CL350 AFM/AOM Limitations (NICE TO KNOW) Rev0124 Flashcards
Learn aircraft limitaions
1
Q
AOM Required Fuel Quantities:
1. 45-min IFR Reserve
2. Hot Spare
3. Inclement Wx
A
- 45-min IFR Reserve: 1850 lbs
- Hot Spare: 6000 lbs
- Inclement Wx: 6000
2
Q
Ice and Rain Protection
Ground Operations
When visible moisture is present or operating on contaminated surfaces
A
OAT +10° or below:
L and R Engine - On
Wing - Off
OAT +5° or below:
Both Eng & Wing - On
AOM 9.16
3
Q
Runway Requirements
Minimum Runway Width
A
70ft
4
Q
Max Runway Slope for Takeoff and Landing
A
+2% uphill
-2% downhill
5
Q
Runway Requirements
Ops Review Required if contaminated length is less than?
A
5500’
6
Q
Specific Airport Restrictions
A
Roadtown, BVI (TUPJ)
Length 3957’ / Width 98’
Day Only
Dry Dpeartures Only
7
Q
RVSM Airspace
Operational Systems Requirements
A
Autopilot (1)
Altitude Alerting Device (1)
ATC Altitude Reporting Transponder (1)
Air Data Computer (2)
Pitot Probe Heaters (2) on probes linked to ADC in use
8
Q
Takeoff Weight
Maximum Takeoff Weight is limited by the most restrictive of the following:
A
- Max certified Takeoff Weight
- Max Runway-limited Takeoff Weight
- Tired Speed and Brake Energy Limit Weights
- Maximum Takeoff Weight (Climb Limited)
- Obstacle Clearance, En Route and Landing Weight Limitations
9
Q
Landing Weight
The maximum landing weight is limited by the most restrictive of the following:
A
Max certified landing weight
Max landing weight (Runway length plus obstacle)
Max Landing weight (climb limit or brake energy limits)
10
Q
Max Zero Fuel Weight
A
28,200 lbs
11
Q
Baggage Compartment Placards
A
Weight limits are placarded above each compartment
12
Q
Max Takeoff and Landing Pressure Altitude
A
10,000’
13
Q
Max Flap Extension Altitude
A
18,000’
14
Q
Max Altitude for Gear Extension
A
18,000’
15
Q
Min Takeoff Weight
A
25,000 lbs
(due to Vmcg)
16
Q
Min Flight Weight
A
24,800 lbs
17
Q
Vmo (above 8000’)
A
320 KIAS
18
Q
Mmo
(above 29,475’)
A
.83 mach
19
Q
Vmo (up to 8000’)
A
300 KIAS
20
Q
Max Tire Groundspeed
A
182 kts
21
Q
Minimum Control Speed
Vmcg (Flaps 10/20)
A
Vmcg Flaps 10: 115 kts
Vmcg Flaps 20: 114 kts
22
Q
Minimum Control Speed
Vmca (Flaps 10/20 takeoff)
A
Vmca Flaps 10 (takeoff): 110 kts
Vmca Flaps 20 (takeoff): 109 kts
23
Q
ECS (Air Conditioning) limitations during ground ops
A
Do not select the AIR SOURCE switch TRIM AIR ONLY while the aircraft is on the ground.
PACK must be operating when electrical power is on for more than 30 minutes and the OAT is above +40C.
24
Q
Pressurization (psi)
Max Differential
A
9.4 (S/N 20886 and before)
10.1 (S/N 20887 and later)
25
Pressuriaztion (psi)
Max Negative
-.5PSI
26
OXYGEN QUANTITY LOW
<700L O2 Remains
27
Crew and Pax Oxygen Masks
Crew and Pax oxygen masks are not approved for use above 40,000' cabin altitude.
Prolonged operation of Pax masks above 25,000' cabin altitude is not recommended.
28
APU Limits:
Max Pressure Altitude to start left engine
9000' (pressure altitude)
29
APU Operating Restrictions (4)
Do not operate the APU under the following conditions:
* During ground de/anti-icing procedures
* Above 37,000'
* Do not use generator above 30,000'
* Do not use bleed air above 20,000'
30
Autopilot Limitations:
Glidepath Angle Limits
If glidepath angle is more than 3.5degrees, disengage autopilot by 160'
*Normal precision approach glidepath: 80'
31
Autopilot Limitations:
5G Limitations
For 5G non-tolerant aircraft operating in the contiguous US airspace, autopilot operation on approach below 1000' is prohibited
32
Max Generator Load
Continuous:
In flight, with 2 or 3 generators operating: 400A
On ground, one generator operating 400A
*Caution using hydraulics with only APU Gen operating
In flight, one generator operating: 500A
Transient (5 minutes): 600A
Do not takeoff with Battery temperature below -20C
33
Electrical Load Limitations:
1 Generator operating
500A
34
Electrical Load Limitations:
Transient (5min)
600A
35
Min airspeed and altitude for Flight Spoiler Extension
Vapp +8
Min 500' AGL
Straight-In Approach (Vref min)
Vapp = Vref+8
Circling Approach (ref+10min)
Vapp = Vref+10+8
Do not select EMER except during emergency conditions or when required by procedure.
36
Max Fuel Quantity:
Pressure Refueling
Gravity Refueling
14,150lbs Pressure Refueling
13,000lbs Gravity Refueling
37
Max Fuel Imbalance
Total fuel \>13,700 = 250 lbs max
Total fuel 10,000-13,700 = 315 lbs max
Total fuel 10,000-4,700 = 450 lbs max
Total fuel \<4,700 = 600 lbs max
38
Min Go Around Fuel
500 lbs per side
(1000 lbs total)
\*Collector tanks hold 500lbs each.
39
Max Fuel Imbalance During Gravity Refueling
250lbs
40
Max single-point refueling pressure
55 psig
Defuel limited to -8 psig
41
Max Bulk Fuel Temp for Takeoff
+50C
With wing bulk fuel temp at +45C or above min fuel load for takeoff is 2,800 lbs
With \<1,000 lbs of fuel per side do not operate engines for more than 30 minutes.
42
Min Bulk Fuel temp, Jet A
-30C
43
Cockpit Speaker Mute System
* When cockpit speakers are muted, both pilots must use headsets
* When one pilot removes headset, select COCKPIT SPEAKER MUTE - OFF
44
Ice and Rain Protection
Frost limitations
*NetJets adheres to the clean wing concept.
Takeoff is prohibited with frost, ice snow or slush adhering to any critical surface (wings, horizontal stabilizer, control surfaces, engine inlets, and upper surface of the fuselage).
Takeoff is permitted with frost adhering to:
a) the underside of the wing when caused by cold soaked fuel; or
b) the upper surface of the fuselage.
45
Ice and Rain Protection
Anti Ice System Required Use
During Flight Operations
1 When visible moisture is present or operating on contaminated surfaces
And:
TAT +10° or below:
Then:
L and R Engine - On
Wing - Optional
Or
2 When visible moisture is present or operating on contaminated surfaces
And TAT +10° or below:
And
If ICE DETECTED and ≤210kts
Then:
ENG and WING Anti-Ice must be selected ON
*Anti Ice Systems Min Usage Temp
SAT -40C or colder
46
Ice & Rain Protection
Takeoff procedure after deice operations with Type II, III, and IV Anti-icing Fluids
The wing anti-ice system must only be selected ON, if required, just prior to thrust increase for takeoff.
47
Anti-Ice Operation:
On Ground with OAT 5C or Below, Just Prior to Takeoff
OAT 5C or below:
* L&R ENG - ON
* Wing - ON*
| *If type II, III, or IV fluid has been applied, select ON just prior to
48
Icing System Operation Limitations:
Min Temperature - L&R Wing/ENG
SAT -40C
49
Required Anti ice if ICE DETECTED EICAS message is displayed or in icing conditions with airspeed below 210kts
WING must be selected ON
50
Min Operating Temperature
-4OC at pressure ALT below 14,000'
51
Anti-Ice Operation:
In Flight, TAT 10C or Below to SAT <-40C
TAT 10C or below:
L&R ENG - ON
Wing - ON (optional)
| if SAT is -40C, Anti-ice systems - OFF
52
Anti-Ice Operation:
On Ground with OAT 5C or Below, Just Prior to Takeoff
OAT 5C or below:
* L&R ENG - ON
* Wing - ON*
| *If type II, III, or IV fluid has been applied, select ON just prior to
53
Max Approach Glide Path Angle
Operations with a glidepath angle greater than 4.5 degrees or greater is prohibited.\*
\*Glidepath angle further limited at airport elevations above 5,000' MSL. see chart , figure 02-01-1
54
Configuration for holding while in icing conditions
Flaps 0
(No Flaps Extended)
55
If a rejected takeoff is performed, or a quick turn is expected, what limitations might be exceeded?
Brake Energy
(Review Charts)
56
Maneuvering Load Factors
Flaps up = +2.6g to -1.0g
Flaps extended = +2.0g to 0.0 g
57
Use of FMS V-speed data
Prohibited for temperatures above ISA +33C
58
Max Latitudes for FMS navigation
Prohibited south of 60 degrees South latitude.
Prohibited North of 73 degrees north latitude and for Canadian Northern Domestic Airspace.
59
Minimum FMS sources for Navigation
FMS navigation prohibited when not receiving:
One GNSS; or
Two DME's; or
One VOR/ DME; or
One IRS
60
RNP Operations
Required CDI Scales
RNP APCH = 0.3nm
Basic RNP = 1.0nm
RNP-2 = 2.0nm
RN-4 = 4.0nm
RNP-10 = 4.0nm
61
Max RNP Leg Lengths
When conducting RNP navigation operations the length of each individual flight plan leg or between the aircraft and the TO waypoint must not exceed:
BASIC RNP-1...............50nm
RNP-2...........................400nm
RNP4 or RNP-10.........500nm (Oceanic)
note: pilot defined waypoints must not be used to create individual legs shorter than the limiting length.
62
FMS messages which must not be annunciated for RNP operations
NO APPR (FMS A1 ON PFD)
LOI (FMS A1 ON PFD)
LOSS ON INTEGRITY (on CDU)
GNSS NOT AVAILABLE (on CDU)
GNSS-FMS DISAGREE (on CDU)
63
FMS Limitations:
SmartPerf Restrictions
*Primary means of calculating PDCS is iPreFlight Genesis
* Both Flight Management Computers must be operating
* Performance data, ETE/ETA and Fuel Remaining information are advisory only
* SmartPerf not approved for operations at airports above 8000' pressure altitude
* When comparing FMS and PDCS derived data, do not mix performance information
* When calcualating ALD on contaminated runways use QRH or PDCS correction factors
64
FMS Limitations:
Latitude Navigation Limitation
Do not use the FMS for the following:
* Navigation at latitudes South of 60deg South
* Navigation at latitudes North of 73 and for Canadian Northern Domestic Airspace
65
VNAV Guidance Limitation
VNAV vertical guidance is prohibited when the barometric altitude is corrected to the landing field elevation (QFE).
66
RNP operations down to LPV minimums are prohibited when these messages are displayed:
Red boxed "VNV" (vertical deviation scale on PFD)
NO APPR (on PFD)
EFIS MISCOMPARE (CAS messge)
EFIS COMP INOP (CAS message)
LPV NOT AVAIL (on CDU)
67
FMS messages which prohibit RNAV operations
FMS DR (PFD, MFD or CDU)
IRS ONLY (PFD, MFD or CDU)
VOR/DME ONLY (CDU) OR V/D ONLY (PFD)
VOR/DME DIST\>40.0 NM ( CDU)
CHK POS (PFD OR CDU)
68
RNP LPV Operations
Required Equipment
Dual PFD
Dual GNSS with SBAS
Dual FMC
69
FMS Limitations:
SmartPerf Restrictions
*Primary means of calculating PDCS is iPreFlight Genesis
* Both Flight Management Computers must be operating
* Performance data, ETE/ETA and Fuel Remaining information are advisory only
* SmartPerf not approved for operations at airports above 8000' pressure altitude
* When comparing FMS and PDCS derived data, do not mix performance information
* When calcualating ALD on contaminated runways use QRH or PDCS correction factors
70
FMS Limitations:
NAV RADIO SELF TEST
Do not initiate NAV RADIO SELF TEST from either NAV radio tuning page on the FMS CDU or MFD nav radio during flight
71
FMS Limitations:
Use of RNAV flight procedures
MUST be retrieved from current database
(Cannot be built by user)
72
FMS Limitations:
En route & Terminals Ops
Current database required or Pilot-verified waypoints
73
FMS Limitations:
Tuning Localizer
Do not tune a localizer on the TUNE page using the identifier only
74
FMS Limitations:
CPDLC INSERT MOD Limitation
Do not use CPDLC INSERT MOD when within 2 minutes of a TO waypoint
75
FMS Limitations:
NAV RADIO SELF TEST
Do not initiate NAV RADIO SELF TEST from either NAV radio tuning page on the FMS CDU or MFD nav radio during flight
76
Standby Instrument Localizer
Prohibited to use standby instrument localizer guidance during localizer backcourse approaches
77
FMS Limitations:
FPLN WIND Limitation
Do not select FPLN WIND update from the ROUTE MENU
78
FMS Limitations:
In Flight Limits
Do not accomplish the following in flight:
* Load pilot routes from the PILOT ROUTE LIST
* Upload flight plansfrom ROUTE MENU (FPLN RECALL)
79
FMS Limitations:
FPLN UPLINK
Do not use in flight. Must be completed or canceled before taxiing
80
FMS Limitations:
CPDLC FLight Plan Updates
Ensure flight plan is loaded in FMS before updating a flight plan through CPDLC
81
FMS Limitations:
Single FMS Restriction
Single FMS restricted to no more than two MFD MAP or HSI displays
82
FMS Limitations:
CPDLC Autoload Restriction
Do not use CPDLC autoload for any clearance containing RTA constraints
83
Standby Compass Use Requirement
L and R WHSLD/WINDOW switches must be temporarily selected OFF while the standby compass is being used.
84
IRS Alignment
Following a successful initial alignment, do not manually re-enter the position in the FMS CDU either immediately before, or immediately after aircraft motion.
If this has occurred, a complete normal shutdown and restart of the aircraft and IRSs must be completed. Failure to do so may lead to a total IRU loss during subsequent flight legs.
85
Max Operating OAT
+50C at sea level
Max temp reduces as pressure altitude increases
Max Temp is +34C at 8,000' (see chart)
86
Fuel transfer systems
Power and Gravity transfer valves shall be selected off for takeoff.
87
Max ITT
Ground Start
650°
88
Max ITT
Air Start
800°
89
Max ITT
Max Reverse
955°
90
Max ITT
Max Continuous
950°
91
Max ITT
Takeoff
955°
\*normal takeoff power limited to 5 minutes
92
Max ITT
APR
955°
APR power (OEI) is limited to 10 minutes
\*use it as necessary during an emergency
93
Max Oil Temp
138°
94
Min Oil Temp:
1. Engine Ground Start
2. Engines Above Idle
3. Takeoff Power
Min Oil Temp:
1. Engine Ground Start -40C
2. Engines Above Idle +5C
3. Takeoff Power +14C
*Between +5C and +14C engines may be operated up to but not including CLB power.
95
Min Oil Pressure - Idle
28 PSI
96
Max N2
Takeoff & Max Continuous
98.0%
97
Max N1
1. APR & Takeoff
2. Max Continuous
3. Max Reverse
1. APR & Takeoff 96. 8%
2. Max Continuous 96. 5%
3. Max Reverse 70.7%
(Auto reduced @ <85kts)
98
Min N2 - Idle
46.0%
99
Engine Cranking
The engine may be motored for up to 5 minutes, followed by a cooling period of 15 minutes.
\*This is different than a start
100
Thrust Reverser Operation
Paved surfaces only
Do not attempt to:
Deploy in flight
Back up the aircraft
Use for touch and go landings
Use above idle thrust below 40 KIAS.
101
Max APU RPM
108%
102
Max APU EGT
Start
973°
103
Max APU EGT
Normal Ops
718°
104
Overspeed Inspection Requirements
A visual inspection of the aircraft is not required when an overspeed event occurs under the following conditions:
* Level flight
* No turbulence
* Landing gear and flaps retracted
* Did not exceed the following: Vmo+15kts, or Mmo+.03
