2008 FAA Funding ProgramKalispell City Airport - S27
James H. Patrick, City Manager
Fred A. Leistiko, Airport Manager
Post Office Box 1997 - Kalispell, Montana 59903
Telephone (406) 250-33065 Fax - (406) 758-7758
TO: City Manager
City Attorney
RE: FAA Funding Program for 20(j
Some of the documents show how much money is allocated to Montana Airport District Office
of the FAA in Helena.
istiko � Fred r,Manager
Kalispell City Airport
Kalispell City Airport - S27
James H. Patrick, City Manager
Fred A. Leistiko, Airport Manager
Post Office Box 1997 - Kalispell, Montana 5990' )
Telephone (406) 250-3 )065 Fax - (406) 758-7758
DATES FUNDING AQ1LQT,9
January 2008 NW Region ADO's meet in Seattle to review and prioritize major projects
scheduled for FY 2009 — 2011. Deadline for projects was June 2007.
April 2008 Notice will be given that all applications and preapplications be submitted to
the ADO no later than May 1, 2008. This includes a valid Environmental
Assessment; a current Airport Layout Plan; and any airspace actions needed to
move the project forward.
May 2008 Based on Capital Improvement Programs submitted in August 2007, the NW
Region will submit its request for funding to the FAA Headquarters in D.C.
June 2008 NW Region submits its FIT 2009 discretionary funding candidate list to the
FAA Headquarters.
June 2008 Bid Openings for Grants using Discretionary or State Apportionment funcim
should be held no later than June 1, 2008. 1
July 2008 Bid Openings for Grants using Primary or Nonprimary f1mds should be held no
later than July 1, 2008.
July 2008 Grants for projects, including land acquisition projects, using Discretionary or
State Apportionment funds to be issued no later than July 1, 2008.
August 2008 Grants for projects using Primary or Nonprimary funding "only" to be issued
no later than August 1, 2009.
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1117, 1 w- IIIIIIIIIIIIIIII qIIIIIIJIgIIIIII 10-0' II]
FY-2007
(Total millions)
* FY-07 State Apportionment
* FY-06 SA Carryover
= $ 1.03
Nonprimary
= $ 7.89
* FY-06 Nonprimary
= $ 2.65
Nonprimary
* FY-04 Nonprimary
= $ 0.07
Total GA Funds Available
$18.06
Total GA Funds Used
Total Discretionary Granted = $ 1.66
Total = $14.80
General Aviation Funding Federal Aviation
October 3, 2007 1-0 Administration 2I
I ipl '11111 I'VICTRIT"
®
(Total millions)
® FY-08 State Apportionment
= $ 5.80 (est.)
* FY-07 SA Carryover
= $ .00
® FY-08 Nonprimary
= $ 7.89 (est.)
® FY-07 Nonprimary
=$ 3.80
FY-06 Nonprimary
= $ 1.06
FY-05 Nonprimary
=$ 0.17
Estimated GA Available
= $18.72 (est.)
Estimated Discretionary
= 1_1.60 (est.)
Estimated Total
= $20.22 (est.)
General Aviation Funding
October 3, 2007
Federal Aviation
rM Administration 3
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S Y S r E M S
PRE-ENGINEERED STRUCTURAL AIRCRAFT CANOPIES
Manufactured by ProtekPark Systems
5513 Vine Street
Cincinnati OH 45217
513/242-0310
PART 1— GENERAL
PART 2 — PRODUCTS
PART 3 — EXECUTION
A. This section covers the furnishing and installing of the structures, footings and all other
items required to furnish and install a complete system.
I K III 1101111,1151EWW-1 _WAI A- 1I
A. Framing for the Aircraft Canopies shall be designed in accordance with all applicable at
and local building codes. Manufacturer to provide written structural analysis prepared and
certified by a professional engineer licensed in the State indicating that the structures and the
footings meet required design loads.
b. Live / Snow Loading — Withstands vertical roof loads based on
ICI3O/130CA/Sl3CCI guidelines or local building codes whichever is greater.
C. If site specific load requirements exceed pre -design loading (below), section sizes
and connections will be bolstered to meet local code.
Dead Load - 10 lbs per psf
Live Load — 30 lbs psf on horizontal projected areas
Wind Load — 90 mph on vertical projected areas
A. Installation shall be by experienced crews employed by the Aircraft Canopy
Manufacturer. The canopies will be erected in accordance with approved
manufacturers drawings and instructions.
B. The structure shall be manufactured in accordance with standard approved
practices. Testing shall be performed in accordance with AS TM standards
and test reports must be certified and submitted by an independent test
laboratory.
1.04 SUBMITTALS:
A. Drawings and calculations shall be submitted by the manufacturer prior to
fabrication. No fabrication of the structures or ordering of materials shall be done
until these submittals are approved by the owner and local building authority.
SIHMEM
" n1l
Approval submittals shall include engineered stamped drawings for the appropriate State, a
full set of engineering calculations, and full equipment submittal.
1111:11:11 r1l
a. Cover Sheet
b. Column / Post Plan
c. Column Anchoring Detail
d. Truss Framing Detail
e. Roof Detail
f. Elevations
g. Gutter Detail (if applicable)
A. Delivery of materials to jobsite in manufacturers packaging
C. Materials to be stored in a clean, dry and covered area that is secure and protected from
weather.
W
A. Structure shall be designed and detailed according to good engineering practice.
The Aircraft Canopies will be a series of connected modules cantilevered from a
single line of columns under the ridge. Columns will be spaced at 21' on center with
cantilevered trusses on each side of each column extending a minimum of 21'-0" to
each eave. Out to out of truss measurement shall be 42' unless specified otherwise.
B. A minimum of 10' clearance is required at the lowest point on the trussed canopies.
C. All structures will have a minimum V2:12 roof slope
D. Concrete footing will have a minimum compressive strength of 4,000 psi after 28 days.
E. Footing reinforcing steel will be ASTM A615 Grade 60 deformed billet steel.
F. Columns will be ASTM A500 Grade B steel tubing with a minimum yield stress of 46,000
lbs. with factory welded brackets and plates of ASTM A36 structural steel plate. No on -site
welding should be required. Columns will be shot blasted, e-coated and powder coated after
fabrication.
G. Trusses will use ASTM A500 steel tubing with a minimum yield stress of 46,000 p.s.i. for
top chord, bottom chord and webs. All trusses will be factory welded. Purlin clips to be
welded to sides of truss top chord. No on -site welding should be required. Trusses to be
designed to minimize roosting or nesting of birds. Truss members will have a full zinc based
organic coating applied to the interior surface for corrosion protection. The exterior coating
will be galvanized and or e-coated and powder coated after fabrication.
11q. Purlins will be ASTM A-500 steel tubing. "C" or "Z" purlins are not permitted. Purlins —
sections will have a full zinc based organic coating applied to the interior surface for
corrosion protection. The exterior coating will be galvanized and or e-coated and powder
coated after fabrication. To minimize any possibility of birds roosting or nesting all purlins
will be located between truss top chords with the top of purlins being flush with the top of
the top chord and with a maximum 3/16" clearance between the ends of the purlins and truss
top chords. Purlins to be bolted to clips on truss top chords with Grade 5 bolts.
1. Roof System will be 26 gauge (UL 90 rated), 36" wide x 1-1/4" high major rib at 12" o.c.
and two minor ribs between major ribs with trapezoidal rib configuration. Field applied
sealant required at side laps and end laps. Minimum slope will be .5:12. Substrate will be
galvalume sheet steel, minimum yield of 80,000 PSI. Panels will be one piece from eave to
ridge -no splicing of deck panels. Panels shall have a finish side coated with a full coat of
premium silicone polyester. Color to be selected from metal roof system manufacturer's
standard offering. Panels will have a minimum 20 year manufacturer's finish warranty
against cracking, checking and fading.
1. Roof fasteners will be self tapping/self drilling type and shall be designed to withstand
specified design loads. Fasteners to be provided with a factory applied coating in a color to
match metal panels. Neoprene washers under heads will be supplied for all roof fasteners.
Fasteners to be located and spaced in a true vertical and horizontal alignment and in a pattern
recommended by panel manufacturer. Proper torque settings to be applied to obtain
controlled uniform compression for a positive seal with out rupturing the neoprene washer.
J. Gutter and Downspouts will be supplied if specified separately. Gutters to match the col
of roof panels. One downspout to be supplied for each 21' x 48' module will be attached
the bottom chord of the truss and to one side of each column. Downspouts to attach at
alternate sides of adjacent columns. I
A. All materials are new, of good quality and without defects which would lessen quality of
work.
C. Canopy erection drawings are furnished at time of shipment.
M
A. General Contractor shall direct, oversee and inspect all site work related to the Aircraft
Canopy Installation. Site preparation must be in accordance with finals drawings and
specifications provided by manufacturer.
B. Canopy contractor shall inspect site and notify general contractor in writing of any
condition/s that may inhibit the proper and timely construction of the canopies. Canopy
contractor is under no obligation to proceed until conditions have been sufficiently corrected.
W-111 01�- -1 �110;1 �x
B. Installation of the entire system and all components shall be in strict accordance with
manufacturer's recommendations.
A. After the system has been fully erected, the general contractor shall provide the materials
and labor to grout the base of the column to produce a finished joint.
B. Canopy contractor shall place all trash and debris into appropriate receptacles provided
the general contractor. I
A. Canopy manufacturer shall provide a one (1) year warranty on materials and workmanship
from the date of substantial completion.
B. Canopy manufacturer shall provide complete warranty information on all manufacture
providing accessories within the system. i
:S Y S T E M S
NOTE:
PIER DIAMETER AND DEPTH TO BE
DETERMINED BY LOADS AND SOIL
CONDITIONS.
Voice: 800.543.7351
F= 513.242.0816
E—mail: ppOroughbros.com
Website: www.roughbros.com
Total Metal Canopy Service: Design + Fabrication « Installation * Parts « Repair Service