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ACM guard (Figure 2-133) and depressing the ACM
JE’IT pushbutton. For single stores loaded on a station,
stores will be jettisoned at lOO-millisecond intervals in
the following sequence:
LDG GEAR handle UP. This mode is activated by the
RIO selecting the station to be jettisoned via the jettison
STA SEL switch and then selecting AUX on the SEL
JE’IT switch. Auxiliary jettison of an A/G store loaded
directly on a BRU-32 is via gravity force only.
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1. Stations 2 and 7 simultaneously
2. Stations IB and 8B simuItaneou~ly
p&i-)
3. Station4
4. Station5
5. Station 3
Since auxiliaryjettison for single A/G stores
loaded directly on BRU-32s is a gravity drop
rathert han an ejection separation,t he aircraft
will he restricted in its flight envelope when
jettisoning through this mode.
6. Station 6. 2.41 MISCELLANEOUS EQUIPMENT
After the release attempt is completed, the SMS updates
the stores inventory. Unlike emergency jettison,
a store that is not released is declared HUNG. Such
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stores are not eligible for launch but are still eligible for
emergency or selective jettison. Additionally, A/G
stores loaded on BRU-32s will still be eligible for auxiliary
jettision.
2.40.3.3 Selective Jettison. Selective jettison is
used to separate single jettisonable stores station-bystationandalso
allows simultaneousjettisonofbothfuel
tanks. The RIO selects the desired station(s) for selective
jettison.
2.41.1 Boarding Ladder. A boarding ladder consisting
of three folding sections is housed in the left fuselage
between the two cockpits. It is held in the closed
position by two mechauicall ocking pins actuatedb y the
ladder control handle in the face of the boarding ladder
The ladderm ust be manually releasedo r stowedf rom the
groundl evel. Unfolding the remainingt wo sectionsp laces
the ladderi n a Rallye xtendedp osition.T he bottom rung of
the ladder is approximately26 inches above the deck when
in a fully extendedp osition, with the nosegearunkneel~
and 12i nchesa bovet he decki fthe nosegeairs kneeled.A
LAD/CANOPY caution light on the pilot caution advisory
panel advises the pilot that the boarding ladder is not in a
full up-and-lockedp osition.
Selective jettison is accomplished by placing the MA
ARM switch to ON, the LDG GEAR handle UP, the
JETTISON STA SEL knob set to the desired station,
and the SEL JJXI switch to JETT. After the release
attempt is completed, the SMS updates the stores inven-
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tory. Unlike emergency jettison, a store that is not released
is declared BUNG. Such stores are not eligible
for launch, but are still eligible for emergency or selective
jettison. A/G stores loaded on BRU-32s will still be
eligible for auxiliary jettison.
2.41.1.1 Boarding Steps and Handhold. There
are two positive locking board steps, one on either side
of the boarding ladder directly below each cockpit. They
may be opened or closed from either cockpit or while
standing on the boarding ladder. A single handhold is
directly above the hoarding ladder. It is a spring-loaded
door that fairs with the fuselage when released.
Do not attempt jettison of external fuel tanks
until wing fuel tanks are depleted. Wing
fuel may be lost if the external tank quickdisconnect
valve sticks in the open position.
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2.40.3.4 Auxiliary (AUX) Jettison. Auxiliary jetti-
SO* is a nonejection release mode for single A/G stores
loaded on BRU-32s. Lie selective jettison, this mode
requires the MA ARM switch to be set to ON and the
2.41.2 Nose Radome. The nose radome is attached
to the aimmfl by a top hinge and bottom mounted latches,
permitting it to be rotatedu p for accessa nd maintenance.
A jury strut attachedt o the lower part of the dome canb e
fastenedto the aimrafi bulkheadt o hold the dome open.A
minimum overheadc learanceo f 16 feeti s requimdw hen
opening the radome. The radar antem must be stowed
before opening the mdome. Antenna stow position is 0”
azimuth and 60“ tilted down.
Note
After the nose radome is raised and the jury
strut fastened in position, release hydraulic
pressure to take the load off the hydraulic
system.
ORIGINAL 2.268
NAVAIR Wl=f4AAD-1
2.41.3 Systems Test and System Power Ground
Panel. The SYS TEST and SYS PWR ground check
panel (Figure 2-135) is on the RIO right console panel
(accessible from the boarding ladder with the canopy
open) for controlling the activation of electrical circuits
using ground external power. The panel cover is designed
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F-14D 飞行手册 Flight Manual 1(188)
