CESSNA CARAVAN II F-406

AIRCRAFT SERIAL # 0059

FULLY AIR-CONDITIONED

CESSNA CARVAN-II F- 406 AIR-CONDITIONED                                 VINTAGE-1992

CAPACITY OF AIRCRAFT PAX CONFIGUATION

Max Pax Capacity                                              12

Baggage 10 Lbs each pax

No cargo space in pax configuration Nil

Cargo door dimension 47 x 41 inches

CARGO CONFIGURATION

Max Cargo                                                         One Tons

RANGE & ENDURANCE

700 Nautical miles plus reserves

3 : 50 Hours

Specifications

HOURS AVAILABLE SINCE LAST CHECK

350:00 Hours to HSI on both engines

Aircraft Serial #                                       0059   DIMENSIONS

Total Aircraft Hours                                             4937.5                            Wing Span (ft./m)                                               49.50ft

Total Aircraft Hours since Last C of A                   228.1 Length (ft./m) 39.02ft Height (ft./m)                                                      13.93ft

Cabin Length (Instrument panel to rear bulkhead)

ENGINES

Manufacturer                                                      P & W Canada                                                                                    224.9 Inch

Model                                                                PT6A-112 Cabin width (in./cm.)                                        56.0 Inch

Rating                                                           500 Shaft Horse Power Cabin Height (in./cm.)                                      51.4 Inch

Take off Headroom (Seat to Ceiling)

& Maximum Continuous Power                            500 Shaft Horse Power Front Seats (in./cm.)                                        51.4 Inch 

Middle Seats (in./cm.)

Recommended TBO (hrs.) 4100:00 Hrs Rear Seats (in./cm.) 38.5 Inch

Left Engine hours                                               1346.7                            Forward Baggage Door Size (in./cm.)            50.8 Inch

Rt. Engine hours 1346.7 Aft Baggage/Utility Door Size (in./cm.)  50x49 Inch

Forward cargo Door Size (in./cm.)             290 x 250 Inch

                                                                                                              Wheel Base(ft/m)                                               7.025 ft

                                                                                                              Wheel Tread(ft/m)                                               14.05 ft

PROPELLERS

Manufacturer                                                    MCauley

No of Blade                                                         3

Type Constant Speed,

                                                                         Auto feathering, electrical FUEL CAPACITY

& hydraulically actuated

Diameter 7.75feet                          Total Capacity 481.5 Gallons

Left Propeller Hours/Cal. Life                               905.7  / 01 May 2009       Useable Fuel 475.0 Gallons

Right Propeller Hours/Cal Life                              1282.2 / 05 June 2008

WEIGHTS

Ramp Weight  9925 Lbs           OIL CAPACITY(qts per engines)  9.2Qrts

Gross Take-off Weight                                        9850 Lbs

Gross Landing Weight 4223 Lbs BAGGAGE WEIGHT & VOLUME

Empty Weight                                                    5522 Lbs Volume (ft.³/m³)                                        10.55

(Includes: unusable fuel, full oil and full Forward Compartment                                               25 

operating fluids) Aft Compartment                                                   31.7 

Useful Load                                                       4223 Lbs Capacity(lbs) wing locker each                           200 Lbs

Zero Fuel Weight 8500 Lbs Forward Compartment                                        600 Lbs

Aft Compartment A/B                                         500 Lbs

Performance FUEL CONSUMPTION EACH

MAXIMUM SPEED High Speed Cruise Power (75%)                    303 Lbs/Hr

(TAS at Mid-Cruise Weight) 230 KTS

Economy Cruise Power (65%)                     295 Lbs/Hr

CRUISE SPEEDS 10.000 Ft

(TAS at Mid-Cruise Weight) Long Range Cruise Power (45%)                     190 Lbs/Hr

High Speed Cruise Power (75%) 225 KTS

(kts/kmh)

Economy Cruise Power (65%) 215 KTS RAT E OF CLIMB Takeoff Power Continuous Power

(kts/kmh) (At see Level and Gross Wt.)

Long Range Cruise Power (45%)               181 KTS Two Engine (fpm/mpm) 1400/427               1300/396

(kts/kmh) Single Engine (fpm/mpm)      240/73                   200/61  

CRUISE RANGE                                        STALL SPEED IAS

(Cruising range includes 45 minute reserve at long range Flaps Down Full flaps          75 Kts

cruise power plus allowance for fuel used during taxi, take-off, Flaps Up (kts./kmh)              94.5 Kts                      

cruise and descent)

Optimum Altitude 10, 000 SERVICE CEILING (MCP POWER)

Standard Fuel Two Engines (100 fpm)                            Above 30,000 ft

High Speed Cruise Power                 303 LB/HR Single Engine (50 fpm)  16,200 ft 

Economy Cruise Power                                       295 LB/HR    TAKE-OFF DISTANCE

(Sea Level, Zero Wind, Standard, Max t/o wt

Long Range Cruise Power 190 LB/HR temperature, t/o Flaps)

Ground Run                                                        2179 ft

Total Distance over 50 ft. Obstacle                        2701 ft

PAX CONFIGURATION                                                                   LANDING DISTANCE Heavy Duty Brakes

Max Pax Capacity     : 12                                                                         (Sea Level, Zero Wind, Standard Temperature)

Baggage                   : 10 Lbs each pax                    Ground Roll                                                         1350 ft

No cargo space in pax configuration Total Distance over 50 ft. Obstacle                         2512 ft

PAX CONFIGURATION                                                                   ACCELERATE-STOP DISTANCE

Max Cargo                 : One Ton                                                               (Sea Level, Zero Wind, Standard Max Weight

                                                                                                              Temperature, t/o Flaps)                                        4000 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.

1-     1600 BTU FREON AIR-CONDITION SYSTEM.

2-     HEATING, VENTILATING & DEFROSTING SYSTEM IS PROVIDED THRU ENGINE BLEED AIR.

3-     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