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DC3/C47 65ARTP:
DC3/C47 65ARTP:
About
Application
History
Specs
Special Engineering
DC3/C47 65ARTP Support:
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Parts
Training
PERFORMANCE:

TAKE OFF PERFORMANCE

ITEM

AMBIENT CONDITIONS

DC3/C47-65ARTP

 

Maximum Weight at Take Off Climb Weight Limit

ISA SL

29000 lbs

 

+30°C @ SL

28500 lbs

 

+20°C @ 4000 ft

26300 lbs

 

Take Off Brake Energy Weight Limit

Special Note: The DC3/C47-65ARTP does not have a Take off Brake Energy Weight Limitation.

ISA SL

N/A

 

+30°C @ SL

N/A

 

+20°C @ 4000 ft

N/A

 

Take Off Distance to 35 ft, at Maximum Take Off Climb Weight Limit

ISA SL

4500 ft

 

+30°C @ SL

4800 ft

 

+20°C @ 4000 ft

5200 ft

 

Accelerate/Stop Distance, at Maximum Take Off Climb Weight Limit

ISA SL

4500 ft

 

+30°C @ SL

4200 ft

 

+20°C @ 4000 ft

4400 ft

 

LANDING PERFORMANCE

Landing Distance (Over 50 ft Obstacle)

ISA SL

3200 ft

 

+30°C @ SL

3450 ft

 

+20°C @ 4000 ft

3400 ft

 

OPERATIONAL LIMITATIONS:

AIRSPEED LIMITATIONS

ITEM

AMBIENT CONDITIONS

DC3/C47-65ARTP

 

VMO  (Maximum Operating)

 

170 KIAS

 

V(Manoeuvring)

 

107 KIAS

 

VLO  (Landing Gear Operating)

 

141 KIAS

 

VLE  (Landing Gear Extended)

 

141 KIAS

 

VFE  (Flap Extended ¼ )

 

133 KIAS

 

VFE  (Flap Extended ½ )

 

97 KIAS

 

VFE  (Flap Extended ¾ to Full)

 

95 KIAS

 

Maximum Demonstrated Cross Wind Component

 

13 Kts

 

Maximum Tail Wind Component

 

10 Kts

 

VMCA  (Minimum Control Speed Air)

 

67 KIAS

 

VMCG  (Minimum Control Speed Ground)

 

60 KIAS

 

WEIGHT LIMITATIONS

Maximum Ramp Weight

 

29300 lbs

 

Maximum Take Off Weight

 

29000 lbs

 

Maximum Landing Weight

 

28750 lbs

 

Maximum Zero Fuel Weight

 

26200 lbs

 

FUEL QUANTITY

Total Fuel Quantity (Standard)

 

7006 lbs

 

Useable Fuel Quantity (Standard)

 

6932 lbs

 

Total Fuel Quantity (Standard + Optional Wing Tanks)

 

12092 lbs

 

Useable Fuel Quantity (Standard + Optional Wing Tanks)

 

12004 lbs

 

MISCELLANEOUS

Center Of Gravity Range

 

13 % to 28 % MAC

 

Maximum Certified Altitude

 

24000 ft

 

Minimum Crew

 

2 (pilot and co pilot)

 

Noise Characteristics

 

No acoustical change was shown under provisions of FAR 21.93 (b)

 

Operating Temperature Limits

 

-40°C to ISA +35°C

 

TECHNICAL DATA:

ITEM

DC3/C47-65ARTP

 

ENGINES

   

Make and Model

Pratt and Whitney Canada, PT6A-65AR

 

Take Off Power

1424 SHP up to 82°F
SFC:- 0.509 lb/SHP/hr

 

Alternate Take Off Power

1230 SHP up to 84°F
SFC:- 0.521 lb/SHP/hr

 

Maximum Continuous Power

1165 SHP up to 101° F
SFC:- 0.522 lb/SHP/hr

 

Maximum Climb and Cruise Power

956 SHP up to 85° F
SFC:- 0.552 lb/SHP/hr

 

Engine Dry Weight

486 lbs

 

PROPELLERS

Make and Model

Hartzell
HC-B5MP-3C/M10876

 

FUSELAGE EXTENSION

Fuselage extension length

40 inch

 

WINGS

Centre wing re-inforcement

Incorporated

 

Wing tips

Modified wing tips

 

TECHNICAL DATA:

ITEM

DC3/C47-65ARTP

 

HYDRAULIC SYSTEM

Engine driven pumps

Gear type engine driven pumps, continuous operation, hydraulic pressure unloading accomplished by standard Douglas hydraulic pressure regulator

 

FLIGHT CONTROL SYSTEM

Control Surfaces (See Note 2)

Covered with Ceconite 101

 

Stability Augmentation System

Electronically controlled Stability augmentation servo and tension spring

 

ELECTRICAL SYSTEM

Starter/Generators

250 Amp

 

Batteries

Two 38 A/H 28 Volt Batteries

 

Electrical Distribution System

Nine bus system with Essential and Emergency Busses and crew selected bus tie capability

 

DE-ICING EQUIPMENT

Engine intake

Full de-icing system installed

 

Propellers

Full de-icing system installed

 

Pitot Heaters

Anti-icing system installed

 

Wing and empennage de-icing

System optional.  Bleed air can be supplied from engine.

 

ITEM

DC3/C47-65ARTP

 

FUEL SYSTEM

Additional fuel tanks (Standard Configuration)

Two Main fuel tanks installed, 125 US Gallons each

 

Fuel quantity indication system

Capacitance Probes and indicators

 

Transfer pumps

Four electrically driven

 

Transfer pump interconnection system

Interconnection system installed to provide fuel transfer capability with a single operable transfer pump.

 

Fuel booster pumps

Four electrically driven

 

ENGINE FIRE EXTINGUISHER SYSTEM

Number of fire extinguishers

Four, two per engine

 

WHEEL BRAKES

Type of Wheel Brakes installed

Goodyear single floating disc brakes

 
For more information, see the downloads section
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