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WorksheetsPBN Final Exam Practice Worksheet
Total questions: 99
Worksheet time: 50mins
How many methods of navigation are there?
2: Radio navigation, Area navigation
3: Dead reckoning, Radio navigation, Area navigation
4: Pilotage (Piloting), Dead reckoning, Radio navigation, Area navigation
None of the above
In the dead reckoning method, the difference of time between estimated point and actual point above how many minutes that the estimated time has to be recalculated?
2 minutes
3 minutes
4 minutes
5 minutes
What is B-RNAV?
The airplane’s navigation equipment is capable of delivering a navigation accuracy to “stay within 1 NM, left and right of track for 95% of the flight time, over a distance of 100 NM between 2 stations.
The airplane’s navigation equipment is capable of delivering a navigation accuracy to “stay within 5 NM, left and right of track for 95% of the flight time, over a distance of 90 NM between 2 stations.
The airplane’s navigation equipment is capable of delivering a navigation accuracy to “stay within 5 NM, left and right of track for 95% of the flight time, over a distance of 100NM between 2 stations.
The airplane’s navigation equipment is capable of delivering a navigation accuracy to “stay within 5 NM, left and right of track for 95% of the flight time.
What is P-RNAV?
The airplane’s navigation equipment is capable of delivering a navigation accuracy to “stay within 1 NM, left and right of track for 95% of the flight time”.
The airplane’s navigation equipment is capable of delivering a navigation accuracy to “stay within 2 NM, left and right of track for 95% of the flight time”.
The airplane’s navigation equipment is capable of delivering a navigation accuracy to “stay within 1 NM, left and right of track for 90% of the flight time”.
The airplane’s navigation equipment is capable of delivering a navigation accuracy to “stay within 2 NM, left and right of track for 90% of the flight time”.
What is FMS stands for?
Flight monitoring system
Flight management system
Flight managing system
Flight monitor system
What are the ground sources signal of the FMS?
NDB, VOR, DME, ILS
NDB, DME, ILS
VOR, DME, ILS
NDB, DME, VOR
What are the letters that signify domestic routes?
H, M, Q, T, V, Y, X, R
H, J, Q, T, V, Y, Z, W
A, B, G, R, L, M, N, P
H, J, Q, T, V, Y, Z, X
What are the letters that signify international routes?
H, M, Q, T, V, Y, X, R
H, J, Q, T, V, Y, Z, W
A, B, G, R, L, M, N, P
H, J, Q, T, V, Y, Z, X
What are the letters that signify domestic RNAV routes?
H, J, Q, T
V, Y, Z, W
Q, T, Y, Z
J, Q, T, W
What are the letters that signify international RNAV routes?
A. A, B, G, R
B. L, M, N, P
C. B, G, R, L
D. A, B, N, O
How many letters indicate NDB?
2
3
4
5
How many letters indicate VOR?
2
3
4
5
How many letters indicate FIX?
2
3
4
5
Which time was the RNP introduced?
1970s
1960s
1990s
What are the requirements for PBN?
Accuracy, Integrity, Availability
Accuracy, Continuity, Availability
Accuracy, Integrity, Continuity, Availability
Accuracy, Integrity, Continuity
PBN is?
RNAV
RNP
Combination of RNAV and RNP
None
RNP using?
Ground navigation equipment
On board navigation equipment
Satellite navigation equipment
Sea navigation equipment
RNAV using?
Ground navigation equipment
On board navigation equipment
Satellite navigation equipment
Sea navigation equipment
RNP using which signal?
Ground signal
GNSS signal
Both
None
What is the PBN manual document?
Doc 9631
Doc 9613
Doc 4444
Doc 8400
What is the main difference between RNAV and RNP:
RNAV has no on-board performance and monitoring alerting
RNAV has on-board performance and monitoring alerting
RNP has no on-board performance and monitoring alerting
None
The accuracy requirement in RNP concept is:
Aircraft must remain within accuracy limit 95% of flight time (The maximum TSE with 95% probability 1 X RNP).
Aircraft must remain within accuracy limit 90% of flight time (The maximum TSE with 95% probability 1 X RNP).
Aircraft must remain within accuracy limit 95% of flight time (The maximum TSE with 95% probability 2 X RNP).
Aircraft must remain within accuracy limit 90% of flight time (The maximum TSE with 95% probability 2 X RNP).
The integrity requirement in RNP concept is:
Probability to transgress the containment limit set as 2 x RNP without alert must be < 10 mũ -5/flight hour
Probability to transgress the containment limit set as 1 x RNP without alert must be < /flight hour
Probability to transgress the containment limit set as 1 x RNP without alert must be < /flight hour
Probability to transgress the containment limit set as 2 x RNP without alert must be < /flight hour
The continuity requirement in RNP concept is:
Probability of RNP capability loss with alert must be < 10 mũ -2/Flight hour
Probability of RNP capability loss with alert must be <10 mũ -3 /Flight hour
Probability of RNP capability loss with alert must be < 10 mũ -4/Flight hour
Probability of RNP capability loss with alert must be < /Flight hour10 mũ -6
TSE equals?
TSE= PDE + PSE + FTE
TSE= PDE + PEE+ NSE
TSE= PDE + PSE + PEE
TSE= PDE + FTE + PSE
RNAV was introduced in?
1960s
1970s
1980s
1990s
What is position accuracy?
Difference between actual and estimated position
Difference between actual and desired position
Difference between desired and estimated position
None above
What is Track – keeping accuracy?
Difference between actual and estimated position
Difference between actual and desired position
Difference between desired and estimated position
None above
A statement of accuracy, integrity, continuity and availability needed is defined in:
Doc 9613
Doc 9650
Doc 8768
Doc 4444
Which RNP type(s) used for helicopters?
RNP 1
RNP 2
RNP 0.3
RNP APCH
Which RNAV type(s) used for en route?
RNAV 10
RNAV 5
RNAV 1
RNAV 2
Which RNAV type(s) used for terminal?
RNAV 10, RNAV 5, RNAV 2
RNAV 10, RNAV 5, RNAV 1
RNAV 5, RNAV 2, RNAV 1
RNAV 10, RNAV 2, RNAV 1
Which RNP type(s) used for en route?
RNP 4, RNP 2
RNP 1
RNP APCH, RNP AR APCH
RNP 0.3
Which RNAV type(s) used for terminal?
RNP 4, RNP 2
RNP 1
RNP APCH, RNP AR APCH
RNP 0.3
Ground-based NAVAIDs for PBN concept are:
VOR, DME, NDB
VOR, DME
GNSS
INS/IRS, FMS
Space-based NAVAIDs for PBN concept are:
VOR, DME, NDB
VOR, DME
GNSS
INS/IRS, FMS
Aircraft – based NAVAIDs for PBN concept are:
VOR, DME, NDB
VOR, DME
GNSS
INS/IRS, FMS
DME geometry solutions require 2 DMEs to be:
30 x 150
30 < X < 150
40 x 160
50 x 170
In RAIM, 4 satellites can do:
Position fix
Faulty signal detected
Faulty signal isolated
None above
In RAIM, 5 satellites can do:
Position fix
Faulty signal detected
Faulty signal isolated
None above
In RAIM, 6 satellites can do:
Position fix
Faulty signal detected
Faulty signal isolated
None above
Which NOTAM includes information about RAIM?
NOTAMN
NOTAMM
NOTAMS
NOTAMJ
How many satellite signals does RAIM receive at least?
3
4
5
6
No safety is considered when the system?
A. Cannot assume appropriate route spacing is 2xRNP
A. Cannot assume appropriate route spacing is 3xRNP
A. Cannot assume appropriate route spacing is 1xRNP
Cannot assume appropriate route spacing is 4xRNP
OBPMA provides alert if accuracy is not met, or:
TSE exceeds 2xaccuracy value >
TSE exceeds accuracy value >
TSE exceeds 2xaccuracy value >
TSE exceeds accuracy value >
RF legs usually used in:
En-route
Terminal, approach
Departure
Ground
FRT usually used in:
En-route
Terminal, approach
Departure
Ground
FRT stands for
Fixed Radius Transitions
Final Radius Transitions
Fixed Radio Transitions
Final Radio Transitions
Approach procedures based on:
RNAV specifications
RNAV and RNP specifications
RNP specifications
None above
Navigation Application is:
Navigation Specification
Navigation Infrastructure
Navigation Specification + Navigation Infrastructure
None above
Strategic goals of an Airspace concept:
Safety, Capacity, Efficiency, Environment, Access
Safety, Capability, Efficiency, Enviroment, Access
Safety, Continuity, Efficiency, Environment, Access
Safety, Availability, Efficiency, Environment, Access
How many Path/Terminator are acceptable for RNAV procedure design?
10
11
12
13
Subset used for RNP AR applications are:
IF, TF, RF, HM
IF, DF, RF, HM
IF, DF, TF, HM
IF, TF, HM, HR
HF (hold fix) leg is defined as:
A point where the aircraft is expected to hold while waiting
A point where the aircraft is expected to hold on the fix for 1 circuit and then continue
A point where the aircraft is expected to hold on the fix for 2 circuits and then continue
A point where the aircraft is expected to hold on the fix for as many circuits as it need and then continue
HA( hold to altitude) leg is defined as:
A point where the aircraft is expected to hold while waiting
A point where the aircraft is expected to hold at an altitude
A point where the aircraft is expected to hold and climb while in the holding pattern
A point where the aircraft is expected to hold at a fixed altitude
in RF leg, single RF turn limited to turns between
2 and 358
3 and 357
1 and 359
4 and 356
Over – fly is required for:
CF/DF , DF/DF, TF/DF
CF/RF, DF/DF, TF/DF
CF/FA, DF/DF, TF/CF
CF/HF, DF/DF, TF/DF
Altitude Termination is always:
AT
ABOVE
AT and ABOVE
AT or ABOVE
When speed increases, turn radius:
Increases
Decreases
Not change
Turn radius not affect by speed
When bank angle increases, turn radius:
Increases
Decreases
Not change
Turn radius not affect by bank angle
How many waypoints are common in RNAV arrival procedure?
3-6
4-6
6-10
5-10
Letter “A” in Path concept stands for:
Altitude
Constant DME arc
Constant Radius
DME distance
Letter “A” in Terminator concept stands for:
Altitude
Constant DME arc
Constant Radius
DME distance
Letter “I” in Terminator concept stands for:
Initial
Next Leg
Track between
Heading to
Letter “C” in Terminator concept stands for:
Course to
Distance
DME distance
Constant radius
Letter “T” in Path concept stands for:
Track between
Direct to
Next Leg
Heading to
RNAV 10 requires … lateral and … longitudinal distance – based separation minima:
40 NM, 40 NM
40 NM, 50 NM
50 NM, 50 NM
RNAV 10 (RNP 10) operational requirements are defined in:
ICAO doc 9613, Volume I, Part B, Chapter 1
ICAO doc 9613, Volume II, Part B, Chapter 1
ICAO doc 9613, Volume I, Part A, Chapter 1
ICAO doc 9613, Volume II, Part A, Chapter 1
RNAV 10 requires … independent long – ranged navigation systems:
1
2
3
4
The navigation systems used for RNAV 10 can be:
INS/IRU or GNSS
INS/IRS, VOR/DME, DME/DME and GNSS
GNSS or DME/DME/IRU
GNSS or DME/DME
The types of position sensors used for RNAV 5 can be:
INS/IRU or GNSS
INS/IRS, VOR/DME, DME/DME and GNSS
GNSS or DME/DME/IRU
GNSS or DME/DME
The navigation systems used for RNAV 2 at or above FL180 can be:
INS/IRU or GNSS
INS/IRS, VOR/DME, DME/DME and GNSS
GNSS or DME/DME/IRU
GNSS or DME/DME
The navigation systems used for RNAV 1 can be:
INS/IRU or GNSS
INS/IRS, VOR/DME, DME/DME and GNSS
GNSS or DME/DME/IRU
GNSS or DME/DME or DME/DME/IRU
RNAV 5 operational requirements are defined in:
ICAO doc 9613, Volume I, Part B, Chapter 1
ICAO doc 9613, Volume II, Part B, Chapter 2
ICAO doc 9613, Volume I, Part A, Chapter 1
ICAO doc 9613, Volume II, Part A, Chapter 2
RNAV 2 and RNAV 1 operational requirements are defined in:
ICAO doc 9613, Volume I, Part B, Chapter 1
ICAO doc 9613, Volume II, Part B, Chapter 3
ICAO doc 9613, Volume I, Part A, Chapter 1
ICAO doc 9613, Volume II, Part A, Chapter 2
The navigation systems used for RNAV 2 below FL180 required:
INS/IRU or GNSS
INS/IRS, VOR/DME, DME/DME and GNSS
GNSS or DME/DME/IRU
GNSS
Typical route spacing for RNAV 5 using for low ATC intervention rate:
16NM uni – directional, 18.5NM bi – directional
15NM uni – directional, 17.5NM bi – directional
14NM uni – directional, 16.5NM bi – directional
13NM uni – directional, 15.5NM bi – directional
Typical route spacing for RNAV 5 using for high ATC intervention rate:
16NM uni – directional, 18.5NM bi – directional
10NM uni – directional, 15.5NM bi – directional
10 – 15 NM
15 – 20 NM
Route spacing for RNAV2:
Above 8 NM
At least 8 NM
Above 7 NM
At least 7 NM
Route spacing for RNAV1:
At least 6 NM
At least 7 NM
At least 8 NM
To be determined
RNP 4 requires … lateral and … longitudinal distance – based separation minima:
30 NM, 30 NM
40 NM, 40 NM
50 NM, 50 NM
60 NM, 60 NM
RNP 4 is intended for use in:
Terminal airspace
Continental airspace
Continental En – route
Oceanic/remote airspace
RNP 4 operational requirements are defined in:
Doc 9613, Volume II, Part C, Chapter 1
Doc 9613, Volume II, Part C, Chapter 2
Doc 9613, Volume II, Part B, Chapter 1
Doc 9613, Volume II, Part B, Chapter 2
Types of position sensors used in RNP 4:
GNSS
GNSS or DME/DME
GNSS, INS/IRS
GNSS, INS/IRS, VOR/DME, DME/DME
Types of position sensors used in RNP 2:
GNSS
GNSS or DME/DME
GNSS, INS/IRS
GNSS, INS/IRS, VOR/DME, DME/DME
Types of position sensors used in RNP 0.3:
GNSS
GNSS or DME/DME
GNSS, INS/IRS
GNSS, INS/IRS, VOR/DME, DME/DME
RNP 2 is intended for use in:
Approach
En – route
SIDs
STARs
RNP 2 operational requirements are defined in:
Doc 9613, Volume II, Part C, Chapter 1
Doc 9613, Volume II, Part C, Chapter 2
Doc 9613, Volume II, Part B, Chapter 1
Doc 9613, Volume II, Part B, Chapter 2
RNP 1 is intended for use in:
Approach
En – route
SIDs, STARs
Ground
RNP 1 applied in SIDs and STARs within ... of the aerodrome reference point (ARP):
10 NM
20 NM
30 NM
40NM
RNP 1 operational requirements are defined in:
Doc 9613, Volume II, Part C, Chapter 1
Doc 9613, Volume II, Part C, Chapter 2
Doc 9613, Volume II, Part C, Chapter 3
Doc 9613, Volume II, Part C, Chapter 4
RNP 0.3 operational requirements are defined in:
Doc 9613, Volume II, Part C, Chapter 5
Doc 9613, Volume II, Part C, Chapter 6
Doc 9613, Volume II, Part C, Chapter 7
Doc 9613, Volume II, Part C, Chapter 8
A – RNP encompasses which phases of flight?
Departure
En – route (oceanic/remote, continental)
Arrival, approach
All
A-RNP recognition is based on navigation systems meeting the performance and functional criteria for:
RNP 2, RNP 1, RNP APCH to LNAV minima
RNP 4, RNP 2, RNP 1 to LNAV minima
RNP 4, RNP 2, RNP APCH to LNAV minima
RNP 4, RNP 1, RNP APCH to LNAV minima
A–RNP operational requirements are defined in:
Doc 9613, Volume II, Part C, Chapter 4
Doc 9613, Volume II, Part C, Chapter 5
Doc 9613, Volume II, Part C, Chapter 6
Doc 9613, Volume II, Part C, Chapter 7
Which of these followings is PBN basic functionality:
Display of Lateral Deviation
RF legs
Parallel offsets
Scaleable RNP
Which of these followings is PBN basic functionality:
Distance/Bearing to “Active” waypoint
RF legs
Fixed Radius Transitions
RNAV Holding
Which of these followings is PBN basic functionality:
Time to “Active” waypoint (or Ground speed)
RF legs
Fixed Radius Transitions
RNAV Holding
Which of these followings is PBN basic functionality:
Failure Indication
Baro – VNAV
Time of arrival control
Scaleable RNP
