10 knots

(FCOM Vol. 1 Rev 2  L.10.2)

Below 25,000' = 270 knots, and above 25,000' = 280 knots or 0.82 Mach (lower) all alt's MM + 15 knots.

(FCOM Vol 1, Rev 2: L.10.2)

Do not operate HF radios during refueling operations.

(FCOM Vol 1: Rev 2: L.10.2)

Avoid weather radar operation when:

1. In a hangar

2. When personnel are within the area normally enclosed by the aircraft nose radome

*Note: The hangar recommendation does not apply to the weather radar test mode.

*This is not a memory item, but is included here to avoid subject duplication with the "familiarity" deck

(FCOM Vol 1 Rev 2: L.10.2)

N702GT-N706GT, N774SA, N775SA:  768,000 lbs   (348,358 kg)

N714SA, N777SA:  768,800 lbs

* These are not listed as limitation memory items but have still been required for memorization.

(FCOM Vol 1 Rev 2: L.10.3)

N702GT-N706GT, N774SA, N775SA: 766,000 lbs (347,451 kg)

N714SA, N777SA: 766,800 lbs

* These are not listed as limitation memory items but have still been required for memorization.

(FCOM Vol 1 Rev 2: L.10.3)

575,000 lbs (260,815 kg)

* These are not listed as limitation memory items but have still been required for memorization.

(FCOM Vol 1 Rev 2: L.10.3)

547,000 lbs (248,115 kg)

* These are not listed as limitation memory items but have still been required for memorization.

(FCOM Vol 1 Rev 2: L.10.3)

1. Do not use the autopilot below 100 radio altitude at airport field elevations above 8,500' (except N704GT)

2. The autopilot must not be engaged below a minimum altitude of 200' AGL, after takeoff.

3. Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged below 200' AGL

(FCOM Vol 1 Rev 2: L.10.3-4)

Do not use FLCH on final approach below 1000' AFE.

(FCOM Vol 1 Rev 2: L.10.4)

1. Headwind: 25 knots

2. Tailwind:  10 knots

3. Crosswind: 25 knots

4. Crosswind CAT II/III: 15 knots

5. Maximum Glideslope: 3.25°

6. Minimum Glideslope:  2.5°

7. Flaps 20 or 30

8. Normal or Single Engine, AFDS must display LAND2 or LAND3

(FCOM Vol 1 Rev 2: L.10.4)

1. Intentional selection of reverse thrust in flight is prohibited

2. Backing the airplane with use of reverse thrust is prohibited

(FCOM Vol 1 Rev 2: L.10.5)

Avoid rapid and large alternating control inputs, especially in combination with large changes in pitch, roll, or yaw (e.g. large side slip angles) as they may result in structural failure at any speed, including below VA.

(FCOM Vol 1 Rev 2: L.10.6)

Maximum altitude with flaps extended = 20,000'

(FCOM Vol 1 Rev 2: L.10.6)

+/- 2%

(FCOM Vol 1 Rev 2: L.10.2)

43,100' pressure altitude

(FCOM Vol 1 Rev 2: L.10.2)

N702GT-N703GT, N705GT-N706GT, N714SA-N777SA:

9,800' pressure altitude

N704GT: 

8,400' pressure altitude

(FCOM Vol 1 Rev 2: L.10.2)

1. Prior to takeoff, maximum allowable difference between Capt or FO altitude display and field elevation is 75'.

2. In the air, 200' difference between CA and FO.

3. Standby altimeter does not meet RVSM accuracy requirements.

(FCOM Vol 1 Rev 2: L.10.2)

(FCOM Vol 1, Rev 2: SP.11.22)

Main door emergency power assists and evacuation slide systems must be armed with the select handle in the ARMED position prior to any aircraft movement.

(FCOM Vol 1 Rev 2: L.10.2)

N714SA, 777SA, N702GT - N706GT:

Do not use SwiftBroadband service for ATC communication.

(FCOM Vol 1 Rev 2: L.10.4)

Maximum and Minimum limits are Red

Caution limits are Amber

(FCOM Vol 1 Rev 2: L.10.5)

1. Maximum fuel temperature 49°C

2. Prior to takeoff min fuel temperature -40°C or 3°C above the fuel freezing point, whichever is higher

3. In-flight minimum fuel temperature must be maintained 3°C or higher above the freezing point of the fuel used

    *Fuel system icing inhibitor additives do not change the min fuel tank temperature limit

(FCOM Vol 1 Rev 2: L.10.5)

Tailwind Limitations During Ground Operation

(Exclusive of Takeoff)

1. Tailwinds and Crosswinds between 30-45 knots limit engine power to a max of 70% N1

2. Avoid thrust levels above that required for normal taxi operation in all tailwinds and crosswinds greater than 45 knots

(FCOM Vol 1 Rev 2: L.10.5)

1. 3 attempts in 60 minutes each (electric and air each)

2. 1 minute between 1st and 2nd start and 2nd and 3rd start (electric and air each)

(FCOM Vol 2:Rev 1: L.10.5)

1. EFB portable keyboard and attaching cable must be stowed for takeoff and landing

2. Excludes N704GT-N706GT (but the panel mounted EFB's are all deactivated at this time)

(FCOM Vol 1 Rev 2: L.10.6)

Do not attempt at latitudes greater than 78° 14.75'

(FCOM Vol 1 Rev 2: L.10.9)

1. Do not modify RNAV procedures

2. If unable to comply, notify ATC for new clearance

3. When on RNAV approach, must go around if "UNABLE RNP" displays and unable to proceed visual

4. Must load RNAV procedure by name from the database.

(FCOM Vol 1 Rev 2: L.10.9)

FAA: RNAV (RNP)ICAO: RNP (AR)Not authorized

(FCOM Vol 1 Rev 2: L.10.10)

Approved fuels:

1. Jet A and Jet A-1 (ASTM-D1655)

2. JP-5 (MIL-DTL-5624)

3. JP-8 (MIL-DTL-93133)

Prohibited fuels:

1. Jet-B

2. JP-4

(think: B4A58)

(FCOM Vol 1 Rev 2: L.10.10)

1. Main tanks must be scheduled to be full if center tank fuel is to be loaded.

2. Center tank may have up to 3000lbs with less than full mains if the center tank fuel + actual zero fuel weight CG limits are observed

*N704GT:  If operating under alternate compliance of AD 2016-11-03, an additional 320kg must be added to the center tank load.

(FCOM Vol 1 Rev 2: L.10.10)

1. Do not use the terrain display for navigation

2. It is prohibited to use look ahead and terrain display within 15 NM of takeoff, approach, or landing when airport or runway are not in the terrain database

(FCOM Vol 1 Rev 2: L.10.10)

Pilots are authorized to deviate from their current ATC clearance to the extent necessary to comply with a TCAS II Resolution Advisory

(FCOM Vol 1 Rev 2: L.10.11)

Flaps 1  -  265 kts          Flaps 5  -  245 kts      Flaps 15  - 230 kts

Flaps 20  - 225 kts         Flaps 25  - 200 kts     Flaps30  - 180 kts

*Note: This is not listed in the limitations section, but has been asked on orals.

(FCOM Vol 2 Rev 2: 9.10.9)

Nominally 235 kts, use PD Takeoff table for the correct tail number to find the max weight.

*Note: This is not a listed in the limitations section, but has been asked on orals.

(FCOM Vol 1 Rev 2: PD.14.2)

38 knots

(FCOM Vol 1 Rev 2: L.10.2)

Must be disconnected below 200 feet on a NON-PRECISION approach but may be disconnected at MDA.

(FCOM Vol 1, Rev 2: L.10.3-4 & NP.21.54)

(QRH, Rev 17: MAN.2.5-6)

Temperature 10°C or less with:

1. Visible moisture (clouds, fog with visibility of one statute mile (1600 m) or less, rain, snow, sleet, ice crystals, and so on) is present

2. Ice, snow, slush, or standing water is present on the ramps, taxiways, or runways

(FCOM Vol 1, Rev 2: SP.16.2)

When Both are True:

1. Temperature 3°C or lower.

2. Anti-Ice on ground required.

(FCOM Vol 1, Rev 2: SP.16.4)

Check that the area behind the airplane is clear.  Then Run-up to a minimum of 50% N1 for approximately 1 second duration every 60 minutes or less.

(FCOM Vol 1, Rev 2: SP.16.4)

1 second duration every 60 minutes or less.

(FCOM Vol 1, Rev 2: SP.16.4)

Condition: 

Cabin altitude is excessive

1.  Don the oxygen masks.

2.  Establish crew communications.

3.  Check the cabin altitude and rate.

4.  If the cabin altitude is uncontrollable (Uncontrollable = the vents are closed and altitude is still increasing)

Then:

SUPRNMRY OXYGEN switch...…Push to ON and hold for 1 second

Without delay, descend to the lowest safe altitude or 10,000 feet, whichever is higher.

To descend (without automation):

Move the thrust levers to idle.

Extend speed brakes.

If structural integrity is in doubt,

limit airspeed and avoid high maneuvering loads.

Descend at VMO/MMO

To descend (with automation):

spin down altitude in altitude window

Select FLCH

Extend speed brakes

speed intervene

adjust altitude in altitude window.

(QRH  2.1  Rev 17)

Condition:

On the ground, an aborted engine start is needed.

1.  FUEL CONTROL switch (affected side) ............... CUTOFF

(QRH 7.1 Rev. 17)

Condition:

Engine speed for both engines is below idle.

1.  FUEL CONTROL switches (both)..........CUTOFF, then RUN

2.  RAM AIR TURBINE switch.........Push and hold for 1 second

(QRH 7.2  Rev 17)

Condition:

During a ground start, one of these occurs:

Autostart did not start the engine, or

Fuel control switch is in RUN at low engine RPM with the autostart switch OFF

1.  FUEL CONTROL switch (affected side) ................ CUTOFF

(QRH 7.4 Rev 17)

Condition:

One or more of these occur:

Eng indications are abnormal, or

Eng indications are quickly nearing or show an exceedance, or

Abnormal Eng noises are heard, possibly with airframe vibration, or

There is no response to thrust lever movement or the response is abnormal, or

Flames in the engine inlet or exhaust are reported

1.  A/T ARM switch (affected side).........Confirm........OFF

2.  Thrust lever (affected side).........Confirm.........Retard until engine indications stay within limits or the thrust lever is at idle

(QRH 7.5 Rev 17)

Condition:

One or more of these occur:

Airframe vibrations with abnormal engine indications

Engine separation

1. A/T ARM switch (affected side)..................Confirm...OFF

2. Thrust lever (affected side)........................Confirm....Idle

3. FUEL CONTROL switch (affected side) .. Confirm .. CUTOFF

4. Engine fire switch (affected side)..............Confirm....Pull

(QRH 7.10 Rev 17)

Condition:

Fire is detected in the engine

1. A/T ARM switch (affected side)....Confirm....OFF

2. Thrust lever (affected side)....Confirm....Idle

3. FUEL CONTROL switch (affected side) ... Confirm ... CUTOFF

4. Engine fire switch (affected side)....Confirm....Pull

5. If the FIRE ENG message stays shown:

Engine fire switch (affected side)......Rotate to the stop and hold for 1 second

6. If after 30 seconds, the FIRE ENG message stays shown:

Engine fire switch (affected side)....Rotate to the other stop and hold for 1 second

(QRH 8.2 Rev 17)

Condition:

One of these occurs:

Stabilizer movement without a signal to trim

The stabilizer is failed

1.  STAB cutout switches (both).............................CUTOUT

2.  Do not exceed the current airspeed.

(QRH Rev 17: 9.1)

Condition:

Airspeed or Mach indications are suspected to be unreliable.  (Items which can indicate unreliable airspeed are listed in the Additional Information section of the QRH.)

Objective:

To identify a reliable airspeed indication, if possible, or to continue the flight using the Flight With Unreliable Airspeed table in the Performance Inflight chapter.

1. Autopilot disengage switch......Push

2. A/T ARM switches (both)..........OFF

3. F/D switches (both).....................OFF

4. Set the following gear up pitch attitude and thrust:

Flaps extended....10 degrees and 85% N1

Flaps up..................4 degrees and 70% N1

(QRH 10.1  Rev. 17)