- •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 EqualTime (PET)
The Effect of Wind on the Position of the PET:
Let A to B total distance D = 500 NM and TAS = 300 kt.
STILL AIR |
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500 |
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300 |
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= HALFWAY |
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60 kt HEADWIND |
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500 |
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360 |
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=250 NM
=300 NM
= Greater than HALFWAY
60 kt TAILWIND |
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500 |
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240 |
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= 200 NM |
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240 |
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= Less than HALFWAY
•In still air the PET is HALFWAY
•If there is a wind then the PET moves INTO WIND
•The stronger the wind the greater the movement INTO WIND
•A gross error check. If you have a headwind component outbound the PET has to be more than halfway between departure and destination
13
Point of Equal Time (PET) 13
245
13 Point of EqualTime (PET)
Single Sector All-engine PET
Fill in the ground speed rectangles at Figure 13.3 and calculate the distance and time to the all-engine PET.
Wind Component A to the PET is +45 kt
Wind Component PET to B is -10 kt
The all-engine TAS |
475 kt |
Engine failure TAS |
380 kt |
The route distance |
2050 NM |
(PET) Time Equal of Point 13
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Figure 13.3 Example all-engine single leg PET |
GS H |
475 |
- 45 = 430 |
GS On |
475 |
- 10 = 465 |
GS out to PET |
475 |
+ 45 = 520 |
X = |
2050 × 430 |
= 985 NM |
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465 + 430 |
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985 NM @ GS out 520 = 113.5 min
246
Point of EqualTime (PET) 13
Engine Failure PET
Figure 13.4 Engine failure Point of Equal Time
The loss of a power unit will necessitate invariably a “drift down” to a stabilizing pressure altitude where the aircraft will either continue ON, or return HOME, at the reduced engine failure TAS/GS, depending on whether the failure occurred before or after the ETA (computed at the all-engine TAS/GS) for the engine failure PET. If the engine failure happened at the PET then, in theory, the pilot could choose to fly to either airfield as the flight times are equal.
Point of Equal Time (PET) 13
247
13 Point of EqualTime (PET)
With reference to Figure 13.5 fill in the ground speed rectangles and calculate the distance and time to the engine failure PET.
(PET) Time Equal of Point 13
Figure 13.5 Example engine failure PET single leg
GS H |
380 |
- 45 = 335 |
GS On |
380 |
- 10 = 370 |
GS out to PET |
475 + 45 = 520 |
X = |
2050 × 335 |
= 974 NM |
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370 + 335 |
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974 NM @ GS out 520 = 112.5 min
The difference in distance between an all-engine and engine failure PET can be seen to be very small, even though in these two examples there was a difference in all-engine and engine failure TAS of 95 kt. Thus an engine failure PET is normally constructed, which may then be used for serious occurrences other than power unit failure.
To calculate the distance X to an engine failure PET use the engine failure TAS to calculate O and H in the formula.
To calculate the distance X to an all-engine PET use the all-engine TAS to calculate O and H in the formula.
To calculate the time to fly to an all-engine or an engine failure PET use the all-engine TAS to calculate the ground speed from the departure point to the PET.
248
Questions - 1
1.Given:
Distance from A to B 1200 NM
GS On |
230 kt |
GS Home |
170 kt |
What is the distance and time to the PET from “A”?
a. |
600 NM |
2 h 37 min |
b. |
510 NM |
2 h 13 min |
c. |
690 NM |
3 h |
d. |
510 NM |
3 h |
2.Given:
Distance from A to B 3200 NM
GS On |
480 kt |
GS Home |
520 kt |
What is the distance and time to the PET from “A”?
a. |
1664 NM |
3 h 12 min |
b. |
1600 NM |
3 h 20 min |
c. |
1664 NM |
3 h 28 min |
d. |
1536 NM |
3 h 12 min |
3.Given:
TAS |
400 kt |
Distance from A to B 2000 NM
A 40 kt headwind is forecast from A to B
What is the distance and time to the PET from “A”?
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a. |
1100 NM |
3 h 03 min |
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b. |
1100 NM |
2 h 30 min |
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c. |
900 NM |
2 h 30 min |
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d. |
1000 NM |
2 h 47 min |
4. |
Given: |
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TAS |
165 kt |
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W/V |
090°/35 |
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A to B |
1620 NM |
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Course |
035° |
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What is the distance and time to the PET from “A”?
a. |
903 NM |
6 h 04 min |
b. |
810 NM |
5 h 42 min |
c. |
708 NM |
5 h |
d. |
912 NM |
6 h 26 min |
Questions 13
Questions 13
249
13 Questions
Questions 13
5. |
Given: |
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TAS |
500 kt |
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W/V |
330°/50 |
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A to B |
2600 NM |
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Course |
090° |
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What is the distance and time to the PET from “A”? |
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a. |
1365 NM |
2 h 36 min |
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b. |
1235 NM |
2 h 22 min |
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c. |
1235 NM |
2 h 36 min |
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d. |
2012 NM |
3 h 53 min |
Questions 6, 7 and 8 are engine failure cases
6. |
Given: |
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GS On |
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300 kt |
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GS Out |
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350 kt |
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GS Home |
250 kt |
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Distance from A to B 1200 NM |
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What is the distance and time to the PET from “A”? |
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a. |
545 NM |
1 h 34 min |
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b. |
654 NM |
1 h 52 min |
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c. |
500 NM |
1 h 40 min |
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d. |
545 NM |
1 h 49 min |
7. |
Given: |
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2 Engine TAS |
450 kt |
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1 Engine TAS |
350 kt |
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Distance from A to B |
3000 NM with a 50 kt tailwind component. |
What is the distance and time to the engine failure PET?
a. |
1285 NM |
3 h 12 min |
b. |
1333 NM |
2 h 40 min |
c. |
1714 NM |
3 h 43 min |
d. |
1285 NM |
2 h 34 min |
8.Given:
2 Engine TAS 480 kt
1 Engine TAS 400 kt
W/V |
330°/80 |
A to B |
3500 NM |
Course |
200° |
What is the distance and time to the engine failure PET from “A”?
a. |
1515 NM |
3 h 23 min |
b. |
1558 NM |
2 h 56 min |
c. |
1515 NM |
2 h 51 min |
d. |
1985 NM |
3 h 44 min |
250
Questions 13
Given the following data answer questions 9 &10
CAS |
190 kt cruising |
Pressure altitude |
9000 ft |
Temperature |
ISA -10°C |
W/V |
320/40 kt |
A to B is a distance |
350 NM |
Course |
350° |
Endurance |
3 hours |
9.What is the distance to the PET?
a.220 NM
b.311 NM
c.146 NM
d.204 NM
10.Given an actual time of departure (ATD) of 11:05, what is the ETA for the PET?
a.12:49
b.12:13
c.11:55
d.12:26
Questions 13
251
13
Answers 13
Answers
Answers - 1
1. 510 NM |
2 h 13 min |
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1200 × 170 |
= 510 NM @ 230 kt = 2 h 13 min |
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230 + 170 |
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2. |
1664 NM |
3 h 28 min |
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3200 × 520 |
= 1664 NM @ 480 kt = 3 h 28 min |
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480 + 520 |
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3. |
1100 NM |
3 h 03 min |
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X |
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2000 × 440 |
= 1100 NM @ 360 kt = 3 h 03 min |
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360 + 440 |
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4. |
912 NM |
6 h 26 min |
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Use your Navigation Computer to get ground speed on and home.
Remember to balance the drift for both outbound and the reciprocal home legs.
There are no short cuts!
X = |
1620 × 183 |
= |
912 NM @ 142 kt = 6 h 26 min |
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142 + 183 |
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5. 1235 NM 2 h 22 min
Use your Navigation Computer to get ground speed on and home.
Remember to balance the drift for both outbound and the reciprocal home legs.
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X |
= |
2600 × 472 |
= 1235 NM @ 522 kt = 2 h 22 min |
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522 + 472 |
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Engine Failure Case |
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6. 545 NM |
1 h 34 min |
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1200 × 250 |
= 545 NM @ 350 kt = 1 h 34 min |
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300 + 250 |
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7. 1285 NM |
2 h 34 min |
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X |
= |
3000 × 300 |
= 1285 NM @ 500 kt = 2 h 34 min |
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400 + 300 |
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252
Answers 13
8. What is the distance and time to the engine failure PET from “A”
1515 NM 2 h 51 min
Use your Navigation Computer to get ground speed on, 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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X = |
3500 × 342 |
= 1515 NM @ 530 kt = 2 h 51 min |
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448 + 342 |
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Information for Qs 9 & 10 |
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ISA at 9000 ft |
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-3 |
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ISA deviation |
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-10 |
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OAT |
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-13°C |
Navigation Computer for TAS 214 kt
Use your Navigation Computer to get ground speed on and home.
Remember to balance the drift for both outbound and the reciprocal home legs.
Ground speed On & Out
Ground speed Home
9. 204 NM
X = |
350 × 249 |
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178 + 249 |
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=178 kt
=249 kt
=204 NM
10.12:13
204 NM @ 178 kt = 1 h 08 min + 11:05 = 12:13
Answers 13
253
13 Questions
Questions - 2
Questions 13
1.Given: Track 355°T
W/V 340°/30 kt TAS 140 kt
Total distance A to B 350 NM
What are the time and distance to the point of equal time between A and B?
a. 75 min |
211 NM |
b. 75 min |
140 NM |
c. 50 min |
140 NM |
d. 114 min |
211 NM |
2.Given:
Course A to B 088°(T) Distance 1250 NM Mean TAS 330 kt W/V A to B 340°/60 kt
The time from A to the Point of Equal Time between A and B is:
a.1 h 54 min
b.1 h 44 min
c.1 h 39 min
d2 h 02 min
3.Distance between airports = 340 NM True track = 320°
W/V = 160°/40 TAS = 110 kt
Distance to PET is:
a.121 NM
b.219 NM
c.112 NM
d.228 NM
4.Flying from A to B, 270 NM True track 030°
W/V 120°/35
TAS 125 kt
What are the distance and time to the Point of Equal Time?
a. 141 NM |
65 min |
b. 141 NM |
68 min |
c. 135 NM |
68 min |
d. 150 NM |
65 min |
254
Questions 13
Questions 13
255
13 Answers
Answers - 2
1 |
2 |
3 |
4 |
d |
b |
c |
c |
Answers 13
256