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Latitude Study Guide > (AOM) other than RED Limitations (Deep Dive) (AOM 1.3.0) > Flashcards

(AOM) other than RED Limitations (Deep Dive) (AOM 1.3.0) Flashcards

1
Q

Fuel Load (AOM 2.3)

A

Before Engine Start: Within 300 lbs. of FUEL TOTAL LOADED (TOT).

Prior to takeoff: Equal to or more than MINIMUM FUEL REQUIRED (MIN).

Use greater of MIN fuel or Equal Time Point (ETP) shown on flight release flight plan page.

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2
Q

Simultaneous Com 1 & Com 2 use (AOM 2.5)

A

Radio signal may become lost or degraded, preventing communications with ATC.

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3
Q

Flight Director Use (AOM 2.8)

A

If not using the flight guidance system, deselect Flight Director.

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4
Q

Automation Hands on Flight Controls and Throttles (AOM 2.8)/ (FOQA Event July 2020)

A

After takeoff and when below 2500 ft AGL (FOQA Event Newsletter) in order to monitor automation actions through tactile feedback, Inside FAF, the PF must hold the flight controls and throttle, unless other required action is necessary (e.g., selecting AFCS mode, setting auto-throttle SPD), in order to monitor the automations actions through tactile feedback.

During departure climb and approach the PF should keep their hand on the thrust levers when below 2500 ft AGL in order to actively monitor their movement should the autothrottle system enter “RETARD” mode and reduce to idle prematurely.

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5
Q

Un-commanded RETARD mode (AOM 2.8.3)

A

During all phases of flight immediately disconnect the autothrottle and manually control speed for the remainder of the flight.

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6
Q

Adjusting Vertical Speed during altitude capture (AOM 2.9.1)

A

May prevent altitude capture.

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7
Q

Prior to turning on batteries (AOM 2.12)

A

Verify gear handle is down. After selecting BATTERIES ON, verify L & R PITOT /STATIC are selected OFF.

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8
Q

Applying Power during maintenance (AOM 2.12.2)

A

Coordinate with maintenance personnel prior to applying power.

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9
Q

POWER ON Checklist (AOM 2.12.2)

A

Do not tow the aircraft during this check

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10
Q

PASS OXY (AOM 2.12.7.6.3)

A

If OFF selected, oxygen supply is unavailable to passenger masks.

If ON is selected, passenger oxygen masks are deployed. Ensure selector is unobstructed to prevent inadvertent mask deployment.

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11
Q

FOB SYNC (AOM 2.12.7.6.5)

A

Accomplish only after refueling.

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12
Q

Weather Radar to Standby (AOM 2.12.7.6.5)

A

Select Standby prior to taxi to protect the antenna. Automatic in Garmin 4.8.

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13
Q

Pilots in Seats (AOM 2.13)

A

Both Pilots must be seated in the cockpit for engine start. At least one Pilot must be seated in the cockpit while an engine is operating.

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14
Q

Minimize Turbine Blade Rub (AOM 2.14)

A

Initiate start within 1 minute of engine shutdown or wait a minimum of 10 minutes after shutdown. If the engine was operated above idle during the previous 30 minutes, operate at stabilized idle, following start, for a minimum of 2 minutes.

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15
Q

Control Lock Use after Block Out (AOM 2.16)

A

If CONTROL LOCK is set to LOCK after block out, perform a full flight control check after it is set to UNLOCK.

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16
Q

Anti-Ice Check (AOM 2.16.3.2)

A

If operating on contaminated surface, accomplish this check when stopped.

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17
Q

Full Route Clearance (AOM 2.16.4.2)

A

Review the effect of clearance changes on any previously briefed or programmed OEI escape procedure.

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18
Q

Static Run-up on painted or slippery surfaces (AOM 2.18)

A

Aircraft may skid, resulting in damage.

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19
Q

Verify Power Set for Takeoff (AOM 2.18)

A

For every takeoff, verify takeoff thrust is set prior to reaching 65 kts.

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20
Q

Noise Abatement Takeoff (AOM 2.18.2)

A

In case of emergency, disregard noise abatement requirements and resume normal takeoff procedures.

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21
Q

Use of FLC during Climb (AOM 2.19.1)

A

Flight Level Change is the only mode that provides low airspeed protection when autopilot is engaged.

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22
Q

Use of FLC during Descent (AOM 2.21)

A

When descending during any segment of an instrument or visual approach, use of FLC mode is prohibited.

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23
Q

CDFA Approach Step-down Altitude Restrictions (AOM 2.21.8.1)

A

All step-down altitude restrictions must be met. Monitor vertical profile comparing Baro-altitude against distance by using FMS distance or DME.

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24
Q

CDFA Approach below DDA (AOM 2.21.8.1)

A

Below the DDA, constant descent flight path, including synthetic glidepath derived by VNAV, does not assure obstacle clearance. Terrain and obstacles must be avoided visually.

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25
Q

Side Step Maneuver (AOM 2.21.14)

A

Do not exceed 30 Degrees of bank.
Complete maneuver no lower than 300 ft AFE.

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26
Q

Visual Approach (AOM 2.21.15)

A

Do not engage in FMS programming below 1000 ft AGL or when established on final approach within 3 nm of runway.

If cleared for a visual approach, an instrument missed approach procedure is not authorized unless it is approved by ATC.

Flight Path must be aligned with runway centerline not lower than 300 ft AGL.

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27
Q

Circle to Land (AOM 2.21.18)

A

Do not exceed 30 degrees of bank.

Conduct approach with autopilot engaged unless inoperative until descent is initiated below MDA.

While circling, use HDG mode to control lateral path and maintain visual contact with the airport at all times.

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28
Q

Missed Approach (AOM 2.22)

A

Initiate missed approach if operating in IMC and any of the following occur: Conditions for missed approach as prescribed by FAR

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29
Q

PFD Indications Necessitating Missed Approach (AOM 2.22)

A

Insert picture

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30
Q

Autothrottle Landing Performance (AOM 2.24.2)

A

Landing with autothrottle engaged adds 3 kts to airspeed at 50 ft above the threshold and 13% to actual landing distance.

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31
Q

Emergency Braking System (AOM 2.24.5)

A

Do not engage the Emergency Braking System unless total brake failure is indicated (i.e., EICAS message of a failed system affecting normal braking).

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32
Q

Generator Cooling (AOM 2.26.1)

A

Operate the engine at idle with a generator load less than 75A for four minutes prior to shutdown (small thrust increases for taxi are acceptable). This allows for generator cooling. Otherwise, a 35 minute cooling period after shutdown is required prior to restart.

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33
Q

Engine Covers (AOM 2.28.2)

A

Do not climb on the wing to install the engine inlet covers.

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34
Q

APU Max Cool (AOM 4.1.2)

A

DO not operate cockpit and cabin temperature controls in MANUAL while MAX COOL and APU BLEED AIR are selected ON. Wait 30 seconds after selecting MAX COOL to OFF before operatiterm-10ng cockpit and cabin temperature controls in MANUAL.

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35
Q

Prolonged Flight in Icing Conditions (AOM 4.2.2)

A

Avoid prolonged flight in icing conditions with the flaps or landing gear extended.

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36
Q

Wing Anti-Ice Maximum Altitude (AOM 4.2.2)

A

FL 410

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37
Q

Cold Temperature Compensation Foreign Airports (AOM 4.2.5)

A

Required when temperature below -10 degrees C.

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38
Q

Selection of Anti-ice on with type II, III, or IV application (AOM 4.2.8.7)

A

Do not select WING ANTI-ICE - ON until just prior to takeoff.

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39
Q

Tactile Inspection (AOM 4.2.8.2.9)

A

Required during ice pellet precipitation or if unable to determine if ice is present.

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40
Q

Start with Battery Power Only (AOM 5.6.3)

A

Amps must be less than or equal to 100 prior to starting the second engine.

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41
Q

(E)GPWS warning while flying the EOP (AOM 6.3.11)

A

Acknowledge the warning, verify on EOP flight path, use all available resources to avoid obstacles, and continue with EOP.

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42
Q

ADS-B Flight ID (AOM 6.7.2)

A

Confirm the flight ID is identical to the callsign filed in the flight plan.

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43
Q

Oil Service Overfill (AOM 7.3.1)

A

Add oil to above MIN and no more than 1/2 inch below MAX in sight gauge.

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44
Q

Coffee Maker (AOM 8.1)

A

Do not fill reservoir to the top as pitch attitudes during takeoff may cause spillage.

Use only coffee capsules provided by NetJets.

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45
Q

Pets with 8 Passengers On-board (AOM 9.1.1)

A

Due to aircraft configuration and emergency exit location no pets may be carried. This does not apply to service animals.

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46
Q

Interpolation of PDCS Data (AOM 9.2.1)

A

Not allowed.

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47
Q

FMS Full Performance Restrictions (AOM 9.2.6)

A

FMS Performance Data (FULL PERF) are advisory data only.

Declared distances (TORA/TODA/ASDA/LDA) that are accounted in PDCS/iPreflight Genesis are not incorporated in FMS and may impact limiting weights.

The FMS TOLD may vary from PDCS/iPreflight Genesis data due to runway surface conditions, obstacles, AFM limitations, V1 optimization, or other variables.

FMS V speeds may be used for wet or dry takeoff or landing, provided the FMS data match the PDCS/iPreflight Genesis V speeds.

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48
Q

TCAS RA vs (E)GPWS (AOM 10.5)

A

(E)GPWS warnings take precedent over TCAS RA.

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49
Q

Cabin Door (AOM 11.2.3)

A

Ensure the outer door handle push paddle remains out while the door is open and when closing to prevent damage to the outer door frame.

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50
Q

Water Barrier (AOM 11.2.6)

A

Must be in position prior to ditching.

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51
Q

45 Minute IFR Reserve Fuel (AOM 12.1.1)

A

1464 lbs. @ FL300, .72 M

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52
Q

Minimum Release Fuel Load (AOM 12.1.1)

A

2564 lbs.

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53
Q

Hot Spare Fuel Load (AOM 12.1.1)

A

4800 lbs.

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54
Q

Emergency Fuel (AOM 12.1.1)

A

1000 lbs.

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55
Q

Inclement Weather Fuel Load (AOM 12.1.1)

A

5000 lbs.

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56
Q

Minimum Runway Dry (AOM 12.1.2)

A

4000 x 70

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57
Q

Max runway slope (AOM 12.1.2)

A

0.02

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58
Q

Runway Ops Review Required (AOM 12.1.2)

A

Dry: less than 4500 ft.
Wet/Contaminated: Less than 5000 ft.
DAAP: Less than 4500 ft.
Width: Less than 75 ft.

59
Q

KVBT Restrictions (AOM 12.1.2)

A

Day Only 4426 x 65

60
Q

TUPJ Restrictions (AOM 12.1.2)

A

Day Only 3957 x 98

61
Q

Operational Equipment for RVSM Operations (AOM 12.1.5)

A

Autopilot, AAD, Transponder, 2 ADC, 2 Pitot probe heaters on the probes linked to ADC in use.

62
Q

Minimum Airspeed in RVSM (AOM12.1.5)

63
Q

Single Engine Reposition (AOM 12.1.6)

A

On uneven ramp, may be relocated to a level area to check affected engine oil level.

Aircraft is parked with the upwind engine exposed to tailwind component in excess of 10 kts, may be relocated to allow for engine start.

64
Q

Single Engine Taxi (AOM 12.1.6)

A

Taxi to another ramp on a single engine is prohibited.

65
Q

Zero Fuel Weight (AOM 12.2.3)

A

21,430 lbs.

66
Q

Baggage Compartment Smoke Detection and Extinguishing System (AOM 12.2.4)

A

Must be operational if baggage is carried in the compartment.

67
Q

Maximum Altitude Flaps Extended (AOM 12.3)

68
Q

Maximum Altitude Gear Extended (AOM 12.3)

69
Q

Maximum Altitude for Takeoff and Landing (AOM 12.3)

A

14,000 ft.

70
Q

Maximum Operating Airspeed (AOM 12.5)

A

305 kts or 270 kts below 8,000 MSL

71
Q

Maximum MMO (AOM 12.5)

72
Q

Maneuvering Speed (AOM 12.5)

A

Approximately (Spaghetti Chart Interpretation) 141 kts- 266 kts

73
Q

Maximum Tire Ground Speed (AOM 12.5)

74
Q

Minimum Speed Brakes Extended (AOM 12.5)

75
Q

Minimum Control Speed Air (AOM 12.5)

A

Flaps 1: 88 kts
Flaps 2: 83 kts

76
Q

Minimum Control Speed Landing (AOM 12.5)

A

Flaps 2 83 kts
Flaps Full: 78 kts

77
Q

Minimum Control Speed Ground (AOM 12.5)

A

Flaps 1: 88 kts
Flaps 2: 91 kts

78
Q

Normal Differential Pressure (AOM 12.6)

A

0-10.2 psi

79
Q

Maximum Differential Pressure (AOM 12.6)

80
Q

Minimum Oxygen Pressure for Dispatch

A

Insert picture

81
Q

Crewmember Oxygen Masks Sustained Operation (AOM 12.7)

82
Q

Passenger Oxygen Masks Sustained Operation (AOM 12.7)

83
Q

APU Use during de/anti-icing procedures (AOM 12.8.2)

A

Prohibited

84
Q

MAX COOL ON while manually operating cockpit and cabin temp controls (AOM 12.8.2)

A

Prohibited

85
Q

APU Use Requiring Main Cabin Door Closure (AOM 12.8.2)

A

After 45 minutes of APU operation in ambient temperatures of 30º C or greater, keep the main cabin door closed except for boarding or deplaning of crew or passengers.

86
Q

APU Automatic Shutdown (AOM 12.8.2)

A

Requires inspection of APU compartment.

87
Q

Autopilot Use Takeoff or Landing (AOM 12.9.1)

A

Do not use autopilot or yaw damper.

88
Q

Autopilot Manual Override (AOM 12.9.1)

A

Do not manually override autopilot during normal flight.

89
Q

Use of Autopilot Prohibited (AOM 12.9.1)

A

Any comparison monitor is activated.
Either PFD is in ATT or HDG reversion.
Either AHRS has failed.

90
Q

Autothrottle Use Ground ARM (AOM 12.9.2)

A

Do not use or arm during taxi. Arm only when cleared for takeoff.

91
Q

Autothrottle use with comparison monitor message (AOM 12.9.2)

A

Only when appropriate sensor reversion selected.

92
Q

Autothrottle RETARD mode (AOM 12.9.2)

A

Unavailable if Radio Altimeter is inoperative

93
Q

Autothrottle use during approach (AOM 12.9.2)

A

Set VREF +3 or greater

94
Q

Battery only Engine Start (AOM 12.10)

A

3 start attempts per hour.

95
Q

Engine Start using GPU to Assist Battery Start (AOM 12.10)

A

3 GPU start attempts drawing 1000A or more are equivalent to one engine battery start.

1 GPU start attempt drawing less than 1000A is equivalent to one engine battery start.

96
Q

Starting Second Engine with Battery Power Assisted by the Operating Engine Generator (AOM 12.10)

A

3 generator-assisted cross starts are equivalent to one engine battery start.

97
Q

Maximum APU Battery Starts Attempts per hour (AOM 12.10)

98
Q

Minimum Battery Temperature for APU Start (AOM 12.10)

A

-20 degrees C.

99
Q

Minimum Battery Temperature for Engine Start (AOM 12.10)

A

-10 degrees C.

100
Q

Maximum GPU Load (AOM 12.10)

101
Q

Maximum engine generator load (in flight or on the ground) (AOM 12.10)

102
Q

Maximum engine generator load (above 35,000 ft) (AOM 12.10)

103
Q

Maximum APU generator load (in flight or on the ground) (AOM 12.10)

104
Q

Pressure Refueling Limits (AOM 12.12)

105
Q

Max Defueling Pressure (AOM 12.12)

106
Q

Total Fuel Quantity (AOM 12.12)

A

11,390 lbs.

107
Q

Aux Hydraulic Pump Minimum Temperature for Operations (AOM 12.14)

A

Do not use auxiliary hydraulic pump in flight or when the SAT is below -40ºC.

108
Q

Aux Hydraulic Pump time of operations (AOM 12.14)

A

When used on the ground, the auxiliary hydraulic pump is limited to two minutes (cumulative) of operation in any 15 consecutive minutes. After two minutes (cumulative) of operation, allow a 15-minute cooling period.

109
Q

ENG/STAB ON Temperature Range (AOM 12.15.1)

A

10 to -35 degrees C.

110
Q

L & R WING ON Temperature Range (AOM 12.15.1)

A

5 to -35 degrees C.

111
Q

Ground Icing Conditions (AOM 12.15.1)

A

Contaminated runway or
SAT is below 10 degrees C. and
Visible moisture (clouds, precipitation, or fog with visibility less than 1 sm.) is present.

112
Q

In Flight Icing Conditions

A

RAT is 10 degrees C. or below and
Visible moisture (clouds, precipitation, or visibility less than 1 sm.) is present.

113
Q

Bleed Air Anti-ice ON (AOM 12.15.1)

A

If on for more than 30 seconds operate both engines at or above 65% N2.

114
Q

Flight in Freezing Rain (AOM 12.15.1)

A

Prohibited

115
Q

Maximum SAT for operation of Bleed Air Anti-ice with thrust lever above IDLE (AOM 12.15.1)

A

20 degrees C. Excluding Ground preflight check

116
Q

Flap Setting with Type II, III, or IV de/anti-ice fluid has been applied (AOM 12.15.2)

A

Flaps 1 maximum

117
Q

WING ANTI-ICE Operation (AOM 12.15.2)

A

Requires ENGINE/STAB ANTI-ICE to be selected ON.

118
Q

WING ANTI-ICE Operation with TYPE II, III, or IV (AOM 12.15.2)

A

ON just prior to takeoff thrust

119
Q

Maximum Altitude for WING ANTI-ICE (AOM 12.15.2)

120
Q

Aircraft Configuration in icing conditions (AOM 12.15.2)

A

Flaps up except for approach and landing

121
Q

EICAS Temperature Restrictions (AOM 12.16.1)

A

Insert picture

122
Q

Display Unit (AOM 12.16.2)

A

Do not depart if any Garmin Display Unit (GDU) is in reversion mode.

123
Q

HR Radio Use during NDB Navigation (AOM 12.18)

A

Do not transmit on HF when navigation is based on ADF.

124
Q

Taxi or Towing (AOM 12.18)

A

Do not tow or taxi until attitude and heading ground alignment is complete (90 sec for AHRS)

125
Q

GPS Approaches (AOM 12.18.1)

A

Must be retrieved from current database.

126
Q

VNAV for Flight Guidance (AOM 12.18.3)

A

VNAC guidance altitudes must be displayed on the MFD map page or GTC flight plan page.

127
Q

VNAV use when Using QFE (AOM 12.18.3)

A

Prohibited.

128
Q

GPS/GNSS Authorized Minima (AOM 12.18.4)

A

LPV
WAAS to LNAV/VNAV
Baro-VNAV to LNAV/VNAV
LNAV

129
Q

Maximum Continuous TO Thrust Static Ground Operation (AOM 12.19.2)

A

Two minutes.

130
Q

Takeoff Thrust, MCT, Cruise, and Reverse Thrust N1 (%) (AOM 12.19.2)

131
Q

Takeoff Thrust, MCT, Cruise, and Reverse Thrust N2 (%) (AOM 12.19.2)

132
Q

Takeoff Thrust, MCT, Cruise, and Reverse Thrust Maximum ITT (AOM 12.19.2)

A

920 degrees C

133
Q

Ground Idle N2 (%) (AOM 12.19.2)

134
Q

Flight Idle N2 (%) (AOM 12.19.2)

135
Q

Starting N2 (%) (AOM 12.19.2)

A

If stabilized idle not achieved within 90 sec of engine light up, as indicated by an increase in ITT, discontinue start.

136
Q

Maximum Oil Consumption (AOM 12.19.3)

A

One quart per eight hours.

137
Q

Reverse Thrust must be at idle (AOM 12.19.5)

A

Below 65 kts.

138
Q

Reverse Thrust Duration with APU running (AOM 12.19.5)

A

30 seconds

139
Q

Reverse Thrust during Touch and Goes (AOM 12.19.5)

A

Prohibited.

140
Q

Reverse Thrust to Back Aircraft (AOM 12.19.5)

A

Prohibited.

141
Q

Lavatory Pocket Door (AOM 12.20)

A

Must be latched open for taxi, takeoff, and landing.

142
Q

Minimum Fuel Uplift for Double Atlantic Bucks (Atlantic Aviation)

A

765 gallons

143
Q

Minimum voltage for battery start

A

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Latitude Study Guide (33 decks)

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