Limitations (Other) Flashcards
Runway Slope
+/- 2%
Maximum Operating Altitude
43,100ft Pressure Altitude
Maximum Takeoff and Landing Altitude
11,000ft pressure altitude
Maximum Tailwind
The capability of the airplane has been satisfactorily demonstrated for
takeoffs and landings with tailwinds up to 15 knotsJD.
RVSM utilising ISFD
Do not fly in RVSM airspace on ISFD alone. The standby altimeter does not meet
RVSM altimeter accuracy requirements.
The maximum demonstrated crosswind for takeoff?
40 knots (gust included)
The maximum demonstrated crosswind component for landing
37 knots (gust included)
Wx radar use near personnel
Avoid weather radar operation when personnel are within the area normally enclosed by the aircraft nose radome.
Prior to takeoff the maximum allowable difference between Captain’s or First Officer’s altitude display and field elevation is?
75 feet
Maximum Taxi Weight
228,383 Kilograms
Maximum Takeoff Weight
227,930 Kilograms
Maximum Landing Weight
172,365 Kilograms
Maximum Zero Fuel Weight
161,025 Kilograms
When the glidepath angle for approach is greater than 3.77 degrees, when must the autopilot be disengaged?
No later than 50 feet below DH/MDA.
Autoland flap and engine limitation?
Autoland capability may be used with flaps 20, 25, or 30, with both engines operative or with one engine inoperative.
What must be displayed on AFDS to autoland?
The autopilot flight director system (AFDS) autoland status annunciation must have LAND 2 or LAND 3 displayed.
Limitation on ACP to establish a SATCOM/cabin conference?
Use of the captains or first officers ACP to establish a SATCOM/cabin conference is prohibited.
Tailwind and Crosswind Ground wind operating envelope?
- 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
The maximum altitude with flaps extended is?
20,000 feet.
Radio Altimeter Flight Restrictions
When operating in U.S. airspace, in the presence of 5G C-Band wireless broadband interference as identified by NOTAM?
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).
Fuel Temperature Limitations
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.
Fuel Loading
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.
GPWS - Look-Ahead Terrain Alerting Limitations?
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.
TCAS Limitations?
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.
