Limitations (Other)

Question 1

Runway Slope

Answer 1

+/- 2%

Question 2

Maximum Operating Altitude

Answer 2

43,100ft Pressure Altitude

Question 3

Maximum Takeoff and Landing Altitude

Answer 3

11,000ft pressure altitude

Question 4

Maximum Tailwind

Answer 4

The capability of the airplane has been satisfactorily demonstrated for
takeoffs and landings with tailwinds up to 15 knotsJD.

Question 5

RVSM utilising ISFD

Answer 5

Do not fly in RVSM airspace on ISFD alone. The standby altimeter does not meet
RVSM altimeter accuracy requirements.

Question 6

The maximum demonstrated crosswind for takeoff?

Answer 6

40 knots (gust included)

Question 7

The maximum demonstrated crosswind component for landing

Answer 7

37 knots (gust included)

Question 8

Wx radar use near personnel

Answer 8

Avoid weather radar operation when personnel are within the area normally enclosed by the aircraft nose radome.

Question 9

Prior to takeoff the maximum allowable difference between Captain’s or First Officer’s altitude display and field elevation is?

Answer 9

75 feet

Question 10

Maximum Taxi Weight

Answer 10

228,383 Kilograms

Question 11

Maximum Takeoff Weight

Answer 11

227,930 Kilograms

Question 12

Maximum Landing Weight

Answer 12

172,365 Kilograms

Question 13

Maximum Zero Fuel Weight

Answer 13

161,025 Kilograms

Question 14

When the glidepath angle for approach is greater than 3.77 degrees, when must the autopilot be disengaged?

Answer 14

No later than 50 feet below DH/MDA.

Question 15

Autoland flap and engine limitation?

Answer 15

Autoland capability may be used with flaps 20, 25, or 30, with both engines operative or with one engine inoperative.

Question 16

What must be displayed on AFDS to autoland?

Answer 16

The autopilot flight director system (AFDS) autoland status annunciation must have LAND 2 or LAND 3 displayed.

Question 17

Limitation on ACP to establish a SATCOM/cabin conference?

Answer 17

Use of the captains or first officers ACP to establish a SATCOM/cabin conference is prohibited.

Question 18

Tailwind and Crosswind Ground wind operating envelope?

Answer 18

• for crosswinds greater than 40 knots, limit thrust to a setting normally used for taxi (45% N1)
• with a tailwind component greater than 5 knots and winds greater than 35 knots, limit thrust to a setting normally used for taxi (45% N1)
• for winds greater than 55 knots, limit engine thrust to idle

Question 19

The maximum altitude with flaps extended is?

Answer 19

20,000 feet.

Question 20

Radio Altimeter Flight Restrictions
When operating in U.S. airspace, in the presence of 5G C-Band wireless broadband interference as identified by NOTAM?

Answer 20

The following are prohibited;
* Instrument Landing System (ILS) Instrument Approach Procedures (IAP) SA CAT I, SA CAT II, CAT II and CAT III;
* Required Navigation Performance (RNP) Procedures with Authorization Required (AR), RNP AR IAP;
* Automatic Landing operations;
* Manual Flight Control Guidance System operations to landing/head-up
display (HUD) to touchdown operation;
* Use of Enhanced Flight Vision System (EFVS) to touchdown under 14
CFR 91.176(a).

Question 21

Fuel Temperature Limitations

Answer 21

Maximum tank fuel temperature at takeoff is 49° C (120° F) for Jet A, Jet A-1.
Tank fuel temperature prior to takeoff must not be less than -29° C
In-flight tank fuel temperature must be maintained at least -42° C, as well as 3° C above the freezing point of the fuel being used. The use of Fuel System Icing
Inhibitor additives does not change the minimum fuel tank temperature limit.

Question 22

Fuel Loading

Answer 22

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

Note: The center tank may contain up to 10000 kilograms of fuel with less than full main tanks provided center tank fuel weight plus actual zero fuel weight does not exceed the maximum zero fuel weight, and center of gravity limits are observed.

Question 23

GPWS - Look-Ahead Terrain Alerting Limitations?

Answer 23

Do not use the terrain display for navigation.

The use of look-ahead terrain alerting and terrain display functions are prohibited within 15 NM of takeoff, approach or landing at an airport or runway not contained in the GPWS terrain database.

Question 24

TCAS Limitations?

Answer 24

Pilots are authorized to deviate from their current ATC clearance to the extent necessary to comply with a TCAS resolution advisory. Evasive maneuvers must not be based solely on information from the traffic display or traffic advisory (TA) without visually sighting the traffic.