DRAFT SOW Att 3 - C-130J Mooring Points Stamped Drawings.pdf

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.

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SHEET NO.

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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"

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DOWEL PRE-EXISTING SLABS. \ I I " #5 REBAR, SIX

DOWEL CAGE -"\ I r- RADIUS = 3 ,,,- EACH WAY, TYP.

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1:7'°" 11::03ANGCBO I

1~;T;LS I

S-2.0