Tupolev Tu-134: Difference between revisions

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Tupolev Tu-134 (view source)

Revision as of 17:53, 13 June 2014

3,750 bytes added ,  13 June 2014
livery list updated, simplified procedures updated
(small edit)
(livery list updated, simplified procedures updated)
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== Simplified procedures ==
== Simplified procedures ==
==== Taxiing ====
* For begin moving use up to 86% N2 a short time.
* Normal taxiing at 62-66% N2 depending weight.
* In turns use 68-70% N2.
* Maximum taxiing speed 35 km/h and 10-15 km/h in turns.
==== Takeoff ====
==== Takeoff ====
# Set flaps to position 1, you'd better do this during taxi.
At MTOW
# Smoothly apply full throttle.
 
# Push the stick slightly forward until at least 60 kts.
* Flaps    10 (20)
# Around 160 kts, slowly pull the stick back to rotate. Rotate toward 10° pitch attitude.
* N2        98-99.5% (full throttle, no more 5 min)
# The plane should takeoff around 180 kts.  
* Elevator trim - 1.5 degrees up
# Retract gear as soon as the aircraft around 1000 ft.
* Switch landing lights ON.
* At 270 km/h up nose (pitch about 10-12 degrees, angle off attack  6-8 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 330-340 km/h retract flaps to 0 degrees.
* 390-400 km/h - reduce throttle to nominal value 91.5-93.0 % N2.
* Accelerate to 500 km/h (460 km/h if need noise reduction procedure)
* Climb to altitude 3000 at 500-480 km/h,from 3000m to 6000m at 480-460 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 91.5-93.0 % N2.
Acceleration time to 0.82M with 93% N2 at 10 600M after reach 10 600M about 10 minutes.
 
{| class="wikitable"
|-
! 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 || 515-520 || 0.81 || 855-860 || 2600
|-
|}
 
At 10 600M
{| class="wikitable"
|-
! 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 81-83% N2 and begin descend 10-12 m/sec at 0.8-0.82M 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  75-68% N2(if practicable).
* Below 5000m reduse trottle to 61.7-72.0% N2 or idle.
* Below 3000m speed less than 460 km/h and vertical speed less than 15 m/sec.
 
==== EMERGENCY Descending ====
* Trottle - Idle (61.7-63% N2), pitch 10-15 degree negative, gear down.
* Speed 600 km/h, 0.82M. Vertical speed 30-50m/sec.
* While ending this mode plane drop 400-500m of altitude.
* After emergency descend do not retract gear.
 
==== Approuching ====
* Typical speed 380-400 km/h at clean plane, and 78-85% N2 and 85-88%N2 with gear down.
* Gear down and extend flaps to 20 degree at 360-340 km/h, 86-88 N2.
* At 300-320 km/h flaps 30 degree.
* Before intercept glideslope flaps 30, gear down, speed 280-300 km/h.
* When intercept glideslope decrease throttle to 81-83% N2.
* In glideslope use 80-86% N2 (75-82% N2 in case small weight)
 
{| class="wikitable"
|-
! Weight (kg) !! Speed (km/h)
|-
| 43000 || 275-285
|-
| 40000 || 267-280
|-
| 35000 || 252-265
|-
| 33000 || 250-260
|}


==== Approach ====
Optimal angle off attack  4.5-6 degrees.
# Set speed to 230 kts.
# Set the flaps to position 1.


==== Landing ====
==== Landing ====
# Set speed to 160 kts.
* At 60 m AGL disengage autopilot.
# Set flaps to position 2.
* At 20 m AGL begin decreasing vertical speed and at 10 m AGL vertical speed must be about -3m/s
# Gear down.
* At 7 m AGL smoothly up nose to create 1-2 degree pitch and begin flare.
* While flare increase pitch to 3-4 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.


==== Landing roll ====
Notes
# Set flaps to position 3.
* Using more than 2.5 degree pitch when flare will result plane up and quickly drop speed with hard landing with gear crash possible.
# Set spoilers to FULL (tap multiple times key "k").
* Using more than recommended glideslope speed will result as above.
# Touchdown SPD 124 kts
* 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.


OPTIONAL: Enable thrust reverse just before touchdown.
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 ==
== Development ==
Line 64: Line 155:
* Aeroflot 1970
* Aeroflot 1970
* Aeroflot 2008
* Aeroflot 2008
* Interflug
* LOT Polish Airlines
* LOT Polish Airlines
* Nordavia
* Nordavia
UR-AOK
185

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