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                                 LAM Airlines Fokker 100
                                    For FS2002 and PRO

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                         Original: BILL ANDERSON/JIM ATKINS
                         Paint: Mario Coelho (mcrabbit@iol.pt)

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                                    Installation
                                    ------------

    Unzip moz2f100.zip  to  the  aircraft  folder  of  your 
    Flight Simulator. 

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                                      Important
                                     ------------

     *** This aircraft is freeware.  Commercial use is forbiden. *************
     *************************************************************************

    Nothing in  these  files will  damage  your  computer
    and authors will accept no liability.
    These files are offered with no warrantees, implied or written.
    ___________________________________________________________________________
     

    


 

    Mario Coelho                                       DEZ 2001






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MODELS and Designs
--------------------

Aircraft designer: JIM ATKINS

AIR MODEL by BILL ANDERSON (ffds)

This F100 air model has been designed for FS200 and PRO edition

512*512pixels textures, full moving parts, transparent cockpit, day and night lights.

AIR FILE: I improve more realistic fly with additional parameters for Joys-ticks with wing 
force and pedals.
Readjustments combined with .air to wich I have added the sections under [Jet Engine] , 
thanks to Patrick Saint-Dizier for some help parameters.




 Enjoy,

 

AIRCRAFT CHARACTERISTICS
------------------------
Length: 116 ft 7 in (35.53 m)
Height:27 ft 11 in (8.51 m)
Wing span: 92 ft 1 in (28.07 m)
Wing area: 998 sqFt
Aspect Ratio: 8.50
Mean Chord: 130 in
Engines: 2 x Rolls Royce TAY 650-15 @ 15,100 lbs st each

MTOW: 98,000 lbs
MLW: 88,000 lbs
Zero fuel weight (this model): 75,640 lb
Fuel capacity: 3,387 USG (22,359 lb) ; 2 wing tanks containing 1278.5 USG each and a center tank containing 830 USG
Total usable fuel: 3,345 USG

Normal cruise settings: Mach 0.754 (075) at FL270, 94 %N1, TAS 450,
fuel flow: FS2000: 3.2 tons/hour or 236 gals/100NM
Long range cruise speed: Mach 0.70
High speed cruise: Mach 0.74
Max cruise speed: Mach 0.75 at 35,000 fts
Max operating speed: 320 Kts or Mach 0.77 (the lowest)
Rough air speed (VRA/MRA): 250 Kts or Mach 0.65
Range with typical payload: 1,300-1,800 NM with IFR reserve
Max cruising alt: 35,000 fts

Stall speeds (at MTOW)
  Clean: 131 Kts
  All down: 86 Kts

LIMITATIONS
-----------
Max speed at which gear may be extended  (VLO ext/VLE): 200 kts
Max landing gear extended altitude: 25,000 ft
Max speed to lower the flaps 8°: 250 kts or Mach 0.50
                       flaps 15 and 25°: 220 kts or Mach 0.45
                       flaps 42° (full): 180 kts or Mach 0.36
Maximum flap extended altitude: 20,000 ft
Max take-off N1: 95.5% ; N2: 103.5% (5 minutes)
Max continuous N1: 95.5% ; N2: 100.5% (unrestricted)

General conditions of tests: ISA (15°C, 1013 hPa at sea level, no wind) ; 98,000 lb at take off (max fuel) ; all speeds are "relative"(IAS)

TAXI, TAKEOFF AND CLIMB
-----------------------
Expect about 50 USG fuel burn for 10 minutes taxi and standby (Idle N1 is 23%, N2 54% and fuel burn 3.5 USG/min)
Flaps positions 0, 8 and 15° are certified for t/o ; normal t/o will be performed with Flaps 8° (1st position) ; flaps 15° should be used for t/o at high elevations and temperatures.
Take-off trim has to be a little bit up (how much will depend on the sensitivity setting of your system)
Apply T/O power (N1 should be 89%, N2 90% and EGT 763°C).
Take off roll (at sea level and ISA conditions) will be about 4,500 ft (35 seconds)
V1 equals Vr and is 140 kts at MTOW in standard conditions
Initial pitch attitude is about 13-15° ; after rotation a maximum positive pitch of 18° is allowed if speed requirements are met (V2+10)
After take off, retract gear, retract flaps at 1000 ft AGL (IAS should be at least 160 kts), decrease pitch attitude to about 10° and let accelerate the aircraft to 250 kts, then adjust ROC (about 3,500 ft initially) to maintain 250 Kts IAS until 10,000 ft (maintaining 90% N1 or decreasing it slightly to reduce the initial ROC)
At 10,000 ft increase N1 to 95%, decrease BA to +6° and let increase IAS to 290 kts ; keep 95% N1 during climb. Normal climb speed is 280-290 kts above 10,000 fts until Mach 0.70. Best rate of climb speed is 250 kts. Climb performance will be degraded above 20,000 fts and you will have to decrease BA from 10° to 6-4° and ROC from 2500 ft/min to 1000-1500 ft/min especially at MTOW and/or high temperature.

Time, covered distance and fuel consumption to FL 350 (ISA conditions, max fuel at engine start), including takeoff
FL     Time     Dist(NM)     Fuel(USG)
---    ----     --------     ---------
100    04:15       14           120
150    06:00       24           185
200    08:00       35           230
250    10:30       52           275
300    13:30       72           315
350    17:15       98           380

CRUISE
------
Cruise speed depend on economic strategy of the company. Real F100 flight computer calculates the right speeds based upon the strategy mode taking into account winds, fuel cost, altitude and weight.
Standard cruise speed of the model is Mach 0.72 at all weights from FL280 through FL340
Fuel economic cruise speed is Mach 0.70 and high cruise speed is Mach 0.74 at FL 320-350
Following are the measured normal cruise values of the model at near MTOW in standard conditions

FL     Mach     TAS(Kts)  Fuel(USG/h)
--     ----     --------  -----------
[Standard] N1=75-76%
280    0.72       428        745
300    0.72       424        690
320    0.72       421        625

[High speed] N1=76-77%
280    0.74       440        760
300    0.74       436        710
320    0.74       432        675

DESCENT
-------
Descent speed schedule is 280 Kts IAS or Mach 0.70 until 10,000 Fts where IAS has to be reduced to 250 Kts.
Descent rate should not exceed 1000 fpm above FL300 and can then be increased to 2000 fpm
Descent thrust will be adjusted to maintain the following settings
- Mach 0.70 until 280 Kts IAS (ROD: 1000 fpm above FL300 / 2000 fpm below)
- 280 Kts to 10,000 Fts QNH
- 250 Kts below 10,000 Fts QNH

Time, covered distance and descent consumption
Measured values at a weight corresponding to 25-30% fuel to 3000 Fts QNH

From FL     Time     Dist(NM)     Fuel(USG)
-------     -----    --------     ---------
340         17:30     105            85
320         15:30      90            75
300         13:30      75            50
280         12:30      70            45

APPROACH PARAMETERS AND FINAL
-----------------------------
For normal approach weights, your normal speed schedule would be as follows:
In the Terminal area, below 10,000 feet: ATC speed limit = 250 kts
Intermediate approach (20-25 NM from touchdown) = 210 kts
At 15 miles back, slow the aircraft to 180 kts
At 10-12 miles back (glide slope alive) select flaps 8° and decrease speed to 160 kts IAS
Intercepting glideslope, select gear down ; descent rate should be 800 fpm without wind.
At about 2000 fts AGL, select 25° flaps and reduce speed to 140 kts ; set full flaps (42°) at 1500 fts AGL and reduce speed to Vref+5 (125 kts) till threshold for a normal landing
Vref at MLW is 120 kts
Note that MLW will be achieved with about 1870 USG fuel remaining in the tanks (55% of the total capacity)

Approach time and fuel consumption (20 NM from touchdown)
Time: about 7-8 minutes
Fuel burn: about 70 USG

IFR DIVERSION
-------------
Fuel consumption for 45 minutes at FL150 and 250 kts IAS: about 400 USG

MAX RANGE (NM) including taxi, t/o, climb and descent (with 45 min IFR reserve i.e 400 USG)
-------------------------------------------------------------------------------------------
FL280: 1600 NM
FL300: 1700 NM
FL320: 1800 NM

