-10 V4 Chapter 5 Flashcards
Rotor Speed (Nr) Limits - %
Maximum (>110 red) - 110%
Transient (yellow) - 105 - 110%
High Rotor Warning Annunciated - 105%
Normal (green) - 97 - 104%
Low rotor warning annunciated - 97%
Transient (red) - 0 - 96%
ENG 1 or 2 OIL PRESSURE (PSI)
120 - Max (>120 red w/box
23 - 120 - Normal (Green)
23 - Min (<23 red)
HYDRAULIC PRESSURE (PSI)
> 3410 - Transient - permitted for 5 sec (yellow) (>= 5 sec red w/box)
3310 - 3400 - Transient - Permitted for 5 min (yellow) (>= 5 min red w/box)
2700 - 3300 - Normal (green)
1260 - Min (<1260 red w/box)
Engine Starter Limitations -
Engine Starts at Ambient Temp of 61F (16C) and below:
Two consecutive start cycles may be made, followed by a 3 MIN rest period, followed by two additional consecutive start cycles.
A 30 minute rest period is then required before any additional starts.
Engine Starter Limitations -
Engine Starts at Ambient Temp above 61F (16C):
Two consecutive start cycles may be made. A 30 minute rest period is then required before any additional starts.
Engine Starter Limitations -
Dual Engine Starts
Dual engine starts are prohibited due to insufficient IPAS air.
Engine Temperature Limitations - (TGT *C)
949 - Max (>949 red)
904 - 949 - Transient, 12 sec (yellow)
880 - 903 - Contingency, 2.5 min (yellow)
847 - 879 - Max rated power, 10 min (yellow)
851 - Max during start
794 - 846 - Intermediate rated power, 30 min (yellow)
793 - Max continuous power
0 - 793 - Normal (green)
Engine Temperature Limitations:
At what temperature does the TGT limiter control limit engine operation? Both Dual Engine (DE) and Single engine (SE)
DE - 879C +/- 5C
SE - 903C +/- 5C
Engine Power Turbine Speed (Np) (Np %)
Np = N2
Max Digital Tape Reading - 120%
119 - Maximum (>119 red w/box)
114 - Engine Overspeed annunciated
104 - 119 - Transient, 12 sec, (yellow w/box at 114)
0 - 103 - Normal
Engine Gas Generator (Ng) Limitations (Ng %)
Ng = N1
- 0 - Maximum (>106.0 red)
- 1 - 106.0 - Transient, 12 sec, (yellow)
- 1 - 105.0 - Normal (green)
- 0 - Minimum engine out warning annunciated (<63.0 red w/box)
Engine Torque Limitations:
Limits - Torque (%) Digital Readouts with Nr <50%
30 - Max (>30 red)
0 - 30 - Normal (Green)
Engine Torque Limitations:
Limits - Torque (%) Digital Readouts with Nr <90%
70 - Max (>70 red)
0 - 70 - Normal (green)
Engine Torque Limitations:
Limits - Torque (%) Digital Readouts - Dual Engine
115 - Max (>115 red)
101 - 115 - Transient, 6 secs (yellow)
0 - 100 - Normal (green)
Engine Torque Limitations:
Limits - Torque (%) Digital Readouts - Single Engine
125 - Max (>125 red)
121 - 125 - Transient, 6 sec (yellow)
111 - 120 - Single engine contingency, 2.5 min, (yellow)
110 - Single Engine maximum continuous power (green)
0 - 110 - Normal (green)
Auxiliary Power Unit (APU) Operating Limits:
APU Clutch Limitation
Avoid prolonged operation at 94% - 96% Nr with the APU running. The APU clutch will oscillate from engaged to disengaged. This creates high loads on the clutch and shall be avoided.
Auxiliary Power Unit (APU) Operating Limits:
Use in flight?
APU operation is prohibited during normal flight.
Auxiliary Power Unit (APU) Operating Limits:
APU Start Limitations
After a fault or aborted start, wait 30 seconds after APU has stopped before attempting another start. After 2 consecutive start attempts, wait 20 minutes before third start attempt. No more than 3 start attempts are permitted in one hour.
Auxiliary Power Unit (APU) Operating Limits:
APU XMSN TEMP 1 and XMSN TEMP 2 Limit
If the temperatures exceed 140*C, the APU shall be shutdown and the transmission fluid allowed to cool for 30 minutes prior to resuming APU Ground operations; or transmission fluid may be cooled by operating an engine with rotor turning.
Weight Limitations - non-tactical ferry flight (lbs)
23000lbs
Weight Limitations - Tactical flying (lbs)
20260lbs
Airspeed Operating Limits:
Airspeed Limits for Autorotation - KTAS
145 KTAS
Airspeed Operating Limits:
Airspeed Limits for Single Engine Operation
Maximum airspeed for single engine operation is the greater of:
- 67% of Vne determined using the Airspeed Operating Limits Chart using the GROSS WEIGHT line.
- The airspeed for minimum power determined from the applicable chapter 7 cruise charts using the MAX END / MAX R/C lines
Airspeed Operating Limits:
Maximum Airspeeds during manual stabilator operations
Maximum airspeeds are based on stabilator position. The stabilator position and nominal airspeed restrictions are dispayed on the FLT FLT SET and SYS pages, as described in Para 2-47d of the -10.
Airspeed Operating Limits:
Maximum rearward and sideward airspeed
45 KTAS for all gross weights