ATM Flashcards

(94 cards)

1
Q

A _______ is an operating procedure or practice that, if not correctly followed, could result _____________.

A

WARNING

in personal injury or loss of life

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2
Q

A ______ is an operating procedure or practice that, if not strictly observed, could result ______________.

A

CAUTION

in damage to or destruction of equipment

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3
Q

A ____ highlights essential information of a ________.

A

NOTE

non-threatening nature

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4
Q

What is the semi-annual flying-hour requirement for a FAC 1 aviator?

A

70 hours

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5
Q

For a dual seat designated aviator, the semi-annual flying requirement is ___ hours, of which ___ must be flown in each crew station.

A

70

15

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6
Q

How many simulation hours may be applied to an aviator’s semi-annual flying hour requirement?

A

12 hours

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7
Q

What is the semi-annual LCT requirement for a dual seat designated FAC 1 aviator?

A

15 hrs

4.5 hrs in each seat

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8
Q

What is the semi-annual NVD (NVG and NVS) requirement?

A

9.0 hours

3 hours in each device

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9
Q

To be considered NVG current, every __________ an aviator must take part in at least a _____________ while wearing NVG.

A

60 consecutive days

1-hour flight in the aircraft

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10
Q

To be considered NVS current, every _________ an aviator must take part in a _________, or a _________.

A

60 consecutive days
1-hour flight in the aircraft while using NVS
1-hour flight in the LCT while using NVS

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11
Q

An aviator must participate every _______ in a 1-hour flight in the aircraft at night while using NVS.

A

120 consecutive days

i.e. - cannot reset twice in LCT

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12
Q

What is the common condition regarding the HDU?

A

P* and P fitted with a boresighted display unit (HDU)

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13
Q

______ may approve instances when wearing an HDU during task performance is not desired.

A

The PC

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14
Q

What tasks will not be performed when performance planning indicates that OGE power is not available?

A
Alt/Airspeed Takeoff
VMC Approach (termination to an OGE hover)
Respond to Engine Failure
Instrument Takeoff
Terrain Flight (NOE)
Vertical Masking and Unmasking
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15
Q

What are the common standards for ALL tasks? (3)

A

Crew Coordination per Ch. 6 of the ATM
Do not exceed aircraft limitations
Utilize applicable terminology

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16
Q

What are the common standards for HOVER? (7)

A

Heading +/-10 degrees / Altitude +/-2’ IGE (10 OGE)
Drift - 3’ IGE or 12’ OGE
OGE - establish/announce forced landing/flyaway plan
Ground Track w/in 3’ / Constant rate of movement and turn

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17
Q

What are the common standards for IN-FLIGHT? (7)

A

Heading +/-10*, Ground track alignment w/min drift
Altitude +/-100’, Airspeed +/-10 KTAS, IVSI +/-200 FPM
Trim +/- ball width, Ack LO-BUG

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18
Q

What are the common standards for all tasks with APU or ENG(s) operating? (2)

A

Maintain Airspace Surveillance (Task 1026)

Apply appropriate environmental considerations

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19
Q

Minimum Safe Altitude (MSA) is defined as the _____

A

minimum safe height above the surface or obstacles to which the aircraft can descend in a masked condition.

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20
Q

Minimum Maneuvering Altitude (MMA) is defined as the _______.

A

altitude above the mask or barriers at which the aircraft may safely hover.

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21
Q

Visual barriers (areas so dimly viewable that a determination cannot be made if they contain barriers or obstacles) will be treated as _______.

A

physical obstacles

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22
Q

The ___ has overall responsibility for the crew mission briefing. The __ may direct the other crewmember to __________.

A

PC

perform all or part of the crew briefing

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23
Q

The crew will validate the _________ by comparing the manual or electronic performance planning and _______________ (conditions permitting).

A

aircraft PERF page

results of the hover power check

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24
Q

What are the four methods of validating the PERF Page?

A

CUR PERF mode weight, balance, and CG values
ENG 1 and ENG 2 TQ factor (ETF) values against HIT log
ENG 1 and ENG 2 TGT limiter validation
Hover Power Check

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25
In performance planning, what is the permissible range of the ATF?
0.9 to 1.0
26
In performance planning, what is the permissible range of the ETF?
0.85 to 1.0
27
A reduction in GWT of approximately ____ lbs equates to a change of approximately _ knot(s) less minimum SE airspeed and __ knot(s) greater maximum SE airspeed.
200 lbs | 1 knot, 1 knot
28
What changes in environmental conditions require a re-computation of PPC?
5*C +1,000' PA +1,000' lbs
29
One of the four standards for Preflight Inspection: Activate the ___________, select the desired format, and enter the correct data into the ____.
Load Maintenance Panel | LMP
30
The ___ will ensure a walk-around inspection is complete prior to each flight.
PC
31
Tactical situation permitting, use a flashlight _________ to supplement available lighting when performing preflight at night. _________ are difficult to see using a flashlight with a colored lens.
with an unfiltered lens | Hydraulic leaks, oil leaks, and other defects
32
The PLT (backseat crewmember) will announce ___ and ___ starts.
APU and ENG
33
The pilot not on the controls will call out ____________ checks.
before taxi, taxi, before takeoff, before landing, and after landing
34
What are the standards for Task 1026: Maintain Airspace Surveillance?
(1) Clear the aircraft. (2) Announce heading, altitude, or position changes. (3) Alert all sightings that may pose a threat. (4) Ack alerts. (5) Announce when focused inside the aircraft
35
What are the standards for Perform Ground Taxi?
``` Speed appropriate for conditions Ground track +/- 3 feet TQ Appropriate Perform Taxi Check Level Fuselage ```
36
When ground taxi-ing, increase collective to approx. ___ % TQ. High GWTs, soft, rough, or sloping terrain may require the use of more than __ % TQ.
27-30 | 30
37
During Ground Taxi - the P* may temporarily reduce taxi TQ to __ to __ percent for short periods with limited cyclic displacement to reduce negative effects of rotor downwash.
22 to 24 %
38
What are the standards for Hovering Flight
Smooth & Controlled Ascent to a Hover Hover Check near T/O point & in direction of T/O Determine if sufficient power is available for mission Smooth & Controlled Descent with min drift
39
What must the P* announce when ascending to a hover for power checks?
CG and Controllability are Good
40
What are the standards for VMC Takeoff?
HDG +/-10* until 50' off ground or clear of obstacles Ground track alignment with T/O direction A/C in trim above 50' AGL Desired Airspeed +/- 10 KTAS T/O power, not to exceed MAX TQ
41
Due to high gross weight and adverse environmental conditions, when operating at or near maximum power limits, the P* will select ______________ and monitor the ______ during takeoff.
``` the aircraft (A/C) ENG page TQ and TGT ```
42
The height velocity diagram displays "avoid areas". This diagram assumes the availability of a suitable forced landing area in case of engine failure. If surface conditions permit, the P* should _______________.
accelerate the aircraft to minimum single engine airspeed prior to establishing the desired climb rate.
43
The P* can use the _______ mode stabilator control to fine-tune drag vs. airspeed and reduce lower power requirements for a given airspeed. The P* will announce:
manual | the use of the manual stabilator
44
Compute in-flight fuel consumption within _______ of leveling off or entering into the mission profile.
15 to 30 minutes
45
Define "JOKER Fuel"
PC or unit defined fuel state above bingo. It is the point where a training event is terminated or when the flight should begin to return to base. JOKER can be exceeded at the discretion of the PC.
46
Define "BINGO Fuel"
Minimum amount of fuel necessary to fly to a refuel site with the regulatory minimum required fuel reserve. It is not negotiable or extendable.
47
What five things will the P* announce when executing a VMC Approach?
``` Beginning the Approach Terminate to a hover/ground Intended point of landing Any deviation from the approach Use of Manual Stabilator ```
48
What are the considerations for a VMC Approach to a confined area? (SBAT-w)
Size & Suitability, Barriers, Approach Direction, Touchdown & Takeoff point, Wind
49
When conducting a VMC Approach to a confined area, where should the aircrew aim the approach?
Forward 1/3 of the approach area
50
What are the standards for Slope Operations? (5)
(1) Set Parking Brake, (2) HDG +/-5*, (3) Minimum Drift, (4) Don't exceed slope limits, (5) Smooth/Controlled Descent/Ascent
51
When performing a slope landing, orient _______ if possible.
into the wind
52
To avoid ______ during a slope landing, begin to adjust the cyclic and simultaneously reduce the collective to achieve centered cyclic with no less than _______ TQ applied.
droop stop pounding | 25%
53
The Pilot NOT on the Flight Controls will select and monitor _______ during slope landings.
a FLT page
54
When performing a Slope Landing, what must the P* address?
``` Dynamic Rollover (Pivot Point, Rolling Motion, Exceed the Critical Angle) ```
55
When performing a Roll-On Landing, what must the P* announce before touchdown?
Brakes are Released Tail Wheel is Locked Area is Suitable for Landing
56
Aerodynamic braking is accomplished by applying aft cyclic with no less than _____ DE TQ, ____ SE TQ.
30%, 60%
57
A DE Roll-On landing should be accomplished at: | A SE EP Roll-On landing should be accomplished:
at or slightly above ETL | above VSSE
58
For a roll-on landing during night (aided/unaided), the rate of descent during the final ___ feet should be _________.
100 feet | slightly slower than during the day to avoid abrupt attitude changes at low altitudes
59
What are the standards for Perform Single Engine Landing? (4)
(1) A/S at or above VSSE until 10-20 ft above touchdown (2) Ground track alignment with minimum drift (3) Constant approach angle to first 1/3 of the surface (4) Runway or landing area alignment +/- 5 degrees
60
During any OGE hover or low speed OGE hovering operations, the P* will announce his ____________.
forced landing or SE flyaway plan
61
During autorotation, P* will check and call out _____.
Nr, airspeed, and aircraft in trim + any deviations
62
During autorotation, ensure that the airspeed at _____ AGL is not less than ____ KTAS.
130 feet AGL not less than 80 KTAS
63
Prior to initiating an autorotation in the aircraft, the P* will select an _______ on one MPD and direct the P to select an _____ on one MPD to SIMULATE auto-paging.
ENG page
64
Upon reaching the correct entry point, the P* will announce "___________".
ENTERING AUTOROTATION
65
During autorotation, the P* will call out ___________.
Nr, airspeed, trim and announce any deviations during the maneuver
66
An autorotation may be accomplished either "_____" or "______".
Straight In | With Turn
67
When autorotating; prior to ____ AGL, ensure a steady state autorotation is obtained. If conditions are not met, execute a _______.
200 feet AGL | Go-Around
68
When autorotating; between ______ AGL, adjust the cyclic for a smooth, progressive deceleration. Maintain ground track and apply pedal to align the aircraft with the direction of touchdown.
75 - 125 feet AGL
69
When conducting an autorotation (training/eval) in the aircraft, the P* should limit TQ to below ____ to ensure that an autorotational descent is occurring.
10%
70
When responding to NP Failed - HIGH, the malfunctioning engine should be placed in LOCKOUT and then retarded so that TQ is ____ below the good engine ________.
5% below the good engine | +/-5%
71
A locked out engine's ________ protection is disabled.
overtemperature
72
After placing a power lever to LOCKOUT, the engine can be reset by placing the power lever to _____ momentarily.
IDLE
73
When performing Rolling-Takeoff, do not allow the aircraft nose to _____________.
drop below the fuselage level until the aircraft departs the takeoff surface
74
When performing Rolling-Takeoff, position the stabilator to __________.
0 degrees trailing edge down
75
What are the procedural steps for unusual attitude recovery?
Level the pitch and back attitude Establish and maintain a heading Adjust torque to cruise or hover power as applicable Trim the aircraft as required to return to level flight
76
For Terrain Flight Takeoffs, what considerations must be analyzed? (TSLOW)
Tactical Situation <> Long Axis <> Obstacles <> Wind
77
What are the three types of terrain flight takeoffs?
Continuous Angle Altitude over Airspeed Airspeed over Altitude
78
When is a Continuous Angle terrain flight takeoff considered?
This takeoff technique should only be attempted with robust OGE power available (power available > 10% above OGE power required)
79
When is an Altitude over Airspeed terrain flight takeoff considered?
When in an area where maneuver space is limited and/or OGE hover power is marginally available
80
When is an Airspeed over Altitude terrain flight takeoff considered? A ______ must be announced.
When OGE power is not available and/or when sufficient maneuver area exists Abort takeoff point
81
Continuous Takeoff - Altitude over Airspeed Airspeed over Altitude
Robust OGE Power Limited OGE Power OGE Power not Available
82
________ remain the primary sensor for night operations and must be operational _________.
MPNVS and MTADS | prior to takeoff, and during the entire mission
83
Ground Taxi - approximately _______% TQ should be applied. Apply _______ to initiate the taxi (this will help avoid __________)
27-30 TQ as necessary excessive strap pack loads and droop stop pounding
84
Ground Taxi - depending on ground velocity and surface conditions, how may EMERG stops be performed?
wheel brakes aerodynamic braking bringing Aircraft to a hover
85
Ground Taxi - unlocking the tail wheel during rearward taxi causes the wheel to swivel 180 degrees. Use caution ______________, as this puts an excessive load on the tail wheel cam.
so that the tail wheel does not caster around suddenly
86
Ground Taxi - the P* may temporarily reduce taxi TQ to _____% for ______________ to limit the negative effects of rotor downwash. Excessive cyclic input and insufficient TQ may result in _______________.
22-24 short periods with limited cyclic displacement droop stop pounding or excessive strap pack loading
87
Ground Taxi - during SE ground taxi, ______ the required TQ for a given condition.
double
88
Ground Taxi - maintain level attitude with: T/W locked = T/W unlocked =
cyclic & pedal | cyclic
89
Ground Taxi - (SNOW/SAND/DUST) - if ground reference is lost because of snow/sand/dust, __________.
lower the collective and neutralize the flight controls until visual reference is reestablished
90
Ground Taxi - (SNOW) - when initiating ground taxi in snow or ice, apply _____________ to ________.
pressure and counter pressure to the pedals to ensure the wheels are not frozen to the ground
91
Hovering Flight - Anytime the aircraft is brought to an OGE hover, the P* will announce _______________.
his intended forced landing area or flyaway plan
92
Hover power check will be performed at a _______ and in the ______________.
5-foot stationary hover | vicinity and direction of takeoff
93
Hover Power Check - the P will monitor _______ and ______ the hover power check.
aircraft instruments | verify
94
Additional hover power checks must be performed in conjunction with the PERF page and PPC if the load or environmental conditions have increased _______.
1000' PA <> 1,000 lbs <> 5*C