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77 Cards in this Set
- Front
- Back
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Engine Starter Limits
1st Attempt 0 to 30 seconds on ____ minute off |
1 minute off
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Engine Starter Limits
2nd Attempt 0 to 30 seconds on ____ minute off |
5 minute off
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Engine Starter Limits
3rd Attempt 0 to 30 seconds on ____ Minute off |
15 Minute off
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Engine Limits
ITT Military ____ Max Cont. ____ |
Military 810°C
Max Cont. 770°C |
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Engine Limits
Q Military ___ Max Cont. ___ |
Military 83% (1070 SHP)
Max Cont. 83% (916 SHP) |
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Engine Limits
Time Military ___ Max Cont. ___ |
Military 30min
Max Cont. N/A |
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Do not apply rotor brake above what Nr except for emergencies?
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20%
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Maximum Airspeed
Max w/ extended load on the hoist |
30 KIAS
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Xmsn oil temp and press.
Normal Press. Range |
40-70 psi
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Engine (Nf)
Max |
100%
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Engine oil temp. and press.
Norm. Press. Range |
80-112 psi
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Engine oil temp. and press.
Caution press. range |
40-80 psi
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Xmsn oil temp and press.
Max Press. |
70 psi
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What are the lateral COG limits?
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6" left/right of the longitudinal axis
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Ng
Max |
100%
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Xmsn oil temp and press.
Allowable flux |
+ or - 7 psi
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Ng
Accel. Trans. 10 sec limit |
101%
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Ng
Flight Idle |
61% + or - 2%
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Xmsn oil temp and press.
Caution Press. Range |
30-40 psi
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Maximum Airspeed
Max rearward |
30 Knots
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Rotor Power ON
Norm. Op. Range |
97-100%
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Engine oil temp. and press.
Min. Press. |
40 psi
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Engine oil temp. and press.
Allowable Flux |
+ or - 5 psi
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CGB oil Temp. and Press.
Allowable Flux |
+ or - 5 psi
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Intentional flight through known icing conditions with OAT colder than what temp. is prohibited?
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-5° C
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Maximum Airspeed
Max sideward |
35 Knots
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Xmsn oil temp and press.
Min. press. |
30 psi
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ITT
Caution Range |
770°C
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Engine (Nf)
Acceleration transient 10 sec limit |
110%
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CGB oil temp. and press.
Min. Press. |
40 psi
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Engine oil temp. and press.
Max press. |
112 psi
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ITT
Allowable Flux |
+ or - 5°C
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Maximum Airspeed
Cargo doors partially open unsecured |
80 KIAS
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Rotor Power ON
Transient Max |
105%
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CGB oil Temp. and Press.
Norm. Press. range |
60-85 psi
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Prohibited Maneuvers
1. 2. |
1. Aerobatic maneuvers
2. Abrupt movement of flight controls (Control rate movement of flight controls at a rate of full travel to 2 seconds or less) |
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ITT
Max |
810°C
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Engine Torque
Caution Range |
71-83%
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CGB oil Temp. and press.
Caution Press. Range |
40-60 psi
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Maximum Airspeed
Cargo doors fully open secured |
Vne/120 KIAS <
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Dual Ammeter
Max; except when using gen to start other engine |
225 Amps
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ITT
During start monitor ITT above... |
870°C
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Rotor Power ON
Transient Min |
91%
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CGB oil temp. and press.
Max Temp |
116°C
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Engine oil temp. and press.
Max Temp. |
116°C
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Engine Limits
Ng Military ___ Max Cont. ___ |
Military 100%
Max Cont. 100% |
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Transmission
Caution Range |
88-100%
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Engine Torque
Max allow steady state Q Split |
4%
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CGB oil temp. and press.
Max Press. |
85 psi
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Particle Sep. should be in AUTO when visible moisture is evident at what temp?
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Below 5°C
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Engine Torque
Max |
83%
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Rotor Power OFF
Min |
91%
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Xmsn oil temp and press.
Max Temp |
110°C
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ITT
Max ITT during Start |
1090°C
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Maximum Airspeed
Max steady state for autorotations |
110 KIAS
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Starting and stopping rotors with winds above what speed is prohibited?
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45 kts
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Maximum Airspeed
Max |
130 KIAS
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Engine (Nf)
Normal Range |
97-100%
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Rotor Power OFF
Max |
105%
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Pitot heat should be turned on when?
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Visible moisture with temp below 10°C
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Dual Ammeter
Caution Range |
200-225 Amps
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Transmission
Max |
100%
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Dual Ammeter
Max; except when using gen to start other engine |
225 Amps
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ITT
During start monitor ITT above... |
870°C
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CGB oil temp. and press.
Max Temp |
116°C
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Operation in ambient temp. above/below is prohibited?
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52°C/-54°C
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Engine Limits
Ng Military ___ Max Cont. ___ |
Military 100%
Max Cont. 100% |
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Engine Torque
Max allow steady state Q Split |
4%
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Particle Sep. should be in AUTO when visible moisture is evident at what temp?
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Below 5°C
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Rotor Power OFF
Min |
91%
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ITT
Max ITT during Start |
1090°C
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ENGINE FIRE IN FLIGHT
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FIRE PULL HANDLE - PULL (AFFECTED ENGINE)
Nr - MAINTAIN WITH COLLECTIVE BEEP SWITCH - MAXIMUM AIRSPEED - 55 KNOTS MINIMUM FIRE EXT. SWITCH - MAIN (RESERVE IF NECESSARY) |
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MAIN DRIVESHAFT FAILURE
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AUTOROTATE
THROTTLES - FLIGHT IDLE |
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COMPLETE LOSS OF TAIL ROTOR THRUST (UNCONTROLLABLE)
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AUTOROTATE
THROTTLES - FLIGHT IDLE |
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SINGLE ENGINE FAILURE DURING FLIGHT
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Nr - MAINTAIN WITH COLLECTIVE
BEEP SWITCH - MAXIMUM AIRSPEED - 55 KNOTS MAXIMUM |
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DUAL ENGINE FAILURE
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AUTOROTATE
THROTTLES - FLIGHT IDLE |
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ENGINE FIRE ON THE GROUND
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THROTTLES - OFF
FIRE PULL HANDLE - PULL (AFFECTED ENGINE) |
