Case File
efta-02391775DOJ Data Set 11OtherEFTA02391775
Date
Unknown
Source
DOJ Data Set 11
Reference
efta-02391775
Pages
1
Persons
0
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From:
Lvjet
Sent:
Friday, January 16, 2015 12:06 AM
To:
jeevacation@gmail.com
Subject:
flap update
Jeffrey,
Gulfstream te=h's just went to hotel,. we worked as much as we could =ntil dark.
so far, The Avionics Tech informs t=e electrical system is doing what its suppose to, we =ave proven the flap selector
valve is passing fluid as it =hould, so flap selector valve is not the problem,.
=div> precautionary, We ordered a PDU, Power Distribution =nit,. located in Main wheel well, this is hydraulic power
m=tor that drives flap and Stabilizer. tomorrow the plan is t= disconnect each flap drive unit, and manually turn to chec=
freedom of travel,. two per flap,. these flap actuators =ave a Blow back mechanism which prevents flaps from retractin=
in flight in case of hydraulic failure or drive brake,. =/div> then we will disconnect the stab drive unit and=20check for
freedom of movement.
at this point =ech support is thinking PDU unit internal failure, ours is=20original 1988,. But very low failure item.
gutt =s tells me one of flap dive actuators is binding, or B=ow back mechanism is engaging, we will determine this
tomorro=,. makes sense since we can extend,.
better update tomorrow
</=iv>
thx.
Larry
1
EFTA_R1_01418150
EFTA02391775
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