SOW Att 3 - C-130J Mooring Points Stamped Drawings.pdf
PDF 484 KB Posted
- Attached to
- Construct 176WG ADS Pad Federal contract opportunity
- Solicitation number
- W50S6L-20-B-0016
About this file
This document contains details for a federal solicitation seeking construction services. The solicitation requests bids to construct a concrete foundation pad and associated support work for a Relocatable Simulator Shelter at the 176th Air Defense Squadron, 176th Wing Campus, Alaska Air National Guard in Joint Base Elmendorf-Richardson, Alaska. The project includes a base bid and two optional bid items, with a total project value between $250,000 and $500,000. Interested contractors are encouraged to attend an organized site visit on July 14, 2020 at 2:00 PM Alaska Standard Time. Bids are due by July 30, 2020 at 2:00 PM AKST and must be submitted according to the instructions in the solicitation. The North American Industry Classification System code for this work is 236220 and the solicitation is anticipated to be a total small business set-aside, with a small business size standard of $39.5 million average annual revenue.
View the file
Other files for this federal contract opportunity
| File | Type | Posted |
|---|---|---|
| Bid Abstract_ADS Pad BetaSAM.pdf | ||
| Amendment 3 - Questions and Answers.pdf | ||
| Amendment 2 -Questions and Answers.pdf | ||
| Solicitation W50S6L-20-B-0016.pdf | ||
| SOW Att 2 - ANG RSS Site Prep_Release_v3.1.pdf | ||
| Amendment 1 -Questions and Answers.pdf | ||
| Solicitation W50S6L-20-B-0016.pdf | ||
| Solicitation W50S6L-20-B-0016.pdf | ||
| SOW - Construct 176WG ADS Training Pad 20200622.pdf | ||
| SOW Att 2 - ANG RSS Site Prep_Release_2.0.pdf | ||
| SOW Att 1 - RSS Concept Site Plan.pdf |
Show all 11
On GovTribe
Work with this file on GovTribe
- Download the original file
- Contacts named in this file
- Similar government files
- Ask GovTribe AI about this file
Text version
ALASKA AIR NATIONAL GUARD 176TH WING
C-130J SUPER HERCULES
AIRCRAFT MOORING ON STANDARD 30-FOOT SPACED TIE-DOWN RING GRID
SHEET INDEX
ID NAME
T1.0 COVERSHEET
S-1.0 MOORING POINT PLAN
S-2.0 DETAILS
MOORING/ TIE-DOWN DESIGN
THE C-130J IS A 4-ENGINE TURBOPROP MILITARY AIRCRAFT
UTILIZED IN SEARCH AND RESCUE, AERIAL REFUELING, AIRDROP,
TRANSPORT, HUMANITARIAN AND COMBAT MISSIONS AROUND
THE WORLD. NEW TIE-DOWN POINTS ARE REQUIRED AS THE
FORMER C-130 MODEL UTILIZED DIFFERENT TIE-DOWN POINTS.
UNIFIED FACILITIES CRITERIA (UFC) 3-260-01 REQUIRED MOORING
ANCHORS FOR FIXED-WING AIRCRAFT THAT WILL RESIST A
15,250-POUND FORCE APPLIED AT 19 DEGREES RELATIVE TO THE
PAVEMENT SURFACE.
UNLESS SPECIFICALLY WAIVED IN WRITING BY THE FACILITY
COMMANDER, NEWLY CONSTRUCTED AIRCRAFT PARKING
APRONS WILL INCLUDE AIRCRAFT MOORING POINTS DESIGNED
FOR A 67,800-NEWTON (15,250-POUND) LOAD, AS SPECIFIED IN
TM 1-1500-250-23 AND APPLIED AT 19.15 DEGREES (19.15°) FROM
THE PAVEMENT SURFACE. TESTING OF NEW MOORING POINT
INSTALLATIONS IS NOT REQUIRED; HOWEVER, IF TESTING IS
PERFORMED FOLLOW UFC 3-260-01 FIGURE B11-2.
MOORING POINTS FOR RIGID PAVEMENTS WILL BE PROVIDED BY
EMBEDDING THE MOORING DEVICES IN STANDARD ELMENDORF
AIRFIELD CONCRETE MIX REQUIREMENTS. MOORING POINTS
SHALL BE AT LEAST 3-FEET FROM THE EXISTING JOINTS.
MOORING POINTS LESS THAN A MINIMUM OF 3-FEET FROM ANY
PAVEMENT EDGE OR JOINT THE CONTRACTOR SHALL REMOVE
CONCRETE TO THE EXISTING JOINT REPLACE. REINFORCING
STEEL REBAR SHOULD BE PLACED AROUND THE MOORING
POINTS AS ILLUSTRATED.
THE TIEDOWNS ARE DESIGNED TO BE INSTALLED AT THE
EXISTING 176TH WING ALASKA AIR NATIONAL GUARD PARKING
APRONS.
[*THESEcoNsrRITCfior~fooCl.JrV1ENrs weRE cREATED AND scALE:o To sE PRINTED AT 100% oN 11"x11" PAPER 1 100% DESIGN
~"''""'''{<6,.i A~. qf. A~:1&'\t<o ,~'t·· ~;)t,•, ~.:..-49 TH ~ "-. * ~
~~~/Ii;; · ···~ ~ . . ...... ??.:-:- l ~ · · : .... p~;rick LeMay :~ ~ f! {b ·. CE-11007 . ·~;
'• 64>;;.. . . · ~<§ .-~-\~tLipROFES0SiG~~.:
LeMay Engineering & Consulting, Inc.
4272 Chelsea way Anchorage, AK 907,250.9038
0:: 0:::
LU Cl) :::> C>
0... LU _J
:::::> _J z
(/) :::::> 0 z
0 0:: 0:::
~ LU <{
"";- I ~ en (.) ::i
REVISION SCHEDULE
# l DESCRIPTION l DATE
IW~&Y II°"' I ;Rl 04/01/2020
1::'"" 11:~3ANGC130 I
1;:RSHEET I
SHEET NO.
T-1.0
I
NOTES - - 330" - -
I 30"
• RAMP MOORING POINT
0 AIRPLANE MOORING POINT I
f I 131"
11294" --~
360" t I
143"
I
360"
I I t "'\ ' I - .
I
> I
360"
360"
180" 180" - +- 180" 180" 180" - 180" 180"
30' 30' 30' ----
I I G) MOORING POINT PLAN 100% DESIGN
II
~""'-'-"-'\:\•r /a/ -.""OF A '\~> .. ::~~. · ..... ~1& \.~co
,,.~~· •. t•j '0. '.T ' 1~*-'4 TH · ..• ~ ~ . ........ : ... ~ .. l ~J ·.. Patrick LeMay :~ ~
'#6°\·.. CE-11007 .. ·~,:
'• .,,~ • • • • .• ~<§ ,-'\{to PROFEs.s\o~~'-::-
LeMay Engineering & Consulting, Inc.
4272 Chelsea way Anchorage, AK 907,250.9038
I 0::
0:::
II wen ::> a.. UJ
:::> _J z en :::> 0 I-z
0 0:: 0::::
('*') UJ <(
~I ;2 Cl)
II () ::s
REVISION SCHEDULE
# DESCRIPTION l DATE
1-·, II"'" l BRL 04/01/2020
1-···· r ., I PML 020003 ANG C130
1:~;ING POINT PLAN _I
S-1.0
MOORING PROFILE NOTES
1. CONTRACTOR TO REMOVE ADDITION EXISTING CONCRETE AND
REPLACE WHEN THE MINIMUM DISTANCE FROM SAW CUT TO AN
UN-DOWELED JOINT IS 3'.
2. BAR WILL BE NUMBER 7 (0.875") NON-DEFORMED AISI 8620H
STEEL.
3. FOR INSTALLATION IN PREEXISTING SLABS, INSTALL 1"0 X 16"
DOWEL RODS CENTERED AT HALF SLAB DEPTH, ALL FOUR SIDES
AS SHOWN IN THE PLAN VIEW.
REBAR DETAIL NOTES
1. EDGE OF RETROFIT PATCH WILL BE MINIMUM 3' FROM NEAREST JOINT IN BOTH
DIRECTIONS TO REDUCE RISK FOR SYMPATHETIC CRACKS IN EXISTING SLAB. IF
TIE-DOWN MUST BE CLOSER TO JOINT, THEN EXPAND RETROFIT PATCH TO THE
NEAREST JOINT.
EXISTING MOORING AND GROUNDING POINT NOTES
1. THE EXISTING PARKING PADS ON ELMENDORF FOR THE C-130J ALREADY HAVE
INSTALLED GROUNDING POINTS. EXISTING GROUNDING POINTS TO REMAIN.
2. TO BE FULLY COMPLIANT WITH UFC GUIDELINES AND TO ENSURE THAT NEW
MOORING POINTS ARE A MINIMUM OF 3-FEET AWAY FROM ANY EXISTING
PAVEMENT JOINTS, ALL EXISTING MOORING POINTS BE FILLED AND LEVELED
OFF WITH EPOXY. MEDIUM-VISCOSITY PRIME BOND 3000 EPOXY OR BITTER
SHOULD BE USED TO FILL EXISTING MOORING POINTS.
CONCRETE AND BONDING POINTS
1. THE EIGHT REBAR DOWELS USED TO SECURE THE REBAR CAGE
SHALL BE BOUND WITH EPOXY IN THE CORE-DRILLED HOLES
WITHIN THE EXISTING CONCRETE PAD. NEW CONCRETE SHOULD BE
POURED WHILE THE EPOXY IS STILL TACKY. IF EPOXY IS ALLOWED
TO CURE FOR MORE THAN 24-HOURS, THE SURFACE EPOXY
SURROUNDING THE DOWEL SHALL BE ROUGHENED TO HELP
INCREASE BOND STRENGTH. LOW-VISCOSITY PRIME BOND 3900
EPOXY OR BETTER SHOULD BE USED IN SECURING THE REBAR
DOWEL.
2. ALL CONCRETE SAW CUTS SHALL BE FILLED USING STANDARD
ELMENDORF AIRFIELD JOINT SPECIFICATIONS. CONTRACTOR
SHALL VERIFY REQUIREMENTS WITH THE AIRFIELD MANAGER.
3. CONTRACTOR SHALL USE STANDARD ELMENDORF AIRFIELD
SPECIFICATIONS FOR CONCRETE. CONTRACTOR SHALL VERIFY
REQUIREMENTS WITH THE 673 CES PAVEMENTS ENGINEER.
5"
I
DOWEL PRE-EXISTING SLABS. \ I I " #5 REBAR, SIX
DOWEL CAGE -"\ I r- RADIUS = 3 ,,,- EACH WAY, TYP.
L.l Lj <J m==~=~=~~\~~://; ___ ~ <J Lj 10" MINIMUM
<J I
G) MOORING PROFILE
3'-6"
® REBAR DETAIL
SCALE: 1 1/2" = 1'-0"
I
WIRE TIE
2'
<J
"" 4 ·'
. "4 "
" v " .
·11 / <J I
~ 7 .. _j Lj l- 6" L'.J I . 5"
3'
3'-6"
_J
8"
L REBAR D
" 8" ~
~ ALLJOIN
/ TIED.
v " T., ~ t " -~
~ 1'
~ (-\ ,," " i "
" 7" \__ _/ - r - 3"MIN " 4"' " . " " .
. f I., 7" t
4 12" MIN
" 4 ~
- 6" ~
- 1· -ii .
Lj
OWELCAGE,
TS ARE WIRE
100% DESIGN
A~.9f.~~1&\~~~ ---.L~.· *.t•j '-0"· ._, 'I, ; *:. 4~ -~~ ........ .": ~- ~ ~··~ ~~ ~ ~ .e~'tf? ... ~;~.~ ~J •. Patrick LeMay :~ ~ '#t~··. CE-11007 . . ·~...:
'• ~~·· .. . . · ·~r$ --\,{to PROFEs.s10~~..?'
LeMay Engineering & Consulting, Inc.
4272 Chelsea way Anchorage, AK 907,250.9038
0::: 0:::
<( w en :J <.9 a.. w _J
:::::> .....I z en :::::> 0 I-z
0 0::: 0:::
('I') w <(
"-;- I ~ en
REVISION SCHEDULE
11 l DESCRIPTION l
DATE
l'"'M"' II"" I BRL 04/01/2020
1:7'°" 11::03ANGCBO I
1~;T;LS I
S-2.0
File details come from the government source that posted it. Updated .