Chapter 9 of AOM Flashcards
1
Q
9.2.1
45 min fuel requirement per Netjets
A
2019 lbs
2
Q
9.2.1
Minimum Release Fuel
A
4000 lbs
3
Q
9.2.1
Hot Spare Required Fuel
A
8500 lbs
4
Q
9.2.1
Emergency release fuel
A
1500 lbs
5
Q
9.2.2
Minimum dry runway length for release
A
4500 feet
6
Q
9.2.2
Minimum runway width for release
A
75 feet
7
Q
9.2.2
Max runway slope for release
A
(+-) 2%
8
Q
9.2.2
Chief Pilot/ACP Approval required if runway length is less than: (dry/wet)
A
Dry: Less than 5000 feet Wet: Less than 5800 feet
9
Q
9.2.2
What is the foot note (1) with regards to minimum length required for release
A
Upon arrival, land if LPA calculated length is less than the landing distance available
10
Q
9.2.3 (Red Letter)
Max crosswind for Dry and Wet Runway
A
24 knots
11
Q
9.2.3 (Red Letter)
Max Crosswind Fair/Medium Contaminated runway conditions
A
15 knots
12
Q
9.2.3 (Red Letter)
Max crosswind for poor runway conditions
A
10 knots
13
Q
9.2.4 (Red Letter)
Max tailwind
A
10 knots
14
Q
9.2.5
What is the maximum Mach number in RVSM
A
.83 Mach
15
Q
9.3.3 (Red Letter)
Max Certified Ramp and Taxi weight
A
48,300 lbs
16
Q
9.3.3 (Red Letter)
Max Certified Takeoff weight
A
48,200 lbs
17
Q
9.3.3 (Red Letter)
Max Certified Landing weight
A
38,000 lbs
18
Q
9.3.3
Max Certified Zero fuel weight
A
32,000 lbs
19
Q
9.3.4
Max weight in the baggage compartment
A
900 lbs
20
Q
9.4 (Red Letter)
Max Certified Altitude for Operations
A
41,000 feet
21
Q
9.4
Max Certified Pressure Altitude for Takeoff and Landing
A
10,000 feet
22
Q
9.4 (Red Letter)
Max Certified altitude for Flaps Extended (Odd number?)
A
15,500 feet
23
Q
9.4
Max Certified altitude for landing gear extended
A
20,000 feet
24
Q
9.4
Minimum Certified altitude for use of Flight Spoilers
A
300 feet
25
9.5
Minimum temperature for takeoff
-40 degrees C
26
9.5
Maximum temperature for takeoff and landing
ISA +35
27
9.5
What does the AOM ask you to refer to with respect to Altitude and temperature operations
Refer to the AFM
28
9.6 Vfe (**Red Letter**)
Max airspeed for flaps 20
231 knots
29
9.6 Vfe (**Red Letter**)
Max speed for flaps 30
197 knots
30
9.6 Vfe (**Red Letter**)
Max speed for flaps 45
189 knots
31
9.6 Vle (**Red Letter**)
Max landing gear extended speed (knots/mach)
250/.7
32
9.6 Vlo (**Red Letter**)
Max landing gear operating speed (knots/mach)
197/.6
33
9.6
Max tire speed
182 knots
34
9.6 Vturb (**Red Letter**)
Max Turbulent air penetration speed (knots/mach)
280/.75
35
9.7
Max press differential
9.2 psi
36
9.7
Max negative relief
-0.5 psi
37
9.7 (**Red Letter**)
Max Press Differential for taxi and takeoff
0.2 psi
38
9.7 **(Red Letter**)
Max Press Differential for Landing
0.2 psi
39
9.8
With respect to Oxygen duration for over water ops what does the AOM ask you to refer to?
Oxygen Duration tables in FCOM Supplemnts
40
9.8
Max number of pax including lap children
14 due to number of installed oxygen masks
41
9.9.1
What are the time restrictions for starting the APU using the aircraft batteries on the ground or in-flight
Three 30-second start attempts of continuous cranking, followed by a 20 minutes of cooling time. Followed by two further 30-second attempts. If not successful do not attempt additional starts for at least 35 minutes
42
9.9.1
What are the time limits for starting the APU with a ground power unit (GPU)
Two 15 seconds start attempts of continuous cranking, followed 20-minutes of cooling time. Two further 15-second attempts of continuous cranking If not successful do not attempt additional starts for at least 35 minutes
43
9.9.1 (**Red Letter**)
How many APU start attempts in an hour
3
44
9.9.1 (**Red Letter**)
What is the Max altitude for starting the APU
20,000 feet
45
9.9.1
Minimum Temperature for starting the APU
-40 degrees C
46
9.9.1
Maximum Temperature for the APU during start
974 degrees C
47
9.9.1 (**Red Letter**)
Maximum operating altitude for the APU Bonus: does this include bleed air?
20,000 feet No. 15,000
48
9.9.1
Can you use the APU for single engine in-flight restart
APU use prohibited
49
9.9.1 (**Red Letter**)
Maximum altitude for bleed air use
15,000 feet
50
9.10
Do not use the Autopilot for what three things
Takeoff
Landing
Any approach with a glidepath angle greater than 40
51
9.10. Autoflight
What are the Autopilot Minimum Altitude (AGL):
After takeoff
Cat I ILS or LPV (GS less than 5.30)
IPA to MDA
320 ft
80 ft
320 ft
52
9.11.1 Electiral (Batteries)
Minimum votage for engine start or APU start
22 v
53
9.11.2 AC Generator Load Limits
What is the Generator load limit from
0 to 20,000 feet (Main / APU)
20,001 to 35,000 feet (Main / APU)
Above 35,000 feet
Main 30 / APU 30
Main 30 / APU 0
Main 25
54
9.11.3 DC TRU Load Limits
Maximum Continuous
100 amps
55
9.12 External Lights
What are the limitation on RECOG TAXI LTS
Do not illuminate while the aircraft is not moving
56
9.12 External Lights
What is the limitation on the Landing Lights
Do not illuminate on the ground, except for takeoff or landing
57
9.14 Fuel
What is the fuel quantity in lbs for the left or right main tanks
4,860 lbs each
58
9.14 Fuel
What is the fuel capacity of the Auxiliary tank
7,168 lbs
59
9.14 Fuel
What is the fuel capacity of the tail tank
3,112 lbs
60
9.14 Fuel
What is the total fuel capacity (Pressure fueling) of all the tanks (**Red Letter**)
20,000 lbs
61
9.14 Fuel
What is the total fuel capacity if Gravity fueling (aircraft level)
Reduce pressure fueling weight by 7%
62
9.14 Fuel
Fuel imbalance (**Red Letter**)
What is the max fuel imbalance during Taxi, Takeoff and Landing
400 lbs
63
9.14 Fuel
Fuel imbalance (**Red Letter**)
What is the max imbalance during flight
800 lbs
64
9.14 Fuel
What is the Minimum fuel1 per tank for go-arounds
500 lbs
1 Bank and pitch must be limited to wings level and 100 nose up
65
9.14.1 Auxiliary Tank Fuel Load Restrictions
What are the restrictions for the Aux tank
See AOM page 9-7
66
9.14.2 Fuel Temperature Limitation
Do not takeoff if engine fuel temperature is below what temperature
BONUS: Where do you find this temperature reading
Below 5o
On the EICAS synoptic "Summary" page
67
9.14.2 Fuel Temperature Limitations
What temperature must Bulk fuel stay above
Must remain above it applicable freezing point
68
9.14.3 Fuel Jettison
What are the 2 limits for fuel jettison
1. Flap must be 0
2. Do not jettison in known lightning conditions
69
9.14.4 Fuel transfer
Can you takeoff with fuel transfer on
No. Must be off during takeoff
70
9.14.4 Fuel Transfer
During normal Operation can you use the tail tank transfer system as a center of gravity conrol device
No. During normal operations it must remain in the automatic mode
71
9.14.4 Fuel Transfer
During manual transfer operations how do you determin Aux Tank Quantity when the Tail Tank contains greater than (1) 1200 lbs (2) less than 1200 lbs (Table 9.16 : Page 9-8 of the AOM)
1. 2.75 x tail tank qty
2. 2.2 x tail tank qty
72
9.14.4 Fuel Transfer
Can you manually transfer tail tank fuel with more than 7000 lbs of fuel in the Aux tank
No, do not do this...
73
9.14.4 Fuel Transfer
What is the **Caution** associated with manual tail tank fuel transfer
Continuously monitor aux tanks quantity for overfill
74
9.16.1 Ice and Rain Protection
What are the 3 things for icing conditions exist on the ground when
1. SAT is 10o or below
2. Visible moisture (rain, snow or vis less than 1 sm) is present
3. Operating on contaminated surfaces
75
9.16.1 Ice and Rain Protection
What are the 3 things for Icing conditons to exist in flight
1. EICAS mssage ICE is displayed
2. TAT is 10o C or below
3. Visiable moistrue (rain, snow or vis lest than 1 sm) is present
Except when SAT is -40o C or below
76
9.16.1 Ice and Rain Protection
What is the restriction pertaining to flight in freezing rain
Prohibited
77
9.16.2/3 Engine/Wing (**Red Letter)**
In accordance with Chp 4 para 6.4 operate COWL's on when the temp on the ground is...
OAT 10o C or below
78
9.16.2/3 Engine/Wing (**Red Letter**)
In accordance with Chp 4 para 6.4 operate COWL's on and Wings Norm2 when the temp on the ground is...
OAT 5o C1 or below just prior to takeoff
1 Anytime temp is 5o C or below, even when all of the conditions above are not present, operate WING anti-ice during taxi. Turn off prior to takeoff.
2 If anti-ice fluid was applied select NORM prior to takeoff
79
9.16.2/3 Engine/Wing (**Red Letter**)
In accordance with Chp 4 para 6.4 operate COWL's on, Wings Norm when the temp inflight and below 22,000 feet is...
TAT 10o or below3
3 Unless SAT is -40o C or below
80
9.16.2/3 Engine/Wing (**Red Letter**)
In accordance with Chp 4 para 6.4 operate COWL's on, Wings Norm when the temp inflight and above 22,000 feet is...
TAT 10oC or below3 and ice detector has failed
3 Unless SAT is -40o C or below
81
9.16.4 Probes
What is the limitation on the ground with regards to Probe heat
Limited to 2 min when the temp is 15o C or greater
82
9.17.1 Display Unit Operating Temperature
What is the restrictions on Display Units when on the ground and the temperature exceeds 40o C
Do not power on for more than 30 min unless one air conditioning pack is operating and pax door is closed
83
9.18.3 Brakes
What is the min turn time with regards to breaks not including RTO's
15 min
Refer to AFM for RTO brake cooling times
84
9.19.3 Synthetic Vision System (SVS)
Can you use SVS for navigation
No
85
9.19.3 Sysnthetic Vision System (SVS)
When operating outside WGS-84 and NAD-83 what must you do with SVS
Deselect SVS prior to FAF
86
9.16.3 Synthetic Vision System (SVS)
When must you de-select SVS
When conducting an approach to a runway **not** in the FMS flight plan (e.g., side-step maneuver)
87
9.19.1 Electronic Flight Instrument System (EFIS)
When must you **not** use MAP PLAN display for navigation
When operating north of 70N or south of 70S
88
9.19.1 Electronic Flight Instrument System (EFIS)
OBSTACLE symbols on MFW MAP are to be used for...
Situational Awareness only
89
9.19.4 Integrated Flight Imformation System (IFIS)
Can you use IFIS Charts databases when **not** current
Use is Prohibited
90
9.19.4 Integrated Flight Information System (IFIS)
Can Geopolitical boundaries, Controlled and Special Use airspace on the MFD MAP be used for navigation
Use is Prohibited
91
9.19.4 Integrated Flight Information Systems (IFIS)
Can the aircraft sysmble on any charts (apprach or taxi) be used for navigation or precision maneuvers on the ground
Use is Prohibited
92
9.19.5 Terrain Awareness System (TAWS)
What three countries does the TAWS database accunt for known man-made obstrucions
Canada
US
Mexico
93
9.19.5 Terrain Awareness Warning System (TAWS)
If landing at an airport **not** contained in the TAWS database what must be done with the TAWS
Select TAWS TERRAIN OFF
94
9.19.5 Terrain Awareness Warning System (TAWS)
If QFE operations with no GPS sensors available what must be done with TAWS
Select TAWS TERRAIN OFF
95
9.19.5 Terrain Awareness Warning System (TAWS)
Can you navigate based on the terrain awareness display
No
96
9.19.6 RNAV and RNP Operations
The aircraft is equipped with the Rockwell Collins Pro Line 21 Avionics System. What Table in the AOM can you find authorized IFR Operations
Table 9.17
97
9.19.7 FMS
Can you use the FMS as the primary source of navigation during Dead Reckoning operations
No
98
North of 73o and Candadian Northern airspace flights can the FMS be used as the primary source of navigation
No
99
9.19.7 FMS
In flight can you use the FPLAN RECALL or laod a route from PILOT ROUTE within the FMS
No
100
9.19.7 FMS
Is tuning NAVAID using identifier only on the FMS authorized
No
101
9.19.7 FMS
To retrieve approaches from the FMS does the database have to be current
Yes
102
9.19.7 FMS
To use the FMS for terminal operations and en route must the database be current or pilot-verified
Yes
103
9.19.7 FMS
To conduct dual FMS approaches must the flight plans be identical
Yes
104
9.19.7 FMS
To continue an approach past the FAF using the FMS what must be displayed on the PFD
APPR
105
9.19.7 FMS
For approach guidance while conducting appraches using WGS-84 or NAD-83 coordinates reference data the FMS must use input from were
GPS
106
9.19.7 FMS
If two air data computers are available is FMS thrust data primay
Yes
107
9.19.7 FMS
If two flight management computers are available is FMS V speed informations primary
Yes
108
9.19.7 FMS
RNP operations require verification of PFD CDI scale annuciation, what table in the AOM can you reference
Table 9.18: RNP Scale Limits
109
9.19.7 FMS
If the FMS message LOSS OF INTEGRITY is displayed can you continue RNP operations
No, Prohibited
110
9.19.7 FMS
If the GNSS-FMS DISAGREE message is displayed on the FMS can you continue RNP operations
No, Prohibited
111
9.19.7 FMS
If NO APPR is displayed on the FMS can you continue RNP operations
No, Prohibited
112
9.19.7 FMS
If the message UNABLE RNP is displayed can you continue RNP operations
No, Prohibited
113
9.19.7 FMS
Is the FMS fuel and range information advisory information or Primary infromation
Advisory only
114
9.19.7 FMS
Can operations be predicated upon Required Time of Arrival (RTA) or fuel remaining calculations
No
115
9.19.8 VNAV
Using QFE barometric altitudes can you use VNAV
No
116
9.19.8 VNAV
After go-around can I use VNAV
No, not until completion of the missed approach procedure
117
9.19.8 VNAV
During climb can I use VFLC (FLC with VNAV) when the airspeed reference is displayed as Mach
No, do not use VFLC
118
9.19.9 Approach
