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47 Cards in this Set
- Front
- Back
B757 Flap Speed Limits
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1...........................240
5...........................220 15..........................210 20..........................195 25..........................190 30..........................162 |
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B767 Flap Speed Limits
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1...........................250
5...........................230 15..........................210 20..........................210 25..........................180 30..........................170 |
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UPS is approved to use the B757/767 FMC for enroute and terminal RNAV operations, but not
_______________. |
RNAV approaches
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RNP stands for:
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Required Navigation Performance (RNP)
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RNAV1
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Crosstrack error/deviation should be limited to 0.5 NM
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RNAV2
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Crosstrack error/deviation should be limited to 1 NM
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Required Equipment for RNP
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1FMCandCDU
1 VOR and 2 DME receivers 1 IRU in the NAV mode 1autopilotorflight director and the AFDS LNAV mode 2 map displays (can be from the same FMC) GPS or DME/DME/IRU with updating Current nav database |
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The B757 and B767 are not authorized to fly Q routes in ____________ and RNAV routes in ____________ ?
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Gulf of Mexico
Alaska |
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Engine Anti-ice is required when
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Engine Anti-Ice –10°TAT
Engine anti-ice must be on during all ground and flight operations when icing conditions exist or are anticipated except during climb and cruise when the temperature is below –40°C SAT |
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NON PRECISION APPROACH
configure when? |
NON PRECISION APPROACH
4. 4 miles GEAR DOWN flaps 20 2. 2 miles flaps 30 ldg chk list 1. 1 mile walk the panel |
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The ASA monitors what?
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ASA
F -FCCs I -ILS Receivers I -IRS’s R -Radar Altimeter E -Electrical System S -Auto-pilot OR FIIREP like pirep |
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ASA when tells you what on the top and bottom?
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What you can do.
What you can't do. |
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CAT II, III AUTO-BRAKE CHART
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CAT II, III AUTO-BRAKE CHART
Easy to misread. G/S intercept runway length needs to Be longer than the number in the briefing guide ie: 35R in SDF needs MAX auto-brakes |
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03.04.09.03
WEATHER REQUIREMENTS FOR Departure ALTERNATE |
03.04.09.03
WEATHER REQUIREMENTS FOR Departure ALTERNATE WX is below CAT I mins The alternate needs to be: Within 1 hour or Within 300 nm |
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Destination Alternate forecast WX mins vs
destination |
Destination Alternate
Unlike, at a destination, both ceiling and visibility must be forecast at the alternate ETA to be at least as good as that derived from the following: |
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03.04.05.01
FLIGHT DIRECTOR AND AUTO COUPLER POLICY |
03.04.05.01 FLIGHT DIRECTOR AND AUTO COUPLER POLICY
Do not dispatch an aircraft to a destination forecast to be below 3/4 statute mile visibility or RVR 4000 unless the aircraft has either (a) operable dual flight director systems or (b) one operable flight director and an operable auto coupler. A single flight director with dual display does not satisfy this requirement. |
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PW start procedure
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PW 18% N2 min
position fuel control switch to RUN at maximum motoring: Oil pressure rise: (757) Prior to selecting RUN EGT rise: Within 20 seconds after selecting RUN/RICH N1 Indication: (PW) At EGT rise. (PW) engine reaches stabilized idle within 90 seconds after selecting RUN |
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RR start procedure
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RR 25% N3
Position fuel control switch to RUN at max motoring: Oil pressure rise: (757) Prior to selecting RUN EGT rise: Within 20 seconds after selecting RUN/RICH N1 Indication: (RR) Prior to selecting RUN |
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GE start procedure
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767 15% N2
Position fuel control switch to RUN at max motoring: Oil pressure rise: (767) Prior to stabilized IDLE EGT rise: Within 20 seconds after selecting RUN/RICH N1 Indication: (767) Within 30 seconds after N2 stabilized at IDLE |
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IRS
What information does it give us? |
HATSWAP
Heading Accleration Track Speed Wind Attitude Position |
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IRS
What instruments does it give information to? |
IAFWY
4 I: VSI HSI RDMI ADI 3 A: brake Accel, AntiSkid, ASA 2 F: FCC FMC W WX Radar Y Yaw |
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IRS
What can cause it to flash? |
no bad moves, faults
no input position. bad position input, the aircraft is move or faults |
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IRS's, on battery power for the 757 what lives and dies?
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757
L and C die after 5 minutes R remains |
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IRS's, on battery power for the 767 what lives and dies?
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767
L and C live and R dies after 5 minutes |
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Fire Protection
SYS-Fail Switch/Light |
Is a press to test and
also a reset like the Master Caution to be ready to warn of another failure |
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What happens when you move the gear handle down.
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Press is provided to the actuators
Releases door uplocks light comes on Releases gear uplocks light comes on extends gear |
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What do you see when gear extension is successful.
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3 green and doors and gear lights are off
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What happens when you move the gear handle up.
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Pressure is provided to the up acutuators
Door and gear lights come on then off after uplocks are engaged |
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How many gear position indicators are there?
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2 which are redundant
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TRACTALL
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Thrust
Region Airspeed Bugs Climb Restriction Trim Apu Level Off Log Book |
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B757 Which hydraulics power what brake systems?
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L---Alternate
C---Nothing R---Normal-Reserve-Accum |
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B767 Which hydraulics power what brake systems?
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L---nothing
C---Alternate-Reserve R---Normal-Accumulator |
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The Reserve Brake switch does what?
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Turns on the electric hyd pump.
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B757 and B767 Which hydraulics power what brake systems? (stated in another way.
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Right-Normal
Right-Accumulator Standpipe-Reserve Heavy-Alt |
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How do you establish crew communication?
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Put on oxygen mask
Switch from boom to mask Switch on speaker talk to the other and thumbs up |
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ATM bucks
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Altimeter
Tailwind MELS Bleeds |
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Before top of descent
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A-
I-install approach R-Radios B-Brief A-Approach Check List G-Go around Brief |
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Reserve fuel input on preflight
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Domestic Rules
• Enter alternate + reserves International Rules • (B757) alternate + 6000 lbs • (B767) alternate + 8000 lbs |
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Pilots must not fly an RNAV procedure unless
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Pilots must not fly an RNAV procedure unless it is retrievable by procedure name from the
FMC database and conforms to the charted procedure. |
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Some approaches restrict the use of DA with the statement in the Jeppesen Briefing Strip: “For
uncompensated Baro-VNAV systems, LNAV/VNAV not authorized below -15C or above 48C.” All B767 aircraft have ____? |
uncompensated Baro-VNAV systems
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To avoid unnecessary RAs:
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vertical speed should be reduced to 1000 FPM when within 2000
feet of a level off altitude. |
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The PF must respond immediately to satisfy corrective RAs by:
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disconnecting autopilot and
autothrottles and using positive control inputs in the direction and magnitude TCAS advises. Attempt to visually acquire the conflicting traffic while complying with the RA. |
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The TCAS mode selector should be selected to TA ONLY during the following situations:
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• If one engine is inoperative
• If takingoff or landing at an airport elevation above 5300 feet MSL • During operations beyond ISA +/-27.8°C (50°F) • When required by the MEL or Non-Normal procedure |
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GO-AROUND PROCEDURE
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Push G-A switch and call
“Go-around thrust Flaps 20.” pos rate gear up |
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Single Eng Go around
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Push G-A switch and call
“Go-around thrust Flaps 5.” |
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How many ground carts are required for engine start
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2
3 on the RR during severe cold |
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APU pneumatic output is controlled barometrically.
How and when? |
In climb it shuts off air at 23000.
In descent it restores air at 20000. |