performante si caracteristici aeronave.pdf

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ROMATSA - DMTA PERFORMANTE !i CARACTERISTICI AERONAVE

DO ACH/ODF MAN000" ACFT "

CAPITOLUL I - Definitii I/21 DATA: septembrie 2001, editia 1.0 revizuita

PPEERRFFOORRMMAANNTTEE!!ii

CCAARRAACCTTEERRIISSTTIICCIIAAEERROONNAAVVEE

CCAATTAALLOOGGDDEEPPRREEZZEENNTTAARREE

VVOOLLUUMMUULL""

ROMATSA


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DATA: septembrie 2001, editia 1.0 revizuitaI

PERFORMANTE !iCARACTERISTICI AERONAVE

CATALOG DE PREZENTARE

VOLUMUL "


Edi!ia : 1.0 revizuita

Data edi!iei: 04.09.2001

Statut : Document aprobat

Clasificare : Document ROMATSA


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DATA: septembrie 2001, editia 1.0 revizuitaIII

Pagin& de semn&turi

Nivel Func'ie/nume Semn&tura Data

Aprobat Director General Marin VOICU

Director DMTA Dan ESTER

Director DMRT Mihai BRANISTE

Director DMRE Aurica COJOC

Avizat

Director DMSC Bogdan DONCIU

Verificat%ef Serviciu ACH Ioan DELIANIS

%ef Serviciu ODF Stefan CUCU

ElaboratExpert ACH Gheorghe MANEA

Referent ODF Radu CHIVU

Referent ODF Virginia COMAN

Referent ODF Elisabeta PLAMADEALA

Consultant ACH Vasile POPA


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DATA: septembrie 2001, editia 1.0 revizuitaIV

Fi!a de nregistrare a edi'iilor !i amendamentelor

Nr.Edi!ie

Nr.Amd.

Data Con!inut pe scurt Data #i semn$turade introducere

Paginiafectate

1.0 - Iulie 2001 Document aprobat toate

1.0revizuita

Septembrie2001

Document aprobat, editierevizuita

toate


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DATA: septembrie 2001, editia 1.0 revizuitaV

Lista paginilor efective

Cod document: DO ACH/ODF MAN0001 ACFT 1

Nr. Pag. Data

Nr.

Amendament Nr. Pag. Data

Nr.

Amendament


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Introducere 1/21 DATA: septembrie 2001, editia 1.0 revizuita

Introducere

Scopul lucrarii

Prezentul document sintetizeaza, ordoneaza #i prezinta, intr-un prim volum,

performantele #i 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 #i a sistemului FDP/RDP, pentrufluidizarea optima #i mentinerea sigurantei zborurilor.

Datele prezentate se vor regasi in sistemul IDS, care are la baza aplicatii dezvoltate deServiciul de Automatizari in Management din cadrul Administratiei Centrale ROMATSA.

Domeniul de aplicare

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

- analiza datelor existente;- consultarea urm$torilor 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 #i 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 utila de informatii pentru personalul operativ.

Referin'ePentru intocmirea acestui document, s-au folosit numeroase documente, publicatii #i

alte surse 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 #i caracteristici aeronave, sintetizeaza, ordoneaza #i prezintaperformantele #i 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 #i caracteristici ale acesteia. Macheta contine de asemenea, opoza color a aeronavei, schita acesteia #i graficul profilului de urcare.

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

de urcare pe verticala corespunzatoare pentru 75% din MTOW (Maximum Take Off 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.


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Referitor la graficul profilului de urcare, precizam de asemenea ca:- linia rosiereprezinta performantele de urcare in configuratie de scurt curier;- linia albastrareprezinta performantele de urcare in configuratie de lung curier;- linia verdereprezinta performantele de urcare in configuratie de mediu curier.Datele prezentate in graficul profilului de urcare sunt aproximative si se recomanda a fifolosite numai orientativ. Performantele propriu-zise ale unei aeronave la un moment dat pot

diferi considerabil, ele depinzand de greutatea si configuratia aeronavei, conditiilemeteorologice, politica operatorului aerian, etc.

In macheta care sintetizeaza principalele performante #i caracteristici ale fiecareiaeronave 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 #i minute)Weights (Kg): MTOW (Maximum Take Off Weight)

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

Length

HeightToD (Take-off distance)LD (Landing distance)Emergency 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 deSIWL (Single Wheel Load, valoare extrasa din Aicraft Operations Manual) #i 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)RoC at SL/OEI (fpm)Initial cruising altitude / FLIAS (Indicated Air Speed) up to FL 100 (kt)IAS FL 100 up to FL 200 (kt)IAS FL 200 up to FL 300 (kt)Mach number above FL 300

*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


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- Operational Data - Cruise

Absolute ceilingService ceilingOptimum ceilingService ceiling/OEIM/IAS optimum at optimum cruising level (M/kt)

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

- Operational Data Descent

RoD (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 (kt)Maximum speed for RoD below FL 160 (kt)Maximum rate of descent in emergency descent situation from FL max to safety level

- Operational Data for Approach

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

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 #i 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 #i a volumului 2al Catalogului de Prezentare a Performantelor #i Caracteristicilor Aeronavelor.

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


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Bibliografie 4/21 DATA: septembrie 2001, editia 1.0 revizuita

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)


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CAPITOLUL I - Definitii 7/21 DATA: septembrie 2001, editia 1.0 revizuita

Airsta ir

Retractable stairway built into aircraft.

ICAO App roach categories

The following ICAO table indicates the specified range of handling speeds (IAS) for eachcategory of aircraft to perform the manoeuvres specified. These speed ranges have beenassumed for use in calculating airspace and obstacle clearance requirements for eachprocedure.

Table ": ICAO Aircraft categories (speeds in kt)

MAX SPEEDS forMissed Approach

Aircraftcategory

Vat

Range ofSpeeds for

InitialApproach

Range ofFinal

ApproachSpeeds

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 no ise

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

Anhedra l

Downward slope of wing from root to tip.

An gle of attack *

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

Angle of inc idence

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

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


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Elevon

Wing trailing-edge control surface combining functions of aileron and elevators.

F

Factored

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

Fail op eratio nal

System which continues to function after any single fault has occurred.

Fai l safe

Structure or system which survives to a failure (in case of system may no longer functionnormally).

Far

Federal Aviation Regulation

Far Pt 23

Defines the airworthiness of private and air taxi aeroplanes of 5.670 Kg (12.500 lb.) MTOWand below.

Far Pt 25

Defines the airworthiness of public transport aeroplanes exceeding 5670 kg (12500 lb.)

MTOW.

Far f ie ld leng th

Defines the length measured on the runway necessary for take off and landing of theaircraft, at MTOW, S/L, ISA +15C, dry RWY, zero slope.

Take o ff fi eld len g th at S/L , ISA+15C

Defines the length, measured on the runway, from break release to 35 ft up in the airnecessary for take off of the aircraft.

Land in g f ield len g th at S/L , MLW , ISA+15C

Defines the length, measured on the runway, from 50 ft up in the air to full stop of theaircraft.

Feathering

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

Final Appro ach Speed

Typical speed for the final approach segment.


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Finesse

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

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 707 - 320 19.4

Douglas DC-8 17.9

Airbus A 320 17

Boeing 767- 200 19

Boeing 747-100 17.7

Douglas DC-10 17.7

Lockheed Tristar L1011 17.0Douglas DC-9 (1966) 16

Boeing 727-200 16.4

Fokker 50 (1966) 16.5

Flap

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

Flaperon

Wing trailing edge surface combining functions of flap and aileron.

Fl igh t crew m ember

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

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.

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

Flight recorder

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

Flight t ime

The 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.


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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.

Foreplanes

Pivoted canard surfaces forming part of the primary flight control system with authority in

pitch and possibly also in roll.See also canards.

Free turbin e

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

Fuel (capacity)

Maximum internal fuel capacity of the aircraft.

G

Glide s lope

Element giving vertical (height) guidance in ILS.

Green aircraf t

Aircraft flyable but unpainted, unfurnished and basically equipped;

Gunship

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

H

Hold ing procedure

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

Hold ing sp eedSpeed maintained by aircraft during holding procedure.

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


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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 (14000 ft) inclusive 425 km/h(2)

(230 kt)

315 km/h(4)

(170 kt)

520 km/h(3)

(280 kt)

315 km/h(4)

(170 kt)

above 4250 m to 6100 m (14000 ft to20000 ft) inclusive

445 km/h(5)

(240 kt)

above 6100 m to 10350 m (20000 ftto 34000 ft) inclusive

490 km/h(5)

(265 kt)

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

Above 10350 m (34000 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 (230kt), the holdingshould also be promulgated at this higher speed whenever possible.(3)The speed of 520 km/h (280kt) (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 kt) should be used for holding proceduresassociated with airway route structures.

Hovering cei l ing

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

I

Inert ia l n avigat ion

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

Instrument meteorological cond it ions (IMC)

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

Ins t rument approach and land ing o perat ions

Instrument approach and landing operations using instrument approach procedures areclassified as follows:

Non-prec is ion appro ach and land ing operations

An instrument approach and landing which does not utilise electronic glide pathguidance.


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Prec is ion approach and land ing operations

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

Categories o f precis ion app roach and landing o perat ions (JAR - OPS):

Categor y I (CAT I) op eration

A 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.

Categor y II (CATII) op eration

A 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.

Categor y III A (CAT III A) op eration

A precision instrument approach and landing with:a) decision height lower than 30 m (100 ft) or no decision height; andb) a runway visual range not less than 200m.

Categor y III B (CAT III B) op eration

A 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 75 m.

Categor y III C (CAT III C) op eratio n

A 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

Jo ined wing

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

L

Large aerop lane

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


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Load factor

Design factor (g limit) for airframe of the aircraft.

Lo ad Classif icat ion Num ber (LCN)

Defines the bearing strength of runway pavement.

Local iser

Element giving steering guidance in ILS.

Long -range / norm al cru is ing speed / Mach number

Typical speed range for normal cruise and long-range economical cruise in kt and machnumber. The comparison between kt and Mach number will vary in accordance with theaircrafts` altitude or flight level.

M

Max imum mass

Maximum certified take-off mass.

Maximum c ru is ing speed / Mach number

Typical 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.

Min imum clean sp eed

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

Min imum equipment l is t (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 more

restrictive than the MMEL (master minimum equipment list) established for the aircraft type.

Min imum descent a lt i tude (MDA) or min im um 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

Night

The hours between the end of evening civil twilight and the beginning of morning civil twilightor such other period between sunset or sunrise, as may be prescribed by the appropriateauthority.


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

O

Operat ional con tro l

The 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.

Operat ional f l ight plan

The operator`s 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.

Operat ional manual

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

Operator

A person, organisation or enterprise engaged in or offering to engage in an aircraftoperation.

Opt imum

The best that is possible.

Opt imum sp eed

The speed of an aircraft to obtain maximum range in minimum flight time with minimum fuelconsumption.

Opt imum level

A level of aircraft in normal operation to maintain optimum speed.

P

Payload

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

Plane

A lifting surface (for example wing, tailplane).

Pilot- in-commandThe pilot responsible for the operation and safety of the aircraft during flight time.


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Primary-f l ight con tro ls

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

Primary-f l ight disp lays

Single screen bearing all data for aircraft flight path control.

Profan

A 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-al t i tude

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

Port

Left side of the aircraft, looking forward.

Psychoact ive sub stances

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

R

Radar vector in gPerformance of navigational guidance to aircraft in the form of specific headings, based onthe use of radar.

Radius of act ion

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

Range

The distance an aircraft can fly with specified load and usually while making allowance for

specified additional manoeuvres (directions, stand off, go-around and so on).

Rate of cl im b

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

Rate of desc ent

Vertical distance flown by an aircraft in a unit of time, during descend, given in feet / minunder ISA conditions at maximum landing weight (MLW). These data depend on many

external influences and differ in daily operations.


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Redundant

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

Required navigat ion perform ance (RNP)

A statement of the navigation performance necessary for operation within a defined

airspace.

RNP type

A 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.

Runw ay visu al 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, ussualy a V-tail, that control both yaw and pitch attitude.

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.

Sensit ive alt imeter

Altitude indicator of mechanical type, having acute sensitivity.

Service cei l ing

Altitude at which an aircraft with normal rated load is unable to climb faster than 100 fpmunder ISA conditions.

Sidel ine nois e

EPNdB (Effective Perceived Noise, in decibel) measure of aircraft landing and taking off atpoint 0,25 NM (two or three engined) or 0,35 NM (four engined) from runway center line.

Sidest ick

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

Slat

Auxiliary 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.

Speci fic fue l consum pt ionRate at which fuel is consumed divided by power or thrust developed and thus a measure ofengine efficiency.


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State of reg istry

The state on whose register the aircraft is entered.

Stal ling speed

Airspeed at which aircraft stalls at 1g, that is wing lift suddenly collapses.

Standard Day

ISA temperature and pressure.

Starboard

Right side of the aircraft, looking forward.

Stealth

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

Stic k sh aker

Stall-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.

Tai lp lane

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

Transponder

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

Turbofan

Gas turbine jet engine generating most thrust by a large-diameter cowled fan, with small

part added by jet from core.

Turbojet

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

Turboprop

Gas turbine in which as such energy as possible it from gas jet and used to drive reductiongearbox and propeller.


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U

Unfactored

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

Usable fuel

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

Useful load

Usable fuel plus payload.

W

Wet Hous ing fuel

Wet wing often has extra connotations of integral tankage.

Wheelbase

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

Widebody

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

Wingle t

Small 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.


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CAPITOLUL II Performante si Caracteristici Aeronave 21/21 DATA: septembrie 2001, editia 1.0 revizuita

CAPITOLUL II - PERFORMANTE !iCARACTERISTICI 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

30B722 B727-200 BOEING


30/177


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

59BE9L BEECH 90 BEECHCRAFT

60C130 C-130 LOCKHEED


31/177


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 Skymaster 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

88DC10 DC-10 MCDONNELL DOUGLAS

89DC87 DOUGLAS DC-8-73 MCDONNELL DOUGLAS

90DH8A DASH8-100 DE HAVILLAND


32/177


33/177


121LJ25 LEAR JET 25 GATES LEARJET

122LJ28 LEARJET 28 GATES LEARJET






128MD11 MD-11 MCDONNELL DOUGLAS






134N262 N-262, Fregate 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 (kt) 340to Optimum IAS (kt) 300

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


0.76Mach above FL 300 0.84to Optimum Mach 0.80

310Initial cruising altitude/FL

Operational Data Climb

Technic al Data

Dimensions (m)

45Wing Span54Length

16Height

Weights (kg)

134000MTOW140000MLW

2400ToD (m)

1000LD (m)

Engines L2J

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

CrewPassengers

Operational Data Cruise

410Absolute ceiling (x100 ft)

410Service ceiling (x100 ft)

330Optimum ceiling (x100 ft)

140Service ceiling/OEI (x100 ft)

0.80M/IAS optimum at opt imum cru ising l evel (M/kt)

0.76M/IAS at optimum cruising

level (M/kt)0.84to

0.79M/IAS at maximum

certificated altitude (M/kt)

0.84to

460True Air Speed (kt)

280Turbulence Penetration Speed (kt)

0.79 (M)

Operational Data Descent

Below FL 160From FL 310 to

FL 160

From FL max

to FL 310

RoD (fpm)

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

2000 3000 2000

0.80 300 3000.84 320 340

340Maximum operating speed (kt/M) 0.84/

8000Max. rate of descent in "emergency

descent" (fpm)

230Min. clean

speed (kt)

130Final

Approach

speed (kt)

Emergency exits 6

1 of144

Operation al Data for

Approach

SIWL/LCN

A-300-600

MTOW 75%

ROMATSA

FL


35/177



Manufacturer

AIRBUS INDUSTRIES

Type ICAO

A30B

WTC

H

APP Category C












Technic al Data

Dimensions (m)

45Wing Span54Length

16Height

Weights (kg)

157000MTOW171700MLW

2200ToD (m)

1000LD (m)

Engines L2J

Fuel cap. (ltr)Range (NM) 3000

CrewPassengers








level (M/kt)0.84to



0.84to



0.79 (M)



FL 160

From FL max

to FL 310

RoD (fpm)


2000 3000 2000

0.80 300 3000.84 320 340



descent" (fpm)

230Min. clean

speed (kt)

130Final

Approach

speed (kt)

Emergency exits 6

2 of144


Approach

SIWL/LCN

A-300-B2/4

MTOW 75%

ROMATSA

FL


36/177


37/177



Manufacturer

AIRBUS INDUSTRIES

Type ICAO

A313

WTC

H

APP Category C












Technic al Data

Dimensions (m)

44Wing Span47Length

16Height

Weights (kg)

164000MTOW124000MLW

2400ToD (m)

900LD (m)

Engines L2J


CrewPassengers








level (M/kt)0.84to



0.84to



0.78 (M)



FL 160

From FL max

to FL 310

RoD (fpm)


2000 3000 2000

0.80 300 3000.84 320 340



descent" (fpm)

230Min. clean

speed (kt)

130Final

Approach

speed (kt)

Emergency exits 6

4 of144


Approach

SIWL/LCN

A-310-300

MTOW 75%

ROMATSA

FL


38/177



Manufacturer

AIRBUS INDUSTRIES

Type ICAO

A318

WTC

M

APP Category C












Technic al Data

Dimensions (m)

34Wing Span32Length

12.5Height

Weights (kg)

59000MTOW56000MLW

1700ToD (m)

1400LD (m)

Engines L2J


CrewPassengers








level (M/kt)0.82to



0.82to



0.78 (M)



FL 160

From FL max

to FL 310

RoD (fpm)


2000 3000 2500

0.79 300 3000.82 320 335



descent" (fpm)

220Min. clean

speed (kt)

130Final

Approach

speed (kt)

Emergency exits 6

5 of144


Approach

SIWL/LCN

A-318

Not Available

Not Available

Not Available

ROMATSA

FL


39/177



Manufacturer

AIRBUS INDUSTRIES

Type ICAO

A319

WTC

M

APP Category C












Technic al Data

Dimensions (m)

34Wing Span34Length

12.5Height

Weights (kg)

64000MTOW61000MLW

1800ToD (m)

1400LD (m)

Engines L2J


CrewPassengers








level (M/kt)0.82to



0.82to



0.78 (M)



FL 160

From FL max

to FL 310

RoD (fpm)


2000 3000 2500

0.79 300 3000.82 320 335



descent" (fpm)

220Min. clean

speed (kt)

130Final

Approach

speed (kt)

Emergency exits 6

6 of144


Approach

SIWL/LCN

A-319

MTOW 75%

ROMATSA

FL


40/177



Manufacturer

AIRBUS INDUSTRIES

Type ICAO

A320

WTC

M

APP Category C












Technic al Data

Dimensions (m)

34Wing Span38Length

12.5Height

Weights (kg)

73500MTOW64500MLW

1900ToD (m)

1400LD (m)

Engines L2J


CrewPassengers








level (M/kt)0.82to



0.82to



0.78 (M)



FL 160

From FL max

to FL 310

RoD (fpm)


2000 3000 2500

0.79 300 3000.82 320 335



descent" (fpm)

220Min. clean

speed (kt)

130Final

Approach

speed (kt)

Emergency exits 6

7 of144


Approach

SIWL/LCN

A-320

MTOW 75%

ROMATSA

FL


41/177



Manufacturer

AIRBUS INDUSTRIES

Type ICAO

A321

WTC

M

APP Category C












Technic al Data

Dimensions (m)

34Wing Span44.5Length

11.8Height

Weights (kg)

83000MTOW73500MLW

2400ToD (m)

1100LD (m)

Engines L2J


CrewPassengers








level (M/kt)0.82to



0.82to



0.78 (M)



FL 160

From FL max

to FL 310

RoD (fpm)


2000 3000 2500

0.79 300 3000.82 320 340



descent" (fpm)

220Min. clean

speed (kt)

140Final

Approach

speed (kt)

Emergency exits 8

8 of144


Approach

SIWL/LCN

A-321

MTOW 75%

ROMATSA

FL


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












Technic al Data

Dimensions (m)

60.3Wing Span58Length

17.9Height

Weights (kg)

230000MTOW180000MLW

2600ToD (m)

1200LD (m)

Engines L2J


CrewPassengers








level (M/kt)0.86to



0.86to



0.82 (M)



FL 160

From FL max

to FL 310

RoD (fpm)


2000 3000 2500

0.82 310 3100.86 330 340



descent" (fpm)

220Min. clean

speed (kt)

140Final

Approach

speed (kt)

Emergency exits 8

9 of144


Approach

SIWL/LCN

A-330-200

Not Available

ROMATSA

FL


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












Technic al Data

Dimensions (m)

60.3Wing Span63.6Length

16.7Height

Weights (kg)

230000MTOW185000MLW

2800ToD (m)

1300LD (m)

Engines L2J


CrewPassengers








level (M/kt)0.86to



0.86to



0.82 (M)



FL 160

From FL max

to FL 310

RoD (fpm)


2000 3000 2500

0.82 310 3100.86 380 340



descent" (fpm)

220Min. clean

speed (kt)

140Final

Approach

speed (kt)

Emergency exits 8

10 of144


Approach

SIWL/LCN

A-330-300

MTOW 75%

ROMATSA

FL


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












Technic al Data

Dimensions (m)


16.7Height

Weights (kg)

275000MTOW185000MLW

2800ToD (m)

1200LD (m)

Engines L4J


CrewPassengers








level (M/kt)0.86to



0.86to



0.82 (M)



FL 160

From FL max

to FL 310

RoD (fpm)


2000 3000 2000

0.82 300 3000.86 320 340



descent" (fpm)

220Min. clean

speed (kt)

140Final

Approach

speed (kt)

Emergency exits 8

11 of144


Approach

SIWL/LCN

A-340-200

MTOW 75%

ROMATSA

FL


45/177



Manufacturer

AIRBUS INDUSTRIES

Type ICAO

A343

WTC

H

APP Category C












Technic al Data

Dimensions (m)


16.7Height

Weights (kg)

271000MTOW190000MLW

3000ToD (m)

1200LD (m)

Engines L4J


CrewPassengers








level (M/kt)0.86to



0.86to



0.82 (M)



FL 160

From FL max

to FL 310

RoD (fpm)


2000 3000 2000

0.82 300 3000.86 320 340



descent" (fpm)

220Min. clean

speed (kt)

140Final

Approach

speed (kt)

Emergency exits 8

12 of144


Approach

SIWL/LCN

A-340-300

MTOW 75%

ROMATSA

FL


46/177



Manufacturer

AIRBUS INDUSTRIES

Type ICAO

A345

WTC

H

APP Category C












Technic al Data

Dimensions (m)


17.9Height

Weights (kg)

365000MTOW236000MLW

3000ToD (m)

2100LD (m)

Engines L4J


CrewPassengers








level (M/kt)0.86to



0.86to



0.82 (M)



FL 160

From FL max

to FL 310

RoD (fpm)


2000 3000 2000

0.82 300 3000.86 320 340



descent" (fpm)

220Min. clean

speed (kt)

138Final

Approach

speed (kt)

Emergency exits 8

13 of144


Approach

SIWL/LCN

A-340-500

Not Available

Not Available

Not Available

ROMATSA

FL


47/177



Manufacturer

AIRBUS INDUSTRIES

Type ICAO

A346

WTC

H

APP Category C












Technic al Data

Dimensions (m)


17.9Height

Weights (kg)

365000MTOW254000MLW

3200ToD (m)

2300LD (m)

Engines L4J


CrewPassengers








level (M/kt)0.86to



0.86to



0.82 (M)



FL 160

From FL max

to FL 310

RoD (fpm)


2000 3000 2000

0.82 300 3000.86 320 340



descent" (fpm)

220Min. clean

speed (kt)

145Final

Approach

speed (kt)

Emergency exits 8

14 of144


Approach

SIWL/LCN

A-340-600

Not Available

Not Available

Not Available

ROMATSA

FL


48/177


underwing landing gear, regular tail low set.

Manufacturer

AIRBUS INDUSTRIES

Type ICAO

A381

WTC

H

APP Category D












Technic al Data

Dimensions (m)


24.1Height

Weights (kg)

560000MTOW383000MLW

3350ToD (m)

2000LD (m)

Engines L4J


CrewPassengers








level (M/kt)0.89to



0.89to



0.84 (M)



FL 160

From FL max

to FL 310

RoD (fpm)


2000 3000 2000

0.85 310 3200.89 330 340



descent" (fpm)

220Min. clean

speed (kt)

145Final

Approach

speed (kt)

Emergency exits 16

15 of144


Approach

SIWL/LCN

A-380-100

Not Available

Not Available

Not Available

ROMATSA

FL


49/177


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



Technic al Data

Dimensions (m)


7.57Height

Weights (kg)

21092MTOW19500MLW

1030ToD (m)

620LD (m)

Engines L2T


CrewPassengers






200M/IAS optimum at opt imum cru ising l evel (M/kt)

200M/IAS at optimum cruising

level (M/kt)240to

200M/IAS at maximum


240to



N/A (M)



FL 160

From FL max

to FL 310

RoD (fpm)


N/A 1000 1500

N/A 230 220N/A 230 240

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


descent" (fpm)

140Min. clean

speed (kt)

120Final

Approach

speed (kt)

Emergency exits 4

17 of144


Approach

SIWL/LCN

BAe-748

MTOW 75%

ROMATSA

FL


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












Technic al Data

Dimensions (m)


7.59Height

Weights (kg)

18600MTOW16700MLW

1090ToD (m)

970LD (m)

Engines L2T


CrewPassengers








level (M/kt)225to

200M/IAS at maximum


220to



N/A (M)



FL 160

From FL max

to FL 310

RoD (fpm)


N/A 2000 2000

N/A 220 240N/A 230 240



descent" (fpm)

136Min. clean

speed (kt)

105Final

Approach

speed (kt)

Emergency exits 4

18 of144


Approach

SIWL/LCN

ATR-42-300

MTOW 75%

ROMATSA

FL


52/177



Manufacturer

AEROSPATIALE/ALENIA

Type ICAO

AT45

WTC

M

APP Category B












Technic al Data

Dimensions (m)


7.59Height

Weights (kg)

18600MTOW16700MLW

1475ToD (m)

1095LD (m)

Engines L2T


CrewPassengers








level (M/kt)230to

200M/IAS at maximum


220to



N/A (M)



FL 160

From FL max

to FL 310

RoD (fpm)


N/A 2200 2000

N/A 220 240N/A 240 240



descent" (fpm)

140Min. clean

speed (kt)

106Final

Approach

speed (kt)

Emergency exits 4

19 of144


Approach

SIWL/LCN

ATR-42-500

Not Available

Not Available

Not Available

ROMATSA

FL


53/177



Manufacturer

AEROSPATIALE/ALENIA

Type ICAO

AT72

WTC

M

APP Category B












Technic al Data

Dimensions (m)


7.65Height

Weights (kg)

24500MTOW21350MLW

1408ToD (m)

1210LD (m)

Engines L2T


CrewPassengers








level (M/kt)230to

220M/IAS at maximum


235to



N/A (M)



FL 160

From FL max

to FL 310

RoD (fpm)


N/A 2000 1800

N/A 220 235N/A 230 240



descent" (fpm)

150Min. clean

speed (kt)

120Final

Approach

speed (kt)

Emergency exits 4

20 of144


Approach

SIWL/LCN

ATR-72

MTOW 75%

ROMATSA

FL


54/177

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

landing gear, normal tail low set.

Manufacturer

BRITISH AEROSPACE

Type ICAO

ATP

WTC

M

APP Category B












Technic al Data

Dimensions (m)


7.59Height

Weights (kg)

22930MTOW22250MLW

1329ToD (m)

1128LD (m)

Engines L2T


CrewPassengers








level (M/kt)230to

230M/IAS at maximum


240to



N/A (M)



FL 160

From FL max

to FL 310

RoD (fpm)


N/A 2000 1500

N/A 220 240N/A 230 240



descent" (fpm)

150Min. clean

speed (kt)

128Final

Approach

speed (kt)

Emergency exits 6

21 of144


Approach

SIWL/LCN

ATP JETSTREAM 61

MTOW 75%

ROMATSA

FL


55/177


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 ICAO

B350

WTC

L

APP Category B












Technic al Data

Dimensions (m)


4.37Height

Weights (kg)

6804MTOW6800MLW

421ToD (m)

408LD (m)

Engines L2T


CrewPassengers








level (M/kt)240to

205M/IAS at maximum


240to



0.46 (M)



FL 160

From FL max

to FL 310

RoD (fpm)


2000 2000 1500

220 230 240225 240 250



descent" (fpm)

150Min. clean

speed (kt)

125Final

Approach

speed (kt)

Emergency exits 2

23 of144


Approach

SIWL/LCN

BEECH Super King Air 350

MTOW 75%

ROMATSA

FL


57/177

Passengers transport aircraft, high wing monoplan, all-weather operation, four jet engines, underfuseage landing

gear, T-tail.

Manufacturer

BRITISH AEROSPACE

Type ICAO

B461

WTC

M

APP Category B





N/ARoC at SL/OEI (fpm)







Technic al Data

Dimensions (m)


8.61Height

Weights (kg)

43091MTOW37875MLW

1466ToD (m)

1173LD (m)

Engines L4J


CrewPassengers





Service ceiling/OEI (x100 ft)



level (M/kt)0.73to



0.73to



0.64 (M)



FL 160

From FL max

to FL 310

RoD (fpm)


2000 2500 2000

0.70 280 3000.73 300 300



descent" (fpm)

210Min. clean

speed (kt)

130Final

Approach

speed (kt)

Emergency exits 4

24 of144


Approach

SIWL/LCN

BAe-146-100

MTOW 75%

ROMATSA

FL


58/177


gear, T-tail.

Manufacturer

BRITISH AEROSPACE

Type ICAO

B462

WTC

M

APP Category B












Technic al Data

Dimensions (m)


8.59Height

Weights (kg)

43998MTOW38555MLW

1655ToD (m)

1189LD (m)

Engines L4J


CrewPassengers





Service ceiling/OEI (x100 ft)



level (M/kt)0.73to



0.73to



0.64 (M)



FL 160

From FL max

to FL 310

RoD (fpm)


2000 2500 2000

0.70 280 3000.73 300 300



descent" (fpm)

210Min. clean

speed (kt)

130Final

Approach

speed (kt)

Emergency exits 4

25 of144


Approach

SIWL/LCN

BAe-146-200

MTOW 75%

ROMATSA

FL


59/177


gear, T-tail.

Manufacturer

BRITISH AEROSPACE

Type ICAO

B463

WTC

M

APP Category C












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