Dimensions:
Length 152' 7" 152' 7"
Wing Span 107'10" 107'10"
Max Height 30' 7" 30' 7"
Weights (lbs):
Empty 88,000 91,900
Fuel 39,306 51,285
Payload 38,250 33,500
MTOW 156,000 172,500 Max Take-off Weight
MLW 142,000 150,000 Max Landing Weight
MZF 130,000 135,000 Max Zero Fuel Weight
Engines:
MD-90-30
- 2*111.1kN International Aero Engines V2525-D5 Turbofans (2*25,000
lb) thrust
MD-90-50
- 2*124.44kN International Aero Engines V2528-D5 Turbofans
(2*28,000 lb) thrust
Operating Performance: MD-90-30/-50
- Vno/Mno 340/0.76 Mach Normal Operating Speed
- Mmo 0.84 Mach Max. Operating Speed
- Vne/Mne 499/0.90 Mach Never Exceed Speed
- Vat 138-140 knots Landing @ Runway Threshold Speed @ MLW
full flap/Gear down
* DO NOT Exceed 250kts @ or
Below 10,000ft Altitude.*
Take-off speed@ MTOW:
- V1 135-140kts @ flap2/3 (V1 is the go or no-go decision speed)
- VR 140-145kts (VR is the rotation speed ie lift-off speed)
- V2 150-160kts (V2 is the safe climb-out speed)
MD-90-30 MD-90-50
V2 155 155
Vat 140 140
Econ Cruise 438/FL350 438/FL350
Range nm 2,085 3,022
ILS & Approach speed @
MLW:
- 180 kts Flap2 (Kyb 2) to full flap/gear down @ Vat 133 -
140 kts
- Vat = 1.30 Vso (Vso is stall speed @ full flap/gear down)
Cruise Speeds:
- Max. Cruise speed 499 KTAS @ cruise altitude 30,000 - 35,000ft
depending on weight
- Long Range Cruise speed 439 KTAS Cruise Altitude 30,000 -
35,000ft depending on weight.
- Typical Cruise Speed is 0.76 - 0.82 Mach @ FL300 - FL350
When flying long routes (over 2hrs) with MTOW, climb to FL300
& hold Alt with cruise speed 0.78 - 0.80 Mach , then fly that
level for 30 min. then climb to FL310 - 320 @500 fpm and so on
until you reach FL350 @ 0.78 - 0.82 Mach
Try not exceed 91% N1 during cruise in order to have available
thrust for emergencies & be more efficient with fuel burn.
The reason I mentioned the above procedure with X-Plane is to
avoid too much nose pitch up attitude which put the aircraft wing
@ higher angle of attack causing speed bleed leading to a clean
stall if you are not careful.
The time taken between cruise climb is important because the
aircraft will burn fuel (losing weight), your speed will gradually
increase @ the same N1 setting , your aircraft pitch up will decrease
helping you for the next cruise climb. Rate of climb at these
alts should be between 300-500 fpm in order not to lose speed
rapidly. The more you climb to FL350 the more the air density
is less the better the engine fuel consumption (more range)&
the less is thrust.
I usually output data for N1 on the screen & switch the
EICAS to fuel management to observe aircraft status on fuel burn
& range.
You should carry fuel enough for the flight + 40mins for diversions
& emergencies i.e. if your trip is 2hrs long, you load fuel
for the required 2hrs flight plus fuel for an extra 40 min. You
should know your aircraft's average fuel consumption for the type
of engines fitted with in order to determine the fuel weight required
for the flight. Remember that weight is drag, drag is more fuel
burn which costs money (for virtual pilots flying for virtual
airlines:), so do not carry fuel more than you need. You have
a destination to go to & MLW limit. You do not want to arrive
to your destination with total weight above MLW!.
FAR Field Lengths
Take-off Landing
MD-90-30 7,000 ft 5,130 ft
MD-90-50 7,700 ft 5,340 ft
Take-off Check List
- Allowable Take-off Weight (MTOW or lower) Checked
- Flaps Set
- Trim Set
- Autopilot Controls Off
Final Landing Check List
- Gear Down/Green
- Flaps/Slats Set/ 3 or 4
- Speed Brakes Armed (shift-8)
- ILS freq/Glide Slope Tuned
During Descent Check
- Check Allowable Landing Weight (MLW 210,000 lb. or lower)
- Review your ILS approach & Runway heading
ROC Rate Of Climb
Below 10,000ft
- max. 4000 fpm @ 250kts (fpm is Feet per minute)
* DO NOT Exceed 250kts @ or
Below 10,000ft Altitude.*
Above 10,000ft to Cruise Flight Level FL
- 2200fpm from 10,000 - 20,000ft @ 280 - 340kts
- 1800 - 1500fpm from 20,000 - 26,000ft
- 1400 - 500fpm from 26,000 - 35,000 ft depending on weight.
ROD Rate Of Descent
- From Cruise FL to 10,000ft hold 0.79 Mach until 290 kts,
reduce thrust for 2500 fpm
- Below 10,000ft rate of descent varies with ATC requirements,
but is between 800 - 3000fpm
- In normal conditions 250kts idle descent , then slow &
configure speed so as to not add power until on Glide Slope.
- Glide Slope descend is between 1500 - 500fpm depending on
your situation
- At Runway Threshold descend between 400 - 200fpm for a smooth
touchdown landing.
MLW = Maximum Landing Weight
MTO = Maximum Take-off Weight
V2 = Safe Climb-out speed (The speed after Vr, Rotation speed or Lift-off speed)
Vat = Landing speed at runway threshold Flap/Gear down (X-Plane @ 50'...25'...10')
Vapr= Approach Speed , just add 5-10kts to Vat with flap/gear down @ MLW or less
Vno = Normal Operating Speed
Vmo = Maximum Operating Speed
Vne = Never Exceed Speed
FL350 = Flight Level 35,000'
Thanks to Mohammed Gazzawi, Designer/Test Pilot MGXP
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