aircraft pavement design & evaluation chart package for “e ... fileaircraft pavement design...

Transport Canada Technical Programs

Aircraft Pavement Design & Evaluation Chart Package for

“E - K” Aircraft

To obtain Pavement Design and Evaluation Charts for aircraft not included in the packages, please contact our Technical Programs staff: a) By Mail at:

Technical Programs (AARJD) International Aviation and Technical Programs Transport Canada Enterprise Building 427 Laurier Avenue West, Suite 1110 Ottawa, Ontario Canada K1A 0N5

b) By Fax at: (613) 998-4860 c) By visiting our Transport Canada Internet web site at:

http://www.tc.gc.ca/CivilAviation/International/Technical/menu.htm

June 2004

Aircraft Pavement Design & Evaluation Chart Packages

This document contains “Pavement Design & Evaluation Charts” (DEC’s) for aircraft models beginning with the letters “E” through “K”. Both flexible and rigid pavement charts are available for most aircraft. For light weight aircraft, only a flexible pavement chart has been included because rigid pavement design requirements for the aircraft fall well below minimum design thicknesses for concrete slabs. On flexible pavement charts for light weight aircraft, only the design curve at the stated maximum operating weight is shown along with a line indicating minimum pavement thickness requirements for the aircraft. In most cases, the flexible pavement design curve will fall either fully or partially below the minimum thickness requirements line. The charts have been developed using Transport Canada and Public Works Government Services Canada (PWGSC) methods for the structural design of flexible and rigid airfield pavement systems. The appropriate technical publications should be consulted for complete details on design terminology, assumptions, theory, methods, and pavement construction material requirements. To use a “Flexible Pavement Design and Evaluation Chart”:

a) For Design - Enter the chart with an “S” value on the top horizontal axis. Proceed downwards to the “1.00 Design Line”, then horizontally across to the appropriate aircraft weight line, and downwards to read the required pavement granular design thickness “t” from the bottom horizontal axis.

b) For Evaluation - Enter the chart with the existing pavement granular thickness “t” value on the bottom horizontal axis. Proceed upwards to the appropriate aircraft weight line, and then horizontally across to intersect with a vertical line extended down from the appropriate “S” value on the top horizontal axis. Interpolate the point of intersection between the set of “Overload Ratio” curves to determine the degree of pavement structural overload. Full operations by the aircraft can normally be permitted for overload ratios <= 1.25.

To use a “Rigid Pavement Design & Evaluation Chart”:

a) For Design - Enter the chart with a “k” value on the top horizontal axis. Proceed downwards to the “1.00 Design Line (2.75 MPa)”, then horizontally across to the appropriate aircraft weight line, and downwards to read the required slab thickness ”h” from the bottom horizontal axis.

b) For Evaluation - Enter the chart with the existing slab “h” value on the bottom horizontal axis. Proceed upwards to the appropriate aircraft weight line, and then horizontally across to intersect with a vertical line extended down from the appropriate bearing modulus “k” value on the top horizontal axis. Interpolate the point of intersection between the set of “Overload Ratio” curves to determine the slab flexural stress (MPa) and the degree of pavement structural overload. Full operations by the aircraft can normally be permitted for overload ratios <= 1.25.

To obtain “Pavement Design & Evaluation Charts” for aircraft not included in the package, please contact our Technical Programs staff as shown on the cover page above.

Flexible Pavement Design & Evaluation ChartAbaque de Calcul d'une Chaussée Flexible

Embraer 170, 175

% Load on Main Gear% Poids sur Atterrisseur Principal

Tire Pressure (MPa)Pression des Pneus

47.5

1.04

Subgrade Bearing Strength - S (kN)Force Portante du Sol Support

Pavement Equivalent Granular Thickness - t (mm)Epaisseur Granulaire Equivalente d'une Chaussée

600 mm

30 50 70 90 110 130

300 500 700 900 1100 1300

2.00 1.50 1.25 1.00 Overload Ratio

200 225

275 325

368

Operating Weight (kN)

Rigid Pavement Design & Evaluation ChartAbaque de Calcul d'une Chaussée Rigide

Embraer 170, 175



47.5

1.04

Bearing Modulus - K (MPa/m)Module de Réaction du Sol Support

Concrete Slab Thickness - h (mm)Epaisseur de la Dalle de Beton

600 mm

10 30 50 70 90 110 130 150

120 140 160 180 200 220 240 260

368325275225200Operating Weight (kN)

Overload Ratio1.00

(2.75 MPa)

1.25(3.50 MPa)

1.50(4.10 MPa)

2.00(5.50 MPa)


Embraer 190, 195



47.5

1.10



600 mm

30 50 70 90 110 130 150

300 500 700 900 1100 1300 1500

2.00 1.50 1.25 1.00 Overload Ratio

250 300

350 425

481



Embraer 190, 195



47.5

1.10



600 mm

10 30 50 70 90 110 130 150

140 160 180 200 220 240 260 280


Overload Ratio1.00

(2.75 MPa)

1.25(3.50 MPa)

1.50(4.10 MPa)

2.00(5.50 MPa)


Embraer EMB-110 Bandeirante



47.5

0.62



30 40 50 60 70 80 90 100

0 50 100 150 200 250 300 350

2.00 1.50 1.25 1.00 Overload Ratio

35

45

59



Embraer EMB-110 Bandeirante



47.5

0.62



10 30 50 70 90 110 130 150

60 70 80 90 100 110 120 130


Overload Ratio1.00

(2.75 MPa)

1.25(3.50 MPa)

1.50(4.10 MPa)

2.00(5.50 MPa)


Embraer EMB-120 Brasilia



47.5

0.76



400 mm

30 40 50 60 70 80

200 300 400 500 600 700

2.00 1.50 1.25 1.00 Overload Ratio

70

90

119



Embraer EMB-120 Brasilia



47.5

0.76



400 mm

10 30 50 70 90 110 130 150

70 80 90 100 110 120 130 140


Overload Ratio1.00

(2.75 MPa)

1.25(3.50 MPa)

1.50(4.10 MPa)

2.00(5.50 MPa)


Embraer ERJ-145 Series



47.5

0.90



400 mm

30 50 70 90 110

200 400 600 800 1000

2.00 1.50 1.25 1.00 Overload Ratio

100 150

175 200

237



Embraer ERJ-145 Series



47.5

0.90



400 mm

10 30 50 70 90 110 130 150

100 120 140 160 180 200 220 240


Overload Ratio1.00

(2.75 MPa)

1.25(3.50 MPa)

1.50(4.10 MPa)

2.00(5.50 MPa)


Fokker 50



47.5

0.59



450 mm

30 40 50 60 70

200 400 600 800 1000

2.00 1.50 1.25 1.00 Overload Ratio

120

160

205



Fokker 50



47.5

0.59



450 mm

10 30 50 70 90 110 130 150

80 100 120 140 160 180 200 220


Overload Ratio1.00

(2.75 MPa)

1.25(3.50 MPa)

1.50(4.10 MPa)

2.00(5.50 MPa)


Fokker 60



47.5

0.62



450 mm

30 40 50 60 70 80

200 400 600 800 1000 1200

2.00 1.50 1.25 1.00 Overload Ratio

130

170

226



Fokker 60



47.5

0.62



450 mm

10 30 50 70 90 110 130 150

80 100 120 140 160 180 200 220


Overload Ratio1.00

(2.75 MPa)

1.25(3.50 MPa)

1.50(4.10 MPa)

2.00(5.50 MPa)


Fokker 70



47.5

0.81



584 mm

30 50 70 90 110 130

200 400 600 800 1000 1200

2.00 1.50 1.25 1.00 Overload Ratio

225 250

300 350

410



Fokker 70



47.5

0.81



584 mm

10 30 50 70 90 110 130 150

120 140 160 180 200 220 240 260


Overload Ratio1.00

(2.75 MPa)

1.25(3.50 MPa)

1.50(4.10 MPa)

2.00(5.50 MPa)


Fokker 100



47.5

0.94



587 mm

30 50 70 90 110 130 150

200 400 600 800 1000 1200 1400

2.00 1.50 1.25 1.00 Overload Ratio

225 275

325 400

452



Fokker 100



47.5

0.94



587 mm

10 30 50 70 90 110 130 150

130 150 170 190 210 230 250 270


Overload Ratio1.00

(2.75 MPa)

1.25(3.50 MPa)

1.50(4.10 MPa)

2.00(5.50 MPa)


Fokker F27 Friendship



47.5

0.57



450 mm

30 40 50 60 70

200 400 600 800 1000

2.00 1.50 1.25 1.00 Overload Ratio

120

160

205



Fokker F27 Friendship



47.5

0.57



450 mm

10 30 50 70 90 110 130 150

80 100 120 140 160 180 200 220


Overload Ratio1.00

(2.75 MPa)

1.25(3.50 MPa)

1.50(4.10 MPa)

2.00(5.50 MPa)


Fokker F28 Fellowship



47.5

0.53



550 mm

30 40 50 60 70 80 90

200 400 600 800 1000 1200 1400

2.00 1.50 1.25 1.00 Overload Ratio

175 200

250 275

325



Fokker F28 Fellowship



47.5

0.53



550 mm

10 30 50 70 90 110 130 150

90 110 130 150 170 190 210 230


Overload Ratio1.00

(2.75 MPa)

1.25(3.50 MPa)

1.50(4.10 MPa)

2.00(5.50 MPa)


Gulfstream G100



47.5

0.86



340 mm

30 40 50 60 70 80

200 300 400 500 600 700

2.00 1.50 1.25 1.00 Overload Ratio

60

80

111



Gulfstream G100



47.5

0.86



340 mm

10 30 50 70 90 110 130 150

70 80 90 100 110 120 130 140


Overload Ratio1.00

(2.75 MPa)

1.25(3.50 MPa)

1.50(4.10 MPa)

2.00(5.50 MPa)


Gulfstream G159



47.5

0.83



420 mm

30 40 50 60 70 80 90

200 300 400 500 600 700 800

2.00 1.50 1.25 1.00 Overload Ratio

100

120

156



Gulfstream G159



47.5

0.83



420 mm

10 30 50 70 90 110 130 150

80 90 100 110 120 130 140 150


Overload Ratio1.00

(2.75 MPa)

1.25(3.50 MPa)

1.50(4.10 MPa)

2.00(5.50 MPa)


Gulfstream G200



47.5

0.86



340 mm

30 40 50 60 70 80 90

200 300 400 500 600 700 800

2.00 1.50 1.25 1.00 Overload Ratio

80

120

159



Gulfstream G200



47.5

0.86



340 mm

10 30 50 70 90 110 130 150

80 100 120 140 160 180 200 220


Overload Ratio1.00

(2.75 MPa)

1.25(3.50 MPa)

1.50(4.10 MPa)

2.00(5.50 MPa)


Gulfstream II



47.5

1.04



460 mm

30 50 70 90 110

200 400 600 800 1000

2.00 1.50 1.25 1.00 Overload Ratio

150 175

225 250

294



Gulfstream II



47.5

1.04



460 mm

10 30 50 70 90 110 130 150

110 130 150 170 190 210 230 250


Overload Ratio1.00

(2.75 MPa)

1.25(3.50 MPa)

1.50(4.10 MPa)

2.00(5.50 MPa)


Gulfstream III



47.5

1.21



460 mm

30 50 70 90 110 130

200 400 600 800 1000 1200

2.00 1.50 1.25 1.00 Overload Ratio

150 200

225 275

312



Gulfstream III



47.5

1.21



460 mm

10 30 50 70 90 110 130 150

120 140 160 180 200 220 240 260


Overload Ratio1.00

(2.75 MPa)

1.25(3.50 MPa)

1.50(4.10 MPa)

2.00(5.50 MPa)


Gulfstream IV



47.5

1.21



460 mm

30 50 70 90 110 130

200 400 600 800 1000 1200

2.00 1.50 1.25 1.00 Overload Ratio

175 225 250 275

334



Gulfstream IV



47.5

1.21



460 mm

10 30 50 70 90 110 130 150

120 140 160 180 200 220 240 260


Overload Ratio1.00

(2.75 MPa)

1.25(3.50 MPa)

1.50(4.10 MPa)

2.00(5.50 MPa)


Gulfstream V



47.5

1.37



460 mm

30 50 70 90 110 130 150

200 400 600 800 1000 1200 1400

2.00 1.50 1.25 1.00 Overload Ratio

200 250

300 350

405



Gulfstream V



47.5

1.37



460 mm

10 30 50 70 90 110 130 150

140 160 180 200 220 240 260 280


Overload Ratio1.00

(2.75 MPa)

1.25(3.50 MPa)

1.50(4.10 MPa)

2.00(5.50 MPa)


Hawker 1000 (BAe 1000A)



47.5

0.83



320 mm

30 40 50 60 70 80 90

200 300 400 500 600 700 800

2.00 1.50 1.25 1.00 Overload Ratio

70

100

138



Hawker 1000 (BAe 1000A)



47.5

0.83



320 mm

10 30 50 70 90 110 130 150

80 90 100 110 120 130 140 150


Overload Ratio1.00

(2.75 MPa)

1.25(3.50 MPa)

1.50(4.10 MPa)

2.00(5.50 MPa)


Hawker 400 XP (Beech 400A)



47.5

0.86



30 50 70 90 110

0 100 200 300 400

2.00 1.50 1.25 1.00 Overload Ratio

50

60

73



Hawker 400 XP (Beech 400A)



47.5

0.86



10 30 50 70 90 110 130 150

70 80 90 100 110 120 130 140


Overload Ratio1.00

(2.75 MPa)

1.25(3.50 MPa)

1.50(4.10 MPa)

2.00(5.50 MPa)


Hawker 800, 800XP



47.5

0.83



320 mm

30 40 50 60 70 80

200 300 400 500 600 700

2.00 1.50 1.25 1.00 Overload Ratio

70

100

125



Hawker 800, 800XP



47.5

0.83



320 mm

10 30 50 70 90 110 130 150

70 80 90 100 110 120 130 140


Overload Ratio1.00

(2.75 MPa)

1.25(3.50 MPa)

1.50(4.10 MPa)

2.00(5.50 MPa)


Hercules C-130 (Military)



47.5

0.67



1524 mm

30 40 50 60 70 80 90 100

600 800 1000 1200 1400 1600 1800 2000

2.00 1.50 1.25 1.00 Overload Ratio

350 450

550 650

778



Hercules C-130 (Military)



47.5

0.67



1524 mm

10 30 50 70 90 110 130 150

140 170 200 230 260 290 320 350


Overload Ratio1.00

(2.75 MPa)

1.25(3.50 MPa)

1.50(4.10 MPa)

2.00(5.50 MPa)


Hercules L-100 (Commercial)



47.5

0.74



1524 mm

30 40 50 60 70 80 90

600 800 1000 1200 1400 1600 1800

2.00 1.50 1.25 1.00 Overload Ratio

325 425

500 600

693



Hercules L-100 (Commercial)



47.5

0.74



1524 mm

10 30 50 70 90 110 130 150

140 160 180 200 220 240 260 280


Overload Ratio1.00

(2.75 MPa)

1.25(3.50 MPa)

1.50(4.10 MPa)

2.00(5.50 MPa)


HS/BAe 125 (All Series to 600)



47.5

0.83



320 mm

30 40 50 60 70 80

200 300 400 500 600 700

2.00 1.50 1.25 1.00 Overload Ratio

60

80

112



HS/BAe 125 (All Series to 600)



47.5

0.83



320 mm

10 30 50 70 90 110 130 150

70 80 90 100 110 120 130 140


Overload Ratio1.00

(2.75 MPa)

1.25(3.50 MPa)

1.50(4.10 MPa)

2.00(5.50 MPa)


HS/BAe 700



47.5

0.88



320 mm

30 40 50 60 70 80

200 300 400 500 600 700

2.00 1.50 1.25 1.00 Overload Ratio

60

80

114



HS/BAe 700



47.5

0.88



320 mm

10 30 50 70 90 110 130 150

70 80 90 100 110 120 130 140


Overload Ratio1.00

(2.75 MPa)

1.25(3.50 MPa)

1.50(4.10 MPa)

2.00(5.50 MPa)


HS/BAe 748



47.5

0.51



480 mm

30 40 50 60 70

200 400 600 800 1000

2.00 1.50 1.25 1.00 Overload Ratio

100 125

150 200

227



HS/BAe 748



47.5

0.51



480 mm

10 30 50 70 90 110 130 150

80 100 120 140 160 180 200 220


Overload Ratio1.00

(2.75 MPa)

1.25(3.50 MPa)

1.50(4.10 MPa)

2.00(5.50 MPa)


Ilyushin IL-18



47.5

0.80



1050 mm

770 mm

30 40 50 60 70 80

300 500 700 900 1100 1300

2.00 1.50 1.25 1.00 Overload Ratio

350 400

475 550

625



Ilyushin IL-18



47.5

0.80



1050 mm

770 mm

10 30 50 70 90 110 130 150

90 110 130 150 170 190 210 230


Overload Ratio1.00

(2.75 MPa)

1.25(3.50 MPa)

1.50(4.10 MPa)

2.00(5.50 MPa)


Ilyushin IL-62, 62M



47.0

1.65



1650 mm

800 mm

30 70 110 150 190

400 800 1200 1600 2000

2.00 1.50 1.25 1.00 Overload Ratio

650 900

1150 1375

1648



Ilyushin IL-62, 62M



47.0

1.65



1650 mm

800 mm

10 30 50 70 90 110 130 150

170 200 230 260 290 320 350 380


Overload Ratio1.00

(2.75 MPa)

1.25(3.50 MPa)

1.50(4.10 MPa)

2.00(5.50 MPa)


Ilyushin IL-76T



47.0

0.64



2580 mm

2060 mm

30 50 70 90 110

200 600 1000 1400 1800

2.00 1.50 1.25 1.00 Overload Ratio

800 1025

1250 1450

1677



Ilyushin IL-76T



47.0

0.64



2580 mm

2060 mm

10 30 50 70 90 110 130 150

120 150 180 210 240 270 300 330


Overload Ratio1.00

(2.75 MPa)

1.25(3.50 MPa)

1.50(4.10 MPa)

2.00(5.50 MPa)


Ilyushin IL-76TD



47.0

0.66



2580 mm

2060 mm

30 50 70 90 110

200 600 1000 1400 1800

2.00 1.50 1.25 1.00 Overload Ratio

900 1125

1325 1550

1775



Ilyushin IL-76TD



47.0

0.66



2580 mm

2060 mm

10 30 50 70 90 110 130 150

130 160 190 220 250 280 310 340


Overload Ratio1.00

(2.75 MPa)

1.25(3.50 MPa)

1.50(4.10 MPa)

2.00(5.50 MPa)


Ilyushin IL-86



31.2

0.88



1490 mm

1250 mm

30 40 50 60 70 80 90 100 110

500 700 900 1100 1300 1500 1700 1900 2100

2.00 1.50 1.25 1.00 Overload Ratio

1075 1325

1550 1800

2054



Ilyushin IL-86



31.2

0.88



1490 mm

1250 mm

10 30 50 70 90 110 130 150

130 160 190 220 250 280 310 340

20541800155013251075


Overload Ratio1.00

(2.75 MPa)

1.25(3.50 MPa)

1.50(4.10 MPa)

2.00(5.50 MPa)


Jetstream 31, 32 (BAe)



47.5

0.39



30 40 50 60 70

0 100 200 300 400

2.00 1.50 1.25 1.00 Overload Ratio

40

55

69



Jetstream 31, 32 (BAe)



47.5

0.39



10 30 50 70 90 110 130 150

60 70 80 90 100 110 120 130


Overload Ratio1.00

(2.75 MPa)

1.25(3.50 MPa)

1.50(4.10 MPa)

2.00(5.50 MPa)


Jetstream 41 (BAe)



47.5

0.83



402 mm

30 40 50 60 70 80

200 300 400 500 600 700

2.00 1.50 1.25 1.00 Overload Ratio

60

80

107



Jetstream 41 (BAe)



47.5

0.83



402 mm

10 30 50 70 90 110 130 150

60 70 80 90 100 110 120 130


Overload Ratio1.00

(2.75 MPa)

1.25(3.50 MPa)

1.50(4.10 MPa)

2.00(5.50 MPa)


KC-10 (McDonnell Douglas)



39.0

1.22



1626 mm

1372 mm

30 50 70 90 110 130

600 1000 1400 1800 2200 2600

2.00 1.50 1.25 1.00 Overload Ratio

1800 1975

2175 2375

2593



KC-10 (McDonnell Douglas)



39.0

1.22



1626 mm

1372 mm

10 30 50 70 90 110 130 150

170 210 250 290 330 370 410 450

25932375217519751800


Overload Ratio1.00

(2.75 MPa)

1.25(3.50 MPa)

1.50(4.10 MPa)

2.00(5.50 MPa)


KC-135 Stratotanker



47.5

1.38



1540 mm

960 mm

30 50 70 90 110 130

400 800 1200 1600 2000 2400

2.00 1.50 1.25 1.00 Overload Ratio

800 925

1050 1200

1342



KC-135 Stratotanker



47.5

1.38



1540 mm

960 mm

10 30 50 70 90 110 130 150

140 170 200 230 260 290 320 350


Overload Ratio1.00

(2.75 MPa)

1.25(3.50 MPa)

1.50(4.10 MPa)

2.00(5.50 MPa)

aircraft pavement design & evaluation chart package for “e ... fileaircraft pavement design...

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