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BEECH 1900C AIRCRAFT
SERIAL # UC-165 FULLY
AIR-CONDITIONED
BEECH
1900C AIR-CONDITIONED VINTAGE
– 1991 CAPACITY OF AIRCRAFT PAX
CONFIGURATION
Max
Pax Capacity 19 Baggage 10
Lbs each pax No
cargo space in pax configuration Nil Cargo
door dimension 49 x 52 inches CARGO CONFIGURATION Max
Cargo Two Tons RANGE & ENDURANCE 800
Nautical miles plus reserves 3
: 50 Hours HOURS AVAILABLE SINCE LAST CHECK Detail First 10th November, 2007 Specifications
Aircraft
Serial # UC-165 DIMENSIONS Total
Aircraft Hours 12888.3 Wing
Span (ft./m) 54' 6" Total
Aircraft Hours since Last C of A 50.9 Length (ft./m) 57' 10" Height
(ft./m) 14' 11"
ENGINES
Cabin Length (Instrument panel to rear
bulkhead)
Manufacturer
Pratt
& Whitney Model
PT6A-65B Cabin width (in./cm.) 54" Rating 1100
Shaft Horse Power Cabin
Height (in./cm.) 57"
Take-off
3600 Shaft Horse Power Headroom (Seat to Ceiling) Recommended
TBO (hrs.) 6000
Hrs Left
Engine hours 2105.6 Forward Baggage Door Size (in./cm.) nnn Rt. Engine hours 2195.6 Aft Baggage/Utility Door Size (in./cm.) Forward cargo Door Size (in./cm.) 47 x 41 Inch PROPELLERS
Wheel Base
(ft./m)
72.64 cm
Manufacturer Hartzell
HC-B4MP-3A
Wheel Track (ft./mm) 52.32
cm
Number
of Blades 4 Type
Constant
Speed, Full
Feathering, Reversing Counter weighted &
Hydraulically actuated Diameter 109' 5" Total Capacity 4555.6 lbs Left
Propeller Hours/Cal. Life 45.3 Useable Fuel 4497.0 lbs Right Propeller Hours/Cal Life 555.5 WEIGHTS Ramp
Weight 16710 Lbs Gross
Take-off Weight 16600 Lbs Gross
Landing Weight 16100 Lbs BAGGAGE WEIGHT & VOLUME Empty
Weight 10088.6 Lbs Volume
(ft.³/m³) (Includes:
unusable fuel, full oil and full Forward
Compartment operating
fluids) Aft
Compartment
Useful
Load 6899 Lbs Zero
Fuel Weight 14000
Lbs Forward
Compartment Lbs Aft
Compartment A/B Lbs Performance FUEL CONSUMPTION EACH ENGINE
MAXIMUM SPEED
High
Speed Cruise Power (75%) 990
Lbs/Hr
(TAS
at Mid-Cruise Weight) 247
KTS Economy
Cruise Power (65%) 682
Lbs/Hr CRUISE SPEEDS 48 Mac
(TAS
at Mid-Cruise Weight) Long
Range Cruise Power (45%) 612
Lbs/Hr High Speed Cruise Power (75%) 262 KTS (kts/kmh)
Economy
Cruise Power (65%) 252 KTS RAT E OF CLIMB Takeoff
Power Continuous Power (kts/kmh) (At
see Level and Gross Wt.) 3400 3000
Long
Range Cruise Power (45%) 225 KTS Two Engine (fpm/mpm)
2100 (kts/kmh) Single
Engine (fpm/mpm) 800
CRUISE RANGE STALL SPEED IAS
(Cruising
range includes 45 minute reserve at long range Flaps Down Full flaps 89 Kts cruise
power plus allowance for fuel used during taxi, take-off, Flaps Up (kts./kmh) 96 Kts
cruise
and descent) Optimum Altitude 10, 000 SERVICE CEILING (MCP POWER) Standard Fuel Two Engines (100 fpm) 25000 ft High Speed Cruise Power 3121 Torque Single Engine (50 fpm) 11000ft Economy
Cruise Power 2134 Torque
TAKE-OFF DISTANCE (Sea Level, Zero Wind, Standard,
Max t/o wt Long
Range Cruise Power 1652 Torque temperature,
t/o Flaps) Ground
Run 2673 ft Total Distance over 50 ft.
Obstacle 3990 ft
LANDING DISTANCE Heavy Duty Brakes
(Sea Level, Zero Wind,
Standard Temperature)
Ground
Roll
2680 ft
Total
Distance over 50 ft. Obstacle 4000
ft ACCELERATE-STOP DISTANCE (Sea
Level, Zero Wind, Standard Max weight Temperature, t/o Flaps) ft RANGE & ENDURANCE 700
Nautical miles plus reserves 3:
50 Hours HOURS AVAILABLE SINCE LAST
CHECK 350:00 Hours to OPTIONAL EQUIPMENT ON
BOARD. 1600
BTU FREON AIR-CONDITION SYSTEM. HEATING,
VENTILATING & DEFROSTING SYSTEM IS PROVIDED THRU ENGINE BLEED AIR. AIRCRAFT
CERTIFIED FOR FULL ICING CONDITION OPERATION. AVIONICS ON BOARD.
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