FOKKER F27-500

FOKKER F27-500

AIRCRAFT SERIAL # 10686

FULLY AIR-CONDITIONED

FOKKER F27-500 AIR-CONDITIONED VINTAGE – 1985

CAPACITY OF AIRCRAFT PAX CONFIGURATION

Max Pax Capacity: 50

Baggage: 10 Lbs each pax

No. cargo space in pax configuration: Nil

Cargo door dimension: 47 x 41 inches

CARGO CONFIGURATION

Max Cargo: Five Tons

RANGE & ENDURANCE

800 Nautical miles plus reserves

5:30 Hours

HOURS AVAILABLE SINCE LAST CHECK

Check ‘B” due in July 2007

Specifications

DIMENSIONS

Aircraft Serial # 10686 Wing Span(ft./m) 95' 1.8" (29 m)

Total Aircraft Hours 16936:55 Length (ft./m) 82' 2.5" (25.02 m)

Total Aircraft Hours since Last C of A: 10:05 Height (ft./m) 29' (8.84 m)

Cable Length(Instrument panel to rear bulkhead)

ENGINES

Manufacturer: Rolls Royce

Model: Dart 552-7R Cabin width (in./cm.) 8' 10" (2.7 m)

Rating wet take off: 2180 Shaft Horse Power Cabin Height (in./cm.) 9' 1.7" (2.79 m)

Take-off dry take off: 2167 Shaft Horse Power Headroom (Seat to Ceiling)

& Maximum Continuous Power: 2167 Shaft Horse Power Front Seats (in./cm.)

Middle Seats (in./cm.)

Recommended TBO (hrs.) 4500:00 Hrs Rear Seats (in./cm.)

Left Engine hours 2089:50 Forward Baggage Door Size (in./cm.)

Rt. Engine hours 1746:35 Aft Baggage/Utility Door Size (in./cm.)

Forward cargo Door Size (in./cm.) 47x41 Inch

PROPELLERS Wheel Base (ft./m): (31' 11.3")

Manufacturer:                                                                 Dowty Rotal                                Wheel Track (ft./mm) 7200 mm (23' 7.5")Number of Blades:                                                          4                                  Type:                                                                            Constant Speed,
                                                                                    Auto feathering, electrical              FUEL CAPACITY
                                                                                    & hydraulically actuated

Diameter 11' 6" (3.5m) TotalCapacity 4100 kg

Left Propeller Hours/Cal. Life 26:10 Useable Fuel 4000 kg

Right Propeller Hours/Cal Life 29:55

WEIGHTS

Ramp Weight Lbs OIL CAPACITY(qts) per engines) 25.0 pints

Gross Take-off Weight 45900 Lbs

Gross Landing Weight 42000 Lbs BAGGAGE WEIGHT & VOLUME

Empty Weight 28894.8 Lbs Volume (ft.³/m³)

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

operating fluids) Aft Compartment

Useful Load 17016 Lbs Forward Compartment Lbs

Zero Fuel Weight 40200 Lbs Aft Compartment A/B Lbs

Performance FUEL CONSUMPTION EACH

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

(TAS at Mid-Cruise Weight) 220 KTS Economy Cruise Power (65%) Lbs/Hr

CRUISE SPEEDS

(TAS at Mid-Cruise Weight) 26000 Ft Long Range Cruise Power (45%) Lbs/Hr

High Speed Cruise Power (75%) 235 KTS

(kts/kmh)

Economy Cruise Power (65%) 220 KTS RAT E OF CLIMB Takeoff Power Continuous Power

(kts/kmh)

(At see Level and Gross Wt.)

Long Range Cruise Power (45%) 205KTS Two Engine (fpm/mpm)

(kts/kmh) Single Engine (fpm/mpm)

CRUISE RANGE STALL SPEED IAS

(Cruising range includes 45 minute Flaps Down Full flaps Kts

reserve at long range cruise power plus allowance, Flaps Up (kts./kmh)

for fuel used during taxi, take-off cruise and descent)

Optimum Altitude 10, 000 SERVICE CEILING(MCP POWER)

StandardFuel Two Engines (100 fpm)

High Speed Cruise Power 1600 LB/HR Single Engine (50 fpm)

Economy Cruise Power 1550 LB/HR TAKE-OFF DISTANCE

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

Long Range Cruise Power 1500 LB/HR temperature, t/o Flaps)

Ground Run ft

Total Distance over 50 ft. Obstacle ft

LANDING DISTANCE Heavy Duty Brakes

(Sea Level, Zero Wind, Standard Temperature)

Ground Run ft

Total Distance over 50 ft. Obstacle ft

ACCELERATE-STOP DISTANCE

(Sea Level, Zero Wind, Standard Max weight ft

Temperature, t/o Flaps)

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	-	-	-
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