2P board #2 Flashcards
Def. of warning
Explanatory information about an operating procedure, practice, or condition that may result in injury, death, or loss of aircraft if no carefully observed
Shall
used only when application of a procedure is mandatory
Land as soon as practicable
Extended flight is not recommended. The landing site and duration of flight are at the discretion of the pilot in command
5 steps in emergency
Maintain control of the aircraft
Alert crew
Determine the precise nature of the problem
Complete the applicable emergency procedure or take action appropriate for the problem
Determine landing criteria and land as required
Cycle
If the circuit breaker is in, pull circuit breaker out, and then push circuit breaker back in. If circuit breaker is out, do not change condition.
Reset
If circuit breaker is out, push circuit breaker in. If circuit breaker is in, do not change condition
Max number of people in cabin
3, Can do more for emergency/SAR
Starter limits
OAT <16, on off 60 sec
on - off 60 sec
on - off 60 sec
on - off 30 minutes
OAT 16-52 on - off 60 sec
on - off 30 minutes
Start cycle defined as starter initiation, acceleration, and dropout
Backup hyd pump limits
With rotors static
OAT 33-38
24 on 72 minutes off
39-60
16 on 48 minutes off
Compressor section
5 stage axial and a single stage centrifugal rotor/stator assembly
Airflow of combustion
30% of total airflow for combustion
70% T2 P3 Combustor and turbine cooling engine oil seal pressurization
C-PWR
Sets max permissable TGT to 903, limits at 891+_10
Auto C power turns C power on when one engine is below 50% torque, opposite engine sets max of 891+_10
TGT limiting
When TGT approaches 878 EDECU prevents any further fuel flow. MRP prevents at 866+_10
LDS Malfunction
Roll pin failure or LDS cable malfunction
PCLs in idle - Ng 3-4 percent higher than other engine
PCLs fly collective full down - 1-2 percent torque diff, Nr and both Np 1-2% above 100
In flight - notice torque splits for certain flights, collective increase/decrease below 75%
Utility Module
Routes fluid from backup pump to 1 and 2 transfer modules, second stage of the tail rotor servo, rescue hoist, APU accumulator
Priority valve secures power to rescue hoist in the event backup hyd pressure decreases
Velocity fuse secures fluid to APU accumulator if flow rate exceeds a prescribed limit
Engine anti-ice/Start bleed valve
5th stage bleed air to the engine
Open during starts
Closes above 90 percent Ng
Can flameout engine with a temporary hangup of variable geometry with low collective settings
Malfunctioning ON with above 90 Ng or above 94 Ng if OAT greater than 15 Not ON below 88 Ng Not ON with switch being turned on No rise in TGT with switch ON
May reduce max torque by 18%