2006 300CBi Presentation February 2006
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Transcript of 2006 300CBi Presentation February 2006
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SCHWEIZER
MODEL 300CBi HELICOPTER
GENERAL DESCRIPTION AND OPERATING COMPARISON
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TH-55 OSAGE - U.S. ARMY EXPERIENCE
P R I MAR Y U . S . AR MY TR AI NE R 1965-1988
OVE R 60,000 P I LOTS TR AI NE D
OVE R 4,000,000 F LI G H T TR AI NI NG H O U RS
OVER 12,000,000 TOUCHDOWN AUTOROTATIONS
ONLY 1 CATEGORY AACCIDENT SINCE
TRAINING BEGAN AT FT. RUCKER (1972)
TH-55/TH-300C WORLDS
STANDARD MILITARY TRAINERS
SCHWEIZER
MODEL 300CBi
HELICOPTER
MODEL 269 SERIES HELICOPTERS
OVE R 3750 AI RC RAF T P R OD U CE D
P R I M AR Y TR AI NE R F OR MI L ITAR Y I N 24 C OU N TR I E S
OVE R 20 MILLION H OU RS ON FLE ET
M I LE S TO NE S -1964-F ir s t TH-55A t o U . S . Ar m y
1970-H ugh es dev eloped M odel 300C
1983-P rogra m Tra nsit ioned to Schw eizer
2005-1000TH Sch w eizer helicopter produced
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MODEL 300CBi GENERAL
ARRANGEMENT
PRINCIPLE DIFFERENCES
300C Vs 300CBi
E ngin e C ha n ge: L ycom ingH IO-360-G 1A, 180 mx h p;injected; 2200 hours MTBO
G r oss Weigh t : R ed uced t o1,750 lbs, 687 lbs useful loa d
P ilot -in -C omma n d: S w i t ch edto right side
F uel Ta n k (S t a n da r d ): 32.5ga llons usea ble
I nspect ion a n d Ma in t en a n ce:
D esign upgra des; componentlives exceed 4,000 hours
AE S sy st em a nd a vionicsincluded a s sta nda rdequipment
WEIGHTS LBS. KG
Gross Weight 1750 793.8
Empty Weight 1088 493.5
Crew (2) & Baggage 400 163.3
Fuel 195 88.4
Payload 67 48.5
SCHWEIZER
MODEL 300CBi
HELICOPTER
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Airfra me: - Night light w it h st robe bea cons- Extruded a luminum sla t- Im proved door gla ss mounting syst em- Heavy duty skids
Cockpit Int er ior : - D ua l cont rols- P IC r ight side- Int erna l stora ge compar tment
E ngine & D rive S yst em: - L ycoming H IO-360-G 1A inject ed engine
- Foa m ca rtr idge a ir inta ke system- Noise reduction upsta ck- One-piece upper pulley h ub- Automa tic rotor enga gement syst em- St a rt-up overspeed limiter
Avionics: - B endix King KY96A comm t ra nsceiver- G a rmin G TX 320A tra nsponder- ACK A-30 blind encoder- Int ercom
EQUIPMENT AND UPGRADES
STANDARD ON 300CBi
SCHWEIZER
MODEL 300CBi
HELICOPTER
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R22B 300CBi
855 1,088
178 195
400 400
-63 67
Certified Gross Weight
Operating Weight
Weight Margin
WEIGHT IN POUNDS
1,433
1,370
1,683
1,750
Crew Weight & Baggage
Empty Weight - Equipped
Full Fuel (29.7 Gal/32.5 Gal)
C ockpit S ize: 25% la rger ; 10 inches w ider
C ont rol S ystem: C onvent iona l cont rol; st a bleha ndling cha ra ct eristics, no
ca rburetor hea t r eq uired
U seful Loa d:
SUITABILITY FOR TRAINING
RELATIVE TO R22
SCHWEIZER
MODEL 300CBi
HELICOPTER
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F ly in g q ua lit ies a n d h a n dlin g
cha ra ct erist ics of 269 serieshelicopters ra t ed good t oexcellent
Margin of sa fety is cr it ica l for
tra ining a ircra ft - R22B isina dequa te under cert a inconditions
Au t or ot a t ion sa fet y m a r gin of
300CB i is excellent
Low rot or RP M w a rningsyst em on 300C B i
SAFETY CHARACTERISTICS -
STUDENT MARGINS
Aut orot a t ion Ind ex C ha rt
(t/k = E nerg y of rot or syst em/E ner gy needed t o hover)
SCHWEIZER
MODEL 300CBi
HELICOPTER
i
iESHP
HOGESLSX550
1/2IR
2
P/E=
ESHP
HOGESLSX550
1/2IR
2
P/E=
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Tr i-level energy
a bsorption syst em
23 in ch es of st r oke
I njur y Acciden t a nd
Fa ta lity ra t esignifica nt ly low er
th a n R22B
SAFETY CHARACTERISTICS
CRASHWORTHINESS
ARTICULATED ROTOR SYSTEMMAST: ROLLOVER PROTECTION
RAPID THROTTLERESPONSE: RESERVEPOWER
ROTOR IMPINGEMENTOUTSIDE CREW ENVELOPE
ENERGY ABSORPTION, CRUSHABLE STRUCTURE; 23 INCHESOF STROKE
DUAL STROBE LIGHTS - VISIBLE FROM ALL ANGLES
LOW AFT MOUNTED ENGINE
ENGINE AND FUEL SYSTEM OUTSIDE OFENCLOSED STRUCTURE
PROVEN DYNAMIC SYSTEM
SCHWEIZER
MODEL 300CBi
HELICOPTER
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Inspect ions and Service Schedule:
L ubr ica t e - 25 h ou rs
Oil ch a n ge - 50 h ou rs
100 hour inspect ion - 12 manhours 600 hour inspect ion - 30 manhours
C omponent Lives:
H I O-360-G 1A E n gin e:
Injected engine - no ca rburetor heat requirement
2,200 hou r MTB O
Less scheduled and unscheduled maintena nce
MAINTENANCE - MINIMIZEDOWNTIME AND
DIRECT OPERATING COST
300C LIFE 300CBiLIFE
3,600 4,0002,100 4,200
2,500 4,200
1,900 4,000
3,000 4,000
M/R Drive Shaft
M/R Transmission Overhaul
COMPONENT
M/R Pitch Bearing ShaftTail Boom Assembly
Horizontal Stabilizer
SCHWEIZER
MODEL 300CBi
HELICOPTER
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H over performa nce a t gross weight is a pproxima tely the sa me.
At higher density a l t itudes or w ith equa l pa yloa d & fuel
w eight s, 300C performa nce is superior
PERFORMANCE - RELATIVE TO
300C
H over C eiling, Ou t -of-G round E ffect H over C eiling, I n-G round E ffect
SCHWEIZER
MODEL 300CBi
HELICOPTER
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0
50,000
100,000
150,000
200,000
250,000
300,000
1 2 3 4 5
R-22B
300CB
CASH OUTFLOW VS. YEARS IN SERVICE
800 flight hours per year
Domestic operator Aircraft at list prices
YEARS
DOL
LARS
Conklin a nd deDecker subst a nt iat ed tota l cost of ow nership for 300CB a nd R 22 to be approximat elyequa l - t he 300CB offers more favora ble ca sh flow (See Economic Ana lysis of the Schw eizer 300CBa nd R obinson-R22B 2, Conklin a nd deD ecker Avia t ion I nforma t ion, J a nua ry 26, 2001).
SCHWEIZER
MODEL 300CBi
HELICOPTER
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S pa res S upport
Wa rra nt y
Overh a ul E xch a nge P rogra m
Ma in ten a nce Tr a in in g
Technica l Representa t ive Suppor t
Tech n ica l P ublica t ion s
PRODUCT SUPPORTSCHWEIZER
MODEL 300CBi
HELICOPTER
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Cockpit Layout
ADVANTAGES OF SCHWEIZER
300CBi FOR FLIGHT TRAINING
10 inches w ider a nd 25% more volume t ha n R22.
Conventiona l cont rol system no nega tive ha bit tr a nsfer.
Adjusta ble a nt i-t orque pedals w ith 5.4 inches of tr a vel -
ena bles pilot s of near ly a ny size to be comfort a bly seat ed.
Inst rument pa nel and useful loa d accommodat es full IF R
instrument panel.
St a nda rd E quipment includes instruments a nd a vionics
requ ired for VFR, da y/night flight t ra ining.
Only production helicopter t o offer 360 visibilit y from
pilots seat - far exceeds FAA requirements of AC-27-1.
Right ha nd pilot-in-comm a nd position.
SCHWEIZER
MODEL 300CBi
HELICOPTER
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Operational Advantages
ADVANTAGES OF SCHWEIZER
300CBi FOR FLIGHT TRAINING
140 lbs. more useful loa d th a n R22 a t compa ra ble endur a nce. Automa tic rotor engagement system.
Injected engine elimina tes carb heat requirement .
E xcellent t hr ottle correla t ion elimina t es need for t hr ott le governor.
Low cockpit vibra tion a nd noise levels.
Typica l fuel consum ption in t ra inin g opera t ion 10.5 ga llons/hour .
S t a rt -up overspeed limiter.
Optiona l P .I.C. position.
Lowest fly over noise profile of a ny piston h elicopter.
Optiona l ca pability t o fly w ith t hree crewm embers.
Wide selection of optiona l a vionics a nd equipment .
SCHWEIZER
MODEL 300CBi
HELICOPTER
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ADVANTAGES OF SCHWEIZER
300CBi FOR FLIGHT TRAINING
St a ble a nd responsive ha ndling cha ra cteristics.
Cy clic cont rol well bala nced under a ll flight conditions.
E xcellent t hr ott le correlat ion elimina tes need for thr ott le
governor (FAA mandated in R22).
180 hp engin e provides excellent pow er m a rgins.
Flight Properties
Flight hours required by st udent pilot s to solo or achieve ra t ings is
document ed to be 20 to 30%less th a n R22; SF AR 73 ma nda t es
minimums for R22.
Convent iona l cont rols enha nce cockpit coordina t ion a nd a bility of
instructor to demonst ra te m a neuvers or t a ke over contr ol of a ircra ft.
Cockpit size, robust st ructur e, a nd st a ble flight properties ar e
confidence builders t o stud ents.
J eppesen tr a ining ma teria l is ta ilored to 300CB i and fa cilita tes
learning.
Training Effectiveness
SCHWEIZER
MODEL 300CBi
HELICOPTER
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Safety and Crashworthiness
General
In th e first 200,000 hours of opera tion, there w ere no fa t a lities, only one injury
a ccident in a 300CB , a nd a t ot a l of only eleven a ccidents.
NTSB sta tistics substa nt iat e tha t 269 Series helicopters ha ve the low est
a ccident ra te a nd fa ta lity ra t e per flight hour of an y pist on-pow ered helicopter.
300CB iconta ins the sa me sa fety a nd cra shw orth iness feat ures of the Model
300C.
FAA ha s imposed no SF ARs on a ny S chweizer helicopters a nd n o minimum
a mount of t ime before solo.
Safety
Forgiving flight cha ra cteristics ena ble stu dent pilot or instr uctor to recover a n
a ircra ft a fter an improper contr ol movement . Significa nt a re its:
- la rge pow er reserve;
- ra pid response to thr ott le inputs; a nd
- forgiving ha ndling char a cteristics
SCHWEIZER
MODEL 300CBi
HELICOPTER
ADVANTAGES OF SCHWEIZER
300CBi FOR FLIGHT TRAINING
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ADVANTAGES OF SCHWEIZER
300CBi FOR FLIGHT TRAINING
Safety (cont)
Low rotor speed wa rning indicators.
E xceptiona l a ut o-rota t iona l properties becau se of high kinet ic energy in
a rt icula ted rotor system.
D yna mic system proven by over 18 million flight hours.
No concerns r egar ding ca rbur etor ice.
Crashworthiness
E nergy a bsorpt ion 23 inches of stroke a chieved th rough compression
of la nding gear , crusha ble sub-floor, a nd seat str ucture.
No incident of blad e impingement int o ca bin of an y 269 Series
helicopters. No incident of in-flight brea k-ups or a irborne ta ilboom str ikes on a ny
269 Series aircra ft ma nufactured during la st t w enty years.
E ngin e an d fuel syst em out side of enclosed stru cture.
Ma st provides rollover protection .
Safety and Crashworthiness (cont)
SCHWEIZER
MODEL 300CBi
HELICOPTER
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ADVANTAGES OF SCHWEIZER
300CBi FOR FLIGHT TRAINING
Performance
S t a nda rd fuel t a nk provides 2.5 hours of tra ining plus reserves.
S ea level, IS A performa nce a t gr oss weight is compa ra ble to
t ha t of 300C.
H over performa nce, ra nge, endur a nce, an d speeds a re more
th a n a dequa te for ab initio tr a ining role.
Wider CG envelope th a n R22 a nd w ith significa ntly few eroperating restrictions.
St a rt-up and shut dow n in gusty conditions is not a n
opera tional limita tion for a rticula ted, t hree-bladed rotor system
a s on 300CB i.
SCHWEIZER
MODEL 300CBi
HELICOPTER
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ADVANTAGES OF SCHWEIZER
300CBi FOR FLIGHT TRAINING
Maintainability
Lowest Finit e Life Limit on a ny life-limited component is 4000 hours.
En gineered to minimize maint enan ce ma n hours per flight hour a nd
downtime.
100%field ma inta ina ble no fa ctory overha ul at 2000 hours or aft er
ten years.
Ma intena nce int ervals simplified a nd a ligned:- 100 hour genera l inspections a vera ge 10-12 hours ; a nd
- periodic ma int ena nce scheduled every 600 hours.
Schedule overha ul time for engine at 2200 hours; for ma in a nd t a il
rotor tra nsm issions a t 4200 hours.
SCHWEIZER
MODEL 300CBi
HELICOPTER
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ADVANTAGES OF SCHWEIZER
300CBi FOR FLIGHT TRAINING
Customer Support
Cont inuous P roduct Impr ovement - S ince int roduction of th e
300CB , Schw eizer engineering ha s ma de over 90 product
improvements which have increased performance, lowered
opera ting costs, a nd increased r eliability.
E xcellent spa res support a nd technical support fr om Schw eizer
Aircra ft a nd it s service netw ork. B est w a rra nty of a ny piston-pow ered helicopter.
High q ua lity factory insura nce progra m.
Competit ive finan ce progra m w ith no hourly reserve and t erms out
to tw enty yea rs.
SCHWEIZER
MODEL 300CBi
HELICOPTER
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1 See E conomic Ana lysis of the S chweizer 300CB a nd Robinson-R22B2 ba sed on Typical U .S.
Opera tions , Conklin a nd deDecker Aviat ion Informa tion, J a nua ry 26, 2001.
ADVANTAGES OF SCHWEIZER
300CBi FOR FLIGHT TRAINING
Cost Consideration
Conklin a nd deD ecker Report 1 substa ntia tes tha t t ota l cost of
ow nersh ip (i.e., the cost to a cqu ire a nd opera t e) for a 300CB a nd R 22
is a pproxima tely equa l th e 300CB offers m ore fa vora ble ca sh flow .
Resa le value of 300CB i is much higher t ha n R 22 (2000 hour C B sells
for 65% of orig ina l cost ; 2000 hour R22 for 20%).
B eca use of cost equiva lency per flight hour a nd t he low er number of
hours required to a chieve ra tings, t he cost to th e student to a chieve
a ra t ing is less tha n in R22.
SCHWEIZER
MODEL 300CBi
HELICOPTER