Kingair 350


Beechcraft Kingair 350

Le cockpit du 350

Intérieur de C-GJDE

Toutes les commodités!

Voilà les cubes de glace!

Manuel d'aéronef

Description

Manufacturer: Beechcraft Raytheon
Designation: 350
Nickname: SuperKingair
Type: medium-range executive

Dimensions

Length: 46' 8"
Height: 14' 4"
Wingspan: 57' 11"
Cabin width: 54"
Cabin length: 24' 10"
Cabin height: 57"
Cargo door width: 49"
Cargo door height: 52"
Pressure vessel volume: 443 cu. ft.
Cargo area: 303 cu. ft.
Number of Passengers: 11

Weight Limits

Max Ramp Weight: 15 100 lbs
Max Takeoff Weight: 15 000 lbs
Max Landing Weight: 15 000 lbs
Max Zero-fuel Weight: 12 500 lbs
Operating Empty weight: 9 320(JDE)/9 411(RTH)/9 160(WWD) lbs
Max Baggage compartment weight: 550 lbs

Propulsion

No. of Engines: 2
Powerplant: Pratt&Whitney PT6A-60A
Thrust (each): 1050 shp

Performance

Max Cruising Speed: 311 kts
Certified Ceiling: 35 000 ft

Airspeed for safe operation(15 000 lbs)

Takeoff decision speed(V1): 99 KIAS
Rotation speed(Vr):104 KIAS
Takeoff safety speed(V2): 109 KIAS
Takeoff safety speed(V35): 114 KIAS
2-engine best angle of climb(Vx): 125 KIAS
2-engine best rate of climb(Vy): 140 KIAS
1 engine out best angle of climb(Vxse): 125 KIAS
1 engine out best rate of climb(Vyse): 125 KIAS
Intentional 1 engine inoperative speed(Vsse): 110 KIAS
Maneuvering speed(Va): 184 KIAS
Turbulent Air penetration: 170 KIAS
Air minimum control speed(Vmca), Flaps up: 94 KIAS
Air minimum control speed(Vmca), Flaps approach: 93 KIAS
Max Gear extension(Vlo): 184 KIAS
Max Gear retraction(Vlo): 166 KIAS
Max Gear extended(Vle): 184 KIAS
Max Flap extension(Vfe), approach: 202 KIAS
Max Flap extension(Vfe), full down: 158 KIAS
Stall(Full flaps)(Vso): 81 KIAS
Stall(flaps up)(Vso): 96 KIAS
Maximum operating speed(Vmo), sea level-21 000': 263 KIAS
Maximum operating speed(Vmo), 21 000-35 000: 263-194 KIASor M0.58 whichever is lower
Max speed for effective windshield anti-icing: 226 KIAS

Cruise climb speeds

Sea Level-10,000: 170 KIAS
10,000-15,000: 160 KIAS
15,000-20,000: 150 KIAS
20,000-25,000: 140 KIAS
25,000-30,000: 130 KIAS
30,000-35,000: 120 KIAS

Fuel & Oil capacity

Total usable fuel: 539 US g./ 3611 lbs
Main fuel system: 380 US g./ 2546 lbs
Auxiliary fuel system: 159 US g./ 1065 lbs
Total Oil capacity: 16 quarts per engine

Avionics

Collins Pro-Line II includes:
  • Nav: Dual Collins VIR-32
  • ADF: Collins ADF 60A
  • XDR: Dual Collins TDR-94
  • DME: Dual Collins 42
  • MCS: Dual Collins MCS-65 Compass System
  • ALT: Dual Collins ALT-55 Radio Altimeter
  • Radar: Collins WXR-840 Color Radar
  • Dual 750 VA Flite-Tronics PC-17A Inverters
  • Dual Universal Navigation UNS 1C with Universal Navigation Uplink with Third Com VHF 22A
  • King KHF 950 HF System
  • King Mark VI GPWS (Ground Proximity Warning System)
  • Auto-Pilot / Flight Director - Collins APS-651 Auto-Pilot with EFIS-85
  • Three Tube Dual Processor
Five-Inch Flight Director System Includes:
  • EADI - 85 Horizon Indicator
  • EHSI - 85 Course Indicator
  • CHP - 86B Remote Heading/Course Control
  • DPU - 85 and MPU - 85 Display Processors
  • APP - 65 and PCP - 65 Auto-Pilot Control
  • Altitude Pre-Select
  • Vertical Speed Hold
  • Climb / Descent Mode
  • Altitude Hold
  • Indicated Airspeed Hold
  • Yaw Damper
  • Manual Electric Trim
King CAS 66 TCAS I
Jet 2'' Standby Attitude Indicator with PS 835 Power Supply
Shadin Air Data Dedicated to UNS 1 C's GPS System
Pedestal Extension
Dual GTE MagnaStar Digital Telephone
Third King KA91 GPS Antenna and Third Com Antenna for Handheld System
BF Goodrich WX-1000E Stormscope

Optional Exterior Equipment :

Raisbeck Aft Body Strakes
Raisbeck Wing Lockers
Brake De-Ice
Kevlar Avionics Door Ice Shields


ENGINE OPERATING LIMITS

OPERATING
CONDITION
TORQUE
%(1)
MAXIMUM
ITT c
GAS
GENERATOR
RPM % N1
PROP RPM N2
OIL PRESS
PSI(2)
OIL TEMP
(3)(4)
STARTING
---
1000(5)
---
---
0 to 200
-40(min)
IDLE
---
750(6)
62(min)
1050(min)
60(min)
-40 to +110
TAKEOFF
100
820
104
1700
90 to 135
0 to 110
MAX CONT
100
820
104
1700
90 to 135
0 to 110
CRUISE CLIMB
(7)
785
104
1700
90 to 135
0 to 110
MAX CRUISE
(7)
820
104
1700
90 to 135
0 to 110
MAX REVERSE
---
760
---
1650
90 to 135
0 to 99
TRANSIENT
156(8)
850(8)
104
1870(8)
200
0 to 110


(1) Torque limits applies within range of 1000-1700 propeller RPM (N2). Below 1000 propeller RPM, torque is limited to 62%.

(2) Normal oil pressure is 90 to 135 psig at gas generator speeds above 72%. With engine torque below 62%, minimum oil pressure is 60 psig at normal oil temperature(60 degrees to 70 degrees C). During extremely cold starts, oil pressure may reach 200 psi. Oil pressure under 90 psig are undesirable. Under emergency conditions, to complete a flight, a lower oil pressure limit of 60 psig is permissible at reduced power level not ecxeending 62% torque. Oil pressures below 60 psig are unsafe and require that either the engine be shut down or a landing be made at the nearest suitable airport, using the minimum power required to sustain flight. Fluctuations of plus or minus 10 psi are acceptable.

(3) A minimum oil temperature of 55 C is recommended for fuel heater operation at takeoff power.

(4) Oil temperature limits are -40 C and +110 C. However, temperatures between 99 C and 110 C are limited to a maximum of 10 minutes.

(5) This value is time limited to 5 seconds.

(6) High ITT at ground idle may be corrected by reducing accessory load and/or increasing N1 RPM.

(7) Cruise torque values vary with altitude and temperature.

(8) These values are time limited to 20 seconds.






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