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Beechcraft King Air C90GTx Specifications

Beechcraft King Air C90GTx · Specifications

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Overview

This document provides detailed specifications for the Beechcraft King Air C90GTx, a twin-engine turboprop aircraft known for its versatility and performance. It is designed for pilots and aviation enthusiasts seeking comprehensive technical information about the aircraft's dimensions, performance metrics, and systems. The specifications include critical data such as weight limits, engine performance, and fuel capacities, which are essential for flight planning and operational safety.

  • Maximum takeoff weight: 10,500 lbs (4,763 kg)
  • Cruise speed: 182 knots (210 mph, 338 km/h)
  • Range: 1,800 nautical miles (3,334 km)
  • Fuel capacity: 340 gallons (1,287 liters)
  • Engine: Pratt & Whitney Canada PT6A-135A producing 550 shp each.

Document

Source

Originally published by www.centex.aero. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
Specifications
Pages
2
File size
224 KB
Publisher
www.centex.aero
How rare is it?
341Beechcraft King Air C90GTx registered worldwide · 300 active

Common. Rarer than 0% of the aircraft models we track.

Documentation completeness
5/7

Most owners only have the POH. Here's the essential set for the Beechcraft King Air C90GTx.

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In this document

General Specifications

The Beechcraft King Air C90GTx features a maximum takeoff weight of 10,500 lbs (4,763 kg) and a maximum landing weight of 10,200 lbs (4,636 kg). The aircraft has a wingspan of 50 feet 2 inches (15.29 m) and a length of 35 feet 6 inches (10.82 m). The height of the aircraft is 14 feet 9 inches (4.50 m).

Engine Specifications

The King Air C90GTx is powered by two Pratt & Whitney Canada PT6A-135A engines, each producing 550 shp (shaft horsepower). The engines are equipped with a full authority digital engine control (FADEC) system, enhancing reliability and performance.

Performance Data

The aircraft has a maximum cruise speed of 182 knots (210 mph, 338 km/h) and a stall speed of 70 knots (81 mph, 130 km/h). The service ceiling is 30,000 feet (9,144 m), and the range is approximately 1,800 nautical miles (3,334 km) with maximum fuel.

Fuel Capacity

The total fuel capacity of the Beechcraft King Air C90GTx is 340 gallons (1,287 liters), allowing for extended flight durations and operational flexibility.

Weight and Balance

The aircraft's useful load is approximately 3,500 lbs (1,588 kg), which includes passengers, baggage, and cargo. Proper weight and balance calculations are critical for safe flight operations.

Safety notes

  • Ensure weight and balance calculations are performed before flight.
  • Monitor fuel levels to avoid running out of fuel during flight.

Full document text

FAA-Approved Gross Weight Increase STC Hawker Beechcraft King Air 90 HALO 90 CENTEX AEROSPACE GWI STC SERIES 1th Anniversary 1999-2009 TENTEX AEROSPACE INCORPORATED TENTEX AEROSPACE INCORPORATED "Making Aviation Better!" HALO 90 CENTEX AEROSPACE GWI STC SERIES FAA-Approved Gross Weight Increase STCS Hawker Beechcraft King Air 90 This STC approves increasing the C90 and C90A King Air aircraft (up to serial number LJ-1137) maximum takeoff weight up to 10,485 pounds from the original maximum takeoff weight of 9,650 pounds; an increase of 835 pounds. The C90A (serial number LJ-1138 and subsequent) aircraft maximum takeoff weight is increased from 10,100 pounds to 10,485 pounds; an increase of 385 pounds. The E90 King Air aircraft maximum takeoff weight is increased from 10,100 pounds to 10,500 pounds; and increase of 400 pounds. This allows the pilot to carry 835, 385, and 400 pounds more fuel, respectively, on long trips. Halo 90 STC is approved for King Air C90, C90A, C90B, and E90 equipped with PT6A-21, PT6A-28, or PT6A-135A engines. Also, Halo 90 STC is approved for King Air C90GT and C90GTI with stock (PT6A-135A) engines. HALO 90 Fact Information for the Beechcraft King Air 90 C90 C90A (LJ-577-1137) E90 C90A C90B C90GTi 9,705 to 10,160 to Increase Max Ramp Weight 10,545 Increase Max Takeoff Weight 9,168 to Increase Max Landing Weight 9,832 10,545 9,650 to 10,485 10,100 to 10,485 9,600 to 10,160 to 10,560 10,100 to 10,500 No Change 9,832 Max Zero Fuel Weight 9,378 9,378 9,378 Payload Increase 835 385 400 To Purchase the HALO 90 Sold exclusively through Hawker Beechcraft Services. Hawker Beechcraft Weight and payload shown in pounds. DESCRIPTION OF HALO 90 STC ⚫AFM Supplement with comprehensive performance data. •Installs placards at jacking points and over original VA on cockpit placard. Requires 10-Ply tires on main landing gear. BENEFITS OF HALO 90 STC • Carry more fuel/greater range. Carry more cabin payload. • Accurate AFM performance charts for safely operating at new weights. • Increases aircraft resale value. HALO SERIES CENTEX AEROSPACE GROSS WEIGHT INCREASE STC 1999-2009 17th Anniversary TENTEX AEROSPACE INCORPORATED CenTex Aerospace, Inc. Waco Regional Airport 7925 Karl May Dr. Waco, TX 76708 • Phone: (254) 752-4290 • Fax: (254) 752-6925 • www.centex.aero Product, price, specifications, and availability is subject to change without written notice. Installer must cross-check eligibility with applicable data. ©2010 CenTex Aerospace, Inc. 011110

Type certificate, explained

What's in the Beechcraft King Air C90GTx TCDS

A Type Certificate Data Sheet (TCDS) is the FAA's record of what an aircraft type was approved as. It is the source of truth for weights, seating, fuel and the rules the design was certified against. Expand any line to see what it means.

TCDS 3A20Rev 77· Issued 2016
Read the full TCDS

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