Sales Portfolio

Featuring: Sale of (5) MD83 Air Frames and (8) Pratt Whitney JT8D-218 Engines

The MD-83 is a member of the large DC-9/MD-80/MD-90 family of aircraft first delivered as the stage 1 noise compliant DC-9-10 series in 1965, with the latest and last model being the MD-90, first delivered in 1993.The MD-83 is a twin engine, narrowbody, stage 3, two man crew aircraft typically seating 135 passengers in mixed class configuration. Typical range with full passengers at 160,000 lb MTOW is approximately 2500 nautical miles, sufficient for short to medium range domestic operations. The MD-81 and MD-82 typically offer the same capacity at lower weights and with shorter ranges.

Specifications
Type: Twin-turbofan, short/medium-range commercial transport
Powerplant: 2 x Pratt & Whitney JT8D-219 turbofans rated at 93.4 kN (21,000 lb st) each. Fuel Capacity: 26,260 l (6,939 US Gal, 5,778 Imp Gal)
Accommodation: Flight Crew: 2
Passengers: up to 172 Pax
Freight Holds: 3 – forward, center and rear
Dimensions, Wing Span: 32.82 m (107 ft 8 in)
External: Wing Area: 118 sq m (1,270 sq ft) Aspect Ratio: 9.62
Length Overall: 45.06 m (147 ft 10 in)
Maximum Height: 9.02 m (29 ft 7 in)
Wheel Track: 5.08 m (16 ft 8 in)
Wheel Base: 22.07 m (72 ft 5 in)
MD-87: 19.18 m (62 ft 11 in)
Dimensions, Total Cabin Length: 30.78 m (101 ft 0 in) Internal: Maximum Width: 3.07 m (10 ft 3 in)
Maximum Height: 2.06 m (6 ft 9 in) Passenger Deck Area: 89.65 sq m (965 sq ft) Passenger Cabin Vol: 191.9 cu m (6,778 cu ft) Forward Hold: 13.14 cu m (464 cu ft)
Center Hold: 9.80 cu m (346 cu ft)
Rear Hold: 12.54 cu m (443 cu ft)
WEIGHTS: Empty Operating Weight: 18,795 kg (41,437 lb) MTOW (dry engines): 72,600 kg (160,000 lb) Max Zero-Fuel Weight: 55,338 kg (122,000 lb) Max Landing Weight: 63,276 kg (139,500 lb)

Pratt &Whitney’s JT8D and JT8D-200 series engines are one of the most popular modern commercial engines ever made. More than 14,750 of them have been built, amassing more than 673 million hours of reliable service since 1964. A modern derivative, the -200 series, covers the 18,500- to 21,700-pound thrust range and is the exclusive power for the popular MD-80 series aircraft. Since starting service in 1980, more than 2,900 engines have been produced.

Specifications
Type: Two-shaft turbofan Performance Ratings:
T-O Thrust, dry: -209: 82.2 kN (18,500 lb) to 25 deg C
-217: 88.96 kN (20,000 lb) to 25 deg C
-217A: 88.96 kN (20,000 lb) to 28.9 deg C
-217C: 88.96 kN (20,000 lb) to 25 deg C
-219: 93.4 kN (21,000 lb) to 25 deg C
Max Cruise Thrust: -209: 22.0 kN (4,945 lb)
-217, -217A,
-217C 23.31 kN (5,240 lb)
Configuration: No of Fan Compressor Stages: 14
No of Turbine Stages: 4
No of Combustors:
Combuster Type:
Compressor Type:
Cannular Axial flow
Application: -217A/C
-219 MD-81/82/88 and MD-87
MD-82/83/88 and E-8C J-Stars