DLA MIL-F-25173 A-1956 FASTENER CONTROL PANEL AIRCRAFT EQUIPMENT《航空器装置控制面板扣件》.pdf
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1、MIL-F-25173LW3G)16 FEBRUARY 1956=F-25173(USAF)1h K y 1955IKCLITASX SFECIPICAWFAsmYEi, COSTSOL PAfAKL,M- mThis specMicatlon has bam awro by tie ntof the Air Force and by tbe UaVJ Bureau of A8r0mutlCa.1. SamM w.9 SP9CifmIti0n COW- Om tsm Of CCQI-1 P-Q f-2. MFLICABLS KJORfP2t on date Of intiwtiO f bfi,
2、 f s X Of fi SWCiCa tiOn tO tie tent “j1,., ,)ISpmified herein:.sPBXFICATIONSFederal(x)-A-33.8w-A-325QQ-U-151 “QQ-P-li16ly Plate ad Sheet#Aaninum PJloY 6=, %=5, SodS, SbIWS dwire, 2t011B or Dram!4etals; Omeial Swcificatio* for Intictiori ofPI.At Pr.=sermtion, Packagiwr, packing mdMarking ofA use of(
3、coPim of specifications,stamk=-ds, drawings, ad whlations =q*d by cOn-tractors in comection with specificpromuwm nt functions should be obtained from theprocuring activity or as directed by the contracttig OfflcEr.)3. R.FLWIZMINls3.1 Qualification.- The f astmars furnled under this specificationehel
4、l be aproduct whi.,has been tested and has passed the Qualification teats .w8cif led herein.3.2 Materials.-.3.2.1 Selection of materials.- In using mtarials, pruhcts, snd tm.mites notSCifiCal?J ibimt=d hereh, applicable SW4ficatiom and standards shall be selectedin accordalm with ANA Bulletin No. lh
5、3.3.2.1.1 Met.a16.- Het-slashall be of the corrosion-resistanttype or suitablytreated to resi=mceion. h fuels, salt mrv, Or atispher cOnditiO tO *ich tiefastenersray be subjectedwhen in storage : i. during normal service use.3.2.1.2 Dissimilarmetals.- lbde suitab4 protected against electrolyticcmro-
6、sion, disstiilarmetals shall not be usei in intimate contact vith each other. OratingAND10398 defties dissMMr rnetah.).- Fastener studs shall be bardemd to prevent damage toscrew(a) DDW510S A SSALL SE SUCH TSAT *TALLATIOM OF 27-ISCM BE MADE ISTO IHE?IODSTISOFIUWL310USAS SFllXFXED.(b) DII!EWILWSAWLY
7、AFTSR ITALLATIOM.SILTFASTSTiESSTDDDlnENs4EN ymm2Cm7S . 05Ki3SoIHEfbfHE SFEZIFIKO, lWSSANCJLStASOLES il”,. .FIOUPX 2. Stud flstener, aircxaft equipn?mtcontrol panelItProvided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-I H?.L-F-25173A(M)I3 .IJ cOMtructim.-
8、) 3.1$.1 Fastener stud head.- with the fastener stud unlocked, the toP surface ofthe htmd shall rzti titbti e outline dimensions as shown kn figure 2.3.11.2 screwdriverslot.- The screwdriver slot in tJIefastener stud head sbsXiconform to the d.i.mnsionsshown in figure 2. with .thafastener In the tie
9、d Positiun,the acreudriverslot Eha.11be in line uitb the wire of the receptacle strip.3JJ.3 stud munting and rem- NOmt Of we fas- ud *- haccordanceUiti fi be possible to renvve a damaged fastener studUImUMY and sui=%IIII-I a naOne, thout g tie -. by *e w Of S-hand tm3S nhich rhall be designed by the
10、 fmtener manufacturer.3.5 Performance.-3.5.1 Lacking tOrqlm.-3.5.1.1 nnxim. locking tom m.- me mxlmia tirque required to lock the fastenershall.be 8 pmii-imhea .3.5.1.2 M.rAmtm locking tOrque.- ne torque re+red ta lock tie faatermrshallbe 2.5 Pmnd-tithes.3.5.1.3 Absolute maximum tom w.- The absolute
11、 -mm torquerequired to lockthe fatiener shall be 133 Wrcent of Che maximum locking torque with the additim of aO.010-inch shim between the panel and receptacle.3.5.1.11 Absolute mlnimnn torque.- lhe absolute mi.nl.mmtorque required to hcktAe fastener =all be b7 percent of fliemidm.m 10 32 stitaoffas
12、teners !undBs436M.ed)as sbwn in ff.gurs2, four apecimms as Bhmm in figure 3, fOUrSFUS “.ssh %= II,fo as *W in fiIOU= 5, wf two SPcfmms e asshoun in figures3, II, and 5, monnted an sheets having a total thickness of O.010 inchless than th.total nominal thicknessswctiied for each. Samples submitted fO
13、r qual.i-ficat.itmte.:.ing shall be accompaniedby two campletesets of detail !rMufEiCttingdrawings O each fastener item submittedfor test. Samples shallbe identifiedwith themanufacturesown t number and any additional informationrequired by the authorizingletter (se? 6.lJ).11.2.2 Tests.- The Qualific
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