220 General Flashcards
Gear speeds
250 - max extension and operating
220 - max retraction
Turbulence pen speed
280/.75 (lower)
FLAP SPEEDS
230 -1
210 -2
210 -3
190 -4
170 -5
PFCC on FFOD
“POPMD”
Pouches sealed (2) - docs and elementary work
O2
Pins (3)
Mics
Door, Documents
Emergency equip check (7 items)
Hood, axe, extinguisher, flashlights (2) and gloves, vests (3),
Escape rope and hatch
Fuel burns
30 Air
10 Ground 2 engine
2 APU
Max landing weight
57833
Thrust Limits related to oil temp
Below -6C: idle
-6C to 21C: 30% N1
21C to 49C: 50% N1
Wingspan
115’1”
Ice shedding on ground
Whenever 3*C or below and visible moisture in any form is present.
60% N1 momentarily, every 30 mins. First run-up during taxi done as soon as possible. Heavy snow, min 10 seconds and more frequent.
Max 43kt crosswind, 18kt tailwind
APU bleed max
23000
“Fuel imbalance” indication at _______
454
Limitations with fuel >2830 in either wing..
- APU must be monitored
- Left engine started first
- If center tank <10670, transfer into centre tank
Normal allocations of ADSPs 1-4
1 - CA PFD
2 - FO PFD
3 - ISI
4 - backup
APU fuel is fed from where?
LH fuel tank, L or R boost pumps or LH ejector
Engine fire button action (7)
-bottles armed
• Fuel shut‐off,
• Hydraulic shut‐off
• FADEC commands engine shut‐down,
• Fan air valve closes,
• Bleed air (PRSOV) closes,
• VFG deactivates.
Max TOW
67.5/69.8 (125-133)
Tire Limit speed
195
Cowl anti-ice on when?
OAT 10C or below and visible moisture in any form is present (at or below 1500 AGL)
Wing anti-ice on when, on ground?
OAT 5C or below and visible moisture in any form.
QRH must be used for what procedure?
Smoke/Fire/Fumes
Max Fuel
17400
Min Oil Temp for start
-40C
Max APU Start attempts
3/hour, 2 min delay between
Max Take-off parameters (Time/EGT)
5 mins (10 if single engine)/1054C
Oil Temp in flight
49C to 163C (can go to 174 for up to 20min)
49C minimum for take-off
Oil Pressure min/max
50.3 - 175.3
If -20 or below and wet/contaminated what must be remembered
If turnaround > 2 hours, cycle reversers at least twice, must take-off within 5 mins, otherwise repeat.
Max start attempts before 30 min cooling
3 attempts, or 4 mins continuous cranking
Engine wind limits
43 kts cross, 18 tailwind for starting or ice shedding
Oil consumption limits
.4 gt/hr (.38L)
No derate or flex when?
Windshear, downdrafts
Contaminated
Anti-skid or AT inop
(Can derate with anti-ice on, but no flex)
Pushing TOGA button does what? (3)
- Arms AT (if not previously armed)
- sets FD to pitch guidance, and
- synchronizes heading bug
Cold soaking and hydraulics
temperatures below -40°C, hydraulics must be warmed up so that HYD 3 reservoir temperature is at least -6°C for take off
No Wing Anti ice when?
Above 15 TAT
Min speeds for RAT
148 electrics
115 hydraulics
Max altitude for wing A/I test
31000 (do for 3 mins)
FBW Pitch compensation to?
33 degrees bank
60 degrees bank displays when over ___ and gone when below ___
40, 30
Starter aborts when (5)
Hot or hung
Loss of EGT data
N1 locked rotor
Igniter or fuel ctrl fail
when EDM activates automatically, what happens? (7)
- Masks
- Belts
- AP and AT on
- HDG mode present heading
- 15000’ set, idle descent VMO-5
- Aural ‘EMERGENCY DESCENT’ and EICAS
- 7700
When is ROLLOUT active on an autoland?
2 seconds after WOW
When is the ROLLOUT command bar removed on an autoland?
Below 30 kts
Calls 500 and below on a Cat III LAND 3
CA: Inside 1500 AAE “LAND 3” (when displayed)
FO: 500 (monitor or call), “STABLE”
FO: “200” (monitor or announce with no DH)
CA: “ROGER”
or
FO: “APPROACHING MINS” 80 above DH, with DH (monitor or announce)
CA: CONTINUE or GO AROUND FLAPS
FO: “NO RETARD” or silent
CA: “ROGER” (if no retard)
CA: “AUTOPILOT OFF”
Reactive windshear between what altitudes?
10-1500
PRM breakout (set heading 30 degrees away from parallel during approach)
AP and FD OFF
CA: Turn to assigned heading and climb/descend
FO: set Hdg and Alt, FLC
CA: AP ON
Speed Man, VFE-5, “FLAP __” (CA)
“POSITIVE RATE” (FO), “GEAR UP” (CA)
Flaps on speed
AFTER GA CHECKLIST
Predictive windshear, inhibited on take-off when? Active when?
OFF: 80 kts to 50’,
ON: 50’ to 2400’
Predictive windshear, active on approach when?
2300’ down to 50’
Engine operation prohibited in ______________ conditions with temp below __________.
Ground fog, -18
Design VA
300/.80
Contamination:
- Trace of any deposit is ______
- Frost is ______
wet
Critical items on power down/up (8 minutes min)
- FAs must log out of CMS
- termination checklist
- 3 min blacked out.
- no PAs or seat belt sign while CMS initializing (8 mins)
- no changes in electrical power or hyd switches while PBIT running (FLT CTRL IN TEST), approx 2 mins.
- power up from APU only.
Max take-off alternate distance
351 NM
Must be planned to land with no less than ______ EFOB. If planned EFOB is less, will add ______ fuel.
1300, SUPP.
For manual landing, autopilot disconnect by _____
80 feet
Permitted to fly overwater flight legs within ____ of a suitable emergency landing site
400nm
Ensure arrive at destination _______ 72 hours of ____________
within, the last service check
Min oxygen for dispatch
2 pers:____
3 pers: ____
900 (950 mountainous)
1200 (1300..)
Landing gear is extended and retracted hydraulically by pressure from hyd system #_______
1
The backup for hyd system #1 eng driven pump #1 is ___________
Power transfer unit (PTU)
The backup for hyd system #2 eng driven pump 2 is ___________
AC motor pump (ACMP 2B)
Slat system uses pressure from hyd systems ___________
2 and #3
Max dry crosswind TO _____
Max dry crosswind LDG _____
32
29
Icing conditions exist in flight when…
TAT of 10°C or below, and visible moisture in any form present (except when the SAT is -40°C or below).
What must be ensured during an approach and landing in icing conditions, or if there is evidence of ice accretion?
VREF, VAC and VGA speeds must be increased by 5 KIAS if landing flap 5
If the total passenger count indicates more passengers than the LDF but within tolerance, what must be done?
Adjust the ZFW by 80kg per extra passenger
Second segment climb starts ___________, and continues up to at least ___________ and is flown at _______ with config as__________
once the landing gear is up
400 AGL
V2
Flap in TO position
For a passenger evacuation using the ECL, both pilots must____________
Select the ECL on their respective DUs, DU2 and DU3
What are trhe PWS 1) caution and 2) warning indications (per phase of flight)?
1) Caution for take-off and approach:
“MONITOR RADAR DISPLAY”
2): Warning for Take off and climbout (50’ to 2400’):
“WINDSHEAR AHEAD, WINDSHEAR AHEAD”
Warning for Approach and landing (2300’ to 50’):
“GO AROUND, WINDSHEAR AHEAD”
The minimum fuel quantity for go-around is ______ kg per wing (with the airplane level) and at a maximum airplane climb attitude of 10 degrees nose up.
442
Following bank angles permitted at green dot:
Maximum bank angle of ______° at altitudes up to ________ ft.
Maximum bank angle of _______° at altitudes above _______ ft.
30 degrees, 31,500
15 degrees, 31,500
Points to remember for
RNP AR approaches (5)
Verify auth’d on 10-10
Verify “RNP AR APP” displayed prior to first wpt
Speed MAN prior to IAF
AP flown
Final flap prior to FAF
If flying LNAV/VNAV mins vs LPV what must be remembered?
Change arrival data box from LPV to RNP
WAI test limit based on
TAT or
SAT?
TAT
Fuel transfer switch goes which way to accomplish moving fuel to right tank?
MAN XFR -R (select where you want fuel to go
Take off with tail wind:
limits and considerations
Max 15 knots, high wind procedure if over 10 knots
Landing with tailwind:
limits and considerations
-Max 15 knots
-no flap 4 landings beyond 10kt tailwind,
-prohibited beyond 10 with any failed system where a Non-Normal code is required.
When would ‘TOO LOW GEAR’ sound on a normal approach?
below 1000’ AGL when the flaps are at 4, and gear not selected down.
Autoland is permitted during Cat I operations provided:
-LAND 2 or LAND 3 is displayed on the ASA
-Autoland wind limits apply
Can we conduct a manual landing from a CAT II approach?
Only if AL not available, APPR2 required, disconnect between DH and 80’
What are the FD modes during windshear escape (take-off and approach)
Take-off: TO/WSHR
Approach: GA/WSHR
These remain active until another selection is made!
For EDM to activate automatically
Aircraft alt above F250
Cabin Alt above 14,500
When major things happen when aircraft enters terrain caution or warning range ?
-PLAN display to MAP with TERRAIN overlay
-WXR cancelled
-scale to 10NM
-“CAUTION TERRAIN’ or “TERRAIN TERRAIN, PULL UP, PULL UP”
“CAUTION, TERRAIN” sounds ____ seconds before terrain conflict.
60
“TERRAIN, TERRAIN, PULL UP PULLUP” sounds ____ seconds before terrain conflict.
30
For TAWS, orange indicates _____ below and _____ above and red indicates exceeding _____ above aircraft
500, 2000
2000
Flaps only extend at which lever positions?
2,3,4,5
Slats deploy (further) at which lever positions
1,4,5
220 eye to wheel height in feet?
21’
Altimeter limit on pre flight cross check
maximum allowable difference between Captain’s and FO altitude display and field elevation is 75 ft
Altimeter limit in cruise
200’ (RVSM)
During take-off phase what speeds are targeted for all engines _____ and single engine _____?
V2 +10 (all engine)
V2 (single engine)
On take-off rotation, bank angles in excess of ____ and pitch in excess of ___ may result in striking aircraft nacelle/tail
15 degrees bank
10 degrees pitch
