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oversweep position when applicable. If the wings are
not in oversweep, ensure that the emergency WING
SWEEP handle position corresponds with the actual
wing position. Leave the emergency WING SWEEP
handle guard up, extend the emergency WING SWEEP
handle, and pull WING SWEEP DRIVE NO. 1 and WG
SW DR NO. ZMANUV FLAP circuit breakers (LDl,
LEl). Crossbleeds tartss hould not be performedu nless
the area aft of the aircraft is clear. Tiedowns should not
be removeda nd enginess houldn ot be startedunlesst he
auxiliary brake air pressure gauge indicates a full
charge.
8-1
8.2 START AND POSTSTART
Shipboard start andpoststartprocedu abbreviations
of the shore-basedc hecklists are as delineatedf or the
poststart-pilotp rocedures.C ertain stepsa re omitted because
aircraft are spotted too close together to allow the
wings to be swept forward while tied down. Cranking
the left engine prior to starting the right, as outlined in
the shore-basedp roceduresw ill ensure that auxiliary
brake pressure is available and will ensure that backup
flight control module is full of hydraulic fluid prior to
cycling.
8.2.1 Carrier Alignment. Carrier alignment of the
INS and SAHRS concurrently or of the INS alone can
be accomplished using SINS data or manually entered
ship’s position, speed, and heading. A stored heading
SINS alignment is also available.
8.2.1.1 Concurrent SINS Alignment. For either
data-link or deck-edge-cabletr ansmissiono f SINS data:
1. Ensure SAHRS AC/DC cb’s (lA3,lAS, lA6,913)
are pulled prior to application of electrical power.
2. DATA LINK power switch-ON.
3. DATA LINK MODE switch - CAINSWPT.
4. Verify parking brake is set.
Note
Application of SAHRS power prior to selecting
CV ALIGN will not allow SAHRS to
properly align.
5. NAV MODE switch - CV ALIGN.
6. Reset SAHRS cb’s.
7. Select OWN A/C MFD format by depressing
DATA pushbutton on MFD MENU1 display. The
CV SINS DATA format will appear.
ORIGINAL
NAVAIR Ol-Fl4AAD1
8. Verify that SHDG is not boxed. If it is, depressth e
SHDG pushbutton to unbox it.
9. Monitor the progress of alignment by observing
the QUAL and TIME acronyms and the align scale
on the MFD OWN A/C format. The SINS (ship)
latitude, longitude, and INS north and east velocities
can be evaluated on the MFD OWN A/C format.
An INS ALIGN COMPLETE message will
normally occur in 7 minutes. At this time the align
quality should be below 1 nm per hour.
8.2.1.2 Concurrent SINS Stored Heading Carrier
Alignment. Perform a reference alignment by
following the SINS carrier align procedurein paragraph
8.2.1.1. When the INS ALIGN COMPLETE message
appears on the HUDiVDI formats, return the NAV
MODE switch to OFF.
Note
Do not select SAHRS during CV ALIGN to
check alignment progress. Wait until INS
alignment is complete and INS has been selected
on the NAV MODE switch before selecting
SAHRS.
10. SAHRS alignment progress may be monitored at
this time by selecting the NAV page.
Note
3. Repeats teps9 and 10o fconcurrentS INS alignment.
8.2.1.3 Concurrent Manual Carrier Alignment.
Manual carrier alignment should be used only when
SINS data or the SINS carrier align mode is unavailable.
This can be determinedb y the appearanceo f the CV
MAN DATA format on the MFD with MAN boxed.
. The SAHRS alignmentp rocessw ill initiate
a&r the INS determines a valid true heading
(approximately at INS quality value of
5). SAHRS quality value should reinitiate
to approximately 3 1.2 at that time.
l If power has been applied to the aircraft
foranextendedperiodoftimepriortoINS
CV align being initiated, the SAHRS may
complete a ground align (NORM) and a
SAHRS complete messagea ppearso n the
MFD. After the INS CV align is initiated,
the SAHRS will initiate a concurrent CV
align normally, but another SAHRS align
complete message may not occur.
11. It is advisable to continue alignment after appearance
of the INS ALIGN COMPLETE messageif
time permits. When ready to take the alignment,
the inertial navigation mode may be selected by
setting the NAV MODE switch to INS.
Note
Although SINS alignment normally requires
no entry of data, if a SINS alignment takes
place at any carrier location other than the
flight deck, then it is advisable to enter the
correct vertical lever arm via the DEU. This
is the height in feet of the aircraft INS above
the carrier SINS location. This entry can be
made only via the DEU by calling up the
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F-14D 飞行手册 Flight Manual 2(35)
