Ch. 5 - Limitations (LIMITS) Flashcards

1
Q

Minimum crew to fly the helicopter?

A

PLT and CPG

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2
Q

Minimum crew for ground maintenance runs?

A

MTP (PLT station). Technical observer may be authorized to occupy the CPG station during ground maintenance at the discretion of the commander.

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3
Q

Nr - Rotor Speed Limitations

A

110 Maximum (>110 red)
106-110 Transient (yellow)
95-105 Normal (<97 low rotor annunciated, >97 green)
0-94 Transient (red)

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4
Q

[NOTE] It is normal for oil pressure to be high during first start when oil is cold. __________.

A

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.

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5
Q

ENG OIL PSI

A
120 Maximum (>120 red w/box)
23-120 Normal
23 Minimum (<23 red)
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6
Q

HYD PSI

A

> 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)

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7
Q

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.

A

start initiation
output drive shaft
starter dropout
60 second / 60 second

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8
Q

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.

A

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.

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9
Q

Engine Starts at Ambient Temperatures Above 16*C: ____ consecutive start cycles may be made. A ____ rest period is then required before any additional starts.

A

TWO consecutive start cycles may be made. A 30 MINUTE rest period is then required before any additional starts.

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10
Q

Dual engine starts are _____ due to ______.

A

prohibited due to insufficient IPAS air

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11
Q

TGT Limiter Control Values

A

DE: 866 +/- 12 *C
SE: 891 +/- 12 *C

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12
Q

Turbine Gas Temperature (TGT) Limits

A
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)
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13
Q

Engine Power Turbine Speed (Np) Limitations

A

121 Maximum (red)
115 Engine Overspeed Annunciated
106-121 Transient, 12 sec (yellow; w/box at 115)
0-105 Normal (green)

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14
Q

Engine Gas Generator (Ng) Limitations

A
  1. 1 Maximum (>105.1 red)
  2. 3-105.1 Transient, 12 sec (yellow)
  3. 1-102.2 Normal (green)
  4. 0 Minimum engine out warning annunciated (<63.0 red w/box)
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15
Q

Engine Torque (Nr < 50%)

A
30 Maximum (>30 red)
0-30 Normal (green)
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16
Q

Engine Torque (Nr <90%)

A
70 Maximum (>70 red)
0-70 Normal (green)
17
Q

Engine Torque Limitations (SE)

A
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)
18
Q

Engine Torque Limitations (DE)

A

115 Maximum (>115 red)
101-115 Transient, 6 sec (yellow)
0-100 Normal (green)

19
Q

[CAUTION] Avoid prolonged operation at _____ Nr with the APU running. The APU will ________. This creates high loads on the clutch and shall be avoided.

A

94-96% Nr

oscillate from engaged to disengaged

20
Q

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 ______.

A

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.

21
Q

[CAUTION] Do not operate the APU for more than ___ at a XMSN TEMP 1 or 2 of ______. Shut down APU to prevent damaging _______.

A

5 minutes
120-130*C
accessory gearbox components

22
Q

During prolonged ground operations greater than ___, observe XMSN TEMP 1 and 2 on the SYS page. If the temperature exceed 130*C, __________, or _____.

A

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.

23
Q

The aircraft maximum gross weight is _____ pounds, except for non-tactical ferry flights, which may not exceed ______.

A

20,260 lbs

23,000 lbs

24
Q

Maximum Airspeed for Autorotation

A

145 KTAS. Above 145 KTAS, drag on the rotor system will cause Nr to decay rapidly.

25
Q

Airspeed limits with one engine inoperative is the greater of:

A

67% Vne

MAX END / MAX R/C airspeed

26
Q

Maximum rearward / sideward flight is ____

A

45 KTAS

27
Q

The searchlight is designed for operation (extend/retract/rotate) at speeds up to ____. However, as long as operation is not attempted, the lighthead can be left in any extended position at speeds up to ___.

A

90 KTAS

Vne

28
Q

Maximum Airspeed with Symmetrically Loaded Fuel Tanks

A

130 KTAS

29
Q

Maximum Airspeed for Stores Jettison

A

130 KTAS
Hover-45 KTAS (minimize side-slip)
45-130 KTAS (ball centered)

30
Q

Maximum Airspeed for External Tanks Jettison

A

100 KTAS

31
Q

Intentional Maneuvers beyond attitudes of ___ in pitch or ___ in roll are prohibited.

A

+/- 30* in pitch

+/- 60* in roll

32
Q

Avoid aggressive directional or lateral control inputs greater than _____ when conducting combat maneuvers requiring a left turn. This is to prevent _________.

A

1 inch/second

excessive tail rotor scissors loads

33
Q

Avoid large pedal step inputs in arresting right hovering / low speed yawing turns greater than _____. This is to prevent _______.

A

60*/second

excessive tail rotor drive system loads

34
Q

Flight with the canopy open is prohibited, except for ______.

A

smoke/fume elimination

35
Q

Landing Limits

A

pitch change from a hover greater than 7* nose up or 12* nose down, or a roll attitude greater than 10*

36
Q

Flight into ____ or _____ ____ turbulence or into ____ _____ turbulence is prohibited

A

Flight into KNOWN or FORECAST EXTREME turbulence or into KNOWN SEVERE turbulence is prohibited

37
Q

Intentional flight into ____ or ____ ____ icing conditions is prohibited. Flight in light or trace icing is authorized _________.

A

Intentional flight into KNOWN or FORECAST MODERATE icing conditions is prohibited. Flight in light or trace icing is authorized ONLY AS A TRANSIENT CONDITION.

38
Q

Maximum airspeed for rotor start/stop

A

45 knots to prevent droop stop damage