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20. CANOPY handle -CLOSE.
21. FIRE DETI’I’BST -TEST.
22. THROTTLE MODE switch - BOOST.
23. Throttle friction lever - As Desired.
24. Left engine - Start.
25. RDR switch- STBY.
26. TCS switch - STBY.
21. IRST switch - STBY.
EnsureT ARPS maintenancep ersonnelh ave
loaded sensors and cleared aircraft before
initiating power to TARPS pod.
28. [T] TARPS control panel SYSTEM switch -
RDY.
Note
The Poststart Checklist shall be completed
with respect to aircraft configuration and
switch positions prior to taxi.
7.9 FIELD CARRIER LANDING PRACTICE
7.9.1 Preflight Inspection. A normal preflight inspection
will be conducted with specific attention directed
to tire condition, nosestrut extension, AOA probe
conditions, and windshield cleanliness. Check that the
hook bypass switch is in FIELD.
7.9.2 Takeoff. The takeoffwill be individual.
NAVAIR 01.Fl4AAD-1
7.9.3 Radio Procedures and Pattern Entry. A
radio check with Paddles is advisable before pattern
entry to co&m Charlie time. Approaches to the field
for break will be controlled by the tower and t&n
switchedtoPaddlesforFCLPpatterncontml.Atnotime
will an aircraft remain in the pattern without a UHF
receiver. On each succeeding pass, the following
voice report will be made at normal meatball acquisition
positions:
1. Side number
2. TOMCAT
3. Ball/Clam
4. Fuel state
5. Type of approach, if appropriate (automatic,
degraded, etc.).
7.9.4 Pattern. The pattern should be a racetrackwith
the 180” approximately l-1/4 miles abeam at 600 feet
above field elevation (see Figure 74). The length ofthe
groove should be adjusted to give a wings-level descent
on the glideslope of20 to 25 seconds (approximately 3/4
mile). For maximum gross weight at touchdown, refer
to Chapter 4, Operating Limitations. The turn to the
downwind leg should be commenced after climbing to
pattern altitude (600 feet AGL) utilizing 30” angle of
bank and 150 KCAS. Turning t?om the 180’ power
should be adjusted to maintain optimum angle of attack.
A gradual descent may be commenced at this position
with a minimum altitude of 450 feet AGL at the 90”
position and 350 feet AGL as a minimum until the pilot
is receiving glideslope information. At approximately
49, the meatball appearso n the Fresnel lens.F ly a rate
of descent such that the ball is centered as the aircraft
arrives wings-level in the groove. For manual, automatic,
and DLC approach techniques, refer to Carrier-Based
Procedures,C hapter 8.
7.9.5 Night FCLP. All provisions that apply to day
FCLP also apply to night FCLP, plus the following
items:
1. External lights-BRIGHT and STEADY.
2. Hook bypass switch -FIELD.
When comfortably situated in the pattern, instruments
should be flown as much as possible up to the
45” position.
7-37 ORIGINAL
NAVAIR Ol-F14AAD1
“‘CROOWINO’ NOTE
u ” INOlCATES LsOTERMlMOLoGY USEDOVER
THE UHF TO DESCRl8E THE PATTEFtN.
“AWROACH TURN”
Figure 7-4. Field Carrier Landing Practice
ORIGINAL 7-38
NAVAIR 01.F14AAD-1
CHAPTER 8
Carrier-Based Procedures
8.1 CARRIER PREFLIGHT
8.1.1 Launch. Applicable aircraft launching bulletins,
the CV and LSO NATOPS Manuals and the pertinent
CV air operations manual shall be read by all flight
crewmembers prior to carrier qualification. In addition,
the predeploymentle ctures yllabusc ontainedi n Chapter
I of the CV NATOPS Manual shall be completed.
8.1.2 Briefing. A thorough briefing shall be accomplished
by the flight leader prior to launch. This briefing
should call particular attention to current BINGO fields,
emergencyprocedurespeculiartocarrieroperations,operating
area NOTAMS, fuel management, and ship
NAVAID status. Aircraft configuration, gross weight,
expectedW OD, and applicablel auncht rim settingsw ill
be verified prior to man-up.
8.1.3 Preflight. Preflight inspection should be accomplished
with particular attention given to nosestrut,
main landing gear, tires, hook, and underside of the
fuselage.N ote carefully the actual wing sweep,t he lateral
spacing between parked aircraft, and the general
direction of engine exhaust. Do not preflight the aircraft
topside at? of the bleed air doors if spotted with the tail
outboard of the safety nets. In the cockpit, particular
attention should be given to the flightcrew displays to
ensure that the retaining devices have been installed.
Ensure that the WING SWEEP handle is secure in the
　
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