曝光台 注意防骗
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(1) Autopilot - EngageV; erifyN o Transient.
(2) Checkf or smootho perationin CSS.
b. Headingh old.
(1) Headingh old - Engage.
(2) Let3a ndr ightp edasl ideslip- CheckR eturnt o ReferencHe eading.
(3) CSS letI or right to 5’ roll - Aircmtl ShouldR eturnt o 0” Angleo f Bank
c. Altitude hold
(1) ALT hold - Selec(t verifyA /P REF advisoryil luminates).
(2) A/P REF - NWSp ushbutton- Depres(sv erifyA /P REFa dvisoryg oeso ff).
(3) Check for altitudec ontrol.
(a) A30 feet in level flight.
(b) 60 feet in 30° angle of bank.
d. Groundt rackh old @ESTs teeringn ot selected).
(1) GT hold - Selec(tv erifyA /P REF advisoryo n).
(2) A/J?R EF - NWSp ushbutton- Depres(sv erifyA /F REFa dvisoryg oeso ut).
10.20
NAVAIR 01.F14AAD-1
PROFILE
ABC
A
(3) Verify A/P establishesc rab into wind to hold selectedt rack.
(4) Autopilot emergencyd isengagep addle switch - Depress.
(5) PITCH and ROLL STAB AUG switches - ON.
76. Negative alpha/FOD check (20,000 feet, 300 knots).
a. Tbrottles - MJL..
b. Roll inverted in wings-level attituda and set - l.Og.
p&i-)
Negative-g maneuvering at high gross weight should be
avoided because of possiblility of aircmfl departure.
c. Check for nomal engine operation and FOD or loose gear.
77. Air-to-air check.
a. Weapon selector switch - LR
b. Test target - Select.
c. Attacksteering - LAR-Vc.
d. Collision steering.
e. Attacksteering - LAR-V,.
(1) MR.
(‘4 SR
f. Target intercept.
(1) VSLhigh.
(2) VSL low.
(3) hml.4
(4) PLM.
(5) PAL.
(6) Select gun.
(7) Observe proper HUD display.
10-21 ORIGINAL
NAVAIR Ql-FUAAD-1
PROFILE
A
A
A
ABC
ABC
ABC
ORIGINAL
g. Glmsigllt - check
(1) RTGSiMANUAL.
(2) MMGS.
78. Air-to-groundc heck.
a. SelecAt /G.
79. Fuel dump check.
a. Speedbraksew itch - EXT.
b. DUMP switch - DUMP.
(Observen o ibe1d ump).
c. Speedbraksew itch - RET (observefu el dump).
d. DUMP switch - OFF.
80. Fuels ystemc heck( totalt ie1l esst han8 ,000p ounds).
a, WING/EXT TRANS switch - OFF.
b. FUEL FEED switch - FWD/R
Monitor5 00-PounSdp lit,A FT/L High.
c. FUELFEED switch - AFT/L
Monitor5 OOPoonSdp lit,F WDiR HIGH.
d. FUELFEEDswitch - NORM.
Verify FWD/Rh igh splitr emainsc onstant.
103.14 Approach
81. Landingc hecklistc omplete.
82. ACLSIARA-63 - Check.
83. AirspeedanAd OA(15 unitsA OA) - Check.
a. AOA, INDEXER, HUD.
(1) Gross weight pods.
(2) Airspsea- knots (124 knotsW knotsa t 44.000-pouugdr ossw eight.A dd 3
knotsp er2 ,000p oundso ver4 4,000-poungdr ossw eight).
10.22
NAVAIR 0%F14AAD-I
10.3.15 Touchdown
84. Verify exhaust nozzle less than 26 percent.
a Three to seven seconds atIer touchdown, nozzles 100 percent.
85. Walkaroundimpection - Complete.
10.4 FUNCTIONAL CHECKFLIGHT PROCEDURES (RIO)
10.4.1 Prestart
1. ICS.
a Normal.
b. Backup.
c. Emergency.
2.lNDLT-TEST.
3. Seat adjustment - Check.
4. canopy rigging,
a Both cockpit handles same position during operation.
b. BOOST not required to close.
5. NAV MODE switch - ALIGN.
a After displays are on, verify and/or enter alignment coordinates.
10.4.2 Poststart
6. Multifunction display.
8. Verify navigation display.
7. ALR-67 - BIT.
8. Altimeter - Set and Check; Record Error
When the local barometric pressure is set, all altimeters should agree within 75 feet at
field elevation.
10.4.3 Taxi
9. BDHI - Cross-CheckHeading WithVDI/HUD.
IO-23 ORlGlNAL
NAVAIR 0%FMAAD-1
‘ROFILE
A 10. NW - check (at takeoff end of runway).
Groundspeed
IO.44 Takeoff and Climb
11. Engine romp - Check at ML.
9 12. Airspeed - check (200 knots).
A
Pllot Standby
KIAS
13. Altimeter - Check.
RIO Standby
KIAS
A
A
ABC
INSISAHRS ALTIMETER
14. Tacan and NSV position - Cross-Check.
15. MS navigation and radar mapping check.
a. Radar map - Check All Range Scales.
10.4.5 15,000-Foot Checks
16. Stroctural integrity check.
a. Anti-g valve operation,
b. Set radar power switch to STAY before pilot ECS chock
ORIGINAL to-24
Time
95 to 104 nominal
HUD
KCAS
NAVAIR WFIUAD-I
10.4.8 20,000-Foot Checks
17. Radar power switch - XMIT (airstarts complete).
10.4.7 Climb to 35,000 Feet
18. Engine instmmeota - Record.
OIL (PSI)
I Left Right Limits
I 25 to 65 I
RPM (%)
EGT (“C)
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F-14D 飞行手册 Flight Manual 2(54)
