Frontier Master Question File Flashcards

1
Q

How​ is BURN​ fuel on the flight plan calculated?​

A

The amount of fuel burn in pounds and time based​ on forecast winds, the flight plan ​route, and includes one instrument approach and​ landing.

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2
Q

Do all cabin​ seats need to be assigned if a flight deck or flight attendant jumpseat is ​to be utilized?

A

No. the flight deck and flight attendant jumpseats may be assigned on a discretionary ​basis regardless of whether all cabin seats are occupied or​ not.​

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3
Q

Must a Frontier employee have the letters ACM on his/her Frontier ID badge to occupy the flight deck jumpseat?

A

Yes, unless the Frontier employee has a signed Letter of Authorization from Frontier ​Flight Ops management.


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4
Q

The ACM Jumpseat Briefing Card may be used to satisfy the ACM briefing ​requirement?

A

True

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5
Q

​Employees with knowledge of an accident involving an aircraft for which they ​performed a​ safety-sensitive or​ security-related function at or near​ the time of the ​accident may not use alcohol for​ ____ hours after the accident unless​ he or she has ​been given​ a post accident test for drugs and alcohol, or​ if Frontier Airlines has ​demonstrated that​ their performance could not​ have contributed to the accident.​

A

8

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6
Q

Which of the following qualifies the flight crew to fly into “Special Airports”?

​(Select ALL answers that apply)

A

​Within the preceding 12 calendar months, the captain or first officer has made an entry ​to that airport, including​ takeoff and landing, while serving as a flight crewmember.​ ​​

Within the preceding 12 calendar months, the captain has qualified by using pictorial ​means for that airport. ​​ 


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7
Q

When the first officer has less than 100 hours of flight time​ as SIC in type airplane ​being flown at Frontier, the captain (unless a check airman) must​ make all takeoff ​and landings​ in what conditions?

(Select ALL answers that apply)​

A

When the​ crosswind component for the runway to be used is in excess of 15 knots.​

When the braking action​ on the runway to be used is less than “good”.​ ​​


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8
Q

Which of the following describes emergency authority?

(Select ALL answers that ​apply)

A

​In an emergency situation that​ requires immediate decision and action, the pilot in ​command may take any action deemed necessary under the circumstances.​

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9
Q

Who has operational control to refuse a passenger?

A

The CRO


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10
Q

Who has​ the authority to cancel a flight?

A

Only Systems Operations Control (SOC).​ 


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11
Q

Which of the following requires an alternate airport?

(Select ALL answers that ​apply)

A

Any flight released under supplemental operations.

​​ ​If severe icing conditions are forecast at the destination within one hour of the ETA, a ​suitable alternate must​ be listed on the release.

When dispatched Method 2.


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12
Q

Which of the following is NOT required before a revenue flight may block out?​

A

The Final Flight Information List.

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13
Q

If the planned route is changed by ATC​ prior to takeoff, and the resulting stage ​length increases​ by more than ____ NM, the captain must​ obtain an ARTR.

A

100NM

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14
Q

Which of the following best describes Method 1?

A

If an engine failure occurs anywhere from V1 to the destination, the aircraft will​ clear ​all​ obstructions 5 SM on either side of the intended route by 1,000 feet until reaching ​the destination.

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15
Q

​How​ is CONTINGENCY fuel on the flight plan calculated?

A

​Fuel in time as well as in pounds based on holding at 15,000 MSL at Green Dot
.

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16
Q

Which of the following best describes method 2?

A

If an engine failure occurs, the aircraft will be able to divert​ to at least one suitable ​airport (driftdown alternate)​ from flight planned cruise altitude and clear all​ obstacles 5 ​SM on either side​ of the route of flight by 2,000 feet until reaching the diversion airport.

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17
Q

Which of the following would require an ARTR?

(Select ALL answers that apply)

A

An alternate is added or​ changed.

An MEL is added.

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18
Q

What does ALTN​ fuel on the flight plan consist of?​

A

Climb to cruise flight altitude, cruise flight to the most​ distant alternate, one (1) ​approach and landing, planned at a cost index of 0.​ ​​

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19
Q

Are Simple Special Procedures​ mandatory to follow in both IMC and VMC? If so, ​to what altitude?

A

They are mandatory in IMC until​ 3,000’ AFE (if radar vectors are not​ available)​ and ​VMC until reaching 1,000ft AFE unless otherwise specified.​


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20
Q

Which of the following are ways to determine Actual Landing Performance?

(Select ALL answers that apply)

A

​The AWP solution.

The QRH landing distance Performance section.


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21
Q

What are some strategies for dealing​ with weight restricted flights?

A

Remove COMAT (not AOG).

​Obtain child counts.

​Increase the PMtOW or reducing tanker fuel (if any).​ ​


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22
Q

Which of the following are approved methods to get Weight and Balance ​Information for departure?

A

AWP Solution (Primary Method).

Computer-Generated W&B Manifest from Centralized Load Planning.

Manual W&B Read Back Form located in the diversion kit. ​​ 


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23
Q

Which of the following fuel considerations are required prior to departure?

A

When dispatched under Ops Spec B043 (As noted on the dispatch release),​ the aircraft ​must​ have enough contingency fuel to fly for a period of 10 percent of that portion of ​the enroute time where the aircraft’s position cannot be “reliably fixed” at least once ​each hour.


The aircraft must have enough fuel to fly to the airport to which it is dispatched; ​thereafter, to fly to and land at the most distant alternate airport (when required) for the ​airport to which it is dispatched; and​ thereafter,​ to fly for 45minutes at​ normal cruising ​fuel consumption.

The aircraft must have enough fuel to​ consider one instrument approach and possible​ ​missed approach at the destination, wind and other weather conditions forecast, ​anticipated traffic delays, and any other known conditions that may delay​ landing of the ​aircraft. ​​

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24
Q

Frontier is authorized to conduct​ the following approaches EXCEPT​

A

(SA) CAT I Approaches

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25
Q

How​ can the flight crew determine if​ an airport is “Terrain Sensitive”?

A

Via a mountain symbol at the top of the first page of the AIP​.

Via contours published on any SID, STAR, or approach procedure​.

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26
Q

Which of the following statements is FALSE?​

A

When a discrepancy has been entered into the aircraft logbook, ONLY MCC must be ​notified.


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27
Q

Who must be notified after entering a​ discrepancy in the Logbook?

A

MCC through the responsible dispatcher.

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28
Q

Which of the following is a correct way(s)​ to make a correction to a logbook ​entry?

A

​To correct a single word or phrase error, draw a line through the entry and add the ​corrected information adjacent to the lined-out item.​ ​​

To correct an entire entry block, draw​ a diagonal line through​ the entry and write “Entered​ in Error” (or​ “EIE”)​ on the diagonal line.​

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29
Q

How​ is RESERVE fuel​ on the flight plan calculated?

A

Reserve fuel of 45 minutes flight time is​ based on last cruise altitude in the flight plan.​

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30
Q

Which of the following logbook entries requires the captain’s signature?

A

Computer​ Reset

Flight Crew Placard

Follow-up Required

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31
Q

Which of the following best describes the CDL (Configuration Deferral List) ​Program?​

A

The CDL Program allows for continued operations with missing secondary airframe and ​engine parts.

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32
Q

​Which of the following best describes the MEL (Minimum Equipment List)?

A

The MEL Program​ allows for a temporary change in type design to address missing or ​inoperative equipment in order to maintain the validity of the​ airworthiness certificate.​


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33
Q

Which of the following best describes the NEF (Nonessential Furnishing) ​program?

A

The NEF Program allows the deferral of inoperative, damaged or missing items that will​ ​have no effect on the safe operation of the aircraft, and which are​ not required by ​certification standards or operating rules.​

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34
Q

Which of the following best describes an ODM (Other Deferred Maintenance)​ ​item?

A

ODM Items include deferrals that are​ “crew visibility” in nature and utilize​ an INFO-ONLY placard​ to notify​ air​ crewmembers that the item on the placard has been ​documented​ and is​ being tracked by the maintenance department. ​​

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35
Q

​Is Frontier​ permitted to depart an airport VFR and then pickup​ an IFR clearance?

A

Yes, under certain weather conditions and provided an IFR clearance is obtained ASAP, ​but no further than 50 NM from​ departure airport.​ 


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36
Q

What is Class II (two) navigation?

A

Any navigation conducted outside of Class I navigation.


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37
Q

When is the autopilot required to be used (coupled) to conduct an approach?

A

When the weather is less​ than 4000 RVR​ (3/4 SM) and the autopilot is available for use.

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38
Q

Which of the following is Frontier authorized to conduct in international airspace?

A

A “VMC Approach”​

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39
Q

Prior​ to crossing a​ FIR boundary for​ international flights, the flight​ crew should ​obtain the latest weather (METAR and TAF) for the destination and alternate​ (if ​applicable).

A

True

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40
Q

Where is Frontier authorized to conduct SLOPs?

A

Gulf of Mexico

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41
Q

How​ does the flight crew determine snowfall intensity when determining what ​holdover times to use?

A

​If another form of obscuration is being reported along with snow (e.g., fog/haze/smoke), ​then use the Tower reported snowfall intensity.

​If no obscuration is present on the Tower reported snow intensity, then use the​ ​“Snowfall Intensities As A Function Of Prevailing Visibility” Table located on the ​DeIce Card to determine snowfall intensity. ​​ 


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42
Q

​Anti-icing with the flaps/slats extended is permitted.​

A

​False

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43
Q

​Deicing with the flaps/slats extended​ is permitted.​

A

True

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44
Q

A flight can takeoff if the holdover time expires if the flight crew performs a pre-​takeoff contamination check (exit row check, and that check is satisfactory) within ​5 minutes of advancing the thrust levers​ for takeoff.

A

​True

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45
Q

When does the Tarmac Delay clock start for DEPARTURES?

A

Five (5) minutes after the last passenger is boarded.​

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46
Q

An ARTR is required if a flight diverts to an alternate that is different from that ​published on the dispatch release.

A

​True

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47
Q

When are security searches required?

A

​International flights (not including Alaska).

First flight of the day. ​​

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48
Q

A flight to Puerto Rico is Not considered an international flight for security ​search purposes?

A

​True

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49
Q

The captain must​ be informed of all individuals on board carrying firearms.​

A

True

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50
Q

What are the 4 levels of threat?

A

​Level 1: Verbal

Level 2: Physical​

Level 3: Imminent threat of death or serious bodily injury​

​Level 4: Attempted or actual breach of the flight deck​

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51
Q

Where can the flight crew find a list​ of Ops Specs​ C070 approved airports?​

A

Airport Information Pages​

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52
Q

Where can the flight crew find coded departure routes and instructions on how to ​uplink these routes into the MCDU? ​


A

Airport Information Pages​ ​


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53
Q

If an International flight diverts and does not​ clear customs what does the flight ​need to continue to its destination?​

A

A permit to proceed.

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54
Q

What does the TEST​ acronym consist of when giving the Emergency Preparation?

A

​T –​ Type of Emergency

E –​ Evacuation anticipated (yes/no) ​​

S –​ Signals to brace, evacuate or remain seated (review as appropriate)​

T –​ Time​ remaining until landing

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55
Q
A
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56
Q

What is the purpose of the flight attendant emergency whistle​ (EW)?

A

To indicate a Threat Level 2, 3, or 4 situation.

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57
Q

When are manual engine starts recommended?​

A

After​ aborting a start because​ of an engine stall, EGT overlimt, or low starter air ​pressure.


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58
Q

In flight, BOTH flight directors should be either ON​ or OFF.​

A

True

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59
Q

Which of the following is TRUE regarding the announcement of​ FMA changes?

A

Workload permitting and unless specified otherwise e.g. (CAT II/III task sharing), all ​FMA changes (as indicated by a​ white box)​ will​ be announced by the PF below FL 180. ​At or above FL 180, the Vertical and Lateral Mode Changes (i.e., second and third ​columns of the FMA) will​ be announced by the PF.​

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60
Q

During preflight and prior to the application of electrical power, you notice​ the ​battery voltage is below 25.5 volts, how should you recharge the batteries?

A

Ensure external power is supplied to the aircraft and select the BAT 1 and 2 pbs to the ​AUTO position.

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61
Q

On the preflight check, if engine oil quantity is not displayed on the ENG SD ​page, how should you check the oil quantity on NEO aircraft?​

A

Set the ENG 1 and 2 FADEC GND PWR pb-sw on the overhead maintenance panel to ​ON​ in order to display the oil​ quantity on the ENG​ SD page. After the check of the engine ​oil quantity, set the ENG 1 and 2 FADEC GND PWR pb-sw to OFF.


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62
Q

When is a full ADIRU alignment required?

A

Before the first​ flight of​ the day, when there is a crew change, prior​ to all international ​flights (including Alaska) or prior to flights in Class 2 airspace.​

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63
Q

When is a fast ADIRU alignment required?

A

​Any time the difference between the IRS position and the FMGC position exceeds 5 ​NM.


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64
Q

During refueling, what might happen if​ the FUEL MODE SEL pb-sw is left in the ​MAN position on the ground and the CTR TK​ L​ XFR pb-sw​ and CTR TK R​ XFR ​pb-sw are not in the off position?

A

The center tank fuel transfer will​ not stop when the wing tanks become full and a fuel ​spillage may occur.


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65
Q

Just prior to pushback, if the NW STRG DISC​ is not displayed on the ECAM, but ​the ground crew confirms that the steering selector bypass pin is in the towing ​position, what must the flight crew do?​

A

Make a logbook entry. Contact MCC​ through the responsible dispatcher. ​


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66
Q

If a heading is assigned by ATC prior to takeoff, what HDG should be​ preset on ​the FCU to disarm NAV mode?

A

Runway HDG

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67
Q

No turns in HDG mode will​ be commenced below ____ ft AFE (VMC) or ____ ft​ ​AFE (IMC); unless otherwise required by the departure procedure?

A

​400’ VMC

1,000 ​’ IMC

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68
Q

How​ could you quickly determine​ if​ you can take shortcuts off your filed route if ​you are dispatched via method 2?​

A

Reference the “Terrain Analysis Common Aircraft Weights” on the back of the Normal ​Checklist.

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69
Q

What altitude should be set on the FCU for a “Visual Approach” utilizing a ​published procedure as backup reference?

A

The published missed approach altitude for the approach being used.​

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70
Q

What altitude should be set​ on the FCU for a “Visual Approach” with no ​procedure backup as​ a reference?

A

1,500 feet AFE

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71
Q

Why is entering 0.3 on the PROG page of​ the MCDU for RNAV approaches ​required?

A

​To ensure that the​ FMS stays​ in 0.3 for the missed approach rather than defaulting back ​to RNP 1.0.

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72
Q

Why is deselecting navaids in the MCDU for a RNAV RNP​ approach required?

A

In the event of GPS loss, IRS only navigation may be more accurate than DME/DME ​position updating in the short term.​


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73
Q

Which of the following statements are TRUE if speedbrakes are used above 315 ​knots/M .75 with the AP engaged?

A

Rate of retraction of the speedbrakes​ are slow, the total time for retraction from​ full ​extension is approximately 25 seconds.

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74
Q

During the flare on landing, the PM will​ monitor the pitch attitude on the PFD ​and call “Pitch” whenever approaching/or​ reaching what pitch attitudes?

A

A321: 7.5° pitch attitude

A319 or A320: 10° pitch attitude

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75
Q

When should the after landing checklist be called​ for?

A

After​ clearing the runway and the aircraft is safely established on a taxiway, but not before​ taxi/runway crossing restrictions are clearly understood by both crewmembers.​

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76
Q

After​ landing, how long should we wait before starting the APU?

A

​2 minutes after​ stowing the Thrust​ Reversers.

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77
Q

After​ taxi-in and during parking, you attempt to shut down an engine (you​ move​ ​the ENG MASTER 1 or​ 2 to OFF). However, the engine does not shut​ down. ​What should​ you do?

A

Switch the affected master lever ON, then OFF. If the engine still fails to shut down, ​press the affected ENG​ FIRE pushbuton.

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78
Q

After​ parking the aircraft, you notice a maintenance status message (Class​ 2 ​message). A few seconds later, the Class 2 message disappears. A logbook write-​up is required for the class 2​ message that disappeared.

A

True

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79
Q

Which of the following statements should be followed when performing the ​Securing Checklist?

A

After​ having switched off the ADIRS, wait at least 10 seconds before switching off the ​electrical supply to ensure that the ADIRS memorize the last​ data.

Wait at least​ 5 minutes after​ BLOCK IN to accomplish the securing procedure to allow ​the FMGC/AOC​ to complete the DONE PHASE and enter the PREFLIGHT PHASE.​

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80
Q

​In flight prior to manipulation, both the Pilot Flying (PF) and Pilot Monitoring ​(PF) must confirm.

A

Engine master switches, IR selector, All guarded controls.

Thrust Levers (During an ECAM or QRH procedure)

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81
Q

​In most situations, the following sequence is the basic one that should be followed ​by the flight crew during​ an abnormal/emergency​ situation.​ ​ ​1.​ ​ Memory Items,​ ​ ​2.​ ​ OEBs,​ ​ ​3.​ ​ ECAM, ​ ​4.​ ​ QRH Procedures, then ​5.​ ​ Abnormal​ & Emergency Procedures (time permitting).​ ​However, this sequence may not cover all operational situations. Therefore, the​ ​flight crew should exercise their judgement and adapt the sequence of actions to ​the real conditions.

A

True

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82
Q

For an abnormal procedure during approach, perform the normal checklist first, ​then the ECAM/ABNormal procedure or​ checklist.

A

False

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83
Q

For an abnormal procedure during takeoff, perform the after Takeoff ​checklist​ first, then the ECAM/ABNormal​ procedure or checklist. (Not ​applicable​ to Engine Fire, Oil​ Lo Press, Eng. Overlimit, Engine Failure, and ​Engine Stall)
.

A

True

84
Q

Which of the following statements are TRUE?

A

​If red LAND​ ASAP is part​ of the ECAM procedure, land as soon as possible at the ​nearest airport at which a safe landing can be made.​

​If amber LAND​ ASAP is part of the ECAM procedure, consider landing at the nearest ​suitable airport.

85
Q

While performing an ECAM for an engine failure, the pilot flying (PF) will call ​”Stop ECAM Actions” prior to the pilot monitoring (PM) reading the​ ______ page ​in order​ to complete the after takeoff checklist.

A

Status

86
Q

What is the​ purpose of an ECAM advisory?

A

An ADVISORY informs the crew that a​ parameter is approaching a limitation and ​enables the flight crew to monitor the drifting parameter.

87
Q

Where can the flight crew find triggering conditions for various ADVISORY​ ​situations or associated recommendations for an ECAM ADVISORY?

A

QRH procedure section

88
Q

​What is the purpose of the “Summary” sections within the QRH?

A

To help the flight crew perform actions in the case of an ELEC EMER​ CONFIG or dual ​hydraulic failure.

89
Q

Where can the flight crew find the Computer Reset Table?

A

QRH procedure section

90
Q

Where can you find Frontier’s procedures on Engine Out Standard Instrument​ ​Departures (EOSID’s) as​ well as Complex Missed Approaches utilizing an ​EOSID?​

A

FOM VOL II –​ Supplementals –​ Special Procedures and/or the AIPs​

91
Q

​Crews operating at airports that utilize EO Complex Procedures shall set up and ​brief the procedure to be ready for an engine failure.​

A

​True

92
Q

When performing the Class 2 Nav Accuracy check, FM position is considered ​reliable if

A

Error ≤​ 3NM​

93
Q

When performing the Class 2 Compass Deviation Check, all headings should be ​within ____ degrees of each other?

A

​5

94
Q

Which of the following statements is TRUE?

A

Compliance with a​ TCAS II resolution advisory (RA) is required unless the captain ​considers it unsafe to do so, or unless the pilot has better information about the cause of ​the RA and can maintain​ safe operation.​

95
Q

If the engines and/or​ landing gear​ need to be deiced, what actions must be taken?

A

A logbook entry. Notify MCC​ through the responsible Dispatcher so the engines​ and/or ​landing gear are deiced properly.​

96
Q

Do not move flaps or slats, flight control surfaces, or trim surfaces, if they are not ​free of ice.

A

​True


97
Q

When must ENGINE​ ANTI-ICE be ON?

A

During all ground and flight operations when icing conditions exist​ or are anticipated, ​except​ during climb and cruise when the SAT is below -40°C.

During descent in icing conditions, even if​ the SAT​ is below -40°C

98
Q

When should WING ANtI-ICE be selected on?

A

In flight, whenever there is indication that​ airframe icing exists.

99
Q

Takeoff in moderate and heavy freezing rain is prohibited.​

A

​True

100
Q

​After​ landing, if flaps/slats are NOT free of contamination, leave flaps/slats​ in the ​current configuration. Coordinate with ground/deice crew for cleaning/deicing of ​the flaps/slats prior to flap retraction.

A

True

101
Q

What computer provides reactive windshear detection?

A

​FAC

102
Q

When is reactive windshear available?

A

​At landing: from 1300 ft RA​ to 50 ft RA (with at least CONF 1 selected).

At takeoff: 3 sec after liftoff up to 1300 ft RA​ (with at least CONF 1 selected).

103
Q

What are the 3 types of​ engine failure procedures?

A

Standard, Simple-Special, and Complex-Special Engine Failure Procedure.


104
Q

How​ does a​ Simple-Special​ Engine Failure Procedure differ from a Standard ​Engine Failure Procedure?​

A

The Simple-Special Procedure differs​ from Standard Procedures​ in that a turn to a ​NAVAID or heading is required before reaching 1,000’ AFE.

105
Q

Which of the following best describes the “DECELERATED APPROACH” ​technique?

A

​The aircraft reaches the stabilized approach altitude in the landing configuration and at ​Vapp.

106
Q

What is the recommended technique​ to capture the glideslope from above?

A

Use V/S 1500 ft/min to ensure the A/THR is in SPEED mode rather than IDLE mode.​

107
Q

What approaches require the flight crew to monitor and use raw data for an ​approach?

A

VOR, LOC, ILS and LDA​ approaches​ ​​

108
Q

Frontier is authorized to conduct approaches that have published climb gradients ​in the missed approach with all engines operating for any given aircraft, ​condition, weight, and configuration for climb gradients less than ____ feet per ​nm?

A

937

109
Q

F9 is approved to utilize RNAV (RNP) approaches when Cold Temperature ​Altitude Corrections apply.​

A

False

110
Q

Frontier flight crews are authorized to build an RNAV VISUAL (RVFP) ​approach manually in the FMGC.

A

False

111
Q

Due to database limitations, aircraft​ equipped with the Honeywell​ Step 1A​ FMS ​do not have LDA approaches stored when the same runway has an ILS stored ​(e.g., SFO LDA DME 28R). In these cases, if the LDA​ approach is accepted, the ​flight crew is required to…

A

Manually hard tune the LDA​ frequency by entering the LDA​ identifier and verify the ​correct inbound course.


112
Q

What are the lowest minimums for a CAT II approach?​

A

100 ft DH: 1,000 RVR 


113
Q

What are the lowest minimums for a CAT III approach?

A

​Fail Operational Capable Aircraft​ (FMA -​ CAT 3 DUAL) - 100 ft​ AH: 300 RVR

Fail Passive Capable Aircraft (FMA - CAT 3 SINGLE) - 50 ft​ DH: 600​ RVR​

114
Q

What are the lowest minimums for a CAT IIIB approach?

A

100 ft AH: 300 RVR

115
Q

To use an alert height for a CAT III approach, the aircraft​ must be…​

A

CAT III DUAL capable (Fail Operational)

116
Q

Which of the following best describes a Cold Temperature Restricted Airport ​(CTRA)?

A

Airports which require cold temperature altitude corrections to applicable​ instrument ​approach procedures when the​ temperature at the airport is at​ or below a specified value.


117
Q

How​ can you determine if an airport​ is a​ Cold Temperature Restricted Airport ​(CTRA)?

A

CTRAs and the associated temperature limits are published in the “NOTES” section of ​Jeppesen approach charts.

118
Q

Which approach type do​ Cold Temperature corrections apply to?

A

​ILS approach

119
Q

What are Frontier’s 2 recommended strategies to​ apply if an engine failure ​occurs during cruise?

A

Standard Strategy and Obstacle Strategy


120
Q

Which of the following choices best outlines the Obstacle Strategy for an engine​ ​failure in cruise?

A

Set MCT, A/THR OFF, Set and Pull HDG as Appropriate, Determine Cruise Flight ​Level, Notify ATC, Set Green Dot Speed and Pull.

121
Q

Which of the following choices best outlines the Standard Strategy for an engine ​failure in cruise?

A

Set MCT, A/THR OFF, Set and Pull HDG as Appropriate, Determine Cruise Flight ​Level, Notify ATC, Set M.78/300kts and Pull.​

122
Q

Which of the following best describes S Speed?

A

Minimum Slat Retraction Speed - A green ‘S’ symbol​ appears when the flap selector is ​in position 1 and is the lowest speed to select flaps 0.​

123
Q

Protection speeds (e.g., Vα PROT, Vα MAX, VMAX, etc.) are computed by​…

A

The FAC

124
Q

Which of the following statements are TRUE?

A

Alpha floor​ is available from​ lift off to 100 ft RA on approach. A/THR needs to be ​available, it does not need to be active.​

Alpha floor​ is a​ protection that automatically sets the thrust at TOGA, regardless of ​thrust lever position, when the​ aircraft reaches​ a very high angle of​ attack.

125
Q

When would you get a “TOGA​ LK” with a​ flashing amber box on the FMA?​

A

After​ the Alpha Floor protection has been activated, Alpha floor conditions are no ​longer​ met, and TOGA thrust is active.​ ​​

126
Q

​If the thrust levers are in the CL detent (both engines operative) OR​ one thrust ​lever is in the MCT detent (one engine operative), “THR LCK” will​ appear on ​the FMA if…

A

The Auto-thrust​ Fails or the FCU A/tHR​ push button is pushed.​

127
Q

Which of the following best describes the alpha/speed lock function?​

A

The alpha/speed lock function inhibits slat retraction at​ high angles of​ attack and low air​ ​speeds.

128
Q

What pilot action is required to cancel TOGA LK?​

A

Disconnect the autothrust.

129
Q

What are the 3 types of​ ECAM failures?

A

Independent,​ Primary, and Secondary

130
Q

Which of the following describes the possible types of ECAM failures?

A

Independent Failure - A failure​ that​ does not affect other systems.

Primary - A failure that​ affects other systems and causes secondary failures.​


Secondary Failure -​ A failure that is caused by a primary failure.

131
Q

After​ completion of the ECAM, the flight crew will refer to the QRH​ Procedures ​section of the QRH to determine if procedures apply (i.e., non-ECAM ​procedures) and complete the procedures as​ required. Time permitting the flight ​crew will refer to the Abnormal & Emergency Procedures contained in the QRH. ​What does “Time​ permitting” mean?​

A
132
Q

What buses​ are​ powered by the emergency generator?

A

​DC​ ESS and​ DC​ ESS Shed Bus​

AC​ ESS and​ AC​ ESS Shed Bus​

133
Q
A
134
Q

What powers the emergency generator?

A

​Blue hydraulic pressure from the RAT.

135
Q

Which of the following statements is true when pressing the RAT​ MAN ON pb ​located on the HYD Panel?

A

RAT provides Blue HYD pressure only.

136
Q

What does the illumination of the amber SMOKE light in the GEN 1 LINE ​pushbutton indicate?

A

Smoke detected in the avionics ventilation ducting.


137
Q

When performing the PRELIMINARY FLIGHT DECK​ PREPARAtION, what ​is the minimum Battery Voltage?

A

25.5 Volts


138
Q

What precautions must you take when disconnecting an IDG?

A

​Do not press and hold the IDG​ pb for​ more than 3 seconds.

Do not disconnect the IDG when the​ engine is not operating or windmilling.

139
Q

With the APU START pb AVAIL (green) light illuminated and the​ EXT PWR ​pb ON​ (blue) light illuminated, which system is powering the aircraft (Assuming ​Both Engines are Shut Down)?

A

​External Power

140
Q

In Aircraft equipped with center tank fuel pumps, which of the following ​statements are TRUE?

A

​With the MODE SEL pb-sw in AUtO, before​ or after the start sequence the center tank ​pumps automatically run if the slats are retracted.

With the MODE SEL pb-sw in AUTO, the center tank pumps automatically stop 5 min ​After center tank low level is reached.

With the MODE SEL pb-sw in AUTO, the center tank pumps automatically run at ​engine start for 2 mins.​

141
Q

What will cause the FAULT light to illuminate on​ the Fuel MODE SEL pb?

A

When the center​ tank contains more than 550 lbs of fuel and the wing tank has less than ​11,000 lbs of fuel.


142
Q

What actions occur when an ENGINE FIRE pushbutton is​ pressed?

A

The respective hydraulic shutofff, pack flow control, and engine bleed valve closes.​

The aural fire warning is silenced and the fire​ extinguisher squibs arm.

143
Q

What actions occur when the APU FIRE pushbutton is pressed?

A

The APU low-pressure fuel valve closes and the APU fuel pump shuts off.​

The APU generator is deactivated. The APU​ bleed and X bleed valves close.​

144
Q

On the primary​ flight display, what do the large red chevrons indicate?

A

Pitch attitude greater​ than 30°.

145
Q

What does the yellow speed trend line on the airspeed display indicate?​

A

The speed the aircraft will reach in 10 seconds if acceleration/deceleration​ remains ​constant.

146
Q

Which of the following is TRUE regarding VLS?

A

VLS represents lowest selectable speed providing​ an appropriate margin to​ the stall ​speed. In approach mode VLS is equivalent to Vref.​

147
Q

How​ is VLS​ displayed on the PFD?

A

VLS is represented by the top of​ the amber strip along the airspeed scale.​

148
Q

Which of the following are TRUE regarding altitude/speed constraint circles?

A

​Amber -​ Constraint is predicted to be​ missed.​

Magenta –​ Constraint is​ predicted to be satisfied.

White –​ Constraint​ is not taken into account.


149
Q

What does the appearance of a green arrow indicate at the bottom of the E/WD ​screen?

A

Information has overflowed off the screen and the pilot must scroll​ down using the CLR​ ​pushbutton on the ECAM panel.

150
Q

What is the active range​ of the A/THR?

A

From just above IDLE up to and including the CL detent​ (both engines operating).

From ​just​ above IDLE up to and including​ the MCT detent​ (1 engine inoperative).

151
Q

When will the RAT automatically extend?

A

The RAT will automatically extend if AC BUS​ 1​ & 2 are not powered and airspeed >​ ​100 knots.

152
Q

What is the approach category for the A319/A320?​

A

Category C

153
Q

​What is the maximum crosswind limitation for takeoff?

A

​35kts

154
Q

What is the maximum crosswind limitation for landing?

A

38kts

155
Q

What is the maximum tire ground speed?

A

195kts

156
Q

What is the maximum windshield wiper operation speed?

A

230 KIAS

157
Q

What is the maximum aircraft speed with the cockpit window open?

A

200 KIAS

158
Q
A
159
Q

(On A320/321 Aircraft) the maximum taxi speed when making a turn is ​_____kts when the aircraft weight is​ greater than _____lbs?​

A

20kts

167,550lbs ​​

160
Q

What is the maximum altitude to start the APU using battery power only (Elec​ ​Emerg Config)?​

A

25,000 feet MSL

161
Q

What is the autopilot minimum engagement height after takeoff​ (if SRS is ​indicated)?

A

100 feet AGL ​​

162
Q

What is the autopilot minimum engagement height enroute?

A

900 feet AGL

163
Q

What is the minimum oil temperature required before takeoff?

A

19 degrees​ Celsius

164
Q

What is the maximum time to use TOGA​ thrust with all engines operating?

A

5 min


165
Q

What is the maximum time to use TOGA​ thrust with one​ engine inoperative?

A

10 min

166
Q

What is the maximum altitude that the Flaps or Slats may be extended?

A

20,000 feet MSL

167
Q

What is the minimum height the autopilot can be engaged during a GO-Around ​(if SRS is indicated)?

A

100 feet AGL

168
Q

To meet​ Frontier’s Stabilized Approach Criteria, by 1,000 ft AFE, the aircraft ​must​ be…

A

On the correct vertical path (“Glidepath”).​

​On the correct lateral path (“Course”).​

​In a steady rate of descent not to exceed 1,200 FPM.

169
Q

To meet​ Frontier’s Stabilized Approach Criteria, by 1,000 ft AFE, the aircraft ​must​ be…

A

Absent any GPWS Warnings and Cautions.​

​In the final landing configuration (Landing Gear​ and Flaps Extended).​ ​​


170
Q

To meet​ Frontier’s Stabilized Approach Criteria, by 500 ft AFE, the aircraft must​ ​be…

A

In a steady rate of descent not to exceed 1,000 FPM.​

Within -5 to​ +15 knots of target speed for approach.


171
Q

What does “Correct Lateral​ Path” mean in terms of Frontier’s​ Stabilized ​Approach Criteria?

A

± one dot for ILS/LOC, ½ dot for VOR, or 0.3 NM cross track for RNAV GPS (Not ​applicable​ to RNAV RNP approaches)

172
Q

What is the maximum tailwind limitation for Takeoff (A319/A320)?​

A

15kts

173
Q

What is the maximum tailwind limitation for Takeoff (A321)?

A

10kts

174
Q

What is the maximum tailwind limitation for LANDING (A319/320)?​

A

10kts

175
Q

What is the maximum tailwind limitation for LANDING (A321)?​

A

10kts

176
Q

What is the maximum wind speed for passenger door operation?

A

65kts

177
Q

What is the maximum wind speed for cargo door operation?

A

40kts, unless the aircraft nose is oriented into the​ wind, or if the cargo door is on the ​leeward side of the aircraft, then operation of the cargo door is permitted in winds up to ​50kts.


178
Q

If the aircraft nose is oriented into the​ wind, or if the cargo door is on the leeward ​side of the aircraft, operation of the cargo door is permitted in winds up to _____kts. If wind speed begins to exceed these limitations, the cargo door must ​be closed before the wind speed exceeds _____kts?​

A

50kts

65kts

179
Q

What are the recommended turbulent air penetration speeds Below FL200 ​(A319/320)?

A

250kts

180
Q

What are the recommended turbulent air penetration speeds from FL200 to ​FL310 (A319/320)?

A

275kts

181
Q

What are the recommended turbulent air penetration speeds Above FL310 ​(A319/320)?

A

.76 Mach

182
Q

What are the recommended turbulent air penetration speeds Below FL200 ​(A321)?

A

270kts

183
Q

What is the recommended turbulent​ air​ penetration speeds From FL200 to FL310 ​(A321)?

A

300kts

184
Q

What is the recommended turbulent air penetration speeds​ Above FL310 ​(A321)?

A

.76 Mach

185
Q

At what height must the autopilot be turned off for an RNAV visual approach?

A

500 feet AGL

186
Q

When must the autopilot be turned off for a Non-Precision Approach?

A

DDA/DA

187
Q

At what height must the autopilot be turned off for a Non-Autoland ILS with a ​CAT 1 FMA?

A

160 feet AGL

188
Q

At what height must the autopilot be turned off for a Non-Autoland ILS with a ​CAT 2/3 FMA?

A

80 feet AGL

189
Q

When must the autopilot be turned off for an autoland approach?​

A

ROLLOUT/Taxi Speed

190
Q

Frontier’s​ policy is to set up for, brief, and fly a CAT II or CAT III autoland IF ​the reported RVR/visibility is at or below _____ or ______ AND​ all of the ​requirements for an autoland can be met.

A

½ mile

2400 RVR

191
Q

What is the minimum engine oil quantity for CEO​ aircraft​ prior to each flight?

A

9.5 qt + .5qt per every hour of​ estimated flight time.

192
Q

Takeoff at reduced thrust is prohibited…

A

When suspected, reported, or known windshear​ is​ present.

On slippery or contaminated runways.

When a Special Departure Procedure specifies full thrust for takeoff.​

193
Q

What is the minimum engine oil quantity for NEO aircraft prior to each flight?​

A

​9.0 qt + .5 qt per every hour of estimated flight time and not below 10.6 qt. If​ engines ​have been shut down for more than 60 minutes, decrease these values by 3 qt.​

194
Q

Which of the following are memory items for “LOSS OF BRAKING”?

A

​REV—–MAX

BRAKE PEDALS—–RELEASE

A/SKID OFF—–ORDER

A/SKID & N/W STRG—–OFF

BRAKE PEDALS—–PRESS​

MAX BRK PR—–1000PSI

​IF STILL NO BRAKING: PARKING BRAKE—–SHORT SUCCESSIVE ​APPLICATIONS

195
Q

What is the memory item for “SMOKE/FUMES/AVNCS SMOKE”?

A

OXY MASK/GOGGLE—USE/100%/EMERG


196
Q

Which of the following are memory items for “STALL WARNING​ AT LIFT-OFF”?

A

​THRUST—–TOGA

PITCH​ Attitude—–15°

BANK—–WINGS LEVEL

197
Q

Which of the following are memory items for “Windshear​ WARNING -​ ​PREDICTIVE Windshear” when Airborne?

A

THR LEVERS—–TOGA​

AP (if engaged)—–KEEP ON​

SRS ORDERS—–FOLLOW ​​

198
Q

Which of the following are memory items for “Windshear​ WARNING -​ ​Reactive​ Windshear” for AIRBORNE, INITIAL CLIMB, or LANDING?

A

THR LVRS​ AT​ TOGA—–SET or CONFIRM​

AP(if engaged)—–KEEP ON​

SRS ORDERS—–FOLLOW

199
Q

​Which of the following are memory items in the event of​ an “UNRELIABLE ​SPEED​ INDICATION”?

A

​AP/FD—OFF

A/THR—OFF

Below THR RED​ ALT—–15°/TOGA

Above THR​ RED​ ALT and Below FL 100—10°/CL

​Above THR​ RED​ ALT and Above FL 100—5°/CL

FLAPS—Maintain Current CONFIG​

FLAPS (if​ CONF FULL)—SELECT​ CONF​ 3 AND Maintain

SPEEDBRAKES—CHECK​ RETRACTED

L/G—UP​

200
Q

Which of the following are memory items in the event of​ a “EGPWS ​WARNING”?

A

AP—–OFF

PITCH——PULL UP​

THRUST LEVERS——TOGA

201
Q

Which of the following are memory items in the event of​ a “TCAS ​WARNING”?

A

AP (if engaged)—OFF

BOTH FDs—OFF

Respond promptly and smoothly to an RA by adjusting or maintaining the pitch, as ​required, to reach the green area and/or​ avoid the​ red area of the vertical speed scale.

202
Q

Which of the following are memory items in the event of​ an “EMERGENCY ​DESCENT”?

A

CREW OXY MASK—–USE

SIGNS—–ON​

EMER DESCENT—–INITIATE

​If A/THR not Active, THR​ LEVERS—–IDLE

SPD​ BRK—–FULL

203
Q

Which of the following are memory items in the event of​ a “STALL ​RECOVERY”?

A

NOSE DOWN PITCH CONTROL—–APPLY

BANK—–WINGS LEVEL​

THRUST—–INCREASE SMOOTHLY AS​ NEEDED

SPEEDBRAKES—–CHECK​ RETRACTED​

FLIGHT PATH—–RECOVER SMOOTHLY​

​If clean configuration and below 20,0000 feet, FLAP 1—–SELECT​

204
Q

Which of the following are memory items in the event of​ a “Windshear​ ​WARNING​ - Reactive Windshear” If after V1?

A

THR LEVERS—–TOGA

REACHING VR—–ROTATE

SRS ORDERS—–FOLLOW

205
Q

Which of the following are memory items in the event of​ a “Windshear​ ​WARNING​ - PREDICTIVE Windshear” Landing?

A

GO​ AROUND—–Perform

AP (IF ENGAGED)—–KEEP ON