{"id": 152, "category": null, "questions": [{"id": 637, "category": null, "answers": [{"id": 1867, "content": "1000 ft/min", "correct": true}, {"id": 1868, "content": "2000 ft/min", "correct": false}, {"id": 1869, "content": "3000 ft/min", "correct": false}, {"id": 1870, "content": "500 ft/min", "correct": false}], "type": "MCQuestion", "difficulty": "medium", "content": "

After an emergency descent, below FL100, the crew should limit the rate of descent to approximately ____ ft/min, except during approach phase.

", "explanation": "

FCTM-PRO-ABN-MISC-EMER DESCENT

\r\n\r\n

In this situation, the rate of descent should be limited to 1000ft/min.

", "created_at": "2021-09-23T09:09:43.939515Z", "updated_at": "2021-09-23T09:09:43.939543Z", "allow_comments": true, "status": "accepted", "reviewer_feedback": "", "last_reviewed_at": null, "answer_order": "random", "allow_multiple_answers": false, "author": 9, "reviewer": null, "quiz": [31, 8, 38, 121, 152]}, {"id": 425, "category": null, "answers": [{"id": 1202, "content": "To increase the margin to AOAstall.", "correct": true}, {"id": 1203, "content": "To reduce the drag.", "correct": false}, {"id": 1204, "content": "To reduce the possibility of a secondary stall.", "correct": false}, {"id": 1205, "content": "To greatly increase the value of the AOA associated to a stall.", "correct": false}], "type": "MCQuestion", "difficulty": "medium", "content": "

During a stall recovery, once the flight path is recovered, what is the reason to select Flaps 1 below FL200?

", "explanation": "

FCTM-PR-AEP-MISC-Stall Recovery

\r\n\r\n

You must select flaps 1 below FL200 in order to increase the margin to AOAstall.

", "created_at": "2021-03-24T16:07:02.926062Z", "updated_at": "2021-09-19T16:38:24.520219Z", "allow_comments": true, "status": "accepted", "reviewer_feedback": "", "last_reviewed_at": null, "answer_order": "random", "allow_multiple_answers": false, "author": 9, "reviewer": null, "quiz": [38, 152]}, {"id": 602, "category": null, "answers": [{"id": 1773, "content": "the abnormal attitude law", "correct": true}, {"id": 1774, "content": "the alternate law", "correct": false}, {"id": 1775, "content": "the direct law", "correct": false}, {"id": 1776, "content": "the mechanical Back-Up", "correct": false}], "type": "MCQuestion", "difficulty": "medium", "content": "

If for any reason, the aircraft goes far outside the normal flight envelope and reaches an extreme attitude, the flight control law will be modified to:

", "explanation": "

FCOM-DSC-27-20-20-Abnormal Attitude Law

\r\n\r\n

The abnormal attitude law will engage and will provide the PF with maximum efficiency to recover normal attitude.

", "created_at": "2021-09-12T15:39:38.402604Z", "updated_at": "2021-09-12T15:39:38.402632Z", "allow_comments": true, "status": "accepted", "reviewer_feedback": "", "last_reviewed_at": null, "answer_order": "random", "allow_multiple_answers": false, "author": 9, "reviewer": null, "quiz": [31, 15, 106, 123, 152]}, {"id": 561, "category": null, "type": "TFQuestion", "difficulty": "medium", "content": "

In case of HYD LO LVL the affected hydraulic system can be used until the end of the flight.

", "explanation": "

FCOM-PRO-ABN

\r\n\r\n

This statement is incorrect, the ecam and the abnormal procedure ask to switch the affected pump(s) off and therefore the affected hydraulic system becomes inoperative. Remember that there is no hydraulic fluid transfer between systems.

", "created_at": "2021-07-19T15:31:10.410522Z", "updated_at": "2021-07-19T15:31:10.410547Z", "allow_comments": true, "status": "accepted", "reviewer_feedback": "", "last_reviewed_at": null, "correct": false, "author": 9, "reviewer": null, "quiz": [31, 17, 106, 152]}, {"id": 268, "category": null, "type": "TFQuestion", "difficulty": "medium", "content": "

Since the A320 is fly-by-wire, all flight control surfaces are only electrically controlled and hydraulically actuated.

", "explanation": "

FCOM-DSC-27-10-10-Basic Principle

\r\n\r\n

This statement is false.

\r\n\r\n

Flight controlled surfaces are electrically controlled and hydraulically actuated but stabilizer and rudder can also be mechanically-controlled (Mechanical Backup).

\r\n\r\n

Note: Rudder is mechanical however yaw damping, turn coordination and trim is electrically controlled and hydraulically actuated.

", "created_at": "2021-01-30T20:27:16.707474Z", "updated_at": "2023-09-28T19:12:49.521204Z", "allow_comments": true, "status": "accepted", "reviewer_feedback": "

Update

\r\n\r\n

actuated as per the note in the FCOM, also operated used.

", "last_reviewed_at": "2023-09-28T19:12:49.514581Z", "correct": false, "author": 9, "reviewer": 9, "quiz": [31, 15, 36, 102, 152]}, {"id": 498, "category": null, "answers": [{"id": 1451, "content": "AP off", "correct": true}, {"id": 1452, "content": "ATHR off", "correct": true}, {"id": 1453, "content": "FD off", "correct": true}, {"id": 1454, "content": "\"UNRELIABLE AIRSPEED\" [callout], 10\u00b0/CLIMB", "correct": true}, {"id": 1455, "content": "\"UNRELIABLE AIRSPEED\" [callout], 15\u00b0/TOGA", "correct": false}, {"id": 1456, "content": "SPEEDBRAKES check retracted", "correct": true}, {"id": 1457, "content": "L/G up", "correct": true}, {"id": 1458, "content": "If flaps Full select flaps 3 else maintain current configuration", "correct": true}, {"id": 1459, "content": "maintain current configuration", "correct": false}], "type": "MCQuestion", "difficulty": "medium", "content": "

[MEMORY ITEM] What are your immediate actions for UNRELIABLE AIRSPEED at
\r\n8000 ft? (if the safe conduct of the flight is impacted)

", "explanation": "

FCOM-PRO-ABN-NAV-Unreliable Speed Indication

\r\n\r\n

FCOM-PRO-ABN-ABN-00-Abnormal and Emergency Callouts

\r\n\r\n

The associated callout is: "UNRELIABLE AIRSPEED"

\r\n\r\n

Below thrust reduction altitude: 15°/TOGA

\r\n\r\n

Between thrust reduction altitude and FL100: 10°/CLIMB

\r\n\r\n

Above FL100: 5°/CLIMB

", "created_at": "2021-06-23T21:30:18.991290Z", "updated_at": "2021-07-06T19:22:04.603453Z", "allow_comments": true, "status": "accepted", "reviewer_feedback": "", "last_reviewed_at": null, "answer_order": "random", "allow_multiple_answers": true, "author": 9, "reviewer": null, "quiz": [33, 38, 152]}, {"id": 596, "category": null, "type": "TFQuestion", "difficulty": "medium", "content": "

The "STALL" warning is available in direct law.

", "explanation": "

FCOM-DSC-27-20-20-Direct Law

\r\n\r\n

This statement is correct, the stall and overspeed warnings are available in alternate and direct law.

", "created_at": "2021-09-10T12:08:03.578698Z", "updated_at": "2021-10-24T19:33:23.047589Z", "allow_comments": true, "status": "accepted", "reviewer_feedback": "", "last_reviewed_at": null, "correct": true, "author": 9, "reviewer": null, "quiz": [31, 15, 36, 102, 106, 152]}, {"id": 513, "category": null, "answers": [{"id": 1512, "content": "Loss of all ECAM Cautions and Warnings", "correct": true}, {"id": 1513, "content": "Loss of all master caution and warning lights", "correct": true}, {"id": 1514, "content": "Loss of all aural warnings", "correct": true}, {"id": 1515, "content": "Loss of all amber and red lights on the overhead panel.", "correct": false}, {"id": 1516, "content": "Loss of Radio height and decision height callouts", "correct": true}], "type": "MCQuestion", "difficulty": "medium", "content": "

What is the impact of a FWS 1+2 Fault ?

\r\n\r\n

(select all that apply)

", "explanation": "

31-05-30-Architecture

\r\n\r\n

PRO-ABN-FWS 1+2 Fault

\r\n\r\n

In case of FWS 1+2 Fault, ECAM Cautions and Warnings, aural warnings, master caution and warning lights are lost. The radio height and decision height callouts are also lost.

\r\n\r\n

", "created_at": "2021-07-11T19:24:43.072868Z", "updated_at": "2021-08-26T15:09:56.895976Z", "allow_comments": true, "status": "accepted", "reviewer_feedback": "", "last_reviewed_at": null, "answer_order": "random", "allow_multiple_answers": true, "author": 9, "reviewer": null, "quiz": [31, 19, 36, 102, 38, 89, 106, 152]}, {"id": 297, "category": null, "answers": [{"id": 868, "content": "When cabin altitude exceeds 14000ft.", "correct": true}, {"id": 869, "content": "When cabin altitude exceeds 10000ft.", "correct": false}, {"id": 870, "content": "It is not automatic, only the flight deck can control the deployment.", "correct": false}], "type": "MCQuestion", "difficulty": "medium", "content": "

When do the passenger oxygen masks automatically drop down?

", "explanation": "

FCOM-DSC-35-30-10-Operation

\r\n\r\n

The masks automatically drop down if the cabin pressure altitude exceeds 14000ft (or 16000ft if the aircraft is fitted for high altitude airfields).

", "created_at": "2021-02-24T15:23:22.182435Z", "updated_at": "2021-04-25T16:02:04.670127Z", "allow_comments": true, "status": "accepted", "reviewer_feedback": "", "last_reviewed_at": null, "answer_order": "random", "allow_multiple_answers": false, "author": 9, "reviewer": null, "quiz": [23, 152]}, {"id": 137, "category": null, "answers": [{"id": 443, "content": "0.28 nm", "correct": true}, {"id": 444, "content": "1 nm", "correct": false}, {"id": 445, "content": "0.36 nm", "correct": false}, {"id": 446, "content": "5% of the current airway width.", "correct": false}], "type": "MCQuestion", "difficulty": "medium", "content": "

Which figure of merit triggers the rejection of the GPS position by the FMS ?

", "explanation": "

FCOM-DSC--22_20-20-20-General

\r\n\r\n

If the figure of merit is above 0.28nm, the FMS will reject the GPS position.

", "created_at": "2021-01-21T03:39:18.895216Z", "updated_at": "2022-03-05T16:34:05.836621Z", "allow_comments": true, "status": "accepted", "reviewer_feedback": "", "last_reviewed_at": null, "answer_order": "random", "allow_multiple_answers": false, "author": 9, "reviewer": null, "quiz": [31, 9, 74, 116, 152]}], "is_premium": false, "title": "November 2024", "description": "Monthly quiz - 10 questions", "type": "monthly", "random_order": false, "max_questions": null, "exam_paper": false, "pass_mark": 0, "success_text": "", "fail_text": "", "draft": false, "created_at": "2024-10-29T16:16:07.886489Z", "updated_at": "2024-10-31T10:43:04.283758Z", "publish_after": "2024-11-01T00:00:01.000000Z"}

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