Manuevers Flashcards
TO profile
PF - “Set Thrust”/Push N1 Switch
PM - “Thrust Set”
rotate towards 15 deg
400’ - “LNAV/HDG SEL”
1000’ - “VNAV/FLCH (set speed)”
A/P
flaps up - after TO check
GA profile (2 eng)
“GA, Flaps 20”
Positive Rate - “Gear Up”
400’ - “LNAV/HDG SEL”
1000’ - “Set Speed”, “Climb Thrust”
flaps up - VNAV/FLCH, A/P, after TO check
GA profile (1 eng)
“GA, Flaps 5” (nearly full rudder)
Positive Rate - “Gear up”
400’ - LNAV/HDG SEL
1000’ - “Set Speed”
flaps up - FLCH/(VNAV), CON, A/P
(FMA - FLCH, MCT, A/P)
(E/O), (NNC), After Takeoff
85% level
Eng Fire/Fail on TO
small rudder/slow pitch; 10 deg 400’ - LNAV/HDG SEL, memory items 1000’ - “V/S 200”, Set Speed, A/P flaps up - FLCH, CON, E/O, NNC, After TO Check
-takeoff {trim 13 - 10sec}
-approaching altitude - 82%
-level {trim 8 - 6 sec}
-descend - 60%,
no power change when adding flaps
-final - 70% - {trim 5.5}
Visual pattern
- 1500 AGL (2700)
- fly to left side of ‘crop circle’ down river (2-2.5 nm PROG p2)
- base of triangle abeam - GR DN, F20
- turn when nose light green
- V/S -400, F30 Lndg Ck
APP mode should not be selected until (4)
- tune and identified
- intercept heading
- pointers in proper position
- clearance
(CHIP) Clearance Heading Identified Pointers
Why use C A/P?
powered from L AC, will auto switch to R AC with power failure
How do you get PROC TURN on legs page?
select any transition, then clean up legs page
Circle
Fix page - EPH 2 nm/GABBI 1840 ft
LAVSR
2 nm - Gr Dn, F 20 (“Approaching Glidepath”)
10 nm scale, fly off
HDG HLD, HDG 190 deg
just after 1900 push ALT HLD, push again at 1820
MA ALT, HDG SEL
HDG HLD, HDG 150 (check TRK)
base of triangle on edge of runway - HDG SEL
downwind - F 30, Landing Checklist
base of triangle abeam end of runway - turn final
VASI one white - A/P, A/T, FDs - off, FO FD - on
HDG to final approach course
Must retard thrust while pitching down to maintain PAPI
1 Eng ILS
G/S alive - GR DN, F 20, retard thrust one knob width - 65%
G/S capture - set MA altitude, Lndg checklist
Reject (why)
> 80 kts
- Fire
- Failure
- Predictive Windshear
- Unsafe/Unable to fly
NNC
GPWS
Autopilot - disconnect Autothrottle - disconnect Pitch - 20 deg/wings level Max Thrust Retract speedbrakes Do not change configuration
Windshear
TOGA Switch - push (Autopilot - disconnect) (Autothrottle - disconnect) Pitch - 15 deg/wings level Max Thrust Retract speedbrakes Do not change configuration
Stall
procedure
Autopilot - disconnect Autothrottle - disconnect - Nose down/wings level - Thrust as needed - Retract speedbrakes - Do not change configuration
(5/10 deg, stay below PLI)
STALL - Level Off
(5000 ft)
(config)
A/P - engaged
A/T - disarmed
“Expedite descent to 4000 ft”
Thrust - idle
Speedbrakes - extend