Aircraft Sales Contact:
aircraftsales@dodson.com
 phone:  1 (785) 878-4000
fax:  1 (785) 878-8888
2155 Vermont Road
Rantoul, KS  66079
Habla Espanol?
Aviones o Partes por Venta? Necesita Cotizacion?- pregunte por Lisa,
Ext. 1113
 

 
 
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Turbine Conversion DC3/C47-TP
(several aircraft available)

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(Several Aircraft Available)
950 TT Since IRAN (Inspect and Repair As Necessary)
23,000 Hours since new
U.S. or South African Certification (Standard or Commercial)
ENGINES

PT6A-65AR
Automatic Power Reserve (APR) System (1425 SHP)
LE:  0 Hours Since Hot Section Inspection
914 Hours Since New
S/N:  Various Engine Options Available
RE:  0 Hours Since Hot Section Inspection
1505 Hours Since New
S/N:  Various Engine Options Available

 PROPELLERS
Hartzell HC-B6 MP-3C 5-Blade
LP:  0 Hours Since Overhaul
RP:  0 Hours Since Overhaul

 AVIONICS
Pilot Flight Director System
Century 41 Autopilot System
Bendix Color Weather Radar
Dual Garmin 430 Digital Communication Transceivers
Dual Garmin 430 Digital Navigation Receivers
Dual Garmin 430 GPS
Dual Becker Automatic Direction Finders
Dual RMI Radio Magnetic Indicators
Dual Slaved HSI Horizontal Situation Indicators
Dual IVSI Systems
Dual Turn Coordinators
Dual Audio Control Panels
Dual Marker Beacons
Dual Airspeed Warning Systems
Dual Stall Warning Systems
KT76A Transponder
Collins Radar Altimeter
DME Distance Measuring Equipment
Altitude Preselect System
Slaved Compass
Glideslope
Emergency VHF System
High Frequency Radio

INTERIOR
Seating for Three Crew Members, Various Seating and Configuration Options Available.
Large, Stand-Up Cargo Cabin with Steel Cargo Floor.

The Refreshment Center Features a Coleman Cooler, Hot Box, Wash Basin, Two Storage Drawers, Ice Service, Waste Bin and Dispensers for Cold Water, Coffee, Sugar, Milk and Soup.
The Private Aft Lavatory has a Holding Tank Chemical Toilet. Other Amenities Include a Storage Cabinet Next to Potty Door, and a Belted Fold-Up Frame for a Four-Place Divan.

 EXTERIOR
Overall White. Ready for Accent Striping, personalized to Customer's Color and Style Preference.

UPGRADED FEATURES & MODIFICATIONS
Long-Range Fuel System 1030 Gallons
Digital Fuel Flow Instruments
Shadin Fuel Flow Computer
Electrical and Fuel Management Panel
Aircraft Accessory Systems Panel
Dual Electric Trim Systems
New Cockpit Panels, Instruments, Overhead Panels and Gauges
Century Yaw Damper
New Kaydex Gill Liners
Paratrooper Streamlined Door Modification
Modified Door Jettison System
Standard Double Cargo Door (70" High x 84" Wide)
Cargo Area (420" Long x 78" Wide)
Steel Cargo Floor
Douglas Tie Down Tracks Across Ceiling, Sides and Floor
Power Setup for Cargo Winch
Hot Props
Autofeather System
Prop Sync System
Prop Anti-Ice System
Plumbed for Deice System
Pilot's Clock
Digital OAT System
Static Inverters
Dual 28 Volt Electrical Systems
Auto Start/Abort System
Engine Fire Detection & Extinguishing Equipment
Emergency Hot Bus Modification
Upgraded Heater System
Throttle Quadrant Modification
Slit Rivets (Replaced 2000)
Ground Power Switch Guard
New Window Trim
Paratrooper Jump Lights and Bells
Front-To-Back Intercom System
Central Lock System
Crew Jumpseat with Audio Control Panel
Fourth Audio Control Panel (Next to Cargo Doors)
Three Large Cabinet-Style Storage Bins in Cockpit Area
Cockpit Privacy Door
Dual Map Cases
Crew Sheepskin Covers

TECHNICAL INFORMATION

DESCRIPTION

WEIGHT

MAXIMUM ALLOWABLE TAKE-OFF WEIGHT

13 154 kg

BASIC EMPTY WEIGHT

6 962 kg

2 CREW @ 91 kg

182 kg

EMPTY OPERATING WEIGHT

7 144 kg

MAXIMUM LOAD

6 010 kg

MAXIMUM FUEL LOAD

3 224 kg

MAXIMUM USEABLE FUEL

3 190 kg

MAXIMUM LOAD WITH MAXIMUM FUEL

2 786 kg

VFR RESERVE – 45 min @ 371 kg/hr

272 kg

BURN-OFF

408 kg/hr

TAS

170 kts

AVAILABLE EN-ROUTE FUEL – FULL TANKS EXCL RES

2 918 kg

 

Range versus Load

 

FUEL: KG

ENDURANCE: HRS

RANGE: KM

LOAD: KG

2918

07 hr 08 min

2250

2792

2668

06 hr 33 min

2057

3042

2419

05 hr 56 min

1865

3292

2169

05 hr 19 min

1672

3542

1920

04 hr 42 min

1480

3792

1671

04 hr 05 min

1289

4042

1421

03 hr 28 min

1096

4292

1171

02 hr 52 min

903

4542

922

02 hr 15 min

711

4792

672

01 hr 40 min

518

5042

423

01 hr 02 min

325

5292

BURN-OFF MAY VARY SLIGHTLY WITH ALTITUDE AND CLIMB.

DISTANCES CALCULATED FOR ZERO WIND CONDITIONS


 

GENERAL PARTICULARS

WINGSPAN

95’ 0”/ 28.956  Meters

LENGTH

66’ 9.5”/ 20.3454  Meters

HEIGHT

29” 6”/  8.9916  Meters
(LEVEL POSITION to TOP of FIN)

CARGO COMP. LENGTH

35’ 1.5”/ 10.6985  Meters

CARGO COMP WIDTH. (FLOOR  LEVEL)

7’ 0” (VARIES)/ 2.1336 Meters

CARGO COMP HEIGHT

6’ 6”. (VARIES)/ 1.9812 Meters

CARGO COMP VOLUME

1225 cu ft./34.82 Cubic Meters

FUEL 

TOTAL USEABLE FUEL CAPACITY

1030 U.S. Gallons/ 3897.8 Liters
CRUISE

NOMINAL FUEL CONSUMP@ 26900 Lb. GR. Weight

1000 lb/hr (10,000 ft, ISA)/453.59

WEIGHTS

MAXIMUM WEIGHTS (lbs./kg)
Ramp Weight 29,300 lbs/13290 kg
Maximum Take-Off Weight 29,000/13154
Maximum Landing Weight 28,750/13041
Maximum Weight in Cargo Compartment 11,790/5347.9
Maximum Zero Fuel Weight 26,200/11884

STANDARD AIRPLANE WEIGHTS (lbs.)
Standard Empty Weight 15,710/7125.9
Maximum Useful Load (including ramp fuel) 13,590/6164.3

CARGO SPACE		  
Main Compartment (S.F.) 287.6
Lavatory Compartment (S.F.) 15.0
Cargo Door Size (in. wide x in. high) 84 inches x 56 inches
2.13360x1.42240 Meters

SPECIFIC LOADING		  
Wing Loading (lbs. per sqr. ft.) 28.7/13.018 kilos per S.F.
Power Loading (lbs. per hp) 10.2/4.6266 kilos per S.F.

 

TAKE OFF PERFORMANCE (ISA SL, 29 000 lb GTOW.)

STALL SPEED. (CLEAN)

69 KIAS.

STALL SPEED
            (GEAR + FLAPS, EXTENDED)

64 KIAS.

V1

78 KIAS.

VR

80 KIAS.

V2

86 KIAS.

T/O DIST. (TO 35 ft)

3600 ft

ACC/ STOP DIST

3220 ft

FIRST SEGMENT CLIMB

1.9% Gross Grad.

SECOND SEGMENT CLIMB

4.0% Gross Grad.

EN ROUTE CLIMB. (2000 ft AGL)

2.1% Gross Grad.

 

LANDING PERFORMANCE. ( ISA SL, 26 900 lb GLW.)

APPROACH SPEED VREF.

84 KIAS

LANDING DIST. (50 ft OBSTACLE)

2750 ft. (NO REVERSE POWER)

APPROACH CLIMB

4.0% Gross. Grad.

BALKED LANDING CLIMB

5.2% Gross. Grad.
NOTE:TAKE OFF AND LANDING PERFORMANCE TABLES SHOWN ASSUME
WIND= 0 kts AND RUNWAY SLOPE = 0%.

 

CRUISE PERFORMANCE (ISA, 10 000 ft AMSL, 26 000 lb GW.)

            PERCENTAGE CRUISE  PWR

KTAS

TOTAL FUEL FLOW

100% CRUISE POWER

196 KTAS

1017 lb/hr/ 461.30 kg

80% CRUISE POWER

182 KTAS

884 lb/hr/ 400.98 kg

60% CRUISE POWER

165 KTAS

764 lb/hr/ 346.54

 

RANGE ( 1 Hour Reserve)

POWER SETTING

AMBIENT CONDITIONS

FUEL FLOW

TRUE AIRSPEED

RANGE

60% CRUISE

10000 ft, ISA

764 lb/hr

165 kTAS

1325 nm/3132.38 Kilometers

80% CRUISE

10000 ft, ISA

884 lb/hr

182 kTAS

1240 nm/1995.59 Kilometers

100% CRUISE

10000 ft, ISA

1017 lb/hr

196 kTAS

1133 nm/1823.39 Kilometers

Indicated airspeed at 60% Cruise power = 138 kIAS.

Indicated airspeed at 80% Cruise power = 154 kIAS.

Indicated airspeed at 100% Cruise power = 167 kIAS.

Fuel on climb, @ 29 000 lb AUW, power set to Max Climb, fuel flow as follows:-

1000 ft...................................1151 lb/hr. (522.09 Kg) Total.

3000 ft...................................1103 lb/hr. (500.31 Kg) Total.

5000 ft...................................1076 lb/hr. (488.07 Kg) Total.

8000 ft...................................1042 lb/hr. (472.64 Kg) Total.

11000 ft..................................991 lb/hr. (449.51 Kg) Total.

13000 ft..................................944 lb/hr. (428.19 Kg) Total.

The following information is provided for evaluation purposes only.

Although every attempt has been made to ensure the accuracy of the information contained herein, Dodson International, its Agents and employees accept no responsibility or liability for any claims which may arise, directly or indirectly, from the use or application of this information in any manner. 

CONTACT:
J.R. Dodson at aircraftsales@dodson.com


 The Preceding Preliminary Information Is For Discussion Purposes Only, Is Subject To Verification By Purchaser,
Is Subject To Change Without Notice, And Is Not To Be Considered A Representation Of This Aircraft.
Interested Parties Should Rely Upon Their Own Inspection Of The Aircraft And Its Records.
Aircraft Is Offered Subject To Prior Sale Or Withdrawal From Market.