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Property of Lear Siegler

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Property of Lear Siegler. NAVIGATIONAL COMPUTER SLIDE RULE. Terminal Learning Objective At the end of this lesson the student will: Action: Identify the components of the navigation computer slide rule problems Condition: Given a computer and situational data - PowerPoint PPT Presentation

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Page 1: Property of Lear Siegler

Property of Lear Siegler

Page 2: Property of Lear Siegler

NAVIGATIONAL COMPUTERSLIDE RULE

Page 3: Property of Lear Siegler

Terminal Learning Objective

At the end of this lesson the student will:

Action: Identify the components of the navigation computer slide rule problems

Condition: Given a computer and situational data

Standard: In Accordance With (IAW) Field Manual (FM) 3-04.240

Page 4: Property of Lear Siegler

Enabling Learning Objective (ELO) #1

Action: Identify the scales, values, and spacing of the navigation computer slide rule

Condition: Given a navigation computer

Standard: IAW FM 1-240

Page 5: Property of Lear Siegler

SLIDE RULE SCALES

Outer Scale: Stationary - Miles, Distance, or Quantity

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SLIDE RULE SCALES

Inner Scale: Rotating - Time or Rate

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SLIDE RULE VALUES

Values: Represent multiples of 10 on either

scale, e.g. 70 can represent .07, .7, 7.0, 70,

700, 7000, etc., dependentupon decimal placement.

Page 8: Property of Lear Siegler

SLIDE RULE VALUES

Time scale values: 70 minutes on the

outer ring of the rotating scale can be convertedto 1:10 (one hour, ten minutes) on the hours

scale on the inner ring of the rotating scale

70 minutes

1 hr, 10 min

Page 9: Property of Lear Siegler

SLIDE RULE SPACING

Spacing: spaces between numbers are not constant on

either scale.

From 60 to 15 (clockwise), unit values are 1.

From 15 to 30 (clockwise), unit values are 2.

From 30 to 60 (clockwise), unit values are 1/2.

Page 10: Property of Lear Siegler

DECIMAL PLACEMENT

The units between 21 and 22 are represented by 5 spaces. The second unit past 21 can be read as 21.4 or 2140.

Read this as? 74, 7.4, 740

Read this as? 37.5, 375, 3750

21.4 or 2140.

Page 11: Property of Lear Siegler

Questions?

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Enabling Learning Objective (ELO) #2

Action: Identify components of the slide rule computer

Condition: Given a navigation computer

Standard: IAW FM 1-240

Page 13: Property of Lear Siegler

DISTANCE CONVERSIONINDICES

NAUT index - located at scale value 66, used for converting to

nautical miles.

STAT index - located at scale value 76, used for converting to

statute miles.

KM index - located at scale value 122, used for converting

to kilometers.

Page 14: Property of Lear Siegler

INNER SCALE INDICES

SPEED index - located at 60 on the inner scale and

represented by a large black arrow. It is the hour index.

36 index - located at 36 on the inner scale and represented by a small arrow. It is the second

index (divides one hour into3,600 seconds).

Page 15: Property of Lear Siegler

INNER SCALE WINDOWS

ALTITUDE COMPUTATIONS WINDOW

Located immediately to the right of the hour index.

True altitude computations.

Temperature scale - • Located inside of window.• Temperature range from - 80° C to + 50°C.

Page 16: Property of Lear Siegler

INNER SCALE WINDOWS

ALTITUDE COMPUTATIONS WINDOW

True altitude computations.

Altitude scale - • Located under temperature window.• Altitude range from

-2000 ft to 34,000 ft in increments of 2000 ft, 35,000 ft to 80,000 ft use the same mark.

Page 17: Property of Lear Siegler

INNER SCALE WINDOWS

AIRSPEED COMPUTATIONS WINDOW

Located across fromthe hour index.

Used for True airspeed anddensity altitude computations.

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INNER SCALE WINDOWS

AIRSPEED COMPUTATIONS WINDOW

True airspeed computations.

Temperature scale - • Located above window.• Temperature range from + 50°C to - 80°C.• Negative temps are right, positive temps are left.

Page 19: Property of Lear Siegler

INNER SCALE WINDOWS

AIRSPEED COMPUTATIONS WINDOW

True airspeed computations.

Altitude scale - • Located in window.• Altitude range from

-2000 ft to 80,000 ft in increments of 1000 ft.

Page 20: Property of Lear Siegler

INNER SCALE WINDOWS

DENSITY ALTITUDE WINDOW

Located above airspeed window and used to determinedensity altitude.

• Uses airspeed window to set up temperature and altitude.• Altitude range from - 10,000 ft to 80,000 ft, increments of 1,000 ft.

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Questions?

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Enabling Learning Objective (ELO) #3

Action: Compute simple proportion problems

Condition: Given a navigation computer and data

Standard: IAW FM 1-240

Page 23: Property of Lear Siegler

PROPORTIONS

A simple proportion is afractional relationship between

numbers and is expressed as a ratio.

Example:• 20:40 represents a fraction of one-half

(reduced to it’s lowest common denominator),or expressed as a ratio, 1:2 (one to two).

• 12:16, 12 on the outer scale over 16on the inner scale is a 3/4 or three to fourrelationship.

Page 24: Property of Lear Siegler

Proportions In Problem Solving

Problem:• How many pounds are in 120 gallons of JP- 8?

Solution:• At least three factors must be known to solve

for the unknown (X).• There are 6.7 pounds in each gallon of JP-8.• The three known are:

1. 6.7 lbs.2. 1 gallon3. 120 gallons

• The ratio is: 6.7 : X 1 120

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Proportions In Problem Solving

Problem:• How many lbs are

in 120 gallons of JP- 8?

1. Set 6.7 on the outer scale over 1.0 on the inner scale.

2. Find 120 on the inner scale and read 805 lbs above 120 gallons.

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Questions?

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Enabling Learning Objective (ELO) #4

Action: Convert distance measurements

Condition: Given a navigation computer and data

Standard: IAW FM 1-240

Page 28: Property of Lear Siegler

Distance Measuring Units

Problem:• How many statute miles equals 90 nautical

miles? How many kilometers equals 90 nautical miles?

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Problem:• X SM = 90 NM?

X KM = 90 NM?

1. Set 90 NM under the NAUT index.

2. Read 104 SM under the STAT index.

Distance Measuring Units

2. Read 166 KM under the KM index.

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Questions?

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Enabling Learning Objective (ELO) #5

Action: Determine ground speed

Condition: Given a navigation computer and situational data

Standard: IAW FM 1-240

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Ground speed equals distancedivided by time.

Problem:• What is the ground speed if it takes

35 minutes to fly 80 nautical miles?

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Problem:• 35 Min to fly 80

NM. GS = X.

Ground Speed Problems

1. Set 35 (inner scale) under 80 (outer scale).2. Read 137 kts (knots) over the speed index, (60 minutes).

Page 34: Property of Lear Siegler

Ground speed equals distancedivided by time.

Problem:• What is the ground speed if it takes

if it takes 9 minutes to fly 28 kilometers?

NOTE!Ground speed is measured in knots (nauticalmiles per hour). You must convert distance to nautical miles in order to solve for knots!

Page 35: Property of Lear Siegler

Problem:• 9 min to fly 28

KM. GS = X.

Ground Speed Problems

1. Set 28 under the KM index.

2. Read 15.2 NM under the NAUT index.First, convert KM to NM.

Page 36: Property of Lear Siegler

Problem:• 9 min to fly 28

KM. (15.2 NM). GS = X.

Ground Speed Problems

3. Set 15.2 (outer scale) over 9 (inner scale.

4. Read GS, 101 kts, over the 60 index.

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Questions?

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Enabling Learning Objective (ELO) #6

Action: Determine time required

Condition: Given a navigation computer and situational data

Standard: IAW FM 1-240

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Time equals distance dividedby ground speed.

Problem:• How much time is required to fly 333

nautical miles at a ground speed of 174 knots?

Page 40: Property of Lear Siegler

Problem:• Dis. = 333 NM,

GS = 174. Time = X.

Time Required Problems

1. Set 60 index under 174.

2. Read 115 minutes, under 333.

NOTE!115 min can be read as

1hr, 55 min, on inner scale of rotating scale.

Page 41: Property of Lear Siegler

Questions?

Page 42: Property of Lear Siegler

Enabling Learning Objective (ELO) #7

Action: Convert time-distance problems

Condition: Given a navigation computer and situational data

Standard: IAW FM 1-240

Page 43: Property of Lear Siegler

Convert Time-Distance Problems

Problem:• If 50 minutes are required to travel 120

nautical miles, how many minutes are requiredto travel 86 nautical miles at the same rate?

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Problem:• 50 min. = 120NM

X min = 86NM.

Time-Distance Problems

1. Set 50 min under 120 NM.

2. Read 36 min under 86 NM.

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Convert Time-Distance Problems

Problem:• Your ground speed is 130 knots, you have

flown for 1 hour and 20 minutes. How many nautical miles have you traveled?

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Problem:• GS = 130 knots,

1 hr, 20 min, distance = X

Time-Distance Problems

1. Set speed index under 130.

2. Read the distance, 174 NM, over the 1hr, 20 min mark.

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Questions?

Page 48: Property of Lear Siegler

Enabling Learning Objective (ELO) #8

Action: Solve rate-time-distance problems using the 36 index

Condition: Given a navigation computer and situational data

Standard: IAW FM 1-240

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Solving problems using the 36 index.

NOTE!Use the 36 index whenever the distance is

less than 1/10th of the ground speed.

Used whenever time must be calculated in seconds and minutes instead of minutes and hours.

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Solving problems using the 36 index.

Problem involving less than 60 seconds:• What is the time required if the ground

speed is 100 knots and the distance is 0.5 NM?

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Problem:• GS = 100 knots,

distance = 0.5NM time required = X.

Solving problems using the 36 Index

1. Set 36 index (3,600 sec) under 100 NM.

2. Read the time, 18 seconds, under the 0.5 NM mark.

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Solving problems using the 36 index.

Problem involving more than 60 seconds:• What is the time required if the ground speed

is 95 knots and the distance is 5 nautical miles?

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Problem:• GS = 95 knots,

distance = 5NM time required = X.

Solving problems using the 36 Index

1. Set 36 index (3,600 sec) under 95 NM.

2. Read the time, 190 seconds,(3 min, 10 sec), under the 5 NM mark.

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Questions?

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Enabling Learning Objective (ELO) #9

Action: Determine rate of fuel consumption

Condition: Given a navigation computer and situational data

Standard: IAW FM 1-240

Page 56: Property of Lear Siegler

Fuel Consumption

Rate of fuel consumption equals gallons offuel consumed divided by time.

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Fuel Consumption

Problem:• What is the rate of fuel

consumption if 30 gallons of fuelare consumed in 111 minutes(1 hour, 51 minutes)?

Page 58: Property of Lear Siegler

Problem:• 30 gallons,

111 minutes (1+51), GPH = X.

Fuel Consumption

1. Set 111 minutes under 30 gallons.

2. Read the rate, 16.2 gallons over the speed (60) index.

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Fuel Consumption

Problem:• What is the rate of fuel

consumption if 300 lbs of fuelare consumed in 111 minutes(1 hour, 51 minutes)?

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Problem:• 300 lbs,

111 minutes (1+51), PPH = X.

Fuel Consumption

1. Set 111 minutes under 300 pounds.

2. Read the rate, 162 pounds over the speed (60) index.

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Questions?

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Enabling Learning Objective (ELO) #10

Action: Compute true airspeed

Condition: Given a navigation computer and situational data

Standard: IAW FM 1-240

Page 63: Property of Lear Siegler

Compute True Airspeed

True airspeed is calibrated airspeedcorrected for pressure and temperature.

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Compute True Airspeed

Problem:• What is the TAS if the FAT

is - 15° C, the pressure altitude is8,000 ft, and the CAS is 125 knots?

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Compute True Airspeed

NOTE!Use window marked

“FOR AIRSPEED AND DENSITY ALTITUDE COMPUTATION”

Page 66: Property of Lear Siegler

Problem:• FAT = - 15° C,

PA = 8,000ft, CAS = 125 kts, TAS = X.

Compute True Airspeed

1. Set 8,000 ft under - 15° in the airspeed computation window.

2. Over 125, inner scale, read TAS 137 kts.

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Questions?

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Enabling Learning Objective (ELO) #11

Action: Compute density altitude

Condition: Given a navigation computer and situational data

Standard: IAW FM 1-240

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Solving for Density Altitude

Density altitude is pressure altitudecorrected for temperature.

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Compute Density Altitude

NOTE!Use the same window as for true altitude computations -

“FOR AIRSPEED AND DENSITY ALTITUDE COMPUTATION”

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Compute Density Altitude

Problem:• What is the density

altitude if the FAT is - 15°C andthe pressure altitude is 8,000 ft?

Page 72: Property of Lear Siegler

Problem:• FAT = - 15° C,

PA = 8,000ft, DA = X.

Compute Density Altitude

1. Set 8,000 ft under - 15° in the airspeed computation window.

2. Over DA index, read DA 6,200 ft.

NOTE!

Accurate results can only be obtained by using pressure altitude. Pressure altitude can be obtained by setting the altimeter to 29.92” of mercury and reading the pressure altitude

directly from the altimeter.

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Questions?

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Enabling Learning Objective (ELO) #12

Action: Compute true altitude

Condition: Given a navigation computer and situational data

Standard: IAW FM 1-240

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Solving for True Altitude

True altitude is the altitude above MSL.True Altitude is determined bycorrecting indicated altitude

for temperature and pressure.

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Compute True Altitude

NOTE!Use the window labeled

“FOR ALTITUDE COMPUTATIONS”

Page 77: Property of Lear Siegler

Compute True Altitude

Problem:• What is the true altitude

(TALT) if the FAT is - 15°C, thepressure altitude is 2,000 ft and theindicated altitude (IALT) is 2,100 ft?

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Compute True Altitude

1. Set 2,000 ft under - 15° in the altitude computation window.

2. Above 2,100 ft (IALT), read 1910 ft (TALT).

Problem:• FAT = - 15° C,

PA = 2,000 ft, IALT = 2,100 ft.

Problem:• FAT = - 15° C,

PA = 2,000 ft, IALT = 2,100 ft.

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Questions?

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Questions?

For reference while working problems:

FM 3-04.240 Chapter 5, Paragraph 5-1 through 5-17

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Property of Lear Siegler