-
T/O
Advance thrust levers to -
Push __ switch (Capt only)
80 knots -
V1 -
Vr-
Initial pitch attitude-
Positive Rate -
At 400 radio altimeter -
At thrust reduction height -
After flap retraction -
- 1.1 EPR
- EPR switch
- "80 knots", "check"
- V1
- "Rotate"
- 15 degrees
- "gear up"
- select roll mode
- select VNAV
- "after takeoff checklist"
-
V1 CUT:
Rotate to ___ANU
At Positive Rate -
At acceleration altitude -
At CMS -
- 12.5 ANU
- "gear up, heading select runway heading"
- "set speed Vref30 + 80, V/S set 200fpm"; flaps up on schedule
- "FLCH, Vref30 + 80, max con thrust";"A/P on" (optional)
-
ILS Approach
Flaps on downwind -
Flaps on base -
At G/S alive -
G/S capture -
- "flaps 1"
- "flaps 5"
- "gear down, flaps 20", arm speedbrake
- "flaps 30", set missed approach altitude
-
VNAV approach
Verify the the ___ is shown on the final approach segment of the LEGS page.
Verify that ____ is engaged or that the _____ is captured.
Approx 2 miles before FAF and after ALT HOLD or VNAV PATH is annunicated (3) -
Approach glide path -
Glide path intercept -
When at least 300 feet below MAP altitude -
500 ft AFE -
100 ft above MDA(H) -
- VNAV glide path angle
- LNAV, localizer
- set DA(H) or MDA(H); select or verify VNAV; select or verify speed intervention.
- "gear down, flaps 20", arm speedbrake
- "flaps 30"
- set MAP
- "500 feet"
- "approaching minimums"
-
Approach using V/S
Approx 2 NM before FAF and after ALT HOLD (4)-
Prior to FAF -
At 0.2NM from FAF, select -
500 ft AFE-
100 ft above MDA(H)-
At MDA(H) capture -
- open V/S window; set MDA, select speed intervention; "gear down, flaps 20", arm speedbrake
- "flaps 30"
- V/S down 1000fpm, "landing checklist"
- "500 feet"
- "approaching minimums"
- set missed approach altitude
-
GO-AROUND:
at the same time (2) -
verify (2) -
verify positive rate -
At 400 ft radio altimeter -
At acceleration altitude (2)-
Retract flaps -
After flaps retraction (3) -
- push the GA switch; "flaps 20"
- rotation to go-around attitude (initally 15, 12.5s/e); thrust increase
- "gear up"
- select roll mode
- set speed to the planned maneuver speed (Vref+80 s/e); V/S 200fpm s/e
- on schedule
- FLCH or VNAV; "climb thrust"; "after T/O checklist"
-
STALL RECOVERY:
At first indication of stall (3) -
As engine accelerates -
- smoothly apply max power; smoothly decrease pitch attitude to approximately 5 ANU; level wings.
- counteract the nose up pitch tendency with positive forward control column pressure and nose down trim.
-
STEEP TURNS:
As bank angle is increased into the turn an increase in ____ and ____ is required -
Trimming during this maneuver is -
What is required to detect deviations early enough to be corrected by small adjustments?
Airspeed changes very slowly because of small changes in thrust and drag. Therefore -
- pitch and thrust
- not recommended
- rapid instrument scan
- Anticipate thrust changes and apply them atthe first indication of change.
-
RAPID DESCENT -
7 items (note:A/P on is recommended)
- Initiate tuen if required
- Select lower altitude on MCP
- Select FLCH
- Select speed Mmo / Vmo
- Close thrust levers
- Extend speedbrakes
- Notify ATC
-
GROUND PROX WARNING (5):
- disengage A/P
- disengage A/T
- aggressively apply MAX thrust
- simultaneously roll wings level and rotate to an intial pitch attitude of 20ANU.
- retract speedbrakes
note:if terrain remains a threat, rotate to stick shacker. Do not change configuration.
-
WINDSHEAR - MANUAL FLIGHT (7):
- disconnect A/P
- push either G/A switch
- aggressively apply max thrust
- disconnect A/T
- simultaneously roll wings level and rotate toward an intial pitch attitude of 15ANU
- retract speedbrakes
- follow flight director GA gusidance (if available),
Note:do not change configuration
-
WINDSHEAR - AUTOMATIC FLIGHT (5):
- press either G/A switch
- verify GA mode annunciations
- verify thrust advances to GA power
- retract speedbrakes
- monitor system performance
NOTE:do not change configuration
|
|
