Long-Range Jet

MCDONNELL DOUGLAS DC-8-72

Manufacturing Years: 1969

Passengers

4,830

Range

N/A

Avg. Price

$12,039

Operating Cost/Hr

Performance

Range

4,830

Cruise Speed

459 knots

Service Ceiling

42,000′

Takeoff Distance

7,700′

Landing Distance

10,500′

Operating Cost

$12,039/hr

Cabin

Maximum Capacity

33 passengers

Length

Width

11' 6"

Height

Cabin Volume

0 cu ft

Baggage Volume

Galley

Mid-cabin bar, fully-equipped galleys & bar, Mid-cabin bar, fully-equipped galleys & bar

Lavatory

Master & aft lav, Master & aft lav

Avionics & Systems

Engine Model

CFM International CFM56-2C5

Engine Count

Thrust per Engine

22,000 lbs

Fuel Capacity

24,275 gallons

Engine OEM

MCDONNELL DOUGLAS

Avionics System

Dual Collins ADF-60A, Dual, Dual Honeywell FZ-500/Pro Line, Dual Collins VHF-21D, Dual Collins DME-40, Dual Honeywell FZ-500, IFR, Dual Universal UNS-1F w/GPS, Dual Collins 628T-1 w/Motorola NA-135 SELCAL, Dual, Triple Litton LTN-92, Dual Collins VIR-31A, Dual Collins ALT-55B, Dual, Universal Aero-I 3-channel, Universal, Collins TCAS-4000, Dual Collins TDR-94D, Collins TWR-850 w/RTA-585 transceiver

Weight & Balance

Max Takeoff Weight

335,000 lbs

Max Landing Weight

240,000 lbs

Zero Fuel Weight

195,000 lbs

Basic Operating Weight

238,547 lbs

Max Ramp Weight

338,000 lbs

Operating Costs

Hourly Costs

Fuel Cost

$10,377/hr

Maintenance Cost

$334/hr

Total Operating Cost

$12,039/hr

Cost per Mile

$29.51

Annual Costs

Crew Cost

$394,000/year

Hangar Cost

$397,341/year

Insurance Cost

$72,419/year

Maintenance & Production

Engine Overhaul Cost

$1,228,000

Market Data

No Current Data Available

Market data for this aircraft is currently unavailable. Please check back later or contact us for the latest information.

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Range Map

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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

Galley

11' 6"

Width

* Floor plan is representative and may vary by individual aircraft configuration

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