Cessna Citation Mustang — Airworthiness Directives

This document provides detailed specifications and descriptions for the Cessna Citation M2, Model 525, specifically for units 525-0900 to TBD. It serves as a comprehensive reference for evaluating the design, performance, and equipment of the aircraft. The document outlines the aircraft's certification, dimensions, weights, performance metrics, structural design, systems, and more. It is intended for use by pilots, maintenance personnel, and aviation enthusiasts seeking in-depth knowledge of the Citation M2. The information is crucial for understanding the operational capabilities and technical specifications of the aircraft, ensuring safe and efficient operation.

• Maximum Takeoff Weight: 10,700 lb (4,853 kg)
• Maximum Landing Weight: 9,900 lb (4,491 kg)
• Maximum Altitude: 41,000 ft (12,497 m)
• Maximum Cruise Speed: 400 KTAS (741 km/h)
• NBAA IFR Range: 1,300 nm (2,408 km)
• Standard Empty Weight: 6,746 lb (3,060 kg)
• Fuel Capacity: 3,296 lb (1,495 kg)