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* Lockheed Martin C130H-30 Hercules
* Also known as the L-382G (L100-30)
* Super Hercules
* UN Inspectorate Team ZS-JIZ
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File L382G_UN.ZIP

For FS2002 PRO only due to the B747_400 Panel used.

FS2002 Std Users can use this plane by changing the panel
to one of the freeware C130 panels available on the net

Rev6 redesign with steerable nose gear,
New Props with tips, New LG Doors and
New motion sequences, FS2002 lighting package

New AF99/AA Design & Original artwork by: Barry Blaisdell
email: barrywb@snet.net

UN livery by Bob May
email: wem162@worldonline.co.uk

Visit the Premier Aircraft Design Web Site
http://www.flightsimnetwork.com/premaircraft/
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NOTAM: This aircraft is in FS2002 Format !
NOTAM: AF99 DOES NOT SUPPORT FS2002 LANDING LIGHTS
OR VIRTUAL COCKPITS, OR ROLLING WHEELS...But the rest we got.

FYI, to operate the landing lights - press CTRL L to turn them on or off.

AND ...... in case you're wondering..... the patch of light on the inside of
Engine 1 and Engine 4 at night comes from aimable spotlights in the
forward fuselage. These are used by the crew to check the engines and
wing leading edges for build up of ice.
****************************************************************************

Special Thanks to my longtime friend Jens Borgstroem (Duckling Air)
for creating the Flight Dynamics for this Aircraft.
Visit Duckling Air, the Virtual Airline in Denmark:
http://www.danbbs.dk/~jbdk/duckling/ and
http://www.Duckling-Air.dk/

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Spec's from Jane's "All the Worlds Aircraft" Book
Manufacturer: Lockheed-Martin, Marrietta, Georgia, USA

Type : Medium range freighter


L100-30 / C130H-30 Specifications:

Powerplant:
-----------
L-100-30 - Four 3362kW (4508shp) Allison 501D22A turboprops
driving four blade constant speed propellers.

Performance:
------------
L-100-30 - Max cruising speed 571km/h (308kt). Range with max
payload 2472km (1334nm), range with no payload 8950km
(4830nm). L-100J - Max cruising speed approx 663km/h (358kt).
Range with max payload and reserves 3701km (1998nm)
( External tanks fitted under wings ).
! This version has NO external tanks fitted !

Weights:
-------
L-100-30 - Operating empty 35,260kg (77,736lb), max takeoff
70,310kg (155,000lb). L-100J - Operating empty 34,438kg
(75,923lb), max takeoff 70,310kg (155,000lb).

Dimensions:
-----------
L-100-30/L-100J - Wing span 40.41m (132ft 7in), length 34.37m
(112ft 9in), height 11.66m (38ft 3in). Wing area 162.1m2
(1745.0sq ft).

Capacity:
---------
L-100-30 - Flightcrew of three or four. Max payload of 23,158kg
(51,054lb) comprising pallets or containers.

Production:
-----------
Approximately 40 civil L-100s are in commercial service.



History:
--------
Lockheed's L-100 freighters are the civil equivalents of the
venerable military C130 Hercules, and have proven to be of
immense utility, particularly in undeveloped countries.

Lockheed initiated design of the Hercules in response to a
1951 US Air Force requirement for a turboprop powered freighter.
This resulted in the C130 Hercules, which first flew in prototype
form on August 23 1954.
The USAF ordered the C130 into series production in September 1952,
and since that time 2200 have been built.

The C130's appeal to freight operators led Lockheed to develop a
civil version. The first commercial versions were based on the C130E
model, and a demilitarised demonstrator first flew in April 1964.
This initial civil development, the Model 382, was awarded civil
certification in February 1965. This model was soon followed up by
the 382B, or the L-100, which introduced an improved freight handling
system.

Sales of these initial versions were slow, leading Lockheed to develop
the 2.54m (8ft 4in) stretched L-100-20 (Model 382E), which offered
better freight capacity and operating economics.
The L-100-20 was certificated in October 1968, but was soon followed
by the even longer L-100-30.
The -30 was 2.03m (6ft 8in) longer than the 20, first flew in August
1970, and was delivered from December that year.
Most civil Hercules sales have been of the L-100-30 variant.

The L-100J is a commercial derivative of the new generation C130J
Hercules II. Improvements include new Allison AE 2100 advanced turboprop
engines driving six blade props, two crew EFIS flightdeck and significantly
lower maintenance and operating costs.
The C130J first flew on April 5 1996, while US FAA certification was awarded
in September 1998.
The L-100J is based on the stretched fuselage C-130J-30.

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ALL FILES ARE Copyrighted 2000/2001/2002 by the individual authors.

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Enjoy flying the C130-30 ... The 'Herc way'.

December 2002

Barry Blaisdell

Premier Aircraft Design

Wingspan: 90 FT
Length : 84'-3"
Height : 24.7 FT
Weight : Empty 25,888 lbs / Maximum Take off 43,000 lbs
Speeds : Max Cruise 284 Kts / Stall Speed with Flaps 78kts.
Power : Two 2,500 SHP P&W Canada PW 123B Turboshaft Engines
driving Hamilton-Standard 14SF-23, 4 blade 13 ft Dia Propellers.
Fuel : 835 US Gal ( standard )
Range : 878 Nautical Miles w/50 PAX, standard fuel tanks
1.177 Nautical Miles w/50 PAX, with optional LR fuel tanks
( which is the case with this Q311 model ).
Max Rate of Climb: 1,900 FPM min. at MSL.
Normal Cruise altitude : 15,100 - 16.000 ft acc. to Jane's.
- other sources state alt up to round 20.000ft "
Max. certified Alt.: 25.000 ft

December 2002

Barry Blaisdell

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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
programs, including freeware and shareware, 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 2002 by the author(s).