Chapter 8 - Normal Procedures

Question 1

Mission planning begins when the _______ and extends to the ______ of the helicopter. It includes:

Answer 1

mission is assigned <> preflight

Check of limits/restrictions, Weight/Balance, PPC, Pubs, Flight Plan, Crew Briefing

Question 2

Mission related information may be transferred to the aircraft ______.

Answer 2

via the DTC

Question 3

The preflight may be made as comprehensive as _______ at the discretion of the _______.

Answer 3

conditions warrant

PC

Question 4

[WARNING] Do not preflight or postflight until __________.

Answer 4

armament systems are safe

Question 5

[WARNING] All __________ shall be installed when the helicopter is on the ground and removed prior to flight.

Answer 5

ASE and pylon safety pins

Question 6

[WARNING] During preflight, and after _______ when the AWS was used, the barrel will be inspected for ______.

Answer 6

all live fires

cracks

Question 7

[NOTE] Check ________ to verify rocket zone loading in addition to physical check.

Answer 7

Load Maintenance Panel (LMP)

Question 8

[CAUTION] Closing two or more gaspers will cause the blower to operate in a _______, increasing _____. Operating will all gaspers closed may cause ________.

Answer 8

stall region….. noise levels

the blower to overheat and shutdown

Question 9

[CAUTION] To prevent heat damage to the SP, the APU must be started with ____ of the initiation of battery ops when FAT > ___, within ____ when FAT is ____, and within ___ when FAT < ___.

Answer 9

1 minute - FAT > 43C
3 minute - FAT 32-43C
20 min - FAT < 32*C

Question 10

[NOTE] When starting the A/C on EXT PWR, pausing at the BATT position for more than ____ before rotating the MSTR IGN switch to the EXT PWR position will ____.

Answer 10

10 seconds

preclude the IDM from functioning

Question 11

[WARNING] To prevent injury to personnel, ensure _________ are clear prior to operating the APU.

Answer 11

pylons/stabilator

Question 12

[WARNING] Do not _________ with ____ engaged. ______ engagement may be cleared by applying hydraulic power and completing a __________.

Answer 12

start engines…. BUCS

BUCS….. FLT CNTRLS IBIT

Question 13

[NOTE] Loss of aircraft power to DEC will generate ______.

Answer 13

No fault codes

Question 14

[NOTE] Maintenance action is required after _____ failures of the ______ IBIT.

Answer 14

two consecutive

FLT CNTRLS

Question 15

[CAUTION] The crew will ensure that both EGIs have ______. This will prevent erroneous velocity data signals from the EGIs being sent to the FMC, which ______.

Answer 15

aligned properly

should prevent an uncommanded scheduling of the stabilator.

Question 16

[CAUTION] In the event that one or both EGIs will not align after initial startup or after performing ON-ground Manual Reset and Alignment Procedures, _______.

Answer 16

the aircraft shall not be flown until cleared by maintenance personnel.

Question 17

[CAUTION] With both EGIs disabled, _________. Manual control of the stabilator will be required. The ____ will remain operational if required.

Answer 17

FMC functions such as SAS and Hold Modes will not be available….. BUCS

Question 18

[CAUTION] Engine starts above ________, may be unsuccessful and require an abort because of exceeding the temperature limits.

Answer 18

6000’ Density Altitude

Question 19

[CAUTION] If nose gearbox heaters are active and left powered on for an extended period of time, ______________.

Answer 19

damage could result to the nose gearbox housing.

Question 20

[CAUTION] During a rotor brake LOCK start, if rotor blades begin to rotate: Set RTR BRK switch to - ____.

Answer 20

OFF

Question 21

[CAUTION] If ENG 1 or ENG 2 start advisory remains displayed after ________: Position ENG START switch to IGN ORIDE, then _____.

Answer 21

66%-68% Ng

OFF

Question 22

[CAUTION] During ENG Start, TGT must be less than ____ before moving the power lever to IDLE.

Answer 22

80*C

Question 23

A “Normal Start” is used if the engine was shutdown at least _______ ago.

Answer 23

4 hours

Question 24

During WARM start: IGN ORIDE, allow ___ to increase to _____ then OFF. After the first engine is placed in the OFF position, motoring of the second engine is permitted.

Answer 24

Ng

18%-20%

Question 25

When performing a cross-start (no APU), ensure Ng of opposite engine is ___ Ng. This will ensure sufficient IPAS air is supplied.

Answer 25

95% Ng

Question 26

[CAUTION] Prior advancing POWER levers, ensure that both engines are stabilized (________).

Answer 26

Np, Ng, TQ, and Oil PSI

Question 27

[CAUTION] While advancing POWER levers to FLY, ensure that both engines indicate a rise in ___ to confirm that the ___________ are engaged.

Answer 27

TQ | sprag clutches

Question 28

[CAUTION] If an engine indicates near 0% TQ, _______.

Answer 28

retard POWER lever of affected ENG to OFF

Question 29

[WARNING] Do not cycle anti-ice bleed and start valve more than _____ to determine _________. Valve malfunction can cause ENG flameout. Do NOT fly the aircraft if TGT rise is less than ____ or switch cycling is required.

Answer 29

ONCE.... proper operation | 50*C

Question 30

[CAUTION] When operating at high power settings, ensure anti-ice is in the _ mode. Failure of the anti-ice/detector during _ _ _ could result in severe Np/Nr droop.

Answer 30

MANUAL | high power settings

Question 31

[NOTE] When using TGT reference table, FAT must be rounded _ and pressure altitude must be _ _ to the nearest value.

Answer 31

up | rounded off

Question 32

[NOTE] If the UNLOCK pushbutton fails to illuminate, _ _ _ _ _ _ _ light pedal inputs.

Answer 32

taxi forward a short distance while making

Question 33

[CAUTION] Excessive cyclic displacement with low power settings will result in _ _ _.

Answer 33

droop stop pounding

Question 34

[CAUTION] Excessive forward cyclic displacement with low power settings will result in _ _ _ _.

Answer 34

high strap pack loads

Question 35

[NOTE] If you have been operating the TADS/PNVS on the ground for _ _ _ _, perform a _ before takeoff.

Answer 35

15 minutes or longer | SANUC

Question 36

[NOTE] Anytime the load or environmental conditions increase significantly (_ _ _ _, _, or _ _), the aircrew will perform additional power checks.

Answer 36

1,000 lbs gross weight, 5*C, or 1,000' PA

Question 37

NOE/A mode may be engaged at any time, however stabilator will not schedule until TAS < _ KTAS.

Answer 37

80 KTAS

Question 38

The MANUAL stabilator mode is used for positioning the stabilator to help minimize _ _ _ _ _ _ _ _ _.

Answer 38

minimize airframe vibrations when hovering in crosswinds or tail winds

Question 39

[NOTE] Prior to landing, external stores may be placed in the _ _ _ by selecting the _ _ button on the WPN UTIL page.

Answer 39

ground stow position | GROUND STOW

Question 40

[WARNING] The potential exists for accidental dispensing of CMDS during hot reload. The CMDS must be selected as _ on the _ page of the MPD and the safety pin installed by the ground crew.

Answer 40

SAFE on the ASE page

Question 41

[CAUTION] PLT and CPG shall perform their _ _ _ prior to entering the FARP.

Answer 41

armament safety checks

Question 42

[CAUTION] Radio transmissions shall be limited to _ _ _ until refueling has been completed.

Answer 42

EMERGENCIES ONLY

Question 43

[NOTE] When icing conditions exist or are predicted, the _____ located on each hellfire launcher must be manually placed in the ____ position.

Answer 43

ARM/SAFE | ARM

Question 44

[NOTE] When icing conditions exist, ensure that TADS/PNVS _______ are free of ___.

Answer 44

gear teeth | ice

Question 45

[NOTE] Some thru-flight data will be lost unless the THRU-FLIGHT button is selected within ____ of power-up.

Answer 45

one minute

Question 46

[NOTE] Loss of aircraft power to the DEC will generate _______.

Answer 46

no fault codes

Question 47

[NOTE] If one or both EGIs displays a position error greater than ____ from the AC's known position, or if EGI OP Check is out of tolerance, ______.

Answer 47

one nautical mile | perform the on ground manual reset and alignment procedure

Question 48

[NOTE] If HDG selection is not displayed or is removed while the current position data is being entered, ________ and then quickly _____ re-enter the current position.

Answer 48

perform an INU1 and INU2 reset | within one minute

Question 49

[NOTE] When using TGT reference table, FAT must be rounded ___ and PA must be rounded off to the _____.

Answer 49

UP | nearest value

Question 50

[CAUTION] To prevent damage to the engines, the AI system shall be manually activated when _________.

Answer 50

the aircraft is flown in visible moisture and the FAT is less than 5*C

Question 51

[CAUTION] When operating at high power settings, ensure AI is in the ____ mode. Failure of the AI/detector during high power settings could result in _____.

Answer 51

manual | sever Np/Nr droop

Question 52

[CAUTION] Care should be exercised when operating the helicopter in rough terrain to prevent damage to the _____.

Answer 52

underside antennae

Question 53

[CAUTION] When conducting RAPID refueling / rearming, the BFT must be _____.

Answer 53

switched OFF to prevent it from emitting network pings

Question 54

[CAUTION] If the APU is INOP got to _______. Failure to comply will result in loss of operating systems displays and indicating systems during shutdown

Answer 54

ENGINE SHUTDOWN (EXT PWR) PLT/CPG

Question 55

[CAUTION] If an ENG is shut down EMER Shutdown without cooling for 2 min and it must be restarted, it must be done within ___ or must be allowed to cool for ____.

Answer 55

5 minutes | 4 hours

Question 56

[CAUTION] In the event of an Nr sensor malfunction, go to ________. Failure to follow this procedure could result in damage to ______.

Answer 56

``` ENG SHUTDOWN (EXT PWR) PLT/CPG APU, APU clutch, APU driveshaft and XMSN ACC Gearbox ```

Question 57

[NOTE] APU may be started at anytime when the aircraft is _____.

Answer 57

on the ground

Question 58

How long may HIT/A-ICE checks be deterred when operating in adverse conditions (dust, desert, beach, river bed)

Answer 58

5 flight hours maximum

Question 59

[CAUTION] Ice removal shall never be done by _______. Remove ice by _____.

Answer 59

scraping or chipping | applying heat or de-ice liquid

Question 60

[WARNING] When between 4.5*C and 21*C and > 70% humidity: set cockpit temperature to ____ and select ____. Select _____ for the remainder of the flight.

Answer 60

60*F DEFOG OFF | CANOPY ANTI-ICE ON

Question 61

[NOTE] If a crewmember must change the cockpit temperature, change the temperature in ______ IOT prevent ____.

Answer 61

one cockpit at a time | the possibility of both cockpits fogging at the same time

Question 62

[CAUTION] Between __ and ___*C, the TADS should be manually selected off after powerup IOT prevent degradation / damage.

Answer 62

4*C - 30*C

Question 63

What is the maximum wind velocity for rotor start or stop?

Answer 63

45 KTAS

Question 64

For moderate turbulence, what should airspeed be limited to?

Answer 64

150 KTAS