Procedures Flashcards
Engine Start
Packs……Off
APU Bleed……On
Engine Start selector……GRD
Increase in N2 RPM……Verify
N1 Rotation……Verify
Engine Start Lever……Idle Detent (when N2 reaches 25% or max motoring)
Fuel Flow and EGT indications within 15 sec……Verify
At 56% (63% MAX) N2 RPM……Check start switch moves to off. If not, position START switch to OFF
Duct Pressure…….Verify Decreasing
Start Valve Open light……Verify extinguished
EGT start limit……Verify
Engine Indications……Monitor (N1 19.4%, N2 58.8%, EGT 410°C, FF 600 / MAX 20.1%, 70.3%, 610°C, 600)
After Engine Start
After Start valve closed and engine stabilized at idle:
- Gen switch (operating engine)……On
- GRD PWR (if used)……Off
- External air source and power source (if connected)……Disconnect
Missed Approach Profile
- TO/GA switch
- Thrust levers advance……Verify (if go-around Intitiated after touchdown, verify speed brakes retract and autobrakes disarm)
- PF “Going-around, flaps 15/5”
- PF “Check thrust”
- Pitch attitude……Adjust, as required
- Flaps……Set
- Thrust setting……Verify (ensure GA on FMA)
- PM of PF “Positive rate”
- PF “Gear up”
- PF “Set missed approach altitude”
At 400’
• Roll mode (on order)…….Verify LNAV or HDG SEL
At 800’
• PF “Level change, set CMS (or desired speed), flaps 5/1”
• Flaps retract……Announce
• Flaps……Retract flaps on command
When “Flaps Up”
• Autopilot……As desired
• PF “After Takeoff Checklist”
NADP 1
- Normal T/O to 400’
- Climb to acceleration altitude at V2 + 20
- Thrust reduction altitude at 1500’
- Acceleration altitude (3000’ AFE)
- Accel to 250 knots
- Retract flaps on schedule
- “Flaps up, After Takeoff Checklist”
*Max AOB 15° until reaching V2 + 15, 30° thereafter
NADP 2
- Normal takeoff to 400’
- Accelerate to V2 + 20
- Thrust reduction / acceleration altitude (usually 800’)
- Accelerate to CMS (Vref 40 + 70)
- Retract flaps on schedule
- “Flaps up, After Takeoff Checklist”
- 3000’ AFE
- Accelerate to 250 knots
When do you arm LNAV
After loading winds, dep/arrival, and verifying the route
When do you arm VNAV
After calculating CMS and adding it to the CLB page
When do you arm autothrottle
After entering/loading OAT on the N1 page
ILS/GLS Profile
• Set FMC/Radios After cleared for the approach • ARM APP Mode After 2500’ callout • PF “(Approach), (Runway), (Final app course), min\_\_\_ baro/radio” • PM “\_\_\_ in/hPa” At glide slope capture • PF “Set TDZE” By 1500’ or FAF, whichever occurs later • Gear down By 1000’ RA • Arm speed brakes • PF “Flaps \_\_\_, landing checklist” • Set speed At 1000’ RA after auto callout • PF “Set missed approach altitude. Cleared to land/no landing clearance” At 500’ auto callout • PF “Stable/unstable, going-around” At minimums auto callout • PF “Landing/going around”
LOC or VOR approach
Same setup and stabilized approach plan as any approach.
• Calculate and set a DDA for any of the following
- Published MDA
- VNAV is not available (V/S used)
- Cold temperature altitude corrections entered
When cleared for the approach
• Lateral - select/verify appropriate roll mode
• Altitude - select/verify next MCP altitude restriction
- No lower than FAF int altitude until TDZE requirements are met
- Set TDZE when: established on the approach and VNAV engaged
• Vertical - select/verify appropriate vertical mode
• Speed - speed window may be used outside FAF. Inside FAF speed window should be closed
• FMAs - confirm they match what is expected and briefed
• TDZE - Set once set on the approach
RNAV (GPS/GNSS) and RNAV (RNP) Approach Procedures
• FMC — Set
-Verify GPS is updating prior to IAF (NAV STATUS pg 1)
-RNAV (GPS): manually set RNP to 0.30
-RNAV (RNP): set RNP per approach plate
-One pilot displays PROG pg 4/4 to verify ANP/RNP/XTK ERROR
• Radios — Set
-tune 108.0 (recommended)
-Inhibit all VOR and DME updating from NAV OPTIONS pg 2 prior to IAF
• EFIS control panel — Set
-Both pilots in map mode and at least one in 10nm scale or less by FAF
• Altimeter setting tolerance — Set local
-Crosscheck CA and FO altimeter is 100’ or less by FAF
After cleared for the approach, below the transition level, and/or no later than immediately following the 2500’ callout:
• Standard callouts
• LNAV — Engage/arm
-monitor PROG pg 4 for XTK error inside IAF
• Vertical mode — Engage/arm
-VNAV required for RNP approaches. Monitor PROG pg 4 for VERT DEV. Cannot exceed 75’ inside the FAF
Single Engine ILS/GLS
- Intercept localizer with Flaps 5 at Flaps 5 maneuver speed
- When glide slope is 1-1.5 dots set Gear down, Flaps 15, Arm speed brakes, set Vref 15+5
- With good weather and adequate time, consider zeroing out rudder trim prior to landing (not required)
Single Engine Go-Around
- Fly one of the following:
- Engine failure procedure from ACARS landing data
- T/O / MA on the applicable airport info page
- If no engine failure procedure is listed track extended runway centerline
- Apply go-around thrust, press TO/GA, rotate to F/D pitch (aprox 13°)
- “Going-around, Flaps 1, check thrust”
- “Positive rate, gear up, set missed approach altitude”
- Adjust pitch to maintain Vref 15 + 5
- At 400’ AFE: Call “HDG SEL/LNAV”
- At 800’ AFE: “Set CMS” - Accelerate and clean-up as appropriate
- “Set max continuous thrust” for climb
- Abbreviated After T/O checklist
Single engine non-precision approach
- Flown Flaps 15 with VNAV (If available)
- Intercept FAC with Flaps 5 at Flaps 5 maneuver speed
- At aprox 1-1.5 nm from FAF: Gear down, Flaps 15
- Descend on VNAV to DA/DDA, or if VNAV is not available, descend at 1000’/min to MDA
- Keep in rudder trim
- Flown using autopilot
Engine Failure on takeoff after V1
- Announce “Engine failure”
- Maximum thrust may be selected (TO/GA switch), but be prepared to compensate for increased asymmetry.
- Smoothly apply rudder to parallel or gradually return to runway centerline.
- Accelerate to Vr - V2
- Rotate to 7-11° - Do not follow flight director commands until established in climb
- Apply rudder and aileron to maintain heading
- “Positive rate, Gear up”
- Once established in climb target V2 for climb
- Fly appropriate engine failure procedure
- At 400’ AFE: Verify “HDG SEL/LNAV”
- At 800’ AFE: If VNAV not armed for T/O, “Set CMS”
- At CMS: “Set max cont thrust” (N1 LIMIT page)
- Climb to 1500’ AFE min.
