• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-25 08:35来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

(b) Cleanbumperwasherwithchlorothane,orequivalentandattachto housingwithathinfilmof Locktite495adhesive,orequivalent.
NOTE: Specialtools,P/n7801-T1,7801-T2and7801-T3canbepurchasedfromC.E.F. Industries,423InterstateRoad,Addison,Illinois
(c) Inserttoolfixture77801-T1and7801-T2intowormshaftbearingbores.Insertpinthroughtool
withdepthgaugefrom milledsurfaceofhousingtooutsidediameter(O.D.)of pin, add1/2 diameter ofpinandrecord thisdimension(Zdimension).Removetoolfixtures.
fixturesandbearingbores(referto Figure501).Takemeasurement
newO-ringsin worm shaftboreof housing.Applya thin filmor20%AeroshellNo.7
(d)
Install

greaseand80%MobilJetII Oil lubricant,orequivalentto O-rings.

(e)
Insertwormshaftintohousing.

(f)
Insertbothballbearingsintohousing,makingsurebearingsareseated.


(g)Attachoneoutputflangeandsecurewithfourscrews.Onoppositesideattachoutputflange
withtwoscrews.Usinga dialindicator,checkendplayofwormshaftandaddshimasrequired toobtain0.004to 0.010inchendplay.Securewithfourscrews.
(h)
Inserttool7801-T3ontosplineofwormshaftandcheckthatshafttorquedoesnotexceed12 inches.

(i)
Insertfrontbearingassemblyintofronthousingassembly.


NOTE:Shoulderofbearingis to bepressedintobumperwasher.
EFFECTIVITY:
PAGE
040-999  27-50-00 7

27-50-00 Jan 10/90
PIPERAIRCRAFT

PA-42-720(Advanced Trainer)
MAINTENANCEMANUAL
A. Flaps(continued)
11.Assemblyof FlapTransmission(continued)
(j) Takemeasurementfrommilledsurfaceofhousingto innerraceYdimension.SubtractZ
dimensiontakeninfirstmeasurement (referto Figure501).
fromYdimension

(k) Measurewidthofwormgearface.TakehalethethicknessandsubtractthisfromA dimension
obtainedin secondmeasurement.Subtract0.001/0.002inchfromresults.Thisistheshim
thicknessrequired(referto Figure501).
(l) Placeshimovertopoffrontbearing.Placewormgearovershim,shoulderendup.
(m)Takemeasurement to shoulder
frommilledsurfaceof housing ofwormgearW dimension (referto Figure501). MeasurewidthofrearbearingKdimension.Subtractthetwomeasurements.
Subtract0.001/0.002fromresults.Thisistheshimrequired.
NOTE:Donotinstalltheshimatthistime.
(n)Applyapproximately1/8oz.of lubricationconsistingof 20% AeroshellNo.7greaseand80%
MobilJetIIOil,orequivalentmixture,to worm shaftandwormgear. Rotatewormshaftwhile
applying.

(o) Installball screwandtube assemblythroughbearingandwormgearin front housingand line up keyways.
NOTE: Keepwormgearandwormshaftinmeshwhileinserting.
(p)
Insertkey in keyway.

(q)
Placeshim,previouslydeterminedontop of wormgear.

(r)
Placerearbearing,flangesideup, in housing.

(s)
Place lockwasher over ballscrew. Threadlocknut(chamferedsidedown)ontoscrew.


CAUTION: MAKESUREBALLNUTANDTUBEASSEMBLYIS POSITIONEDAWAYFROM HOUSINGBEFORETIGHTENINGLOCKNUT.
(t) Tightenlocknutto a torque of80 in. lbs.minimumtoalignlockwashertangwithslotin nut.
Bendtangintoslot.
CAUTION: MAKESURETHATNOCHIPSARE FORMEDDURINGTIGHTENINGOF NUT.
(u)
Aftertighteningnut,measuredistancefrommilledsurfaceofhousingtoouterraceofrearbearing.Readingshouldbebetween0.001/0.004inch.

(v)
PlaceO-ringintoO-ringgrooveinhousing.Installrearhousingandattachwithbolts.Tightenboltstoatorqueof35-40in. lbs.


EFFECTIVITY:

PAGE8 27-50-00
040-999

Jan10/9027-50-00
PIPER AIRCRAFT
PA-42-720 (Advanced Trainer)
MAINTENANCE MANUAL

A. Flaps (continued)
Pin 0.328"O.D. 
PinDia. divide by 2 = 0.164" (0.328"ref) X +0.164" (Z)Firstreading First Measurement NOTE:Shouldread0.750"(ref) 
(A) Second reading 
Bearing  Front Bearing 

SecondMeasurement
Third Measurement
FlapTransmissionMeasurements
Figure501 (Sheet1 of 2)


EFFECTIVITY: 040-999 27-50-00 Jan 10/90
PIPERAIRCRAFT
PA-42-720(Advanced Trainer)
MAINTENANCEMANUAL

A. Flaps(continued)
FrontBearing
RearBearing

Measurerearbearing
"K"width,subtractfrom
dimension"W"

Subtract0.001/0.002" W for shim requirement -K ANS
WormGear
Fourth Measurement

Flap Transmission Measurements Figure501(Sheet2of2)
EFFECTIVITY:
040-999

Jan10/90
275000
PIPERAIRCRAFT
PA-42-720(AdvancedTrainer)

MAINTENANCEMANUAL

A. Flaps (continued)
12. Serviceand Inspectionof FlapTransmissionInternalComponents(CALCO)
CAUTION: ALL DEFECTIVEOR WORNPARTSMUSTBE REPLACEDWITHNEWPARTS. DONOT ATTEMPTTO REPAIRDEFECTIVEPARTS.
(a)
Washalldisassembledpartsin a suitabledry cleaningsolvent.

(b)
Thoroughlycleanoff oldsealantandadhesive.
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:夏延飞机维护手册 Cheyenne IIIA PA-42-720 AMM 1(119)