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<strong>Airfield</strong> <strong>Concrete</strong> <strong>Pavement</strong><br />

Smoo<strong>th</strong>ness<br />

October 27‐28, 2010<br />

Presented by:<br />

Mr. Tony Gerardi<br />

APR Consultants, Inc.


The Primary Reason We Strive to Build<br />

and Maintain Smoo<strong>th</strong> <strong>Pavement</strong>s is to<br />

Minimize Aircraft Dynamic Response,<br />

and Maximize Aircraft Performance


Roughness Defined<br />

1. Shock Loading<br />

Short waveleng<strong>th</strong> roughness <strong>th</strong>at is too fast for <strong>th</strong>e tires and<br />

suspension system to fully react. (rattles instruments, t jars<br />

avionics)<br />

2. Single Axle Loading<br />

Short waveleng<strong>th</strong> roughness <strong>th</strong>at <strong>th</strong>e tires and suspension system<br />

are capable of reacting to. (Increases O&S costs, passenger<br />

complaints)<br />

3. Whole Aircraft Loading<br />

Longer waveleng<strong>th</strong> roughness <strong>th</strong>at excites <strong>th</strong>e whole aircraft<br />

(Aircraft fatigue damage, reduces braking ability, reduces<br />

pavement life)<br />

Note: Types (1) and (2) can be detected by a 16’ Straightedge or<br />

a Profilograph; Type (3) cannot


Why Be Concerned About Runway<br />

Roughness<br />

Aborted<br />

Takeoff<br />

Poor Braking<br />

Performance<br />

Increased Operational &<br />

Support Costs & Aircraft Fatigue Damage<br />

Reduces <strong>Pavement</strong>’s Useful Life and<br />

Could Result in Costly Unscheduled Repairs<br />

Pilot and Passenger Complaints


IPRF Research on Airport <strong>Pavement</strong> Smoo<strong>th</strong>ness:<br />

Research Goals ‐ IPRF 02‐4<br />

1. Develop a smoo<strong>th</strong>ness handbook for all<br />

stakeholders<br />

2. Overview of capabilities for off <strong>th</strong>e shelf profiler<br />

types to capture data for 16’ straightedge use<br />

3. Develop target smoo<strong>th</strong>ness criteria<br />

4. Identify construction practices <strong>th</strong>at result in<br />

smoo<strong>th</strong> pavements


New <strong>Pavement</strong> Acceptance Specifications<br />

• FAA AC‐150/5370; (P‐501) 16‐Foot Straightedge<br />

using a .25 inch maximum allowable deviation<br />

anywhere along <strong>th</strong>e straightedge.<br />

• California Profilograph; Typical specification is a PI of<br />

5‐7 inches per mile<br />

• Bo<strong>th</strong> me<strong>th</strong>ods will produce a smoo<strong>th</strong> ride if grade<br />

control is maintained.<br />

• APR’s experience shows bo<strong>th</strong> me<strong>th</strong>ods to be<br />

conservative


Evolution of Airport <strong>Pavement</strong> Smoo<strong>th</strong>ness 16‐<br />

Foot Straightedge<br />

“Max Deviation Anywhere Along <strong>th</strong>e Leng<strong>th</strong>”


Various Profiling Devices<br />

• Walking Profilers<br />

▫ Sufficient Accuracy for <strong>Airfield</strong> Evaluation<br />

▫ Relatively Inexpensive<br />

▫ Can Track All Event Waveleng<strong>th</strong>s<br />

▫ Some Units Can be Painfully Slow


Various Profiling Devices<br />

• Inertial Profilers<br />

▫ Van, Truck or ATV Mounted<br />

▫ Faster <strong>th</strong>an Walking Type<br />

▫ Sub Millimeter Accuracy<br />

▫ Texture can Adversely<br />

Affect Ride Readings<br />

– Not as Repeatable As<br />

Walking Profilers<br />

– More Expensive<br />

– Difficulty Tracking Longer<br />

Waveleng<strong>th</strong> Events<br />

– Acceleration Room


O<strong>th</strong>er Profilers<br />

Rolling Inclinometer<br />

Wet or Dry Profiler


Device Evaluation Summary<br />

• All Device Types Tested Have <strong>th</strong>e Required Accuracy<br />

to Assess Airport <strong>Pavement</strong>s Using <strong>th</strong>e P‐501<br />

Specification (16‐Foot Straightedge)<br />

• Not All of <strong>th</strong>e Devices can be used to Compare to<br />

Design Grade<br />

• Each Type Has Advantages and Limitations


Evolution of Airport <strong>Pavement</strong> tSmoo<strong>th</strong>ness Assessment<br />

California Profilograph<br />

PI of 5-7 Inches/Mile is Conservative


13<br />

Profilograph<br />

• The California Profilograph<br />

has become <strong>th</strong>e industry standard<br />

for assessing pavement smoo<strong>th</strong>ness<br />

Pros:<br />

Faster <strong>th</strong>an a Straightedge<br />

Identifies Multiple Events<br />

Good for Short Waveleng<strong>th</strong> Events<br />

Accepted by <strong>th</strong>e Industry<br />

Matches Diamond Grinding<br />

Process<br />

Cons:<br />

Misses Long Waveleng<strong>th</strong> Events<br />

No Raw Profile is Produced<br />

d<br />

No Baseline Profile for Future<br />

Comparisons


Courtesy: ACPA TB-006P “Constructing Smoo<strong>th</strong> <strong>Concrete</strong> <strong>Pavement</strong>s”


15<br />

Profile Index<br />

• A Profile Index (PI) of 5 is<br />

Conservative<br />

▫ Great if you can get it, but from<br />

a Ride Quality Perspective, it is<br />

Conservative<br />

• IPRF 02‐4 Compared PI Values to<br />

Aircraft Simulation<br />

▫ Runway wi<strong>th</strong> PI’s from 12 to 14<br />

Yielded d Acceptable Ride Quality


16<br />

Taxi: Boeing 737-800 Aircraft 172500 lbs GW<br />

extension 2 (Grade Removed)<br />

Air Temperature = 59 (°F) Field Elevation = 0(f (ft) Headwind = 0( (kts)<br />

Profile Filename = extension2.dat Sim. Start = 0 (ft) RQF = 1.8300<br />

Output Filename = SIM01.out Taxiing Speed = 50 (knots) Complete Simulation = Yes<br />

1.0<br />

0.5<br />

Pilot’s Station Acceleration<br />

0.4<br />

PSA (g's<br />

)<br />

0.0<br />

-0.5<br />

-0.4<br />

CGA (g's)<br />

-1.0<br />

1.0<br />

0.5<br />

0.0<br />

-0.5<br />

-1.0<br />

0.5<br />

Aircraft’s Center of Gravity Acceleration<br />

Runway’s Profile<br />

0.4<br />

-0.4<br />

Elevatio on (in)<br />

0.0<br />

-0.5<br />

0 250 500 750 1000 1250 1500 1750 2000<br />

Distance (feet)<br />

737-800 Conducting a 50-Knot Taxi – Runway had a PI of 12-14


17<br />

The California Profilograph Relative to<br />

a Modern Commercial Aircraft<br />

Boeing 777-200ER<br />

Gear Spacing 84 feet 11 inches<br />

Equates to 3.4 California Profilograph leng<strong>th</strong>s<br />

Or 5.3 Straightedges 16 feet long<br />

Image Courtesy Boeing Commercial Aircraft Company


18<br />

Profilograph Limitations<br />

• Longer Waveleng<strong>th</strong>s are Missed using <strong>th</strong>e Profilograph or 16’ Straightedge<br />

▫ Aircraft Response is Dependant upon Gear Spacing & Speed of Encounter<br />

• This is <strong>th</strong>e Primary Reason APR uses True Profile Measurement<br />

▫ All Waveleng<strong>th</strong>s and Amplitudes are Identified


In-Service Runway<br />

Major Commercial Airport<br />

Elevation (in)<br />

Eleva ation (in)<br />

1<br />

0<br />

-1<br />

-2<br />

2<br />

0<br />

EWR Runway 4L Sou<strong>th</strong> Extension, 12.5 Feet LOC<br />

EWR Runway 4L Sou<strong>th</strong> Extension, 12.5 Feet ROC<br />

EWR Runway 4L Sou<strong>th</strong> Extension, Centerline<br />

12 Feet Left of Center<br />

Centerline<br />

Elevation<br />

(in)<br />

2.5<br />

0.0<br />

12 Feet right of Center<br />

0 500 1000 1500 2000 2500<br />

Distance (feet)


3.0<br />

16-Foot Straightedge Simulation<br />

In-Service Runway<br />

Starting Point = 0 (ft) Threshold Value = 0.25 (in)<br />

Percent Exceeded Threshold (0.25 in) = 6.69% Overall<br />

Dev viation From<br />

Straight Ed dge (in)<br />

2.5<br />

20 2.0<br />

1.5<br />

1.0<br />

0.5<br />

0.25<br />

0.0<br />

0 500 1000 1500 2000 2500<br />

Distance (feet)


3.0<br />

100-Foot Straightedge Simulation<br />

In-Service Runway<br />

Starting Point = 0 (ft) Threshold h Value = 1 (in)<br />

Percent Exceeded Threshold (1 in) = 21.06% Overall<br />

De viation From<br />

Straight Edge (in)<br />

2.5<br />

2.0<br />

1.5<br />

1.0 1<br />

05 0.5<br />

0.0<br />

0 500 1000 1500 2000 2500<br />

Distance (feet)


Aircraft Response to This Runway…<br />

22


23<br />

Corrective Action<br />

• When Analyzed wi<strong>th</strong> a California Profilograph<br />

▫ Profile Index may suggest a slightly rough pavement<br />

▫ BUT, <strong>th</strong>e PI trace will miss <strong>th</strong>e 100‐foot long peaks<br />

▫ Grinding off scallops identified by Profilograph will not fix<br />

<strong>th</strong>e problem<br />

• Grind to Desired Grade, Mud Jack or Replace Panels


What do you <strong>th</strong>ink of when “Smoo<strong>th</strong>ness”<br />

is discussed<br />

• Most stakeholders focus on <strong>th</strong>e 16‐Foot Straightedge<br />

or <strong>th</strong>e Profilograph; The Industry Focus is on <strong>th</strong>e<br />

short waveleng<strong>th</strong>s<br />

• The specifications also require a maximum of .5 inch<br />

deviation to design grade<br />

• Bo<strong>th</strong> are important to insure good aircraft ride<br />

quality<br />

• Should incentive pay include adherence to grade<br />

control


Some Airport Owners are Questioning <strong>th</strong>e<br />

Use of PI for Incentive Pay<br />

• Are we paying extra for diamond grinding to obtain<br />

unnecessary smoo<strong>th</strong>ness levels<br />

• Should parking aprons, taxiways and runway outer<br />

lanes have <strong>th</strong>e same PI requirement<br />

• Should <strong>th</strong>e decision to diamond grind be on a case<br />

by case basis; especially for non‐keel section<br />

pavements


26<br />

Recommended Option to Assess<br />

Smoo<strong>th</strong>ness<br />

• Use True Profile Measurement to Identify ALL<br />

waveleng<strong>th</strong>s<br />

• Opens up <strong>th</strong>e Possibility to Use ANY Straightedge<br />

Leng<strong>th</strong><br />

• True Profile also Serves as <strong>th</strong>e <strong>Pavement</strong>’s Baseline<br />

Profile for <strong>Pavement</strong> Management Needs


Why a Baseline Profile<br />

• Enables <strong>th</strong>e owner to track settlement or upheaval<br />

• It’s a new tool in <strong>th</strong>e <strong>Pavement</strong> Management tool<br />

box<br />

• It is a reflection of <strong>th</strong>e pavement’s structural integrity<br />

(any change in <strong>th</strong>e base, sub‐base or surface is<br />

reflected in <strong>th</strong>e profile measurement)<br />

• It enables <strong>th</strong>e owner to see a problem coming and<br />

plan accordingly


Compare 2006 to 2010<br />

(Grade Removed)<br />

Elevation (in) Elevation (in)<br />

Elevation<br />

(in)<br />

Elevation (in) Elevation (in) Ele evation (in)<br />

0.0<br />

-2.5<br />

0.0<br />

-2.5<br />

0.0<br />

-2.5<br />

0.0<br />

-2.5<br />

0.0<br />

-2.5<br />

00 0.0<br />

-2.5<br />

ATL Runway 10, 15 Feet Left of Center ATL Runway 10, Centerline Profile ATL Runway 10, 15 Feet Right of Center<br />

Runway 10-28 at ATL, 12 Feet LOC Runway 10-28 at ATL, Centerline Runway 10-28 at ATL, 12 Feet ROC<br />

Left of Center<br />

Centerline<br />

2006<br />

Right of Center<br />

Left of Center<br />

Area of Differential Settlement<br />

Centerline<br />

2010<br />

Right of Center<br />

7500 7750 8000 8250 8500 8750<br />

Distance (feet)


Compare 2006 to 2010<br />

(Grade Removed)<br />

1<br />

0<br />

ATL Runway 10, Centerline Profile<br />

Runway 10-28 at ATL, Centerline<br />

Elevation (in)<br />

-1<br />

-2<br />

-3<br />

2006<br />

-4<br />

1<br />

0<br />

Ele evation (in)<br />

-1<br />

-2<br />

-3<br />

800 cu.yds.<br />

3”<br />

2010<br />

-4<br />

8000 8100 8200 8300 8400 8500 8600 8700 8800<br />

Distance (feet)


500-Foot Straightedge Simulation<br />

ATL 10 CL_2006.dat<br />

Starting Point = 0 (ft) Threshold Value = 1 (in)<br />

Percent Exceeded Threshold (1 in) = 26.46% Overall<br />

4.0<br />

Vertical Curves<br />

2006 Baseline Data<br />

Deviation From Straigh ht Edge (in)<br />

3.5<br />

3.0<br />

25 2.5<br />

2.0<br />

1.5<br />

1.0<br />

0.5<br />

1<br />

0 1000 2000 3000 4000 5000 6000 7000 8000<br />

0 000 000 3000 000 5000 6000 000 8000<br />

Distance (feet)


4.0<br />

500-Foot Straightedge Simulation<br />

ATL 10 CL.dat<br />

Starting Point = 0 (ft) Threshold Value = 1 (in)<br />

Percent Exceeded Threshold (1 in) = 32.12% Overall<br />

Vertical Curves<br />

2007 Data<br />

Deviation From Straigh ht Edge (in)<br />

35 3.5<br />

3.0<br />

25 2.5<br />

2.0<br />

15 1.5<br />

1.0<br />

0.5<br />

Area of Settlement<br />

1<br />

0.0<br />

0 1000 2000 3000 4000 5000 6000 7000 8000<br />

0 000 000 3000 000 5000 6000 000 8000<br />

Distance (feet)


4.0<br />

500-Foot Straightedge Simulation<br />

ATL RW 10_CL.dat<br />

Starting Point = 0 (ft) Threshold Value = 1 (in)<br />

Percent Exceeded Threshold (1 in) = 45.55% Overall<br />

Vertical Curves<br />

2010 Data<br />

Deviation From Straigh ht Edge (in)<br />

35 3.5<br />

3.0<br />

2.5<br />

2.0<br />

1.5<br />

1.0<br />

0.5<br />

Area of Settlement<br />

1<br />

0 1000 2000 3000 4000 5000 6000 7000 8000<br />

0 000 000 3000 000 5000 6000 000 8000<br />

Distance (feet)


What is <strong>th</strong>e Cause of <strong>th</strong>e Differential<br />

Settlement<br />

• Some<strong>th</strong>ing is different in <strong>th</strong>is area.<br />

• Is <strong>th</strong>is a wet area<br />

• Different type of fill material<br />

• Different compaction<br />

• What about <strong>th</strong>e Parallel Taxiway in <strong>th</strong>e same area<br />

• The rate of settlement seems to have accelerated since 2007.<br />

• What will it be next year<br />

• Does not affect aircraft response at <strong>th</strong>is point.<br />

• How much is too much


IPRF Research on Airport <strong>Pavement</strong><br />

Smoo<strong>th</strong>ness: Research Goals ‐ IPRF 02‐4<br />

1. Develop a smoo<strong>th</strong>ness handbook for all<br />

stakeholders<br />

2. Overview of capabilities for off <strong>th</strong>e shelf profiler<br />

types<br />

3. Identify construction practices <strong>th</strong>at result in<br />

smoo<strong>th</strong> pavements<br />

4. Develop target smoo<strong>th</strong>ness criteria


String Line Sag<br />

Saw cuts and<br />

string line stakes<br />

Wand pressure, cable tension,<br />

curling and warping


60 6.0<br />

5.5<br />

5.0<br />

4.5<br />

Elevation (in n)<br />

4.0<br />

35 3.5<br />

3.0<br />

2.5<br />

Potential Birdba<strong>th</strong> Area<br />

Paving Lane Seam<br />

2.0<br />

1.5<br />

10 1.0<br />

0.5<br />

0.0<br />

0 10 20 30 40 50 60 70<br />

Distance (feet)<br />

Birdba<strong>th</strong> Detection – Transverse Profile


Birdba<strong>th</strong><br />

Birdba<strong>th</strong> Detection – Flood Area


Recommended Target Smoo<strong>th</strong>ness Values<br />

for All <strong>Airfield</strong> <strong>Pavement</strong>s<br />

• Rolling Straightedge Leng<strong>th</strong><br />

• Threshold of Acceptability<br />

• <strong>Pavement</strong> Section Leng<strong>th</strong><br />

500 Feet<br />

• Allowable SSI per Section 5%<br />

• Must Repair Value for Keel Section<br />

.5‐Inch<br />

• Must Repair Value for Outer Lanes<br />

.75‐Inch<br />

25 Feet<br />

.35 Inches<br />

Target Values Require Field Testing<br />

Note 1: Repeated bumps (3 or more) in <strong>th</strong>e keel section .25 inches or greater will require repair.<br />

Note 2: Any longitudinal step bump greater <strong>th</strong>an .25‐inch in <strong>th</strong>e keel section will require repair.<br />

Note 3: Exceptions apply for intersecting runways, drains on taxiways and ramps.


(in)<br />

10 1.0<br />

0.9<br />

0.8<br />

16-Foot Straightedge g Emulation<br />

Straightedge g Smoo<strong>th</strong>ness Index (16-Foot)<br />

% Exceeded .25” Threshold Per Section<br />

Runway 24R; Station 0+00 is at Painted Threshold<br />

Starting Point = 0 (ft) Threshold Value = 0.25 (in)<br />

Percent Exceeded Threshold (0.25 in) = 0.88% Overall<br />

0.0 0.0 4.5 0.0 0.0<br />

0.0 0.0 4.5 0.0 0.0<br />

SSI is a me<strong>th</strong>od <strong>th</strong>at quantifies <strong>th</strong>e effect of multiple bumps & dips<br />

.88% Overall<br />

Deviatio on From Str raight Edge<br />

0.7<br />

0.6<br />

05 0.5<br />

0.4<br />

0.3<br />

0.2<br />

0.1<br />

Threshold of acceptability<br />

Must Repair<br />

Threshold of Acceptability<br />

025 0.25<br />

00 0.0<br />

0 50 100 150 200 250 300 350 400 450 500<br />

Distance (feet)


Ano<strong>th</strong>er Possible Smoo<strong>th</strong>ness Assessment<br />

Me<strong>th</strong>od for <strong>Airfield</strong> <strong>Pavement</strong>s<br />

(Not Part of IPRF Study)<br />

• Use Profilograph<br />

• Threshold of Acceptability<br />

• <strong>Pavement</strong> Section Leng<strong>th</strong> 500 Feet<br />

• Must Repair Value for Keel Section .5‐Inch<br />

• Must Repair Value for Outer Lanes .75‐Inch<br />

25 Feet<br />

10‐12 12 Inches (Keel Section)<br />

Target Values Require Field Testing<br />

• Include True Profile for Grade Control and to Establish a<br />

Baseline Profile<br />

• Baseline Profile Data is a Deliverable


Things to Consider<br />

1. Tie incentive pay to grade control (long waveleng<strong>th</strong><br />

roughness) in addition to P‐501 or<br />

PI values; example‐commuter jet video<br />

2. Field test “Target” smoo<strong>th</strong>ness criteria<br />

3. Validate APR’s experience <strong>th</strong>at t current specs are<br />

conservative; need additional field tests comparing<br />

aircraft ride quality to PI<br />

4. Consider a different smoo<strong>th</strong>ness criteria for outer<br />

lanes, taxiways and aprons<br />

5. Should diamond grinding decisions be made on a<br />

case by case basis


IPRF Handbook<br />

• Handbook Can Be Obtained <strong>th</strong>rough <strong>th</strong>e IPRF Office<br />

▫ 02‐04 “<strong>Airfield</strong> <strong>Concrete</strong> <strong>Pavement</strong> Smoo<strong>th</strong>ness ‐ A Reference”<br />

▫ http://www.iprf.org/products/main.html<br />

/ /

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