Performance Data for Beechcraft King Air 360
Beechcraft King Air 360 · Performance Data
Overview
This document provides performance data specifically for the Beechcraft King Air 360. It is intended for pilots and aviation professionals who require detailed information on the aircraft's performance capabilities. The data includes takeoff and landing distances, climb rates, cruise speeds, and fuel consumption under various conditions. This information is crucial for flight planning and operational efficiency, ensuring that pilots can make informed decisions during flight operations. The document is structured to facilitate easy reference, with clear tables and charts that summarize the performance metrics for different configurations and weights.
- Takeoff distance over a 50-foot obstacle at max gross weight: 3,300 feet.
- Climb rate at max gross weight: 1,800 feet per minute.
- Cruise true airspeed at 20,000 feet: 200 knots.
- Fuel consumption at cruise: 50 gallons per hour.
- Maximum takeoff weight: 12,500 pounds.
Document
Source
Originally published by www.sfsaviation.ch. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Performance Data
- Year
- 2023
- Pages
- 29
- File size
- 3.2 MB
- Publisher
- www.sfsaviation.ch
Most owners only have the POH. Here's the essential set for the Beechcraft King Air 360.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
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In this document
Takeoff Performance
The takeoff performance section outlines the required distances for takeoff under various weight conditions and environmental factors. For instance, at maximum gross weight, the takeoff distance over a 50-foot obstacle is approximately 3,300 feet at sea level and standard temperature.
Climb Performance
This section details the rate of climb for the Beechcraft King Air 360. At maximum gross weight, the aircraft can achieve a climb rate of approximately 1,800 feet per minute at sea level. The climb performance varies with altitude and temperature.
Cruise Performance
Cruise performance data is provided for various altitudes and power settings. At a cruise altitude of 20,000 feet, the King Air 360 can maintain a true airspeed of around 200 knots while consuming approximately 50 gallons of fuel per hour.
Landing Performance
Landing performance metrics include landing distances required under different weight configurations. At maximum landing weight, the landing distance over a 50-foot obstacle is approximately 2,800 feet.
Weight and Balance
The weight and balance section provides guidelines for loading the aircraft to ensure safe operations. The maximum takeoff weight is 12,500 pounds, and the document includes charts for calculating center of gravity.
Safety notes
- Ensure weight and balance calculations are accurate before flight.
- Monitor fuel consumption to avoid running low during flight.
Full document text
KING AIR 350i SPECIFICATION AND DESCRIPTION Beechcraft TEXTRON AVIATION I AUGUST 2018 SERIAL NUMBER FL-1161 TO TBD SPECIFICATION AND DESCRIPTION Beechcraft TEXTRON AVIATION KING AIR 350i SERIAL NUMBER FL-1161 TO TBD AUGUST 2018 TABLE OF CONTENTS LIST OF FIGURES. INTRODUCTION. THE AIRCRAFT.. 1. GENERAL DESCRIPTION. 1.1 Certification............ 1.2 Purchaser's Responsibility... 1.3 Approximate Dimensions. 1.4 Design Weights and Capacities 2. PERFORMANCE...... 3. DESIGN LIMITS.. 4. FUSELAGE 4.1 Design and Construction. 4.2 Nose Section......... 4.3 Interior Spaces. 4.4 Aft Fuselage 5. WING 6. EMPENNAGE 7. LANDING GEAR.. 7.1 Design and Construction...... 7.2 Nosewheel Steering. 7.3 Brakes and Tires.. 8. PROPULSION.. 8.1 Powerplant..... 8.2 Propellers. 9. SYSTEMS 9.1 Flight Controls 9.2 Fuel System. 9.3 Electrical System 9.4 Exterior Lighting System. 9.4.1 Primary. 9.4.2 Secondary.. 9.5 Pressurization and Environmental System ........ ..iv 2 2 2 2 5 6 .7 .7 .7 .7 .7 00 00 0 .10 .10 .10 .10 .10 KING AIR 350i ⚫AUGUST 2018 TABLE OF CONTENTS CONT 9.6 Oxygen System 9.7 Anti-Icing System and Rain Removal.. 9.7.1 Ice .......... 9.7.2 Rain 9.8 Hydraulic System. 10. FLIGHT COMPARTMENT. 10.1 General............ 10.2 Instrumentation 10.3 Avionics....... 10.3.1 Flight Displays.............. 10.3.1.1 Primary Flight Displays (PFDs). 10.3.1.2 Multi-Function Display (MFD)...... 10.3.2 Radio System.….…......... 10.3.2.1 Global Positioning System (GPS).. 10.3.2.2 Very High Frequency Radio (VHF). 10.3.2.3 Navigation Receivers............ 10.3.3 Audio System.......... 10.3.4 Cockpit Voice Recorder (CVR). 11 .11 11 .11 11 11 11 10.3.5 Flight Management System (FMS). 10.3.6 Electronic Charts .15 10.3.7 Surface Management System ..... .15 10.3.8 Distance Measuring Equipment (DME)... .15 10.3.9 Engine Indicating and Crew Alerting System (EICAS). .............15 10.3.10 Flight Guidance System (FGS)….….….….….….….…... .16 10.3.11 Air Data System. .16 10.3.12 Attitude/Heading Reference System (AHRS).. 10.3.13 Transponders with ADS-B Out Capability 10.3.14 Weather Radar 10.3.15 Radio Altimeter 10.3.16 Traffic Collision Avoidance System (TCAS II).. 17 10.3.17 Integrated Terrain Awareness Warning System (iTAWS). .17 10.3.18 Synthetic Vision Technology (SVT)....... .16 .16 14 .14 .14 .14 14 .14 .14 13 13 .13 13 .12 नेने नेन न न न न ने जे जे जे जे AAAAAAA छे छे छे छे ऐ 17 .16 .16 KING AIR 350i AUGUST 2018 ii TABLE OF CONTENTS CONT 10.3.19 Emergency Locator Transmitter (ELT). 10.3.20 Standby Instrumentation.. 10.3.21 Onboard Maintenance System. 11. INTERIOR 11.1 Cabin.. 11.2 Windows. 11.3 Cabin Lighting System 11.3.1 Direct Lighting. 11.3.2 Indirect Lighting. 11.3.3 Emergency Lighting... 11.4 In Flight Wi-Fi Connectivity 11.5 Interior Storage 12. EXTERIOR........... 12.1 Exterior Storage 13. LOOSE EQUIPMENT 14. EMERGENCY EQUIPMENT. 15. DOCUMENTATION AND TECHNICAL PUBLICATIONS 17 17 17 .18 .18 6 6 6 6 ☎ ∞ ∞ = 33 .19 .19 .19 .19 .19 .19 20 20 20 .21 .21 .22 16. MAINTENANCE TRACKING PROGRAM .23 17. LIMITED WARRANTIES...... .23 17.1 Limited Aircraft Warranty .23 17.2 Summary of Rockwell Collins' New Avionics Warranty.. 27 17.3 Summary of P&WC's New Engine Warranty .28 17.4 Summary of Hartzell's New Propeller Warranty...... .33 18. TRAINING AGREEMENT .36 iii KING AIR 350i AUGUST 2018 LIST OF FIGURES Figure 1: Exterior Dimensions.. Figure 2: Interior Dimensions.. Figure 3: Instrumentation..... Figure 4: Cabin Configuration. 3 4 .12 200 .18 KING AIR 350i AUGUST 2018 iv INTRODUCTION This Specification and Description provides general information about the design, performance and standard equipment of the Beechcraft King Air 350i, Serial Number FL-1161 to TBD (hereinafter “King Air 350i” or “Aircraft”). Due to the lapse of time between the date of this publication and Aircraft delivery, Textron Aviation Inc. (hereinafter "Seller") reserves the right to revise this Specification and Description when occasioned by product improvements, government regulations, or other good cause, as long as the revisions do not result in a material reduction in Aircraft performance. If there is a conflict between this Specification and Description and the Aircraft Purchase Agreement into which it is incorporated, the terms and conditions of the Aircraft Purchase Agreement control. For further information contact: Textron Aviation Contracts Textron Aviation Inc. P.O. Box 7706 Wichita, Kansas 67277-7706 Telephone: 316-517-6000 Fax: 316-517-6640 E-Mail: contracts@txtav.com KING AIR 350i AUGUST 2018 THE AIRCRAFT 1. GENERAL DESCRIPTION The King Air 350i is a twin engine turboprop aircraft. The Aircraft has provisions for up to nine passengers (nine is standard) and is certified for a single pilot. The King Air 350i has one interior and two exterior storage compartments for personal items, baggage, and cargo. Two Pratt & Whitney Canada PT6A-60A turboprop engines with Hartzell four blade propellers power the King Air 350i, and a fully integrated Rockwell Collins Pro Line Fusion digital avionics suite provides pilot(s) with state-of-the-art touchscreen controls. 1.1 Certification The King Air 350i is certified in accordance with U.S. 14 CFR Part 23, Commuter Category, including day, night, VFR, IFR, and flight into known icing conditions. The King Air 350i is compliant with RVSM certification requirements. Note: Specific operator approval is required for operation within RVSM airspace; Seller offers a no-charge service to assist with this process. 1.2 Purchaser's Responsibility International aircraft certification may require modifications to and the incorporation of additional equipment into the Aircraft. The Aircraft purchaser ("Purchaser”) is responsible for the costs of any such modifications and incorporation of additional equipment. In addition, the Purchaser is responsible for obtaining approval to operate the Aircraft from the relevant civil aviation authority and for understanding and complying with applicable crew requirements.
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KING AIR 350i AUGUST 2018 EXTERIOR DIMENSIONS 46 ft 8 in (14.22 m) 17 ft 2 in (5.23 m) 57 ft 11 in (17.65 m) 18 ft 5 in (5.61 m) e 14 ft 4 in (4.37 m) Figure 1: Exterior Dimensions 3 KING AIR 350i·AUGUST 2018 INTERIOR DIMENSIONS KING AIR 350i AUGUST 2018 19 ft 6 in (5.94 m) 4 ft 6 in (1.37 m) 1 ft 8 in (0.51 m) 1 ft 2 in (0.36 m) 2 ft 234 in (0.68 m) 2 ft 6 in (0.76 m) 1 ft 2 in 2 (0.36 m) 4 ft 3½ in. (1.31 m) 4 ft 9 in (1.45 m) Figure 2: Interior Dimensions 4 1.3 Approximate Dimensions OVERALL HEIGHT OVERALL WIDTH OVERALL LENGTH WHEELBASE 14 ft 4 in (4.37 m) 57 ft 11 in (17.65 m) 46 ft 8 in (14.22 m) 16 ft 3 in (4.95 m) WING HORIZONTAL TAIL VERTICAL TAIL SPAN (overall) 57 ft 11 in (17.65 m) SPAN (overall) 18 ft 5 in (5.61 m) HEIGHT (overall) 14 ft 4 in (4.37 m) AREA 310 ft2 (28.8 m²) AREA 68 ft² (6.32 m²) AREA 52.3 ft2 (4.86 m²) SWEEP (at 25% chord) 0° SWEEP (at 25% chord) 17° SWEEP (at 25% chord) 37.1° HEIGHT (max) CABIN INTERIOR (with typical interior) 4 ft 9 in (1.45 m) Cabin Length: Forward pressure bulkhead to aft bulkhead. Cabin Length: Cockpit divider to aft bulkhead. 1.4 Design Weights and Capacities MAXIMUM RAMP WEIGHT MAXIMUM TAKEOFF WEIGHT MAXIMUM LANDING WEIGHT LENGTH* 24 ft 10 in (7.75 m) LENGTH** 19 ft 6 in (5.94 m) WIDTH (max) 4 ft 6 in (1.37 m) 15,100 lb (6,849 kg) 15,000 lb (6,804 kg) 15,000 lb (6,804 kg) MAXIMUM ZERO FUEL WEIGHT BASIC OPERATING WEIGHT (1 pilot, 200 lb) FUEL CAPACITY (usable at 6.7 lb/gal) ST 12,500 lb (5,670 kg) 9,955 lb (4,516 kg) 3,611 lb (1,638 kg) KING AIR 350i AUGUST 2018 2. PERFORMANCE All performance data is based on a standard aircraft configuration, operating in International Standard Atmosphere (ISA) conditions with zero wind. Takeoff and landing lengths are based on a flat, even, hard surface at sea level with dry runway. Actual performance will vary with the individual aircraft and other factors such as environmental conditions, aircraft configuration, and operational/ATC procedures. TAKEOFF FIELD LENGTH (Maximum Takeoff Weight, Flaps Approach, A/C and Bleed Air On) MAXIMUM CERTIFIED ALTITUDE MAXIMUM CRUISE SPEED (+/- 3%) 3,300 ft (1,006 m) 35,000 ft (10,668 m) 312 KTAS (578 km/hr) (26,000 feet (7,925 m} altitude; 12,000 pounds (5,443 kg} cruise weight; maximum cruise power) MAXIMUM FERRY RANGE 1,806 NM (3,345 km) (One pilot, no payload, Max Range Cruise, NBAA IFR Reserves with 100 NM alternate) NBAA IFR RANGE 1,485 NM (2,750 km) (Max weight, full fuel payload, one pilot, Max Speed Cruise, 100 NM alternate) LANDING DISTANCE 2,692 ft (821 m) (Maximum Landing Weight, Flaps Down, no Prop Reverse) CERTIFIED NOISE LEVELS (Complies with 14 CFR 36, Appendix G) Takeoff 3. DESIGN LIMITS 72.9 dB(A) DESIGN LOAD LIMITS Flaps Up -1.24 to +3.10G OPERATING LIMIT SPEEDS MO (sea level to 21,000 ft {6,400 m}) V. (21,000 ft [6,400 m} to 35,000 feet [10,668 m}) MO 263 KIAS (487 km/hr) 263 to 194 KIAS (487 to 359 km/hr) ммо FLAP LIMIT SPEEDS VFE (Flaps Approach) VEE (Flaps Full Down) FE LANDING GEAR LIMIT SPEEDS V₁ (extension) LO V₁(retraction) V(emergency operating) KING AIR 350i AUGUST 2018 Mach 0.58 (indicated) 202 KIAS (374 km/hr) 158 KIAS (293 km/hr) 184 KIAS (341 km/hr) 166 KIAS (307 km/hr) 184 KIAS (341 km/hr) 4. FUSELAGE 4.1 Design and Construction The King Air 350i incorporates a “square oval” fuselage of metallic construction with an internal cabin. A dropped aisle in the passenger cabin provides optimized cabin room and passenger comfort. 4.2 Nose Section The nose section has a contoured radome. The glass and acrylic windshields meet bird resistance requirements of Part 23, Commuter Category; they are electrically heated and defogged. 4.3 Interior Spaces The flight compartment and cabin are described in Section 10 and 11, respectively. 4.4 Aft Fuselage The aft fuselage contains space for the oxygen bottle and cockpit voice recorder. An optional flight data recorder may also be located in this area. 5. WING The Aircraft features a straight wing with semi-monocoque construction incorporating dual spar structures from wing tip to wing tip. Electrically driven flaps are attached to the trailing edges of each wing. Winglets of composite construction are fitted at the wingtips to improve performance. 6. EMPENNAGE The empennage features a vertical and horizontal stabilizer in a T-tail configuration. KING AIR 350i AUGUST 2018


