y12 general purpose aircraft - catic sudamericana 090324.pdf · y1 2_ 2 y12 general purpose...
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Y12 General Purpose Aircraft
Y12_ 2 Y12 General Purpose Aircraft
Technical Description
Ø Twinturboprop light generalpurpose aircraft Ø 1719 passenger transport and wide variety of
multirole operations Ø Meeting the airworthiness regulation of CAAC,
CAA, FAA Ø High reliability and safety Ø Remarkable STOL performance Ø Easy handling and maintenance Ø Costeffective
General
Y12_ 3 Y12 General Purpose Aircraft
Technical Description
Y12 Series Y12 II Ø PT6A27 engine, 3blade propeller Ø MTOW/Payload: 5300kg/1700kg Ø 17 seats
Y12 IV Ø PT6A27 engine, 3blade propeller Ø MTOW/Payload : 5670kg/1980kg Ø 19 seats Ø Winglet layout
Y12 E (“Hot and high” version) Ø PT6A135A engine, 4blade propeller Ø MTOW/Payload : 5670kg/1980kg Ø 19 seats Ø Winglet layout
Y12_ 4 Y12 General Purpose Aircraft
Technical Description
Milestone
1982 Maiden flight of Y12 II 1985.05 First delivery 1985.12 CAAC Type Cer tificate to Y12 II 1986.12 Expor t of fir st Y12 II 1990.06 CAA Type Cer tificate to Y12 II 1991.04 CAA Production Cer tificate to Y12 II 1994.07 CAACType Cer tificate to Y12IV 1995.03 FAA Type Cer tificate to Y12 IV 1995.09 FAA Production Cer tificate to Y12IV 2001.12 CAAC Type Cer tificate to Y12 E
Y12_ 5 Y12 General Purpose Aircraft
Technical Description
Missions
Ø Passenger transport Ø VIP transport Ø Cargo transport Ø Maritime patrol Ø Air ambulance Ø Troop transport and parachuting Ø Geological survey Ø Aerial photography Ø Aerial raining, forest seeding
Y12_ 6 Y12 General Purpose Aircraft
Technical Description
Airworthiness
Ø Y12 series are designed, tested and manufactured to the requirements of FAR part 23 including Amendments No. 231 through 2342 Ø The noise level is up to the specification of FAR part 36
Y12_ 7 Y12 General Purpose Aircraft
Technical Description
Improvement of Y12
Y12IV’s modifications ØWinglet layout ØMTOW up to 5,670 kg Ø 19 seats Ø Aft outside cargo door
Y12E’s modifications Ø PT6A135A and 4 blades propeller
Ø Steering nose wheel
Y12_ 8 Y12 General Purpose Aircraft
Technical Description
Y12 World Customers
BANGLADESH CAMBODIA CHINA ERITREA FIJI GUYANA IRAN KENYA KIRIBATI LAOS MALAYSIA
MAURITANIA MONGOLIA NAMIBIA NEPAL PHILIPPINES PAKISTAN PERU SRI LANKA TANZANIA VANUATU ZAMBIA
Y12_ 9 Y12 General Purpose Aircraft
Technical Description
Dimensions
Aircraft Length 14.86m 48.75ft
Wing Span 19.2m 63.0ft
Aircraft Height 5.675m 18.62ft
Wheel Track 3.61m 11.84ft
Wheel Base 4.702m 15.43ft
Y12_ 10 Y12 General Purpose Aircraft
Technical Description
Weights
Y12II Y12IV/E
Max. takeoff weight 11680 lb. / 5300 kg 12,500Ib / 5,670kg Max. landing weight 11680 lb. / 5300 kg 11,900lb / 5,400kg Max. zerofuel weight 10800 lb. / 4900 kg 11,430 lb / 5,188 kg
Max. payload 3750 lb./1700 kg 4,370lb / 1,984kg Max. usable fuel 2710 lb./1230 kg 2,710 lb / 1,230 kg
Y12_ 11 Y12 General Purpose Aircraft
Technical Description
Performance
Y12 II Y12 IV Y12 E
Ecomonic cruise speed (TAS) (ISA, 10,000ft, MTOW)
Ceiling (ISA, MTOW, two engines)
Rateofclimb (ISA, SL, MTOW, two engines)
Rateofclimb (ISA, SL, MTOW, one engine)
Tak eoff distance (ISA, SL, MTOW) Tak eoff roll
(ISA, SL, MTOW) Landing distance
(ISA, SL, MLW, with brake only) Landing roll
(ISA, SL, MLW, with brake only) Max. range
(ISA, 10,000ft, MTOW, 45 min. holding)
140 KTAS / 260 km/h 145 KTAS / 270 km/h
22,966 ft / 7,000 m 22,966 ft/ 7,000 m
1,535 ft/min / 7.8 m/s 1,535 ft/min / 7.8 m/s
295 ft/min / 1.5 m/s 285 ft/min / 1.45 m/s
1,607 ft / 490 m 1,480 ft / 450 m
1,213 ft / 370 m 1,050 ft / 320 m
707 nm / 1,310 km 723 nm / 1,340 km
2,066 ft / 630 m 1,935 ft / 590 m
1,115 ft / 340 m 1,080 ft / 330 m
140 KTAS / 260 km/h
22,966 ft / 7,000 m
1,594 ft/min / 8.1 m/s
276 ft/min / 1.4 m/s
724 nm / 1,340 km
1,400 ft / 425 m
1,115 ft / 340 m
2,035 ft / 620 m
1,115 ft / 340 m
Y12_ 12 Y12 General Purpose Aircraft
Technical Description
Payload vs. Range
Y12_ 13 Y12 General Purpose Aircraft
Technical Description
High Performance
Ø Remarkable STOL performance: • 340 m landing roll with brake only • 200 m landing roll of Y12II with brake and reverse
Ø Good “Hot and high” performance offered by Y12E Ø Exceptional airfield adaptability:
• Takeoff and landing on unpaved airfields • or poorprepared strips
Ø VFR or IFR flying at day and night Ø Flying at icing condition
Y12_ 14 Y12 General Purpose Aircraft
Technical Description
Cabin Layout
Y12_ 15 Y12 General Purpose Aircraft
Technical Description
Passenger Comfort
Ø 1.7mheight cabin Ø NORDAM interior decoration Ø Large windows Ø Large front and rear luggage
compartments Ø 1719 seat configurations
Y12_ 16 Y12 General Purpose Aircraft
Technical Description
Proven Engine System
Ø Proven Pratt &Whitney PT6 series turboprop engines
Ø Hartzell propellers with full feathering and revering capability
Ø High reliability, economics and ease of maintenance
Ø “Hot & high” performance offered by PT6A135A engines
Y12IV Y12E
Engine model PT6A27 PT6A135A
Takeoff power 2 x 620 SHP 2 x 620 SHP
Propeller type Hartzell Hartzell
Propeller blade 3 4
Y12_ 17 Y12 General Purpose Aircraft
Technical Description
Advanced Cockpit
Ø Stateoftheart avionics Ø High reliability and good maintainability
Y12_ 18 Y12 General Purpose Aircraft
Technical Description
Deicing System
Ø Propellers Ø Engine air intakes Ø Leading edge of wing
and tail Ø Pilot and stall
warning tab
Y12_ 19 Y12 General Purpose Aircraft
Technical Description
Avionics
Standard equipment Optional equipment
Ø Collins and Bendix King series available on customer’s option
Pictorial Navigation Sys tem
PN101 1 USA
VHF Transceiver VHF251 2 USA
VOR Receiver VIR351 1 USA
Glideslope Receiver GLS350 1 USA
HF Transceiver HF230 1 USA
Audio Control Panel AUD251H 1 USA
Beacon Marker MKR350 1 USA
Auto Direction Finder ADF650A 1 USA
Distance Measure Equip ment
DME451 1 USA
Transponder TDR950 1 USA
Altitude Encoder 10142011934 1 USA
Radio Altimeter ALT50 1 USA
Cockpit Voice Recorder A100A 1 USA
Weather Radar RDR1400C/RDS 2000
1 USA
Autopilot APS65 1 USA
GPS KLN90B 1 USA Ground Proximity Warning System
MKVI 1 USA
Y12_ 20 Y12 General Purpose Aircraft
Technical Description
Optional Equipment
Ø Wing and empennage deicing system (Goodrich Co.)
Ø Ramp ventilation system in cockpit Ø Natural ventilation system in cabin Ø Heating system in cabin Ø Emergency locating system
(ELT310010) Ø Steering nose wheel Ø Oxygen system Ø Toilet
Y12_ 21 Y12 General Purpose Aircraft
Technical Description
Multirole Versions
Ø Maritime patrol Ø Cargo transportation Ø Parachute jumping Ø Air dropping Ø Geological survey Ø Aerial photography Ø Ambulance Ø Forest seeding and fire protection Ø Artificial raining
Y12_ 22 Y12 General Purpose Aircraft
Technical Description
Mission Equipment: I. Passenger Version Standard Seating
2 Pilots+17/18/19 PAX
II. Corporate VIP Seats Foldable Table Food Galley Toilet
2 Pilots+10 PAX
Passenger/Corporate Transport
Y12_ 23 Y12 General Purpose Aircraft
Technical Description
Cargo Transport
Ø 2 tons payload Ø Cabin floor payload
154Ib/ft 2 (750kg/m 2 ) Ø Large cargo door for
easy loading and unloading
Ø Suitable for short and unpaved runway
Y12_ 24 Y12 General Purpose Aircraft
Technical Description
Air Ambulance
Missions
Ø Medical rescue Ø Transport of wounded
or sick personnel Ø Military and civil
operation Seat Stretcher Firstaid kit
Mission capacity
Ø 6 stretchers + 4 seats
Y12_ 25 Y12 General Purpose Aircraft
Technical Description