Attachment 5 - Air Force Technical Order (TO) for Fire Extinguishers .pdf

PDF 2 MB Posted

Attached to
HALON Fire Extinguisher Testing for Moody AFB Federal contract opportunity
Solicitation number
FA4830-21-Q-0010
Issued by
Department of the Air Force Air Combat Command

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Other files for this federal contract opportunity

Other files attached to HALON Fire Extinguisher Testing for Moody AFB, newest first.
File Type Posted
Attachment 1 - Combo-Synopsis.pdf PDF
Attachment 2 - Clauses Incorporated By Reference.pdf PDF
Attachment 3 - Performance Work Statement.pdf PDF
Attachment 4 - Time Compliance Technical Order (TCTO).pdf PDF

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From: SHORT, JOSEPH G GS-11 USAF AFLCMC/WNUS

To: f10rp.todo@robins.af.mil lawrence.leblanc@beale.af.mil keun.lee@osan.af.mil

F10T5.TODO@ROBINS.AF.MIL

manuel.rios@osan.af.mil gregory.young@lajes.af.mil F10U6.TODO@robins.af.mil

19MXG.QA@US.AF.MIL

482mxg.f11lt.todo@us.af.mil 725AMS.QA@us.af.mil

8MXG.TODO@KUNSAN.AF.MIL

john.ward@randolph.af.mil dale.cook@edwards.af.mil 496abs.todo@moron.af.mil wanda.storrs@offutt.af.mil 919mxg.mxq.f120ltodo@eglin.af.mil

122MXG.TODO@ANG.AF.MIL

F123J.TODO@ANG.AF.MIL

john.hearn.1@us.af.mil silverflag.todo@tyndall.af.mil 128.arw.todo@ang.af.mil michael.annicelli@ang.af.mil

101ARW.TODO@ANG.AF.MIL

153mxg.mxqif128ftodo@ang.af.mil joshua.anderson@ang.af.mil devan.abram@ang.af.mil 133mxg.todo@ang.af.mil brian.gilbert@ang.af.mil vera.sweat@ang.af.mil 628CES.CED@us.af.mil garrett.cowsert@ang.af.mil joel.womack@barksdale.af.mil 440mxg.mxq.f12hw.todo@us.af.mil anthony.fernandez@ang.af.mil steven.lawter@mildenhall.af.mil 309as.todof13oz@chievres.usafe.af.mil 6mxg.mxqa@us.af.mil david.loomis@whiteman.af.mil

66.ABG.CE.TODO@HANSCOM.AF.MIL

173fw.mxq@ang.af.mil favies.hill@hurlburt.af.mil 507mxg.mxq.f13ud@tinker.af.mil carla.bernard@malmstrom.af.mil charles.tehan@luke.af.mil rommel.fronda@yokota.af.mil jay.wingfield@andersen.af.mil john.courgis@mcguire.af.mil trent.thompson@sheppard.af.mil lyndsey.cooper@laughlin.af.mil amanda.wease@eielson.af.mil 436CES.CEF@us.af.mil charles.peel@dobbins.af.mil 45ces.todo@us.af.mil russell.rowley@youngstown.af.mil robert.cook@hickam.af.mil robert.ganley@us.af.mil michael.newbury@tyndall.af.mil darryl.robinson-02@mcconnell.af.mil shawn.smith@ang.af.mil 7MXG.TODOF12HY@dyess.af.mil megan.thiel@westover.af.mil jo.peppey@eglin.af.mil timothy.stehley@minot.af.mil 171.ARW.F16LN.TODO@ang.af.mil victor.dejesus.4@us.af.mil kelly.tucker@ang.af.mil john.neagos@ang.af.mil laura.stahl@ang.af.mil marco.baiera@osan.af.mil micrtc.f17iytodo@ang.af.mil timothy.edwards.2@ang.af.mil F17ZB.TODO@hill.af.mil dyncorp.smtlf1814todo@trab.afcent.af.mil danna.jones.ctr@auab.afcent.af.mil william.ponder.ctr@afcent.af.mil F182J.TODO@ang.af.mil stacy.kellow@azphoe.ang.af.mil

72OSS.OSMA.ATCALS@TINKER.AF.MIL

71ftw.todo@us.af.mil 185arw.todo@ang.af.mil folcontract@acc.af.mil felipe.vazquez@hickam.af.mil

CHRISTINA.ZUNIGA@ANG.AF.MIL

rebecca.starmer@ang.af.mil cindy.patrick.ctr@us.af.mil scott.brende@sdsiou.ang.af.mil nttr.rsstodo@nellis.af.mil 611ASG.cce@us.af.mil hale.kisacik@incirlik.af.mil susan.melcher@ang.af.mil leland.mckenney@ang.af.mil paul.barsalou@ang.af.mil 126lrs.msgtodo@ang.af.mil ellen.brocki@ang.af.mil david.ordway@mildenhall.af.mil james.hutchison@ang.af.mil Satop.Interims@tinker.af.mil OCALC.ENGLC.Work@tinker.af.mil Candy.watson@us.af.mil kenneth.goree.1@us.af.mil Mark.McCay@kaiseraircraft.com 452mxg.mxq.todo@us.af.mil 97mx.mxqt.f10r3todo@altus.af.mil

437MXG.QA.TODOORG@US.AF.MIL

rudolf.gustafson.ctr@us.af.mil 134arw.todo@ang.af.mil jacob.anderson@elmendorf.af.mil 420scms.gulaab.todo@tinker.af.mil 314mxg.todo@us.af.mil aaron.joyce@scott.af.mil

F118H.TODO@LUKE.AF.MIL

60mxgtodo@us.af.mil richard.miller.47@us.af.mil 55.AMXSMXASF11MZ.2DO@offutt.af.mil F11NY.TODO@us.af.mil henry.diogo@langley.af.mil amc.a4mmp.f-11petodo@us.af.mil 27SOW.F11PR.TODO@Cannon.af.mil 62mxg.todo@us.af.mil 47FTW.F11SF.TODO@us.af.mil michael.latter@westover.af.mil aaron.chasse@ang.af.mil 721amxs.mxq.todo@ramstein.af.mil 355mxgtodof121t@dm.af.mil 58MXG.TODO@kirtland.af.mil 140wg.topm@ang.af.mil 15mxg.todov3@hickam.af.mil george.w.white@uscg.mil 33mxg.mxqa.f1246todo@eglin.af.mil f.124todo@holloman.af.mil 115fw.mxgtodo@ang.af.mil f126m.todo@ang.af.mil 172mxg.f126s.todo@ang.af.mil 147mxg.mxqf126utodo@ang.af.mil 189aw.mxgtodo@ang.af.mil F1271.TODO@ang.af.mil gerald.stohlman@ang.af.mil 161ARW.MXQF127TODO@ang.af.mil mxqt.f127mtodo@ang.af.mil 121arw.mxgf127xtodo@ang.af.mil 125mxg.mxqf1281todo@ang.af.mil f1286.todo@ang.af.mil f1287.todo@ang.af.mil julie.zajec@carswell.af.mil F128D.TODO@ang.af.mil 124mxgmxq.todo.1@ang.af.mil halidie.oneal@ang.af.mil 154WGMXG.TODO@us.af.mil 157.arw.mxq@ang.af.mil f1298.todo@ang.af.mil

F1299.TODO@ANG.AF.MIL

143mxg.qa.todo@anf.af.mil 100mxsTODO@mildenhall.af.mil charles.carter@ang.af.mil 177fw.todof129I@ang.af.mil tammy.langlois@ang.af.mil 144fw.mxg.todo@ang.af.mil maria.pranke@elmendorf.af.mil patrick.hawkins@ang.af.mil carmen.rodriguez@ang.af.mil f12aq.todo.119wg@ang.af.mil

1SOMOS.TODO@HURLBURT.AF.MIL

86mxg.qatodo@ramstein.af.mil steven.gardner.1@us.af.mil kymberly.mckenzie@ang.af.mil 728ams.mxqaf12e2todo@incirlik.af.mil 726ams.mxqf12emtodo@spangdahlem.af.mil

352SOG.TODO@MILDENHALL.AF.MIL

43AMXS.TODO@us.af.mil

434MXG.F*12FP.TODO@US.AF.MIL

sean.quinby@seymourjohnson.af.mil 509mxg.todo@us.af.mil vincent.thompson@us.af.mil F12GZ.TODO@wpafb.af.mil afmca4mf12h5todo@wpafb.af.mil 735ams.todo@hickam.af.mil 917FG.F12HM.TODO@us.af.mil 914mxg.mxq@us.af.mil wendy.santos@whiteman.af.mil 459TODO@afncr.afmil 95RS.TODO@mildenhall.af.mil 552MXG.TODO@Tinker.af.mil charles.younker1.ctr@afncr.af.mil

301MXG.QA@US.AF.MIL

f12k8.todo@tyndall.af.mil 92amxs.mxq@us.af.mil 53weg.todo@tyndall.af.mil 433LG.LGQ@us.af.mil 353sog.todo@kadena.af.mil 35ces.firedept@us.af.mil

730ams.todo@us.af.mil F13SH.todo@ellsworth.af.mil 5mxgtodo@minot.af.mil

CC: Satop.Interims@tinker.af.mil; OCALC.ENGLC.Work@tinker.af.mil;

Candy.watson@us.af.mil

Subject: THIS IS INTERIM OPERATIONS SUPPLMENT (IOS) 13F4-4-121S-3, DATED 26

NOVEMBER 2013

Signed By: joseph.short.2@robins.af.mil

Importance: High

//UNCLASSIFIED//

1. THIS PUBLICATION SUPPLEMENTS T.O. 13F4-4-121, DATED 10 JANUARY 1991

THROUGH CHANGE 11, TITLE: OPNL, SERV & MAINT INSTR W/IPB FOR FIRE EXTINGUISHER,

WHEELED LIQUIFIED GAS, 150 LB. CAPACITY-- PN 03496 AND 05673--NSN 4210-01-140-2233

AND 4210-01-332-0793. A SUITABLE REFERANCE TO THIS SUPPLEMENT WILL BE MADE ON

THE TITLE PAGE OF THE BASIC PUBLICATION. COMMANDERS ARE RESPONSIBLE FOR

BRINGING THIS SUPPLEMENT TO THE ATTENTION OF ALL AFFECTED AIR FORCE PERSONNEL.

MAJCOMs, FOAs, AND DRUs ARE RESPONSIBLE FOR FORWARDING THIS IOS TO

SUBORDINATE UNITS NOT INCLUDED AS ADDRESSED ON THIS MESSAGE.

2. DISTRIBUTION STATEMENT A: APPROVED FOR PUBLIC RELEASE: DISTRIBUTION IS

UNLIMITED. PUBLIC AFFAIRS CASE NUMBER 05-07138. SUBMIT RECOMMENDED CHANGES

OR PROBLEMS WITH THIS TECHNICAL ORDER TO 406 SCMS/GUEE, ROBINS AFB, GA 31098.

QUESTIONS CONCERNING TECHNICAL CONTENT SHALL BE REFERRED TO AFLCMC/WNUS.

3. PURPOSE: THIS SUPPLEMENT IS ISSUED TO AMEND BASIC MANUAL WITH UPDATE

INSTRUCTIONS.

4. ON TITLE PAGE, CHANGE NOMENCLATURE, MODEL NUMBER, PART NUMBER AND

NSN BLOCK TO READ AS FOLLOWS: FIRE EXTINGUISHER, WHEELED LIQUIFIED GAS, 150 LB.

CAPACITY, MODEL 600, PART NO. 07351, 03496 AND 05673/NSN 4210-01-457-9062/NSN

4210-01-140-2233/NSN 4210-01-332-0793.

5. ON PAGE ii, LIST OF ILLUSTRATIONS, DELETE PART NUMBER 03496 AT THE END OF

TITLE OF FIGURES 1-1, 4-1 AND 7-1.

6. ON PAGE 1-1, PARAGRAPH 1-2, CHANGE TO READ AS FOLLOWS: THE PURPOSE OF THIS

MANUAL IS TO PROVIDE OPERATION AND MAINTENANCE PERSONNEL WITH THE INFORMATION

NECESSARY TO OPERATE, SERVICE, MAINTAIN, AND REPAIR THE 150 POUND WHEELED, LIQUIFIED GAS FIRE EXTINGUISHERS, MODEL 600, PART NUMBER 07351, 03496 AND 05673. THE MODEL 600 FIRE EXTINGUISHER (SEE FIGURE 1-1) IS PRODUCED BY AMEREX CORPORATION, PO BOX 81, TRUSSVILLE AL.

35173 (FSCM 54905).

7. ON PAGE 1-1, FIGURE 1-1, FIGURE TITLE, DELETE PART NUMBER 03496.

8. ON PAGE 4-3, FIGURE 4-1, FIGURE TITLE, DELETE PART NUMBER 03496.

9. ON PAGE 7-1, PARAGRAPH 7-1, a, CHANGE TO READ AS FOLLOWS: EQUIPMENT COVERED. THIS ILLUSTRATED PARTS BREAKDOWN COVERS THE 150 LB. CAPACITY LIQUIFIED GAS HALON 1211 WHEELED FIRE EXTINGUISHER, MODEL 600, PART NO. 07351, 03496 AND 05673, MANUFACTURED BY AMEREX

CORPORATION AND ITS COMPONENT PARTS. THE NATIONAL STOCK NUMBERS FOR THE AMEREX

EXTINGUISHER IS NSN 4210-01-457-9062, 4210-01-140-2233 AND 4210-01-332-0793.

10. ON PAGE 7-3, FIGURE 7-1, FIGURE TITLE, DELETE, 03496, AMEREX.

11. ON PAGE 7-4, FIGURE 7-1, ADD NEW PART NUMBER ON FIRST LINE AS FOLLOWS:

PART NUMBER; 07351, FSCM; 54905, DESCIPTION; FIRE EXTINGUISHER, WHEELED LIQUIFIED

GAS, 150 LB CAPACITY, MODEL 600, LIME YELLOW (REPLACES PART NUMBERS 03496,

05673), UNITS PER ASSY; 1, USABLE ON CODE; A, SMR CODE; PAOBZ.

12. ON PAGE 7-4, FIGURE 7-1, PART NUMBER 03496, CHANGE DESCRIPTION TO: FIRE

EXTINGUISHER, WHEELED LIQUIFIED GAS, 150 LB CAPACITY, MODEL 600, LIME YELLOW

(NON-PROCURABLE, REPLACED BY PART NUMBER 07351) AND CHANGE SMR CODE TO:

PAOBZ.

13 ON PAGE 7-4, FIGURE 7-1, PART NUMBER 05673, CHANGE DESCRIPTION TO: FIRE

EXTINGUISHER, WHEELED LIQUIFIED GAS, 150 LB CAPACITY, MODEL 600, FOREST GREEN

(NON-PROCURABLE, REPLACED BY PART NUMBER 07351) AND CHANGE SMR CODE TO:

PAOBZ.

13. THE TECHNICAL CONTENT MANAGER FOR THIS SUPPLEMENT IS: JOSEPH SHORT,

AFLCMC/WNUS, DSN 472-7442, COMM (478) 222-7442, EMAIL:

JOSEPH.SHORT.2@US.AF.MIL. THE TO MANAGER FOR THE SUPPLEMENT IS CANDY WATSON,

406 SCMS/GUEE, DSN 468-3896, COMM (478) 926-3896, EMAIL:

CANDY.WATSON@US.AF.MIL.

END OF SUPPLEMENT

mailto:JOSEPH.SHORT.2@US.AF.MIL

From: SHORT, JOSEPH G GS-11 USAF AFLCMC/WNUS

To: lawrence.leblanc@beale.af.mil; keun.lee@osan.af.mil; F10T5.TODO@ROBINS.AF.MIL;

manuel.rios@osan.af.mil; gregory.young@lajes.af.mil; F10U6.TODO@robins.af.mil;

19MXG.QA@US.AF.MIL; corey.runge@homestead.af.mil; 725AMS.QA@us.af.mil;

8MXG.TODO@KUNSAN.AF.MIL ; john.ward@randolph.af.mil;

dale.cook@edwards.af.mil; wanda.storrs@offutt.af.mil ;

919mxg.mxq.f120ltodo@eglin.af.mil; 122MXG.TODO@ANG.AF.MIL;

F123J.TODO@ANG.AF.MIL; john.hearn.1@us.af.mil; silverflag.todo@tyndall.af.mil;

128.arw.todo@ang.af.mil; michael.annicelli@ang.af.mil; 101ARW.TODO@ANG.AF.MIL;

153mxg.mxqif128ftodo@ang.af.mil; joshua.anderson@ang.af.mil;

devan.abram@ang.af.mil; corey.hoerdt@ang.af.mil; brian.gilbert@ang.af.mil;

vera.sweat@ang.af.mil; 628CES.CED@us.af.mil; garrett.cowsert@ang.af.mil;

sean.quinby@seymourjohnson.af.mil; vincent.thompson@us.af.mil;

joel.womack@barksdale.af.mil; brenda.miller.2@us.af.mil;

anthony.fernandez@ang.af.mil; charles.younker1.ctr@andrews.af.mil;

steven.lawter@mildenhall.af.mil; 309as.todof13oz@chievres.usafe.af.mil;

bryan.dufour@us.af.mil; david.loomis@whiteman.af.mil;

cathy.levangie@hanscom.af.mil; 173fw.mxq@ang.af.mil; favies.hill@hurlburt.af.mil;

507mxg.mxq.f13ud@tinker.af.mil; carla.bernard@malmstrom.af.mil ;

charles.tehan@luke.af.mil; rommel.fronda@yokota.af.mil;

jay.wingfield@andersen.af.mil; john.courgis@mcguire.af.mil;

trent.thompson@sheppard.af.mil; lyndsey.cooper@laughlin.af.mil;

amanda.wease@eielson.af.mil; christopher.young@dover.af.mil;

charles.peel@dobbins.af.mil ; leonard.johnson@patrick.af.mil;

russell.rowley@youngstown.af.mil; robert.cook@hickam.af.mil;

robert.ganley@us.af.mil; ronnie.price@tyndall.af.mil; darryl.robinson- 02@mcconnell.af.mil; shawn.smith@ang.af.mil; 7MXG.TODOF12HY@dyess.af.mil;

megan.thiel@westover.af.mil; jo.peppey@eglin.af.mil; timothy.stehley@minot.af.mil;

jaime.albertson@papitt.ang.af.mil; victor.dejesus.4@us.af.mil; kelly.tucker@ang.af.mil;

john.neagos@ang.af.mil; laura.stahl@ang.af.mil; marco.baiera@osan.af.mil;

micrtc.f*17iytodo@ang.af.mil; timothy.edwards.2@ang.af.mil; F17ZB.TODO@hill.af.mil;

danna.jones.ctr@auab.afcent.af.mil; F182J.TODO@ang.af.mil;

stacy.kellow@azphoe.ang.af.mil; 72OSS.OSMA.ATCALS@TINKER.AF.MIL;

71ftw.todo@us.af.mil ; 185arw.todo@ang.af.mil; folcontract@acc.af.mil;

felipe.vazquez@hickam.af.mil; CHRISTINA.MILLER@ANG.AF.MIL;

rebecca.starmer@ang.af.mil; cindy.patrick.ctr@elmendorf.af.mil ;steven.efaw@dyess.af.mil; scott.brende@sdsiou.ang.af.mil;

glenn.parrent.ctr@nellis.af.mil; hale.kisacik@incirlik.af.mil; susan.melcher@ang.af.mil;

leland.mckenney@ang.af.mil; ; penny.smedley@ang.af.mil; ellen.brocki@ang.af.mil;

david.ordway@mildenhall.af.mil; james.hutchison@ang.af.mil;

Mark.McCay@kaiseraircraft.com; 452mxg.mxq.todo@us.af.mil;

97mx.mxqt.f10r3todo@altus.af.mil; 437MXG.QA.TODOORG@US.AF.MIL;

134arw.todo@ang.af.mil; jacob.anderson@elmendorf.af.mil;

420scms.gulaab.todo@tinker.af.mil; 314mxg.todo@us.af.mil; aaron.joyce@scott.af.mil;

F118H.TODO@LUKE.AF.MIL; 60mxgtodo@us.af.mil; richard.miller.47@us.af.mil;

55.AMXSMXASF11MZ.2DO@offutt.af.mil; rebecca.mitchell@patrick.af.mil;

henry.diogo@langley.af.mil; eulunda.dewalt@scott.af.mil;

27SOW.F11PR.TODO@Cannon.af.mil; marilyn.eubank@us.af.mil;

47FTW.F11SF.TODO@us.af.mil ; manuel.millan@moron.af.mil;

michael.latter@westover.af.mil; aaron.chasse@ang.af.mil ;

721amxs.mxq.todo@ramstein.af.mil; 355mxgtodof121t@dm.af.mil;

58MXG.TODO@kirtland.af.mil; sarah.mccann@ang.af.mil;

15mxg.todov3@hickam.af.mil; george.w.white@uscg.mil;

33mxg.mxqa.f1246todo@eglin.af.mil; adam.richter@holloman.af.mil;

115fw.mxgtodo@ang.af.mil; f126m.todo@ang.af.mil; joseph.bowman@ang.af.mil;

147mxg.mxqf126utodo@ang.af.mil; 189aw.mxgtodo@ang.af.mil;

F1271.TODO@ang.af.mil; gerald.stohlman@ang.af.mil;

161arw.mxqf127todo@ang.af.mil; jennifer.campbell@ang.af.mil;

dayne.pritchard@ang.af.mil; f1286.todo@ang.af.mil; f1287.todo@ang.af.mil;

julie.zajec@carswell.af.mil; F128D.TODO@ang.af.mil; robert.haun@ang.af.mil;

halidie.oneal@ang.af.mil; alohilani.andres@hickam.af.mil; 157.arw.mxq@ang.af.mil;

f1298.todo@ang.af.mil; F1299.TODO@ANG.AF.MIL; georgina.whitfield@ang.af.mil;

100mxsTODO@mildenhall.af.mil; charles.carter@ang.af.mil;

177fw.todof129I@ang.af.mil; tammy.langlois@ang.af.mil; 144fw.mxg.todo@ang.af.mil;

maria.pranke@elmendorf.af.mil; patrick.hawkins@ang.af.mil;

carmen.rodriguez@ang.af.mil; f12aq.todo.119wg@ang.af.mil;

1SOMOS.TODO@HURLBURT.AF.MIL; 86mxg.qatodo@ramstein.af.mil;

steven.gardner.1@us.af.mil; kymberly.mckenzie@ang.af.mil;

728ams.mxqaf12e2todo@incirlik.af.mil; 726ams.mxqf12emtodo@spangdahlem.af.mil;

352SOG.TODO@MILDENHALL.AF.MIL; brent.dewitt@us.af.mil;

carol.duncan@grissom.af.mil; 509mxg.todo@whiteman.af.mil;

F12GZ.TODO@wpafb.af.mil; afmca4mf12h5todo@wpafb.af.mil;

735ams.todo@hickam.af.mil; lloyd.webb.2@us.af.mil; 914mxg.mxq@us.af.mil;

wendy.santos@whiteman.af.mil; 459TODO@afncr.afmil;

raymond.shanks@mildenhall.af.mil; 552MXG.TODO@Tinker.af.mil;

debra.cook.2@us.af.mil; f12k8.todo@tyndall.af.mil; nicholas.ehman@us.af.mil;

53weg.todo@tyndall.af.mil; 433LG.LGQ@us.af.mil; 353sog.todo@kadena.af.mil;

35ces.eod@misawa.af.mil; 730ams.todo@us.af.mil; F13SH.todo@ellsworth.af.mil;

laurie.murphy.1@us.af.mil; 5mxgtodo@minot.af.mil; yvonda.lefebvre@peterson.af.mil;

9mxg.todo@beale.af.mil; denis.shchetina@lakenheath.af.mil ;

9120f1401todo@barksdale.af.mil; 317AGQA.TODO@dyess.af.mil;

scott.thull@hurlburt.af.mil; f144y.todo@hill.af.mil; 22mxg.todo.1@us.af.mil;

916MXG.TODO@seymourjohnson.af.mil; 362trs.rfb.todo@sheppard.af.mil;

rodney.gunter.2.ctr@us.af.mil; glenn.dennison@us.af.mil;

AFRL.RXQ.F148R.TODO@tyndall.af.mil; 436mxg.todo.org@us.af.mil;

randy.putnam@columbus.af.mil; cornelius.wooten@ang.af.mil;

126arw.mxgtodo@ang.af.mil; 87lrs.lgrftodo@us.af.mil; 1fw.todos@langley.af.mil;

shawn.murphy@langley.af.mil; 14ces.cef@columbus.af.mil;

MSG.CEFCCE@maxwell.af.mil; andrew.wells@keesler.af.mil;

55MXG/MXQPTODO@offutt.af.mil; F16NX.TODO@NELLIS.AF.MIL;

christopher.clunk@wpafb.af.mil; 379emxgtodo@auab.afcent.af.mil;

F17HI.TODO@robins.af.mil; LORI.WILLIS@MAAB.AFCENT.AF.MIL;

380emxs.todo@adab.afcent.af.mil; Brendan.Courtney@ang.af.mil;

eric.rauch@westover.af.mil; 733ams.qa@kadena.af.mil; 563RQGOL- A.QA.TODO@nellis.af.mil; benjamin.salmon@andersen.af.mil;

lyndsy.pumala@ang.af.mil; daniel.partl@ilpeor.ang.af.mil;

164mxg.mxqf1846todo@ang.af.mil; melissa.martin@ang.af.mil;

jason.strickland@oktuls.ang.af.mil; afnorth.a4.omb@tyndall.af.mil;

F188C.todo@arnold.af.mil; f188u.todo@us.af.mil ; nttr.techlib@nellis.af.mil;

23mxg.todo@moody.af.mil; 8F8.TODO@tyndall.af.mil; 23.mxg.todo@moody.af.mil;

2MXG/MXQI.F18GD.TODO@barksdale.af.mil; jordan.lyndell@altus.af.mil;

MELISSA.HUSTON@ANG.AF.MIL; Butch.McCarty@bgab.afcent.af.mil;

kristin.martin@ang.af.mil ;f18pe.todo@patrick.af.mil ;

lawrence.tatro@mostjo.ang.af.mil ;f18vk.todo@edwards.af.mil ; thule.todo@us.af.mil;

timothy.stevens@mibatt.ang.af.mil; randolph.raymond.ctr@eglin.af.mil ;daniel.orzel@luke.af.mil; 57mxgcsctodo@nellis.af.mil ;373TRSDET17.F196P.TO@cannon.af.mil ; 451emxg.todo@kdab.afcent.af.mil ;F19BX.TODO@robins.af.mil ; william.midwood@ang.af.mil;

mary.lee@elmendorf.af.mil; esmeralda.martinez@cafres.ang.af.mil;

jason.martin.1@hickam.af.mil; 386emxg.qatodo@asab.afcent.af.mil;

monica.ciccarone@tyndall.af.mil; afgsca4mxf19hmtodo@barksdale.af.mil;

paul.barsalou@ang.af.mil; 18mxg.todooffice@kadena.af.mil; john.miele@moody.af.mil;

Ryan.Higgins.ctr@wpafb.af.mil ;jeremy.gerrish.1@us.af.mil ; F187X.TODO@hill.af.mil;

bryan.webber@us.af.mil; 120FW.mxg.todo@ang.af.mil;

727SOAMXS.F19KG.TODO@CANNON.AF.MIL;

Cc: Satop.Interims@tinker.af.mil ; candy.watson@us.af.mil

Subject: THIS IS AN INTERIM OPERATION SUPPLEMENT (IOS) TO 13F4-4-121S-2, DATED 21

OCTOBER 2013.

Signed By: joseph.short.2@us.af.mil

Importance: High

//UNCLASSIFIED//

1. THIS PUBLICATION SUPPLEMENTS T.O. 13F4-4-121, DATED 10 JANUARY 1991

THRU CHANGE 11, DATED 9 AUGUST 2013 AND SUPERCEDES IOS 13F4-4-121S-1, DATED 10

OCTOBER 2013 , TITLE: OPNL, SERV & MAINT INSTR W/IPB FOR FIRE EXTINQUISHER,

WHEELED LIQUIFIED GAS, 150 LB. CAPACITY-- PN 03496 AND 05673--NSN 4210-01-140-2233

AND 4210-01-332-0793. A SUITABLE REFERANCE TO THIS SUPPLEMENT WILL BE MADE ON

THE TITLE PAGE OF THE BASIC PUBLICATION. COMMANDERS ARE RESPONSIBLE FOR

BRINGING THIS SUPPLEMENT TO THE ATTENTION OF ALL AFFECTED AIR FORCE PERSONNEL.

MAJCOMs, FOAs, AND DRUs ARE RESPONSIBLE FOR FORWARDING THIS IOS TO

SUBORDINATE UNITS NOT INCLUDED AS ADDRESSED ON THIS MESSAGE.

2. DISTRIBUTION STATEMENT A: APPROVED FOR PUBLIC RELEASE: DISTRIBUTION IS

UNLIMITED. PUBLIC AFFAIRS CASE NUMBER 05-07138. SUBMIT RECOMMENDED CHANGES

OR PROBLEMS WITH THIS TECHNICAL ORDER TO 406 SCMS/GUEE, ROBINS AFB, GA 31098.

QUESTIONS CONCERNING TECHNICAL CONTENT SHALL BE REFERRED TO AFLCMC/WNUS.

3. PURPOSE: THIS SUPPLEMENT IS ISSUED TO AMEND BASIC MANUAL WITH UPDATE

INSTRUCTIONS AND SUPERCEDES IOS 13F4-4-121S-1, DATED 10 OCTOBER 2013.

4. ON PAGE 5-1, PARAGRAPH 5-2, ADD THE FOLLOWING TO THE END OF THE EXISTING

PARAGRAPH: IF MAINTENANCE IS TO BE PERFORMED BY CONTRACT, THE CONTRACTOR

MUST PERFORM ALL MAINTENANCE AND INSPECTIONS USING THIS TECHNICAL MANUAL (TO

13F4-4-121). THE OWNING UNIT MUST ENSURE THAT THE CONTRACTOR IS PROVIDED A

CURRENT COPY OF THIS MANUAL OR ENSURE THAT THEY ARE ON DISTRIBUTION IAW

TO 00-5-1.

5. ON PAGE 5-1, PARAGRAPH 5-6, ADD THE FOLLOWING PARAGRAPH: WHEN THE DATE

OF THE CYLINDER REACHES 12 YEARS, THE OWNING UNIT MUST MAKE AN ECONOMICAL

DECISION TO HAVE THE CYLINDER AND DISCHARGE HOSE HYDROSTATICALLY PROOF

PRESSURE TESTED IN CONJUNCTION WITH A 6 YEAR COMPLETE MAINTENANCE OR DISPOSE

OF THE FIRE EXTINGUISHER IAW PARA 6-3.

6. ON PAGE 5-1, PARAGRAPH 5-6.1, ADD THE FOLLOWING NEW PARAGRAPH WITH

STEPS AFTER PARA 5-6: CONSIDERATIONS FOR AN ECONOMICAL DECISION SHOULD

INCLUDE THE FOLLOWING COST FACTORS:

a. 6 YEAR COMPLETE MAINTENANCE/INSPECTION.

b. ALL SCHEDULED REPLACEMENT PARTS AND OBVIOUS UNSCHEDULED

UNSERVICEABLE PARTS.

c. HYDROSTATIC PROOF PRESSURE TEST OF THE CYLINDER AND DISCHARGE HOSE

(SEE PARAGRAPH 5-29).

d. SHIPPING AND HANDLING.

e. IF THE FIRE EXTINGUISHER NEEDS REFURBISHMENT (SEE PARAGRAPH 5-31).

7. ON PAGE 5-1, PARAGRAPH 5-6-2, ADD THE FOLLOWING NEW PARAGRAPH AFTER

NEW PARA 5-6.1: HYDROSTATICALLY PROOF TESTING MUST BE COMPLETED IN

ACCORDANCE WITH NFPA (NATIONAL FIRE PROTECTION ASSOCIATION) STANDARD 10 AND

CGA (COMPRESSED GAS ASSOCIATION) PAMPHLET C-6. REFER TO PARAGRAPH 5-29 FOR

ADDITIONAL INFORMATION AND COMPLETE DETAILS ON HYDROSTATIC PROOF TESTING.

THE FOLLOWING WEB SITE IS PROVIDED IN AIDING USERS IN LOCATING AUTHORIZED

CYLINDER TEST FACILITIES: HTTP://WWW.PHMSA.DOT.GOV/HAZMAT/REGS/SP-

A/APPROVALS/CYLINDERS (SEE AUTHORIZED DOT CYLINDER REQUALIFIERS).

8. ON PAGE 5-1, PARAGRAPH 5-6.2, ADD NOTE AFTER NEW PARA 5-6.2: NOTE;

SHIPPING PRESSURIZED FIRE BOTTLES AFTER THEY HAVE EXCEEDED THE 12-YEAR POINT

(WITHOUT A HYDROSTATIC TEST) IS AGAINST DEPARTMENT OF TRANSPORTATION

REGULATIONS. PLAN ACCORDINGLY.

9. ON PAGE 5-3, PARAGRAPH 5-11, STEP a., CHANGE LAST SENTENCE TO READ AS FOLLOWS: IF DAMAGE IS FOUND AND DOUBT EXISTS TO THE INTEGRITY OF THE CYLINDER, IT

MUST BE HYDROSTATICALLY PROOF PRESSURE TESTED (IF ECONOMICAL) OR DISPOSED OF

IAW PARAGRAPH 6-3. REFER TO PARAGRAPH 5-29 IF HYDROSTATIC PROOF PRESSURE

TESTING IS NEEDED.

http://www.phmsa.dot.gov/hazmat/regs/sp-a/approvals/cylinders http://www.phmsa.dot.gov/hazmat/regs/sp-a/approvals/cylinders

10. ON PAGE 5-3, PARAGRAPH 5-11, STEP c., CHANGE TO READ AS FOLLOWS: CHECK THE

DATE OF MANUFACTURE PRINTED ON THE EXTINGUISHER LABEL (NAMEPLATE) OR ON THE

AGENT CYLINDER DOME/CYLINDER CARRIAGE FLANGE. THE CYLINDER MUST BE

HYDROSTATICALLY PROOF PRESSURE TESTED EVERY 12 YEARS OR DISPOSED OF IAW

PARAGRAPH 6-3. ALSO, THE DISCHARGE HOSE MUST HAVE A HYDROSTATIC PROOF

PRESSURE TEST EVERY 12 YEARS (CONCURRENTLY WITH THE CYLINDER’S HYDROSTATIC

PROOF PRESSURE TEST).

11. ON PAGE 5-4, PARAGRAPH 5-13, CHANGE TO READ AS FOLLOWS: EVERY SIX YEARS

THE EXTINGUISHER SHALL BE EMPTIED AND SUBJECTED TO COMPLETE MAINTENANCE

PROCEDURES. ONCE THE COMPLETE MAINTENANCE PROCEDURES HAVE BEEN

PERFORMED, THE NEXT 6 YEAR COMPLETE MAINTENANCE REQUIREMENT SHALL BEGIN

FROM THAT DATE.

12. ON PAGE 5-5, PARAGRAPH 5-14, STEP e., CHANGE NOTE AFTER STEP E. TO READ AS

FOLLOWS: IF ANY MOISTURE IS EVIDENT OR A HYDROSTAT TESTING HAS BEEN

ACCOMPLISHED, PURGE WITH HOT AIR AND OVEN DRY THE CYLINDER AT 130°F TO 160°F

UNTIL THOROUGHLY DRY. ALWAYS INSPECT CYLINDER INTERIOR FOR MOISTURE

IMMEDIATELY BEFORE ASSEMBLY OF THE EXTINGUISHER.

13. ON PAGE 5-12, PARAGRAPH 5-19, STEP b. (1), CHANGE NOTE AFTER SUBSTEP (1) TO

READ AS FOLLOWS: IF ANY MOISTURE IS EVIDENT OR A HYDROSTAT HAS BEEN

ACCOMPLISHED, PURGE WITH HOT AIR AND OVEN DRY THE CYLINDER AT 130°F TO 160°F

UNTIL THOROUGHLY DRY. ALWAYS INSPECT CYLINDER INTERIOR FOR MOISTURE

IMMEDIATELY BEFORE ASSEMBLY OF THE EXTINGUISHER.

14. ON PAGE 5-18, PARAGRAPH 5-28, FIRST CAUTION, CHANGE TO READ AS FOLLOWS: CAUTION

HALON 1211 IS A CORROSIVE CHEMICAL WHEN MIXED WITH EVEN THE SLIGHTEST AMOUNT OF

MOISTURE. AFTER MAINTENANCE OR HYDROSTAT TESTING, ENSURE THAT CYLINDERS ARE

THOROUGHLY DRIED BEFORE RECHARGING. FAILURE TO PURGE ALL MOISTURE FROM CYLINDER MAY

CAUSE THE CYLINDER TO CORRODE AND AS A RESULT COULD CAUSE STRUCTURAL FAILURE OF

CYLINDER.

15. ON PAGE 5-21, PARAGRAPH 5-29, ADD THE FOLLOWING PARAGARPH TITLE: 12 YEAR

HYDROSTATIC PROOF PRESSURE TEST OF CYLINDER AND HOSE/COMPLETE MAINTENANCE

(OPTIONAL).

16. ON PAGE 5-21, PARAGRAPH 5-29, ADD STEP a. AS FOLLOWS: a. THE 12 YEAR

HYDROSTATIC PROOF PRESSURE TEST OF THE CYLINDER AND DISCHARGE HOSE IS

ACCOMPLISHED IN CONJUNCTION WITH PERFORMING 6 YEAR COMPLETE MAINTENANCE.

FOR COMPLETE MAINTENANCE PROCEDURES, REFER TO PARAGRAPHS 5-12 THROUGH 5-28.

IF IT IS NOT ECONOMICAL TO PERFORM THIS TASK DISPOSE OF FIRE EXTINGUISHER IAW

PARAGRAPH 6-3.

17. ON PAGE 5-21, PARAGRAPH 5-29, ADD STEP b. AND SUBSTEPS AS FOLLOWS:

b. ONCE THE FIRE EXTINGUISHER HAS BEEN FULLY DISASSEMBLED, PERFORM

HYDROSTATIC TESTING AS FOLLOWS:

(1). PERFORM HYDROSTATIC PROOF PRESSURE TEST ON CYLINDER AT 480

PSI (3310 KPA). PERMANENT VOLUMETRIC EXPANSION OF THE CONTAINER

MUST NOT EXCEED 10% OF THE TOTAL EXPANSION. REJECT CONTAINERS

EXCEEDING 10% PERM. EXPANSION.

(2). TESTING TO BE PERFORMED BY AN APPROVED AGENCY IN ACCORDANCE

WITH CGA PAMPHLET C-1 "WATER JACKET VOLUMETRIC EXPANSION

METHOD" OR "DIRECT EXPANSION METHOD" OR OTHER SUITABLE METHOD.

CGA PAMPHLETS MAY BE ORDERED FROM: COMPRESSED GAS

ASSOCIATION, INC.500 FIFTH AVE.NEW YORK NY 10036

(3) THE HOSE ASSEMBLY MUST BE HYDROSTATICALLY PROOF PRESSURE

TESTED AT THE SAME AS THE CYLINDER INTERVAL TO 300 PSI (2068 KPA) OR

REPLACED .

18. ON PAGE 5-21, PARAGRAPH 5-29, ADD, CAUTION AFTER PARA 5-29, STEP b. (3) TO

READ AS FOLLOWS: CAUTION; HALON 1211 IS A CORROSIVE CHEMICAL WHEN MIXED WITH

EVEN THE SLIGHTEST AMOUNT OF MOISTURE. AFTER MAINTENANCE OR HYDROSTAT

TESTING, ENSURE THAT CYLINDERS ARE THOROUGHLY DRIED BEFORE RECHARGING. FAILURE

TO PURGE ALL MOISTURE FROM CYLINDER MAY CAUSE THE CYLINDER TO CORRODE AND AS

A RESULT COULD CAUSE STRUCTURAL FAILURE OF CYLINDER.

19. ON PAGE 5-21, PARAGRAPH 5-29, ADD SUBSTEP (4): AFTER HYDROSTATIC PROOF

PRESSURE TESTING, HOT AIR PURGE CYLINDER AND OVEN DRY CYLINDER AT 130 TO 160°F

UNTIL CYLINDER INTERIOR IS THOROUGHLY DRY. ALWAYS INSPECT CYLINDER INTERIOR FOR

MOISTURE IMMEDIATELY BEFORE INSTALLING VALVE AND GAUGE ASSEMBLIES.

20. ON PAGE 5-29, FIGURE 5-6, ADD ILLUSTRATION FOR HYDROSTAT ADAPTER ALONG

WITH NOTE: AND FIGURE TITLE AS FOLLOWS:

FIGURE 1. HYDROTEST ADAPTER AMEREX CORP. PART NUMBER 05152

21. THE TECHNICAL CONTENT MANAGER FOR THIS SUPPLEMENT IS: JOSEPH SHORT,

AFLCMC/WNUS, DSN 472-7442, COMM (478) 222-7442, EMAIL:

JOSEPH.SHORT.2@US.AF.MIL. THE TO MANAGER FOR THE SUPPLEMENT IS CANDY WATSON, 406

SCMS/GUEE, DSN 468-3896, COMM (478) 926-3896, EMAIL: CANDY.WATSON@US.AF.MIL.

END OF SUPPLEMENT

mailto:JOSEPH.SHORT.2@US.AF.MIL

TO 13F4-4-121

TECHNICAL MANUAL

OPERATION, SERVICE AND MAINTENANCE

WITH

ILLUSTRATED PARTS BREAKDOWN

FIRE EXTINGUISHER, WHEELED

LIQUIFIED GAS, 150 LB. CAPACITY

PART NO. 03496 AND 05673

NSN 4210-01-140-2233

NSN 4210-01-332-0793

AMEREX CORPORATION

(FSCM 54905)

F09603-82-C-2199

DISTRIBUTION STATEMENT A - Approved for public release; distribution is unlimited. PA Case Number 05-07138. Submit recommended changes or problems with this Technical Order to 406 SCMS/GUEE, Robins AFB, GA 31098. Questions concerning technical content shall be referred to

AFLCMC/WNZED.

Published Under Authority of the Secretary of the Air Force

10 JANUARY 1991 CHANGE 11 - 22 JULY 2013

CURRENT

SUPPLEMENTS

13F4-4-121S-3 13F4-4-121S-2

Basic and all changes and supplements have been merged to make this a complete publication.

1386378769E Text Box See SUPP S-3

NOTE: The portion of the text affected by the changes is indicated by a vertical line in the outer margins of the page. Changes to illustrations are indicated by shaded or screened areas, or by miniature pointing hands.

INSERT LATEST CHANGED PAGES. DESTROY SUPERSEDED PAGES.

LIST OF EFFECTIVE PAGES

*Zero in this column indicates an original page.

USAF

Page *Change No. No.

Page *Change No. No.

Page *Change No. No.

Dates of issue for original and changed pages are:

Title A i ii iii iv Blank 1-1 - 1-3 1-4 Blank 2-1 - 2-2 3-1 3-2 4-1 - 4-2 4-3 - 4-4 5-1 5-2 5-3 - 5-4 5-5 5-6 5-7 5-8 - 5-11 5-12 5-13 5-14 - 5-15 5-16 - 5-17 5-18 5-19 - 5-21 5-22 - 5-28 5-29 5-30 5-31 Added 5-32 Blank 6-1 6-2 Blank 7-1 7-2 7-3 7-4 7-5

7-6 7-7 7-8 7-9 7-10 - 7-13 7-14 Blank 8-1 - 8-2

Original. . . . . . . . . .0 . . . . . 10 January 1991 Change . . . . . . . . . .1 . . . . . . 1 January 1992 Change . . . . . . . . . .2 . . . . .15 October 1992 Change . . . . . . . . . .3 . . . . . . 15 March 2002 Change . . . . . . . . . .4 . . . 5 September 2002 Change . . . . . . . . . .5 . . . . . . . 10 April 2005

Change . . . . . . . . . . 6 . . . . . . . 15 May 2007 Change . . . . . . . . . . 7 . . . . . . . 19 June 2007 Change . . . . . . . . . . 8 . . . . .25 October 2010 Change . . . . . . . . . . 9 . . . . . . . 21 May 2012 Change . . . . . . . . . . 10 . . .8 September 2012 Change . . . . . . . . . . 11 . . . . . . . 22 July 2013

A Change 11

TOTAL NUMBER OF PAGES IN THIS PUBLICATION IS 68, CONSISTING OF THE FOLLOWING:

TABLE OF CONTENTS

Section Paragraph Page

I INTRODUCTION. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-1 1-1 INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-1 1-5 DESCRIPTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-2 1-7 HOSE WITH SUPPORT. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-2 1-9 AGENT STORAGE CYLINDER ASSEMBLY. . . . . . . . . . . . . . . . . . . . . . . . . . 1-2 1-11 CARRIAGE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-2 1-13 LEADING PARTICULARS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-3

II PREPARATION FOR USE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-1 2-1 UNPACKING AND HANDLING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-1 2-2 New Unit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-1 2-3 New Unit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-1 2-4 Used Unit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-1 2-5 PREPARATION FOR OPERATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-1

III THEORY OF OPERATION. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-1 3-1 EXTINGUISHING AGENT. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-1 3-7 EQUIPMENT OPERATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-2

IV OPERATING INSTRUCTIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-1 4-1 CONTROLS AND INSTRUMENTS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-1 4-2 Pressure Gauge . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-1 4-3 Discharge Valve and Lever . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-1 4-4 Nozzle Valve and Lever . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-1 4-5 Nozzle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-1 4-6 Agent Level Gauge . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-1 4-7 Pressure Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-1 4-8 OPERATION. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-1 4-9 Pre-Operation Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-1 4-10 Operation Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-1 4-11 SHUTDOWN . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-2 4-13 POST FIRE OPERATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-2

V INSPECTION, MAINTENANCE, RECHARGING, AND TESTING . . . . . . . . . . . . . . . . . . . 5-1 5-1 GENERAL. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-1 5-7 INSPECTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-1 5-9 SERVICE MAINTENANCE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-3 5-12 COMPLETE MAINTENANCE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-4 5-15 CORRECTIVE MAINTENANCE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-5 5-17 NOZZLE VALVE ASSEMBLY PART NUMBER 05011 . . . . . . . . . . . . . . . . . 5-6 5-18 DISCHARGE VALVE ASSEMBLY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-8 5-19 CYLINDER ASSEMBLY. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12 5-20 AGENT LEVEL GAUGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-13 5-21 HOSE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-15

5-22 HOSE SUPPORT BRACKET AND NOZZLE MOUNT ASSEMBLY . . . . . . . 5-16

5-23 WHEEL AND TIRE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-16 Change 11 i

TABLE OF CONTENTS - Continued

Section Paragraph Page 5-24 CARRIAGE ASSEMBLY. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-17 5-26 RECHARGE INSTRUCTIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-17 5-27 RECHARGING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-17

5-29 DELETED

5-30 TROUBLE SHOOTING GUIDE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-21 5-31 CORROSION PREVENTION AND PAINTING. . . . . . . . . . . . . . . . . . . . . . . . . 5-31

VI PREPARATION FOR SHIPMENT AND STORAGE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-1 6-1 SHIPMENT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-1 6-3 STORAGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-1 6-3 DISPOSAL. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-1

VII ILLUSTRATED PARTS BREAKDOWN . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7-1 7-1 INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7-1

7-2 FEDERAL SUPPLY CODE FOR MANUFACTURERS (FSCM) . . . . . . . . . . . 7-2

VIII NUMERICAL INDEX . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8-1

LIST OF ILLUSTRATIONS

Number Title Page

1-1 150 lb. Wheeled, Liquified Gas, Fire Extinguisher, Part Number 03496 . . . . . . . . . . . . . . . . . . 1-1 2-1 Pressure-Temperature Chart . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-2 4-1 150 lb. Wheeled, Liquified Gas, Fire Extinguisher, Part Number 03496 . . . . . . . . . . . . . . . . . . 4-3 5-1 Discharge Hose Coiling Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-24 5-2 Agent Level Gauge Body and Plastic Indicator Face Part Number 06780 . . . . . . . . . . . . . . . . . 5-25 5-3 Agent Level Gauge Alignment Part Number 06780 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-25 5-4 Fire Extinguisher Recharge System. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-26 5-5 Recharge Adapter Assemblies. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-28 5-6 Deleted 5-7 Reflective Material Location and Specifications. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-30 7-1 150 lb. Wheeled, Liquified Gas, Fire Extinguisher, 03496, Amerex . . . . . . . . . . . . . . . . . . . . . 7-3 7-2 Nozzle Valve Assembly, 05011, Amerex . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7-6 7-3 Discharge Valve, 05006, Amerex . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7-8 7-4 Nozzle Valve Assembly, 05295 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7-10 7-5 Pull Pin and Lanyard Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7-12 ii Change 10

1386378769E

LIST OF TABLES

Number Title Page

1-1 Leading Particulars . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-3 3-1 Halon 1211 Physical Properties . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-1 5-1 Allowable Leakage Rate . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-20 iii/(iv blank)

SECTION I

INTRODUCTION

1-1 INTRODUCTION.

1-2 The purpose of this manual is to provide operation and maintenance personnel with the information necessary to operate, service, maintain, and repair the 150 pound wheeled, liquified gas fire extinguishers, part number 03496 and 06425.

Part number 03496, see Figure 1-1, was produced under Contract Number F09603-84-C-1819. These units were manufac-tured by Amerex Corporation, PO Box 81, Trussville AL 35173 (FSCM 54905).

Figure 1-1. 150 lb. Wheeled, Liquified Gas, Fire Extinguisher, Part Number 03496 1-1

1386378769E Text Box See SUPP S-3

1386378769E

1-3 Section I, in this manual, contains a brief description of the fire extinguisher and lists the leading particulars. Section II provides instructions necessary to prepare the fire extinguisher for use. Section III describes the fire extinguishing agent and how the equipment operates. Section IV covers unit operation. Section V provides maintenance instructions for the fire extinguisher and includes preventive maintenance, service maintenance, corrective maintenance and repair. Section VI includes information on unit shipment and storage. Section VII contains the illustrated parts breakdown and illustrations of the fire extinguisher with key index numbers to aid in locating and identifying the detail parts. Section VIII contains an alpha-numerical listing of all part numbers.

1-4 The 150 pound wheeled, liquified gas fire extinguisher is a portable fire extinguisher capable of being towed at speeds up to 15 mph over a level, paved surface. The wheeled fire extinguisher is used to provide large scale, fire protection where mobility is needed to reach local, separated, multiple fire hazard areas and combat flammable liquid, electrical or carbon-aceous fires. The unit is charged with 150 pounds of Bromochlorodifluoromethane, Halon 1211 (BCF) fire protection agent and pressurized with nitrogen (N2) to 200 ± 20 psig to facilitate agent discharge.

1-5 DESCRIPTION.

1-6 Basically, the 150 pound, wheeled, liquified gas, fire extinguisher consists of a hose with support, agent storage cylinder assembly and carriage for transportation.

1-7 HOSE WITH SUPPORT.

1-8 The hose, which provides mobility to the operator when fighting a fire, has a nozzle valve assembly at its end to permit flow control. The hose support is used to mount the hose and nozzle. The extinguisher hose is looped around the hose support and the nozzle valve assembly is held by the nozzle mount and clips. Some extinguishers may have an upgraded hose rack/ nozzle mount which utilizes a retaining ring and no longer uses the hose clips.

1-9 AGENT STORAGE CYLINDER ASSEMBLY.

1-10 The agent storage cylinder assembly is equipped with the cylinder discharge valve with safety outlet, pressure valve, and agent level gauge. The cylinder assembly is steel fabricated, conforms to the Department of Transportation 4BW240 Specification, and has an internal volume of 4,350 cubic inches, nominal. The cylinder assembly is used to store the extinguishing agent under pressure. The cylinder assembly mounts between the carriage and hose support assemblies.

1-11 CARRIAGE.

1-12 The carriage is a welded steel tube assembly with two (2) either pneumatic or semi-pneumatic tires and wheels mounted on a steel axle. The carriage is equipped with a three (3) inch I.D. lunette for towing. The axle is welded to the carriage and positions the wheels off the ground when the unit is in a vertical position. The carriage assembly provides mobility and is used to mount the cylinder assembly with hose support.

1-2

1-13 LEADING PARTICULARS.

1-14 Leading particulars for the 150 pound, wheeled, liquified gas, fire extinguisher are contained in Table 1-1.

Table 1-1. LEADING PARTICULARS

Fire Extinguisher Agent Halon 1211

(Bromochlorodifluoromethane) In accordance with Specification MIL-B-38741

Pressurant Gas Nitrogen (N2)

Operating Temperature -40°F (18°C) to -135°F (57°C) Safety Outlet Discharge

400 to 500 psig at 70°F (20.1°C)

Approx Discharge Time 44 Seconds Range-Agent Throw 35 to 50 ft Weight:

Agent 150 lbs normal Vehicle Charged 325 lbs ± 15 lbs

Dimensions:

Height 59 inches Width 29 inches Depth 36 inches

Cylinder Assembly:

Design DOT 4BW240 Internal Volume 4,350 cubic inches nominal

Pressure:

Service 200 ± 20 psig Test 480 psig Burst 960 psig minimum

Wheel:

Type Pneumatic, light duty. Some units have been delivered with semi-pneumatic wheels.

Tire Size 16 inches X 4.00 inches

Hose:

Type Rubber Size 3/4 in. I.D.

Length 50 ft 1-3/(1-4 blank)

SECTION II

PREPARATION FOR USE

2-1 UNPACKING AND HANDLING.

2-2 New Unit. The new 150 pound, wheeled, liquified gas, fire extinguisher will be received at the operation site as a completely assembled, uncharged and unpressurized unit. A tag will be attached which says: "CAUTION This extinguisher is not charged. Follow charging instructions in service manual before putting to use. Remove tag only after extinguisher is properly charged." Special unpacking procedures are not required. When handling the fire extinguisher, observe the normal precautions used when handling equipment to be pressurized and avoid damage that might occur when dropping it.

2-3 New Unit. Cylinder & valve assemblies from the factory have been internally dried and contain dry nitrogen at 5 psig or slightly above. The discharge valve should remain closed until the extinguisher is charged.

2-4 Used Unit. The fire extinguisher will be received at the maintenance site as a completely assembled empty or partially filled, pressurized unit. The unit may or may not be packaged. Unpacking and handling procedures are the same as for a new unit, as applicable.

2-5 PREPARATION FOR OPERATION.

2-6 The fire extinguisher is designed to withstand environmental exposure; therefore, the unit should be stored in a convenient, readily detected location. New units need to be charged with Halon 1211 and nitrogen before they are ready to use. Refer to Service Maintenance paragraph 5-9.

2-7 To ensure used units are ready for operation, visually inspect the pressure gauge and agent level gauge. The pressure gauge should be in the green zone, 200 ± 20 psig range and the pointer in the agent level gauge should indicate agent level at the full mark, 150 pounds.

2-8 Temperature of extinguisher can affect pressure gauge reading and agent level gauge reading. Nominal "properly charged" marking on both gauges is correct for 70°F (21°C). Generally as temperature goes up the two gauge readings go up and conversely low temperature results in low gauge readings.

2-9 The relative pressure gauge vs temperature reading for the Amerex 150 pound Halon wheeled extinguisher is as follows:

2-10 It is best to inspect gauge readings when unit temperature is near 70°F. Tables 2-9, 2-12 are of use in estimating unit pressure and agent fill conditions at other temperatures.

Temperature °F: -40 32 70°F 120 135 Pressure Gauge psig: 127 168 200 263 288 Temperature °C: 140 0 21°C 49 57 2-1

2-11 The Pressure-Temperature Chart is attached to the cylinder top. The minimum psig and maximum gauge read-ings are found directly to the left of where a vertical line from the selected temperature cuts through the two curves.

The gauge reading will be between the minimum and maxi-mum points on a properly charged unit.

Figure 2-1.

2-12 The cylinder contains Halon 1211 agent in mostly liquid form. Agent level gauge uses a float to sense liquid level and position gauge point. Height of liquid agent above the inside bottom of container is as follows:

The liquid level height changes +1.40 in. to -1.25 in. from the nominal 70°F position over the operating temperature range.

2-13 Temperatures of 90°F and above will cause the agent level indicator on a properly charged unit to read well up into the overcharged area. If confirmation of a proper amount of Halon 1211 charge is required, weigh the unit and compare with the gross weight shown on the extinguisher label.

2-14 Temperatures below 40°F will cause the agent level indicator to show below the FULL mark. Units in cold environ-ments may be check weighted or brought inside for warm up to determine a satisfactory agent fill weight.

2-15 Weighing the unit on a scale is the most accurate method to determine if an extinguisher is properly charged.

Temperature -40°F 70°F 122°F 135°F Agent Height 15.22 in. 16.47 in. 17.79 in. 17.86 in.

Temperature -40°C 21°C 50°C 57°C 2-2

SECTION III

THEORY OF OPERATION

3-1 EXTINGUISHING AGENT.

3-2 The extinguishing agent Halon 1211 (BCF) is a halogenated hydrocarbon chemically identified as bromochlorodifluo-romethane. Its chemical symbol is CBrC1F2. Halon 1211 is a colorless, faintly sweet-smelling, electrically nonconductive gas, at ambient conditions having an approximate boiling point of 25°F (-3.4°C) and a freezing point of -256°F (-160°C).

Halon 1211 is a liquified gas under its own vapor pressure in a closed container at ambient temperatures.

3-3 Halon 1211 is a clean, multipurpose fire fighting agent. Effective for Class ABC fires, Halon 1211 extinguishes by chemically interrupting the fire chain reaction, the continuing combination of oxygen, fuel and heat. Halon 1211 does not extinguish by depleting the oxygen supply. Discharged as an 85% liquid/15% vapor stream, Halon 1211 offers long discharge range, which helps the operator to stay at a safe distance while fighting a fire. The liquid/vapor discharge allows Halon 1211 to flow around obstructions when extinguishing tough-to-reach fires.

3-4 Halon 1211 has a low level of toxicity. It has been approved for use in portable fire extinguishers by Underwriters Laboratories in Standard No. 1093 and in local applications by NFPA in Standard No. 12B (1990 edition) and NFPA403 (2003 edition). The Federal Aviation Administration Advisory Circular 20-42B also recommends the use of Halon 1211 portables on commercial aircraft.

Although Halon 1211 vapor has a low toxicity, its decomposition products can be hazardous. On decompo-sition, Halon 1211 has a characteristic sharp, acrid odor, even in concentrations of only a few parts per million. The odor characteristic provides a built-in warning system for the agent and at the same time creates a noxious irritating atmosphere for those who are in the hazard area during and following a fire.

Leave and/or ventilate the area after fighting the fire.

3-5 Physical characteristics of Halon 1211 are indicated in Table 3-1.

TABLE 3-1. HALON 1211 PHYSICAL PROPERTIES

Formula CBrC1F2

Boiling Point 25°F (-3.4°C)

Freezing Point -256°F (-160°C)

Liquid Density 114 lb/ft3 (1830 kg/m3) at 68°F (20°C)

Vapor Pressure 19.6 psig at 68°F (20°C)

Specification MIL-B-38741 Change 6 3-1

3-7 EQUIPMENT OPERATION.

3-8 In a charged extinguisher ready for operation, the extinguishing agent is stored under pressure in the cylinder assembly and retained in the cylinder by the cylinder discharge valve. Operating the cylinder discharge valve lever opens the discharge valve allowing pressurized extinguishing agent to flow from the cylinder via the cylinder syphon tube through the discharge valve to the extinguisher hose and nozzle valve assembly.

3-9 With the nozzle valve closed, the extinguisher nozzle with hose attached can be carried by hand to the fire hazard.

With pressurized extinguishing agent up to the nozzle, opening the nozzle valve will permit agent flow through the nozzle to the fire. Pictographic operating instructions on the extinguisher illustrate how to put it into operation.

3-10 The fire extinguisher includes a pressure gauge and safety outlet. The pressure gauge indicates the cylinder internal pressure. In the eventuality that a high cylinder pressure buildup should occur, the safety outlet is designed to relieve at 400 to 500 psig.

3-2

SECTION IV

OPERATING INSTRUCTIONS

4-1 CONTROLS AND INSTRUMENTS.

4-2 Pressure Gauge. The fire extinguisher, see figure 4-1, includes a pressure gauge. The pressure gauge is used to monitor the cylinder pressure.

4-3 Discharge Valve and Lever. The discharge valve, which includes pressure gauge and safety outlet, is used to retain the agent contents in the cylinder, see figure 4-1. The Discharge Valve includes a hand operated lever that operates the Discharge Valve to allow or stop agent flow from the cylinder to the hose and nozzle valve assembly. The safety outlet relieves pressure at 400 to 500 psig.

4-4 Nozzle Valve and Lever. The nozzle valve is located at the free hose end and is used to retain the agent in the hose, see figure 4-1. The nozzle valve includes a hand operated lever that operates the nozzle valve to allow or stop the discharge of agent through the extinguisher nozzle.

4-5 Nozzle. The nozzle is located on the outlet side of the nozzle valve, see figure 4-1.

4-6 Agent Level Gauge. The agent level gauge provides a visual display of the level of liquified Halon 1211 in the cylinder.

4-7 Pressure Valve. The pressure valve is located on the discharge valve, see figure 4-1. The valve is used during cylinder assembly service recharge.

4-8 OPERATION.

4-9 Pre-Operation Procedure. Transport the fire extinguisher to the fire hazard area and locate the extinguisher within the scope of the 50 foot long hose. At the fire hazard site, position fire extinguisher in vertical position with wheels off ground.

NOTE

The extinguisher may be operated in either the vertical or reclined position. However, the unit in the reclined position will discharge less agent.

4-10 Operation Procedure. Perform unit operation, see figure 4-1, as follows:

Make certain the discharge nozzle is closed (down position) and the extinguisher is upright before begin-ning the following steps.

1. Pull on pin to remove and open tank discharge valve by rotating (pulling) valve lever at top of tank toward the hose 90°. The hose is now pressurized.

2. Pull the nozzle with lever in the CLOSED position from the hose storage mount and extend the hose toward the fire.

Change 6 4-1

3. NOTE: Stand at least 30 feet away from fire before opening the nozzle valve.

Grasp nozzle firmly and aim nozzle at base of fire.

Be prepared for backward reaction (movement) of the nozzle as discharge begins.

4. Hold hose and nozzle firmly to allow for discharge recoil. Open nozzle by pulling handle toward you.

The concentrated agent and the by-products resulting from application to a fire are toxic when inhaled.

After use, leave the area and ventilate well before returning. Symptoms of over-exposure to pure Halon 1211 are: dizziness, impaired coordination, and reduced mental acuity.

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