AH-64(E) 5&9's Flashcards

1
Q

Airspeed limit for external stores jettison.

A

100 KTS

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2
Q

The minimum crew required for maintenance ground runs (engine running) is an ___ occupying the ___ station. A ___ may be authorized to occupy the ___ station at the discretion of the ___.

A

MTP
Pilot
Technical Observer
CPG
Commander

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3
Q

If limits are exceeded, entries shall be made on a DA Form ___-__-_

A

2408-13-1

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4
Q

Dual engine starts are prohibited due to insufficient ___ air.

A

IPAS

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5
Q

Force trim will not be turned off except in a ___ or ___ ___ mode.

A

Failed
Partial Failed

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6
Q

Engine oil pressure on start can __________________________.

A

Can be high but must return to normal limits after 5 minutes at idle.

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7
Q

A starting cycle is the interval from start initiation and acceleration of output driveshaft, from ___ RPM, to ___ ___.

A

0 RPM
Starter Dropout

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8
Q

Avoid large pedal step inputs in arresting right hovering/low speed lawing turns greater than ___.

A

60 Degrees per second.

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9
Q

Airspeed limits Single Engine Operating

A

67% of VNE from the Gross Weight Line

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10
Q

Max wind velocity for rotor starts or stops is ___

A

45 kts

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11
Q

Engine torque limits when NR < 50

__ Max (>__ __)
__ Normal (__)

A

30 Max (>30 Red)
0-30 Normal (Green)

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12
Q

Maximum NP vertical tape indication is __

A

120

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13
Q

Airspeed limits with Crashworthy External Fuel System (CEFS) installed is ___

A

130 kts

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14
Q

Engine torque limits when NR <90

__ Max (>__ __)
__ Normal (__)

A

70 Max (>70 Red)
0-70 (Green)

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15
Q

Airspeed limit for autorotation

Maximum (Limit) = __
Minimum (ATM Procedure) = __

A

145 Max
70 Minimum

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16
Q

Maximum airspeed with searchlight extended __

A

90 kts

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17
Q

Intentional maneuvers beyond attitudes of ___ in pitch and ___ in roll are prohibited.

A

60
120

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18
Q

Engine Starts 61* and below:

__ Consecutive start cycles may be made, followed by a __ minute rest period, followed by __ additional consecutive start cycles. A __ minute rest period is then required.

A

2
3
2
30

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19
Q

Engine Starts above 61*

__ Consecutive start cycles may be made, then a __ minute rest period is required.

A

2
30

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20
Q

TGT Limiter:

Dual Engine: ___+- ___
Single Engine: ___+-___

A

879 +- 5
903+- 5

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21
Q

Aircraft Max Gross Weight

Tactical = ___
Ferry = ___

A

Tactical = 20,260
Ferry = 23,000

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22
Q

Airspeed limits for rearward and sideward flight.

A

45 kts

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23
Q

Landing limits:

Nose up: ___
Nose down: ___
Left wheel low: ___
Right wheel low: ___

*Data is NOT available above GWT ___

A

7
10
10
10

17,650

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24
Q

Main transmission input drive clutch failure – in flight:

-

A

Achieve safe single engine flight conditions or land.

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25
Q

APU Fire – In flight:

A

Illuminated APU fire button – Press
Fire DISCH buttons – Press

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26
Q

ENG 1 or 2 Fire – On Ground:

-

A

Power Levers – OFF
Illuminated ENG fire button – Press
Fire DISCH buttons – Press

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27
Q

Single Engine Failure

-

A

Achieve safe single engine flight conditions or land.

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28
Q

ENG 1 or 2 Overspeed:

-

A

Collective – Adjust to maintain NR within limits.

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29
Q

ENG 1 or 2 Fire – In flight:

-

A

Achieve safe single engine flight conditions or land.
Illuminated ENG fire button – Press
Fire DISCH button – Press

30
Q

Dual Engine Failure

A

Autorotate
Chop Button – Reset if present

31
Q

Hydraulic Failure – Primary and Utility Hydraulic PSI Low

A

Emergency hydraulic button – ON
*Land without delay!

32
Q

Canopy Jettison

-

A

Helmet Visors – Down
Area around helicopter – clear of personnel
Canopy jettison handle – operate

33
Q

Emergency landing in wooded areas (power off)

-

A

Autorotate

34
Q

Dual Engine Fuel PSI Low

-

A

Fuel Page Boost Button – Press

35
Q

NP Failed Low – Low Rotor RPM

-

A

Collective – Adjust to maintain NR within limits

36
Q

Flight Control Malfunction

-

A

FMC release button – Press

37
Q

APU Fire – On Ground

-

A

APU – OFF
Illuminated APU Fire Button – Press
Fire DISCH Button – Press

38
Q

BUCS Fail

-

A

Transfer flight controls to the rear crew station.

39
Q

Engine Compressor Stall

-

A

Collective – Reduce to maintain NR within limits.

40
Q

IHADSS Fail or IHADSS Stale

-

A

Exit the NOE environment.

*IHADSS = Integrated Helmet and Display Sight System

41
Q

Extended APU Ground Operations:

During prolonged ground operations greater than __ minutes, observe transmission temperatures on the ENG SYS page. IF temperatures exceed __ the APU shall be shutdown and the transmission fluid allowed to cool for __ minutes.

A

30 Min
140*C
30 Min

42
Q

NP split during an autorotation can increase from __ to __.

A

100 to 105

43
Q

Transmission PSI:

__ Normal (_)
__ Minimum (<__ __ with box)

A

25-100 Normal (Green)
25 Minimum (<25 red with box)

44
Q

NGB PSI:

__ Normal (_)
__ Minimum (<__ __ with box)

A

25-100 Normal (Green)
25 Minimum (<25 red with box)

45
Q

Minimum hydraulic pressure required to move the flight controls.

A

1650 PSI

46
Q

Turbulence:

Flight into __ or __ __ turbulence or into known __ turbulence is prohibited.

A

Known
Forecasted extreme
Severe

47
Q

Icing:

Intentional flight into __ or __ __conditions is prohibited. Flight in __ or __ icing is authorized ONLY as a __ __. If icing is encountered, exit __.

A

Known
Forecasted Moderate
Light
Trace
Transient Condition
Practicable

48
Q

Emergency Shutdown:

-
-

A

Power Levers – OFF
APU – OFF (if applicable)
Rotor Brake Switch – BRK
Master Ignition – OFF

49
Q

Hydraulic Pressure Limits:

__ Transient permitted for __ seconds
__ Transient permitted for __ minutes
__ Normal
__ Minimum

A

> 3410 Transient permitted for 5 seconds
3310 – 3400 transient permitted for 5 minutes
2700-3300 Normal
1260 Minimum

50
Q

Dual Engine Torque Limits

__ Max
__ Transient for __ seconds
__ Normal

A

115 Max
101-115 Transient for 6 seconds
0-100 Normal

51
Q

ENG 1 or 2 NP Limits:

__ Max
__ “ENG OVERSPEED” Annunciated
__ Transient __ Seconds
__ Normal

A

119 - MAX
114 - ENG OVERSPEED annunciated
104-119 - Transient for 12 seconds
0-103 - Normal

52
Q

Rotor Speed Limits (NR)

__ Max
__ Transient
__ “ROTOR HIGH” Annunciated
__ Normal
__ “ROTOR LOW” Annunciated
__ Transient

A

110 - Max
105-110 - Transient
105 - ROTOR HIGH Annunciated
97-104 - Normal
96.5 - ROTOR LOW Annunciated
0-96 – Transient

53
Q

Airspeed limits for stores jettison:

__ Max
Hover to 45 - _______
45 to 130 - _______

A

130 – Max
Minimize side slip (if possible)
Ball Centered

54
Q

Loss of tail rotor thrust – continued flight POSSIBLE:

-

A

Airspeed – 100 kts minimum (until 10-20 feet above touchdown)

55
Q

Ditching (POWER OFF)

-
-

A

Autorotate
Canopy – Jettison prior to entering water
Cyclic – Position in the direction of roll
Exit once rotors have stopped turning

56
Q

APU Operating Limits:

After a fault or abort, wait __ seconds.
After __ consecutive start attempts, wait __ minutes.
No more than __ attempts per hour.

A

30 seconds
2
20 minutes
3 attempts

57
Q

Single Engine Torque Limits:

__ Max
__ Transient permitted for __ seconds
__ Single Engine contingency for __ minutes
__ Single Engine Max Continuous Power (MCP)
__ Normal

A

125 – Max
121-125 – Transient for 6 seconds
111-120 – Single Engine Contingency for 2.5 minutes
110 – Single Engine Max Continuous Power
0-110 – Normal

58
Q

ENG 1 or 2 Oil Pressure (PSI) Limits

__ Max
__ Normal
__ Minimum

A

120 – Max
23-120 – Normal
23 – Minimum

59
Q

Engine Gas Generator (NG) Limits

__ Max
__ Transient for __ seconds
__ Normal
__ Minimum (ENG OUT warning annunciated)

A

106 – Max
105.1-106 – Transient for 12 seconds
63.1-105 – Normal
63 – Minimum

60
Q

Main Transmission Tail Rotor Bevel-Idler

-
-
-

A

Emergency Hydraulic Push Button – Press ON
Collective – Reduce (compromise between rate of turn and descent)
Power Levers – OFF (10-20 feet above touchdown)
Collective – Increase to cushion touchdown

Land without delay!

61
Q

NVS Failure:

A

Exit the NOE Environment
Pilot on the controls, NVS Select SW – Select Alternate Sensor

62
Q

Tail Rotor Fixed Pitch – Forward Flight

If pedals are jammed:
-

A

Collective – Adjust to minimize yaw rate
Cyclic – Oppose Yaw

Break into BUCS

63
Q

Tail Rotor Fixed Pitch – Low Airspeed or Hover:

If pedals are jammed:
-

A

Collective – Adjust to minimize yaw rate
Cyclic – Minimize Drift

Break into BUCS

64
Q

Loss of Tail Rotor Thrust – Continued Flight NOT Possible (low airspeed or hover)

-

A

Collective – Reduce (Compromise between rate of turn and descent)
Power Levers – OFF (5-10 feet above touchdown)
Collective – Increase to cushion touchdown.

65
Q

Engine Temperature Limits (TGT)

__ MAX
__ Transient for __ seconds
__ Contingency for __ minutes
__ Max rated power for __ minutes
__ Max during ENG starts
__ Intermediate rated power for __ minutes
__ Max Continuous Power
__ Normal

A

949 – Max
904-949 – Transient for 12 seconds
880-903 – Contingency for 2.5 minutes
847-879 – Max rater power for 10 minutes
851 – Max during ENG start
794-846 – Intermediate Rated Power for 30 minutes
793 – Max continuous power
0-793 – Normal

66
Q

Airspeed limits at 9,000’ DA and greater:

Level flight = __ - __
Maneuvering flight = __ - __

A

40 – 130
57 – 108

67
Q

Dual MP Failure – MP 1 and MP 2 Fail:

-

A

Exit the NOE Environment

68
Q

Single MP Operation:

-
OR
-

A

NVS Select Switch – Reselect
OR
Crewmember (NOT on the controls) – Assume the controls

69
Q

NGB Temperature Limits

__ Max
__ Normal

A

134 – Max
0-134 – Normal

70
Q

Transmission Temperature Limits

__ Max
__ Normal

A

141 – Max
32-134 - Normal