Hi Friends:
The best flying version of the Tu-134 is here:
www.avsimrus.com/f/fs2004-aircrafts-40/scs-tu-134-2-0-original-59825/zipFor problems help in English you can find here:
www.protu-154.org/forum/viewforum.php?f=24&sid=7fadd8c948580270af05a0f4a84c7fc4A brief introduction of handling the system you can find here its for on older versión but less the numbers of subwindows everthing Works:
www.protu-154.org/forum/viewtopic.php?t=3571Here is a quick guide on flying the TU134 as published on the FAQ section of the Tu 134s forum:
PRINCIPLE CHARACTERISTICS
max. Empty weight: 30572 kg
max. Fuel weight: 14400 kg
max. Takeoff weight: 49000 kg
max. Landing weight: 43000 kg
max range: 3500 km (with fuel reserves for 1 hour)
Minimum runway length for takeoff: 2400 m.
minimum runway length for landing: 2200 m.
Operation Altitudes: 10 100m. - 12 100 m
ALTITUDE/WEIGHT LIMITATIONS
Weight (tons)/ max. Altitude (meters)
<44.5 / 10 600
44.5 / 11 100
41 / 11 600
37.5 / 12 100
SPEED LIMITATIONS
Maximal allowable Speed: 600 km\h or .82M
Minimum speed with a clean configuration: 330 km\h
Max. speed for Landing Gear deployment: 400 km\h
speed limitations for flaps extention:
10 * 400 - 310 km\h
20 * 400 - 290 km\h
30 * 340 - 240 km\h
TAXIING
Initial movement will take place when throttles are advanced to 86% RPM.
taxiing is performed at 62-66% RPM with normal weight.
Engine revolutions may be increased to a maximum of
68-70% RPM.
Maximal Taxiing speed is 35 km\h and 10-15 km\h for
turns.
TAKEOFF
Flaps: 10 * (or 20 *, depending on conditions)
Engine operating mode: 98%-99.5%
stabilizer: 1,5 * up.
Switch the headlights to "High" ("Low", depending on
the conditions)
at 270km\h pull back the yoke firmly but smoothly to
detach the nose gear off the ground.
The Pitch angle should be in the range of 10*-12 *, the angle of attack 6*-8*.
Liftoff will occur at a speed of approximately 290 km\h.
ATTENTION: the speed limitation for the front landing
gear strut is-310 km\h; For the main struts - 330 Km/h
After passing 5m on the RA,make sure that the speed
increases and retract the landing gear.
After 50m on the RA (at night) or 200m RA (day),turn off
and to retract the headlights.
After reaching 120m, and a speed of 330-340km\h, retract
the flaps.
When reaching the speed of 390-400km\h establish
nominal engine operating regime (91.5%-93%).
Accelerate to 500km\h IAS (For noise abbatement takeoff
- 460 Km/h)
Maintain 500Km/h until reaching 3000m.After passing
3000m until the required cruise level maintain
480-460Km/h
Time to flight level:
9100m - 21 min.
10600m - 26 min.
CRUISE
On the assigned echelon(flight level) accelerate to the
required speed at 91,5%-93% RPM.
Acceleration to 0.82M with an engines power of 93%
at 10600m is approximately 10 minutes.
Recommended speeds:
Alt(m) Reg(%RPM) Spd(Km/h) Mch GrndSpd(Km/h) FF(Kg/h)
9600 90 520 .75 820 2600
10100 91 500 .78 830 2300
10600 93 515-520 .81 855-860 2250
Recommended cruise speed MACH 0.79 - 0.81
Recommended regimes: 89%-92%
ATTENTION:above 93% RPM,the aircraft will reach critical
speed.
DESCENT
decreased engine revolutions to 81%-83%, and begin the
descent with a vertical speed of 10-12 m/s.
Attentively follow the speed ,do not exceed 600km\h IAS.
After crossing 8000m.Set th first engine to 81% RPM,and
the second to idle. Or: to first to 81%, and the second
to- 75%-68%.
Under 5000m.establish a regime of 61.7%-72% RPM to both
engines.
Under 3000m do not exceed 460km\h and a vertical velocity of more than 15 m/s
APPROACH
When entering approach altitude establish a speed of 400-380km\h with a clean wing.
The regime should be approximately 75-85%.
Extend the landing gear. After getting"THREE GREENS", extend the flaps to 20* and simultaneously establish a regime of 85%-88%. Bleed off speed to 360-340Km/h.
at a speed of 300-320km\h extend the flaps further to 30* with a simultaneous decrease of speed to 280-300km\h.
When the flight directors glideslope needle is near the middle (i.e just before establishment on the glideslope) decrease the regime to 81-83%.
When established, maintain 80-86% (with light weight 75-82%)
Speeds on the glide slpe, taking the weight into
account:
Weight (tons) speed (km\h)
43 275-285
40 267-280
35 252-265
33 250-260
optimum angle of attack on the glideslope 4* - 6*
LANDING
At DH (60m.)d isconnect the autopilot iif it was previously engaged.
From 20m. begin to decrease the vertical velocity.
Approaching 10m, the vertical velocity must be 3m\s.
at 7m, increase angle of attack by 1*-2 * and continue levelling off to an altitude of 3m.
At this point move the throttles to idle and land.
After landing extend spoilers and reverse thrust. At 250 Km/h one can use the breaks.
Reverse is turned off at 110km\h, but if necessary, it may be used until the aircraft comes to a complete stop.
idealy, landing speed should be to 20km\h less than the speed on the glideslope.
Kind regards
Walter