FAA RUNWAY AND TAXIWAY DESIGN STANDARDS BASED ON …

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Transcript FAA RUNWAY AND TAXIWAY DESIGN STANDARDS BASED ON …

DANVILLE CITY COUNCIL WORK SESSION
AUGUST 3, 2010
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THE CHALLENGE: ACCOMPLISH NEEDED FEDERALLY-FUNDED IMPROVEMENTS TO THE AIRPORT’S PRIMARY RUNWAY WHILE MINIMIZING
OPERATIONAL IMPACTS AND PRESERVING IMPORTANT EXISTING
AIRPORT FEATURES.
• CURRENT FEDERAL AVIATION AUTHORITY (FAA) DESIGN STANDARDS
FOR AIRPORTS WITH JET OPERATIONS SIMILAR TO DANVILLE’S
AIRPORT CALL FOR SHORTER, MORE NARROW RUNWAYS AND
TAXIWAYS THAN ARE NOW IN PLACE. TO DOWNSIZE DANVILLE’S
AIRPORT WOULD SIGNIFICANTLY REDUCE ITS ECONOMIC
DEVELOPMENT POTENTIAL.
• THE FAA ‘S CAPITAL PROJECT FOCUS IS ON STANDARDIZING AIRPORT
INFRASTRUCTURE RATHER THAN MINIMIZING OPERATIONAL IMPACTS
DURING CONSTRUCTION.
THE FAA SHOULD IMPLEMENT THE
DANVILLE PROJECT IN A FASHION THAT SUSTAINS BASIC OPERATIONS.
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PROPOSED STRATEGY: WITH ASSISTANCE OF THE
CONGRESSIONAL DELEGATION AND COMMONWEALTH OF
VIRGINIA, SECURE
MODIFICATIONS TO STANDARD TO
ALLOW FOR NECESSARY IMPROVEMENTS, MINIMIZE COSTS
AND OPERATIONAL IMPACTS, AND PRESERVE CURRENT
AIRPORT FEATURES.
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 AVERETT UNIVERSITY FLIGHT INSTRUCTION
 CIVIL AIR PATROL MISSIONS
 GENERAL AVIATION FLIGHT ACTIVITY (PRIVATE, MEDICAL, ECT.)
 FRACTIONAL OWNERSHIP JET TRAFFIC
 CHARTER OPERATIONS
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 TOTAL OF 294 JET AIRCRAFT ARRIVALS COMPLETED
 TOTAL OF 588 JET AIRCRAFT OPERATIONS COMPLETED
 MIX OF AIRCRAFT REFERENCE CODES: BII, CII, DII
 PRIMARY JET CUSTOMERS – NETJETS, GOODYEAR AND GIBBS INT.
 TOTAL OF 22 ARRIVALS COMPLETED BY GULFSTREAM IV AIRCRAFT
 GULFSTREAM IV DII AIRCRAFT REFERENCE CODE (77’.8 WINGSPAN)
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
REDUCE THE LENGTH OF RUNWAY BY 607’

NARROW THE PRIMARY RUNWAY TO 100’

NARROW TAXIWAYS TO 35’ IN WIDTH

CORRECT LINE OF SIGHT OBSTRUCTION – 2600’

MODIFY DRAINAGE ALONG 5000’ OF RUNWAY

GRADE AREAS OUTSIDE RUNWAY - 5500’

REDUCE PAVEMENT STRENGTH TO 66,000 LBS
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
AVAILABLE RUNWAY PAVEMENT WILL BE LESS THAN 3000 FEET

JET AIRCRAFT OPERATIONS WILL BE RESTRICTED

NO INSTRUMENT APPROACHES WILL BE AVAILABLE

FUEL SALES WILL BE REDUCED BY MORE THAN FIFTY PERCENT

FLIGHT INSTRUCTION AND CAP ACTIVITIES WILL BE CONSTRAINED

ANTICIPATED LOSS OF MULTI-ENGINE AIRCRAFT BASED AT AIRPORT
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Option
Work
Areas
Sequence
Focus
Use of
Both
Runways
Available
Runway
Length
LPA Group
Five
By Sections
to Improve
Flexibility
and Access
Yes
3000 Feet
FAA
Four
By Activity
to Reduce
Cost
No
< 3000 Feet
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
PAVED AIRCRAFT OVERRUN AREA WILL BE REDUCED IN LENGTH

JET AIRCRAFT OPERATIONS WILL BE RESTRICTED BASED ON LOAD

FUEL SALES WILL BE REDUCED

THIRTY-FIVE FT WIDE TAXIWAYS WILL RESTRICT LARGE JET AIRCRAFT ACCESS

AIRPORT DEVELOPMENT OPPORTUNITIES WILL BE CONSTRAINED
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OUR RECOMMENDATIONS TO
IMPROVE SAFETY AND ACCESS
A – Maintain runway length, width and paved
aircraft overrun area
B - Correct line of sight obstruction
C - Correct drainage adjacent along 5000’
pavement section
D - Maintain existing drainage system for new
pavement section that presently meets
FAA design standards
E - Maintain width of all taxiways
F - Program funds to accelerate project
* Sequence construction work to maintain
3000 feet of available pavement
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Description
Examples/Total
Alternate A
5893 Foot Option
Alternate B
6500 Foot Option
Airfield Electrical
$307,000
$360,000
Excavation
$693,500
$730,000
Pavement
$3,092,050
$3,623,625
Total Cost Estimate
$9,124,045
$9,832,681
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AIRCRAFT CATEGORY
A
B
C
D
E
AIRCRAFT CATEGORY
I
II
III
IV
V
VI
APPROACH SPEED (knots)
<91
91-121
121-141
141-161
>166
WINGSPAN (feet)
<49
49-78
79-117
118-170
171-213
214-262
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Examples of FAA Airplane Design Group Requirements
Airplane
Group
Runway
Width
Taxiway
Width
Aircraft
Model
Maximum
Take Off
Weight (lb)
CII
100’
35’
Challenger 600
41,250
CIII
100’
50’
Boeing 737-500
133,500
CIV
DII
150’
100’
75’
35’
Boeing 707
Gulfstream IV
333,600
71,780
DIII
100’
50’
MDC-MD-83/88
160,000
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Aircraft
Type
Max
Take/
Off
Weight
6500
Ft
59° F
Dry
6500
Ft
90° F
Dry
5900
Ft
59° F
Dry
5900
Ft
90° F
Dry
%
Loss
59° F
Dry
%
Loss
90° F
Dry
Citation X
35700
35700
35358
35700
33855
0.0
(4.2)
Hawker
800 XP
Falcon
2000
G-200
G-IV SP
G-V
28000
28000
28000
28000
27161
0.0
(3.0)
36500
36500
35786
35488
34164
(2.8)
(4.4)
35450
74600
90500
35450
74600
88822
32907
74110
86743
34454
73770
88822
31606
70550
83882
(3.4)
(1.1)
(3.2)
(3.7)
(4.8)
(3.2)
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Aircraft
Type
Distance
(Max.
Landing
Weight)
Charter
Operator
59° F Dry
Charter
Operator
59° F Wet
Charter
Operator
77° F Dry
Charter
Operator
77° F Wet
Citation
Excel
Citation VI
Citation X
Hawker
400 XP
Falcon 2000
3388
5648
6495
5801
6671
3059
3502
3590
5098
5837
5984
5863
6713
6882
5246
6043
6132
6033
6949
7052
3161
5268
6058
5268
6058
G – 200
GIV – SP
3261
3209
5435
5348
6250
6151
5585
5348
6422
6151
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Decrease of
Usable Fuel
(lbs)
5900 Ft
Runway
59° F - Dry
Decrease of
Usable Fuel
(lbs)
5900 Ft
Runway
90° F - Dry
Citation X
0
(1503)
.8
Hawker 800 XP
0
(839)
.6
Falcon 2000
(1012)
(1622)
.6
1.0
G – 200
(1196)
(1301)
.6
0.6
G IV – SP
(830)
(3560)
.2
1.1
G-V
(2938)
(2861)
.9
0.9
Aircraft
Type
Decrease
In Range
(Hours)
59° F - Dry
Decrease
In Range
(Hours)
90° F - Dry
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