One forward and one aft entry or service door on opposite sides open
at least one A/C pack or equivalent ground cooling operating.
757 Equipment Cooling Requirements 41 to 49C
At least one A/C pack or equivalent ground cooling operating.
757 Equipment Cooling Requirements More than 49C
Two A/C packs or equivalent ground cooling oprerating
On takeoff do not engage autopilot CWS or CMD below
500 feet AGL
When conducting a non-precision instrument approach, the flight crew maynot use an autopilot at an altitude more than
50 feet below the approved minimum descent altitude (MDA)
The flight director has not been assessed in any abnormal configuration exceptthat used in a single engine approach.
It may be used in these configurationsbut must be closely monitored.
Use of aileron trim with the autopilot engaged is
Do not use the autopilot below 100 feet radio altitude at airport pressure altitudes above
The autothrottle must not be used in a
single engine approach
Blue Sky Network D1000(A) SATCOM system is not approved for use for
Air Traffic Services (ATS) communication.
Blue Sky Network D1000(A) SATCOM system is not authorized to substitute or supplement the existing
High Frequency (HF) or Very High Frequency (VHF) communications systems for ATS operations.
Do not extend speed brakes in flight when wing flaps are at position
25 or 30
Do not use speed brakes in flight below
800 feet AGL
Do not extend flaps above
Avoid rapid and large alternating control inputs, especially in combinationwith large changes in pitch, roll, or yaw (e.g. large sideslip angles), as they mayresult in structural failure at any speed, including
757 Maximum allowable fuel weight: Main tanks
15,450 lbs ea.
757 Maximum allowable fuel weight: Center Tanks
757 Maximum allowable fuel weight: Total
767 Maximum allowable fuel weight: Main Tanks N120DL/N123DL
43,097 lbs ea.
767 Maximum allowable fuel weight: Center Tanks N123DL/N120DL
32,376 lbs *
* Maximum of 22,000 lbs (10,000 kg) with less than full main (wing) tanks.
767 Maximum allowable fuel weight: Total N120DL/N123DL
767 Maximum allowable fuel weight: Main Tanks N763BD/N637TW/N125RD/N764BK
19,548 kg ea.
767 Maximum allowable fuel weight: Center Tanks N763BK/N637TW/N125RD/N764BK
38,646 kg *
* Maximum of 22,000 lbs (10,000 kg) with less than full main (wing) tanks.
767 Maximum allowable fuel weight: Total N763BD/N637TW/N125RD/N764BK
Maximum fuel imbalance 757:
884 Kg / 1,950lbs.
Maximum fuel imbalance 767:
1,134 kg / 2,500 lbs
757 / 767 Maximum fuel temperature Jet A, JetA1, JP-5, JP-8
757 Maximun fuel temperature JetB, JP-4
767 Maximun fuel temperature JetB, JP-4
757 Minimum fuel temperature:
-45C or 3C above freeze point
767 Minimum fuel temperature:
-43C or 3C above freeze point, whichever is higher
757 Main Tank Maximum fuel with less than full main wing tanks.
2,000 lbs (907kg)
767 Main Tank Maximum fuel with less than full main (wing) tanks.
22,000 lbs (10,000 kg)
With fuel jettison system installed (N763TW, N125RD, N764RD) no less than
10,300 lb (4,672kg) of fuel must be in main tanks.
Do not jettison fuel with
flap position 25 or 30 (N637TW, N125RD)
757/767 Center tank fuel pump switches must not be "ON" unless
personnel are available in the flight deck to monitor low PRESS lights
767/757 For ground operations prior to engine start: The center tank fuel pump switches must not be positioned ON unless
the center tank contains usable fuel. With center tank fuel pump switches ON, verify both center tank fuel pump low PRESS lights are illuminated and EICAS CTR L FUEL PUMP and CTR R FUEL PUMP messages are displayed.
757/767 For ground operations after engine start and flight operations:The center tank fuel pump switch must be selected OFF when
the respective CTR L FUEL PUMP or CTR R FUEL PUMP messages displays. Both center tank fuel pump switches must be selected OFF when either the CTR L FUEL PUMP or CTR R FUEL PUMP message displays if the center tank is empty. During cruise flight, both center tank pump switches may be reselected ON whenever center tank usable fuel is indicated.
757/767 De-Fueling And Fuel Transfer When transferring fuel or de-fueling center or wing tanks, the fuel pump low PRESS lights must be monitored and the respective fuel pump switches positioned to
"OFF" at the first indication of low pressure. Prior to transferring fuel or de-fueling, conduct a lamp test of the respective fuel pump low PRESS lights.
Intentional dry running of center tank fuel pump (CTR L PUMP or CTR R FUELPUMP message on EICAS) is
757 Defueling main wing tanks with passengers onboard is prohibited if maintank fuel pumps are powered. De-fueling center wing tank with passengers onboard is prohibited if the center wing tank fuel pumps are powered with the automatic center tank fuel pump power removal system inhibited. Fuel may betransferred from tank to tank, or the aircraft may be de-fueled with passengers onboard, provided fuel quantity in the tank from which fuel is being trans-ferred is maintained above
2,000 pounds (900 kilograms).
757/767 Fuel Usage (No Center Tank Fuel):
Use tank-to-engine fuel feed for takeoff and landing with all operable main tank boost pumps ON and the crossfeed valve(s) CLOSED.
757 Normal Procedures The center tank fuel pump switch(es) must be selected OFF at
the first indication of fuel pump low pressure any time during the flight. This includes low pressure indications that may occur because of pitch attitude
757 Takeoff and Initial ClimbThe center tank fuel pumps must be OFF for takeoff if center tank fuel is less than
5,000 pounds (2,300 kilograms) with the airplane ready for initial taxi. Both center tank fuel pumps should be repositioned ON above 10,000 feet or after the pitch attitude has been reduced to begin acceleration to climb speed, if more than 1,000 pounds (500 kilograms) remain in the center tank.
757 Climb, Cruise and DescentBoth center tank fuel pump switches must be selected OFF when center tankfuel quantity reaches approximately
1000 pounds (500 kilograms) during climb, cruise, or descent. For airplanes not equipped with a center tank scav-enge system, this 1,000 pounds (500 kilograms) of center tank fuel may only beused in a low fuel situation.
NOTE:In cruise flight, center tank fuel may be reduced to approximately 800 pounds (400 kilograms) as necessary to extinguish the FUEL CONFIG light and EICAS "FUEL CONFIG" message. This allows the FUEL CONFIG alert to activate for fuel imbalance or low fuel situations.
757 FUEL CONFIG Indication. The FUEL CONFIG light will illuminate when thereis fuel in the center tank that exceeds 1,200 pounds (600 kilograms) and thecenter tank fuel pump switches are OFF. Do not accomplish the FUEL CONFIG-URATION non-normal checklist prior to or during takeoff with less than 5,000pounds (2,300 kilograms) of fuel in the center tank, unless there is an imbal-ance between main tanks or fuel is low in either main tank.
After canceling theFUEL CONFIG message, monitor fuel quantity indications and accomplish theappropriate procedure or checklist if a main tank imbalance or main tank lowfuel quantity situation occurs.
757 Non-Normal Procedures
Low Fuel. In a low fuel situation, both center tank pumps may be
selected ONand all center tank fuel may be used regardless of the amount of fuel remain-ing in the tank.
757 Non-Normal Procedures
Pump Failure. If a center tank fuel pump fails with fuel in the center tank,
accomplish the FUEL PUMP non-normal checklist.
757 Additional Information
Fuel Loading. For the time period that AD 2002-19-52 and AD 2002-24-51 arein effect, the zero fuel gross weight of the airplane plus the weight of centertank fuel may exceed the maximum zero fuel gross weight by up to 5000pounds (2300 kilograms) for takeoff, climb, cruise, descent and landing, pro-vided
that the effects of balance (CG) have been considered.
WARNING:Do not reset a
tripped fuel pump circuit breaker.
The fuel designation is per Rolls-Royce O.I. F-211 (535-E4) –B, Appendix 2. Thefollowing fuels and mixtures thereof are approved for use:
Jet A, JetA-1, JP-4*, Jet B*, JP-5, JP-8
*Use of JP-4/JET B is prohibited when modified or intermixed enginefuel controls are installed. The lower refueling station access panel will be placarded "DO NOT USE JP-4/JET B FUEL."
757 Load main tanks equally 1. If main tanks are full and more fuel is required,
load the center tanks.
907 Kg (2,000 lbs) of fuel may be loaded in the centertank with less than full wing tanks, provided the weight of fuel in the centertank plus actual ZFW does not exceed maximum ZFW, and balance limits areobserved.
757 When defueling center or main tanks, the Fuel Pump Low Pressure indicationlights must be monitored and the fuel pumps positioned Off at
the first indi-cation of fuel pump low pressure.
757 Intentional dry running of a center tank fuel pump (DCTR L FUEL PUMP or CTRR FUEL PUMP message displayed on EICAS) is
Defueling with passengers on board is
Perform an operational check of the fuel crossfeed valve(s) during
the last hour of cruise flight during each extended range operation
The crossfeed valve(s) may be OPEN to
correct fuel imbalance
OPEN the cross-feed valve
for minimum fuel operation
The engine anti-ice must be ON during all ground and flight operations whenicing conditions exist or are anticipated, except during climb and cruise whenthe temperature is below –40°C SAT. Prior to descent in visible moisture andTAT less than 10° C, including SAT less than -40° C, nacelle anti-ice switch mustbe in the
Note: Do not rely on airframe visual icing to turn engine anti-ice on.
Use the temperature and visual moisture criteria specified in this section.Delaying the use of engine anti-ice until ice buildup is visible from thecockpit may result in severe engine damage and/or flameout.
Icing conditions exist when:
Icing conditions exist when OAT is 10°C or below during ground operations, takeoff, initial climb or go-around and:
• visible moisture (clouds, fog with visibility less than one mile, rain, snow, sleet, ice crystals) is present, or
• standing water, ice, slush, or snow is present on the ramps, taxiways, or runwaysIce, Rain and Snow
Aircraft equipped with CF6-80A (N120DL and N123DL)
Prior to reducing thrust for descent in visible moisture and TAT less than 10oC,including SAT less than -40oC,
nacelle anti-ice switch must be in the ON posi-tion. At or below 22,000 ft., wing anti-ice selector must be in the ON position. When these icing condition (visible moisture and TAT less than 10C, including SAT less than -40C) are no longer present or anticipated, place the nacelle and wing anti-ice selectors in the OFF (or AUTO) position.
Landing gear operation (extend/retract)
270 knots / .82M
Landing gear extended:
270 knots / .82M
Landing gear extended with alternate system:
250 knots / .75M
With a single operational FMC, during VOR approaches, one pilot must have raw data from the VOR associated with the approach displayed on the RDMI, RMI or HSI in the VOR mode,
no later than the final approach fix.
Pilots are authorized to deviate from their current ATC clearance to the extent necessary to comply with a
TCAS II RA.
The pilot should not initiate evasive maneuvers using information from the traffic display only or on a traffic advisory (TA) only without
visually sighting the traffic.
Compliance with TCAS resolution advisories (RA) is required unless the pilot
considers it unsafe to do so
Maneuvering opposite to a RA (especially a RA involving altitude crossing) is extremely hazardous and PROHIBITED unless it is
visually determined to be the only means of assuring safe separation
All TCAS RAs must be flown
Do not follow flight director commands while performing an
When the TCAS II voice message “CLEAR OF CONFLICT” is announced the pilot must promptly return to the
If the fail light is illuminated on the TCAS / Mode S control panel,
select the alternate transponder (position “1” or “2”) on the TCAS / Mode S control panel.
757 The flight crew must close the pneumatic isolation valve except when opened for
airconditioning on the ground, engine start or emergency / abnormal operation of the airconditioning / anti-ice systems.
The APU starter duty cycle is a maximum of three consecutive starts or attempts within a
Main door emergency evacuation slide systems must be armed and engage-ment of each girt bar with the sill fitting verified prior to taxi, takeoff, and landing whenever
passengers are carried.
The cabin pressurization system must be operable at takeoff whenever
cargo is carried in the lower cargo compartment.
GE CF6 80 A2
P&W PW4056, PW4060
MAX THRUST TAKEOFF
Aircraft N120DL or N123DN
may not depart any airport at a weight heavier than that listed in the APD for the airport runway and ambient conditions plus 8°C assumed temperature. All takeoffs will be reduced by at least 8°C.(Assumed temperature = ambient + 8°C minimum).Normal (reduced) thrust takeoff is still prohibited anytime the following condi-tions are present:
• Runways are contaminated or slippery.
• Anti-skid system is inoperative.
• The aircraft has been anti-iced.
• A Special Departure Procedure specifies full thrust for takeoff.
• An MEL or COM restriction requires max thrust.
NOTE:Thrust settings may be increased to maximum N1 at any timeduring takeoff if needed.If actual conditions demand MAX Thrust Takeoff,
all maximum thrust takeoffsmust have an approval from Flight Operations upper management. This doesnot apply to emergency use of maximum thrust.Any max thrust takeoffs required by our maintenance program must be coor-dinated and approved by Flight Operations upper management.
757 EGT limit Takeoff
850 C Five Minutes
767 CF6 EGT limit Takeoff
941 C Five Minutes
767 PW4056/4060 EGT limit Takeoff
650 C Five Minutes
757 EGT Maximum Continuous
795 C Continuous
767 CF6 EGT Maximum Continuous
895 C Continuous
767 PW4056/4060 EGT Maximum Continuous
625 C Continuous
757 EGT Starting Ground and Flight"
CF6 767 EGT Starting Ground and Flight
750 C Momentary, 2 Sec.
PW 4056/4060 EGT Starting Ground and Flight
535 C Momentary, 2 Sec.
757 EGT Overtemperature
870 C 20 Seconds
The flight crew shall not blank Engine Vibration Display
Maximum and minimum limits:
The engine limit display markings on EICAS may be used to determine compliance with the maximum and minimum limits and precautionary ranges. If EICAS markings show more conservative limits than those specified above
limit markings shown on EICAS must be observed.
Engine Ignition On for
takeoff, landing and turbulence
NOTE: Continuous ignition is automatically provided in icing conditions when engine anti-ice is on.
757 Engine Starter
Normal Duty Cycle:
Up to two minutes continuous then run down to zero N3 followed by;
Up to a further two minutes continuous operation then run down to zero for N3 followed by;
Up to a further two minutes continuous operation then run down to zero N3
and allow to cool for 15 minutes.
757 Extended Duty Cycle:
Up to four minutes continuous operation followed by 15 minute wait.
757 Re-engagement Speed:
"0% N3—Recommended 0-20% N3—Normal Re-engagement is not recommended above 20% N3 except in case of fire.
Re-engagement above 30% N3 may result in starter or gearbox damages.
767 Engine Starter Normal Duty Cycle:
Continuous for 5 minutes.
Cool for 30 seconds per minute of operation.
After 2 consecutive 5 minute cycles, cool the starter for 10 minutes prior to each subsequent starter duty cycle.
767 Engine Starter Extended duty cycle:
Zero to five minutes on--let N2 run down to zero before re-engaging starter.
Five to ten minutes on--followed by a ten minute cooling period.
Ten to fifteen minutes maximum on--followed by a fifteen minute cooling period.
767 Engine Starter reengagement speed:
0% N2 Recommended.
0-20% N2 Normal.
30% N2 permissable for purging fuel or to clear a fire.
NOTE: Re-engagement above 30% N2 may result in starter or gearbox damage
Maximum oil temperature unrestricted use:
Minimum oil temperature for starting:
Minimum oil temperature for advancing throttles:
Operate engines at taxi thrust settings for a minimum of:
five minutes prior to applying takeoff thrust.
Operate the engines at idle thrust for a minimum of three minutes prior to
shutdown following reverse thrust usage.
Do not use the terrain display for
The use of look-ahead terrain alerting and terrain display functions are prohibited during
The use of look-ahead terrain alerting and terrain display functions are prohibited with 15 nm and approaching to land at an airport not
contained in the GPWS terrain database
If GPS is not installed:
The look-ahead terrain alerting and terrain display functions must be inhibited by selecting the TERR OVRD switch to OVRD if:
operating outside the United States National Airspace and the FMS data- base and charts are not referenced to the WGS-84 reference datum, unless the FMS has been found to be suitable for navigation in that airspace, or
the FMS is operating in IRS NAV only.
For takeoff and if FMS position updating is not accomplished,
verify actual runway position by ensuring that, with the 5 or 10 nm range selected on the EFIS control panel, the aircraft symbol is displayed at the appropriate point on the runway symbol.
Verify that an operational check of the Flight Deck Access System has been accomplished according to approved procedures