- •Textbook Series
- •Contents
- •1 Air Information Publications
- •Introduction
- •Format of an AIP
- •Automatic Terminal Information Service (ATIS)
- •Aerodrome Communication Facilities
- •Aerodrome Radio Navigation and Landing Aids
- •Other Sources
- •Search and Rescue
- •Questions
- •Answers
- •2 Fuel Policy and Fuel Monitoring
- •Universal Application of Fuel Policy
- •Realistic Trip Fuel
- •Reserve Fuel
- •Calculation of Contingency Fuel
- •Fuel Monitoring
- •Special Cases 1 – Decision Point Procedure
- •Special Cases 2 – Isolated Aerodrome Procedure
- •Questions
- •Answers
- •3 Nautical Air Miles
- •Nautical Air Miles
- •Questions
- •Answers
- •4 Single-engine Piston Aeroplane (SEP)
- •Introduction
- •Single-engine Piston Aeroplane
- •Cruise Power Settings Tables
- •Range Profile Figure
- •Endurance
- •Questions
- •Answers
- •5 Multi-engine Piston Aeroplane (MEP)
- •Introduction
- •MEP 1-Fuel, Time and Distance to Climb Data
- •MEP 1-Range at Standard Temperatures
- •MEP 1-Cruise Power Setting and Fuel Flow
- •MEP 1-True Airspeed
- •MEP 1-Endurance
- •MEP 1-Descent Fuel, Time and Distance
- •Questions
- •Answers
- •Introduction
- •Aeroplane Data and Constants
- •Optimum Cruise Altitude
- •Short Distance Cruise Altitude
- •Answers to Simplified Flight Planning
- •Questions
- •Answers
- •En Route Climb
- •Cruise/Integrated Range Tables
- •Questions
- •Answers
- •Descent Table
- •Exercise 1
- •Exercise 2
- •Answers to Integrated Flight Planning
- •8 MRJT Additional Procedures
- •ETOPS – CAP 697 MRJT1
- •Non-normal Operations
- •Fuel Tankering
- •Answers
- •9 Topographical Chart
- •Introduction
- •World Geodetic System of 1984 (WGS84)
- •Aeronautical Information
- •Topographical Information
- •Miscellaneous
- •Establishment of Minimum Flight Altitudes
- •The Minimum Grid Area Altitudes (Grid MORA)
- •Choosing Cruising Levels
- •Altimeter Errors and Corrections
- •Exercise 1
- •VFR Exercise 2
- •Answers
- •Exercise 1 Answers
- •VFR Exercise 2 Answers
- •10 Airways
- •Introduction
- •Air Traffic Services (ATS) Routes/Standard Routes
- •Area, Low and High Level Charts
- •Exercise 1
- •Exercise 2
- •Answers to Examples/Exercises
- •Answers Exercise 1
- •Answer Airways Exercise 2
- •Projection
- •Track Direction/Magnetic Variation/Distance
- •Grid Navigation
- •Exercise 1
- •Answers to Exercise 1
- •Exercise 2
- •Answers
- •AT(H/L) 1 & 2 Information
- •Exercise 3
- •12 ATC Flight Plan
- •Introduction
- •Definitions
- •Annexes to This Chapter
- •Specimen CA48
- •Item 19: Supplementary Information
- •Item 15
- •Use of DCT (Direct)
- •Exercise 1
- •Exercise 2
- •Exercise 3
- •Exercise 4
- •Answers
- •Annex 2
- •13 Point of Equal Time (PET)
- •Introduction
- •Derivation of Formula
- •The Effect of Wind on the Position of the PET:
- •Single Sector All-engine PET
- •Engine Failure PET
- •14 Point of Safe Return (PSR)
- •Introduction
- •Derivation of the Formula
- •Transposing the Formula to the Navigation Computer
- •The Effect of Wind on the Location of the PSR
- •Single Leg PSR
- •Derivation of the Formula for Variable Fuel Flows
- •15 Revision Questions
- •Revision Questions
- •Answers to Revision Questions
- •Specimen Examination Paper
- •Answers to Specimen Examination Paper
- •Explanations to Specimen Examination Paper
- •16 Index
Point of Safe Return (PSR) 14
Transposing the Formula to the Navigation Computer
Figure 14.3 Transposing formula to the navigation computer
The Effect of Wind on the Location of the PSR
Let E = 10 h; TAS = 300 kt. |
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STILL AIR |
T |
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× |
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min |
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+ |
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D |
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min @ kt |
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NM |
(Answer 1500 NM) |
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50 kt HEADWIND OUT |
T |
= |
× |
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min |
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+ |
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D |
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min @ kt |
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NM |
(Answer 1458 NM) |
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50 kt TAILWIND OUT |
T |
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× |
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min |
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+ |
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D |
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min @ kt |
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NM |
(Answer 1458 NM) |
Point of Safe Return (PSR) 14
•In still air the distance to the PSR is the greatest.
•Any wind component reduces the distance to the PSR.
•This distance is the same for a HEAD or TAIL wind of the same value.
•The greater the wind component the greater the reduction in the distance to the PSR.
261
14 Point of Safe Return (PSR)
Single Leg PSR
(PSR) Return Safe of Point 14
Figure 14.4 Example PSR
Study the Figure 14.4 and, using the formula, calculate the time and distance to the PSR. The aircraft is flying towards its destination at a TAS of 220 kt with a wind component of +45 kt. Its Total Endurance is 7 h 40 min and the Safe Endurance is 6 h; use TAS 220 kt throughout.
Workings
6 × 175 |
= 2 h 23 mins @ 265 kt = 632 NM |
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265 + 175 |
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(Answer: 2 h 23 min, 632 NM) |
262
Questions - Single Leg PSR
1. |
Given: |
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Total endurance |
7 h 40 min |
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Safe endurance |
6 h |
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GS Out |
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230 kt |
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GS Home |
170 kt |
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What is the time and distance to the PSR from “A”? |
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a. |
2 h 33 min |
587 NM |
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b. |
3 h 15 min |
750 NM |
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c. |
3 h 27 min |
794 NM |
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d. |
2 h 33 min |
434 NM |
2. |
Given: |
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Total endurance |
5 h |
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Reserves required |
1 h |
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GS On |
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250 kt |
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GS Out |
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280 kt |
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GS Home |
320 kt |
What is the time and distance to the PSR from “A”?
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a. |
2 h 40 min |
747 NM |
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b. |
2 h 15 min |
629 NM |
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c. |
2 h 08 min |
597 NM |
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d. |
1 h 52 min |
523 NM |
3. |
Given: |
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Total endurance |
300 min |
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Required reserves |
45 min |
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TAS |
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140 kt |
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Course |
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050° |
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W/V |
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270°/30 |
What is the time and distance to the PSR from “A”?
a. |
148 min |
401 NM |
b. |
125 min |
338 NM |
c. |
90 min |
242 NM |
d. |
106 min |
287 NM |
Questions 14
Questions 14
263
14 Questions
Questions 14
4. |
Given: |
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TAS |
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160 kt |
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W/V |
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100°/30 |
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A to B |
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1620 NM |
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Course |
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030° |
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Depart A at |
09:30 UTC |
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Total endurance |
4 h |
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Safe endurance |
3 h 20 min |
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What are the distance, time and ETA to the PSR from “A”? |
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a. |
94 min |
231 NM |
11:04 |
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b. |
106 min |
261 NM |
11:16 |
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c. |
128 min |
315 NM |
11:38 |
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d. |
106 min |
296 NM |
11:16 |
5. |
Given: |
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TAS |
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500 kt |
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W/V |
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330°/50 |
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A to B |
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4600 NM |
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Course |
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090° |
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Total endurance |
12 h |
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Safe endurance |
10 h |
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What is the time and distance to the PSR from “A”?
a. |
4 h 45 min |
2480 NM |
b. |
2 h 22 min |
1235 NM |
c. |
5 h 42 min |
2974 NM |
d. |
4 h 45 min |
2242 NM |
264
Answers 14
Answers - Single Leg PSR
1. |
2 h 33 min |
587 NM |
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T = |
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6 × 170 |
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= 2 h 33 min @ 230 kt = 587 NM |
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230 + 170 |
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2 |
2 h 08 min |
597 NM |
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T = |
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4 × 320 |
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= 2 h 08 min @ 280 kt = 597 NM |
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280 + 320 |
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3. |
106 min |
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287 NM |
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Use your Navigation Computer to get ground speed out and home.
Remember to balance the drift for both outbound and the reciprocal home legs.
There are no short cuts!
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T = |
255 × 116 |
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= 106 mins @ 162 kt = 287 NM |
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162 + 116 |
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4. |
106 min |
261 NM |
11:16 |
Use your Navigation Computer to get ground speed out and home.
Remember to balance the drift for both outbound and the reciprocal home legs.
Answers 14
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T = |
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200 × 168 |
= 106 min @ 148 kt = 261 NM |
ETA 11:16 |
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148 + 168 |
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5. |
4 h 45 min |
2480 NM |
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Use your Navigation Computer to get ground speed out and home.
Remember to balance the drift for both outbound and the reciprocal home legs.
T = |
10 × 472 |
= 4 hr 45 min @ 522 kt = 2480 NM |
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522 + 472 |
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265