80T-105 Cv Natops Chpt 3-6

Front 1

The --- officer shall be responsible for the control of airborne aircraft except when control is assigned to other authority

Back 1

Operations

Front 2

The ----- officer is responsible to the operations officer for coordination of all matters pertaining to flight operations the proper functioning of the CATCC and shall determine the type of approach and required degree of control

Back 2

Air operations

Front 3

This officer determines the case launch and/or recovery

Back 3

Air officer

Front 4

This officer is responsible for visual control of all aircraft operating in the Carrier control zone

Back 4

Air officer

Front 5

Under supervision of the air officer the --- is responsible for the visual control of aircraft in the terminal phase of the approach immediately prior to landing

Back 5

LSO

Front 6

All signals given by the LSE are advisory with the exception of the "---- " and "----" which in all cases are mandatory

Back 6

Wave off & hold

Front 7

The pilot is responsible for the safe and orderly conduct of the flight as directed by which manual

Back 7

OPNAVINST 3710.7

Front 8

This officer is responsible for mission control of aircraft assigned to him or her

Back 8

CDC officer

Front 9

What is the most prominent factor in the Carrier controls on the effects the type of departure and/or recovery

Back 9

Weather

Front 10

During case I the ceiling and visibility in the carrier control zone are no lower than --- feet and --- nautical miles respectively

Back 10

3000ft/5nm

Front 11

During case II the ceiling and visibility in the Carrier controls on are no lower than --- feet and --- nm respectively

Back 11

1000ft/5nm

Front 12

During case III the ceiling or visibility in the Carrier control zone on are lower than --- feet and --- nm respectively; or

Back 12

1000ft/5nm Or a nighttime departure or recovery (1/2 hour after sunset and 1/2 hour before sunrise)

Front 13

What are the 4 degrees of control

Back 13

Positive

advisory

monitor

non radar

Front 14

Positive control shall be used when controlling helicopters if the ceiling is lower than how many feet

Back 14

500

Front 15

The control shall be utilized when the traffic density in an operating area requires a higher degree of control for safety of flight than required under visual flight rules

Back 15

Advisory

Front 16

This control shall be utilized only when aircraft are operating VMC outside controlled airspace and the responsibility for separation from other traffic can be safely assumed by the pilot

Back 16

Monitor

Front 17

This control shall be used when shipboard radar is an operative or so degraded as to be inadequate to provide radar separation of air traffic under conditions normally requiring positive control

Back 17

Nonradar

Front 18

This officer is responsible for EMCON

Back 18

Operations officer

Front 19

COD Aircraft will attempt to establish communications in route prior to arriving on station if no radio contact is made the COD will

Back 19

Return to base

Front 20

This officer shall be responsible for setting the proper HERO conditions for control of radar and radio emissions while handling ordinance susceptible to RF energy

Back 20

Operation

Front 21

Aircraft operating at 50 miles or more from the monitoring antenna shall be separated by a minimum of --- miles

Back 21

5mi

Front 22

Aircraft operating less than 50 miles from the monitoring antenna shall be separated by a minimum of --- miles

Back 22

3

Front 23

Aircraft on a designated approach or established downwind and inside of 12 miles shall be separated by a minimum of --- miles

Back 23

2

Front 24

Aircraft established on final within 5 miles she'll be separated a minimum of --- miles

Back 24

1 1/2mi

Front 25

Air search radars that rotate in excess of ---- RPM are the only radar acceptable for an ASR approach

Back 25

7 rpm

Front 26

Aircraft provided positive control with air search radars that do not rotate in excess of 7 RPM shall be separated by a minimum of --- miles

Back 26

5mi

Front 27

Aircraft provided non radar control, utilizing a published approach should be separated by how many miles/ minutes

Back 27

2 minutes/ 5 miles separation when using DME

Front 28

Roman01 Has boltered and is climbing to angels 1.2 expecting a turn downwind; shooter22 has just reported abeam with a state of 5.6 what is the minimum required lateral separation between the two aircraft

Back 28

2 mi

Front 29

Shooter13 is level angels 1.2 dirty passing through the 3NM fix on final; what is the closest the next aircraft following shooter13 can be on final

Back 29

4.5nm

Front 30

Jet and Turboprop aircraft operating at altitude's up to and including FL --- shall be separated by 1000'

Back 30

FL290

Front 31

Vertical separation May be reduced to 800' when inside of --- nm

Back 31

12

Front 32

Receiver aircraft being provided positive control so be separated by a minimum of --- feet vertically from tinker aircraft until visual separation between the two aircraft can be maintained

Back 32

500 ft

Front 33

If the tanker aircraft is holding overhead mother at angel's 3 and an aircraft is directed to signal tank trick or treat for two what minimum altitude should the receiver aircraft be issued

Back 33

Angels 2.5

Front 34

Aircraft operating above F L2 90 she'll be separated by --- feet

Back 34

2000ft

Front 35

Helicopters shall be separated by ---feet vertically

Back 35

500ft

Front 36

Ships call sign shall be used on initial contact with which control position

Back 36

Marshal

Front 37

Radio circuits used for the control of air traffic shall be recorded how often during hours of operation

Back 37

Continuously

Front 38

CATCC Shall ensure --- frequencies are recorded during case I/case II operation

Back 38

Prifly

Front 39

What are three broad categories of aircraft emergencies

Back 39

Communication failure

NAVAID Failure

Other aircraft system failures

Front 40

Aircraft in a state of emergency within visual range of the ship will normally be controlled by

Back 40

Air officer

Front 41

Outside the visual range of the ship aircraft in an emergency she'll be controlled by either ---/---

Back 41

CDC/CATCC

Front 42

CATCC Shall conduct a radio check with the plane guard helicopter at least every --- minutes during case III

Back 42

20min

Front 43

The designated plane guard helicopter is on station when operating within --- (day) or --- (night) of the Carrier

Back 43

20nm/10nm

Front 44

During recovery of aircraft with Forward firing ordinance a plane guard helicopter shall not be positioned on the starboard side from the ---- to the --- degree relative bearing within ---nm from the Carrier

Back 44

360-090 / 5nm

Front 45

Which mode I Squawk means desire tanker to join

Back 45

70

Front 46

Which mode I Squawk means intend bingo

Back 46

71

Front 47

Which mode I Squawk means desire acft to assist

Back 47

72

Front 48

What does the "H" in HEFOE stand for

Back 48

Hydraulic

Front 49

What does the last "E" in HEFOE stand for

Back 49

Engine

Front 50

Approximately --- minutes before launch flight crews will be ordered to man aircraft

Back 50

45

Front 51

Helicopters shall take departure to port holding and shall not cross the bow within --- miles or the Stern within --- miles

Back 51

5mi/3mi

Front 52

The aircraft's crew shall be ready for flight in all aspects in which alert launch position

Back 52

Alert condition I

Front 53

In which alert launch position can minor maintenance be performed

Back 53

Alert condition IV

Front 54

The minimum standard separation of departure radials under instrument conditions is --- degrees

Back 54

20°

Front 55

The assignment of departure radials is normally dependent on what 3 factors

Back 55

-Number of carriers in the formation

-Mission of the aircraft

-Those radials reserved for emergencies, letdowns, or helicopter holding

Front 56

Aircraft shall normally launch on the departure frequency that shall be monitored by the ---

Back 56

Tower

Front 57

Condition and CAP launches will be on a frequency designated by --- and monitored by the tower

Back 57

CDC

Front 58

Single piloted aircraft that are assigned operating altitudes below --- feet shall not change frequencies or IFF/SIF codes until a level altitude and cruise configuration have been attained

Back 58

2500ft

Front 59

If an aircraft has lost communications during departure and it's on top/IMC the aircraft will proceed to the applicable emergency Marshall and commence a descent to depart that fixed at---

Back 59

EEAT

Front 60

A mandatory report for departing aircraft passing FL180 (or assigned departure altitude if lower) if not on top

Back 60

Popeye

Front 61

In the event of lost communications and the aircraft has a TACAN DME failure with good azimuth, the aircraft shall proceed to approximately --- miles reverse course and proceed inbound on the assigned departure radial at the emergency Marshal assigned altitude, and enter overhead

Back 61

50 mi

Front 62

In the event of lost communications and the aircraft has a TACAN failure with good azimuth and good DME, the aircraft will proceed inbound on the departure radial, climbing or descending to the emergency Marshal assigned altitude after holding for --- minutes

Back 62

30 min

Front 63

Helicopters experiencing lost communications should remain at or below --- feet and Arc To enter starboard Delta

Back 63

300 ft

Front 64

After a clearing turn case I departure jets/Turboprops proceed straight ahead paralleling the BRC at --- feet until NM

Back 64

500ft/7nm

Front 65

After a clearing turn jet aircraft on a case II departure proceed straight ahead at 500' paralleling the BRC at --- NM turn to intercept the --- arc maintaining visual conditions until established on the departure radial

Back 65

7nm/10nm

Front 66

During a case to jet departure the 500' restriction is lifted after -- NM if the climb can be continued in visual conditions jets shall maintain --- knots until VMC on top

Back 66

7nm/300kts

Front 67

After a clearing turn, Turboprop aircraft on a case II departure parallel the BRC at 500'. at --- NM, turn to intercept the --- NM arc, maintaining visual conditions until established outbound on the departure radial

Back 67

6nm/7nm

Front 68

Turboprop aircraft on a case II departure maintain -- feet until 12 NM on the departure radial

Back 68

500ft

Front 69

COD Aircraft will depart straight ahead unless otherwise directed and maintain --- feet until --- NM during a case II departure

Back 69

500ft/12nm

Front 70

A minimum launch interval of --- sec shall be used between aircraft during case III departures

Back 70

30sec

Front 71

When possible a --- second interval will be provided when launching a jet aircraft following a Turboprop

Back 71

60sec

Front 72

Jet aircraft climb straight ahead accelerating to 300 knots crossing 5nm at --- feet or above during a case III departure

Back 72

1500ft

Front 73

At 7nm during a case III jet departure aircraft execute turn to fly the --- NM arc until intercepting the departure radial

Back 73

10 nm

Front 74

Turboprop aircraft climb straight ahead to --- ft, accelerating to --- knots after level off during a case III departure

Back 74

1000ft/250kts

Front 75

Turboprop aircraft maintain --- feet until --- nm on the departure radial during a case III departure

Back 75

1000ft/12nm

Front 76

During a case III departure COD aircraft shell depart straight ahead unless otherwise directed and maintain 1000' until ---nm

Back 76

12nm

Front 77

Case II/III shall rendezvous between --- miles from the Carrier on the left side of the departure radial at a prebriefed altitude

Back 77

20 & 50 mi

Front 78

During a case III helicopter departure, the aircraft will Arc Within --- miles to intercept the assigned departure radial and climb to departure altitude & will commence on the departure radial outside --- nm

Back 78

3mi/12nm

Front 79

Transient helicopters approaching the Carrier for landing shall contact Marshall control at least --- miles out

Back 79

25mi

Front 80

During --- recoveries of fixed wing aircraft, shall not be conducted currently with case III departures

Back 80

Case I/II

Front 81

During a case one recovery aircraft shall normally be switched to tower control at --- nm after reporting the ship in sight

Back 81

10nm

Front 82

The jet and Turboprop port holding pattern is a left hand pattern tangent to the BRC or expected BRC with the ship in the ---- position and a maximum diameter of --- nm

Back 82

3 o'clock/5nm

Front 83

Flights shall be established at their assigned port holding pattern altitude --- nm prior to entering the pattern

Back 83

10nm

Front 84

In the port holding/ spin pattern, a minimum of --- feet vertical separation between holding altitudes shall be maintained

Back 84

1000ft

Front 85

What is the minimum altitude assigned for the port holding pattern

Back 85

2000ft MSL

Front 86

A low overhead port holding pattern at --- feet may be used at the discretion of the --- and should be used as the primary method of recovering COD aircraft and/or other aircraft with a requirement to recover first

Back 86

1200ft/Air Officer

Front 87

Where shall departure from the port holding pattern for break entry be accomplished

Back 87

Aft of the ships beam

Front 88

Where should a spin normally be initiated

Back 88

At the bow

Front 89

The spin pattern shall be flown at --- feet within --- nm of the ship

Back 89

1200ft/3nm

Front 90

A maximum of --- aircraft shall be in the landing pattern at one time

Back 90

6

Front 91

No aircraft shall break more than --- miles ahead of the ship

Back 91

4mi

Front 92

What is The landing pattern altitude

Back 92

600ft

Front 93

The COD starboard holding pattern shall be a right hand racetrack pattern between --- and --- relative to the BRC

Back 93

045 & 135 degrees

Hint 93

#'s should equal 90°

Front 94

The COD starboard holding pattern shall be flown at --- feet or at --- feet if approved by the airbus with the closest point of approach no closer then --- nm

Back 94

500ft/1000ft/1nm

Front 95

Unless previously brief to the contrary when more than one helicopter is operating in the holding pattern all helicopter shall fly a --- hand pattern at --- feet maintaining --- knots

Back 95

Right/300ft/80kts

Front 96

Entry into the brake shall be made at --- feet

Back 96

800ft

Front 97

The landing pattern downwind leg is flown at 600', --- nm abeam the ship's stern

Back 97

1 to 1 1/2nm

Front 98

When can zip lip be broken

Back 98

As required to ensure safety of light

Front 99

What is another name for a straight-in approach

Back 99

A drag approach

Front 100

If a drag approach is requested it shall be initiated at sufficient distance astern for the aircraft to be established positively on glide path and approach airspeed at a minimum of --- nm for jet/Turboprop aircraft

Back 100

1-1/2nm

Front 101

COD aircraft conducting straight-in (drag) approach from port holding or starboard Delta should be established at --- feet within --- nm AFT of the ship to de-conflict with aircraft descending to the initial (3nm astern 800') from the port holding pattern

Back 101

600ft/3nm

Front 102

Which type of recovery shall be utilized when weather conditions are such that the flight may encounter instrument conditions during the descent, but visual conditions of at least 1000' ceiling and 5 miles visibility exist at the ship

Back 102

Case II

Front 103

T/F case III Recoveries may be conducted concurrently with case I and II launches

Back 103

True

Front 104

T/F case II Recoveries shall not be conducted concurrently with case III departures

Back 104

True

Front 105

The maximum number of aircraft and a case II landing pattern is limited to

Back 105

6

Front 106

If the flight does not have the ship inside at 10nm during a case II recovery, the flight mount may descend do not less than --- feet

Back 106

800ft

Front 107

If the flight does not have the ship in sight at --- miles during a case III recovery, both aircraft shall be vectored into a Bolter/waveoff pattern and action taken to conduct a case III recovery for the remaining flights

Back 107

5mi

Front 108

Advisory control is provided by Marshal from check in until the aircraft is advised of which "----" which indicates positive control

Back 108

Radar contact

Front 109

The primary TACAN Marshal fix is the --- degree radial relative to the expected final Bearing

Back 109

180°

Front 110

The primary Marshal holding pattern for fixed wing aircraft is a --- hand, --- minute racetrack pattern

Back 110

Left/6min

Front 111

In no case will the base altitude of the primary marshal holding pattern be lower than --- feet

Back 111

6000ft

Front 112

All aircraft shall be established at their assigned Marshal attitude no closer than --- nm from the assigned Marshal fix

Back 112

10nm

Front 113

Aircraft shall avoid climbs or discents when inside --- radials from the Marshal radial on the holding side and --- radials on the non-holding side, unless under positive control

Back 113

30°/10°

Front 114

The primary TACAN Marshal holding pattern for helicopters is the --- degree radial relative to the ---

Back 114

110°/ Expected final bearing

Front 115

The primary TACAN Marshal holding pattern for helicopters is a right hand racetrack pattern with --- nm legs

Back 115

2nm

Front 116

The primary TACAN Marshal holding pattern for helicopter starts at --- feet and --- miles

Back 116

1000ft/5mi

Front 117

For multiple helicopters each successive Marshal holding fix adds --- nm of distance and --- feet of altitude

Back 117

1nm/5ft

Ex: 6nm & 1500', 7nm & 2000ft etc

Front 118

All fixed wing aircraft are issued an emergency Marshal radial--- degrees relative to the expected final bearing

Back 118

150°

Front 119

The emergency Marshal holding pattern for fixed wing aircraft is a --- hand --- minute race track pattern

Back 119

Right/6min

Front 120

Helicopter emergency Marshal radial is the same as normal helicopter Marshal radial, with helicopter emergency holding normally commencing at --- miles

Back 120

7mi

Front 121

If overhead Marshal is used as the emergency Marshal fix, EEATs should be how often

Back 121

Every other minute

Front 122

Under instrument conditions, a section of --- aircraft is the maximum number authorized in any one flight

Back 122

2

Front 123

Fixed wing aircraft will normally have a minimum of --- feet vertical separation in the Marshal pattern

Back 123

1000ft

Front 124

Vertical separation May be reduced to 800' when inside --- nm

Back 124

12nm

Front 125

Helicopters shall be separated by a minimum of --- feet vertically in the Marshal pattern

Back 125

500ft

Front 126

When overhead Marshal is utilized, the assigned outbound penetration Bearing shall be updated during recovery to maintain a minimum of --- degrees clockwise from the reciprocal of the final bearing

Back 126

25°

Front 127

Unless weather or operating circumstances dictate otherwise, aircraft departing Marshal will normally be separated by --- min

Back 127

1min

Front 128

This person establishes approach minimums that reflect significant changes in operational capabilities, such as may be occasioned by decreased proficiency of the CATCC or embarked air wing

Back 128

Commanding officer

Front 129

Jet/Turboprop aircraft shall descend at 250 knots and --- feet per minute until platform is reached, at which point the descent shall be shallowed to --- feet per minute

Back 129

4000ft/2000ft

Front 130

What altitude is platform

Back 130

5000ft

Front 131

Unless otherwise directed, aircraft shall commence transition to a landing configuration at the --- nm fix

Back 131

8nm

Front 132

Aircraft shall pass through the 6 mile DME fix at --- foot altitude --- knots, then commence slowing to final approach speed

Back 132

1200ft/150kt

Front 133

Helicopter shall descend at --- knots and --- feet per minute from Marshal, crossing 145ﾟrelative to the final bearing at or above --- feet

Back 133

90kts/500ft/900ft

Front 134

Unless otherwise directed, helicopters shall commence transition to a landing configuration prior to the --- nm fix

Back 134

3nm

Front 135

Jet or Turboprop aircraft on the CV-1 approach will correct from the Marshal radial to the final bearing at --- miles

Back 135

20mi

Front 136

The pilot shall make a gradual correction when the final bearing is within --- degrees of the reciprocal of the marshal radial

Back 136

10nm

Front 137

The pilot shall turn --- degrees when the final bearing is greater than 10ﾟ from the reciprocal of the marshal radial

Back 137

30°

Front 138

If not established on the final bearing at --- miles jet or Turboprop aircraft on the CV-1 approach shall fly the 12 mile arc until intercepting final bearing

Back 138

12mi

Front 139

If final bearing decreases on the CV-2 approach, fly --- degrees of penetration turn and Arc To the new final bearing

Back 139

90°

Front 140

If final bearing increases on the CV-2 approach, fly the standard penetration turn continuing to intercept the new final bearing prior to --- DME fix

Back 140

10 DME

Front 141

Aircraft conducting PALS mode I approaches with ceiling and visibility less than 200' and/or 1/2 mile must be equipped with an ---

Back 141

operable independent monitor

Front 142

Normally between --- to --- miles, the pilot will receive via data link a landing check discreet signal to indicate positive data link communications between aircraft and ship

Back 142

4/8mi

Front 143

The final controller will acquire the aircraft between --- and --- miles and the PALS ready/lock-on discreet light will illuminate

Back 143

3.5/8mi

Front 144

What are the minimums for a jet non- precision approach

Back 144

600ft/1-1/4mi

Front 145

What are the minimums for a jet mode I approach

Back 145

As certified

Front 146

What are the minimums for a jet mode II approach

Back 146

200ft/1/2mi

Front 147

What are the minimums for a Turboprop non-precision approach

Back 147

400ft/1mi

Front 148

What are the minimums for a jet/Turboprop mode III approach

Back 148

200ft/1/2mi

Front 149

What are the minimums for a helicopter non-precision approach

Back 149

300ft/3/4mi

Front 150

PALS mode I qualified aircraft without an operating ILM maybe certified to minimums of --- ceiling and --- visibility

Back 150

200ft/1/2mi

Front 151

How many seconds of coupled flight should be flown prior to intercepting glidepath on a mode I approach

Back 151

30sec

Front 152

Who shall suspend mode I approaches when PALS certification/ Verification restrictions (ex: WOD limits, deck motion parameters, etc) are exceeded

Back 152

CCA officer

Front 153

PALS --- approach is a training approach using needles instrument presentation mode II as well as mode III information

Back 153

Mode IIT

Front 154

During a mode III approach an aircraft usually intercepts glidepath at approximately --- miles

Back 154

3mi

Front 155

During a mode III approach helicopters shall pass the 3 mile DME fix at --- feet in a landing configuration and maintain --- feet until interception of the glidepath or until otherwise directed

Back 155

500ft/500ft

Front 156

During an ICLS approach, --- information shall be used to intercept and fly centreline and glideslope and --- information shall be used for DME information until reaching ICLS minimum

Back 156

ILM/TACAN

Front 157

When precision approach radar or suitable visual landing aids are not available, jet aircraft on final approach should continue descent to --- or --- feet from Turboprop aircraft after passing the 3 mile DME fix

Back 157

600ft/400ft

Front 158

A fixed wing aircraft bolters and radio contact is not reestablished, he will proceed downwind and commence turn to final at the --- DME or past abeam position

Back 158

4nm or 2 min

Front 159

If a helicopter is waved off and radio contact is not reestablished reenter through the --- nm DME fix or turn inbound --- minutes passed abeam

Back 159

3nm/2min

Front 160

Signal Delta shall be accompanied by the number of minutes of delay in even increments but never less than

Back 160

4

Front 161

When signal Delta is issued commenced aircraft above --- feet shall level off at the next lower odd altitude and hold on the inbound bearing at a Range in nm equal to holding altitude in thousands of feet plus base distance (angels +15)

Back 161

7000ft

Front 162

When signal Delta is issued aircraft at or below 7000' will

Back 162

Continue the approach

Front 163

To preclude two aircraft having the same EAT new EAT's Shall be issued from

Back 163

The latest to the earliest

ex: Top of the holding pattern to the bottom

Front 164

Aircraft between Marshal and 7000' that have established Delta holding and subsequently realized lost communications prior to acknowledging new EAT shall

Back 164

Commence approach immediately

Front 165

Night EMCON recovery shall be employed when operating under EMCON conditions and the ceiling and visibility are at least

Back 165

3000ft/5nm

Front 166

Helicopters shall not cross within --- miles of the ships bow and within ---miles of a ship's stern without specific approval of the air officer

Back 166

5mi/3mi

Front 167

Only those tinkers that have a known good store and sufficient fuel to meet receiver fuel requirements shall display the

Back 167

Tinker strobe pattern

Front 168

Minimum tanker pattern altitude shall be --- feet during case I/II operations

Back 168

1500ft

Front 169

Case I/II tanker pattern is a --- circle within --- nm of the CV during launch and recovery operation

Back 169

Left hand/5nm

Front 170

Tanking shall not be attempted below --- feet during case I/II and --- feet during case III

Back 170

1500ft/2500ft

Front 171

When directed to "hawk" (closely monitor) a particular aircraft that is a potential receiver, the tanker pilot should position the tanker to be at the --- position of the low state aircraft as it bolters were waves off

Back 171

2 o'clock

Front 172

The minimum altitude for a rendezvous shall be 1500' day 2500' night, ensuring a minimum of --- feet vertical separation between receiver and tanker aircraft until visual separation can be maintained

Back 172

500ft

Front 173

Unless special circumstances exist, the tanker should not proceed more than --- miles ahead of the ship

Back 173

10mi

Front 174

The tanking downwind leg should be --- miles abeam and tanking should be completed prior to reaching a point --- miles astern to allow for proper pattern entry

Back 174

3-5mi/6mi

Front 175

The tanker aircraft shall be level during the turn to final bearing and given sufficient clearance to pass through --- miles at 1200'

Back 175

6mi

Front 176

If recovery tanker is established --- feet abeam, the 6 mile gate is not required

Back 176

1200ft

Front 177

The --- is the primary visual landing aid for pilot glideslope control and is known as the ball

Back 177

IFLOLS

Front 178

An early or late commencement from Marshal is generally considered to be --- before or after the assigned EAT

Back 178

15sec

Front 179

Marshal will normally provide pilots with time information at initial check in every --- minute after marshaling commences and at ---minutes to first push

Back 179

10min/5min

Front 180

Recovery times are estimates calculated by the air boss and are referred to as --- for case I recoveries --- times for case II recoveries and --- times for case III recoveries

Back 180

Charlie time/break time/ramp time

Front 181

What is the time at which an aircraft is cleared to proceed inbound or penetrate from a preassigned fix if no further instructions are received

Back 181

EAT

Front 182

What is the time assigned prior to launch at which an aircraft is cleared to proceed inbound or penetrate from a preassigned fix under lost communications condition

Back 182

EEAT

Front 183

During case II recoveries, the air boss issues the break time to CCA with at least --- minutes prior notice

Back 183

20min

Front 184

The EAT assigned to the first aircraft or flight is --- minutes prior to the break time, as this is the amount of time required to fly the case II approach profile to the break position during case II recoveries

Back 184

5min

Front 185

The air boss issues the ramp time to CCA with at least --- minutes prior notice

Back 185

20min

Front 186

The C V-1 approach normally requires --- minutes to fly from commencement to landing

Back 186

8min

Front 187

Primary responsibility for determining aircraft configuration (gear, hook, flaps, and speed brake settings) reside with the

Back 187

LSO

Front 188

CATTC shall update fuel states every --- minutes

Back 188

10min

Front 189

The decision to divert aircraft is made by

Back 189

Commanding officer

Front 190

Marshal is responsible for the control of all aircraft in Marshal and during the initial part of the instrument approach let down until aircraft have descended to platform (-----) when control is transferred to approach

Back 190

5000' normally at 20nm

Front 191

The port holding pattern is a circular left hand pattern oriented on the BRC with the ship in the --- o'clock position maximum diameter of --- nm

Back 191

3 o'clock/5nm

Front 192

The base altitude in the port holding pattern shall not be less than --- feet

Back 192

2000ft

Front 193

Aircraft must be established at their assigned holding altitude --- nm prior to entering the low holding pattern

Back 193

20nm

Front 194

The high holding pattern is typically a circular left hand overhead pattern with the Carrier at the center of the pattern and a maximum diameter of --- nm

Back 194

10nm

Front 195

The starboard holding pattern, referred to as the starboard Delta shall be a right hand racetrack pattern between --- degrees and --- degrees relative at --- feet (1000' if approved by the air boss) oriented on the ship's heading with the closest point of approach no closer then --- nm

Back 195

045-135°/500ft/1nm

Front 196

For helicopters the starboard Delta shall be a right hand racetrack pattern between --- degrees and --- degrees relative at --- feet or below with the closest point of approach no closer then ---nm

Back 196

045-110°/300ft/1nm

Front 197

When can zip-lip be broken

Back 197

Any time an apparent safety of flight situation develops

Front 198

The initial is located --- nm astern of the Carrier at an altitude of --- feet

Back 198

3nm/800ft

Front 199

The break shall not commence at a distance of more than --- nm ahead of the Carrier

Back 199

4nm

Front 200

What is the altitude of the break

Back 200

800ft

Front 201

The case I and case II landing pattern is a --- foot left hand race track pattern oriented on the BRC with the downwind leg at a distance of --- to --- nm from the Carrier

Back 201

600ft/1 to 1 1/2nm

Front 202

Jet/ turboprop aircraft that have been authorized to conduct a straight-in approach will commence their letdown at sufficient distance from the Carrier to be established on glideslope and approach speed at a minimum distance of --- nm from the Carrier

Back 202

1.5nm

Front 203

The spin pattern is a --- foot pattern, oriented on the BRC, with a maximum distance of --- nm from the Carrier

Back 203

1200ft/3nm

Front 204

Who determines the type of instrument approach procedures and required degree of control with recommendations from the CCA watch officer and CATC supervisor

Back 204

Air Ops Watch Officer

Front 205

During a case II recovery control is provided by CATCC until aircraft are within ---nm of the Carrier and the pilot reports the Carrier in sight "see you" at which time control is transferred to PriFly

Back 205

10nm

Front 206

During a case II recovery, if the ship is not in sight at --- nm, the CCA watch officer will instruct CATCC to vector aircraft into the bolter/waveoff pattern and take action to conduct a case III recovery

Back 206

5nm

Front 207

The minimum vertical separation between aircraft and Marshal is --- feet

Back 207

1000ft

Front 208

During a case III recovery, one formation flight can hold at every other marshal altitude normally beginning with angels ---

Back 208

7

Front 209

During case II recoveries, approaches in actual instrument conditions by formation flights of more than --- are not authorized

Back 209

2

Front 210

At no time during the instrument approach letdown shall CATCC authoriz aircraft to descend below the initial altitude of --- feet during case to recovery

Back 210

???

Front 211

The minimum base altitude is --- feet for aircraft in the Marshal holding pattern

Back 211

6000ft

Front 212

T/F During case III recoveries, a flight of two will be approved for emergency purposes

Back 212

True

Front 213

During case II recoveries a --- foot vertical separation is normally assigned between flights of two, to enable one aircraft in each flight to be reassigned to the lower --- foot altitude should a transition to a case III recovery procedure be required

Back 213

2000ft/1000ft

Front 214

During case II recoveries, aircraft are often assigned a 2 minute bolter hole after the third flight, to ensure no more than --- aircraft are in the landing pattern

Back 214

6

Front 215

Why do the first aircraft departing from Marshal have a higher probability of being waved off

Back 215

Due to delays that develop in launch operations

Front 216

On a CV-1 instrument approach, aircraft are marshaled at a TACAN Marshall fix, which is located --- degrees relative to the --- at a distance of one mile for every 1000' of altitude pluse 15 miles (angels +15) and conduct an instrument approach letdown

Back 216

180°/ EFB

Front 217

The bridge provides CCA with the Fox corpin approximately --- minutes prior to commencement of each recovery

Back 217

30min

Front 218

The only constraint imposed upon having more than one Marshall fix is that the fixes shall be separated by --- degrees or more from one another and from the emergency Marshall fix

Back 218

30°

Front 219

Carriers that use the offset Marshal will normally use either --- or --- degrees

Back 219

20°/30°

Front 220

The heading to which aircraft turned to intercept the final bearing is called the

Back 220

Inbound heading

Front 221

The CV-1 Marshal pattern is a --- hand, --- minute racetrack pattern with the inbound leg passing over the marshall's fix (IAF)

Back 221

Left hand/ 6min

Front 222

---- Minutes in trail is the optimum interval for aircraft departing Marshal during case III

Back 222

1min or 5mi

Front 223

What degree of control is used during case I operations

Back 223

Advisory

Front 224

Marshal control will create a bolter hole for the furst aircraft by delaying the EAT of the --- aircraft by one minute

Back 224

7th

Front 225

Normally break/ramp time is pushed back because of

Back 225

Delays in launch operations

Front 226

Aircraft commence approach at ---knot traveling approximately every --- minute

Back 226

250kts/4min

Front 227

Marshal control will give aircraft the order to DELTA using a "99" broadcast and shall include a number suffix indicating the number of minutes That the recovery is expected to be delayed in even numbers never less than --- minutes

Back 227

4min

Front 228

If the final bearing is --- degrees or less from the reciprocal of the Marshal radial, aircraft shall make a gradual course correction to intercept the file bearing

Back 228

10°

Front 229

If the final bearing is more than 10ﾟ from the reciprocal of the Marshal radial, aircraft shall make a --- degree course correction to intercept the final bearing

Back 229

30°

Front 230

If an aircraft is not established on the final bearing at 12 DME, the aircraft shall fly the --- DME arc until intercepting the final bearing

Back 230

12 DME

Front 231

Speed changes are issued in --- knot increments above and below the normal approach speed of 250 knots

Back 231

25kts

Front 232

Aircraft instructed to fly speeds in excess of 250 knots should be reduced back to 250 knots prior to --- miles

Back 232

12mi

Front 233

E2 Aircraft reduce speed to --- knots (gear speed) prior to going dirty

Back 233

190kts

Front 234

A wag should not be done inside of --- nm

Back 234

6nm

Front 235

Handoffs to approach control should occur prior to --- nm from the Carrier

Back 235

20nm

Front 236

Single piloted aircraft are required to change frequencies at or before reaching ---

Back 236

5000ft (platform)

Front 237

Marshal will normally initiate the handoff when aircraft reach --- or ---nm from the Carrier

Back 237

22nm/23nm

Front 238

After hand off to final control, --- retains overall responsibility for aircraft separation

Back 238

Approach

Front 239

Aircraft are handed off to final control during a case III recovery, normally between --- and --- nm from the Carrier

Back 239

3.5/8nm

Front 240

If the aircraft has a malfunctioning transponder the pilot must be advised to

Back 240

Report when level at assigned altitude

Front 241

Jet and Turboprop aircraft commence transition to the landing configuration at the --- nm fix

Back 241

8nm

Front 242

Jet aircraft shall pass through the 6nm fix at --- knots in the landing configuration and commence slowing to final approach speed

Back 242

150kts

Front 243

Turboprop aircraft shall conform to jet aircraft approach procedures, but shall commence transition to the landing configuration no later than the --- nm fix

Back 243

6nm

Front 244

The minimum longitudinal separation between 5 and 12nm from the Carrier is ---nm when on a designated approach or established on down wind

Back 244

2nm

Front 245

The minimum longitudinal separation within 5nm from the Carrier is --- nm while established on final

Back 245

1.5

Front 246

Aircraft under non radar control must be separated by --- minutes

Back 246

2min

Front 247

The minimum tanking altitude during case III recoveries is --- feet

Back 247

2500ft

Front 248

On many carriers the minimum tanking altitude is increased to --- feet by Carrier air wing doctrines to ensure that adequate vertical separation will be maintained between the tanker and aircraft taken off the approach

Back 248

3000ft

Front 249

Missed approach procedures are conducted during --- recoveries only

Back 249

case III

Front 250

If no instructions are received prior to reaching --- nm or --- minutes ahead of ship the pilot will turn downwind

Back 250

4nm/2min

Front 251

The bolter pattern is flown at 1200' --- knots in the landing configuration

Back 251

150kts

Front 252

Down wind is flown at a distance of --- nm from the Carrier

Back 252

2nm

Front 253

Every effect is made to create bolter holes that will enable aircraft to be hooked between --- & --- nm downwind

Back 253

4nm/6nm

Front 254

The optimum range for hooking aircraft is --- nm downwind

Back 254

4nm

Front 255

Equally important, aircraft hooked at this range will be provided with a least --- seconds of level flight prior to intercepting the PALS or ICLS glideslope (at approximately 3nm)

Back 255

30sec

Front 256

An aircraft on a downwind leg wider than --- nm should not be hooked to the final bearing, as this usually results in the aircraft rolling out of the turn well left of course

Back 256

2nm

Front 257

To hook an F18 into the final bearing after an E2, the F18 should be hooked when it is at least ---nm past abeam position of the E2

Back 257

2nm

Front 258

Tanker and receiving aircraft shall have --- foot minimum separation until visual separation is established

Back 258

500ft

Front 259

During a signal divert/bingo aircraft are normally instructed to contact departure when passing --- feet during climb out

Back 259

2500ft

Front 260

Approach or final may instruct aircraft to descend to 600' after passing --- nm fix if a nonprecision radar approach will be conducted

Back 260

3nm

Front 261

Final control services are provided from handoff by the approach controller until the aircraft is handed off to the LSO at --- nm or the aircraft reaches precision or nonprecision approach weather minimums

Back 261

.75nm

Front 262

PALS referred to as --- , provides both automatic and manual control of aircraft

Back 262

Easy rider

Front 263

The ICLS referred to as the --- is an ILS type system using independent landing monitor (ILM) and TACAN/DME

Back 263

Bullseye

Front 264

The first use of the ICLS is made possible because of the greater range at which error signals can be received in excess of --- nm compared to approximately --- for PALS

Back 264

20nm/10nm

Front 265

When the ICLS is used as an independent monitor during PALS mode one approaches the ICLS and PALS displays of error signals shall agree to within --- percent of full scale deflection --- to --- needle widths, until reaching mode I approach weather minimums

Back 265

10%/2-3 needle widths

Front 266

If the displays exceed ---- % the mode I approach shall be downgraded to a mode II approach

Back 266

10%

Front 267

The primary instrument approach for helicopters is the --- offset approach

Back 267

CV-3 TACAN

Front 268

Helicopter Marshal altitudes are assigned by CATCC at --- foot intervals from a base altitude of --- feet

Back 268

500ft/1000ft

Front 269

Helicopter Marshall distance are assigned at --- nm intervals for each 500' of altitude beginning at --- from the Carrier

Back 269

1nm/5nm

Front 270

The CV-3 Marshal pattern is a --- hand racetrack pattern with --- legs and the inbound leg passing over the Marshal fix. EATs are normally assigned by CATCC at --- minute intervals

Back 270

RH/2nm/1min

Front 271

Who can adjust approach weather minimums

Back 271

The commanding officer

Front 272

After passing --- DME pilots are instructed to descend to 600' for an ASR approach

Back 272

6DME

Front 273

Helicopters are required to contact CATCC at or before reaching --- nm from the Carrier or when control is transferred by another controlling agency

Back 273

25nm

Front 274

For helicopters, the starboard Delta shall be a right hand race track pattern between 045ﾟ and 110ﾟ relative at --- feet or below, with the closest point of approach no closer then --- nm

Back 274

300ft/1nm

Front 275

The bearing of the CV-3 marshal fix (IAF) is the --- degree TACAN radial relative to the final bearing

Back 275

110°

Front 276

Helicopters shall pass the --- mile DME fix at --- feet in landing configuration, and maintain 500' until interception of the glideslpoe or until otherwise directed

Back 276

3mi/500ft

Front 277

Helicopters are normally instructed to turn downwind into the bolter pattern which is flown at --- feet --- knots on a reciprocal heading to the final bearing and in the landing configuration

Back 277

300ft/90kts

Front 278

What are the minimums for a mode I approach

Back 278

As certified

Front 279

What are the minimums for mode I approach without ILM

Back 279

200ft / 1/2nm

Front 280

What are the minimums for a mode II approach

Back 280

200ft / 1/2nm

Front 281

What are the minimums for a jet non precision approach

Back 281

600ft / 1 1/4nm

Front 282

What are the minimums for a Turboprop nonprecision approach

Back 282

400ft / 1nm

Front 283

What are the minimums for a helicopter nonprecision approach

Back 283

300ft / 3/4nm

Front 284

Departure reference radial (DRR)

Back 284

issued by departure

separated by 20ﾟ

Each squadron given different values

Front 285

Case I & II port holding pattern

Back 285

2000' base

1000' separation

Est at alt by 10nm

Front 286

Inbound heading intercept the final bearing (FB) between what miles

Back 286

10-12nm

Front 287

Standard Marshal

Back 287

180ﾟ relative to EFB

Left hand holding / 6min

Base 6000'/21nm

Front 288

Inbound heading and emergency Marshal are separated by how many degrees

Back 288

30°

Front 289

Emergency Marshal pattern

Back 289

150ﾟ relative to EFB

Right hand holding/ 6 min

Base 6000' /21nm

Front 290

Helicopter starboard holding

Back 290

300' / 80 knots

Front 291

COD starboard holding

Back 291

1000-500ft if approved by boss

No closer than 1nm

Front 292

Initial approach fix

Back 292

3 miles astern/ 800'

Front 293

Spin altitude

Break altitude

Pattern altitude

Back 293

Spin 1200'

Break 800'

Pattern 600'

Front 294

Define Inbound bearing

Final bearing

Base recovery course (BRC)

True heading

Back 294

Inbound bearing - Bearing to the boat

Final Bearing - BRC minus angel deck

BRC - True heading +/- MAGVAR

True Heading - Fox corpen used by bridge

Front 295

Case I jet/Turboprop

Back 295

After clearing turn

Straight ahead at 500'

Parallel BRC until 7nm

Then clear to climb if vmc

Front 296

Case II Turboprop

Back 296

After clearing turn

Parallel the BRC at 500'

At 6nm turn to 7nm arc

maintain vmc until departure radial maintain 500' until 12nm on radial

Front 297

Case II jet

Back 297

After clearing turn

Straight ahead at 500' parallel the BRC

At 7nm turn to 10nm Arc

Maintain VMC until departure radial.

500' lifted at 7nm if VMC

Maintain 300kts

Front 298

Case III Turboprop

Back 298

Climb straight ahead to 1000'

accelerating 250kts

At 5nm turn to 7nm arc outbound to departure radial

Maintain 1000' until 12nm

Front 299

Case III jet

Back 299

Climb straight ahead accelerating to 300kts

Crossing 5nm at or above 1500'

At 7nm turn to 10nm Arc Until departure radial

Front 300

Case II COD aircraft

Back 300

Depart straight ahead unless otherwise directed and maintain 500' until 12nm

Front 301

Case III COD aircraft

Back 301

Depart straight ahead unless otherwise directed and maintain 1000' until 12nm

Front 302

Rendezvous procedures case I

Back 302

as per air wing doctrine

Front 303

Rendezvous procedures Case II/III

Back 303

This aircraft rendezvous between 20 and 50nm From the Carrier on the left side of their departure radial at a pre- briefed altitude