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DeHavilland DHC6-300S Twin Otter
for FS2002 PRO
Royal Nepal Airlines Reg_ID: 9N-ABP

DH6RNA22.ZIP
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FS2002 PRO DHC6-300S TWIN OTTER

DHC6-300S Twin Otter with FULL Moving Parts.
NEW Updated to Rev 6 for FS2002 with new 16 sided fuselage
and new Prop Tips added, All new tail section.
Royal Nepal Airlines Reg_ID: 9N-ABP
All new A/C Design by Barry Blaisdell.
Livery and night textures by Barry Blaisdel
barrywb@snet.net

FS2002 PRO Ver Airfile

Special Thanks to Steve Small for creating
the Flight Dynamics for this Aircraft.
Canberra, Australia
(www.essjay.com)
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NOTAM: This Aircraft is in FS2002 Format
The landing light switch is operated by the CTRL-L Key

NOTAM: SET TAKEOFF TRIM TO NEUTRAL (CENTER)

For all the Key Commands ..Go to the kneepad
in the Aircraft Pulldown of FS2002.
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TO INSTALL: UnZip to your FS2002\AIRCRAFT Folder using
WinZip or similar program making sure the paths option
(Use Subfolders) is turned on.
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NOTAM: This Aircraft is in FS2002 Format
and uses the FS2002 Default Beech KA350 Panel & Sound.

PANEL & SOUNDS

For the BEST Twin Otter Panel on the NET, You can download my
PREMIER PRO PANEL and PRO SOUNDS, which are available from my
Web Site at http://www.flightsimnetwork.com/premaircraft
or from SurClaro or SurClaro.com.....
Read the PROPNL22 INSTALL INSTRUCTIONS
INCLUDED WITH THIS AIRCRAFT
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Aircraft Data:

Wingspan: 65'3"
Length : 53'8"
Height : 19'6"
Weight : Empty 9,7650 lbs / Maximum Take off 12,500 lbs
Speeds : Max Cruise 180 Kts / Normal Cruise 160 Kts KIAS ).
Stall
Speed : Clean - 74 Kts
Dirty - 58 Kts ( with full Flaps )
Power : Two 652 SHP P&W Canada PT6A-27 Turboshaft Engines
driving Hartzell 3 blade 8'-4" Dia Propellers.
Fuel : 400 Gal ( real life )
330 Gal ( FS model - giving room for pax and goods )
Range : 700 Nautical Miles approx.
Rate of Climb: 1,500 FPM at MSL. ( real life )
( FS model - see below )
Ceiling : Approx. 21,000 ft
Normal Cruise Altitude: 5,000-8,000 feet

++++++++++++++++++++++++++++++++++++++++++++++++++++++++
Some FLYING TIPS...By Jens Borgstroem

Speeds:
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Max speed VNE set to: 235 KIAS and 40 Mach
Max Cruise 180 Kts
Normal Cruise 160 Kts KIAS

At FL 210 these are the figures:
N1 = 98 pct approx.
Spd = 172KIAS / .39Mach

Climb rate in FT/min:
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Climb <4.000 = 1.400 - 1.500
Climb 4.000 - 8.000 = 1.200
Climb 8.000 - 14.000= 1.000
Above = 800 - 900

........

Approach ( eg. og std 3* glideslope ):
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approx. 20 NM out - reduce speed to round 150 KIAS
approx. 10NM out - set first flap and reduce to 125 ( comes by itself )
approx. 7NM out - set next flap and reduce to 110
approx. 4NM out - set full flaps and reduce to 90-100, and let the speed
wear off so on final you 'float in' at round 90 over threshold and 83
on touchdown ( on final possibly third notch flaps ).

Slight flare is necessary at touchdown.

On approach she comes in rather flat, like the real bird.

Remember this aircraft has reversed thrust / reversing prop pitch, which
is activated by pressing ( default ) F2 key and hold down.

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ALL FILES ARE Copyright 2001 by the authors.

~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
Nov, 2001

Barry Blaisdell - Premier Aircraft Design
email: barrywb@snet.net
Bob May - Premier Aircraft Design
email: bob@wem162.worldonline.co.uk

Visit Premier Aircraft Web Site
http://www.flightsimnetwork.com/premaircraft/
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LEGAL NOTICE

1. These files are for free use and enjoyment of individual hobby flightsimmers but
the copyright remains with me and any other persons who have contributed to the work.

2. The files should not be altered and cannot be incorporated into other
shareware or freeware programs or published on any electronic or mechanical
media anywhere in the world without my written permission. This includes
CD's or other media offered free, whether as part of a commercial or non-commercial transaction.

3. REPAINTING. You may repaint this aircraft FOR YOUR OWN EXCLUSIVE use
without seeking permission, but if you intend to upload the repainted aircraft to any
web site or bulletin board, including a Virtual Airline site, then contact me first for
permission. I reserve the right to check the files and documentation before publication.

Barry Blaisdell
Contact me by email at: barrywb@snet.net

ALL FILES ARE Copyright 2001 by the author(s).