- •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
4 Questions
Questions 4
Questions
1.Refer to CAP 697 SEP1, fig 2.1 Given: Aerodrome elevation 2500 ft,
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+10°C |
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Initial weight |
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3500 lb |
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Climb to |
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FL140 OAT -5°C |
What is the climb time, fuel, NAM? |
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22 min |
6.5 g |
46 NAM |
b. |
24 min |
7.5 g |
50 NAM |
c. |
2 min |
1.0 g |
4 NAM |
d. |
26 min |
8.5 g |
54 NAM |
2.Refer to CAP 697 SEP1, fig 2.2.3 Given FL75
OAT +10°C Lean mixture 2300 rpm
Find fuel flow (GPH) gallons per hour and TAS.
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68.5 GPH |
160 kt |
b. |
11.6 GPH |
160 kt |
c. |
71.1 GPH |
143 kt |
d. |
11.6 GPH |
143 kt |
3. |
Refer to CAP 697 SEP1 fig 2.4 |
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Given: Aeroplane mass at start up |
3663 lb |
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Fuel load (density 6 lb/gal) |
74 gal |
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Take-off altitude |
sea level |
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Headwind |
40 kt |
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Cruise altitude |
8000 ft |
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Power settings |
full throttle |
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2300 rpm |
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Calculate the range |
20°C lean of peak |
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a. |
548 NM |
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b. |
844 NM |
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c. |
730 NM |
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d. |
633 NM |
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4.Refer to CAP 697, SEP1, fig 2.5 Given FL75
Lean mixture
Full throttle / 2300 rpm
Take-off fuel |
444 lb |
Take-off from |
MSL |
Find endurance in hours
a.5 h 20 min
b.4 h 42 min
c.5 h 12 min
d.5 h 23 min
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Airfield “A” Data |
Elevation |
MSL |
Aircraft plans to cruise to “D” at 23” 2300 rpm power |
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Temp |
+20°C |
Using SEP Fig 2.1 and Fig 2.2 complete the fuel log |
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Departure Mass |
3400 lb |
Calculate the Trip Fuel, Time En route and ETA at “D” |
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Aircraft takes off from “A” at 10:00 |
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and climbs from “A” to FL80 (temperature at TOC is 0°C) |
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Wind Light & Variable |
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FROM |
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ISA |
W/V |
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TAS |
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NGM |
TK |
HDG |
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TIME |
FUEL |
FUEL |
ETA |
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FLOW |
REQD |
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A |
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TOC |
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L & V |
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18 |
120 |
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8 |
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3.4 |
10:08 |
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TOC |
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B |
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80 |
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+5°C |
230/30 |
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160 |
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82 |
120 |
130 |
168 |
29 |
11.8 |
5.8 |
10:37 |
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B |
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C |
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100 |
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0 |
270/40 |
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157 |
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150 |
160 |
174 |
166 |
54 |
11 |
9.9 |
11:31 |
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C |
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D |
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60 |
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-10°C |
200/20 |
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158 |
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80 |
130 |
137 |
150 |
32 |
12.2 |
6.5 |
12:03 |
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TOTALS |
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330 |
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123 |
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25.6 |
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Worked Answers |
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Climb from A to FL80 |
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Cruise |
TAS |
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FF |
(Table 2.2.3) |
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(Fig 2.1) |
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TOC to |
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B |
160 |
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11.8 Using the Standard Day Block |
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Time = 8 min |
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B to C |
157 |
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11 |
Using the Standard Day Block |
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Fuel = 3.4 USG |
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C to D |
158 |
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12.2 Interpolating between Standard Day and ISA -20°C |
Distance = 18 NAM & NGM as no wind
Therefore TOC to B is 100 - 18 = 82 NM
59
Answers- 1 Exercise SEP
4 Answers
Answers 4
4 Answers
Answers
1 |
2 |
3 |
4 |
a |
b |
d |
c |
Answers 4
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