328 New Corporate Livery Proposal. 01/01/2013. 328 JET / DBJ. Colours /
Finishes. Pattern Black 40% tint. Dornier 328-300 (Light Jet). +49 8153 88111
2512.
+49 8153 88111 2512
[email protected] www.328.eu
Dornier 328-300 (Light Jet) 328 New Corporate Livery Proposal
01/01/2013
328 JET / DBJ
Pattern Black 40% tint
23ft 1.5in (7.048m)
10ft 7in (3.22m)
68ft 10in (20.98m)
69ft 8in (21.23m)
Colours / Finishes
Yellow: ref. pantone 109 / RAL 1003 GLOSS Black ref. 90% tint / RAL 7021 GLOSS Silver ref. Akzo Nobel ‘moonglow silver’ E99060 METALLIC
328 TP
C design copyright ctm design london 2013
D328-300 Performance Analysis
Payload vs.CAPABILITY Range (Light Jet) PAYLOAD RANGE 4,000
40
3,500
35 950 NM Range 32 PAX @ 97 kg (3,104 kg)
924 NM Range
30
PAYLOAD (KG)
2,500
25
2,000
20
1,500
1,000
10 Long Range Cruise
ASSUMPTIONS FL 350, Still Air, ISA JAR OPS Reserves (100 NM Alternate) 5 + 5 min Taxi Allowance OEW 9,320 kg, 32 PAX Layout
500
0
15
High Speed Cruise
High Speed Cruise (HSC) Long Range Cruise (LRC)
0
100
200
300
PAX @ 97 KG (213.8 LB)
3,000
400
5
500
600
700
800
900
1,000
1,100
1,200
1,300
1,400
1,500
0 1,600
STILL AIR RANGE (NM) 328 Group - 18/06/2013 - D328-100 & D328-300 Payload Range Charts - 2013-06-18.xlsx / Payload-Range (328-300)
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Page 2
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certification basis Regulations SEATING Crew & Passenger Capacity Cabin Volume Cabin Floor Area Cabin Baggage Volume 35 cu ft 1,0 cu m POWERPLANTS
JAR 25 / FAR PART 25
Engine Manufacturer/Model
3 + 32 = 35 1.183 cu ft 203 sq ft 35 cu ft 226 cu ft 1.653 lb
Takeoff Power PRESSURIZATION Differential Pressure (STD) Sea Level Cabin Altitude Max Operating Altitude - STD Max Operating Altitude - OPT BASIC WEIGHTS Max Ramp Weight Max Take Off Weight Max Landing Weight Max Zero Fuel Weight Typical Operating Empty Weight (incl. crew) Fuel Capacity (fuel density 0.80 kg/l) Max Useful Load Max Payload PERFORMANCE (ISA, SEA LEVEL)
FLIGHT PERFORMANCE (ISA +10°C) FLIGHT LEVEL
DISTANCE
NM
KM
100
185
200
370
300
556
400
741
500
926
Pratt & Whitney Canada/PW 306B
600
1.111
700
1.296
2x 6,050 lb
800
1.482
900
1.667
33,5 cu m 18,9 sq m 1,0 cu m 6,4 cu m 750 kg
2x 26.9 kN
1000 1.852
170 270 350 350 350 350 350 350 350 350
BLOCK TIME
0:32 0:48 1:05 1:21 1:37 1:53 2:09 2:25 2:41 2:56
BLOCK FUEL
LB 954 1.528 1.910 2.358 2.808 3.260 3.715 4.173 4.635 5.085
6,75 psi 16.029 ft 31.000 ft 35.000 ft
465 mbar 4.886 m 9.449 m 10.668 m
34.789 lb 33.510 lb 31.063 lb 27.800 lb 20.28 lb
15.780 kg 15.200 kg 14.090 kg 12.610 kg 9.200 kg
basic configuration
8.011 lb 12.743 lb 7.518 lb
3.634 kg 5.840 kg 3.410 kg
interior
Power Loading - MTOW
2.85 lb/Ib thrust 291 kg/kN
Wing Loading - MTOW Takeoff Field Length - MTOW Initial Rate of Climb - MTOW Gross Climb Cradient 2nd Segment - MTOW
80.2 Ib/sq.ft 4.485 ft 3.690 ft/min 5.4 %
Time to Climb to 31,000 ft 95% MTOW Time to Climb to 35,000 ft 95% MTOW Service Ceiling Single Engine - 95% MTOW Max Cruise Speed - 95% MTOW Landing Field Length - MLW (1/0.6) - 95% MTOW
16,9 min
391.5 kg/sq.m 1.367 m 1.125 m/min
KG 433 693 866 1.070 1.274 1.479 1.685 1.893 2.102 2.307
PAX LOAD
32 32 32 32 32 32 32 32 32 31
SPEED
HSC HSC HSC HSC HSC HSC HSC HSC HSC HSC
• No winds, 5 + 5 min. ground allowance, 3 min. maneuvering allowance 100 nm IFR reserves with 45 min. LRC @ Cruising FL, Passenger weight 225 lb each
Airline Transport Aircraft, alternatively: Corporate/Executive, Special Mission 2 Pilots, 1 Flight Attendant, 32 Passengers & Cargo Operating Empty Weight is subject to equipment installed
32 seats standard, other configurations available as required Galley/Refreshment Center, Aft Lavatory, Wardrobes
avionics (honeywell primus 2000) EFIS, EICAS, 5 CRT’s (7 in x 8 in), Flight Management System Dual Primus II Integrated Radio System, Dual Integrated Avionics Computer Automatic Flight Control System, Dual Digital Air Data Reference Unit Dual Altitude and Heading Reference System, Primus 660 Weather Radar
22,7 min
Mode S Transponder, Fault Recording
24.700 ft
7.529 m
Traffic Alert and Collision Avoidance System (TCAS 2000)
400 kts
460 mi/h / 740 km/h 1.306 m
standard equipment
4.285 ft
Enhanced Ground Proximity Warning System (EGPWS) with Wind Shear Detection & Guidance
Air Turbine Starter, Allied-Signal GTCP 36-150 APU, Ground Spoiler
optional equipment GPS with Non Precision Approach, Primus 880 Weather Radar, HF, CAT II Approach 2nd FMS, RVSM Compliance, FL 350 Electronic Flight Bag, LED lights, SATCOM/WIFi
© 2013 328 Support Services GmbH • www.328.eu • 08-2013
