J41 Technical Data at a Glance 2
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Transcript of J41 Technical Data at a Glance 2
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7/28/2019 J41 Technical Data at a Glance 2
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pwk_0102 - JUL 2011 Produced by the Graphics and Media Team, Technical Publications, BAE SYSTEMS Regional Aircraft, Prestwick email: [email protected]
Jetstream 41 Technical Data - at a glance
BAE SYSTEMS 2011
All rights reserved.The information contained within this brochure is of the nature of
general comment only and does not constitute a warranty or condition
of any contract. Services offered may change. BAE Systems accepts
no liability for the misuse or misinterpretation of such information.
BAE SYSTEMS
Regional Aircraft,
Prestwick International Airport,
Ayrshire,
Scotland KA9 2RW
United Kingdom
Telephone +44 (0)1292 675000
Fax +44 (0)1292 675700email [email protected]
For more information about Regional Aircraft visit:www.regional-services.com
REGIONAL AIRCRAFT
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7/28/2019 J41 Technical Data at a Glance 2
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Typical Seating Layouts
Cost effective...Flexible...Efficient...The ideal feeder aircraft
Avionics
Unrivalled Economics
Operational Characteristics
The Jetstream 41 is proven in service to offer operators a winning combination of quality and efficiency which has resulted in an a ircraft
with the lowest operating costs in its class.
The Jetstream 41 was developed to meet the needs of regional airlines.
It uses the best cost-effective technology in structures, avionics and
systems.
It offers a competitive balance of performance, comfort and reliability at
minimum cost.
The Jetstream 41 is proven in service to have greater productivity than
other similar capacity turboprops.
Design weights/payloads
Max take-off weight 10,886 kg (24,000 lb)
Max landing weight 10,569 kg (23,300 lb)
Max zero fuel weight 9,707 kg (21,400 lb)
Typical operating empty weight 6,622 kg (14,600 lb)
Payload 3,084 kg (6,800 lb)
Fuel capacity 3,306 Itrs (874 US gal)
Operational Performance
Engine Garrett TPE331-14GR/HR
Maximum power 1500SHP/1650SHP
Dual EDZ805 EFIS
Dual AHZ600 AHRS
Dual ADZ800 DADC
Primus 650 Colour Weather Radar
Trimble TNL8100 Long Range GPS or Universal UNS- 1M GPS
FZ-450 Digital Flight Data Recorder
Sundstrand MkVI GPWS or Honeywell EGPWS
Fairchild F100 FDR
Universal CVR-30A CVR
Smiths LED Engine Indicating System
Narco ELT-910 ELT
Bendix/ King CAS66A TCAS
3500
200 600 800
3000
2500
2000
500
1500
0
1000
4000 1000 1200 1400
Range (nm)
Payload
(kg)
29 passengers at 95kg
High speed cruise
ISA, FL250,
JAR reserves
Propeller McCauley, 5 bladed metal
Typical cruise speed 295Kts
J4 1J4 1 J4 1
450mm(17.7in)
420mm(16.5in)
1.88m
(6ft 2in)
1.78m(5ft 10in)
Cabin Cross Section
The proven low cost 30 seater turboprop
The Jetstream 41 offers more seats at higher frequency
for lower risk and lower cost. .. producing greater profit
Jetstream 41 - Technical Data
Primus II SRZ-85X Digital Integrated RadioSystem comprising:
- RCZ-85X Integrated Comms Unit- Dual VHF- Dual VOR/ILS- Dual ADF- Six Channel DME
TG
TG
T
30 seat layout
12 seat corporate layout
29 seat layout with forward galley
29 seat layout with rear galley
TG
I Stand-up headroom of over 1.78m (5ft 10in)I 30/ 29 seats at 30in pitchI Checked baggage capacity 4.81m (170ft )I
Carry on stowage 0.61m (21.5f t )I Underfloor stowage 1.35m (47.5f t )I Total capacity per pax 0.24m (8.6ft )I Full forward or rear galley
3 3
3 3
3 3
3 3
