MCDONNELL DOUGLAS MD-83 Specs refer to the specifications and technical details of the McDonnell Douglas MD-83, a twin-engine, single-aisle jet airliner.
The MD-83 was developed as an improved version of the MD-80 and entered service in 1985. It was designed for short- to medium-haul flights and was widely used by airlines around the world.
The MD-83 specs include the following:
- Length: 45.3 m (148 ft 7 in)
- Wingspan: 32.8 m (107 ft 7 in)
- Height: 9.0 m (29 ft 6 in)
- Maximum takeoff weight: 63,500 kg (140,000 lb)
- Maximum seating capacity: 172 passengers
- Range: 3,060 km (1,900 mi)
- Powered by two Pratt & Whitney JT8D-200 series turbofan engines
The MD-83 was a popular aircraft due to its efficiency, reliability, and low operating costs. It was eventually replaced by the Boeing 717, which offered improved performance and fuel efficiency.
MCDONNELL DOUGLAS MD-83 Specs
The McDonnell Douglas MD-83 Specs encompass various crucial aspects that define the aircraft’s design, performance, and operational capabilities. Here are seven key aspects:
- Length: 45.3 m (148 ft 7 in)
- Wingspan: 32.8 m (107 ft 7 in)
- Height: 9.0 m (29 ft 6 in)
- Engines: Two Pratt & Whitney JT8D-200 series turbofan engines
- Maximum takeoff weight: 63,500 kg (140,000 lb)
- Maximum seating capacity: 172 passengers
- Range: 3,060 km (1,900 mi)
These aspects are interconnected and contribute to the MD-83’s overall efficiency, reliability, and passenger comfort. The aircraft’s relatively compact size and efficient engines enable it to operate on shorter runways and achieve good fuel economy. Its spacious cabin and large seating capacity make it suitable for both short-haul and medium-haul flights. Furthermore, the MD-83’s advanced avionics and flight control systems ensure enhanced safety and navigation capabilities.
Length
In the context of “MCDONNELL DOUGLAS MD-83 Specs”, the length of 45.3 m (148 ft 7 in) is a crucial specification that defines the aircraft’s physical dimensions and has significant implications for its performance and operational capabilities.
- Maximized Cabin Space: The length of the MD-83 allows for a spacious cabin, accommodating up to 172 passengers in a comfortable seating arrangement. This provides airlines with flexibility to configure the cabin layout to meet specific passenger demands.
- Optimized Aerodynamics: The aircraft’s length contributes to its overall aerodynamic efficiency. The extended fuselage reduces drag and improves airflow around the aircraft, resulting in enhanced fuel economy and performance.
- Runway Requirements: The MD-83’s length is within the range that enables it to operate on shorter runways. This versatility allows airlines to utilize the aircraft in a wider range of airports, including regional and smaller hubs.
- Cargo Capacity: The length of the MD-83 provides ample space for cargo storage. The aircraft can accommodate a significant amount of baggage and cargo in its dedicated compartments, making it suitable for both passenger and cargo transportation.
In summary, the length of 45.3 m (148 ft 7 in) is a key aspect of the “MCDONNELL DOUGLAS MD-83 Specs”. It directly influences the aircraft’s cabin capacity, aerodynamic efficiency, runway compatibility, and cargo capabilities, contributing to the MD-83’s overall effectiveness and operational flexibility.
Wingspan
The wingspan of 32.8 m (107 ft 7 in) is a critical aspect of the “MCDONNELL DOUGLAS MD-83 Specs”. It directly affects the aircraft’s aerodynamic performance, stability, and overall efficiency.
The MD-83’s relatively large wingspan contributes to several key advantages:
- Enhanced Lift Generation: The extended wingspan increases the surface area available for lift generation. This allows the aircraft to maintain altitude and maneuver effectively, even at lower speeds.
- Reduced Drag: The optimized wing design minimizes drag by reducing air resistance. This contributes to improved fuel efficiency and extended range, making the MD-83 suitable for medium-haul operations.
- Improved Stability: The wide wingspan provides greater stability during flight, reducing the impact of turbulence and enhancing passenger comfort.
- Increased Roll Control: The extended wingspan provides enhanced roll control, allowing for precise maneuvering and responsive handling, particularly during takeoff and landing.
In summary, the wingspan of 32.8 m (107 ft 7 in) is a vital component of the “MCDONNELL DOUGLAS MD-83 Specs”. It plays a crucial role in the aircraft’s aerodynamic efficiency, stability, and handling characteristics, making it well-suited for a wide range of operating conditions.
Height
The height of 9.0 m (29 ft 6 in) is a crucial aspect of the “MCDONNELL DOUGLAS MD-83 Specs”. It directly impacts the aircraft’s operational capabilities, passenger comfort, and overall efficiency.
The MD-83’s height is strategically designed to optimize several key factors:
- Cabin Comfort: The height of the aircraft provides a comfortable and spacious cabin environment. Passengers have ample headroom and legroom, enhancing their overall flying experience.
- Cargo Capacity: The MD-83’s height allows for a generous cargo hold capacity. The aircraft can accommodate a significant amount of baggage, freight, and other cargo, making it suitable for both passenger and cargo transportation.
- Airport Compatibility: The aircraft’s height is within the range that enables it to operate at a wide range of airports. This flexibility allows airlines to utilize the MD-83 in various locations, including airports with height restrictions.
- Ground Handling: The MD-83’s height facilitates efficient ground handling operations. The aircraft can easily access standard airport infrastructure, such as jet bridges and maintenance facilities.
In summary, the height of 9.0 m (29 ft 6 in) is a vital component of the “MCDONNELL DOUGLAS MD-83 Specs”. It directly influences the aircraft’s cabin comfort, cargo capacity, operational flexibility, and ground compatibility, ensuring its effectiveness and versatility in a variety of operating environments.
Engines
The incorporation of two Pratt & Whitney JT8D-200 series turbofan engines is a defining aspect of the “MCDONNELL DOUGLAS MD-83 Specs”. These engines play a crucial role in the aircraft’s performance, efficiency, and reliability, making them an essential component of the MD-83’s overall design and capabilities.
- Enhanced Performance: The JT8D-200 engines provide exceptional thrust, enabling the MD-83 to achieve impressive takeoff and climb performance. This translates into shorter takeoff distances and reduced time to climb, resulting in improved operational efficiency.
- Fuel Efficiency: The engines are designed to optimize fuel consumption, contributing to the MD-83’s overall economic operation. Advanced design features, such as high-pressure compressors and efficient combustion systems, minimize fuel burn, reducing operating costs and increasing profitability for airlines.
- Reliability and Durability: The JT8D-200 engines have a proven track record of reliability and durability. Their robust construction and advanced materials ensure extended service life, minimizing maintenance downtime and maximizing aircraft availability.
- Reduced Noise and Emissions: The engines incorporate noise-reducing technologies that minimize the aircraft’s environmental impact. By meeting strict noise regulations, the MD-83 is able to operate in noise-sensitive areas, such as near residential communities or airports with stringent noise restrictions.
In summary, the integration of two Pratt & Whitney JT8D-200 series turbofan engines in the “MCDONNELL DOUGLAS MD-83 Specs” is a testament to the aircraft’s focus on performance, efficiency, reliability, and environmental consciousness. These engines are a key factor in the MD-83’s success as a versatile and cost-effective aircraft that has served the aviation industry for decades.
Maximum takeoff weight
The maximum takeoff weight (MTOW) of 63,500 kg (140,000 lb) is a crucial aspect of the “MCDONNELL DOUGLAS MD-83 Specs” as it directly affects the aircraft’s performance, operational capabilities, and safety.
The MTOW represents the maximum weight at which the MD-83 is certified to take off. It is determined by several factors, including structural strength, engine thrust, and regulatory requirements. A higher MTOW allows the aircraft to carry more payload, such as passengers, cargo, and fuel, increasing its overall efficiency and profitability.
The MD-83’s MTOW of 63,500 kg (140,000 lb) enables it to accommodate a maximum of 172 passengers in a typical two-class configuration. It can also carry a significant amount of cargo, making it suitable for both passenger and cargo operations. The aircraft’s powerful Pratt & Whitney JT8D-200 series turbofan engines provide the necessary thrust to achieve takeoff at this weight.
Understanding the MTOW is essential for pilots, airlines, and air traffic controllers. It helps ensure that the aircraft is operated within its certified limits, maximizing safety and efficiency. The MTOW also plays a role in airport planning and infrastructure design, as it determines the required runway length and strength.
Maximum seating capacity
Within the “MCDONNELL DOUGLAS MD-83 Specs”, the maximum seating capacity of 172 passengers is a significant aspect that directly relates to the aircraft’s design, performance, and operational capabilities. It plays a crucial role in determining the aircraft’s overall efficiency, profitability, and suitability for different airline operations.
The MD-83’s seating capacity is a key factor in maximizing passenger revenue. By accommodating up to 172 passengers in a typical two-class configuration, the aircraft allows airlines to offer a higher number of seats and increase their potential earnings. This is particularly important for short- to medium-haul flights, where passenger volume is often high.
Furthermore, the seating capacity directly affects the aircraft’s operating costs. A higher seating capacity means that the aircraft can distribute fixed costs, such as fuel, maintenance, and crew expenses, over a larger number of passengers. This can result in lower operating costs per passenger, making the MD-83 an attractive option for airlines looking to optimize their profitability.
In addition, the MD-83’s seating capacity aligns with the demand for efficient and economical air travel. The aircraft’s size and capacity make it suitable for a wide range of routes, including both high-density and lower-demand markets. This versatility allows airlines to flexibly adjust their capacity to meet varying passenger loads and market conditions.
Understanding the connection between “Maximum seating capacity: 172 passengers” and “MCDONNELL DOUGLAS MD-83 Specs” enables airlines to make informed decisions about their fleet planning and route selection. It also helps them optimize their operations to maximize revenue and efficiency, ultimately contributing to the success of the MD-83 as a reliable and profitable aircraft.
Range
The range of 3,060 km (1,900 mi) is a pivotal aspect of the “MCDONNELL DOUGLAS MD-83 Specs” as it directly influences the aircraft’s operational capabilities, route planning, and market suitability.
- Operational Flexibility: The MD-83’s range enables it to undertake a wide range of short- to medium-haul routes, providing airlines with operational flexibility. It can efficiently connect cities within a region or country, catering to both business and leisure travelers.
- Route Planning: The aircraft’s range allows airlines to optimize route planning by reducing the need for refueling stops. Non-stop flights improve passenger convenience, reduce travel time, and lower operating costs associated with additional landings.
- Market Accessibility: The MD-83’s range opens up new market opportunities for airlines. It can serve underserved or emerging markets where longer-range aircraft may not be economically viable, expanding the reach of air travel and connecting communities.
- Fuel Efficiency: The MD-83’s range is achieved while maintaining fuel efficiency. Its advanced engines and aerodynamic design minimize fuel consumption, resulting in lower operating costs and a reduced environmental impact.
In conclusion, the range of 3,060 km (1,900 mi) is a crucial element of the “MCDONNELL DOUGLAS MD-83 Specs”. It empowers airlines with operational flexibility, efficient route planning, expanded market accessibility, and cost-effective operations. The MD-83’s range has made it a popular choice for airlines worldwide, enabling them to connect passengers and facilitate commerce across diverse regions.
FAQs on “MCDONNELL DOUGLAS MD-83 Specs”
This section addresses frequently asked questions related to the specifications and capabilities of the McDonnell Douglas MD-83 aircraft. By providing concise and informative answers, we aim to clarify common concerns and misconceptions surrounding this aircraft’s technical aspects.
Question 1: What is the maximum takeoff weight of the MD-83?
Answer: The maximum takeoff weight of the MD-83 is 63,500 kg (140,000 lb). This weight limit determines the maximum payload capacity, including passengers, cargo, and fuel, that the aircraft can carry during takeoff.
Question 2: What is the range of the MD-83?
Answer: The MD-83 has a range of 3,060 km (1,900 mi). This range allows the aircraft to operate on short- to medium-haul routes, providing flexibility in route planning and market accessibility.
Question 3: What type of engines power the MD-83?
Answer: The MD-83 is equipped with two Pratt & Whitney JT8D-200 series turbofan engines. These engines provide the necessary thrust for takeoff and efficient operation throughout the flight.
Question 4: What is the maximum seating capacity of the MD-83?
Answer: The MD-83 has a maximum seating capacity of 172 passengers in a typical two-class configuration. This capacity allows airlines to maximize passenger revenue and optimize operating costs.
Question 5: What is the wingspan of the MD-83?
Answer: The wingspan of the MD-83 is 32.8 m (107 ft 7 in). This wingspan contributes to the aircraft’s aerodynamic efficiency, stability, and overall handling characteristics.
Question 6: What is the height of the MD-83?
Answer: The height of the MD-83 is 9.0 m (29 ft 6 in). This height provides ample headroom and legroom for passengers, ensuring a comfortable cabin environment.
In summary, the “MCDONNELL DOUGLAS MD-83 Specs” provide detailed information on the aircraft’s performance, dimensions, and capabilities. Understanding these specifications is crucial for airlines in optimizing their operations, route planning, and overall efficiency.
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Tips on Utilizing “MCDONNELL DOUGLAS MD-83 Specs”
The “MCDONNELL DOUGLAS MD-83 Specs” provide valuable insights for various stakeholders involved in aircraft operations and management. Here are a few tips to optimize the use of these specifications:
Tip 1: Understanding Performance Parameters
Thoroughly familiarize yourself with the aircraft’s performance specifications, including takeoff weight, range, and fuel consumption. This knowledge is crucial for efficient flight planning, payload optimization, and route selection.
Tip 2: Weight and Balance Calculations
Accurate weight and balance calculations are essential for safe and efficient aircraft operation. Utilize the MD-83’s weight and balance data to determine the allowable payload and ensure proper distribution of weight within the aircraft.
Tip 3: Route Planning and Optimization
Plan flight routes with consideration for the MD-83’s range and performance capabilities. Optimize routes to minimize fuel consumption, reduce operating costs, and enhance passenger comfort.
Tip 4: Maintenance and Inspection Schedules
Adhere to the recommended maintenance and inspection schedules outlined in the MD-83’s specifications. Regular maintenance ensures the aircraft’s airworthiness, reliability, and longevity.
Tip 5: Crew Training and Familiarization
Provide comprehensive training for flight crews to ensure their thorough understanding of the MD-83’s systems, procedures, and performance characteristics. This training enhances safety and optimizes aircraft utilization.
Summary:
By incorporating these tips, aviation professionals can effectively utilize the “MCDONNELL DOUGLAS MD-83 Specs” to maximize the aircraft’s performance, safety, and efficiency. These specifications serve as a valuable resource for informed decision-making, ensuring optimal operations and passenger satisfaction.
Conclusion
The “MCDONNELL DOUGLAS MD-83 Specs” provide a comprehensive overview of the aircraft’s design, performance, and capabilities. These specifications are crucial for airlines, pilots, and aviation professionals to optimize the MD-83’s utilization and ensure its safe and efficient operation.
The MD-83’s well-balanced specifications, including its spacious cabin, efficient engines, and reliable systems, have made it a popular choice for short- to medium-haul operations. Its versatility, cost-effectiveness, and passenger comfort have contributed to its success in the aviation industry.
Understanding and leveraging the “MCDONNELL DOUGLAS MD-83 Specs” enables stakeholders to plan effectively, optimize routes, ensure proper weight and balance, conduct efficient maintenance, and provide adequate crew training. By utilizing these specifications, aviation professionals can maximize the MD-83’s potential, enhancing safety, improving operational efficiency, and ensuring passenger satisfaction.