AH-64(E) 5&9's

Question 1

Airspeed limit for external stores jettison.

Answer 1

100 KTS

Question 2

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 ___.

Answer 2

MTP
Pilot
Technical Observer
CPG
Commander

Question 3

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

Answer 3

2408-13-1

Question 4

Dual engine starts are prohibited due to insufficient ___ air.

Answer 4

IPAS

Question 5

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

Answer 5

Failed
Partial Failed

Question 6

Engine oil pressure on start can __________________________.

Answer 6

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

Question 7

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

Answer 7

0 RPM
Starter Dropout

Question 8

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

Answer 8

60 Degrees per second.

Question 9

Airspeed limits Single Engine Operating

Answer 9

67% of VNE from the Gross Weight Line

Question 10

Max wind velocity for rotor starts or stops is ___

Answer 10

45 kts

Question 11

Engine torque limits when NR < 50

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

Answer 11

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

Question 12

Maximum NP vertical tape indication is __

Answer 12

120

Question 13

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

Answer 13

130 kts

Question 14

Engine torque limits when NR <90

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

Answer 14

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

Question 15

Airspeed limit for autorotation

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

Answer 15

145 Max
70 Minimum

Question 16

Maximum airspeed with searchlight extended __

Answer 16

90 kts

Question 17

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

Answer 17

60
120

Question 18

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.

Answer 18

2
3
2
30

Question 19

Engine Starts above 61*

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

Answer 19

2
30

Question 20

TGT Limiter:

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

Answer 20

879 +- 5
903+- 5

Question 21

Aircraft Max Gross Weight

Tactical = ___
Ferry = ___

Answer 21

Tactical = 20,260
Ferry = 23,000

Question 22

Airspeed limits for rearward and sideward flight.

Answer 22

45 kts

Question 23

Landing limits:

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

*Data is NOT available above GWT ___

Answer 23

7
10
10
10

17,650

Question 24

Main transmission input drive clutch failure – in flight:

-

Answer 24

Achieve safe single engine flight conditions or land.

Question 25

APU Fire – In flight: - -

Answer 25

Illuminated APU fire button – Press Fire DISCH buttons – Press

Question 26

ENG 1 or 2 Fire – On Ground: - - -

Answer 26

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

Question 27

Single Engine Failure -

Answer 27

Achieve safe single engine flight conditions or land.

Question 28

ENG 1 or 2 Overspeed: -

Answer 28

Collective – Adjust to maintain NR within limits.

Question 29

ENG 1 or 2 Fire – In flight: - - -

Answer 29

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

Question 30

Dual Engine Failure - -

Answer 30

Autorotate Chop Button – Reset if present

Question 31

Hydraulic Failure – Primary and Utility Hydraulic PSI Low - -

Answer 31

Emergency hydraulic button – ON *Land without delay!

Question 32

Canopy Jettison - - -

Answer 32

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

Question 33

Emergency landing in wooded areas (power off) -

Answer 33

Autorotate

Question 34

Dual Engine Fuel PSI Low -

Answer 34

Fuel Page Boost Button – Press

Question 35

NP Failed Low – Low Rotor RPM -

Answer 35

Collective – Adjust to maintain NR within limits

Question 36

Flight Control Malfunction -

Answer 36

FMC release button – Press

Question 37

APU Fire – On Ground - - -

Answer 37

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

Question 38

BUCS Fail -

Answer 38

Transfer flight controls to the rear crew station.

Question 39

Engine Compressor Stall -

Answer 39

Collective – Reduce to maintain NR within limits.

Question 40

IHADSS Fail or IHADSS Stale -

Answer 40

Exit the NOE environment. *IHADSS = Integrated Helmet and Display Sight System

Question 41

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.

Answer 41

30 Min 140*C 30 Min

Question 42

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

Answer 42

100 to 105

Question 43

Transmission PSI: __ Normal (_) __ Minimum (<__ __ with box)

Answer 43

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

Question 44

NGB PSI: __ Normal (_) __ Minimum (<__ __ with box)

Answer 44

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

Question 45

Minimum hydraulic pressure required to move the flight controls.

Answer 45

1650 PSI

Question 46

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

Answer 46

Known Forecasted extreme Severe

Question 47

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

Answer 47

Known Forecasted Moderate Light Trace Transient Condition Practicable

Question 48

Emergency Shutdown: - - - -

Answer 48

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

Question 49

Hydraulic Pressure Limits: __ Transient permitted for __ seconds __ Transient permitted for __ minutes __ Normal __ Minimum

Answer 49

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

Question 50

Dual Engine Torque Limits __ Max __ Transient for __ seconds __ Normal

Answer 50

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

Question 51

ENG 1 or 2 NP Limits: __ Max __ “ENG OVERSPEED” Annunciated __ Transient __ Seconds __ Normal

Answer 51

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

Question 52

Rotor Speed Limits (NR) __ Max __ Transient __ “ROTOR HIGH” Annunciated __ Normal __ “ROTOR LOW” Annunciated __ Transient

Answer 52

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

Question 53

Airspeed limits for stores jettison: __ Max Hover to 45 - _______ 45 to 130 - _______

Answer 53

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

Question 54

Loss of tail rotor thrust – continued flight POSSIBLE: -

Answer 54

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

Question 55

Ditching (POWER OFF) - - - -

Answer 55

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

Question 56

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

Answer 56

30 seconds 2 20 minutes 3 attempts

Question 57

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

Answer 57

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

Question 58

ENG 1 or 2 Oil Pressure (PSI) Limits __ Max __ Normal __ Minimum

Answer 58

120 – Max 23-120 – Normal 23 – Minimum

Question 59

Engine Gas Generator (NG) Limits __ Max __ Transient for __ seconds __ Normal __ Minimum (ENG OUT warning annunciated)

Answer 59

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

Question 60

Main Transmission Tail Rotor Bevel-Idler - - - - -

Answer 60

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!

Question 61

NVS Failure: - -

Answer 61

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

Question 62

Tail Rotor Fixed Pitch – Forward Flight - - If pedals are jammed: -

Answer 62

Collective – Adjust to minimize yaw rate Cyclic – Oppose Yaw Break into BUCS

Question 63

Tail Rotor Fixed Pitch – Low Airspeed or Hover: - - If pedals are jammed: -

Answer 63

Collective – Adjust to minimize yaw rate Cyclic – Minimize Drift Break into BUCS

Question 64

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

Answer 64

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

Question 65

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

Answer 65

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

Question 66

Airspeed limits at 9,000’ DA and greater: Level flight = __ - __ Maneuvering flight = __ - __

Answer 66

40 – 130 57 – 108

Question 67

Dual MP Failure – MP 1 and MP 2 Fail: -

Answer 67

Exit the NOE Environment

Question 68

Single MP Operation: - OR -

Answer 68

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

Question 69

NGB Temperature Limits __ Max __ Normal

Answer 69

134 – Max 0-134 – Normal

Question 70

Transmission Temperature Limits __ Max __ Normal

Answer 70

141 – Max 32-134 - Normal