines, underwing landing

gear, normal tail low set.

Manufacturer

AIRBUS INDUSTRIES

Type ICAO

A306

WTC

H

APP Category C

2000 2500RoC up to FL 100 (fpm) to

1500 2000RoC FL 100 up to FL 200 (fpm) to


600 800RoC above FL 300 (fpm) to

1000RoC at SL/OEI (fpm)

240IAS up to FL 100 (fpm) 340to Optimum IAS (kts) 300

250IAS FL 100 up to FL 200 (fpm) 330to Optimum IAS (kts) 300


0.76Mach above FL 300 0.84to Optimum Mach 0.80

310Initial cruising altitude

Operational Data Climb

Technical Data

Dimensions (m)

45Wing Span54Length

16Height

Weights (kg)

134000MTOW140000MLW

2400TORA (m)

1000LDA (m)

Engines L2J

Fuel cap. (ltr.) 75500Range (NM) 3000

CrewPassengers

Operational Data Cruise

410Absolute ceiling

410Service ceiling

330Optimum ceiling

140Service ceiling/OEI

0.80M/IAS optimum at optimum cruising level (M/kts)

0.76M/IAS at optimum cruising

level (M/kts)0.84to

0.79M/IAS at maximum

certificated altitude (M/kts)

0.84to

460True Air Speed (kts)

280Turbulence Penetration Speed (kts)

0.79 (M)

Operational Data Descent

Below FL 160

(fpm)

From FL 310 to

FL 160 (fpm)

From FL max

to FL 310 (fpm)

RoD (fpm)

Optimum speed for RoD (kts/M)Maximum speed for RoD (kts/M)

2000 3000 2000

0.80 300 3000.84 320 340

340Maximum operating speed (kts/M) 0.84/

8000Max. rate of descent in "emergency

descent" situation (fpm)

230Min. clean

speed (kts)

130Final

Approach

speed (kts)

Exits 6

1 of144

Operational Data for

Approach

SIWL/LCN Finesse 1/15

A-300-600

MTOW 75%

ROMATSA


35/177



Manufacturer

AIRBUS INDUSTRIES

Type ICAO

A30B

WTC

H

APP Category C












Technical Data

Dimensions (m)

45Wing Span54Length

16Height

Weights (kg)

157000MTOW171700MLW

2200TORA (m)

1000LDA (m)

Engines L2J


CrewPassengers


410Absolute ceiling

410Service ceiling

350Optimum ceiling




level (M/kts)0.84to



0.84to



0.79 (M)


Below FL 160

(fpm)

From FL 310 to

FL 160 (fpm)

From FL max

to FL 310 (fpm)

RoD (fpm)


2000 3000 2000

0.80 300 3000.84 320 340




230Min. clean

speed (kts)

130Final

Approach

speed (kts)

Exits 6

2 of144


Approach


A-300-B2/4

MTOW 75%

ROMATSA


36/177



Manufacturer

AIRBUS INDUSTRIES

Type ICAO

A312

WTC

H

APP Category C












Technical Data

Dimensions (m)

44Wing Span47Length

16Height

Weights (kg)

142000MTOW121500MLW

2400TORA (m)

900LDA (m)

Engines L2J


CrewPassengers


410Absolute ceiling

410Service ceiling

350Optimum ceiling




level (M/kts)0.84to



0.84to



0.79 (M)


Below FL 160

(fpm)

From FL 310 to

FL 160 (fpm)

From FL max

to FL 310 (fpm)

RoD (fpm)


2000 3000 2000

0.80 300 3000.84 320 340




230Min. clean

speed (kts)

130Final

Approach

speed (kts)

Exits 6

3 of144


Approach


A-310-200

MTOW 75%

ROMATSA


37/177



Manufacturer

AIRBUS INDUSTRIES

Type ICAO

A313

WTC

H

APP Category C












Technical Data

Dimensions (m)

44Wing Span47Length

16Height

Weights (kg)

164000MTOW124000MLW

2400TORA (m)

900LDA (m)

Engines L2J


CrewPassengers


410Absolute ceiling

410Service ceiling

350Optimum ceiling




level (M/kts)0.84to



0.84to



0.78 (M)


Below FL 160

(fpm)

From FL 310 to

FL 160 (fpm)

From FL max

to FL 310 (fpm)

RoD (fpm)


2000 3000 2000

0.80 300 3000.84 320 340




230Min. clean

speed (kts)

130Final

Approach

speed (kts)

Exits 6

4 of144


Approach


A-310-300

MTOW 75%

ROMATSA


38/177



Manufacturer

AIRBUS INDUSTRIES

Type ICAO

A318

WTC

M

APP Category C












Technical Data

Dimensions (m)

34Wing Span32Length

12.5Height

Weights (kg)

59000MTOW56000MLW

1700TORA (m)

1400LDA (m)

Engines L2J


CrewPassengers


390Absolute ceiling

390Service ceiling

350Optimum ceiling




level (M/kts)0.82to



0.82to



0.78 (M)


Below FL 160

(fpm)

From FL 310 to

FL 160 (fpm)

From FL max

to FL 310 (fpm)

RoD (fpm)


2000 3000 2500

0.79 300 3000.82 320 335




220Min. clean

speed (kts)

130Final

Approach

speed (kts)

Exits 6

5 of144


Approach


A-318

Not Available

Not Available

Not Available

ROMATSA


39/177



Manufacturer

AIRBUS INDUSTRIES

Type ICAO

A319

WTC

M

APP Category C












Technical Data

Dimensions (m)

34Wing Span34Length

12.5Height

Weights (kg)

64000MTOW61000MLW

1800TORA (m)

1400LDA (m)

Engines L2J


CrewPassengers


390Absolute ceiling

390Service ceiling

350Optimum ceiling




level (M/kts)0.82to



0.82to



0.78 (M)


Below FL 160

(fpm)

From FL 310 to

FL 160 (fpm)

From FL max

to FL 310 (fpm)

RoD (fpm)


2000 3000 2500

0.79 300 3000.82 320 335




220Min. clean

speed (kts)

130Final

Approach

speed (kts)

Exits 6

6 of144


Approach


A-319

MTOW 75%

ROMATSA


40/177



Manufacturer

AIRBUS INDUSTRIES

Type ICAO

A320

WTC

M

APP Category C












Technical Data

Dimensions (m)

34Wing Span38Length

12.5Height

Weights (kg)

73500MTOW64500MLW

1900TORA (m)

1400LDA (m)

Engines L2J


CrewPassengers


390Absolute ceiling

390Service ceiling

350Optimum ceiling




level (M/kts)0.82to



0.82to



0.78 (M)


Below FL 160

(fpm)

From FL 310 to

FL 160 (fpm)

From FL max

to FL 310 (fpm)

RoD (fpm)


2000 3000 2500

0.79 300 3000.82 320 335




220Min. clean

speed (kts)

130Final

Approach

speed (kts)

Exits 6

7 of144


Approach


A-320

MTOW 75%

ROMATSA


41/177



Manufacturer

AIRBUS INDUSTRIES

Type ICAO

A321

WTC

M

APP Category C












Technical Data

Dimensions (m)

34Wing Span44.5Length

11.8Height

Weights (kg)

83000MTOW73500MLW

2400TORA (m)

1100LDA (m)

Engines L2J


CrewPassengers


430Absolute ceiling

390Service ceiling

350Optimum ceiling




level (M/kts)0.82to



0.82to



0.78 (M)


Below FL 160

(fpm)

From FL 310 to

FL 160 (fpm)

From FL max

to FL 310 (fpm)

RoD (fpm)


2000 3000 2500

0.79 300 3000.82 320 340




220Min. clean

speed (kts)

140Final

Approach

speed (kts)

Exits 8

8 of144


Approach


A-321

MTOW 75%

ROMATSA


42/177

Passengers wide bodied transport aircraft, low wingmonoplan, all-weather operation, two jet engines,

underwing landing gear, normal tail low set.

Manufacturer

AIRBUS INDUSTRIES

Type ICAO

A332

WTC

H

APP Category C












Technical Data

Dimensions (m)

60.3Wing Span58Length

17.9Height

Weights (kg)

230000MTOW180000MLW

2600TORA (m)

1200LDA (m)

Engines L2J

Fuel cap. (ltr.) 1E+05Range (NM) 6400

CrewPassengers


410Absolute ceiling

410Service ceiling

350Optimum ceiling




level (M/kts)0.86to



0.86to



0.82 (M)


Below FL 160

(fpm)

From FL 310 to

FL 160 (fpm)

From FL max

to FL 310 (fpm)

RoD (fpm)


2000 3000 2500

0.82 310 3100.86 330 340




220Min. clean

speed (kts)

140Final

Approach

speed (kts)

Exits 8

9 of144


Approach


A-330-200

Not Available

Not Available

Not Available

ROMATSA


43/177

Passengers wide bodied transport aircraft, low wingmonoplan, all-weather operation, two jet engines,


Manufacturer

AIRBUS INDUSTRIES

Type ICAO

A333

WTC

H

APP Category C












Technical Data

Dimensions (m)

60.3Wing Span63.6Length

16.7Height

Weights (kg)

230000MTOW185000MLW

2800TORA (m)

1300LDA (m)

Engines L2J


CrewPassengers


410Absolute ceiling

410Service ceiling

350Optimum ceiling




level (M/kts)0.86to



0.86to



0.82 (M)


Below FL 160

(fpm)

From FL 310 to

FL 160 (fpm)

From FL max

to FL 310 (fpm)

RoD (fpm)


2000 3000 2500

0.82 310 3100.86 380 340




220Min. clean

speed (kts)

140Final

Approach

speed (kts)

Exits 8

10 of144


Approach


A-330-300

MTOW 75%

ROMATSA


44/177

Passengers widebodied transport aircraft, low wingmonoplan, all-weather operation, four jet engines,


Manufacturer

AIRBUS INDUSTRIES

Type ICAO

A342

WTC

H

APP Category C












Technical Data

Dimensions (m)


16.7Height

Weights (kg)

275000MTOW185000MLW

2800TORA (m)

1200LDA (m)

Engines L4J


CrewPassengers


410Absolute ceiling

410Service ceiling

350Optimum ceiling




level (M/kts)0.86to



0.86to



0.82 (M)


Below FL 160

(fpm)

From FL 310 to

FL 160 (fpm)

From FL max

to FL 310 (fpm)

RoD (fpm)


2000 3000 2000

0.82 300 3000.86 320 340




220Min. clean

speed (kts)

140Final

Approach

speed (kts)

Exits 8

11 of144


Approach


A-340-200

MTOW 75%

ROMATSA


45/177



Manufacturer

AIRBUS INDUSTRIES

Type ICAO

A343

WTC

H

APP Category C












Technical Data

Dimensions (m)


16.7Height

Weights (kg)

271000MTOW190000MLW

3000TORA (m)

1200LDA (m)

Engines L4J


CrewPassengers


410Absolute ceiling

410Service ceiling

350Optimum ceiling




level (M/kts)0.86to



0.86to



0.82 (M)


Below FL 160

(fpm)

From FL 310 to

FL 160 (fpm)

From FL max

to FL 310 (fpm)

RoD (fpm)


2000 3000 2000

0.82 300 3000.86 320 340




220Min. clean

speed (kts)

140Final

Approach

speed (kts)

Exits 8

12 of144


Approach


A-340-300

MTOW 75%

ROMATSA


46/177



Manufacturer

AIRBUS INDUSTRIES

Type ICAO

A345

WTC

H

APP Category C












Technical Data

Dimensions (m)


17.9Height

Weights (kg)

365000MTOW236000MLW

3000TORA (m)

2100LDA (m)

Engines L4J


CrewPassengers


410Absolute ceiling

410Service ceiling

350Optimum ceiling




level (M/kts)0.86to



0.86to



0.82 (M)


Below FL 160

(fpm)

From FL 310 to

FL 160 (fpm)

From FL max

to FL 310 (fpm)

RoD (fpm)


2000 3000 2000

0.82 300 3000.86 320 340




220Min. clean

speed (kts)

138Final

Approach

speed (kts)

Exits 8

13 of144


Approach


A-340-500

Not Available

Not Available

Not Available

ROMATSA


47/177



Manufacturer

AIRBUS INDUSTRIES

Type ICAO

A346

WTC

H

APP Category C












Technical Data

Dimensions (m)


17.9Height

Weights (kg)

365000MTOW254000MLW

3200TORA (m)

2300LDA (m)

Engines L4J


CrewPassengers


410Absolute ceiling

410Service ceiling

350Optimum ceiling




level (M/kts)0.86to



0.86to



0.82 (M)


Below FL 160

(fpm)

From FL 310 to

FL 160 (fpm)

From FL max

to FL 310 (fpm)

RoD (fpm)


2000 3000 2000

0.82 300 3000.86 320 340




220Min. clean

speed (kts)

145Final

Approach

speed (kts)

Exits 8

14 of144


Approach


A-340-600

Not Available

Not Available

Not Available

ROMATSA


48/177


49/177


underwing landing gear, regular tail low set.

Manufacturer

AIRBUS INDUSTRIES

Type ICAO

A382

WTC

H

APP Category D












Technical Data

Dimensions (m)


24.1Height

Weights (kg)

590000MTOW390000MLW

3350TORA (m)

2000LDA (m)

Engines L4J


CrewPassengers


430Absolute ceiling

430Service ceiling

370Optimum ceiling




level (M/kts)0.89to



0.89to



0.84 (M)


Below FL 160

(fpm)

From FL 310 to

FL 160 (fpm)

From FL max

to FL 310 (fpm)

RoD (fpm)


2000 3000 2000

0.85 310 3200.89 340 340




220Min. clean

speed (kts)

145Final

Approach

speed (kts)

Exits 16

16 of144


Approach


A-380-200

Not Available

Not Available

Not Available

ROMATSA


50/177

Passengers transport aircraft, low wing monoplan, all-weather operation, two turboprop engines, underwing

landing gear, regular tail low set.

Manufacturer

BRITISH AEROSPACE

Type ICAO

A748

WTC

M

APP Category B




N/A N/ARoC above FL 300 (fpm) to





N/AMach above FL 300 N/Ato Optimum Mach N/A



Technical Data

Dimensions (m)


7.57Height

Weights (kg)

21092MTOW19500MLW

1030TORA (m)

620LDA (m)

Engines L2T


CrewPassengers


250Absolute ceiling

250Service ceiling

220Optimum ceiling


200M/IAS optimum at optimum cruising level (M/kts)

200M/IAS at optimum cruising

level (M/kts)240to

200M/IAS at maximum


240to



N/A (M)


Below FL 160

(fpm)

From FL 310 to

FL 160 (fpm)

From FL max

to FL 310 (fpm)

RoD (fpm)


N/A 1000 1500

N/A 230 220N/A 230 240

242Maximum operating speed (kts/M) N/A/



140Min. clean

speed (kts)

120Final

Approach

speed (kts)

Exits 4

17 of144


Approach


BAe-748

MTOW 75%

ROMATSA


51/177

Passengers transport aircraft, high wing monoplan, all-weather operation, two turbo-prop engines, underfuselage

landing gear, T-tail.

Manufacturer

AEROSPATIALE/ALENIA

Type ICAO

AT43

WTC

M

APP Category B












Technical Data

Dimensions (m)


7.59Height

Weights (kg)

18600MTOW16700MLW

1090TORA (m)

970LDA (m)

Engines L2T


CrewPassengers


250Absolute ceiling

250Service ceiling

220Optimum ceiling




level (M/kts)225to

200M/IAS at maximum


220to



N/A (M)


Below FL 160

(fpm)

From FL 310 to

FL 160 (fpm)

From FL max

to FL 310 (fpm)

RoD (fpm)


N/A 2000 2000

N/A 220 240N/A 230 240




136Min. clean

speed (kts)

105Final

Approach

speed (kts)

Exits 4

18 of144


Approach


ATR-42-300

Not Available

Not Available

Not Available

ROMATSA


52/177


53/177

Passengers transport aircraft, high wing monoplan, all-weather operation, two turbo-prop engines, underfuselage

landing gear, T-tail.

Manufacturer

AEROSPATIALE/ALENIA

Type ICAO

AT72

WTC

M

APP Category B












Technical Data

Dimensions (m)


7.65Height

Weights (kg)

24500MTOW21350MLW

1408TORA (m)

1210LDA (m)

Engines L2T


CrewPassengers


250Absolute ceiling

250Service ceiling

220Optimum ceiling




level (M/kts)230to

220M/IAS at maximum


235to



N/A (M)


Below FL 160

(fpm)

From FL 310 to

FL 160 (fpm)

From FL max

to FL 310 (fpm)

RoD (fpm)


N/A 2000 1800

N/A 220 235N/A 230 240




150Min. clean

speed (kts)

120Final

Approach

speed (kts)

Exits 4

20 of144


Approach


ATR-72

MTOW 75%

ROMATSA


54/177


landing gear, normal tail low set.

Manufacturer

BRITISH AEROSPACE

Type ICAO

ATP

WTC

M

APP Category B












Technical Data

Dimensions (m)


7.59Height

Weights (kg)

22930MTOW22250MLW

1329TORA (m)

1128LDA (m)

Engines L2T


CrewPassengers


290Absolute ceiling

290Service ceiling

250Optimum ceiling




level (M/kts)230to

230M/IAS at maximum


240to



N/A (M)


Below FL 160

(fpm)

From FL 310 to

FL 160 (fpm)

From FL max

to FL 310 (fpm)

RoD (fpm)


N/A 2000 1500

N/A 220 240N/A 230 240




150Min. clean

speed (kts)

128Final

Approach

speed (kts)

Exits 6

21 of144


Approach


ATP JETSTREAM 61

MTOW 75%

ROMATSA


55/177


landing gear, T- tail.

Manufacturer

BEECHCRAFT

Type ICAO

B190

WTC

M

APP Category B












Technical Data

Dimensions (m)


4.72Height

Weights (kg)

7688MTOW7303MLW

1140TORA (m)

844LDA (m)

Engines L2T


CrewPassengers


330Absolute ceiling

330Service ceiling

290Optimum ceiling




level (M/kts)0.51to



0.51to



0.48 (M)


Below FL 160

(fpm)

From FL 310 to

FL 160 (fpm)

From FL max

to FL 310 (fpm)

RoD (fpm)


1000 1500 1000

0.49 220 2350.50 235 240




160Min. clean

speed (kts)

130Final

Approach

speed (kts)

Exits 4

22 of144


Approach


BEECH 1900 D

MTOW 75%

ROMATSA


56/177

Light passengers transport aircraft, low wing monoplan,all-weather operation, two turboprop engines, underwing

landing gear, normal tail low set.

Manufacturer

BEECHCRAFT

Type

Documents

Atlas Avioane de Linie