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TH-67 > TH67-BWS > Flashcards

TH67-BWS Flashcards

TH67 BWS Flashcards

1
Q

NORMA

A 
Selection of Battle Position (ATP 3-04.1)
N-nature of the target
O-bbstacles
R-range to target
M-multiple firing position/lanes
A-area to maneuver
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2
Q

BRASSCRAFO

A 
Selection of Firing Positions (ATP 3-04.1)
B-background
R-range
A-altitude of target
S-sun or full moon
S-shadow
C-concealment
R-rotor wash
A-area to maneuver
F-fields of fire
O-obstacle clearance
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3
Q

GORRDDE

A 
Fundamentals of Recon
G-gain and maintain enemy contact
O-orient on recon obj
R-report all info rapidly and accurately
R-retain freedom to maneuver
D-develop situation quickly
D-do not keep recon assets in reserve
E-ensure continuous reporting
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4
Q

MSL

A

LZ/PZ Recon (Tactical)
M-mission
S-security
L-location

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5
Q

LONGLASSV

A 
LZPZ Recon (Technical)
L-landing formation 
O-obstacles
N-number and type A/C
G-ground slope
L-load availability
A-approach/departure direction
S-size of landing area
S-surface condition
V-vulnerability
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6
Q

VDWC

A 
LZPZ Recon (Met)
V-visibility
D-density altitude
W-winds
C-ceiling
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7
Q

OAKSC

A 
Holding Area Recon (Task 2067)
O-obstacles
A-avenues of app/dep
K-key terrain
S-security
C-cover and concealment
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8
Q

DRMDC

A 
Actions on Contact (Task 1413)
D-deploy to cover
R-report
M-maintain contact
D-develop situation
C-course of action
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9
Q

ATMEP

A 
Target Handover (Task 2471)
A-alert and target desc
T-target location
M-method of engagement
E-execution
P-post engagement
***Direction / Distance / Description***
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10
Q

SRSDM

A 
Ground Route Recon Planning (ATP 3-04.1)
S-start point
R-release point
S-size and comp of friendly force
D-designation of the route
M-mission time and duration
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11
Q

MMMRDFWRB

A 
Tactical Flight Mission Planning (Task 1408)
M-mission
M-map recon
M-mode of flight
R-route
D-distance
F-fuel
W-weather
R-risk assessment
B-brief
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12
Q

MPH

A

Hazards to Terrain Flight (Task 1408)
M-meteorological WX
P-Physical (Man-made/Natural)
H-human

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13
Q

TSLOW

A 
Approach Considerations (Task 1409)
T-tactical
S-suitability
L-long axis
O-obstacles
W-wind
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14
Q

SLOW

A 
Takeoff Considerations (Task 1407)
S-situation
L-long axis
O-obstacles
W-wind
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15
Q

GAF

A

Wind Recognition (Task 1052.09)
G-ground cues
A-aircraft cues
F-foretasted winds

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16
Q

Fundamentals of Reconnaissance

A 
GORRDDE
G-gain and maintain enemy contact
O-orient on recon obj
R-report all info rapidly and accurately
R-retain freedom to maneuver
D-develop situation quickly
D-do not keep recon assets in reserve
E-ensure continuous reporting
17
Q

LZ/PZ Recon (Tactical)

A

MSL
M-mission
S-security
L-location

18
Q

LZ/PZ Recon (Technical)

A 
LONGLASSV
L-landing formation 
O-obstacles
N-number and type A/C
G-ground slope
L-load availability
A-approach/departure direction
S-size of landing area
S-surface condition
V-vulnerability
19
Q

Tactical Flight Mission Planning

A 
MMMRDFWRB
M-mission
M-map recon
M-mode of flight
R-route
D-distance
F-fuel
W-weather
R-risk assessment
B-brief
20
Q

Wind Recognition Cues

A

GAF
G-ground cues
A-aircraft cues
F-foretasted winds

21
Q

Approach Considerations

A 
TSLOW
T-tactical
S-suitability
L-long axis
O-obstacles
W-wind
22
Q

Takeoff Considerations

A 
SLOW
S-situation
L-long axis
O-obstacles
W-wind
23
Q

Ground Route Recon Planning

A 
SRSDM
S-start point
R-release point
S-size and comp of friendly force
D-designation of the route
M-mission time and duration
24
Q

Hazards to Terrain Flight

A

MPH
M-meteorological WX
P-Physical (Man-made/Natural)
H-human

25
Q

Actions on Contact

A 
DRMDC
D-deploy to cover
R-report
M-maintain contact
D-develop situation
C-course of action
26
Q

LZ/PZ Recon (Met)

A 
VDWC
V-visibility
D-density altitude
W-winds
C-ceiling
27
Q

Holding Area Recon

A 
OAKSC
O-obstacles
A-avenues of app/dep
K-key terrain
S-security
C-cover and concealment
28
Q

SPOT Report

A 
SALUTE/SALT-W
S-size
A-activity
L-location
U-unit
T-time
E-equipment
Size Activity Location Time - WhatDoing
29
Q

Slope Abort Criteria

A 
CAMPS
C-cyclic limits
A-aircraft limits
M-mast bumping
P-personal/physical limits
S-sliding
30
Q

Aerial Observation

A 
DILR
D-detect
I-identify
L-locate
R-report
31
Q

Factors that Affect Visual Search

A 
WATCH
W-weather
A-airspeed
T-terrain
C-cues
H-human eye
32
Q

Visual Cues for Visual Search

A 
MCLOSSTT
M-movement
C-color
L-light
O-obvious sightings
S-shadows
S-smoke
T-texture
T-trails
33
Q

LTE (Ch8) DESCRIBE

A
  • -is the occurrence of an uncommanded and rapid right yaw rate which does not subside of its own accord and which, if not quickly reacted to, can result in loss of aircraft control.
    1. WeathercockStability(120-240)
  • winds weathervane a/c into relative wind
  • slow uncommanded yaw left or right
  • right yaw can develop into an LTE
    2. Vortex Ring(210-330)
  • vortex ring state develops around tail rotor
  • uncommanded pitch, roll, and yaw
  • maintaining a precise heading will be impossible
  • pilot workload high
    3. Disc Vortex(280-330)
  • main rotor tip vortices to be directed onto the tail rotor
  • tail rotor operates in an extremely turbulent environment
  • sudden uncommanded right yaw, if uncorrected, develops into spin
34
Q

LTE (Ch9) EMERGENCY

A

This is a situation involving a loss of effective tail rotor thrust WITHOUT a break in the drive system which CANNOT be stopped with full left pedal application. If LTE is experienced, SIMULTANEOUSLY:

  • PEDAL: FULL LEFT.
  • CYCLIC: FORWARD
  • As recovery is affected, adjust controls for normal flight.
  • If spin cannot be stopped and crash is imminent, an AUTO may be the best course of action. Maintain full left pedal until the spin stops, then adjust to maintain heading.

WARNING: COLLECTIVE REDUCTION will aid in arresting the yaw rate; however, if a rate of descent has been established, collective reduction may increase the rate of descent to an excessive value. The resultant large and rapid increase in collective to prevent ground or obstacle contact may further increase the yaw rate, decrease the rotor RPM and cause an over torque and/or over-temperature condition. Therefore, the decision to reduce collective must be based on the pilot assessment of the altitude available for recovery.

35
Q

Dynamic Rollover

A 
A helicopter is susceptible to a lateral-rolling tendency called dynamic rollover. Dynamic rollover can occur on level ground as well as during a slope or crosswind landing and takeoff. Three conditions are required for dynamic rollover:
--pivot point
   right skid downslope
--rolling motion
   left pedal inputs, lateral loading
--exceed critical angle
   crosswind and high roll rates
PHYSICAL FACTORS (MAST-C):
-Main Rotor Thrust
-Aircraft CG/Low fuel
-Sloped landing area
-Tail-rotor thrust
-Crosswind
HUMAN FACTORS:
-Failure to make timely control movements
-Loss of visual reference points
-Inexperience
-Inattention

TH-67 (3 decks)

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