Dornier 328-300 (Light Jet) - 328.eu

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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)

© 2013 328 Support Services GmbH • www.328.eu • 08-2013

Page 2

+49 8153 88111 2512 [email protected] www.328.eu

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