Transmission System Flashcards
Spinny Spin
SETUP: NR decreases from 100-96% with an increase in Q in steady flight
What is wrong?
-1 Section III
Main transmission planetary carrier may have failed.
EP
During a main transmission failure or main xmsn press or main xmsn oil hot caution, what will the loss of cooling oil supply result in?
-1 Section III
Electrical and/or mechanical failure of main generators.
EP
What are some considerations with main transmission failure?
-1 Section III
Avoid rapid or frequent power changes, APU should be started so that the APU generator will be immediatly available (if main generators fail), a running landing is preferable.
EP
If impending transmission failure is suspected, what is the primary consideration?
-1 Section III
Land the helicopter before the failure progresses to gear box seizure or loss of drive to the main and/or tail rotor.
OpsLimits
What aircraft flight condition would cause momentary fluctuations in oil pressure?
-1 Section V
Flying with pitch attitudes above +6 degrees
Hovering in gusty wind conditions
OpsLimits
Under what conditions of the oil pressure should an entry be made in the forms?
-1 Section V
Oil pressure is not steady during steady state forward flight or in a hover
Oil pressure is steady but under 45 psi
Sudden pressure drops (greater than 10 psi) without fluctuation
OpsLimits
What action is prohibited in regards to the gust lock?
-1 Section V
Operating the engine against the gust lock
OpsLimits
What is the maximum NR speed for rotor brake application?
-1 Section V
76% NR (emergencies only)
OpsLimits
What is the maximum NR speed for routine stops with the rotor brake?
-1 Section V
40% NR
OpsLimits
What is the psi range during routine stops with the rotor brake?
-1 Section V
150-180
OpsLimits
What is the duration allowed for the rotor brake to be applied during routine stops?
-1 Section V
12-18 seconds
OpsLimits
What is the psi range for rotor brake starts?
-1 Section V
450-690
OpsLimits
What speed can we operate the engines up to with the rotor brake on? (During rotor brake starts)
-1 Section V
Up to IDLE only
OpsLimits
Can a dual engine start be done with the rotor brake? Is there a time associated with it?
-1 Section V
Yes, single and dual engine starts are allowed.
No, there is no time limit for rotor brake operations with single or dual engine starts, or with operations at IDLE
OpsLimits
What is the maximum wind velocity for rotor start or stop?
-1 Section V
45 knots from any direction
OpsLimits
What is the max NR speed?
-1 Section V
120%
What is the purpose of the input module?
-1 Section 1
Transmit power from the engines to the main transmission.
It also contains the freewheeling unit.
What is the function of the freewheeling unit? (i.e. why do we care)
-1 Section 1
Allows engine disengagement during autorotation.
If an engine isn’t operating it allows the accessory module to continue to be driven by the main rotor. (Still have hydraulic and gens)
What are the five modules of the main transmission?
-1 Section 1
Two input modules, main module, two accessory modules.
What is the purpose of the accessory module?
-1 Section 1
Provides mounting and drive for an electrical generator and a hydraulic pump.
Where is the rotor speed sensor that provides signals for the EICAS and PFD power pods?
-1 Section 1
Right accessory module
Where is the rotor speed sensor that provides input signals to the EDECU for improved transient droop response?
-1 Section 1
Left accessory module.