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165 Cards in this Set
- Front
- Back
Max Operating Altitude (767)
|
43,100 ft
|
|
Max Operating Altitude (757)
|
42,000 ft
|
|
Max Takeoff Weight
767 (60K) 767 (56K) 757 |
407,000
360,000 240,000 |
|
Max LandingWeight
767 (60K) 767 (56K) 757 |
320,000
300,000 198,000 |
|
Max Tailwind (Takeoff and Landing)
|
10 Kts
|
|
Max Takeoff Crosswind
Braking Good - Dry Rwy Braking Good - Wet Rwy |
40 kts
25 Kts |
|
Max LandingCrosswind
Braking Good - Dry Rwy Braking Good - Wet Rwy |
40 kts
40 kts |
|
Minimum Cockpit Oxygen
|
1200
|
|
Engine Starter Duty Cycle
Reengagemnet RPM -First Attempt -Second Attempt |
0 N2
0 N2 |
|
Extended Motoring Re-engagement
<5 minutes |
0 N2
|
|
Extended Motoring Re-engagement
>5 and < 10 minutes |
10 minutes cooling
|
|
Extended Motoring Re-engagement
>10 and < 15 |
15 minutes cooling
|
|
Max Continuous mororing engagement
|
15 minutes
|
|
Minimum Oil for engine start
|
15 quarts
|
|
Max Start attempts for APU in 60 minute period
|
3 attempts
|
|
Time between APU start attempts
|
1 minute
|
|
Max Flap/Slats extended altitude
|
20,000 MSL
|
|
Do not use Speed Brake:
IMC VMC |
FAF or 1500 (whichever is lower)
1000 ft AGL |
|
Threshold no-option Fuel
757 767 |
800 lbs
1100 lbs |
|
Min/Max Fuel Temp (Jet A)
|
-37 +49
|
|
Brake Cooling Time
If less than 74 minutes |
OK to Taxi
|
|
Brake Cooling Time
If more than 74 minutes |
Do Not Taxi
Do Not set parking brake |
|
Minimum Tire Pressure-Nose
757 767 |
145 PSI
160 PSI |
|
Minimum Tire Pressure-Main
757 767 |
180 PSI
200 PSI |
|
Autoland-Max Headwind
|
25 Kts
|
|
Autoland-Max Tailwind
|
10 Kts
|
|
Autoland- Max Crosswind (other than CAT II/III)
|
25 Kts
|
|
Autoland-Max Crosswind
CAT II/III |
15 Kts
|
|
Autopilot engaged after takeoff/go around
|
800 ft AGL
|
|
Autopilot use on Single Autopilot approach
|
50 ft below DA/MDA but not less than 50 ft AGL
|
|
Severe Turbulence
10,000 feet and above Below 10,000 Ft |
290 KIAS/.78 Mach
250 KIAS |
|
How does Flaps 1 differ between the 757 and 767
|
757-Flaps & Slats extended
767-Only slats extended. Flaps extend at position 5 |
|
767-300
What EEC modes are available in channel A or B |
EPR
N1 |
|
Which airplane incorporates the PES?
|
767
|
|
What does the PES consist of?
|
HYD motor in R HYD SYS using trapped L HYD SYS fluid (trims at 1/4 rate)
|
|
Which trim system is available using the PES?
|
Only EEC trim switches on yoke.
|
|
767
How many spoiler panels are on each wing? |
6 panels total
|
|
767
How many spoilers are used for roll at low speeds? |
All 6
|
|
767
How many spoilers are used for roll at high speeds? |
4
|
|
767
For spoiler and aileron use, how is low and high speeds determined? |
High/low speed determined in conjunction with aileron lockout speeds.
Note: 5 spoilers on each wing operate as speed brakes in flight regardless of airspeed. |
|
767
When do the outboard ailerons lock and unlock/ |
Lock: Above 280 TAS
Unlock: Below 240 TAS |
|
767 FUEL CONFIG light indicates.....
|
1) Center tank more than 1200 with Center switches OFF
2) Lateral imbalance of 2000 3) either Main below 2200 |
|
The Best vantage point from the cabin when making a visual check of the wing surfaces is from.....
|
757 - 1st window aft of doors 2 L/R
767-60K - 3rd window forward of mid-cabin lavatory |
|
Pitch attitude at touchdown should be.......
|
757- 5-6 degrees
767 - 5-6 degrees |
|
Landing Gear Limit Speeds
Retraction - Extension - |
Retraction-270KIAS
Extension - 270KIAS/,82M |
|
Landing Gear Limit Speeds for Alternate system...
Extension - |
Extension - 250KIAS/.82
|
|
Max ZFW 767-60K
|
288,000
|
|
767-300
what is the backup to prevent uncontrolled engine acceleration? |
If engine exceeds 117% N1 or 110.3% N2, fuel flow is reduced to minimum settung and locked. Flameout will be likely at low altitude
|
|
767-300
Basic components of EEC, and the "flow" from throttle to engine. |
-Dual Channel A &B Full authority
-A&B channels are identical -No Hydromechanical backup -No mechanical linkage between throttle and EEC -1 channel must be operatingh -EEC is "middle man" between Throttle and Engine Fuel Control. |
|
767
When will the Automatic Reserve Brakes and Steering system activate? What is the purpose of this automatic feature? |
When C HTD reservoir drops below 50%
Purpose: Prevents loss of C HYD reserve fluid, should there be any delay in pushing the RESERVE BKS & STRG switch. Reserves dedicated C HYD fluid for C HYD ELEC 1 pump. Pump output will be restricted to Brakes & NWS. |
|
767
Besides low system pressure and during "High Load" activation, when else will the C HYD Air demand pump auto-operate? |
During HMG operation
|
|
Describe the Stall Warning System on the 767.
|
With flaps/slats retracted......
First, stick shaker, then if AOA increases, or stick shaker operates for several seconds, stick pusher activates. (recall the 757 has stick shaker, then Autoslat operation) |
|
767
What should the crew be prepared to see during a HMG only GO-around |
Blanking of Capt HSI and ADI....will need to use STBY instruments.
|
|
767
The Auto feature of the C HYD Air demand pump is inhibited when? |
if Wing A/I is ON
Note: if WING A/I ON, with no high loads, the pump will operate if low system pressure is detected. |
|
767
BLEED light indicates... BLD OVHT light indicates.... |
BLEED: HPSOV failed full open
BLD OVHT: HPSOV closed due to overtemp |
|
767
Number of idle speeds |
Ground & Approach
|
|
767
Which HYD pump operates regardless of switch position, when the RESERVE BKS & STRG switch is activated? |
C HYD 1
|
|
767 inboard ailerons
Why were they designed to be driven down? How far are they driven down |
To change body angle.....better Approach visibility
they are driven down 50% |
|
N1 Breakaway
|
35% N1
|
|
With the wheels on the runway, and the main landing gear struts extended, aft fuselage contact will occur at what pitch attitude?
|
757 - 12.2 degrees
767 - 9.5 degrees |
|
Define abnormal engine start.
|
-No EGT rise within 20 seconds after moving fuel control switch to RUN
-No N1 increase by 40% N2 -No oil pressure increase before fuel control switch to RUN -High initial fuel flow, or EGT rapidly approaching start limit -Hung start - stabilized idle not attained within 90 seconds (757) or 120 seconds (767) -Engine fuel valve, or fuel spar valve fails to open -EICAS engine display disruption |
|
North/South Latitude IRS restrictions
|
Do not operate in IFR conditions, or at night into airports north of 73 North and South of 60 when the APT NAV aids are referenced to MAG NORTH
|
|
STAB TRIM light on indicates.......
|
1) One STAB brake did not release and
2)Trim rate is 1/2 normal rate |
|
UNSCHED STAB TRIM light on indicates.....
|
1)Stab trim movement without signal from switches. Mach/speed trim,
or Stab trim movement opposite of signal from switches, Mach/speed trim, or A/P |
|
RUDDER RATIO light on indicates....
|
1)Ratio failure
2)SYS reverts to full authority 3)HYD flow reduced to prevent damage |
|
TO CONFIG warning activates when......
|
Either engine accelerated to TO thrust, and
-Slats not in T-O position -Flaps not in T-O position -Flaps or slats disagrees with handle -STAB not in TO range -Speed brake lever not in DOWN detent -Parking brake set |
|
With AC power available, which fule pump will the APU automatically start and use regardless of pump switch position?
With APU running in flight, can this pump be turned OFF with the switch? |
L FWD FUEL PUMP
Yes |
|
How is fire detected in the CARGO compartments?
|
1 or 2 fans draw air from compartment through 2 smoke detectors, normally both detectors must detect smoke to activate warning.
|
|
How many fire detector loops on each engine?
On the APU? Are the loops continuously monitored for faults? |
Engine - 2
APU - 2 Engine and APU are continuously monitored for faults Note: If the system has reconfigured for single loop detection, that loop will activate a fire warning. |
|
When are the fire warning bell & Master warning lights for fire inhibited?
|
From nose strut extension to 400RA,
or From nose strut extension plus 20 seconds (Whichever comes first) |
|
During flight, if 1 Cargo fan fails, the other starts automatically. Will ther eba nay cockpit indication?
|
No cockpit indication
|
|
Is the cargo fire detection system continuously monitored for faults?
|
No cargo fire detection is not continuously monitored.
|
|
when is the Cargo system tested for faults?
|
System is tested once at initial power-up, or manual test with fire test switch.
|
|
What and where is the backup source of fuel pressure to start the APU?
When will this backup source operate? |
DC PUMP in the L tank
Auto operates when no AC power is available (with BAT switch ON & APU switch to ON or START. |
|
AUTO SPD BRK light on indicates......
|
-fault in System
-If armed, may not auto extend on LDG -If armed, may extend in FLT. |
|
SPEED BRAKES light on indicates.....
|
-Lever is aft of ARMED and aircraft below 800RA and above 15 RA
-Lever is aft of ARMED and LDG flaps extended above 15 RA |
|
757 FUEL CONFIG light indicates...
|
1) Center tank more than 1200 Center pumps OFF
2) Imbalance of 1800 lbs 3) Either Main tank below 2200 |
|
757
The BLEED light indicates.... |
Bleed closed due to overtemp
|
|
The HI STAGE light indicates...
|
Bleed due to overpressure
|
|
PACK OFF light
|
1) Pack selector is OFF
2) Loss of air to the pack |
|
757
Is the ENG A/I valve located upstream or downstream of the ENG BLEED valve 767..... |
757-Downstream...ENGIN A/I is not available with associated ENG BLEED closed, unless air is provided from another source
767-Upstream - ENG A/I is not depemdant on ENG BLEED valve position |
|
757
What happens if the L RECIRC fan is turned off, or fails in flight? |
The overboard exhaust valve opens, and an OVBD EX VAL OPEN status message is displayed
|
|
Oxygen masks automatically drop at waht cabin altitiude?
|
14,000 ft
|
|
Once activated, how long will Pax O2 last?
|
Approx 12 minutes
|
|
How is Pax O2 shutoff?
|
Cannot be shutoff
|
|
BUS TIE switches in AUTO arms the AC busses to be powered automatically in what system priority?
|
1) Associated GEN
2) APU GEN 3) Opposite GEN |
|
What bus powers both Battery chargers?
|
GRD SERV BUS
|
|
What busses shed during inflight ENG SHUTDOWN?
|
1) Both Utilities
2) All Galleys 3) Plus additionals (cabin lighting etc) |
|
For Autobrakes to engage on RTO...
|
throttles to idle if above 80 kts
|
|
For speed brakes to engage on landing....
|
-Hydraulic pressure to gear tilt actuator
-no tilt is sensed -throttles to idle |
|
If necessary, what enables the DC BTB to operate?
|
Both BUS TIE switches must be in AUTO
|
|
DC FAIL light on IRS MODE SEL panel indicates.....
|
-DC back up power is not available
-IRU will continue to operate normally with AC power |
|
How many Symbol Generators/
|
3
|
|
How many FCC's
|
3
|
|
Why is it a good idea to start the APU before AUTOLAND?
|
Allows BTB to close if one main AC bus fails below 200 RA
|
|
When are the AC bus tie breakers inhibited from closing?
|
APU not operating and below 200 RA during Autoland
|
|
How are the EEC's powered?
|
Engine driven Permanent magnet alternators.
|
|
Max Flaps/Slats extended altitude?
|
20,000
|
|
Minimum oil temperature for take-off?
|
50 C
|
|
ANTISKID light on indicates...
|
-Fault in active Antiskid SYS
-May have partial Antiskid -Light deactivated with PARKING BRAKE set |
|
Number of Hydraulic Standpipes
757... 767.... |
757 - 3 standpipes for reserve fluid
-Left reservoir -PTU -Center reservoir -RAT -Right reservoir - Normal brakes (through reserve system) 767 - 1 standpipe for reserve fluid -Center reservoir - Reserve Brakes & Steering |
|
Purpose of RAT...
When is it armed... When will it deploy... Minimum airspeed using RAT.. |
-Pressurize the flight control portion of teh C HYD SYS
-Armed on the ground at 80 kts, or anytime in flight -Auto deploys with dual engine failure -Good down to 130 kts |
|
What is the purpose of the PTU?
|
Augments L HYD ELEC pump to operate gear, flaps, slats, and NWS
|
|
Landing CONFIG warning activates when....
|
Any landing gear not down and locked and:
-A/C at or below 800 AGL with either throttle in idle, or -Landing Flaps selected |
|
During prolonged Ground operations in icing conditions, how is accumulated engine ice removed?
|
By advancing thrust (one engine at a time) momentarily to 50% n1 every 15 minutes.
|
|
Starter Duty Cycles...
Normal start attempts... Re-engagement RPM.. |
0% N2
Maintenance must be contacted if second start attempt fails |
|
PULL-UP light indicates....
|
excessive terrain closure with gear and flaps not in LDG position,
or Excessive descent rate |
|
757 EQUIP OVHT light illuminated indicates.....
|
FWD supply fan failed
Overboard exhaust valve did not open when L RECIRC fan stopped Smoke detected in cooling system for more than 5 minutes Low airflow in coolong system on the GRD (GRD crew horn sounds) |
|
The 757 has 3 idle speeds...GRD, FLT, and APPR.
When is APPR idle activated? |
Eng A/I ON,
or Flaps beyond 20 |
|
757
What does ENG LIM PROT light indicate? |
N2 is controlling fuel flow paramaters. Automatic limit protection is lost.
|
|
Where are the Engine Overheat detection sensors located?
|
Upper engine/pylon area
|
|
The APU fault light indicates...
|
APU shutdown due to a fault,
or APU fuel valve is not in the proper position |
|
Pulling the APU Fire Shutoff Handle will.....
|
1) Initiate APU shutdown, if auto-shutdown failed, bypassing the 90 second cooldown,
2) Arms the bottle 3) Silences the fire bell 9and external horn) |
|
757
What is the backup to prevent uncontrolled engine acceleration? |
if N2 reaches 105%, the FCU reduces N2 to 85% and locks the engine at that speed.
Throttle control is regained by shutdown & restart of engine. |
|
What does an illuminated FAULT light on the IRS MODE SEL indicate?
If this occurs during flight, is the IRU usable? |
1) Fault in IRU could cause erroneous output
2) Failure of IRU if on during alignment or in ATT mode (If in flight, IRU may be usable in ATT mode) |
|
EMER DOORS light on indicates.....
ACCESS DOORS light on indicates....... |
EMER DOORS
1) Either overwing exit not closed and locked 2) Either wing slide not closed & locked ACCESS DOORS 1)Radar bay door not closed & locked 2) FWD E/E door not closed & locked |
|
With EMER LIGHTS armed, what will activate the emergency lights?
|
1)Power to the associated charging bus is lost.
2) Exit is opened with slide armed |
|
How many overwing exits
757 767 |
757 - 4
767 - 4 |
|
If the PACK OFF and PACK INOP lights are illuminated, this indicates....
|
Pack has shutdown due to excessive compressor outlet temperature
|
|
If only the PACK INOP light is illuminated, this indicates....
|
1) Excessive pack outlet temp
or 2) Fault in AUTO control system |
|
Any PITOT light on indicates....
AOA/TAT light indicates.. |
1) No or improper heat
2)No or improper heat |
|
When are the Center Fuel Pumps normally inhibited from operating?
|
When the associated Engine N2 is less than 50%
|
|
Min Temp for JET A Fuel
Max Temp |
-37C
+49C |
|
Max Tailwind for Takeoff & Landing
|
10 knots
|
|
MACH SPD TRIM light on
|
Fault in SYS
|
|
SPOILERS light on
|
One or more spoiler panels failed to respond when signaled
|
|
A?P DISC light on indicates
|
Disengages by a fault
Control Wheel disconnect |
|
A/T DISC
|
System Fault
Throttle Disconnect A/T ARM switch to OFF raising reverse levers to interlock Engine RPM fall below EEC activation speed Loss of heat to TAT probe or both AOA probes |
|
OVSPD light
|
A?C has exceeded VMO/MMO
|
|
CABIN ALT light
|
cabin has exceeded 10,000
(light goes out at 8500) |
|
767-300 Max takeoff weight
|
407,000
|
|
757 Max takeoff weight
|
240,000
|
|
When is the #2 CTR HYD pump inhibited on the:
757 767 |
757: When only 1 GEN or EXT PWR is supplying electrical PWR and both CTR SYS pump switches are in ON position.
767: When only 1 GEN or EXT PWR is supplying electrical PWR and the other 3 ELEC HYD pumps are operating. |
|
During flight, the RUDDER RATIO light illuminates, what actions automattically occurred.
|
Rudder ratio changer depressurizes to low speed/full authority and actuator depressurizes 1 channel
|
|
During HMG operation, how are the three IRU's powered?
|
L-Left AC transfer bus
C-Hot Battery bus R-Hot battery bus for 5 minutes, then auto shutdown |
|
Which airplane uses Mach/speed trim system?
When does the system operate? When is it inhibited? |
757
Operates 20 seconds after liftoff with no other commands to STAB Inhibited during trim inputs & A/P engagement. |
|
The alternate gear extension gets its fluid from?
Can it be extended without electrical power? |
Left Hydraulic System
Must have electric power |
|
During Alternate Flap/Slat extension, is assymetry protection provided?
|
Is provided for LE Slats, but NOT for TE Flaps
|
|
"Autopilot" Light indicates
|
-the engaged A/P's are operating in a degraded mode, such as:
-loss of G/S or LOC signal -V/S engaged without being selected -AOA exceeding 6 degrees in V/S, ALT CAP or ALT HOLD |
|
757-Which HYD pump operates regardless of switch position when the RESERVE BRAKES switch is activated?
|
R HYD ELEC pump
|
|
ER Aircraft - What buses are powered by the HMG?
|
AC: L & R AC TFR
-STBY AC -Capt FLT INSTR TFR DC: HBB -BB -STBY DC |
|
Flashing ALIGN lights on the IRS MODE SEL panel indicate...
|
1) Fault in alignment process
2)Initial position not entered 3) Excessive disparity between entered & last position recorded in IRU memory 4) A/C is moving before alignment is complete |
|
NON-ER - On the IRS MODE SEL panel, all three ON DC lights illuminated indicate...
|
1) All IRU's on DC Power
2) L and C run 5 minutes then shutdown 3) R operates until dead battery If L and C shutdown, present position not stored in memory |
|
757 - Which modes will the EEC provide thrust limit protection?
|
EPR, N1
No EGT overtemp protection |
|
ER Aircraft - During HMG operation, the Capt RDMI switches to the ______ IRU
|
Center
|
|
Primary and secondary power sources for STBY DC and AC
|
Primary: L main AC & DC
Secondary: Battery |
|
ER Aircraft: Power sources, in priority for STBY AC and STBY DC
|
STBY AC:
1) L AC TFR 2) battery (via static inverter) STBY DC: 1) L main DC 2) HMG 3) Battery |
|
Engine Ignition must be operating during:
|
-takeoff
-Landing -Heavy Precip -MDT or SVR turbulence -Volcanic Ash encounter |
|
The STBY POWER OFF light indicates
|
Either or both STBY BUSES are unpowered
|
|
What will arm the system for ENG START load shedding?
Load Shedding for ENG START How are busses reset? |
1) APU supplying Electrical AND Pneumatics
2) Both Utilities, All galleys 3) Auto-reset |
|
What buses are powered by the Battery & STBY power system?
|
-HBB
-BB -STBY DC -STBY AC |
|
If the VMO flag appears, the VMO pointer moves to ______
|
260 KTS
|
|
At least one triple A/P APPR and Autoland should be made and recorded within the last ____ days to maintain CAT lll status
______ days to maintain CAT ll status |
30
50 |
|
With the YD switch to ON, will an INOP light shut off HYD power to the YD?
|
Yes
|
|
Flap load relief system:
757: with flaps selected to ___, the flaps blow back to ___ 767- With flaps selected to ___ the flaps blow back to ___ |
757: 30 TO 25
767: 30 or 25 to 20 |
|
With the speed brake lever in the ARMED position, the GRD spoilers auto-extend upon LDG if.....
|
-HYD pressure to LDG gear truck tilt actuators
-No-tilt condition on the GRD -Both throttles idle |
|
757 - When is the PTU automatically activated?
When is the PTU inhibited? |
Automatically activated if L ENG fails or L ENG HYD pump pressure is low
Inhibited if R ENG is not operating |
|
Why does the APU need the battery switych to be on, while on the ground, but not in the air?
|
The airplane battery supplies power for APU fire protection and with no other power available on the ground, fire protection would not be available if the battery switch wasn't on.
|
|
The ALTERNATE BRAKE system has all the capabilities of the NORMAL BRAKE System, except:
|
Autobrakes are not available
|
|
ER Aircraft - When will the HMG auto-start?
|
Loss of both main AC buses
|
|
757 - How many spoiler panels on each wing, and how many are used for roll control?
for Speed brakes? |
6 panels each wing
5 used for roll & speed brakes Spoilers 4 and 9 Ground use only |
|
For autobrakes to engage when landing...
|
-Both throttles at idle
-main gear trucks untilt -wheel spinup -airplane pitch 1 degree or less |
|
What will activate the AUTOSLAT system?
Which airplane? |
757 only
1- Slats in T-O position 2 - Left HYD system pressurized 3 - Stall warning Slats extend to LDG position. When the warning ceases, slats retract to T-O position. There is no AUTOSLAT with ALT FLAP system. |
|
If a spoiler panel loses HYD pressure, will the spoiler float, or lockdown?
|
Lock Down
|
|
What is required for the YD to initiate a successful self test?
|
YD switch to ON and 1 IRS in NAV mode
|