|
N146RD
S/N
32897
(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 |
|
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
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. |
