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 PowerCabin 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 FUEL CAPACITY

                                                                          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    OIL CAPACITY(qts per engine)         14.4 Qts.

Gross Take-off Weight               16600 Lbs

Gross Landing Weight               16100 Lbs   BAGGAGE WEIGHT & VOLUME

Empty Weight                                       10088.6 Lbs                   Volume (ft./m)

(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 HSI on both engines

 

 

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.

 

Name of Equipment

Quantity

Manufacturer

Model

i. HF Communication

N/A

-

-

ii. VHF Communication

02

COLLINS

618M-3, 4

iii. ADF

02

ROCKWELL

51Y-7

iv. ILS/VOR (NAV I & II)

02

COLLINS

51RV-5

v. Marker (M.B)

01

COLLINS

51Z4

vi. DME

01

COLLINS

860E-5

vii. Radio Altimeter

01

COLLINS

860F-1

viii. Airborne Radar System

01

BENDIX/KING

ART2000

ix. ATC Transponder

02

HONEYWELL

MST67A

x. Intercommunication

01

COLLINS

-

xi. SELCAL

-

-

-

xii. ELT

01

ARTEX

C406-N

xiii. EGPWS

01

HONEYWELL

MKVI

xiv. TCAS - II

01

HONEYWELL

TPU67A

xv. GPS

01

BENDIX/KING

KLN900

xvi.      P.A. System

01

COLLINS

346D-2B