Tupolev Tu134
Type  Airliner 

Author(s)  Emmanuel Baranger (3D/FDM), Buckaroo (FDM), Cossack90 (Liveries, Translation) 
FDM  YASim 
aircraft=  tu134 
Status  Early production 
FDM  
Systems  
Cockpit  
Model  
Development repository 
The Tupolev Tu134 (NATO reporting name: Crusty) is a twinengined airliner, similar to the French Sud Aviation Caravelle and the laterdesigned American Douglas DC9, and built in the Soviet Union from 1966–1984. The original version featured a glazed nose design and, like certain other Russian airliners (including its sister model the Tu154), it can operate from unpaved airfields.
Contents
Variants
 Tu134A (glass nose)
 Tu134B (solid nose)
 Tu134UBL (long nose)
Simplified procedures
Taxiing
 For begin moving use up to 86% N2 a short time.
 Normal taxiing at 6266% N2 depending weight.
 In turns use 6870% N2.
 Maximum taxiing speed 35 km/h and 1015 km/h in turns.
Takeoff
At MTOW
 Flaps 10 (20)
 N2 9899.5% (full throttle, no more 5 min)
 Elevator trim  1.5 degrees up
 Switch landing lights ON.
 At 270 km/h up nose (pitch about 1012 degrees, angle off attack 68 degrees, pull yoke about 1/2 it move range) and plane will take off at speed about 290 km/h.
 Maximum ground speed for nose gear 310 km/h and 330 km/h for main gear.
 After hight 5m and positive climb retract gear.
 After 50m(night),200m(day) switch landing lights OFF.
 After hight 120m and speed not less 330340 km/h retract flaps to 0 degrees.
 390400 km/h  reduce throttle to nominal value 91.593.0 % N2.
 Accelerate to 500 km/h (460 km/h if need noise reduction procedure)
 Climb to altitude 3000 at 500480 km/h,from 3000m to 6000m at 480460 km/h,then reduce speed by 5 km/h per 1000m.
 Time to reach 9100M  21 min.
 Time to reach 10600M  26 min.
Cruising
At cruising altitude accelerate to desired speed at 91.593.0 % N2. Acceleration time to 0.82M with 93% N2 at 10 600M after reach 10 600M about 10 minutes.
Altitude meters  N2 (%)  IAS (km/h)  M  TAS (km/h)  Fuel flow (kg/h) 

9 600  90  520  0.75  820  2600 
10 600  91  500  0.78  830  2300 
10 600  93  515520  0.81  855860  2600 
At 10 600M
N2 (%)  IAS (km/h)  Mach  TAS (km/h)  Pitch degree  Angle of attack  Fuel flow (kg/h) 

89  452  0.71  760  2.7  4.2  2050 
90  460  0.72  770  2.0  3.7  2200 
91  500  0.78  830  1.7  3.2  2450 
92  525  0.81  865  1.5  3.0  2700 
93  530  0.82  875  1.5  3.0  2950 
Note: At 93% N2 plane will increase it maximum speed limit.
Descending
 Reduce trottle to 8183% N2 and begin descend 1012 m/sec at 0.80.82M while reach 600 km/h,
 than maintain this speed.
 Above 8100m maintain 83% N2 or more. Pitch 1 2 degree.
 Below 8100m to 5000M one engine 81% N2 and another 7568% N2(if practicable).
 Below 5000m reduse trottle to 61.772.0% N2 or idle.
 Below 3000m speed less than 460 km/h and vertical speed less than 15 m/sec.
EMERGENCY Descending
 Trottle  Idle (61.763% N2), pitch 1015 degree negative, gear down.
 Speed 600 km/h, 0.82M. Vertical speed 3050m/sec.
 While ending this mode plane drop 400500m of altitude.
 After emergency descend do not retract gear.
Approuching
 Typical speed 380400 km/h at clean plane, and 7885% N2 and 8588%N2 with gear down.
 Gear down and extend flaps to 20 degree at 360340 km/h, 8688 N2.
 At 300320 km/h flaps 30 degree.
 Before intercept glideslope flaps 30, gear down, speed 280300 km/h.
 When intercept glideslope decrease throttle to 8183% N2.
 In glideslope use 8086% N2 (7582% N2 in case small weight)
Weight (kg)  Speed (km/h) 

43000  275285 
40000  267280 
35000  252265 
33000  250260 
Optimal angle off attack 4.56 degrees.
Landing
 At 60 m AGL disengage autopilot.
 At 20 m AGL begin decreasing vertical speed and at 10 m AGL vertical speed must be about 3m/s
 At 7 m AGL smoothly up nose to create 12 degree pitch and begin flare.
 While flare increase pitch to 34 degrees if nessesary to maintain vertical speed less than 1m/s.
 Smoothly set throttle to idle and touchdown.
 Apply spoilers. After nose gear touchdown activate reversers.
 At 250 km/h apply breaks.
 Usually reversers off at 110 km/h, but if nesessary it may be used to full stop.
 Typical touchdown speed = GS Speed  20 km/h.
Notes
 Using more than 2.5 degree pitch when flare will result plane up and quickly drop speed with hard landing with gear crash possible.
 Using more than recommended glideslope speed will result as above.
 Speed less than recommended in glideslope need you use more pitch when flare and result will same or if use right flare pitch  to big vertical touchdown speed with result as above.
Recommended in glideslope need you use more pitch when flare and result will same or if use right flare pitch  to big vertical touchdown speed with result as abov
Development
Since the start we added:
 Support for rembrandt
 Reverse thrust
 Autopilot
 Nav, beacon and taxi/landing lights
 Liveries (auto nose selection, based on livery)
To Do
 [3D] Cockpit (basic cockpit done)
Liveries
 Air Koryo
 Aeroflot 1970
 Aeroflot 2008
 Interflug
 LOT Polish Airlines
 Nordavia
 Pulkovo
 Rossiya
 Russian Air Force
 Russian Navy
 UTair
 Ukrainian Government
 Ukrainian Armed Forces
 Ukrainian Navy
External link
