Aircraft Operations and Regulations
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Questions and Answers

What is the minimum dispatch pressure (PSI) required for passenger oxygen when departing from Hong Kong to Europe, assuming a temperature of 21°C?

  • 1100
  • 1500
  • 1600 (correct)
  • 1300

Under what condition is the use of look-ahead terrain alerting and terrain display functions prohibited?

  • Within 15 NM of takeoff, approach, or landing at an airport or runway not contained in the GPWS terrain database. (correct)
  • Within 25 NM of takeoff, approach, or landing at any airport.
  • Only during night operations.
  • When the visibility is less than 1 mile.

If a pilot receives a TCAS II Resolution Advisory (RA), what action is the pilot authorized to take?

  • Inform ATC of the RA but maintain the current ATC clearance.
  • Deviate from the current ATC clearance to the extent necessary to comply with the TCAS II RA. (correct)
  • Request clarification from ATC before taking any action.
  • Comply with the RA only if it does not conflict with existing ATC instructions.

What is the minimum passenger oxygen dispatch pressure required when departing from Europe at 21°C?

<p>1600 PSI (D)</p> Signup and view all the answers

A flight is departing from Hong Kong to a destination in Southern Asia. According to the table, what is the minimum dispatch pressure required for passenger oxygen at 21°C?

<p>1100 PSI (C)</p> Signup and view all the answers

What is the maximum number of APU start attempts permitted within a 60-minute period for both the electric starter motor and the air turbine starter?

<p>3 (D)</p> Signup and view all the answers

What is the minimum waiting time required between the second and third APU start attempts when using an air turbine starter?

<p>1 minute (A)</p> Signup and view all the answers

Which flight control configuration is required during takeoff?

<p>Normal flight control mode (C)</p> Signup and view all the answers

What is the operational advice regarding the use of ground maneuver cameras during approach?

<p>They should not be used. (A)</p> Signup and view all the answers

What is the maximum altitude at which flap operation is permitted?

<p>20,000 feet (D)</p> Signup and view all the answers

An aircraft (HNE - HNK, HNS - HNX) is being prepared for a flight where center tank fuel is required. What is the minimum additional reserve fuel that must be added to the center tank fuel load?

<p>320 kg (B)</p> Signup and view all the answers

An aircraft (HNR, ΚΡΑ - KQZ) has a total main tank fuel of 45,000 kg. What is the maximum fuel imbalance allowed between the main tanks for takeoff?

<p>Between 1,360 kg and 2,041 kg, determined by linear interpolation. (C)</p> Signup and view all the answers

What action should be taken if the fuel density is outside the range of 0.7309 and 0.8507 kg/litre?

<p>The flight must not continue until the fuel density is within limits. (C)</p> Signup and view all the answers

An aircraft (HNE - HNK, HNS - HNX) has a zero fuel weight that is close to the maximum allowable. Under what condition can the center tank contain fuel even if the main tanks aren't full?

<p>The center tank can contain up to 1360 kilograms of fuel 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. (C)</p> Signup and view all the answers

An aircraft (HNR, ΚΡΑ - KQZ) has main tanks containing 50,000 kg of fuel. What is the maximum allowable fuel imbalance for takeoff?

<p>Between 1,360 kg and 2,041 kg, calculated by linear interpolation. (D)</p> Signup and view all the answers

What is the highest latitude at which ADIRU alignment can be attempted, according to the AFM limitations?

<p>78 degrees, 14.75 minutes (D)</p> Signup and view all the answers

Under what condition are all flight operations using magnetic heading or track angle prohibited?

<p>When the loaded ADIRU MagVar table errors exceed 5 degrees. (C)</p> Signup and view all the answers

During an autopilot/flight director ILS approach, what is the maximum allowable error in the ADIRU MagVar table for operations using magnetic north referenced courses or bearings?

<p>3 degrees (A)</p> Signup and view all the answers

For which series of 777-300ER aircraft are MagVar 2015 tables installed?

<p>KPA - KQZ (D)</p> Signup and view all the answers

What action is required when the destination's reported temperature is below the minimum published temperature for the approach?

<p>Instrument approach operations are prohibited unless manual temperature compensated barometric altitude corrections are applied. (C)</p> Signup and view all the answers

Under what circumstances is limiting engine power to a maximum of 70% N1 recommended for ground operations?

<p>When operating in tailwinds or crosswinds between 30 and 45 knots. (A)</p> Signup and view all the answers

What is the procedure following a rejected takeoff (RTO) where thrust reversers were deployed?

<p>Takeoff is prohibited until maintenance action is complete. (A)</p> Signup and view all the answers

What must be done if there is no published minimum temperature for the approach?

<p>Apply manual temperature compensated barometric altitude corrections as specified by the local regulatory authority. (C)</p> Signup and view all the answers

What action should a Commander take after deploying thrust reversers during a rejected takeoff (RTO)?

<p>Contact Maintenance Control to determine whether a maintenance inspection is required before a subsequent takeoff. (C)</p> Signup and view all the answers

What is the impact of cold temperatures on barometric altitudes if not properly compensated for?

<p>It does not assure obstacle clearance. (A)</p> Signup and view all the answers

What functionality of the Flight Management System (FMS) is mentioned in the context of approach barometric altitude temperature compensation?

<p>The Flight Management System does not provide an automatic approach barometric altitude temperature compensation function. (A)</p> Signup and view all the answers

What restriction applies to the intentional use of reverse thrust during flight?

<p>Intentional selection of reverse thrust in flight is prohibited. (C)</p> Signup and view all the answers

During negative G operation, what is the maximum time allowed for oil pressure to be less than 10psid?

<p>15 seconds. (A)</p> Signup and view all the answers

During takeoff with an HNE engine, under what condition is an EGT of 900°C permitted for 10 minutes?

<p>Following engine failure. (D)</p> Signup and view all the answers

What is the maximum N2 compressor rotor speed permitted for an aircraft with HNE engines?

<p>105.0% (A)</p> Signup and view all the answers

An aircraft with KQZ engines experiences an in-flight engine start. What is the maximum permissible EGT?

<p>825°C with no time limit. (A)</p> Signup and view all the answers

An aircraft equipped with HNR engines is operating below 17,000 feet. What is the maximum EGT permitted during takeoff and its corresponding time limit?

<p>1095°C for 30 seconds. (A)</p> Signup and view all the answers

What operational consideration should pilots be aware of regarding the minimum oil pressure for HNE engines?

<p>The minimum oil pressure is 25 psid at Idle RPM. (D)</p> Signup and view all the answers

Which of the following scenarios requires contacting Operations Engineering via IOC for a sector-specific oxygen dispatch pressure calculation?

<p>When oxygen requirements are not explicitly covered in the provided tables or special cases necessitate further reduction of minimum dispatch pressure. (C)</p> Signup and view all the answers

What is the primary reason for the lower minimum dispatch pressure requirements for the 777-300ER compared to the 777-300?

<p>The 777-300ER aircraft are fitted with two crew oxygen bottles, increasing the total available oxygen. (A)</p> Signup and view all the answers

A 777-300 aircraft is preparing for departure from Hong Kong to Northern Asia at 21°C. What is the difference in minimum dispatch pressure compared to a flight from Hong Kong to Europe, both at 21°C?

<p>No difference; the minimum dispatch pressure is the same for both routes. (C)</p> Signup and view all the answers

If a 777-300ER is departing from North America at 21°C with a planned route that includes multiple destinations within North America, what is the lowest acceptable crew oxygen dispatch pressure according to the table?

<p>900 PSI, as this covers both North America and destinations within North America. (C)</p> Signup and view all the answers

A flight crew is preparing a 777-300 for departure from Europe. The current temperature is 16°C, but the listed minimum dispatch pressure of 1300 PSI is for 21°C. How should the crew proceed?

<p>Refer to SP1 - Oxygen - Minimum Dispatch Pressures - Temperature Correction to adjust the pressure accordingly. (B)</p> Signup and view all the answers

Under what condition is the use of engine anti-ice prohibited when the OAT or TAT exceeds 10 degrees C?

<p>Regardless of icing conditions. (A)</p> Signup and view all the answers

What should a pilot do if the primary ice detection system is inoperative and icing conditions are suspected?

<p>Utilize the temperature and visual moisture criteria specified in the AFM to determine when to activate engine anti-ice. (D)</p> Signup and view all the answers

According to the AFM, what defines the existence of icing conditions on the ground and during takeoff?

<p>OAT of 10°C or below with any form of visible moisture. (D)</p> Signup and view all the answers

When operating on ramps, taxiways, or runways, under what conditions related to surface contaminants are icing conditions considered to exist?

<p>When surface snow, ice, standing water, or slush may be ingested by the engines or freeze on engines, nacelles, or engine sensor probes. (C)</p> Signup and view all the answers

During flight, when is engine anti-ice required to be activated if the primary ice detection system is operative?

<p>Automatically, as needed, in response to ice detection signals from the primary ice detection system. (A)</p> Signup and view all the answers

During cold weather operations, an engine run-up to 50% N1 is required. What condition necessitates this procedure?

<p>OAT is between 0°C and -6°C and taxi time reaches 45 minutes. (B)</p> Signup and view all the answers

What action is required if taxi time in freezing fog with visibility of 300 meters exceeds 60 minutes without performing the core ice shedding procedure?

<p>The engine core must be manually de-iced before takeoff is permitted. (C)</p> Signup and view all the answers

Under what circumstances is takeoff permitted when operating in freezing fog with visibility at or below 300 meters without engine core ice shedding?

<p>Takeoff can be achieved within 60 minutes of total taxi time. (C)</p> Signup and view all the answers

After operating in freezing fog, when is a borescope inspection required?

<p>Within 10 flights following the operation in freezing fog. (C)</p> Signup and view all the answers

What is the most critical factor when determining the minimum fuel tank temperature prior to takeoff?

<p>Meeting both the -40°C limit and being at least 3°C above the fuel freezing point, whichever is higher. (D)</p> Signup and view all the answers

Besides Jet A and Jet A-1 what other type of fuel is prohibited?

<p>JP-4. (C)</p> Signup and view all the answers

How should flight crew respond if the Engine Indication and Crew Alerting System (EICAS) displays more restrictive engine limits than those specified in the manual?

<p>Follow the more conservative limits shown on EICAS. (C)</p> Signup and view all the answers

What is the operational significance of amber markings on the Engine Indication and Crew Alerting System (EICAS)?

<p>They represent caution limits that should be monitored. (D)</p> Signup and view all the answers

When is the selection of QFE altitude reference in the Flight Management System (FMS) required?

<p>Whenever QFE is used instead of QNH for the Primary Flight Displays (PFDs). (A)</p> Signup and view all the answers

What is a specific operational restriction regarding the combined use of navigation systems and QFE?

<p>The use of VNAV or LNAV with QFE selected is prohibited. (D)</p> Signup and view all the answers

According to the restrictions for HNS-HNX aircraft operating in U.S. airspace, under what condition are Instrument Landing System (ILS) CAT II and CAT III approaches permitted despite identified 5G interference?

<p>When using an approved alternative means of compliance (AMOC). (B)</p> Signup and view all the answers

For RNP AR operations, what is the minimum RNP value the aircraft is certified to when using LNAV with the autopilot engaged?

<p>0.11 NM (B)</p> Signup and view all the answers

In relation to 5G interference, what resources should pilots consult for a description of its impact on aircraft systems and operational instructions before conducting a flight?

<p>Refer to the latest revisions of Bulletin CAT-140 and CAT-141. (A)</p> Signup and view all the answers

Flashcards

Minimum Dispatch Pressure

The lowest pressure at which passenger oxygen systems can be dispatched for various routes.

Hong Kong to North America/Europe Pressure

Minimum dispatch pressure set at 1600 PSI for flights from Hong Kong to North America, Europe, and Johannesburg.

Pressure for Asia

Minimum dispatch pressure of 1100 PSI for Northern and Southern Asia, and India, Middle East.

TCAS Authority

Pilots may deviate from ATC clearance to follow TCAS II resolution advisories.

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GPWS Guidelines

GPWS terrain display should not be used for navigation near non-database airports.

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Fuel Density Limits

Fuel density must range between 0.7309 and 0.8507 kg/litre.

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Center Tank Fuel Load

With main tanks not full, center tank can hold up to 1360 kg if C.G. limits are followed.

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Reserve Fuel Requirement

Add 320 kg of reserve fuel to the center tank when required for the mission.

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Fuel Imbalance Limits (High)

Imbalance can’t exceed 1,360 kg if total fuel > 51,709 kg.

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Fuel Imbalance Limits (Low)

Imbalance can’t exceed 2,041 kg if total fuel ≤ 22,680 kg.

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APU Start Cycle

The APU allows 3 start attempts in 60 minutes, with specific wait times between attempts.

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Starter Motor Wait Times

The electric and air turbine starter motors require a 1-minute wait between each start attempt.

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Flight Control Limitations

Avoid large control inputs to prevent structural failure; this applies at any speed below VA.

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Takeoff Control Mode

Takeoff must occur only in normal flight control mode for safety.

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Flap Operations Altitude

The maximum altitude for flap extension is 20,000 feet to ensure safety.

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Maximum Oil Temperature

The highest temperature allowed for engine oil, at 143°C for 15 min.

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Minimum Oil Pressure Requirement

Lowest oil pressure acceptable, which is 10psid with no time limit.

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Reverse Thrust Prohibition

Using reverse thrust in flight or to back the airplane is not allowed.

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Rejected Takeoff Procedure

After RTO with thrust reversers deployed, maintenance inspection is required before takeoff.

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Tailwind Engine Power Limit

For ground operations in tailwinds above 30 knots, limit engine power to 70% N1.

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Oxygen Dispatch Pressure

The minimum pressure required for crew oxygen systems at dispatch.

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Temperature Correction for Oxygen

Adjustment of minimum dispatch pressures based on temperature variations.

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Minimum Dispatch Pressure - 777-300

1500 PSI for Hong Kong to certain destinations at 21°C.

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Minimum Dispatch Pressure - 777-300ER

Lower dispatch pressure due to additional oxygen bottles; lower than for 777-300.

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Pressure for Asia Routes

Minimum dispatch pressure is set at 1100 PSI for Northern and Southern Asia, India, and Middle East.

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N1 Low Pressure Limit

N1 limit for HNE - HNQ, HNS - HNX is 100.5%.

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N2 Intermediate Pressure Limit

N2 limit for HNE - HNQ, HNS - HNX is 105.0%.

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EGT Takeoff Limit HNE-HNQ

EGT limit during takeoff is 920°C for 20 seconds.

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Maximum Continuous EGT

Maximum continuous EGT for HNE - HNQ is 850°C without time limit.

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Oil Temperature Limit

Maximum oil temperature for HNE - HNQ is 191°C with no time limit.

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Engine Anti-Ice System

The system prevents ice buildup on engines during flight operations.

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Icing Conditions Definition

Conditions are met when OAT or TAT is 10°C or below with visible moisture.

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Primary Ice Detection System

Detects ice and automatically activates engine anti-ice during flight.

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Use of Anti-Ice Below -40°C

Do not use engine anti-ice if temperature is below -40°C OAT.

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Visual Cues for Anti-Ice Activation

Do not rely on visual cues to activate anti-ice; follow temperature guidelines.

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ADIRU Alignment Limits

ADIRU alignment is not allowed beyond latitudes 78°14.75'.

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MagVar Table Error Limitations

Flight ops using magnetic heading are prohibited if MagVar table errors exceed 5 degrees.

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ILS Approach Restrictions

ILS approaches using magnetic north are prohibited with MagVar errors over 3 degrees.

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MagVar Table Update

To comply, install latest MagVar table, which is the 2015 version.

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Temperature Compensation Requirement

Manual barometric altitude corrections are needed for low temperatures at destination.

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Published Procedure Warning

Using procedures without cold temperature consideration may not ensure obstacle clearance.

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Operational Approval for Corrections

Manual corrections must follow approved procedures by the regulatory authority.

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Low Temp Altimetry Reference

Refer to OM Part A for guidance on low temperature altimetry.

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QFE Selection

QFE altitude reference must be selected in the FMS when using QFE instead of QNH.

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Radio Altimeter Restrictions

Certain operations are prohibited in U.S. airspace due to 5G interference.

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RNP AR Operations

The aircraft can fly RF legs with LNAV and meets FAA RNP AR criteria of 0.11 NM.

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AMOC Compliance

Approved alternative means of compliance for operations with 5G interference.

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LNAV Engagement

LNAV must be engaged for RNP AR operations to function optimally.

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Engine Run-Up Procedure (0°C to -6°C)

Run engines to 50% N1 for 1 min every 45 mins of taxi.

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Engine Run-Up Procedure (-7°C to -13°C)

Run engines to 59% N1 for 1 min every 45 mins of taxi.

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De-Icing Requirement (below -13°C)

If taxi time exceeds 45 mins while colder than -13°C, manually de-ice engines.

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Freezing Fog Taxiing Limits

If total taxi time exceeds 45 mins in freezing fog, perform core ice shed or takeoff must be within 60 mins.

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Fuel Temperature Limits

Fuel tank must be at least -40°C or 3°C above freezing point prior to takeoff.

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JP-4 and Jet B Fuel Restriction

The use of JP-4 and Jet B fuels is prohibited in operations.

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Engine Limit Display Markings

Maximum/minimum limits are red, caution limits are amber on EICAS.

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Borescope Inspection Requirement

A borescope inspection is required within 10 flights; essential for engine health.

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Study Notes

Passenger Oxygen - Minimum Dispatch Pressure

  • Minimum dispatch pressure (at 21°C) varies depending on the destination
  • Different pressures are listed for various locations (e.g., Hong Kong to North America/Europe and Johannesburg, Hong Kong to other than North America/Europe North America and Johannesburg, etc.)
  • Precise PSI values are tabulated for each destination.

GPWS - Look-Ahead Terrain Alerting

  • Terrain display for navigation is not used
  • Look-ahead terrain and terrain display functions are prohibited within 15 nautical miles of takeoff, approach, and landing at airports.
  • Reference Honeywell Document 060-4267-000 for GPWS terrain database.

TCAS

  • Pilots can deviate from current ATC clearances when necessary to comply with TCAS II resolution advisory.

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Description

This quiz covers essential aircraft operations and regulations. Topics include oxygen pressure, TCAS, APU start limits, and flight control configurations. Questions address procedures for safe and compliant flight operations.

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