Civil Helicopter Handbook 07-08

8/13/2019 Civil Helicopter Handbook 07-08

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HANDBOOK

SHEPHARD

S HE PHARD


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Civil Helic pter handbook 2007-08 3 I ro uc io Buy a helic pter, hug trees and save the w rld, says the edit r.

4 Hea hy iscor F recasters agree that the pr spects f r the civil helic pter market are

g d, but n t ab ut exactly h w g d.

7 He icop er speci ca io s Technical speci cati n data f r the w rlds maj r civil helic pters currently

in pr ducti n. This new-l k secti n n w includes a ph t f each aircraft.

Pu isher Sandy D yle [email protected] i or Peter D nalds n [email protected] es a Marke i Ma a er Jane Smith [email protected]

AdVERtISIng SAlES

+44 (0)1753 727004

group Marke i Ma a er Ben Dibble [email protected] ook direc ories a Up a es M han Sadasivan [email protected]

A ver isi Coor i a or Sandra M re [email protected]

Chief Execu iveAlexander Shephard

Pu ishi direc or Andrew Drwiega

SInglE COPY PRICES UK 60Europe 90A o her cou ries US $110

ORdER OnlInEwww.shephar .co.uk

te : +44 (0)1858 438879Fax: +44 (0)1858 461739


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Peter d l s IntROdUCtIOn

WElCOME

Helic pter PoRTFoLIo

While a sl gan suchas save the planet:buy a helic ptermight be stretching the truth

just a bit, helic pters arefully paid up, lentil-eating

tree-huggers in their re- ghting and f rest managementr les f r a start. Trees, it seems h ld the key t staving ffgl bal warming and the resultant c nversi n f ur benignEarthly climate int a lead-melting, acid-raining Venusianh rr r. That is if y u accept the new rth d xy which tellsus that carb n di xide emissi ns fr m human activi ties areheating up the w rld.

Trees st re carbn, h ld s il n steep slpes, slw waterws dwn thus helping t prevent ds, pump water int

the atmsphere and generate xygen. S cutting them dwnwithut replacing them is bad enugh, but setting re t themis much wrse because it releases all that lcked up carbn.

Alth ugh aviati n unfairly takes a l t f heat in thegl bal warming debate, we cant escape the fact thathelic pters have relatively large carb n f tprints when

c mpared with ther vehicles. They burn a l t f f ssil fueland release large am unts f carb n di xide int theatm sphere as a result. Gl bally, h wever, def restati n is amassive s urce f atm spheric carb n di xide that dwarfsaviati ns small but publicly lambasted c ntributi n.Def restati n is resp nsible f r 18% f man-made carb ndi xide emissi ns c mpared with aviati ns meagre 1.7%.

Accrding t a recent article in the UKs Guardiannewspaper, hardly an ap lgist f r aviatin, if trpicalrainfrest in Brazil, Cng and Indnesia cntinues t be

destryed at the current rate f r the next ve years, it willput as much carbn dixide int the atmsphere as everyight in the hist ry f aviatin up t 20 years hence, rs mething like that...

Wrldwide, we are lsing frest at a rate f 15 millinhectares per year, prducing mre carbn emissins than

any single cuntry, even China which recently vert k theUS as the wrlds biggest carbn emitter.While it is nly p litical and ec n mic p licy that can halt

and reverse the l ss f S uth American, Asian and Africanrainf rests, helic pters can play their part in m nit ringand rest rati n, as well as c mbating the damage wr ughtby the wildland res that represent an increasing menaceall ar und the w rld.

Helicpters are als indispensable t ls in general f restmanagement and cmmnly serve t re-seed areas damagedby re r cleared by lgging. Besides tree seeds, th se fgrasses and ther vegetatin alng with fertilizer andprtective misture retaining mulch can be spread efcientlyand quickly by helicpter. Re-frestatin may becme a largemarket f r helicpters in the near future if Chinas rst

natinal plan n climate change cmes t fruitin: it includesan aim t cver 20% f the cuntrys land with frest.Its als 21 years since helic pters played a central r le in

extinguishing what, with ut them, may have turned intne f the m st danger us res the m dern w rld has everseen: the react r re at the Chern byl nuclear p werplantnear Kiev, Ukraine. Maybe that sl gan is justi able after all.

Pe er do a so , E i orp @shephar .co.uk

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PUBLICATIoNS RoToRHUB MAGAZINEThe business magazine f r the civil r t rcraft industry. Sixissues per year.

ANNUAL HANDBooKS Public Service Aviati n, Mili tary Helic pter, Civil Helic pter

oNLINE RoToRHUB.CoM www.rt ru .cm DIRECToRIES www.shephard.c .uk/ irect ry EVENTS www.shephard.c .uk/ evets

EVENTS PoLICE AVIATIoN 2007 7-8 NoVEMBER 2007Amsterdam, Netherlands www.shephard.c .uk/ p lice

SAR 2008 18-20 MARCH 2008B urnem uth, UK www.shephard.c .uk/ s r

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CoNTACTThe Shephard Press, 268 Bath Rad, Slugh, SL1 4DX, UK

Tel: +44 (0)1753 727001 Fax: +44 (0)1753 727002


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Civi He icop er Handb k 2007-084

VIEW M r et f rec st

visit us at www.r t rhub.cm 5

M r et f rec st VIEW

Rather like l ng-range weather f recasting,predicting h w many new helic pters will bedelivered t civil cust mers up t a decade r sahead is n t an exact science. S thsayers in chief f r thehelic pter industry are rival engine manufacturers R lls-R yce and H neywell, b th f wh m naturally have a m rethan passing interest in the health and vitality f a marketsect r that by R lls estimate c uld be w rth $3.6 billi n inengine sales and $16.2 billi n in engine supp rt businessver the next 10 years. Their numbers are in fairly widedisagreement. R lls predicts 6,095 deliveries ver the2007 t 2016 peri d, whereas H neywell says gl baldemand c uld exceed 8,000 ver the 2007 t 2017 peri d.That difference f m re than 1,900 helic pters greatlyexceeds the margin y u w uld expect fr m the extra 12m nths in the H neywell f recast peri d.

R lls-R yces and H neywells f recasts sh w upwardtrends f r the next ve years, but the actual numbers differsigni cantly by 440 helic pters. Admittedly my meth df c mparis n was crude; I measured R lls graph c lumnswith a ruler and came t a number f 3,060 aircraft f r the2007 t 2011 peri d c mpared with H neywells declarednumber f 3,500, but still, 440 helic pters is a l t and al ng way utside likely measurement err rs, even using a

ruler n A4 paper. Assuming Im particularly cr ss-eyedand my measurement is ut by 1 mm, that w uld put me

just ver 16 helic pters ut, n t 440. Hwever, the f recastexcludes deliveries f ex-military aircraft t civil cust mers,but includes new deliveries t the paramilitary market.

A dECAdE OF StAbIlItYR lls civil f recast p ints t stability ver a 10-year peri d,the best years being between 09 and 15 and the spreadbetween the j int thinnest years (08 and 16) and thefattest year (13) being 213 aircraft; 491 playing 704 (R llssays 689 is the peak, but that difference f 15 aircraft iswithin my cr ss-eyed err r all wance f 1 mm n the graph,alth ugh the press release puts the peak in 2016 ratherthan 2013 where it is n the graph.)

Sc tt Crislip, President, Helic pter and Small Gas TurbineEngines f r R lls-R yce, said that the f recast stabilityre ects the l ng-term health f the civil helic pter market,with anticipated new pr duct intr ducti n t wards the endf the decade b lstered by str ng near-term paramilitarydemand fr m law enf rcement agencies. The market isrec gnizing the increasing value and utility f the helic pterin a variety f different r les. R lls-R yce is well-p siti nedin these high value areas with engines in service with m stf the leading airframers and is the leading pr vider fpr pulsi n systems and services f r these high-value light,medium and heavy-lift helic pters. The civil market, he saidwill be d minated by single-engine helic pters, acc untingf r 41% f deliveries, and light twins with 40%.

R lls f recast is based n cust mer new requirementand eet replacement plans, oEM f recasts andcust mer input. H neywells relies n purchaseexpectati ns expressed by nearly 1,000 ightdepartments in N rth America, Latin America,Eur pe, Asia , the Middle East and Africa what theysaid they expected t buy and why.

Theres pr bably m re light t be shed n thesituati n by c mparing f recasts fr m adjacentperi ds fr m the same c mpany rather than tryingt fath m the differences between the appr aches fdifferent rganizati ns. F r H neywell, this yields afairly spectacular 40% increase fr m ne t the nextwhen c mparing its 2002 t 2006 f recast with its2007 t 2011 eff rt. Furtherm re, it is pr bably m reuseful t characterise the f rces driving the marketand the directi ns that gr wth is set t take ratherthan getting t picky with the numbers.

R lls cites a gr wing ffsh re il supp rt market driven by

increasing il prices, expl rati n activity and pr ducti n asb sting demand f r heavy twins such as the S-92 andEC225. P lice and HEMS sales are predicted t be str ng asthe internati nal market expands, while c rp rate salesexpand as ight departments turn t the larger twins.

H neywell Aer spaces 2007 survey has identi edavi nics capabilities, perf rmance and p wer, and directperating c sts as the t p criteria perat rs c nsider whenselecting new helic pters, said Vicki Panhuise, Vice-President, H neywell C mmercial and Military Helic pters,H neywell Defense and Space.

The decisi n t acquire new helic pters is drivenprimarily by the age f current aircraft which is usuallyre ected in an perat rs desire f r better techn l gy,m re range, m re p wer and l wer perating c sts. Survey

results have impr ved f ur years running, and oEMs rep rtstr ng sales activity supp rting ur view that helic pterdemand has great l ng range pr spects in a gr wing gl balecnmy.

The 2007 utl k pr jects annual turbine helic pterdelivery levels exceeding 700 units in the near term, withsurvey based indicati ns that latent demand c uld driverates even higher if capacity limits are n t enc untered,Panhuise said. The impr ved 2007 utl k is als b stedby p tential new oEM entrants ffering aff rdable highvalue platf rms stimulating demand and drawing newperat rs int the turbine segment.

AnOtHER RObInSOn gAME CHAngER?That p tential new oEM entrant is, f c urse, R bins nHelic pters, which has l ng talked f building an entry-levelturbine-p wered helic pter if a suitable p werplant c uldbe f und. Well, ne has. The engine is a l w-c st derivativef the 250 series kn wn as the R lls-R yce 300, designedf r a 2,000 h ur TBo t match the airframe, a R bins nstandard. It will p wer R bins ns new ve-seat R66, which,if its success in the market is f the same rder achievedby the R22 and m re recently the R44 families c uld pr vet be a game changer.

on the subject f game changers, R lls f recast includesthe Bell Agusta Aerspace BA609 tiltr tr r, the rst tw

years pr ducti n f which have s ld ut. Sik rskys c axialX2 techn l gy has been delayed, but ffers an alternativeapprach t high-speed r t rcraft. Hwever, if technicalmerit rather than p litics were the engine f r t rcraftprgress these days, my mney wuld be n GrenBr thers Aviati n and their revival f the gyr dyne c nceptas the way f rward with the best rati f bene t t c st andrisk. As things stand, the Salt Lake City based c mpany hasa m untain t climb in the face f establishmentindifference, but its techn l gies might represent a real wildcard in the r t rcraft market, c nverting high-wing airlinersint high-speed VToL aircraft.

HEAltHY dISCORdby Peter d l sForecasters agree that the prospects for thecivil helicopter market are good, but not aboutexactly how good.

The AgustaWestland AW139 has sold very well in the

growing offshore oil and gas support market.

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SPECIFICaTIonS HELICoPTERS

This secti n lists XXX C mpany name Address Teleph ne and fax numbers

Email addresses Website urls C ntact names C mpany activity

xxx

While every eff rt has been made tpr vide accurate inf rmati n, thepublishers cann t be held resp nsiblef r err rs r missi ns. If y u have anyc mments, additi ns r c rrecti ns y uw uld like t be made please c ntactthe edit r.

7 hELICoPTERSPECIFICaTIonS

33 MAnUFACtURERSbROKERSASSOCIAtIOnS

43 Eha handbook

49 oPERaToRS

91 oPERaToRSaCTIVITIES

105 SUPPLIERS

151 PRodUCT GUIdE

R bins n remains as market leader with increasingsales, b sted by fav rable d llar exchange rates. Avgasfuelled engines d minate market, but the high price andthreatened availability f this fuel is expected t f stermarket f r aff rdable turbines, says R lls, predicting littleimpact fr m diesel engines in the sh rt term, pr bably duet high prices and weight.

H neywell f und purchase expectati ns measured n

the basis f speci c new helic pter buying plans up byeight per cent in 2007 ver 2006 levels. Plans t replacelder aircraft and add extra machines t the eet wereup by ve per cent, alth ugh that is d minated by aircraftin the same size, capability and price class as the existingeet, with nly 11 t 12% f perat rs planningt trade up.

Single engine helic pters d minate in the US at 70% fplanned purchases, and, f r the sec nd year in a r w, havemade a c meback in Eur pe despite regulati ns mandatingtwins ver built up areas, rising t 47% f stated purchaseexpectati ns, acc rding t H neywell.

tHE REgIOnAl OUtlOOKon a ge graphical basis, N rth America d minates,acc unting f r 42% f all planned purchases fnew helic pters. Eur pe acc unts f r ar und 16%, afairly m dest gure f r such a rich regi n, but nethat l ks m re p sitive when y u take int acc untthe increase in the eet replacement and expansi nrate fr m 15% in the 06 survey t ar und 20% inthe 2007 eff rt.

Asia, Paci c, Africa and the Middle East acc unt f r

22% f expected sales and dminate in the renewalstakes as peratrs in these regins tgether expectt buy new aircraft equivalent t between 36 and 37percent f their current eets ver the next ve years.It is n t a unifrm picture f grwth, hwever, aspurchase plans in Latin America drpped by abut10% since its recrd high in the 2006 survey.

In terms f helic pter size categ ry, H neywellcarves the market int light singles, light twins,intermediate twins and heavy lift aircraft. While lightsingles d minate purchase plans at 51%, there is n ta straightf rward relati nship between size andnumbers as intermediate twins c me next with 29%f ll wed by light twins at 16% and heavy liftersrec vering t f ur r ve percent fr m a l w f tw

r s last year.In line with a generally strng glbal ecnmy,

crp rate use is the peratinal categ ry thatdminates new purchase plans at 26%, f llwedby law enfrcement at 19% (dwn substantially frm25% in 06 but d minating N rth American sh ppinglists). EMS is up slightly frm 14 t 16% f wrld

demand, while utility is up substantially frm 11% last yeart 18% in 2007.

EUROPEAn dEMAndUtility demand is particularly strng in Eurpe, accuntingfr 36% f future purchase plans, accrding t Hneywell.Demand fr new aircraft f r il and gas supprt has almstdubled t 14% f the t tal, dminated by peratrs in

Africa and the Middle East.H neywell als tracks usage rates and rep rts that

survey resp ndents l gged between 400 and 550 h ursver the 12 m nths pri r t the survey, representing amderate recvery.

With m st oEMs, acc rding t R lls, rep rtingincreases in sales with s me pr ducti n lines being s ldut ver the next 18-24 m nths, the strength f the gl balec n my and maj r indicat rs such as used aircraftretirements oEM pr tability c ntinuing t l k p sitive,the verall picture is fairly rsy, even if the numbers can betricky t pin dwn.


SPECIFICaTIonS HELICoPTERS

This secti n lists r t rcraft currently in pr ducti n r under devel pment inalphabetical rder (by manufacturer name). It includes ai rcraft built by theriginal manufacturers; licence-built machines, such as Agusta-built Bell designs,f r example, are excluded t save space.

The data includes basic parameters t describe a helic pters capacity andperf rmance. Manufacturers and their agents are happy t supply m re detailedinf rmati n n request. The maximum and cruise speeds and the H ver InGr und Effect (HIGE) and H ver out f Gr und Effect (HoGE) gures assumeInternati nal Standard Atm sphere (ISA) c nditi ns at maximum gr ss weightunless therwise stated.The maximum gr ss weight is the highest weight at which the aircraft ispermitted t y by regulat ry auth rities. Engine ratings are f r take- ff p wer.The gures in the useful l ad secti n are derived by subtracting the emptyweight fr m the maximum gr ss weight s all wance must be made f r fuel andcrew in assessing the payl ad capacity.

While every eff rt has been made tpr vide accurate inf rmati n, thepublishers cann t be held resp nsiblef r err rs r missi ns. If y u have anyc mments, additi ns r c rrecti ns y uw uld like t be made please c ntactthe edit r.

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Engine power (shp)


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SPECIFICAtIOnS helic pters

8 9visit us at www.r t rhub.c m

helic pters SPECIFICAtIOnS

AgUStAWEStlAnd A109 POWERRo or iame er: 36 ft 1 in (11 m)Fuse a e e h: 37 ft 6.78 in (11.45 m) Overae h: 42 ft 9.18 in (13.035 m) r t rs turning Powerp a : 2 x 640 shp (477kW) P&W PW 206C r 670 shp Turb meca Arrius 2K1 Emp y wei h : 3,461 lb(1,570 kg) Max ake-off wei h : 6,284 lb (2,850 kg) Usefu oa : 2,822 lb(1,280 kg) Ca i e h: 6.9 ft (2.1 m) Ca i wi h: 5 ft 3.38 in (1.61 m) Ca ihei h : 4.2 ft (1.28 m) Max sea i : 8 HIgE: 16,600 ft (5,060 m) HOgE: 11,800ft (3,600 m) Max cruise: 156 kt (289 kph) Eco omic cruise: 137 kt (254 kph)Ra e: 521 nm (965 km), Std tanks, n reserve

AgUStAWEStlAnd A109S gRAndRo or iame er: 35 ft 6 in (10.83 m) Fuse a e e h: 38 ft 3 in (11.65 m)Overa e h: 42 ft 6 in (12.96 m) Powerp a : 2 x 735 shp (548 kW) Pratt &Whitney Canada PW207C turb shafts Emp y wei h : 3,649 lb (1,655 kg) Maxake-off wei h : 7,000 lb (3,175 kg) Usefu oa : 3,351 lb (1,520 kg) Ca ie h: 6 ft 3.5 in (1.9 m) Ca i wi h: N/A Ca i hei h : 4 ft 2 in (1.48 m) Maxsea i : 8 HIgE: 14,270 ft (4,350 m) HOgE: 9,350 ft (2,850 m) Max cruise: 155 kt (287 kph) Eco omic cruise: N/A Ra e: 470 nm (870 km)

AgUStAWEStlAnd AW 139Ro or iame er: 45.28 ft (13.8 m) Fuse a e e h: 44.4 ft (13.53 m) Overae h: 54.64 ft (16.65 m) r t rs turning Powerp a : 2 x 1,679 shp (1,252 kW)P&W PT6C-67C Emp y wei h : 7,227 lb (3,300 kg) Max ake-off wei h : 13,227lb (6,000 kg) Usefu oa : 6,000 lb (2,700 kg) Ca i e h: 8.86 ft (2.7 m)Ca i wi h: 6.56 ft (2 m) Ca i hei h : 4.66 ft (1.42 m) Max sea i : 17HIgE: N/A HOgE: 12,000 ft (3,600 m) Max cruise: N/A Eco omic cruise: N/ARa e: 400 nm (750 km), Std tanks, n reserve


AgUStAWEStlAnd A119 KOAlARo or iame er: 36 ft 1 in (10.83 m) Fuse a e e h: 36 ft 3.98 in (11.074 m)Overa e h: 42 ft 9.18 in (13.035 m) r t rs turning Powerp a : 1 x 1,002 shp(747 kW) P&W PT6B-37 Emp y wei h : 3,086 lb (1,400 kg) Max ake-offwei h : 5,732 lb (2,600 kg), 5,997 lb (2,720 kg) with ext l ad Usefu oa :2,845 lb (1,290 kg) 2,911 lb (1,320 kg) with ext l ad Ca i e h: 6.9 ft (2.1 m)Ca i wi h: 5.5 ft (1.59 m) Ca i hei h : 4 ft 2.39 in (1.28 m) Max sea i : 8HIgE: 11,000 ft (3,350 m) HOgE: 8,800 ft (2,680 m) Max cruise: 140 kt (260kph) Eco omic cruise: 115 kt (210 kph) Ra e: 330 nm (610 km), Std tanks, nreserve

AgUStAWEStlAnd EH 101Ro or iame er: 61 ft (18.6 m) Fuse a e e h: 64 ft (19.5 m) Overa e h: 74 ft 10 in (22.8 m) Powerp a : 3 x 2,100 shp (1,554 kW) RR Turb meca RTM322 r 2,000 shp (1,480 kW) GE CT7-6 Emp y wei h : 19,048 lb (8,640 kg)Max ake-off wei h : 32,188 lb (14,600 kg) Usefu oa : 13,140 lb (5,960 kg)Ca i e h: 21 ft 4 in (6.5 m) Ca i wi h: 8 ft 2 in (2.49 m) Ca i hei h : 6ft 2 in (1.88 m) Max sea i : 34 HIgE: 8,000 ft (2,438 m) HOgE: 4,000 ft(1,220 m) Max cruise: 150 kt (278 kph) Eco omic cruise: 140 kt (259 kph)Ra e: 500 nm (926 km)

AMERICAn SPORtSCOPtER Intl UltRASPORt 254Ro or iame er: 21 ft (6.4 m) Fuse a e e h: 17 ft 8 in (5.38 m) blades f ldedOvera e h: 19 ft 2 in (5.84 m) Powerp a : 1 x 55 hp (41 kW) Hirth 2703 rpti nal 65 hp (48 kW) Hirth 3202V tw -str ke engine Emp y wei h : 252 lb(115 kg)Max ake-off wei h : 525 lb (239 kg) Usefu oa : 273 lb (124 kg) Ca ie h: 52 in (1.32 m) Ca i wi h: 30 in (76.2 cm) Ca i hei h : 59 in (1.5 m)Max sea i : 1HIgE: 10,800 ft (3,292 m) HOgE: 7,000 ft (2,134 m) Max cruise: 63 mph (101 kph) Eco omic cruise: 63 mph (105 kph) (FAA restricti n) Ra e: N/A (1.25 hrs endurance)

AMERICAn SPORtSCOPtER Intl UltRASPORt 496Ro or iame er: 23 ft (7.01 m) Fuse a e e h: 17 ft 8 in (5.38 m) bladesf lded Overa e h: 19 ft 9 in (6.020 m) Powerp a : 1 x 95 hp (70.3 kW)Hirth F30 tw -str ke Emp y wei h : 495 lb (225 kgs) Max ake-off wei h : 1085 lb (493 kg) Usefu oa : 590 lb (268 kg) Ca i e h: 53 in (1.346 m)Ca i wi h: 48 in (1.22 m) Ca i hei h : 59 in (1.5 m) Max sea i : 2 HIgE: 10,800 ft (3,292 m) HOgE: 7,000 ft (2,134 m) Max cruise: 98 mph (158 kph)Eco omic cruise: 65 mph (104.6 kph) Ra e: N/A (2.5 hrs endurance)


AMERICAn SPORtSCOPtER Intl UltRASPORt 331Ro or iame er: 21 ft (6.4 m) Fuse a e e h: 17 ft 8 in (5.38 m) blades f ldedOvera e h: 19 ft 2 in (5.84 m) Powerp a : 1 x 65 hp (48 kW) Hirth 706tw -str ke Emp y wei h : 330 lb (150 kg) Max ake-off wei h : 650 lb (295kg) Usefu oa : 320 lb (145 kg) Ca i e h: 52 in (1.32 m) Ca i wi h: 30 in(76.2 cm) Ca i hei h : 59 in (1.5 m) Max sea i : 1HIgE: 10,800 ft (3,292 m)HOgE: 7,000 ft (2,134 m) Max cruise: 104 mph (167 kph) Eco omic cruise: 65mph (105 kph) Ra e: 150 sm (250 km) 2.5 hrs endurance


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10

bEll 206 bIII JEtRAngERRo or iame er: 33 ft 5 in (10.16 m) Fuse a e e h: 31 ft 2.4 in (9.5 m)Overa e h: 38 ft 11.4 in (11.82 m) Powerp a : 1 x 420 shp (313 kW) Allis n250-C20J turb shaft Emp y wei h : 1,678 lb (761 kg) Max ake-off wei h : 3,200 lb (1,451 kg) Usefu oa : 1,522 lb (690kg) Ca i e h: 7 ft (2.13 m)Ca i wi h: 4 ft 2 in (1.28 m) Ca i hei h : 4 ft 2.5 in (1.28 m) Max sea i : 5HIgE: 12,800 ft (3,900 m) HOgE: 8,800 ft (2,682 m) Max cruise: 114.5 kt (212kph) Eco omic cruise: 114.5 kt (212 kph) Ra e: 365 nm (676 km) n reserve

bEll 206 l4 lOngRAngERRo or iame er: 37 ft (11.28 m) Fuse a e e h: 33 ft 2.4 in (10.1 m) Overae h: 42 ft 10.2 in (13.02 m) Powerp a : 1 x 557 shp (415 kW) Allis n 250-C30P turb shaft Emp y wei h : 2,307 lb (1,046 kg) Max ake-off wei h : 4,450 lb (2,018.5 kg) Usefu oa : 2,143 lb (972 kg) Ca i e h: 9 ft (2.74 m)Ca i wi h: 4 ft 2 in (1.28 m) Ca i hei h : 4 ft 2.5 in (1.28 m) Max sea i : 7HIgE: 10,000 ft (3,048 m) HOgE: 6,500 ft (1,981 m) Max cruise: 110 kt (204kph) Eco omic cruise: 110 kt (204 kph) Ra e: 321 nm (594 km) n reserve

bEll 212Ro or iame er: 48 ft (14.6 m) Fuse a e e h: 41 ft 8.1 in (12.7 m) Overae h: 57 ft 3.25 in (17.45 m) Powerp a : 1 x 1,290 shp (961 kW) Pratt &Whitney Canada PT6T 3P Twin Pac Emp y wei h : 6,176 lb (2,801 kg) Maxake-off wei h : 11,200 lb (5,080 kg) Usefu oa : 5,024 lb (2,279kg) Ca ie h: 7 ft 8 in (2.34 m) Ca i wi h: 8 ft (2.43 m) Ca i hei h : 4 ft 1 in (1.24m) Max sea i : 15HIgE: 4,750 ft (1,448 m) HOgE: 8,400 ft (2,560 m) at10,000 lb (4,545 kg) Max cruise: 111 kt (206 kph) Eco omic cruise: 104 kt (193kph) Ra e: 224 nm (415 km) n reserve


bEll 210Ro or iame er: 48 ft (14.6 m) Fuse a e e h: 41 ft 8.1 in (12.7 m) Overae h: 57 ft 3.25 in (17.45 m) Powerp a : 1 x 1,800 Shp H neywell T-53-517Bturb shaft Emp y wei h : 5,210 lb (2,363 kg) Max ake-off wei h : 10,500 lb(4,763 kg) internal, 11,200 lb (5,080 kg) external Usefu oa : 5,034 lb (2,284kg) internal, 5,000 lb (2,268 kg) external Ca i e h: 7 ft 8 in (2.34 m) Ca iwi h: 8 ft (2.43 m) Ca i hei h : 4 ft 1 in (1.24 m) Max sea i : 15HIgE: 15,012 ft (4,576 m) estimated HOgE: N/A Max cruise: 110 kt (204 kph) Ra e: 251 nm (465 km)

Pratt & Whitney Canadas depth ofexperience is leading to productinnovations that are making enginescleaner and greener, as demonstratedby the PW210, a new-generation engine

with the highest power-to-weight ratioand lowest fuel burn for single-engineand intermediate to medium twin-enginehelicopters in the 1,000 shp class.The Eagle is everywhere.

www.pwc.ca

Mary H. Kalogiannis, B.Eng.Senior Staff SpecialistTurboshaft Performance


8/18Civi He icop er Handb k 2007-08




bEll 407Ro or iame er: 35 ft (10.7 m) Fuse a e e h: 33 ft 2.4 in (10.1 m) Overae h: 41.8 ft (12.7 m) Powerp a : 1 x 791 shp (589 kW) Allis n 250-C47turb shaft Emp y wei h : 2,598 lb (1,178 kg) Max ake-off wei h : 5,000 lb(2,267 kg) Usefu oa : 2,402 lb (1,090 kg) Ca i e h: 9 ft (2.74 m) Ca iwi h: 4 ft 9 in (1.738 m) Ca i hei h : 4 ft 2.5 in (1.28 m) Max sea i : 7HIgE: 12,200 ft (3,719 m) HOgE: 10,400 ft (3,170 m) Max cruise: 128 kt (237kph) Eco omic cruise: 115 kt (213 kph) Ra e: 312 nm (578 km)

bEll 412 HPRo or iame er: 46 ft (14 m) Fuse a e e h: 46 ft (14 m) Overa e h: 56ft 2 in (17.1 m) Powerp a : 1 x 1,800 shp (1,341 kW) Pratt & Whitney CanadaPT6T 3P Twin Pac Emp y wei h : 6,789 lb (3,079 kg) Max ake-off wei h : 11,900 lb (5,398 kg) Usefu oa : 5,111 lb (2,318 kg)Ca i e h: 7 ft 8 in (2.34m) exc c ckpit Ca i wi h: 8 ft (2.43 m) Ca i hei h : 4 ft 1 in (1.24 m) Maxsea i : 15 HIgE: 10,200 ft (3,109 m) HOgE: 5,200 ft (1,585 m) Max cruise: 122 kt (226 kph) Eco omic cruise: 122 kt (226 kph) Ra e: 352 nm (652 km)

bEll 429Ro or iame er: 42.3 ft (12.9 m) appr x Fuse a e e h: 39.9 ft (12.17 m)Overa e h: 53.4 ft (16.28 m) r t rs turning, appr x Powerp a : 2 x 710shp (528 kW) Pratt & Whitney Canada PW 207D turb shafts (5 minute take- ffrating) Emp y wei h : 4,300 lb (1,950 kg) Max ake-off wei h : 7,000 lb (3,175kg) Usefu oa : 2,700 lb (1,225 kg) Max sea i : 10 HIgE: 12,000 ft (3,658 m)HOgE: 9,300 ft (2,835 m) Max cruise: 142 kt (264 kph) Ra e: 350 nm (648km) E ura ce: 3.8 hr


bEll 427Ro or iame er: 37 ft (11.3 m) Fuse a e e h: 37.9 ft (11.55 m) Overa e h: 42.9 ft (13.06 m) Powerp a : 2 x 710 shp (528 kW) Pratt & Whitney Canada PW207D turb shafts (5 minute take- ff rating) Emp y wei h : 3,485 lb (1,581 kg)Max ake-off wei h : 6,000 lb (2,722 kg) Usefu oa : 2,515 lb (1,141 kg)Ca ie h: 5.2 ft (1.57 m) at r level Ca i wi h: 4 ft in (1.23 m) just ab ve rlevel Ca i hei h : 4.2 ft (1.3 m) Max sea i : 8 HIgE: 16,200 ft (4,938 m)HOgE: 13,900 ft (4,237 m) Max cruise: 136 kt (252 kph) Eco omic cruise: 126kt (233.5 kph) Ra e: 353 nm (654 km)

bEll 430Ro or iame er: 42 ft (12.8 m) Fuse a e e h: 44.1 ft (13.4 m) Overa e h: 50.5 ft (15.39 m) Powerp a : 2 x 770 shp (573 kW) Allis n 250-C40turb shafts Emp y wei h : 5,285 lb (2,397 kg) Max ake-off wei h : 9,000 lb(4,082 kg) Usefu oa : 3,715 lb (1,685 kg) Ca i e h: 8 ft 6 in (2.59 m)Ca i wi h: 4 ft 11 in (1.5 m) Ca i hei h : 4 ft 9.6 in (1.45 m) Max sea i : 9HIgE: 11,350 ft (3,459 m) HOgE: 8,750 ft (2,667m) Max cruise: 135 kt 250 kphEco omic cruise: 128 kt (237 kph) Ra e: 351 nm (650 km)

bEll AgUStA 609 tIlt ROtORRo or iame er: 26 ft (7.9 m) each, 60 ft (18.3 m) span Fuse a e e h: 44 ft(13.31 m)Overa e h: 44 ft (13.31 m) Powerp a : 2 x 1,940 shp (1,447 kW)Pratt & Whitney Canada PT6C-67A turb shafts Emp y wei h : 10,500 lb (4,763kg) Max ake-off wei h : 16,000 lb (7,258 kg) Usefu oa : 5,500 lb (2,495 kg)Ca i e h: 12.8 ft (3.84 m) (9 seats) Ca i wi h: 58.5 in (1.48 m) (2 seats)Ca i hei h : 56 in (1.42 m) Max sea i : 9 HIgE: 25,000 ft (7,620 m) HOgE: 25,000 ft (7,620 m) Max cruise: 275 kts (509.63 kph) Eco omic cruise: 250kts (464 kph) Ra e: 750 nm (1,390 km)

EnStROM 480bRo or iame er: 32 ft (9.8 m) Fuse a e e h: 29 ft 10 in (9.1 m) Overae h: 37 ft 4.3 in (11.39 m) Powerp a : 1 x 420 shp Allis n 250-C20Wturb shaft derated t 305 shp (227 kW) f r take- ff and 277 shp (206 kW)c ntinu us Emp y wei h : 769 kg Max ake-off wei h : 1,361 kgUsefu oa :592 kg Ca i e h: 7.3 ft (2.2 m) Ca i wi h: 5.87 ft (1.79 m) Ca i hei h : 4.25 ft (1.3 m) Max sea i : 5 HIgE: 12,300 ft (3,750 m) HOgE: 5,400 ft (1,645m) Max cruise: 202 km/h at MToW Eco omic cruise: N/A Ra e: 657 km at3,000 ft, n reserves


bRAntlY IntERnAtIOnAl InC b2bRo or iame er: 23 ft 9 in (7.24 m) Fuse a e e h: 21 ft 1 in (6.43 m) Overae h: 28 ft (8.53 m) Powerp a : 1 x 180 hp (133 kW) Textr n Lyc ming IVo360 AIA fuel injected pist n engine Emp y wei h : 1,070 lb (481 Kg) Max ake-off wei h : 1,670 lb (757 kg) Usefu oa : 600 lb (272 kg) Ca i e h: 6 ft(1.83 m) Ca i wi h: 3 ft 11 in (1.19 m)Ca i hei h : 3 ft 3 in (0.99 m) Maxsea i : 2 HIgE: 3,525 ft (1,074 m) HOgE: N/A Max cruise: 78 kt (145 kph)@75% p wer Eco omic cruise: N/A (max level spd 87 kt, 161 kph @ SL) Ra e: 174 nm (322 km)



EnStROM F 280 FXRo or iame er: 32 ft (9.8 m) Fuse a e e h: 28.7 ft (8.7 m) Overa e h: 37 ft (11.28 m) Powerp a : 1 x 225 hp (168 kW) Lyc ming HIo-360-F1ADturb charged pist n engine Emp y wei h : 1,670 lb (757 kg) with standardequipment Max ake-off wei h : 2,600 lb (1,179 kg) Usefu oa : 930 lb (422kg) Ca i e h: 5.6 in (1.7 m) Ca i wi h: 4 ft 11 in (1.498 m) Ca i hei h : 4ft (1.2 m) Max sea i : 2 HIgE: 13,200 ft (4,023 m) @ 2,350 lb HOgE: 8,700 ft(2,651 m) @ 2,350 lb Max cruise: 101 kt (188 kph) 117 mph Eco omic cruise: 93kt (172 kph) 107 mph Ra e: 260 nm (483 km) 300 sm n reserve

EnStROM F28F FAlCOnRo or iame er: 32 ft (9.8 m) Fuse a e e h: 28.1 ft (8.6 m) Overa e h: 37 ft (11.28 m) Powerp a : 1 x 225 hp (168 kW) Lyc ming HIo-360-F1ADturb charged pist n engine Emp y wei h : 1,640 lb (744 kg) with standardequipment Max ake-off wei h : 2,600 lb (1,179 kg) Usefu oa : 960 lb (435kg) Ca i e h: 5.4 ft (1.7 m) Ca i wi h: 5 ft 1 in (1.55 m) Ca i hei h : 4 .2ft (1.3 m) Max sea i : 2 HIgE: 13,200 ft (4,023 m) @ 2,350 lb HOgE: 8,700 ft(2,651 m) @ 2,350 lb Max cruise: 97 kt (180 kph) 112 mph Eco omic cruise: 89kt (165 kph) 102 mph Ra e: 240 nm (423 km) 263 sm n reserve

EUROCOPtER AS 332 l1 SUPER PUMARo or iame er: 51.12 ft (15.58 m) Fuse a e e h: 53.44 ft (16.29 m) Overae h: 61.35 ft (18.7 m) Powerp a : 2 x 1,820 shp (1,357 kW) Turb mecaMakila 1A1 turb shafts Emp y wei h : 9,832 lb (4,460 kg) Max ake-offwei h : 18,960 lb (8,600 kg) Usefu oa : 9,128 lb (4,140 kg) Ca i e h: 16.44 ft (5.01 m) at r Ca i wi h: 5.9 ft (1.8 m) Ca i hei h : 5.09 ft (1.55m) Max sea i : 22 HIgE: 10,663 ft (3,250 m) HOgE: 7,546 ft (2,300 m) Maxcruise: 144 kt (267 kph) Eco omic cruise: 138 kt (256 kph) Ra e: 655 nm(1,215 km) with std tanks, centre tank + sp ns n tanks


ERICKSOn (SIKORSKY) S-64E/F AIRCRAnERo or iame er: 72 ft (21.95 m) Fuse a e e h: 70 ft 3 in (21.41 m) Overae h: 88 ft 6 in (26.97 m) Powerp a : 2 x 4,500 shp (3,356 kW) Pratt &Whitney JTFD12-4A (S-64E) r 4,800 shp (3,579 kW) JTFD12-5A (S-64F)turb shafts Emp y wei h : 19,234 lb (8,724 kg) Max ake-off wei h : 42,000lb (19,050 kg) (S-64E) r 47,000 lb (21319 kg) (S-64F) Usefu oa : 20,000 lb(9,072 kg) (S-64E) r 25,000 lb (11,340 kg) (S-64F), max external Ca i e h: N cabin aft f c ckpit but pr visi n t t c ntainer p d r re ghting tankand re ll pump system. Ca i wi h: N/A Ca i hei h : N/A Max sea i : 0HIgE: 10,600 ft (3,230 m) (S-64E) Service cei i : 9,000 ft (2,475 m) HOgE: 6,900 ft (2,103 m) (S-64E) Max cruise: 104 kt (193 kph) Eco omic cruise: N/A

Ra e: 230 sm (370 km) with 10% reserve E ura ce: 2 hrs 45 mins (n reserve) (S-64F)

EUROCOPtER AS 332 l2 SUPER PUMA 2Ro or iame er: 53.15 ft (16.2 m) Fuse a e e h: 55 ft (16.79 m) Overae h: 63.98 ft (19.5 m) Powerp a : 2 x 1,845 shp (1,375.5 kW) Turb mecaMakila 1A2 turb shafts Emp y wei h : 10,330 lb (4,686 kg) Max ake-offwei h : 20,500 lb (9,300 kg) Usefu oa : 10,173 lb (4,614 kg) Ca i e h: 18.67 ft (5.69 m) at r Ca i wi h: 5.91 ft (1.8 m) Ca i hei h : 4.76 ft (1.45m) Max sea i : 27 HIgE: 10,236 ft (3,126 m) HOgE: 6,430 ft (1,960 m) Maxcruise: 150 kt (278 kph) Eco omic cruise: 136 kt (251 kph) Ra e: 655 nm(1,215 km) with std tanks, centre tank + sp ns n tanks

EUROCOPtER AS 350 b2Ro or iame er: 35 ft 0.8 in (10.69 m) Fuse a e e h: 35.85 ft (10.93 m)Overa e h: 42.45 ft (12.94 m) Powerp a : 1 x 732 shp (546 kW)Turb meca Arriel 1D1 Emp y wei h : 2,581 lb (1,171 kg)Max ake-off wei h : 4,960 lb (2,250 kg), 5,511 lb (2,500 kg) with external l ad Usefu oa : 2,379 lb(1,079 kg) Ca i e h: 7.94 ft (2.42 m) at r Ca i wi h: 5 ft 4.9 (1.65 m)Ca i hei h : 4.27 ft (1.3 m) Max sea i : 7 HIgE: 9,843 ft (3,000 m) HOgE: 7,546 ft (2,300 m) Max cruise: 133 kt (246 kph) Eco omic cruise: 122 kt (226kph) Ra e: 362 nm (670 km)


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10/18




18

EUROCOPtER bO 105 CbRo or iame er: 32.28 ft (9.84 m) Fuse a e e h: 28.08 ft (8.56 m) Overae h: 38.91 ft (11.86 m) Powerp a : 2 x 420 shp (313 kW) Allis n 250-C20Bturb shafts Emp y wei h : 2,813 lb (1,276 kg) Max ake-off wei h : 5,511 lb(2,500 kg) Usefu oa : 2,698 lb (1,224 kg) Ca i e h: 7.17 ft (2.185 m) Ca iwi h: 4.27 ft (1.3 m) Ca i hei h : 3.84 ft (1.17 m) Max sea i : 6 HIgE: 5,000ft (1,524 m) HOgE: 1,500 ft (457 m) Max cruise: 130 kt (240 kph) Eco omiccruise: 111 kt (205 kph) Ra e: 300 nm (555 km)

EUROCOPtER bO 105 CbS SUPER FIVERo or iame er: 32.28 ft (9.84 m) Fuse a e e h: 28.9 ft (8.81 m) Overae h: 38.91 ft (11.86 m) Powerp a : 2 x 420 shp (313 kW) Allis n 250-C20Bturb shafts Emp y wei h : 2,910 lb (1,320 kg) Max ake-off wei h : 5,512 lb(2500 kg) Usefu oa : 2,564 lb (1,163 kg) Ca i e h: 7.99 ft (2.435 m) Ca iwi h: 4.27 ft (1.3 m) Ca i hei h : 3.84 ft (1.17 m) Max sea i : 6 HIgE: 7,800ft (2,378 m) HOgE: 5,397 ft (1,645 m) Max cruise: 131 kt (243 kph) Eco omiccruise: 111 kt (205 kph) Ra e: 305 nm (564 km)

EUROCOPtER EC 120 bRo or iame er: 32.81 ft (10 m) Fuse a e e h: 31.5 ft (9.6 m) Overa e h: 37.86 ft (11.52 m) Powerp a : 1 x 504 shp (376 kW) Turb meca Arrius 2Fturb shaft Emp y wei h : 1,929 lb (875 kg) Max ake-off wei h : 3,750 lb(1,700 kg) Usefu oa : 1,655 lb (750 kg) Ca i e h: 7.55 ft (2.3 m) Ca iwi h: 4.43 ft (1.35 m) Ca i hei h : 4.10 ft (1.25 m) Max sea i : 5 HIgE: 10,499 ft (3,200 m) HOgE: 7,999 ft (2,438 m) Max cruise: 124 kt (230 kph)Eco omic cruise: 110 kt (204 kph) Ra e: 395 nm (732 km)


EUROCOPtER bO 105 lS A-3Ro or iame er: 32.28 ft (9.84 m) Fuse a e e h: 28.9 ft (8.81 m) Overae h: 38.91 ft (11.86 m) Powerp a : 2 x 500 shp (373 kW) Allis n 250-C28Bturb shafts Emp y wei h : 2,910 lb (1,320 kg) Max ake-off wei h : 5,732 lb(2,600 kg) Usefu oa : 3,248 lb (1,280 kg) Ca i e h: 7.99 ft (2.435 m)Ca i wi h: 4.27 ft (1.3 m) Ca i hei h : 3.84 ft (1.17 m) Max sea i : 6 HIgE: 11,483 ft (3,500 m) HOgE: 8,366 ft (2,550 m) Max cruise: 129 kt (239 kph)Eco omic cruise: 111 kt (205 kph) Ra e: 278 nm (515 km)

I y Sikorsky.

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everyone gets to y a Sikorsky helicopter.

But everyone wants to.

Sikorsky.






EUROCOPtER EC 130Ro or iame er: 35.07 ft (10.69 m) Fuse a e e h: 35.03 ft (10.68 m) Overae h: 41.47 ft (12.64 m) Powerp a : 1 x 847 shp (632 kW) Turb meca Arriel2B1 turb shaft Emp y wei h : 2,998 lb (1,360 kg) Max ake-off wei h : 5,291lb (2,400 kg) Usefu oa : 2,293 lb (1,040 kg) Ca i e h: 7.185 ft (2.19 m)Ca i wi h: 6.12 ft (1.865 m) Ca i hei h : 3.85 ft (1.175 m) Max sea i : 8HIgE: 10,720 ft (3,265 ft) HOgE: 8,740 ft (2,660 m) Max cruise: 127 kt (235kph) Eco omic cruise: N/A Ra e: 358 nm (662 km) t dry tanks at fast cruisespeed

EUROCOPtER EC 135 P1Ro or iame er: 33.46 ft (10.2 m) Fuse a e e h: 33.33 ft (10.16 m) Overae h: 39.7 ft (12.1 m) Powerp a : 2 x 621shp (463 kW) Pratt & WhitneyCanada PW 206Bs Emp y wei h : 3,174 lb (1,440 kg) Max ake-off wei h : 6,000 lb (2,720 kg) Usefu oa : 2,734 lb (1,240 kg) Ca i e h: 10.04 ft (3.06m) at r Ca i wi h: 4.91ft (1.496 m) Ca i hei h : 4.22 ft (1.285 m) Maxsea i : 8 HIgE: 14,599 ft (4,450 m) HOgE: 11,401 ft (3,600 m) Max cruise: 139 kt (257 kph) Eco omic cruise: 134 kt (249 kph) Ra e: 362 nm (670 km)

EUROCOPtER EC 145Ro or iame er: 36.08 ft (11 m) Fuse a e e h: 33.43 ft (10.19 m) Overae h: 42.74 ft (13.03 m) Powerp a : 2 x 750 shp (550 kW) Turb meca Arriel1E2 turb shafts Emp y wei h : 1,742 kg Max ake-off wei h : 3,550 kg Usefuoa : 1,728 kg Ca i e h: 3,44 m, excluding c ckpit Ca i wi h: 1.57 mmax, 1.40 m in rear Ca i hei h : 1.27 m max, 0.99 m in rear Max sea i : 12HIgE: 2,130 m HOgE: 10,000 ft (3,048 m) at 7,500 lb (3,400 kg) in ISA Maxcruise: 245 kph Eco omic cruise: 243 kph Ra e: 670 km


EUROCOPtER EC 135 t1Ro or iame er: 33.46 ft (10.2 m) Fuse a e e h: 33.33 ft (10.16 m) Overae h: 39.7 ft (12.1 m) Powerp a : 2 x 732 shp (546 kW) Turb meca Arrius 2B1Emp y wei h : 3,148 lb (1,428 kg) Max ake-off wei h : 6,000 lb (2,720 kg)Usefu oa : 2,767 lb (1,255 kg) Ca i e h: 10.04 ft (3.06 m) at r Ca iwi h: 4.91 ft in (1.496 m) Ca i hei h : 4.22 ft (1.285 m) Max sea i : 8 HIgE: 14,205 ft (4,330 m) HOgE: 12,139 ft (3,475 m) Max cruise: 139 kt (257 kph)Eco omic cruise: 134 kt (249 kph) Ra e: 356 nm (660 km)

EUROCOPtER EC 155Ro or iame er: 41.34 ft (12.6 m) Fuse a e e h: 41.76 ft (12.73 m) Overae h: 46.91 ft (14.30 m) Powerp a : 2 x 851 shp (635 kW) Turb meca Arriel2C1 turb shafts Emp y wei h : N/A Max ake-off wei h : 10,582 lb (4,800 kg)Usefu oa : 4,887 lb (2,217 kg) including missi n fuel Ca i e h: 8.2 ft (2.5m) Ca i wi h: F ur seats Ca i hei h : 5.18 ft (1.58 m) Max sea i : 14HIgE: N/A HOgE: N/A Max cruise: 143 kt (266 kph) Eco omic cruise: 136 kt(252 kph) Ra e: 450 nm (831 km) with std tanks

EUROCOPtER EC 225Ro or iame er: 53.14 ft (16.2 m) Fuse a e e h: 55 ft (16.79 m) Overae h: 63.98 ft (19.5 m) Powerp a : 2 x 2,413 shp (1,800 kW) Turb mecaMakila 1A4 turb shafts Emp y wei h : N/A Max ake-off wei h : 22,930 lb(10,400 kg) with internal l ad, 24,700 lb (11,200 kg) with external l ad Usefuoa : 11,870 lb (5,380 kg) with internal l ad Ca i e h: 18.67 ft (5.69 m) atr Ca i wi h: 5.91 ft (1.8 m) Ca i hei h : 4.76 ft (1.45 m) Max sea i : 27

HIgE: N/A HOgE: N/A Max cruise: 156 kts Eco omic cruise: N/A Ra e: 783nm

gROEn bROtHERS AVIAtIOn HAWK 5 gYROPlAnERo or iame er: 42 ft (12.8 m) Fuse a e e h: 24 ft (7.32 m) Overa e h: NA Powerp a : 1 x 420 shp R lls-R yce 250 C20S turb pr p Emp y wei h : N/A Max ake-off wei h : 3,500 lb (1,588 kg) Usefu oa : 1,525 lb (692 kg)Ca i e h: 6.25 ft (1.9 m) Hawk 4 Ca i wi h: 4.5 ft (1.37 m) Hawk 4 Ca ihei h : 6.78 ft (2.07 m) Max sea i : 5 HIgE: Cann t h ver Service cei i : 16,000 ft (4,877 m) HOgE: Cann t h ver Max cruise: 140 kt (256 kph) VNEEco omic cruise: 122 kt (223 kph) Ra e: 508 sm (818 km) n reserveE ura ce: 5 hrs (n reserve)


EUROMIl MI-38Ro or iame er: 69 ft 2.75 in (21.1 m) Fuse a e e h: 65 ft 5.5 in (19.95 m)Overa e h: 82 ft 8 in (25.2 m) r t rs turning Powerp a : 2 x 2,500 shp(1,863 kW) Klim v TVA-3000 r Pratt & Whitney Canada PW-127 TS turb shaftsEmp y wei h : 18,518 lb (8400 kg) Max ake-off wei h : 34,392 lb (15,600 kg)Usefu oa : 15,873 lb (7,200 kg) Ca i e h: 35 ft 1.25 in (10.7 m) Ca iwi h: 7 ft 8 in (2.34 m) Max sea i : 0 HIgE: N/A HOgE: 8,203 ft (2,500 m)Max cruise: 148 kt (275 kph) Eco omic cruise: 135 kt (250 kph) Ra e: 701 nm(1,300 km)






HAl AdVAnCEd lIgHt HElICOPtERRo or iame er: 43 ft 3.7 in (13.2 m) Fuse a e e h: 42 ft 3 in (12.89 m)Overa e h: 52 ft (15.87 m) Powerp a : 2 x 1,000 shp (746 kW) Turb mecaTM-333 2B turb shafts r 2 x 1,200 shp (895 kW) LHTEC CTS 800 turb shaftsEmp y wei h : 6,172.9 lb (2,800 kg) Max ake-off wei h : 12,125.3 lb (5,500kg) Usefu oa : 5,952.4 lb (2,700 kg) Ca i e h: 10 ft 11.9 in (3.35 m) Ca iwi h: 6 ft 5.5 in (1.968 m) Ca i hei h : 4 ft 8 in (1.42 m) Max sea i : 14HIgE: 9,850 ft (3,000 m) HOgE: N/A Max cruise: 157 kt (290 kph) Eco omiccruise: 132 kt (245 kph) Ra e: 432 nm (800 km) with 20 min reserve

HAl CHEEtAHRo or iame er: 36.2 ft (11.02 m) Fuse a e e h: 33.62 ft (10.236 m) Overae h: 42.4 ft (12.92 m) Powerp a : 1 x 870 shp (649 kW) HAL-builtTurb meca Art uste IIIB turb shaft Emp y wei h : 2,425 lb (1,100 kg) Maxake-off wei h : 4,300 lb (1,950 kg) Usefu oa : 1,870 lb (850 kg) Ca ie h: 6.43 ft (1.96 m) Ca i wi h: 4.36 ft (1.33 m) Ca i hei h : 4.36 ft (1.33m) Max sea i : 5 HIgE: 16,565 ft (5,050 m) HOgE: 15,100 ft (4,600 m) Maxcruise: 113 kt (209 kph) Eco omic cruise: 103 kt (192 kph) at sea level Ra e: 302.3 nm (560 km)

KAMAn K-1200 K-MAXRo or iame er: 48 ft 4 in (14.68 m) Fuse a e e h: 41 ft 9 in (12.72 m)Overa e h: 52 ft (15.85 m) Powerp a : 1 x derated 1,800 shp (1,343 kW)AlliedSignal Lyc ming T53-17A-1 Emp y wei h : 5,100 lb (2,491 kg) Max ake-off wei h : 6,500 lb (2,949 kg) with ut external l ad, 12,000 lb (5,862 kg) withexternal l ad Usefu oa : 6,000 lb (2,722 kg) Ca i e h: 5 ft (1.52 m) Ca iwi h: 3.17 ft (0.97 m) Ca i hei h : 4.17 ft (1.27 m) Max sea i : 1HIgE: 29,120 ft (8,876 m) at max gr ss weight HOgE: 26,300 ft (8,016 m) at maxgr ss weight Max cruise: 100 kt (185.2 kph) Eco omic cruise: 85 kt (157 kph)Ra e: 270 nm (500 km)


HAl CHEtAKRo or iame er: 36 ft 1.75 in (11.02 m) Fuse a e e h: 33 ft 4.5 in (10.17 m)Overa e h: 42 ft 1.5 in (12.84 m) Powerp a : 1 x 870 shp (649 kW) HAL-built Turb meca Art uste IIIB turb shaft Emp y wei h : 2,711 lb (1,230 kg) Maxake-off wei h : 4,850 lb (2,200 kg) Usefu oa : 2,134 lb (970 kg) Ca ie h: 5 ft 11.64 in (1.82 m) Ca i wi h: 6 ft 1.2 in (1.86 m) Ca i hei h : 4.36ft (1.33 m) Max sea i : 7 HIgE: 9,350 ft (2,850 m) HOgE: 4,920 ft (1,500 m)Max cruise: 113 kt (209 kph) Eco omic cruise: 100 kt (185 kph) at sea levelRa e: 270 nm (500 km)

KAMOV KA 126Ro or iame er: 42.65 ft (13 m) Fuse a e e h: 25.5 ft (7.775 m) Overae h: 42.65 ft (13m) Powerp a : 1 x 720 shp (530 kW) Mars TV-o-100turb shaft Emp y wei h : 4,222 lb (1,915 kg) Max ake-off wei h : 7,165 lb(3,250 kg) Usefu oa : 2,943 lb (1,335 kg) Ca i e h: 6.69 ft (2.04 m) Ca iwi h: 4.1 ft (1.25 m) Ca i hei h : 4.5 ft (1.40 m) Max sea i : 10 HIgE: 3,182ft (970 m) HOgE: 262 ft (80 m) Max cruise: 100 kt (180 kph) Eco omic cruise:88.9 kt (160 kph) Ra e: 384.73 nm (713 km) sf

KAMOV KA 226Ro or iame er: 42.65 ft (13 m) Fuse a e e h: 26.57 ft (8.1 m) Overae h: 42.65 ft (13m) Powerp a : 2 x 450 shp (331 kW) Allis n 250-C20R1turb shafts Emp y wei h : 4,303 lb (1,952 kg) Max ake-off wei h : 7,496 lb(3,400 kg) Usefu oa : 3,190 lb (1,448 kg) Ca i e h: 7.71 ft (2.35 m) Ca iwi h: 5.5 ft (1.54 m) Ca i hei h : 4.52 ft (1.40 m) Max sea i : 10 HIgE: 10,330 ft (3,150 m) HOgE: 8,100 ft (2,470 m) Max cruise: 118 kt (214 kph)Eco omic cruise: 108 kt (194 kph) Ra e: 341 nm (620 km)

KAMOV KA-62Ro or iame er: 44.3 ft (13.5 m) Fuse a e e h: 43.47 ft (13.25 m) Overae h: 51.84 ft (15.80 m) RT Powerp a : 2 x 1,300 shp (970 kW) RKBMRybinsk RD-600 turb shafts Emp y wei h : 8,223 lb (3,730 kg) Max ake-offwei h : 13,779 lb (6,250 kg) r 14,329 lb (6,500 kg) with external l ad Usefuoa : 4,409 lb (2,000 kg) r 5,511 lb (2,770 kg) n h k Ca i e h: 7.49 ft(2.28 m) Ca i wi h: 5.83 ft (1.78 m) Ca i hei h : 4.26 ft (1.30 m) Maxsea i : 18 HIgE: 9,514 ft (2,900 m) HOgE: 6,890 ft (2,100 m) Max cruise: 167kt (300 kph) Eco omic cruise: 144 kt (260 kph) Ra e: 378 nm (700 km) sf, nr


KAMOV KA 32Ro or iame er: 52 ft 2 in (15.9 m) Fuse a e e h: 37 ft 1 in (11.22 m) Overae h: 52 ft 2 in (15.9 m) RT Powerp a : 2 x 2,200 shp (1,619 kW) Klim v TV3-117VMA turb shafts Emp y wei h : 14,990 lb (6,800 kg) Max ake-off wei h : 24,250 lb (11,000 kg) Usefu oa : 11,000 lb (5,000 kg) n h k Ca i e h: 14 ft 10 in (4.52 m) Ca i wi h: 4 ft 3 in (1.3 m) Ca i hei h : 4 ft 4 in (1.24 m)Max sea i : 18 HIgE: 14,107 ft (4,300 m) HOgE: 12,140 ft (3,700 m) Maxcruise: 144 kt (260 kph) Eco omic cruise: 126 kt (230 kph) Ra e: 350 nm(650 km) sf, nr


14/18





KAzAn AKtAIRo or iame er: 32 ft 9.75 in (10 m) Fuse a e e h: 27 ft 4.75 in (8.35 m)Overa e h: 35 ft 8.25 in (10.88 m) Powerp a : 1 x 240 hp (179 kW) RPDVAZ 4265 r tary engine Emp y wei h : 1,334 lb (605 kg) Max ake-offwei h : 2,535 lb (1,150 kg) Usefu oa : 1,201 lb (535 kg) Ca i e h: 3 ft 11.75in (1.2 m) Ca i wi h: 5 ft 7 in (1.7 m) Ca i hei h : N/A Max sea i : 0 HIgE: 7,550 ft (2,300 m) HOgE: 4,265 ft (1,300 m) Max cruise: 103 kt (190 kph)Eco omic cruise: 84 kt (155 kph) Ra e: 324 nm (600 km) E ura ce: 7 hr

KAzAn AnSAtRo or iame er: 37.75 ft (11.5 m) Fuse a e e h: 37.9 ft (11.538 m) Overae h: 45 ft (13.768 m) Powerp a : 2 x Pratt & Whitney/Klim v PK 206Cturb shafts Emp y wei h : N/A Max ake-off wei h : 7,275 lb (3,300 kg)Usefu oa : 3,637 lb (1,650 kg) Ca i e h: N/A Ca i wi h: N/A Ca ihei h : N/A Max sea i : 9 HIgE: N/A HOgE: 5,900 ft (1,800 m) Max cruise: 128 kt (238 kph) Eco omic cruise: 75.5 kt (140 kph) Ra e: 281 nm (520 km)

Md HElICOPtERS Md 520nRo or iame er: 27.4 ft (8.34 m) Fuse a e e h: 25 ft 6 in (7.8 m) Overae h: 28 ft 6 in (8.7 m) Powerp a : 1 x 450 shp (317 kW) Allis n 250-C20Rturb shaft Emp y wei h : 1,586 lb (719 kg) Max ake-off wei h : 3,350 lb(1,519 kg) Usefu oa : 1,764 lb (800 kg) Ca i e h: 8 ft (2.44 m) Ca iwi h: 4 ft 3.5 in (1.31 m) Ca i hei h : 5 ft (1.52 m) Max sea i : 5 HIgE: 9,300 ft (2,835 m) HOgE: 5,600 ft (1,707 m) Max cruise: 124 kt (230 kph)Eco omic cruise: N/A Ra e: 201 nm (389 km)


Md HElICOPtERS Md 500ERo or iame er: 26.4 ft (8.05 m) Fuse a e e h: 24.6 ft (7.49 m) Overae h: 30 ft 10 in (9.4 m) Powerp a : 1 x 420 shp (313 kW) Allis n 250-C20Bturb shaft Emp y wei h : 1,481 lb (672 kg) Max ake-off wei h : 3,000 lb(1,361 kg)Usefu oa : 1,519 lb (689 kg) Ca i e h: 8 ft (2.44 m) Ca iwi h: 4 ft 3.5 in (1.31 m) Ca i hei h : 5 ft (1.52 m) Max sea i : 5 HIgE: 8,500 ft (2,590 m) HOgE: 6,000 ft (1,830 m) Max cruise: 134 kt (248 kph)Eco omic cruise: 129 kt (239 kph) Ra e: 264 nm (488 km)

Md HElICOPtERS Md 530FRo or iame er: 27.4 ft (8.34 m) Fuse a e e h: 24.6 ft (7.5 m) Overae h: 32 ft 1 in (9.78 m) Powerp a : 1 x 650 shp (484 kW) Allis n 250-C30turb shaft Emp y wei h : 1,509 lb (684 kg) Max ake-off wei h : 3,100 lb(1,406 kg) Usefu oa : 1,591 lb (722 kg) Ca i e h: 8 ft (2.44 m) Ca iwi h: 4 ft 3.5 in (1.31 m) Ca i hei h : 5 ft (1.52 m) Max sea i : 5 HIgE: 16,000 ft (4,877 m) HOgE: 14,400 ft (4,389 m) Max cruise: 133 kt (246 kph)Eco omic cruise: 131 kt (243 kph) Ra e: 232 nm (430 km)

Md HElICOPtERS Md 600nRo or iame er: 27.5 ft (8.4 m) Fuse a e e h: 30.5 ft (9.3 m) Overae h: 36.9 ft (11.2 m) Powerp a : 1 x 808 shp (603 kW) Allis n 250-C47turb shaft Emp y wei h : 1,930 lb (875 kg) Max ake-off wei h : 4,100 lb(1,860 kg) Usefu oa : 2,120 lb (961 kg) Ca i e h: 10.5 ft (3.2 m) Ca iwi h: 4.6 ft (1.4 m) Ca i hei h : 5 ft (1.52 m) Max sea i : 8 HIgE: 11,100 ft(3,383 m) HOgE: 6,000 ft (1,828m) Max cruise: 136 kt (252 kph) Eco omiccruise: 125 kt (231 kph) Ra e: 380 nm (704 km)

MIl (KAzAn) MI-17/MI-172Ro or iame er: 69 ft 10.5 in (21.29 m) Fuse a e e h: 60 ft 5.75 in (18.42 m)Overa e h: 83 ft 2 in (25.35 m) Powerp a : 2 x 2000 shp (1470 kW)Klim v TV3 117MT turb shafts Emp y wei h : 15,653 lb (7,100 kg) Max ake-offwei h : 28,660 lb (13,000 kg) Usefu oa : 13,007 lb (5,900 kg) Ca i e h: 17.51 ft (5.37 m ) Ca i wi h: 7 ft 8.25 in (2.34 m) Ca i hei h : 5 ft 10.25 in(1.8 m) Max sea i : 24 HIgE: 7,213 ft (2,200 m) HOgE: 5,775 ft (1,760 m) Maxcruise: 134.9 kt (250 kph) Eco omic cruise: 130 kt (240 kph) Ra e: 318 nm(590 km)


Md HElICOPtERS Md EXPlORERRo or iame er: 33 ft 10 in (10.32 m) Fuse a e e h: 32.4 ft (9.9 m) Overae h: 38 ft 3 in (11.7 m) Powerp a : 2 x 710 shp (529 kW) Pratt & WhitneyCanada PW 207E turb shafts Emp y wei h : 3,375 lb (1,531 kg) Max ake-offwei h : 6,500 lb (2,948 kg) Usefu oa : 3,125 lb (1,599 kg) Ca i e h: 6 ft 3in (1.91 m) exc c ckpit Ca i wi h: 4 ft 9 in (1.45 m) Ca i hei h : 4 ft 7 in (1.4m) Max sea i : 8 HIgE: 12,200 ft (3,719 m) HOgE: 10,000 ft (3,048 m) Maxcruise: 135 kt (250 kph) Eco omic cruise: 123 kt (158kph) Ra e: 293 nm (543km)


15/18





MIl (UlAn UdE) MI-171Ro or iame er: 69 ft 10.5 in (21.29 m) Fuse a e e h: 60 ft 5.75 in (18.42 m)Overa e h: 83 ft 2 in (2.535 m) Powerp a : 2 x 2,070 shp (1,545 kW)Klim v TV3 117VM turb shafts Emp y wei h : 15,653 lb (7,100 kg) Max ake-offwei h : 28,660 lb (13,000 kg) Usefu oa : 13,007 lb (5,900 kg) Ca i e h: 20 ft 10.25 in (6.36 m) Ca i wi h: 7 ft 8.25 in (2.34 m) Ca i hei h : 5 ft10.25 in (1.8 m) Max sea i : 24 HIgE: N/A HOgE: 5,775 ft (1,760 m) Maxcruise: 113 kt (210 kph) Eco omic cruise: N/A Ra e: 307 nm (570 km)

MIl (UlAn UdE) MI-8tRo or iame er: 69 ft 10.25 in (21.29 m) Fuse a e e h: 60.80 ft (18.547 m)Overa e h: 82 ft 10 in (25.24 m) Powerp a : 2 x 1500 shp (1103 kW)Klim v TV2 117A turb shafts Emp y wei h : 15,382 lb (6,968 kg) Max ake-offwei h : 26,455 lb (12,000 kg) Usefu oa : 11,108 lb (5,032 kg) Ca i e h: 17.51 ft (5.37 m) Ca i wi h: 7 ft 8.25 in (2.34 m) Ca i hei h : 5 ft 11 in (1.8m) Max sea i : 30 HIgE: 6,235 ft (1,900 m) HOgE: 2,625 ft (800 m) Maxcruise: 134.9 kt (250 kph) Eco omic cruise: 118.7 kt (220 kph) Ra e: 288.7nm (535 km)

MIl MI-34CRo or iame er: 32 ft 10 in (10 m) Fuse a e e h: 29 ft (8.85 m) Overae h: 37.4 ft (11.71 m) Powerp a : 1 x 325 hp (239 kW) M14 V26 radial pist nengine Emp y wei h : 2,252 lb (1,020 kg) Max ake-off wei h : 3,201 lb (1,450kg) Usefu oa : 949 lb (430 kg) Ca i e h: 2.1 ft (0,96 m) exc c ckpit Ca iwi h: 4 ft (1.23 m) Ca i hei h : 4.13 ft (1.26 m) Max sea i : 4 HIgE: N/AHOgE: 2,950 ft (900 m) Max cruise: 116 kt (215 kph) Eco omic cruise: 92 kt(170 kph) Ra e: 194 nm (360 km)


MIl MI-26tRo or iame er: 105 ft (32 m) Fuse a e e h: 110 ft 8 in (33.3 m) Overae h: 131 ft 3.75 in (40.03 m) Powerp a : 2 x 10,000 (7352 kW) ZMKBPr gress D-136 turb shafts Emp y wei h : 63,134 lb (28,600 kg) Max ake-offwei h : 123,458 lb (56,000 kg) Usefu oa : 60,486 lb (27,400 kg) Ca ie h: 39 ft 4.25 in (12 m) Ca i wi h: 10 ft 6 in (3.2 m) Ca i hei h : 10 ft4.25 in (3.17 m) Max sea i : 85 HIgE: 8,852 ft (2,700 m) HOgE: 5,574 ft(1,700 m) Max cruise: 159 kt (295 kph) Eco omic cruise: 137 kt (255 kph)Ra e: 383 nm (710 km)

MItSUbISHI MH2000ARo or iame er: 12.2 m (40 ft 0.25 in) Fuse a e e h: 12.2 m (40 ft 0.25 in)Overa e h: 14 m (45 ft 11.25 in) Powerp a : 2 x 876 shp Mitsubishi MG5-110turb shafts Emp y wei h : 2,500 kg (5,510 lb) Max ake-off wei h : 4,500 kg(9,920 lb) Usefu oa : 2,000 kg (4,410 lb) Ca i e h: 6.88 ft (2.1 m) Ca iwi h: 6.56 ft (2.0 m) Ca i hei h : 4.59 ft (1.4 m) Max sea i : 10 HIgE: 2,700 m (8,860 ft) @ MToW HOgE: 1,650 m (5,400 ft) @ MToW Max cruise: 250 kph (135 kt) Eco omic cruise: 228 kph (123 kt) Ra e: 780 km (420 nm) @cruise speed, standard tanks, n reserve

MK HElICOPtER gMbH lIgHt HElICOPtER MK IIIRo or iame er: 30.57 ft (9.32 m) Fuse a e e h: 25.8 ft (7.863 m) Overae h: 34 ft 9 in (10.6 m) Powerp a : 1 x 230 ps SMA SR-305 jet fuel pist nengine Emp y wei h : 1,540 lb (700 kg) Max ake-off wei h : 2,600 lb (1,182kg) Usefu oa : 2,337 lb (1,060 kg) Ca i e h: 5.9 ft (1.8 m) Ca i wi h: 4.26 ft (1.3 m) Ca i hei h : 4.26 ft (1.3 m) Max sea i : 2 HIgE: 14,763 ft(4,500 m) HOgE: 9,842 ft (3,000 m) Max cruise: 108 kt (200 kph) Eco omiccruise: 97 kt (180 kph) Ra e: Appr x 431 nm (800 km)

Pzl MI-2Ro or iame er: 47.8 ft (14.56 m) Fuse a e e h: 39.2 ft (11.94 m) Overae h: 57.4 ft (17.42 m) Powerp a : 2 x 425 shp (312 kW) GTD 350 turb shaftsEmp y wei h : 5,313 lb (2,410 kg) Max ake-off wei h : 7,826 lb (3,550 kg)Usefu oa : 2,513 lb (1,140 kg) Ca i e h: 7.44 ft (2.27 m) Ca i wi h: 4.92ft (1.5 m) Ca i hei h : 4.6 ft (1.4 m) average Max sea i : 10 HIgE: 5,167 ft(1,575 m) HOgE: 2,870 ft (875 m) Max cruise: 105 kt (190 kph) Eco omiccruise: 99.5 kt (180 kph) Ra e: 315 nm (580 km)


Pzl KAnIARo or iame er: 47.8 ft (14.56 m) Fuse a e e h: 39.47 ft (12.03 m) Overae h: 57.07 ft (17.4 m) Powerp a : 2 x 426 shp (313 kW) Allis n 250-C20Bturb shafts Emp y wei h : 4,320 lb (1,960 kg) Max ake-off wei h : 7,826 lb(3,550 kg) Usefu oa : 3,505 lb (1,590 kg) Ca i e h: 13.35 ft (4.07 m)Ca i wi h: 4.92 ft (1.5 m) Ca i hei h : 4.95 ft (1.51 m) Max sea i : 14HIgE: 8,202 ft (2,500 m) HOgE: 4,511 ft (1,375 m) Max cruise: 113 kt (210 kph)Eco omic cruise: 103 kt (190 kph) Ra e: 479 nm (886 km)


16/18

Pzl SW-4Ro or iame er: 29.5 ft (9 m) Fuse a e e h: 27 ft (8.25 m) Overa e h: 29.7 ft (9.07 m) Powerp a : 1 x 450 shp (336 kW) Allis n 250-C20R /2 (SP)turb shaft Emp y wei h : 2,094 lb (950 kg) Max ake-off wei h : 3,968 lb(1,800 kg) Usefu oa : 1,874 lb (850 kg) Ca i e h: 7.67 ft (2.34 m) Ca iwi h: 4.92 ft (1.5 m) Ca i hei h : 4.3 ft (1.31 m) Max sea i : 5 HIgE: 7,544ft (2,300 m) HOgE: 5,412 ft (1,650 m) Max cruise: 125.4 kt (232 kph) Eco omiccruise: 108.1 kt (200 kph) Ra e: 468.9 nm (860 km)

Pzl W-3A SOKOlRo or iame er: 51.5 ft (15.7 m) Fuse a e e h: 46.6 ft (14.2 m) Overae h: 61.65 ft (18.79 m) Powerp a : 2 x 900 shp (662 kW) PZL -10Wturb shafts Emp y wei h : 8,487 lb (3,850 kg) Max ake-off wei h : 14,110 lb(6,400 kg) Usefu oa : 5,623 lb (2,550 kg) Ca i e h: 10 ft 6 in (3.2 m)Ca i wi h: 5.08 ft (1.55 m) Ca i hei h : 4 ft 8 in (1.4 m) Max sea i : 14HIgE: 9,906 ft (3,020 m) HOgE: 6,232 ft (1,900 m) Max cruise: 127 kt (235kph) Eco omic cruise: 120 kt (222 kph) Ra e: 672 nm (1,244 km)

RObInSOn R44Ro or iame er: 33 ft (10.05 m) Fuse a e e h: 29.7 ft (9.07 m) Overae h: 38.6 ft (11.76 m) Powerp a : 1 x 225 hp (167 kW) Textr n Lyc ming o-540-F1B5 pist n engine Emp y wei h : 1,424 lb (645 kg) Max ake-off wei h : 2,400 lb (1,089 kg) Usefu oa : 976 lb (443 kg) Ca i e h: 6.9 ft (2.09 m)Ca i wi h: 4.2 ft (1.27 m) Ca i hei h : 4.3 ft (1.31 m) Max sea i : 4 HIgE: 6,400 ft (1,950 m) HOgE: 5,100 ft (1,554 m) at 2,200 lb (997 kg) gr ss weightMax cruise: 113 kt (209 kph) Eco omic cruise: 100 kt (185.2 kph) Ra e: 347nm (643 km)


RObInSOn R22 bEtA IIRo or iame er: 25.2 ft (7.67 m) Fuse a e e h: 20.7 ft (6.3 m) Overae h: 28.7 ft (8.76 m) Powerp a : 1 x 131 hp (94.3 kW) Textr n Lyc ming o-360-J2A pist n engine Emp y wei h : 845 lb (384 kg) Max ake-off wei h : 1,370 lb (621 kg) Usefu oa : 525 lb (239 kg) Ca i e h: 4.3 ft (1.31 m) Ca iwi h: 3.6 ft (1.1 m) Ca i hei h : 4 ft (1.22 m) Max sea i : 2 HIgE: 9,400 ft(2,865 m) HOgE: N/A Max cruise: 96 kt (177 kph) Eco omic cruise: 83 kt (154kph) Ra e: 319 nm (592 km)

ROtORWAY EXEC 162 FRo or iame er: 25 ft (7.62 m) Fuse a e e h: 22 ft (6.705 m) Overae h: N/A Powerp a : 1 x 150 hp (111 kW) 4-cyl, 162 in3 RI 162F f ur-str keEmp y wei h : 975 lb (442.2 kg) Max ake-off wei h : 1,500 lb (680.4 kg)Usefu oa : 525 lb (238.14 kg) Ca i e h: N/A (tw seats) Ca i wi h: N/A(tw seats) Ca i hei h : N/A (tw seats) Max sea i : 2 HIgE: 7,000 ft (2,134m) HOgE: 5,000 ft (1,524 m) Max cruise: 100 kt (185 kph) 115 mph Eco omiccruise: 95 mph (152.9 kph) Ra e: 180 sm (289.67 km)

SCHWEIzER 300CRo or iame er: 26.8 ft (8.2 m) Fuse a e e h: 22.19 ft (6.76 m) Overae h: 30.8 ft (9.39 m) Powerp a : 1 x 190 hp (141 kW) AlliedSignal Lyc mingHIo-360-D1A pist n engine Emp y wei h : 1,100 lb (499 kg) Max ake-offwei h : 2,050 lb (930 kg) Usefu oa : 950 lb (431 kg) Ca i e h: 4.1 ft (1.25m) Ca i wi h: 4.7 ft (1.43 m) Ca i hei h : 4.2 ft (1.28 m) Max sea i : 3HIgE: 10,800 ft (3,292 m) at 1,700 lb HOgE: 8,600 ft (2,612 m) at 1,700 lb Maxcruise: 86 kt (159 kph) Eco omic cruise: 64 kt (118 kph) VNE is 95 kt (176 kph)Ra e: 194 nm (360 km)






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Civil Helicopter Handbook 07-08

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