C90 Powerplant / Props Flashcards
(29 cards)
What model of Engines?
Pratt Whitney
PT-6
135A
Rated Power
550 SHP
Engine Design
Free spinning - not physically connected
Compressor = 3 axial stage + 1 centrifugal stage
Single Power Turbine
Combustion Chamber
25% Air burnt, other 75% used to centre flame - cooling
14 nozzles, (StartUp 10 only, other 4 open passsing 40% N1)
Oil Pressure moves Props to Fine or Coarse Pitch
FINE
Which is Critical Engine
LEFT
Engine Start
Hung Or Hot Start
Keep Condition lever out of indent
If ITT approachs 2nd red line start should be aborted, before it passes 2nd red line
Condition Lever ICO
Starter ONLY for the remainder of 40 sec cycle
Engine Start Time / Limits
40 Secs On / 60 secs OFF
40 Secs On / 60 secs OFF
40 Secs On / 30 mins OFF
What is N1 ?
Limits
Turbine Speed
101.5 %
Transient - 102.6% (
Max Reverse - 88 % (1 min)
What is N2 / Np
Limits
Prop Speed
NOT BELOW - 1100, unless feathered
1900 RPM -
1938 RPM - 7 min
1825 RPM - Reverse
2070 - Transient (
What is ITT ?
Limits
Interstage Turbine Temp
Station 5 - T5
805
Low Idle - 685 - Only when N1 below 70 %
Start Up - 1090 (2 secs)
Transient - 800 (2 secs)
What is P-3
Pressurised Air at Station 3
Bleed Air
Between axial compression and combustion chamber
Reduction Gearbox
15:1
37,500 - 1900
High RPM /Low Tq - Low RMP/High Tq
Engine Auto Ign
When armed, If Tq drops below 400’/lbs
Ignitors energise - Annunciator
Accessory Gear Box - Rear
Starter Gen
Fuel Pump/
Fuel control unit
Oil Scavenger pumps
Optional accessory drives
7 stations with differnet gear ratio’s
Accessory Gear Box - Front
Prop Governors
Prop Tach Generator
Overspeed Governor
Oil Capacity
3.55 USG
(13.4 Ltrs)
Max Consumption - 1 USG every 10 hrs
Oil-Heater Exchange Unit
Use hot oil to heat fuel
Oil Temp Range
0 - 99 Deg C
Start - (-40 Deg C)
104 10 min Transient (10 mins)
60-70 Deg C Normal
Oil Pressure range
85 Psi - 105 Psi
Magnetic Chip Detector
Yellow Annunciator
Monitor engine parameters
Unusual Indications - Shutdown and secure the affected engine
Follow Checklist
Fuel Control Unit
FCU
Meters fuel flow
Fuel flow managed using P3 pressure
Higher P3 - Higher fuel flow
Failure of P3 would result in min fuel flow (48%N1) -
Power and condition levers would have no effect on engine speed
Prop Levers
Sets desired Propeller RPM
Maintained by adjusting prop pitch
Power Levers
Adjusts N1 governor,
Engine Tq
When advanced - N1 - FCU - fuel flow increased
3 Control ranges - Flight / BETA / Reverse separated by lifting over gates