BOEING & AIRBUS AIRCRAFT SPARE PARTS OVERSTOCKED SALE AND DISCOUNTED PRICES: January 2014

AIRCRAFT AUXILIARY POWER UNITS

FOR SALE

3C AERO LLC. Is now supporting the MD80, MD82, MD83, MD87, MD88, MD90, and MD95 Series Aircraft. 3C Aero maintains a very large pool of MD80 series rotables in tagged SV serviceable and OH overhauled conditions and expendables in NS new surplus and FN factory new conditions. We keep the rotables pool restocked with fresh tags 8130-3's and Dual Release EASA forms. We try and maintain stock on most of the high failure or critical items for the aircraft. 3C AERO's AOG (aircraft on the ground requirements) is always available for your support and can be reached at

Email: marketing@3caero.com

Phone: 1-405-466-5053

Because of the high demand and low supply for the APU's and Wheels and Brakes for the MD80 Series Aircraft. 3C Aero has purchased a large MD80 series inventory pool of Auxiliary Power Units for the MD80 series aircraft as well as the wheels and brakes. We are offering the APU's and Wheels and Brakes in both Overhauled and Serviceable conditions for outright sale. The parts are tagged in SV and OH condition and in stock ready to ship. If you have any active requirements for spare parts or wheels brakes or APU''s contact us at marketing@3caero.com

We are stocking most major components for the the McDonnell Douglas MD series aircraft including the McDonnell Douglas MD 81, McDonnell Douglas MD 82, McDonnell Douglas MD 83, McDonnell Douglas MD 87, McDonnell Douglas MD 88 aircraft, McDonnell Douglas MD-90, and the McDonnell Douglas MD-95, or Boeing 717 aircraft.

APU'S FOR SALE AND OR EXCHANGE

DC8, DC9, MD-80, MD-81, MD-82, MD-83, MD-87, MD-88, MD-90, MD-95, AND BOEING 717 AIRCRAFT AUXILIARY POWER UNITS ( APU )FOR SALE

MODEL NUMBER GTCP85-98CKB - PART NUMBER 380678-3-1

MODEL NUMBER GTCP85-98DCB - PART NUMBER 3800368-1-1

MODEL NUMBER GTCP85-98DCK - PART NUMBER 381015-1-2

MODEL NUMBER GTCP85-98DHF - PART NUMBER 381276-1

MODEL NUMBER GTCP85-98DHFB - PART NUMBER 381276-3

MODEL NUMBER GTCP85-98DHFA - PART NUMBER 381276-2

MODEL NUMBER GTCP85-98DCA - PART NUMBER 3800362-1

MODEL NUMBER GTCP85-98CKD - PART NUMBER 380678-5-1

MODEL NUMBER GTCP85-98D - PART NUMBER 380256-1-1

SOME SHARED EDUCATIONAL WIKI FACTS ARE BELOW:

MD-81

The MD-81 (or as it was originally known the DC-9 Super 81 or DC-9-81) was the first production model of the MD-80, and apart from the MD-87, the differences between the various long body MD-80 variants is relatively minor. The four long body models (MD-81, MD-82, MD-83, and MD-88) only differ from each other in having different engine variants, fuel capacities, and weights. The MD-88 and later build versions of the other models have more up-to-date flight decks featuring for example EFIS.

MD-82

An Alitalia MD-82

Announced on April 16, 1979, the MD-82 (DC-9-82) was a new MD-80 variant with similar dimensions to those of the MD-81 but equipped with more powerful engines. The MD-82 was intended for operation from 'hot and high' airports but also offered greater payload/range when in use at 'standard' airfields. American Airlines is the world's largest operator of the MD-82, with at one point over 300 MD-82s in the fleet.

Originally certificated with 20,000 lbf (89 kN) thrust JT8D-217s, a -217A-powered MD-82 was certificated in mid-1982 and became available that year. The new version featured a higher MTOW (149,500 lb (67,800 kg)), while the JT8D-217As had a guaranteed take-off thrust at temperature of up to 29 degrees C or 5,000 ft (1,500 m) altitude. The JT8D-217C engines were also offered on the MD-82, giving improved sfc. Several operators took delivery of the -219-powered MD-82s, while Balair ordered its MD-82s powered by the lower-thrust -209 engine.^[4]^[16]

The MD-82 features an increased standard MTOW initially to 147,000 lb (67,000 kg), and this was later increased to 149,500 lb (67,800 kg). Standard fuel capacity is the same as that of the MD-81, 5,840 US gal (22,100 l), and typical range with 155 passengers is 2,050 nautical miles (3,800 km).^[4]^[16]

MD-83

The MD-83 (DC-9-83) is a longer range version of the basic MD-81/82 with higher weights, more powerful engines, and increased fuel capacity.

Powerplant: Compared to earlier models, the MD-83 is equipped with slightly more powerful 21,000 lbf (93 kN) thrust Pratt and Whitney JT8D-219s as standard.

Performance: The MD-83 features increased fuel capacity as standard (to 6,970 US gal (26,400 l)), which is carried in two 565 US gal (2,140 l) auxiliary tanks located fore and aft of the centre section. The aircraft also has higher operating weights, with MTOW increased to 160,000 lb (73,000 kg) and MLW to 139,500 lb (63,300 kg). Typical range for the MD-83 with 155 passengers is around 2,504 nautical miles (4,637 km). To cope with the higher operating weights, the MD-83 incorporates strengthened landing gear including new wheels, tires, and brakes, changes to the wing skins, front spar web and elevator spar cap, and strengthened floor beams and panels to carry the auxiliary fuel tanks. From MD-80 line number 1194, an MD-81 delivered in September 1985, it is understood that all MD-80s have the same basic wing structure and in theory could be converted to MD-83 standard.^[4]

MD-87

In January 1985 McDonnell Douglas announced that it was to produce a shorter fuselage MD-80 development aircraft, designated the MD-87 (DC-9-87), which would seat between 109 and 130 passengers depending upon configuration. The designation was intended to indicate its planned date of entry into service, 1987.

Dimensions: With an overall length of 130 feet 5 inches (39.75 m), the MD-87 is 17 feet 4 inches (5.28 m) shorter than the other MD-80s but is otherwise generally similar to them, employing the same engines, systems and flight deck. The MD-87 features modifications to its tail, with a fin extension above the tailplane. It also introduced a new low drag "beaver" tail cone, which became standard on all MD-80s.

Powerplant: The MD-87 was offered with either the 20,000 lbf (89 kN) thrust JT8D-217C or the 21,000 lbf (93 kN) thrust -219.

Performance: Two basic versions of the MD-87 were made available with either an MTOW of 140,000 lb (64,000 kg) and MLW of 128,000 lb (58,000 kg) or an MTOW of 149,000 lb (68,000 kg) and an MLW of 130,000 lb (59,000 kg). Fuel capacity is 5,840 US gallons (22,100 l), increasing to 6,970 US gallons (26,400 l) with the incorporation of two auxiliary fuel tanks. Typical range with 130 passengers, is 2,370 nautical miles (4,390 km) increasing to 2,900 nautical miles (5,400 km) with two auxiliary fuel tanks.

Cabin: The MD-87 provides typical mixed-class seating for 114 passengers or 130 in an all economy layout (five-abreast 31 in and 32 in seat pitch). The maximum seating, exit limited, is for 139 passengers.

MD-88

The MD-88 was the last variant of the MD-80, which was launched on January 23, 1986 on the back of orders and options from Delta Air Lines for a total of 80 aircraft.

The MD-88 is, depending on specification, basically similar to the MD-82 or MD-83 except that it incorporates an EFIS cockpit instead of the more traditional analog flight deck of the other MD-80s. Other changes incorporated into the MD-88 include a wind shear warning system and general updating of the cabin interior/trim. These detail changes are relatively minor and were written back as standard on the MD-82/83. The wind shear warning system was offered as a standard option on all other MD-80s and has been made available for retrofitting on earlier aircraft including the DC-9.

Delta's earlier delivered MD-82s were upgraded to MD-88 specification. When McDonnell Douglas was asked why these aircraft were MD-88s and not MD-82s they said that the customer, Delta Air Lines, thought that its specification was sufficiently different to warrant a new designation. Although delivered in December 1987, Delta put the aircraft into service only in January 1988.

Performance: The MD-88 has the same weights, range, and airfield performance as the other long-body aircraft (MD-82 and MD-83) and is powered by the same engines. MDC quotes a typical range for the MD-88 as 2,050 nautical miles (3,800 km) with 155 passengers. Range with 155 passenger is increased to 2,504 nautical miles (4,637 km) with two additional auxiliary fuel tanks (similar to the MD-83).

MD-80 Advanced

McDonnell Douglas revealed at the end of 1990 that it would be developing an MD-80 improvement package with the intent to offer beginning in early 1991 for delivery from mid-1993. The aircraft became known as the MD-80 Advanced. The main improvement was the installation of Pratt & Whitney JT8D-290 engines with a 1.5 in larger diameter fan and would, it was hoped, allow a 6 dB reduction in exterior noise.

Due to lack of market interest, McDonnell Douglas dropped its plans to offer the MD-80 Advanced during 1991. Then in 1993 a "mark 2" MD-80 Advanced version reappeared with the modified JT8D-290 engines as previously proposed. The company also evaluated the addition of winglets on the MD-80. In late 1993, Pratt & Whitney launched a modified version of the JT8D-200 series, the -218B, which was being offered for the DC-9X re-engining program, and was also evaluating the possibility of developing a new JT8D for possible retrofit on the MD-80. The engine would also be available on new build MD-80s.

The 18,000 lbf (80 kN) to 19,000 lbf (85 kN) thrust -218B engine version shares a 98% commonality with the existing engine, with changes designed to reduce NOx, improve durability, and reduce noise levels by 3 dB. The 218B could be certificated in early to mid-1996. The new engine, dubbed the "8000", was to feature a new fan of increased diameter (by 1.7 in), extended exhaust cone, a larger LP compressor, a new annular burner, and a new LP turbine and mixer. The initial thrust rating would be around 21,700 lbf (97 kN) thrust. A launch decision on the new engine was expected by mid-1994, but never occurred. The MD-80 Advanced was also to offer a new flight deck instrumentation package and a completely new passenger compartment design. These changes would be available by retrofit to existing MD-80s, and was forecast to enter service by July 1993.

The MD-80 Advanced was to incorporate the advanced flight deck of the MD-88, including a choice of reference systems, with an inertial reference system as standard fitting and optional attitude-heading equipment. It was to be equipped with an electronic flight instrument system (EFIS), an optional second flight management system (FMS), light emitting diode (LED) dot matrix electronic engine and system displays. A Honeywell windshear computer and provision for an optional traffic-alert and collision avoidance system (TCAS) were also to be included. A new interior would have a 12% increase in overhead baggage space and stowage compartment lights that come on when the door opens, as well as new video system featuring drop-down LCD monitors above.^{[5] T}he lack of market interest for the MD-80 Advanced during 1991 led McDonnell Douglas to drop its plans for the development. Derivatives The MD-90-30 is a stretched variant with updated glass cockpit and two V2500 engines, also Extended Range (ER) version as the MD-90-30ER. The MD-95 was developed as a replacement for the earlier DC-9-30, produced as the Boeing 717

The McDonnell Douglas MD-80 series aircraft is a narrow body twin-engine, short- to medium-range, single-aisle commercial jet aircraft operated by leasing companies commercial aircraft freight companies and commercial airliners. The MD-80 series were lengthened, updated and modified from the older legacy DC-9 model aircraft. The airliner family can seat from 130 up to 172 passengers depending on variant and seating configuration. The MD-80 series was introduced into commercial operations and passenger service in 1980 by Swissair.

The McDonnell Douglas MD series includes the McDonnell Douglas MD-81, McDonnell Douglas MD-82, McDonnell Douglas MD-83, McDonnell Douglas MD-87, and McDonnell Douglas MD-88 aircraft. These all have the same fuselage length except the shortened MD-87. The MD-80 series was followed into service in modified form by the McDonnell Douglas MD-90 in 1995 and the McDonnell Douglas MD-95/Boeing 717 in 1999.