Jecobra Aviation
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DORNIER 328JET aircraft hero image
Mid-Size Jet

DORNIER 328JET

Manufacturing Years: 1997

$1.0M
Average Sale Price
1
On the Market
12
Passengers
740
Range
$1.0M
Avg. Price
$2,162
Operating Cost/Hr

Performance

Range
740
Cruise Speed
405 knots
Service Ceiling
35,000′
Takeoff Distance
4,285′
Landing Distance
4,485′
Operating Cost
$2,162/hr

Cabin

Maximum Capacity
12 passengers
Length
33' 9"
Width
7' 4"
Height
6' 2"
Cabin Volume
1047 cu ft
Cabin Pressure
7.5 psi
Baggage Volume
261
Galley
Wood plank lav & galley flooring, Wood plank lav & galley flooring
Lavatory
Wood plank lav & galley flooring, Wood plank lav & galley flooring

Avionics & Systems

Engine Model
Pratt & Whitney Canada PW306B
Engine Count
2
Thrust per Engine
6,050 lbs
Fuel Capacity
1,196 gallons
Engine OEM
DORNIER
Avionics System
Dual Honeywell HG20201AC, Smith Industries WL-101 (standby), Honeywell IFCS w/dual IC-800C, Honeywell Primus 2000, Apollo SL-40, Dual Honeywell RCZ-833 w/8.33 MHz spacing, Fairchild/L3, Fairchild/L3, Honeywell IFCS w/dual IC-800C, IFR, Dual, Honeywell HG2021GD, Yes w/SELCAL, Dual Honeywell RNZ-851, Dual Honeywell, AlliedSignal EGPWS, Honeywell RT-950

Weight & Balance

Max Takeoff Weight
34,524 lbs
Max Landing Weight
31,725 lbs
Zero Fuel Weight
28,814 lbs
Basic Operating Weight
21,182 lbs
Max Ramp Weight
34,789 lbs

Operating Costs

Hourly Costs

Fuel Cost
$1,447/hr
Maintenance Cost
$202/hr
Total Operating Cost
$2,162/hr
Cost per Mile
$4.96

Annual Costs

Crew Cost
$205,000/year
Hangar Cost
$81,755/year
Insurance Cost
$11,160/year

Maintenance & Production

Engine Overhaul Cost
$483,330

Market Data

Average Ask Price
$1.0M
On Market
1 aircraft
Avg Days on Market
2032 days
% Fleet on Market
9.1%

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Range Map

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0 nm
Maximum Range
0 nm
Typical Range
0 nm
IFR Range
* Range calculations are approximate and may vary based on payload, weather conditions, and flight profile

Floor Plan

Pilots
Passenger Seat

Cabin Cross-Section

7' 4"
6' 2"
33' 9"
Length
7' 4"
Width
6' 2"
Height
* Floor plan is representative and may vary by individual aircraft configuration

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