1990 BEECHCRAFT 1900C 1
Aircraft Summary
General
Year
1990
Manufacturer
BEECHCRAFT
Model
1900C-1
Serial Number
UC-171
Condition
Used
Description
Fresh Phase I-VI inspection, New paint to customer specifications, other engine available with times from 23K to 26K! Financing Available
Airframe
Total Time
23481.0
Engine Program
Engine Program Notes
P&W PT6A-65B Reverse flow, free turbine engines
Flat rated at 1,1,, SHP each
Engine fire detection system w/ fire extinguishers
Left:
Gas Generator
S/N: 32565
Time Since Overhaul: 4107.7
Time Since HSI: 1039
Power Section
S/N: 32078
Time since Overhaul: 2566.2
Right:
Gas Generator
S/N: 32062
Time Since Overhaul: 3509.2
Time Since HSI: 1562.1
Power Section
S/N: 32463
Time since Overhaul: 4313.9
Engine 1
Engine 1 Time
4107
Engine 1 Time Since
SOH
Engine 1 Time Since HSI/MPI/Mid-Life
1039
Engine 2
Engine 2 Time
3509
Engine 2 Time Since
SOH
Engine 2 Time Since HSI/MPI/Mid-Life
1562
Props
Prop Notes
Hartzell HC-B4MP-3A four bladed propellers
Auto feathering with reverse pitch
Propeller synchrophaser with synch scope
0/397.5 Time since overhaul
Avionics
Avionics/Radios
Comm 1: Collins VHF-22A Transceiver with CTL-22 Control & Antenna
Comm 2: Collins CHF-22A Transceiver with CTL-22 Control & Antenna
Nav 1: Collins VIR-32 with Collins EFD-74 EHSI Indicator
Nav 2: Collins VIR-32 with Collins 331A-3G HSI Indicator
ADF: Collins ADF-60A iwht CTL-62 Control and ANT-60 Antenna
Transponder: Dual Collins TDR-90's w/ Single CTL-92 Control and Antennas
DME: Collins DME-42 with CTL 42 Control (Active/Preset)
DME 2: Collins DME-42 with CTL 42 Control (Active/Hold)
RMI: Dual Collins RMI-30's (pilot) VOR-1/ADF and VOR-2/ADF Switching
Compass System #1: Honeywell/Sperry C-14A-43 with Servo Amplifier
Compass System #2: Honeywell/Sperry C-14A
Altitude Alerter: Bendix King KAS-297A
Inverters: Dual Flight Tronics PC-250's (250 VA)
Pilot's Altimeter: Bendix King KEA-346 Encoding Altimeter
Copilot's Altimeter: IDC Kollsman Standard
Audio System: Dual Beech Systems in Edge Lighted Panel
Dual Cockpit Speakers
Dual Audio Switches
CVR: Fairchild A100S
GPWS Sundstrand Mark VI
Radar Altimeter: Collins ALT-55
Weather Radar: Collins WXR-270
TCAS: King CAS-66A with Radar Display
Cabin Briefer: Heads up technologies momolingual, pedestal mounted
Pilot's Horizon Indicator: Collins ADI-84
Pilot's Directional Indicator: Collins EFD-74 EHSI
Copilot's Horizon Indicator: Collins EFD-74 EHSI
Copilot's Directional Indicator: Collins 331A-3G HSI
Avionics Master Switch
Front Mounted Instruments
Flight Hour Meter
Microphone Key in Pilot and Copilot Control Wheels
Emergency Locator Transmitter
Additional Equipment
Additional Equipment
Landing Gear and Brakes:
Hydraulically actuated tricycle landing gear
Aircraft Braking system: Multiple Disc Brakes on each Main wheel
Main Wheel Tire Size: 22 x 6.75-10 (Tubeless 10 ply rating, high flotation)
Nose Wheel Tire Size: 19 x 6.75-8 (Tubeless 8 ply rating, high flotation)
Systems and Controls
Complete Anti-icing and De-icing includes:
Surface Deicing Boots
Electric Propeller Anti-icing
Engine Anti-Icing
Dual Electrically Heated Windshields
Electrically heated pitot tubes
152 Cu. Ft. Oxygen system with Outlets for Two Cre and Occupants
Yaw Damp & Rudder Boost Equipped
Electric Elevator Trim System with Manual Wheel
Flight Instruments:
Two Airspeed Indicators
Two Sensitive Altimeters
Two Instantaneous Vertical Speed Indicators
Compass(Standby Magnetic)
Outside Air Temperature Indicator
Vacuum Gauge
Deice Pressure Gauge
Flap Position Indicator
Cabin Rate of Climb Indicator
Cabin Altitude and Differential Pressure Indicator
Oxygen Pressure Indicator
Two Fuel Quantity Indicators
Electrical 28 Volt DC System:
Two Engine Starter/Generators (250 AMP-28 Volt)
Triple Fed Bus System with Automatic Load Shedding
Air cooled Nickel-Cadmium Battery(34 Ampere Hour Rate)
Battery Charging Current Sensor (Safety Sentinel)
Solid State Generator Controllers
External Power Receptavle with Cockpit Annunciation and Overvoltage Protection
Automatic Solid State Master Warning and Annunciator control Panel System with Self Test and Dimmer System
Voltmeter/Ammeter
Propeller Anti-Ice Ammeter
All Electrical Circuits have Circuit Protective Devices
Exterior
Exterior Notes
New to Customer specifications
Interior
Interior Notes
Custom Commuter/Corporate Quick Change
Inspection Status
Inspection Status
Fresh Phase I through Phase VI inspection....All life limited airframe components mid time or better
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