TM 1-1520-238-23
2-487
2.133.
NO. 1 ENGINE NACELLE REMOVAL/INSTALLATION – continued
aa. Seal rod (90). Use sealing compound (item 174,
App F) and brush (item 34, App F).
ab. Install No. 1 engine louvers (para 4.59).
ac. Install No. 1 engine crossfeed/shutoff valve
(para 10.99).
ad. Install stabilator airspeed transducer (para
9.148).
ae. Install engine anti-ice relay panel (para 12.57).
af. Install ice detector processor (para 12.59).
ag. Install bleed air shutoff valve (para 7.139).
ah. Install ENCU (para 13.3).
ai. Install ENCU overboard exhaust duct (para
13.13).
aj. Install aircraft air pressure fluid manifold (para
7.138).
ak. Install ECS shutoff valve (para 13.15).
al. Install ENCU aft air tube (para 7.155).
am. Install left nacelle radiation shields (para 4.96).
an. Install No. 1 engine (para 4.48).
ao. Install No. 1 engine power available spindle
aft cable (para 4.171).
ap. Install No. 1 engine load demand spindle aft
cable (para 4.177).
aq. Install work platform door (para 2.137).
ar. Install engine nacelle fairing (para 2.135).
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0.50 IN
0.50 IN
APPLY
SEALANT
90
M04-4109-46
