- •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
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Fuel Policy and Fuel Monitoring |
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Monitoring Fuel and Policy Fuel 2
Figure 2.4 Insufficient fuel
A check of the aircraft’s fuel system may be required if it was thought that the excess consumption was caused by a fuel leak or a fuel-gauge fault. An error in computation at flight planning or in the actual fuel amount up-lifted at departure may have been the cause of the shortfall. Aircraft have run short of fuel. Very strong un-forecast headwinds have been encountered. Pounds to kilograms, kilograms to pounds, have been erroneously converted and specific gravities applied incorrectly!
Special Cases 1 – Decision Point Procedure
There is a special case when we may get airborne without sufficient contingency fuel for the planned trip to the destination. This is called decision point procedure.
Decision Point Procedure - ATypical Scenario
Consider the ‘Howgozit’ in Figure 2.6. A flight from Oxford to Faro, in southern Portugal, is planned. There are alternates near Faro - Seville or Jerez, for instance. The total of the final reserve fuel and the alternate fuel is 3000 kg. The trip fuel is exactly 10 000 kg. There is a suitable en route diversion at Lisbon, so contingency fuel is 3%, which comes to 300 kg. This means that we need 13 300 kg at take-off.
Unfortunately, the maximum capacity of our fuel tanks means that we can get in only 13 150 kg at take-off. This is 150 kg short of the minimum requirement. Does this mean that we cannot do this flight? Not necessarily, if there is a suitable en route alternate.
We define the top of descent for going into Lisbon, our alternate, as the Decision Point. We have plenty of fuel to proceed to Lisbon, so this is legal. At this Decision Point, we carry out a fuel check. Unless unforeseen circumstances have arisen, we will probably not have used the contingency fuel and so will still have 150 kg above the expected consumption line for Faro.
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The requirement for contingency fuel is 3% above the trip fuel required for the remainder of the flight, not the start trip fuel. At this stage of the trip, the required contingency fuel is only 55 kg. If the fuel remaining includes this 55 kg contingency fuel plus the remainder of the trip fuel for Faro (along with the usual alternate fuel and final reserve fuel), we continue to Faro. If the fuel remaining comes to less than this figure, we divert to our alternate, Lisbon.
Fuel Policy and Fuel Monitoring 2
Figure 2.5 Oxford to Faro
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Monitoring Fuel and Policy Fuel 2
Figure 2.6 Oxford to Faro
Decision Point Procedure should not be attempted unless the departure fuel is sufficient to guarantee a reasonable expectation of there being enough fuel remaining at the Decision Point to permit continuation to the scheduled destination. The success of a Decision Point Procedure will depend on whether unforeseen events, such as not being cleared to the optimum cruise level or avoidance of weather, have caused the contingency fuel allowance to be used. The normal non-consumption of contingency fuel, which can be a considerable amount (usually 3% at least of the fuel between departure and Decision Point), permits Decision Point Procedure to be feasible and safe.
Departure |
Decision |
Destination |
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Airport |
Point |
Airport |
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En route |
Destination |
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Alternate |
Alternate |
Figure 2.7 Decision point procedure
Comparing the Decision Point Procedure fuel requirement with the normal fuel requirements, the maximum fuel reduction available is the contingency fuel (3% or 5% of trip fuel) between Departure and Decision Point.
Alternatively, we can say that contingency fuel can be reduced down to that required between Decision Point and Destination.
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Special Cases 2 – Isolated Aerodrome Procedure
An ‘Isolated’ aerodrome is defined as an aerodrome for which there is no Destination Alternate. An island in an ocean is a good example, for instance, Easter Island in the South Pacific. In this case the aircraft might have to hold for longer than usual (e.g. in the case of a blocked runway or a tropical storm passing through) with no option of diverting. Reserves normally consist of contingency fuel, alternate fuel and final reserve fuel. In the case of an Isolated aerodrome there is no alternate, so there is no alternate fuel. Instead, for a jet or turboprop aircraft, the combination of final reserve fuel and additional fuel must comprise enough fuel to fly for two hours at normal cruise consumption after arriving at the destination aerodrome. CS-OPS 1 specifies that the fuel must include:
•Taxi fuel
•Trip fuel
•Contingency fuel
•Additional fuel if required but not less than:
•For aeroplanes with reciprocating engines, fuel to fly for 45 minutes plus 15% of the flight time planned to be spent at cruising level, or two hours, whichever is less.
•For aeroplanes with turbine engines, fuel to fly for two hours at normal cruise consumption after arriving overhead the destination aerodrome, including the final reserve fuel.
Fuel Policy and Fuel Monitoring 2
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