Attachment_5_-_PIE_Passenger_Terminal_Expansion_Site_Plan_Concept.pdf
PDF 10 MB Posted
- Attached to
- Passenger Terminal Improvements
- Solicitation number
- 23-0146-RFP - CCNA - Non-Continuing
- Issued by
- Pinellas County, Clewiston City, Florida
View the file
Other files
On GovTribe
Work with this file
- Download the original file
- Contacts named in this file
- Similar government files
- Ask GovTribe AI about this file
Text version
TSA
T S
A
T S
A
TOFA
TO
FA
T O
F A
CRITICAL BOUNDARY POINT
SEE NOTE #1
TAXIWAY C
T A
X I W
A Y
B
T A
X I W
B
TAXIWAY T
T A
X
IW
A Y
H
T
A
X
I W
A
X
I
W
D
R
U
N
W
T
A
X
I W
T S
A
TSA
TSA
T O
F A
TOFA
TOFA
Coast Guard and Sheltair Boundaries with Taxiway C Taxiway Object Free Area (TOFA)
Exhibit 2-1
SHELTAIR LEASE BOUNDARY
PROPOSED TAXIWAY PAVEMENT
PROPOSED TAXIWAY C CL
USCG PROPERTY BOUNDARY
DEMOLISH TAXIWAY/RUNWAY
PAVEMENT
TOFA
TSA
NOTES:
1. NO MONUMENTATION WAS FOUND FOR THIS POINT
IN THE FIELD. HOWEVER, THE POINT WAS SET BASED
ON THE LEGAL DESCRIPTION STATED IN THE EXHIBIT
“A” BOUNDARY SURVEY FOR ST. PETE-CLEARWATER
INTERNATIONAL AIRPORT PREPARED BY NORTHWEST
SURVEYING, INC., DATED JANUARY 18, 2019. THE
LEGAL DESCRIPTION BEGINS AT THE CERTIFIED
COORDINATE REPRESENTING THE SOUTHWEST
CORNER OF SECTION 34, TOWNSHIP 29S, RANGE 16E
(N 1300108.913, E 431206.842; STATE PLANE
COORDINATE SYSTEM, FLORIDA WEST ZONE,
HORIZONTAL DATUM: NAD83 (1990 ADJUSTMENT)).
ON MARCH 29, 2022 THE ACCURACY OF THIS POINT
AND THE ASSOCIATED BOUNDARY LEGAL DESCRIPTION
WAS CONFIRMED IN AUTOCAD BY NORTHWEST
SURVEYING, INC.
2. THE SHELTAIR LEASE BOUNDARY IS NOT DELINEATED
ON THE AIRPORT'S EXHIBIT A PROPERTY MAP. THE
LOCATION SHOWN WAS TAKEN FROM THE "ALT/NSPS
LAND TITLE SURVEY" DOCUMENT PREPARED FOR
SHELTAIR BY W.C. SHERRILL AND COMPANY, LLC.
DATED JULY 11, 2016. IN MARCH 2022, ECHO VERIFIED
THE LOCATION OF THE TWO SOUTHERN CORNERS OF
THE LEASE BOUNDARY (FOUND 2 IRON RODS) TO BE
WITHIN 1-INCH OF THE LOCATION SHOWN IN THE
AUTOCAD FILE THAT REPRESENTS THE REFERENCED
TITLE SURVEY DOCUMENT.
3. THE ROTATIONAL ORIENTATION OF THE TAXIWAY C
CENTERLINE HAS BEEN SET PARALLEL TO THE CLOSED
RUNWAY 9-27 CENTERLINE END COORDINATES. THESE
COORDINATES WERE TAKEN FROM A THIRD-PARTY FAA
ADVISORY 150/5300-18B COMPLIANT SURVEY,
PERFORMED ON THE 318TH DAY OF 2012. THE SURVEY
DATA WAS IN THE FORM OF A UNIVERSAL DATA
DELIVERY FORMAT (UDDF) FILE DOWNLOADED FROM
https://nfdc.faa.gov/nfdcApps/services/publicData/ uddfList.jsp.
RUNWAY 9-27 END COORDINATES USED ARE:
RUNWAY 9 END - N 1300356.057, E 431566.452
RUNWAY 27 END – N 1300482.887, E 436276.377
F i l e
P a t h t a m p f l f s T a m p a P r o j e c t s S t
P e t e C l w t r
C a r g o
A p r o n a n d
R u n w a y
C o n v e r s i o n C
A D
D d w g P
I E
E x h i b i t P r o j e c t
A r e a
C o a s t
G u a r d a n d
S h e l t a i r
B o u n d a r i e s w i t h
T a x i w a y
C a x i w a y
O b j e c t
F r e e
A r e a
T
O F
A d w g
D a t e
P
M
GRAPHIC SCALE IN FEET
20010050
TAXIWAY DESIGN GROUP 4
TAXIWAY OBJECT FREE AREA
(Airplane Design Group IV - 243 ft)
TAXIWAY SAFETY AREA -
(Airplane Design Group IV - 171 ft)
C
FM
A3
-2
A320-200
B737-900W
B737-900W
B737-900W
B737-900ERW
B737-900ERW
C
FM
-7
C
FM
-7 737-800W
7-
0W
C
FM
-7
C
FM
-7 737-800W
7-
0W
CFM
-7
CFM
-7
737-800W
737-800W
TA
XI
W
AY
A
R U
N W
AY
8-
TAXIWAY T
R98'
R98'
R11 0'
280.0'
TA
XI
W
AY
A
.3
7.
5'
G E90
G E90
777-200LR
7-
0L
R
B777
R92
R92'
TAXIWAY A4
A320
TAXIWAY C
B777
TS
A
TSA
TO
FA
TSA
TSA
TO
FA
FUTURE PAVED
SHOULDER EDGE
FUTURE FULL-STRENGTH
APRON EDGE
FUTURE VEHICLE
SERVICE ROAD
FUTURE TERMINAL
AIRCRAFT PARKING
.3
R11 0'
Fi le
P at h:
Y
:\S t.
Pe te
C lw tr\
_C ar go A pr on a nd
R un w ay
C on ve rs io n\
C
AD
D -d w g\
PI
E
Ex hi bi t\P ro je ct A re a
2\ 2-
Ta xi w ay A
Al ig nm en t.d w g
D at e:
/2 0/
:2
PM
GRAPHIC SCALE IN FEET
1005025Taxiway A4 Alignment Exhibit 2-2
PROPOSED TAXIWAY PAVEMENT
PROPOSED TAXIWAY CENTERLINE
PROPOSED TAXIWAY
EDGE MARKINGS
TOFA
TSA
TAXIWAY OBJECT FREE AREA
(Airplane Design Group V)
TAXIWAY SAFETY AREA
(Airplane Design Group V)
TAXIWAY DESIGN GROUP 4 OR 5
NOTES:
1. THE ROTATIONAL ORIENTATION OF THE TAXIWAY A4 CENTERLINE HAS BEEN
SET PERPENDICULAR TO THE RUNWAY 18-36 CENTERLINE END COORDINATES.
THE BASELINE ALIGNMENT OF TAXIWAY A WAS SET PARALLEL TO, AND 500-FT
OFFSET FROM THE RUNWAY 18-36 COORDINATES. THESE COORDINATES WERE
TAKEN FROM A THIRD-PARTY FAA ADVISORY 150/5300-18B COMPLIANT SURVEY,
PERFORMED ON THE 17TH DAY OF 2020. THE SURVEY DATA WAS IN THE FORM
OF A UNIVERSAL DATA DELIVERY FORMAT (UDDF) FILE DOWNLOADED FROM
https://nfdc.faa.gov/nfdcApps/services/publicData/uddfList.jsp. THE RUNWAY 18-36 END
COORDINATES USED ARE:
· RUNWAY 18 END - N 1305490.551, E 433122.687
· RUNWAY 36 END – N 1295863.857, E 434538.668
B737-900W B737-900W
B737-900ERW
B7
-9
W
B737-900W
B7
-9
W
B737-900W
B7
-9
ER
W
B737-900ERW
B737-900W
B737-900W
B737-900W
B737-900W
B737-900ERW
B737-900ERW
B737-900W
B737-900W
B737-900W
B737-900W
B737-900ERW
B737-900ERW
C
FM
-7
C
FM
-7 737-800W
7-
0W
C
FM
-7
C
FM
-7 737-800W
7-
0W
CFM
-7
CFM
-7
737-800W
737-800W
CFM56-7CFM56-7
737-800W
737-800W
CFM56-7
CFM56-7
737-800W
737-800W
C
FM
56-7 C
FM
56-773
7-
0W
737-800W
C
FM
56-7 C
FM
56-773
7-
0W
737-800W
CFM56-7
CFM56-7
737-800W
737-800W
CFM56-7CFM56-7
737-800W
737-800W
CFM56-7CFM56-7
737-800W
737-800W
CFM56
-7
CFM
-7
737-800W
737-800W
CFM56-7CFM56-7
737-800W
737-800W
CFM56-7CFM56-7
737-800W
737-800W
R U
N W
A Y
8-
TAXIWAY T
TA
XIW
AY D
TA
X
IW
A
Y A
TA
X
IW
A
Y A9.
10.20
9.80
10.80
10.40
-1 .8
-0
.8
-0 .7
.6
.6
10.00
.2
11.20
10.60
9.
9.
9.
8.80
8.00
8.
9.
8.
8.4
9.40
11.00
.0
.6
.6
9.
8.80 11.40
.4
10.40
9.60
10.80
.4
10.00
9.80
8.60
9.20
9.60
.0
9.80
9.
8.
7.
8.
8.80
8.80
8.
6.
7.20
7.60
8.00
9.60
9.20
8.00
7.607.40
8.00
6.005.805.80
6.006.20 8.00
10.00
10.80
.0
9.
8.80
9.
-1 .0
-1.0%
-1.0%
-1 .0
-1.0%
-1.1%
-1.
0%
-1.0%
-1 .0
-1 .5
-1.4%
-1.2%
-0.9% -1
.1
-0 .7
-1 .0
-1.0% -1.4%
-1 .1
-1.0%
-1 .0
-1 .0
-1 .0
-1 .0
-1 .0
-1 .1
-1.0%
-0.9%
-1.0%
-1.0%
-1 .5
-1.0%
-1.1%
-1 .3
-1 .0
-1 .0
-1.0%
-1 .1
-1 .1
-3.5%
-3.0%NEW INLET
LOCATION (TYP)
DECOMISSIONED RUNWAY 9-27
TO BE DEMOLISHED
593.8' 59 4'
196.7'196.7'79.0'
164.1'
172.7'
4'
4.
5'
135.0'. 135' 25'
197'197'79' 25'
-1 .0
-1 .0
-1 .0
-1 .0
-1.4%
-1.1%
-1 .0
%-1 .0
-1.2%
-1 .3
-1 .2
TAXIWAY 'C'
B737-800W
(TYP)
-1.
5%
.8
-1 .3
STORMWATER
POND
Fi le
P at h:
Y
:\P ro je ct s\ St
. P et eC lw tr\
_C ar go A pr on a nd
R un w ay
C on ve rs io n\
C
AD
D -d w g\
PI
E
Ex hi bi t\P ro je ct A re a
2\ 2-
Ea st T er m in al
E xp an si on -F ut ur e R am p
G ra di ng
S ch em at ic .d w g
D at e:
5/
/2
5:
P M
Terminal Expansion Grading Concept Exhibit 2-6
0 30 60 120
HORIZONTAL SCALE IN FEET
AutoCAD SHX Text
SD
AutoCAD SHX Text
WATER
AutoCAD SHX Text
SAN
AutoCAD SHX Text
WATER
AutoCAD SHX Text
WATER
AutoCAD SHX Text
WATER
AutoCAD SHX Text
WATER
AutoCAD SHX Text
BACK FLOW
AutoCAD SHX Text
BACK FLOW
AutoCAD SHX Text
BACK FLOW
AutoCAD SHX Text
BACK FLOW
AutoCAD SHX Text
BACK FLOW
AutoCAD SHX Text
BACK FLOW
AutoCAD SHX Text
WATER
AutoCAD SHX Text
BACK FLOW
AutoCAD SHX Text
BACK FLOW
AutoCAD SHX Text
BACK FLOW
AutoCAD SHX Text
SD
AutoCAD SHX Text
SD
AutoCAD SHX Text
SD
AutoCAD SHX Text
SD
AutoCAD SHX Text
SD
AutoCAD SHX Text
SD
AutoCAD SHX Text
SD
AutoCAD SHX Text
SD
AutoCAD SHX Text
SD
TAXIWAY T
TA
XIW
AY D
TA
X
IW
A
Y A
TA
X
IW
A
Y A
B7
-9
W
B737-900W
B7
-9
W
B737-900W
B7
-9
ER
W
B737-900ERW
B737-900W
B737-900W
B737-900W
B737-900W
B737-900ERW
B737-900ERW
B737-900W
B737-900W
B737-900W
B737-900W
B737-900ERW
B737-900ERW
C
FM
-7
C
FM
-7 737-800W
7-
0W
C
FM
-7
C
FM
-7 737-800W
7-
0W
CFM
-7
CFM
-7
737-800W
737-800W
CFM56-7CFM56-7
737-800W
737-800W
CFM56-7
CFM56-7
737-800W
737-800W
C
FM
56-7 C
FM
56-773
7-
0W
737-800W
C
FM
56-7 C
FM
56-773
7-
0W
737-800W
CFM56-7
CFM56-7
737-800W
737-800W
CFM56-7CFM56-7
737-800W
737-800W
CFM56-7CFM56-7
737-800W
737-800W
CFM56
-7
CFM56
-7
737-800W
737-800W
+0
+0
+0
+0
+0
+0
+0
+0
+0
+0
+0
+0
+0
+7
10.80
7+
8+
9+
+0
+0
+0
+0
+0
+0
+0
+0
+0
+0
+7
-1.2%
1+00
2+00
3+00
4+00
5+00
6+00
7+00
8+00
9+00
10+00
A A
B
C
B
C
9.60
.0
9.00
10.00
.8
9.
9.60
8.
80 8.
10.00
.6
.6
.6
.0
9.40
11.00
9.20
8.
8.
8.40
7.20
6.4
7.6
10.00
9.60
8.00
9.60
9.20
8.00
.0
8.80
9.
8.
8.
8.00
DECOMISSIONED RUNWAY 9-27
TO BE DEMOLISHED
TAXIWAY C
TAXIWAY T
Terminal Expansion Cross Sections Exhibit 2-7
Fi le
P at h:
Y
:\P ro je ct s\ St
. P et eC lw tr\
_C ar go A pr on a nd
R un w ay
C on ve rs io n\
C
AD
D -d w g\
PI
E
Ex hi bi t\P ro je ct A re a
2\ 2-
Ea st T er m in al
E xp an si on -F ut ur e C on ce pt ua l C ro ss -S ec tio ns fr om T er m in al to T ax iw ay C
.d w g D at e:
5/
/2
5:
P
M
0 30 60 120
HORIZONTAL SCALE IN FEET
0 3 6 12
VERTICAL SCALE IN FEET
SECTION A-A
SECTION B-B SECTION C-C
PLAN
0 50 100 200
GRAPHIC SCALE IN FEET
AutoCAD SHX Text
WATER
AutoCAD SHX Text
SAN
AutoCAD SHX Text
SD
AutoCAD SHX Text
SD
AutoCAD SHX Text
EOI
AutoCAD SHX Text
EOI
AutoCAD SHX Text
SD
AutoCAD SHX Text
SD
AutoCAD SHX Text
SD
AutoCAD SHX Text
GRADE BREAK STA = 19+67.11 ELEV = 10.84
AutoCAD SHX Text
GRADE BREAK STA = 20+60.00
AutoCAD SHX Text
ELEV = 11.77
AutoCAD SHX Text
GRADE BREAK STA = 22+36.88
AutoCAD SHX Text
ELEV = 11.77
AutoCAD SHX Text
GRADE BREAK STA = 22+99.13 ELEV = 11.15
AutoCAD SHX Text
GRADE BREAK STA = 24+31.20
AutoCAD SHX Text
ELEV = 10.36
AutoCAD SHX Text
2ND LEVEL FLOOR ELEV = 23.0'-24.0'
AutoCAD SHX Text
12:1 MAX
AutoCAD SHX Text
12:1 MAX
AutoCAD SHX Text
PROP GRADE PROFILE (TYP)
AutoCAD SHX Text
EXIST GROUND PROFILE (TYP)
AutoCAD SHX Text
FUTURE TERMINAL BUILDING
AutoCAD SHX Text
BOARDING BRIDGE
AutoCAD SHX Text
BOARDING BRIDGE
AutoCAD SHX Text
EXIST. ELEVATION (TYP)
AutoCAD SHX Text
PROP ELEVATION (TYP)
AutoCAD SHX Text
B737-800W FULLY LOADED SILL HEIGHT 8.5'
AutoCAD SHX Text
A320-NEO FULLY LOADED SILL HEIGHT 11.09'
AutoCAD SHX Text
B737-800W FULLY LOADED SILL HEIGHT 8.5'
AutoCAD SHX Text
A320-NEO FULLY LOADED SILL HEIGHT 11.09'
AutoCAD SHX Text
TERMINAL EXPANSION FFE~11.77'
AutoCAD SHX Text
GRADE BREAK STA = 19+14.56 ELEV = 10.49
AutoCAD SHX Text
2ND LEVEL FLOOR ELEV = 23.0'-24.0'
AutoCAD SHX Text
12:1 MAX
AutoCAD SHX Text
B737-800W FULLY LOADED SILL HEIGHT 8.5'
AutoCAD SHX Text
EXIST. ELEVATION (TYP)
AutoCAD SHX Text
PROP. ELEVATION (TYP)
AutoCAD SHX Text
PROP GRADE PROFILE (TYP)
AutoCAD SHX Text
EXIST GROUND PROFILE (TYP)
AutoCAD SHX Text
FUTURE TERMINAL BUILDING
AutoCAD SHX Text
BOARDING BRIDGE
AutoCAD SHX Text
A320-NEO FULLY LOADED SILL HEIGHT 11.09'
AutoCAD SHX Text
TAXIWAY 'C' CENTERLINE PROFILE
AutoCAD SHX Text
TERMINAL EXPANSION FFE~11.77'
AutoCAD SHX Text
GRADE BREAK STA = 0+37.40
AutoCAD SHX Text
ELEV = 8.12
AutoCAD SHX Text
GRADE BREAK STA = 0+55.00
AutoCAD SHX Text
ELEV = 9.00
AutoCAD SHX Text
GRADE BREAK STA = 1+00.00
AutoCAD SHX Text
ELEV = 9.46
AutoCAD SHX Text
GRADE BREAK STA = 4+61.50
AutoCAD SHX Text
ELEV = 11.77
AutoCAD SHX Text
GRADE BREAK STA = 7+38.98
AutoCAD SHX Text
ELEV = 5.98
AutoCAD SHX Text
GRADE BREAK STA = 12+66.81 ELEV = 11.77
AutoCAD SHX Text
GRADE BREAK STA = 11+46.78 ELEV = 11.77
AutoCAD SHX Text
GRADE BREAK STA = 8+01.51
AutoCAD SHX Text
ELEV = 9.11
AutoCAD SHX Text
GRADE BREAK STA = 8+46.51
AutoCAD SHX Text
ELEV = 9.56
AutoCAD SHX Text
GRADE BREAK STA = 16+23.90
AutoCAD SHX Text
ELEV = 11.00
AutoCAD SHX Text
GRADE BREAK STA = 16+90.07
AutoCAD SHX Text
ELEV = 10.10
AutoCAD SHX Text
GRADE BREAK STA = 17+54.06
AutoCAD SHX Text
ELEV = 6.90
AutoCAD SHX Text
2ND LEVEL FLOOR ELEV = 23.0'-24.0'
AutoCAD SHX Text
12:1 MAX
AutoCAD SHX Text
12:1 MAX
AutoCAD SHX Text
FUTURE TERMINAL BUILDING
AutoCAD SHX Text
EXIST. ELEVATION (TYP)
AutoCAD SHX Text
PROP. ELEVATION (TYP)
AutoCAD SHX Text
PROP GRADE PROFILE (TYP)
AutoCAD SHX Text
EXIST GROUND PROFILE (TYP)
AutoCAD SHX Text
FUTURE GRADE CHANGE, WEST TERMINAL EXPANSION (LONG-TERM)
AutoCAD SHX Text
B737-800W FULLY LOADED SILL HEIGHT 8.5'
AutoCAD SHX Text
A320-NEO FULLY LOADED SILL HEIGHT 11.09'
AutoCAD SHX Text
B737-800W FULLY LOADED SILL HEIGHT 8.5'
AutoCAD SHX Text
A320-NEO FULLY LOADED SILL HEIGHT 11.09'
AutoCAD SHX Text
TERMINAL EXPANSION FFE~11.77'
PV
I 1
0+
.5
EL
EV
.0
PV
I 2
7+
.4
EL
EV
.8
-0.40% 0.60% 0.00%
-0.27%
10+00
8.
11+00
8.
7.
12+00
7.
7.
13+00
7.
8.
14+00
7.
8.
15+00
7.
9.
16+00
7.
9.
17+00
7.
9.
18+00
8.
9.
19+00
8.
9.
20+00
8.
9.
21+00
7.
9.
22+00
7.
9.
23+00
7.
9.
24+00
7.
8.
25+00
7.
8.
26+00
7.
8.
27+00
7.
7.
28+00
8.
PROPOSED GRADE
TAXIWAY C
EXISTING GROUND
EXISTING ELEVATION
PROPOSED ELEVATION
PC
: 1
5+
.5
M id
: 1 5+
.7
PT
: 1
5+
.9
PC
: 1
7+
.5
M id
: 1 8+
.7
PT
: 1
8+
.9
CENTERLINE TERMINAL
EXPANSION
STA. 21+15.62
ELEV. = 9.46'
PVI STA: 21+44.90
PVI ELEV: 9.47
K: 373.95
LVC: 100.00
PV
C
: 2 0+
.9
EL
EV
: 9
.4
PV
T:
1+
.9
EL
EV
: 9
.3
PVI STA: 15+04.64
PVI ELEV: 9.47
K: 165.41
LVC: 100.00
PV
C
: 1 4+
.6
EL
EV
: 9
.1
PV
T:
5+
.6
EL
EV
: 9
.4
PVI STA: 11+83.31
PVI ELEV: 7.53
K: 99.54
LVC: 100.00
PV
C
: 1 1+
.3
EL
EV
: 7
.7
PV
T:
2+
.3
EL
EV
: 7
.8
LOW PT. STA: 11+73.13
LOW PT ELEV: 7.65
10+00 11+00 12+00 13+00 14+00 15+00 16+00
17+00 18+00 19+00 20+00 21+00 22+00 23+00 24+00 25+00 26+00 27+00 28+00
TAXIWAY H
TA
XI
W
AY
A
TA
XI
W
AY
B
TAXIWAY C
DECOMISSIONED RUNWAY 9-27
TO BE DEMOLISHED
Taxiway C Plan and Profile Exhibit 2-8
Fi le
P at h:
Y
:\P ro je ct s\ St
. P et eC lw tr\
_C ar go A pr on a nd
R un w ay
C on ve rs io n\
C
AD
D -d w g\
PI
E
Ex hi bi t\P ro je ct A re a
2\ 2-
Ea st T er m in al
E xp an si on -T ax iw ay C
C en te rli ne E le va tio n.
dw g
D at e:
5/
/2
5:
P M
SHELTAIR LEASE BOUNDARY
PROPOSED TAXIWAY PAVEMENT
USCG PROPERTY BOUNDARY
DEMOLISH PAVEMENT
0 30 60 120
HORIZONTAL SCALE IN FEET
0 3 6 12
VERTICAL SCALE IN FEET
TAXIWAY C PROFILE
TAXIWAY C PLAN
| Sheets and Views |
| Avi-Plan Movements |
File details come from the government source that posted it. Updated .