FJRP159073-MS501-Amd03.pdf

S c a l e

F o r

M i c r o f i l m i n g

I n c h e s

M i l l i m e t e r s date detailed checkeddesigned ofsheet sheets project contract rev.drawing file

PRELIMINARY - NOT

FOR CONSTRUCTION

NORTH CAROLINA AIR NATIONAL GUARD

DOUGLAS INTERNATIONAL AIRPORT

CHARLOTTE, NORTH CAROLINA

KANSAS CITY, MISSOURI

ENGINEERS ARCHITECTS & CONSULTANTS

Project No. - FJRP159073

C-17 TYPE III HYDRANT

REFUELING SYSTEM/

RAMP EXPANSION

94893

C O

P Y

R I G

H T

B U

R N

S

M c D

O N

N E

L L

E

N G

I N

E E

R I N

G

C

O M

P A

N Y

I N

C

D

2 3

C

4 5

A

B

C O

P Y

R I G

H T

MS501

FJRP159073-MS501.DWG

V.KEEBLE

B.COOVER R.PERUE

PIT COVER CAST "FUEL DRAIN"

REFER TO STRUCTURAL DRAWING

FOR BACKFILL DETAILS

HYDRANT CONTROL

VALVE, 6" API 1584,

COUPLER ADAPTER 4"

QUICK DISCONNECTS

LOCATED ABOVE GRATE,

WITH CAPS AND

RETAINING CHAIN

FULL PORT 6" BALL

VALVE

1 1/2" PIPE WITH

BRONZE MALE CAM

TYPE ADAPTOR WITH

DUST CAP

SLOPE FLOOR 3" TO PUMPOUT

OVER WIDTH OF PIT

FULL LENGTH STEP DOWN

PLATFORM/GRATE (REMOVABLE). WELD

RING TO GRATE AT VALVE

PENETRATION, MAXIMUM SPACE

BETWEEN VALVE AND RING 2"

CONNECT VALVE

TO GROUND

COVER HAND HOLE FOR

LIFTING (TYP OF 2)

1 1/2" LOW POINT PUMPOUT

PLAN

FUEL

FUEL

I N

S I D

E

" INSIDE

SECTION B

COUNTERWEIGHT

ALUMINUM COVER

PRESSURE GAUGE,

BELOW GRATE OR

ATTACHED TO PIT WALL

CONE STRAINER

BUNA-N BOOT SEAL

AND (2) S.S. BANDS

1/2" THK.

FIBERGLASS PIT

INSULATING

FLANGE (IF)

COUNTER

WEIGHT

BOLT GROUND

TO VALVE

PIPE SLEEVE WITH

MECHANICAL

ADJUSTABLE

SEGMENTED SEAL IN

SLEEVE. DETAIL A3 /

MS501

PITS FOR PARALLEL

FUEL LINES WILL HAVE

BOTH LOW POINTS IN

ONE PIT

BUTT WELD JOINTS

WELDING BRANCH

BUNA-N SEAL WITH

STAINLESS STEEL

BANDS

1/4" THK. FIBERGLASS PIT

2" CS

IF

2" BALL VALVE

2" MALE CAM TYPE DRY

BREAK CONNECTOR W/

FEMALE DUST CAP. 4 1/2"

FROM TOP OF PIT LID

BUNA-N BOOT COLLAR W/

STAINLESS STEEL

ATTACHMENT BANDS

INSIDE PIT

PIPING C

L

"B" FUEL PIPING SLEEVE W/

3/8"x2" STEEL ANCHOR

RING MOLDED INTO THE

FIBERGLASS PIT WALL BY

MANUFACTURER. SLEEVE

TO EXTEND THROUGH

CONCRETE A MIN OF 4"

WHERE APPLICABLE.

FIBERGLASS PIT WALL

CASING INSULATOR SHALL HOLD

CENTERLINE OF FUEL PIPE ON

CENTERLINE OF CASING

MECHANICAL ADJUSTABLE SEGMENTED

SEAL IN SLEEVE (TYP OF 2 PLACES)

"A" FUEL LINE

SHRINK SLEEVE W/ STAINLESS STEEL

ATTACHMENT BANDS OUTSIDE PIT

A1

HYDRANT OUTLET PIT DETAIL (HYDRANT HOSE TRUCK)

SCALE: NOT TO SCALE

B3

LOW POINT DRAIN PIT (PAVED)

SCALE: NOT TO SCALE

A

MS501

B

MS501

GENERAL NOTES: THIS DRAWING ONLY

1. REFER TO DRAWINGS M-001 AND M-002 FOR

LEGENDS, ABBREVIATIONS AND GENERAL

PROJECT NOTES.

2. PIT LID HINGE TO BE PARALLEL TO THE

AIRCRAFT CENTERLINE AND LID TO OPEN

TOWARD THE AIRCRAFT CENTERLINE.

SEE GENERAL

NOTE 2

FIBERGLASS PIT WALL

PENETRATIONS

A3

MS501

18" CLR

30"

SLOPE

"D" "C"

A3

FIBERGLASS PIT WALL PENETRATIONS

SCALE: NOT TO SCALE

C 3 X 5 CHANNEL

PIPE SUPPORT

WITH U-BOLT

SLOPE

M

I N

M

I N

NOTES:

1. NOT USED.

2. REFER TO S-530 FOR STRUCTURAL DETAILS.

"A" FUEL PIPE

DIAMETER

"B" SLEEVE PIPE

DIAMTER

"C" SLEEVE LENGTH

EXTERIOR

"D" SLEEVE LENGTH

INTERIOR

2" 4"

16" (MIN)

4"

6" 10" 16" (MIN) 4"

FUEL PIT DETAILS

SHEET 1 OF 2

(PAVED)

1 2

REFER TO S-527

FOR HYDRANT PIT

REINFORCEMENT PLAN

1 2

6" F-24

PIPE SUPPORT.

" DIA U-BOLT W/

TEFLON PAD BETWEEN CHANNEL

SUPPORT AND PIPE AND

BETWEEN U-BOLT AND PIPE.

SECTION A

SEE GENERAL

NOTE 2

10" 16" 16" (MIN) 4"

NOVEMBER 2016

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DATE

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REV.

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DESCRIPTION

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INIT

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REVISIONS

AutoCAD SHX Text 10/13/17

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B-3 FINAL SUBMITTAL

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AutoCAD SHX Text 02/07/18

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AMENDMENT 0003

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BC

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BC