Ch. 5 - Limitations (LIMITS) Flashcards
(38 cards)
Minimum crew to fly the helicopter?
PLT and CPG
Minimum crew for ground maintenance runs?
MTP (PLT station). Technical observer may be authorized to occupy the CPG station during ground maintenance at the discretion of the commander.
Nr - Rotor Speed Limitations
110 Maximum (>110 red)
106-110 Transient (yellow)
95-105 Normal (<97 low rotor annunciated, >97 green)
0-94 Transient (red)
[NOTE] It is normal for oil pressure to be high during first start when oil is cold. __________.
Oil pressure should return to normal after 5 min of operation at idle speed. Do not accelerate above ground idle speed until oil pressure can be held at or below maximum limit throughout acceleration.
ENG OIL PSI
120 Maximum (>120 red w/box) 23-120 Normal 23 Minimum (<23 red)
HYD PSI
> 3410 Transient - permitted for 5 sec (yellow; >=5s red w/box)
3310-3400 Transient - permitted for 5 min (yellow; >=5m red w/box)
2750-3300 Normal (green)
1260 Minimum (<1260 red w/box)
Engine Starter Limitations; Air Turbine Starter (ATS)
A starting cycle is the interval from _____ and acceleration of the _____ from zero RPM to ____. The _____ delay between start attempts applies when the first attempt is aborted for any reason. If motoring is required for an emergency, the ____ delay does not apply.
start initiation
output drive shaft
starter dropout
60 second / 60 second
Engine Starts at Ambient Temperatures of 16*C and Below: ____ consecutive start cycles may be made, followed by a ____ rest period, followed by ____ additional start cycles. A ____ rest period is then required before any additional starts.
TWO consecutive start cycles may be made, followed by a 3 MINUTE rest period, followed by TWO additional start cycles. A 30 MINUTE rest period is then required before any additional starts.
Engine Starts at Ambient Temperatures Above 16*C: ____ consecutive start cycles may be made. A ____ rest period is then required before any additional starts.
TWO consecutive start cycles may be made. A 30 MINUTE rest period is then required before any additional starts.
Dual engine starts are _____ due to ______.
prohibited due to insufficient IPAS air
TGT Limiter Control Values
DE: 866 +/- 12 *C
SE: 891 +/- 12 *C
Turbine Gas Temperature (TGT) Limits
949 Maximum (>949 red) 904-949 SE Transient, 12 sec (yellow) 879-903 SE Contingency, 2.5 min (yellow) 852-878 Maximum Rated Power, 10 min (yellow) 851 Maximum during Start 811-851 Intermediate Rated Power, 30 min (yellow) 810 Maximum Continuous Power 0-810 Normal (green)
Engine Power Turbine Speed (Np) Limitations
121 Maximum (red)
115 Engine Overspeed Annunciated
106-121 Transient, 12 sec (yellow; w/box at 115)
0-105 Normal (green)
Engine Gas Generator (Ng) Limitations
- 1 Maximum (>105.1 red)
- 3-105.1 Transient, 12 sec (yellow)
- 1-102.2 Normal (green)
- 0 Minimum engine out warning annunciated (<63.0 red w/box)
Engine Torque (Nr < 50%)
30 Maximum (>30 red) 0-30 Normal (green)
Engine Torque (Nr <90%)
70 Maximum (>70 red) 0-70 Normal (green)
Engine Torque Limitations (SE)
125 Maximum (>125 red) 123-125 Transient, 6 sec (yellow) 111-122 SE Contingency, 2.5 min (yellow) 110 SE Max Continuous Power (green) 0-110 Normal (green)
Engine Torque Limitations (DE)
115 Maximum (>115 red)
101-115 Transient, 6 sec (yellow)
0-100 Normal (green)
[CAUTION] Avoid prolonged operation at _____ Nr with the APU running. The APU will ________. This creates high loads on the clutch and shall be avoided.
94-96% Nr
oscillate from engaged to disengaged
APU operation is ______ during normal flight. After a fault or aborted start, wait _____ before attempting another start. After _______, wait ____ before a ___ start attempt. No more than ______.
APU operation is PROHIBITED during normal flight. After a fault or aborted start, wait 30 SEC before attempting another start. After 2 CONSECUTIVE START ATTEMPTS, wait 20 MIN before a 3rd start attempt. No more than 3 START ATTEMPTS ARE PERMITTED IN ONE HOUR.
[CAUTION] Do not operate the APU for more than ___ at a XMSN TEMP 1 or 2 of ______. Shut down APU to prevent damaging _______.
5 minutes
120-130*C
accessory gearbox components
During prolonged ground operations greater than ___, observe XMSN TEMP 1 and 2 on the SYS page. If the temperature exceed 130*C, __________, or _____.
30 minutes
the APU shall be shutdown and the XMSN fluid allowed to cool for 30 min prior to resuming APU operations; or transmission fluid may be cooled by operating an engine with rotor turning.
The aircraft maximum gross weight is _____ pounds, except for non-tactical ferry flights, which may not exceed ______.
20,260 lbs
23,000 lbs
Maximum Airspeed for Autorotation
145 KTAS. Above 145 KTAS, drag on the rotor system will cause Nr to decay rapidly.