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
View the file
Other files for this federal contract opportunity
| File | Type | Posted |
|---|---|---|
| Attachment 1 - Combo-Synopsis.pdf | ||
| Attachment 2 - Clauses Incorporated By Reference.pdf | ||
| Attachment 3 - Performance Work Statement.pdf | ||
| Attachment 4 - Time Compliance Technical Order (TCTO).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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