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Note
Them aneuvedr eviceA OA signafl rom the nosea lpha
probet o CADCh asa fasterr esponsrea tet hant hes ignal
t?om the left-sidef uselagep robe to AOA indicator,
causinga low reading(e rror)o nt he indicatorT. hise rror
is directlyp roportionatol the aircrafiA OA maneuver
rate. Thereforet,o determinew hen maneuvedr evice
extensioonc cursp, erformt heh igh-AOAm aneuvedr evice
checkb y slowly increasinga ircraftA OA anda llowing
aircratl to stabilize.
d. Maneuvedr evicesre tracta t 8 unitsA OA.
e. ALPHACOMPcb - Out.
63. Approachetso stallsa nda pproaccho nfigurationc heck( approximatel1y5 ,000fe et).
a. Clean stall.
(1) Stabilizein levelf light at 15u nitsA OA.
(2) Ensurem aneuvedre vicesre tracted.
(3) Slowlyd eceleratteo buffet onset.N ote AOA (light air&oneb uffet at 12 to 13
units,i ncreasintgo moderatein tensitya t 15u nitsA OA).
10-16
NAVAIR Ol-Fi4AAD-1
(4) Continue deceleration to 28 units AOA. Note any abrupt or significant rolloff
tendencies.
b. Clean stall with maneuvering devices extended.
(1) Stabilize in level flight at 15 units AOA.
(2) Extend maneuvering devices.
(3) Slowly decelerate to buffet onset. Note AOA (light airtiame buffet at 13 to 14
units AOA).
(4) Continue deceleration to 28 units AOA. Note any abrupt or significant rolloff
tendencies.
(5) When AOA is below 15 units, retract maneuvering devices.
c. Approach configuration check.
(1) Perform landing checklist (ml1 SAS ON, ALPHA COMP cb out).
(2) DLC - Engage.
Check for excessive lateral trim mquimments.
(3) AUTO THROTTLE.
(a) Response to longitudinal stick.
(b) Responset o tom entry, steadyr ollout.
(c) Responsein HOTMORMKOLD.
(d) AUTO THROT light.
1. Manual overtide.
2. CAGE/SEAM button.
d. Dii stall.
Slowly decelerate to level flight to 20 units AOA. Note any abrupt or significant rolloff
tendencies.
e. Attempt speedbrakee xtensiona t MlL power.
f. ALPHACOMF’cb - In.
64. Strnctural integrity check (0.9 Mach at 10,000 feet).
a. High-speeddash - MILTHRUST.
b. High-gturn.
IO-17 ORIGINAL
NAVAIR 0%FMAAD-1
‘ROFILE
46
4B
48
48
9B
9B
c. Anti-g valve operation.
d. HUDg-Cheek.
10.3.9 AIrstarts (20,000 Feet)
65. Radar power switch - STBY (coordinate with RIO).
66. Spooldown air&art.
a. Stabilize at 300 lolots.
b. Right thmttle - OFF Them IDLE at 60-percent rpm.
Note
Subidle stall can be cleared by cycling the throttle to
OFF and immediately returning it to IDLE.
c. Stabilize at 300 hots.
d. Left throttle - OFF Then IDLE at 60-percent rpm.
67. Radar power switch - XMIT (coordinate with RIO).
10.3.10 Climb to 35,000 Feet
68. Fuel management.
FEED
FUS
WING
EXT
TOTAL
Left Rl9ht
69. ECS check
a. Automatic cabin temperaturec ontrot
b. Manual cabin temperature contn~l.
c. Cabii altitude schedule (appmximately 14,000 feet at 35,000 feet).
70. Afterburner light-off - Check (cheek at 210 knots).
a. ASYM LIh4lTER switch - OFF.
IO-18
NAVAIR 0%FMAAD-I
b. Throttles - MAXAB.
I
Verify AB light-off within 10 seconds.
c. Throttles - Less Than MIL.
d. ASYh4 LIMITER switch - ON.
71. Engine instruments (engine MIL power at 0.9 Mach).
OIL (PSI)
Left Right Limits
25 to 65
RPM (%)
EGT (‘C)
107.7 maximum
935’
10.3.11 High-Speed Dash (35,000 Feet)
72. Idle lockup - Check.
a. Jam throttles - MAX AB (acceleratet o 1.2 Mach).
b. Both throttles to MIL until nozzles close, then IDLE above 1.1 Mach and verify less
than 2-percent rpm decay.
Monitor rpm decay while retarding throttles to IDLE to
ensure proper idle lockup operation. Discontinue idle
lockup check if rpm decays more than 2 percent above
1.1 Mach. Place throttles to MIL and decelerate.
c. Jam throttles - MAX AB (accelerate to 1.5 Mach).
d. Engine instmments - Monitor.
NO2 position (“h)
OIL (PSI)
RPM (%)
EGT (“C)
Left Right Limits
50 to 60 (open)
25 to 65
107.7 maximum
935’
e. Mach trim compensation - Check.
10-19 ORIGINAL
‘ROFILE
ORIGINAL
f. wii-sweep program - Check.
g. Comparep itot-staticin strcmentast 1.5M ach.
Pilot stby RIO stby
Altitude
Airspeed
Calibrated
10.3.12 Zoom (40,000 Feet)
73. Pitch up to FL 400.
74. Cabinp ressurizatioann dB CS - Check( approximatel1y7 ,000fe et at 40,000f eet).
1013.13 20,000-Foot Checks
75. AFCS check.
a. Attitodehold.
　
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