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Challenger 605 > Limitations > Flashcards

Limitations Flashcards

1
Q

Structural Weights

Ramp TO
Landing
ZFW
Min Flight
Min Op Empty
A 
Taxi/Ramp ..... 48,300
T/O ..... 48,200
Landing ..... 38,000
ZFW ..... 32,000
Min Flight ..... 26,000
Min Op Empty ..... 22,150
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2
Q

Max Airport Pressure Altitude For T/O and Landing

A

14,000 Ft

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3
Q

Max Operating Altitude

A

41,000 Ft

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4
Q

Max OAT for T/O & Landing

A

ISA +35 C

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5
Q

Minimum OAT for T/O

A

-40 C

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6
Q

Max Runway Slope

A

+/- 2%

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7
Q

Max Tailwind

A

10 Kts

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8
Q

Max Crosswind To Use Reverse Thrust

A

24 Kts

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9
Q

Flaps Up Load Factor Range

A

-1.0G To +2.5G

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10
Q

Flaps Down Load Factor Range

A

0.0G To +2.0G

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11
Q

Max Glide Path Angle Below 1500’

A

4.49 Degrees

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12
Q

Max Gear Extension And/Or Retraction Speed (IAS / Mach)

A

197 KIAS / M .60

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13
Q

Max IAS Flown With Gear Extended & Locked

A

250 KIAS / M .70

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14
Q

Max Altitude For Alternative Gear Extension

A

20,000 Ft Pressure Altitude

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15
Q

Tire Speed Limit

A

182 Knots

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16
Q

Max Turbulence Penetration Speed (KIAS / Mach)

A

280 KIAS / Mach .75

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17
Q

Max RVSM Cruise Speed

A

Mach .83

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18
Q

Max Altitude For En Route Use Of Flaps Or Flaps Extended

A

15,500 Pressure Altitude

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19
Q

Aircraft Dimensions

Length
Wingspan
Tail Height

A

Length ….. 68 Feet 5 Inches
Wingspan ….. 64 Feet 4 Inches
Tail Height …. 20 Feet 4 Inches

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20
Q

Minimum Taxi Strip For 180 Degree Turn

A

61 Feet (w/ 3 Ft Safety Margin)

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21
Q

Safety Zone Around APU Exhaust

A

15 Feet

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22
Q

When Is A Tactile Check For Ice/Frost Required? (3)

A

ONE OF THE FOLLOWING EXIST

Outside Air Temperature Is < Or = 5C

Wing Fuel Temperature Is < Or = 0C

Atmospheric Conditions Have Been Conducive To Frost Formation

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23
Q

What Surfaces Are To Be Checked If A Tactile Check For Ice/Frost Is Required?

A

Wing Leading Edge
Wing Forward Upper Surface
Wing Rear Upper Surface

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24
Q

Takeoff Is Prohibited With Frost, Ice, Snow Or Slush Adhering To What CRITICAL SURFACES?

A 
Wings
Horizontal Stabilizer
Vertical Stabilizer
Control Surfaces
Engine Inlets
Upper Surface Of The Fuselage
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25
Q

Cowl Anti-Ice Ground Operations (ON)

A

OAT Is 10C Or Less And:

  • Visible Moisture In ANY Form Is Present (Including Fog With Visibility Less Than 1 Mile)
  • Ground Surface Are Contaminated With Snow, Ice, Standing Water or Slush
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26
Q

Wing Anti-Ice Ground Operations (ON)

A

OAT Is 5C Or Less And:

  • Visible Moisture In Any Form (Clouds, Fog Or Mist) Is Present Below 400 Ft. AGL, OR
  • Runway Is Wet Or Contaminated, OR
  • In the Presence Of ANY Precipitation (Rain, Snow, Sleet or Ice Crystals)
  • Final Taxi Prior To Takeoff If, Unless Type II, III or IV Anti-Icing Fluids Have Been Applied (Single-Engine Taxi Operations Are Prohibited In These Conditions)
  • L/R WING A/ICE Caution Message May Be Posted Or L(R) HEAT Lights May Go Out During Taxi, But Caution Messages Must Be Verified Off and WING A/ICE ON or WING/COWL A/ICE ON Advisory Message and L(R) HEAT Lights Must Be Verified ON Prior To Take-Off. If Wing Anti-Ice Is Not Required For Take-Off, It Should Be Selected OFF Just Prior To Takeoff.
  • To Prevent Wing contamination From Revers Jet Blast, Operating Thrust Reversers During Taxi Operations On Wet & Contaminated Surfaces Should Be Avoided
  • Confirmed ON For Take-Off When Ground Icing Conditions Exist
  • If Wing Is Selected ON For Take-Off, The Cowl Anti-Ice Must Also Be Selected ON
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27
Q

Rotation Rate & Pitch Attitude On Take-Off

A

Smoothly Toward The Target Pitch Attitude, Then Transition To Speed Control

Not To Exceed Rotations Rates Exceeding 3 Degrees Per Second

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28
Q

Pitch Trim Limitation

A

Pitch Trim Must Be Set According to The Airplane Computed Center Of Gravity

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29
Q

In Flight Icing Conditions & Anti-Ice Fight Operations

A

TAT 10C Or Less And Visible Moisture In Any Form Is Present, Except When SAT Is -40C Or less

Wing & Cowl Anti-Ice Systems
* Must Be ON When Ice Accretion Indicated By ice Detection System

  • Must Be On Below 22,000 FT In Icing Conditions
  • Must Be On At Or Above 22,000 FT When In Icing Conditions And Ice Detector Has Failed
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30
Q

Super-Cooled Large Droplet Icing Limitations

A

Continued Operation Is PROHIBITED In Areas Where Super-Cooled Large Droplet (SLD) Icing Conditions Exist (SLD Icing Conditions Are Indicated By Ice Accretion On The Flight Compartment Side Windows)

Wing And Cowl Anti-Icing Systems Must Be ON In SLD Icing Conditions

Leave Icing Conditions When Side Window Icing Occurs

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31
Q

Engine Limitation Regarding Bleed High Altitude

A

Above 40,000

One Air-Conditioning Unit OR Cowl Anti-Icing Must Be Selected ON For Each Engine

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32
Q

When Is Aircraft Considered Cold Soaked

A

Temperature Below -30C For More Than 8 Hours

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33
Q

Before First Flight Of Day On Cold Soaked Aircraft

A

Motor Engines 60 Seconds; Check Fan Rotation BEFORE Engine Starting Is Initiated

Actuate Thrust Reversers Until Deploy & Stow Cycles Are Less Than 5 Seconds

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34
Q

Oil Temperature Limitations

A

Minimum Starting: -40C
Maximum Continuous: 155C
Maximum Permissible: 163C (15 Minutes Maximum)

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35
Q

Oil Pressure Limitations

A 
Minimum Idle: 25 psi
Minimum Take-Off: 45 psi
Maximum Continuous: 115 psi
Maximum Transient After Cold Start:
130 psi (10 Minutes Maximum; Engine must remain at idle until pressure returns to normal range)
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36
Q

Oil Consumption Limitations

A

Maximum 6.4 oz/hr

.05 US Gallon/hr

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37
Q

Oil Replenishment Limitations

A

Engine Oil Level Must Be Checked Within 15 Minutes to 2 Hours After Shutdown

(Engines Must Be Motored If Period Exceeded)

Maximum Refill Is 2 Qt Without Dry Motoring Engine

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38
Q

Continuous Ignition MUST Be On For What Conditions?

A

Take-Off and Landing On Contaminated Runway

Take-Off With High Crosswind Components

Flight In Moderate Or Greater Rain And/Or Turbulence

Flight In Vicinity Of Thunderstorms

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39
Q

Automatic Performance Reserve (APR) Limitations

A

APR Must Be Operative Prior To Each Take-Off If Take-Off Planning Based On APR Availablility

APR Must Be Selected OFF If APR INOP Caution Message Shown & APR “Off” Performance Must Be Used

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40
Q

Maximum N2 For Starter Use Or Engagement

A

55% N2

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41
Q

Starter Cycle & Cooling Time Limitations

A

3 Consecutive Starts With 5 Minutes Cooling Between ADDITIONAL Cycles

Starter NOT To Be Used If N2 Above 55%

(BUT Dry Motoring Limits Must Be Observed)

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42
Q

Maximum ITT For Ground Starts (Thrust Levers To IDL From SHUT OFF)

A

120C

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43
Q

Maximum ITT For Airborne Starts (Thrust Levers To IDL From SHUT OFF)

A

90C

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44
Q

Dry Motoring Engine Limitations

A

Dry Motoring (Ignition OFF & Thrust Levers At SHUT OFF

Permitted For Ground AND Air Starts

First Cycle, MAX 90 Seconds Then 5 Minutes OFF

Subsequent Cycles, MAX 30 Seconds Then 5 Minutes OFF

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45
Q

When Can Thrust Reversers Be Used?

A

On Ground ONLY

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46
Q

Can You Perform A Go Around After Thrust Reversers Deployed?

A

Thrust Reversers Are Intended For FULL STOP Landings Only

Do NOT Attempt A Go Around After Thrust Reversers Are Deployed

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47
Q

Can You Back Up Aircraft Using Thrust Reversers?

A

Backing The Aircraft With Thrust Reverser Use is PROHIBITED

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48
Q

Can You Take-Off With Thrust Reverser Icon Or Caution Alert Massages On EICAS?

A

Take-Off With ANY TR Icon or Caution Alert Message Shown On The EICAS Is PROHIBITED

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49
Q

What is the N1 limitation for Thrust Reverser use on landing?

A

Reverse Thrust Is Limited To 60% N1 When Below 60 KIAS

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50
Q

Maximum Demonstrated Crosswind Component With Thrust Reverser Use?

A

24 Kts

Demonstrated On A Dry Runway AND Is Considered To Be Limiting

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51
Q

Maximum Fuel Imbalance (Taxi, Take-Off, Landing)

A

400 LB

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52
Q

Maximum Fuel Imbalance (In Flight)

A

800 LB

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53
Q

Maximum Fuel Imbalance (During Refueling)

A

2500 LB

54
Q

Maximum Fuel Quantity (Pressure Fueling/Based On 6.57 Lb/US Gallon)

A

Each Main Tank…..4860 LB
Aux Tank…..7168 LB
Tail Tank…..3112 LB

TOTAL…..20,000 LB

55
Q

Maximum Fuel Quantity (Gravity Fueling)

A

Reduced Maximum Fuel Quantity By 7%…..15,700 LB

BUT

To Avoid AUX HEAVY Message, Max Fuel Quantity…..12,500 LB

56
Q

What Is Limitation For Fuel In Aux Tank

A

Take-Off With Up To 500 LB In Aux Tank Permitted If At Least 1500 LB In EACH Wing And NO FUEL in Tail Tank

For Take-Off Weights Up To 42,400 LB With MORE Than 500 LB In The Aux Tank, Each Wing Tank Must Have At Least 1500 LB

For Take-Off Weights ABOVE 42,400 LB With MORE Than 500 LB In Aux Tank Consult The AFM Limitations Section

57
Q

Minimum Fuel Quantity For A Go Around

A

500 LB In EACH Wing Tank

Maximum Nose Up Attitude 10 Degrees

58
Q

What is normal ratio of fuel in Aux Tank to fuel in Tail Tank?

A

Fuel Distribution For Take-Off Requires The Aux Tank Be Full OR AT LEAST 2.65 times the Tail Tank Quantity

(OR PER PROVISIONAL FUEL CHART)

59
Q

What is the engine fuel temperature limitation for take-off?

A

Take-Off With ENGINE Fuel Temperature LESS THAN 5C Is PROHIBITED

Temperature Reading Taken By Probe Located At The Top Of The Each Engine Fuel Filter Housing

Readout Turns Amber Below 5C & FUEL LO TEMP EICAS Message Displayed

60
Q

What is the bulk fuel temperature limitation for take-off and flight?

A

Bulk Fuel Must Be At Least 10C Above the Fuel Freezing Point (FFP) On Take-Off AND Remain Above The FFP In Flight

Temperature Reading Is Taken From Left Main Tank (Because Right May Be Heated By APU Return Fuel)

Amber Readout AT OR BELOW -37C & BULK FUEL TEMP EICAS Message Displayed

DEPENDS ON THE TYPE OF FUEL
Jet A Freezing Point Is -40C
Jet A-1 Freezing Point Is -47C

61
Q

Are Mixing Of Fuel Grades Permitted & what are some common approved fuels?

A

Approved Fuels Include:
JetA, Jet A1, Jet B
JP-4, JP-5, JP-8
(Consult AFM For Others)

Mixing Of Fuel Grades IS PERMITTED

62
Q

What are limitations on fuel transfer valves for take-off?

A

ALL Fuel Transfer Valves Must Be CLOSED For Take-Off

63
Q

Can tail tank transfer system be used to control center of gravity?

A

In NORMAL operations, the tail tank transfer system must NOT be used for center of gravity control and must remain in automatic mode

64
Q

What is the limitation on ratio of Aux Tank and Tail Tank during manual fuel transfer mode operations?

A

If Tail Tank Quantity Is EQUAL TO OR GREATER THAN 1200 LB
* Aux Tank Quantity Must Be 2.75 Times The Aft Tank Quantity

If Tail Tank Quantity Is LESS THAN 1200 LB
* Aux Tank Quantity Must Be 2.20 Times The Aft Tank Quantity

65
Q

What is the limitation on manual Tail Tank transfer with regard to fuel quantity in the Aux Tank?

A

Manual Tail Tank Transfer NOT PERMITTED with GREATER THAN 7000 LB in Aux Tank

66
Q

Who has responsibility to monitor Aux Tank quantity during manual Tail Tank fuel transfer?

A

THE PILOT

Auxiliary Tank MUST Be Continuously Monitored For Overfill During Manual Tail Tank Fuel Transfer

67
Q

What are the limitations for fuel dumping?

A

Limited To FLAPS 0

PROHIBITED In Vicinity Of Known Lightning Conditions

68
Q

What model Auxiliary Power Unit is installed?

A

Honeywell 36-150 (CL)

69
Q

What is the minimum temperature for starting cold-soaked APU on the ground?

A

-40C

70
Q

What are the APU starting attempt limitations on battery power?

A

Limited To THREE (3) Cranking Attempts Of 30 Seconds Each, Followed By 20 Minutes Off

Followed By TWO (2) MORE Cranking Attempts Of 30 Seconds Each

If No Start, wait at least 35 minutes

71
Q

What are the APU starting attempt limitations on ground power?

A

Limited to TWO (2) Cranking Attempts of 15 Seconds Each, Followed By 20 Minutes Off

Followed By TWO (2) MORE Cranking Attempts of 15 Seconds Each

If No Start, wait at least 35 minutes

72
Q

When do you know you have an APU hung start?

A

If Not More Than 30% RPM Within 60 Seconds

73
Q

What is the pressure altitude limitation for starting the APU?

A

Ground Starting permitted up to 15,000 FT

74
Q

What is the inflight APU starting/operation altitude limit?

A

20,000 FT

75
Q

What is the bleed-air extraction altitude limit for the APU?

A

15,000 FT

76
Q

If Both Engines Are To Be Started From The APU, what limitation is there for the running engine during the start of the second engine?

A

Running Engine Limited To 70% N2

77
Q

During single engine operations, can the APU be used to start the failed engine?

A

If Single Engine, Inflight Engine Starting Via APU Bleed Air Is PROHIBITED

78
Q

If dual engine out, can the APU bleed air be used to start the first engine?

A

If double flameout, APU Bleed Air Is Authorized For Engine Starting

Engine starts via APU bleed air have been demonstrated up to 15,000 FT

79
Q

Maximum Flap Extension Speeds

A

Flaps 20…..231 KIAS
Flaps 30…..197 KIAS
Flaps 45…..189 KIAS

80
Q

Can You Side Slip The Aircraft?

A

AVOID unnecessary and large side-slips during low-speed, high-altitude cruise

Avoid rapid and large alternating control inputs, ESPECIALLY in combination with large changes in pitch, roll, or yaw (large side-slip angles)

MAY CAUSE STRUCTURAL FAILURE AT ANY SPEED

81
Q

Maximum Relief Differential Pressure (Cabin Pressurization)

A

9.2 psi

82
Q

Maximum Negative Differential Pressure (Cabin Pressurization)

A

-0.5 psi

83
Q

Maximum Differential Pressure (Cabin Pressuization) During Taxi, Take-Off and Landing

A

0.2 psi

84
Q

Before Opening Any Aircraft Door, You Must Ensure

A

Airplane Is COMPLETELY Depressurized

85
Q

Minimum Auto Pilot Engagement After Take-Off

A

320 FT AGL

86
Q

Minimum Auto Pilot Use For Visual And Non Precision Approaches

A

320 FT AGL

87
Q

Minimum Auto Pilot Use For Precision Approaches/ILS (What Is Glide Path Limit For The Approach)

A

80 FT AGL (G/P Less Than 3.5 Degrees)

160 FT AGL (G/P Between 3.6 And 4.49 Degrees)

88
Q

What Must The Autopilot Be Coupled To For RVSM Requirements?

A

The ADC Source Coupled To The Active Autopilot Must Be The Same As That Coupled To The ATC Transponder During Flight In RVSM Airspace

89
Q

What limitation is on the Bleed Air System during take-off and landing?

A

10th Stage Bleed Valves Must Be CLOSED During Take-Off And Landing If The Engine Cowl And/Or The Wing Anti-Ice Systems Are On

90
Q

Maximum APU Generator Load

A

30 KVA

91
Q

When can the APU Generator be used as a power source in flight?

A

APU Generator Use NOT Permitted In Flight UNLESS BOTH IDGS Are Offline

92
Q

Maximum IDG Generator Load

A

Below 35,000 Ft…30KVA

Above 35,000 Ft…..25KVA

93
Q

Maximum TRU Load

A

100 Amp

94
Q

Minimum Altitude Flight Spoilers Extended

A

300 AGL

95
Q

Minimum Speed Flight Spoilers Extended

A

Vref + 10 KIAS

96
Q

When Are Stick Shaker And Pusher Switch To Be ON

A

ALL Phases Of Flight

97
Q

Stall Protection Test Limitation

A

ONLY USED FOR SYSTEM TESTING, NOT INFLIGHT

98
Q

Taxi Light Illuminated Limitation

A

MUST Be Selected OFF When Airplane Is Stationary For 10 Minutes Or Longer

99
Q

Limitation If Wheel Fusible Plug Releases

A

Wheels, Brakes, Tires And The Anti-skid Speed Sensors Must Be inspected BEFORE The Next Take Off

Brake Cooling Times From Performance Section MUST Be Observed Between A Landing, OR A Low-Energy Rejected Take-Off, And A Subsequent Take-Off

100
Q

TCAS Limitations (Deviations, Maneuvers, Modes)

A

Pilots ARE Authorized To Deviate From ATC Clearance In Order To Comply With TCAS RA Commands

Pilot Shall Inform ATC Of Deviation Following The Response

Evasive Maneuvers MUST NOT Be Made Solely On Information Presented On The Traffic Display

Transponder Has Been Demonstrate ONLY For The Purposes Of Surveillance Modes A, C and TCAS Functions

101
Q

Missing Airframe An/Or Nacelle Parts

A

Operations Must Be In Accordance With The AFM As Amended By The CDL (Configuration Deviation List)

102
Q

Electrical/Avionics Equipment Temperature Limitation

A

During Ground Operations At Ambient Temperatures ABOVE 40C

Operation Of Electrical/Avionics Equipment Must Be Limited To 30 Minutes UNLESS:

  • At Least One Air-Conditioning Pack Is Operating AND
  • The Passenger Door Is CLOSED
103
Q

FMS Database Information

A

MUST BE VERIFIED AS BEING CURRENT

104
Q

Can pilot-defined FMS approaches in IMC be used?

A

NO…This is PROHIBITED

105
Q

FMS Must Be Operated In Accordance With The Latest Edition Of What?

A

Airplane Flight Manual

Flight Management System FMS 6000 Pilot’s Guide

106
Q

Operations Can Not Be Predicated On The Following FMS Performance Data

A

ETE/ETA

Fuel Remaining

These Are Advisory Only

107
Q

What Is The Limitation On FMS Flight Plans When Conducting DUAL FMS Approach Operations

A

FMS Flight Plans MUST Be Identical

108
Q

Use Of FMS Instrument Approaches Past The FAF Is Prohibited Unless

A

APPR Is Annunciated On The PFD

Might Be Different On WAAS Equipped Aircraft????

109
Q

Limitation On Use Of VNAV For V-MDA Approaches

A

Use Of VNAV Vertical Guidance Between The FAF and Missed Approach Fix Is PROHIBITED

110
Q

When Using FMS Approach Performance Data For A Runway With A Displaced Threshold

A

The Pilot Must Manually Enter The RWY LENGTH Value With The ACTUAL Available Landing Distance From A Published Chart

111
Q

Navigation By Use Of GPWS Information

A

MUST NOT Be Predicated Upon The Use OF The Terrain Awareness Display

112
Q

When Using GPWS In QFE Operations

A

If GPS is NOT available,

  • Terrain Inhibit Should Be Selected
113
Q

Limitation On Airborne Flight Information System (AFIS)

A

AFIS Must Not Be Used For Flight Planning

114
Q

Minimum Voltage Of APU Battery For APU Start

A

22V

115
Q

APU Start Cycles

A

Using Aircraft Batteries
1,2 & 3 Attempt….30 Seconds ON….20 Min OFF
4 & 5 Attempt….30 Seconds ON….35 Min OFF

Using Ground Power
1 & 2 Attempt…..15 Seconds ON…..20 Min OFF
3 & 4 Attempt…..15 Seconds ON…..35 Min OFF

116
Q

Engine Start RPM And Max ITT

A

20% Minimum

903 C 50 For Seconds

117
Q

Engine Acceleration Max ITT

A

930 C For 5 Seconds

118
Q

Engine Max Continuous N2, N1 & ITT

A

N2…..99.2
N1…..98.6
ITT…..899 C

119
Q

Engine Max Normal Takeoff N2, N1 & ITT

A

N2…..98.3
N1…..96.2
ITT…..884 C (5 Min) / 900 C (2 Of The 5 Min)

120
Q

Engine Max Takeoff APR Operating N2, N1 & ITT

A

N2…..99.4
N1…..98.6
ITT…..899 (5 Min) / 928 (2 Of The 5 Min)

121
Q

Use Of Safety Harness (Seated)

A

Above FL250 At Least 1 Pilot Must Wear A Safety Harness

122
Q

Ground Operations At Ambient Temps ABOVE 40 C

A

Operation Of Electrical/Avionics Equipment Must Be Limited To 30 Minutes UNLESS At Least One Air Conditioning Pack Is Operating AND The Passenger Door Is Closed

123
Q

Maximum Contaminant Depths

A

Standing Water…..0.25 In Takeoff / 0.50 In Landing
Slush….. 0.25 In Takeoff / 0.50 In Landing
Wet Snow….. .5 In Takeoff / 1.0 In Landing
Dry Snow….. 1.2 In Takeoff / 2.4 In Landing

124
Q

Max APU EGT On Start

A

974 C

125
Q

Max APU EGT (NOT On Start)

A

731 C

126
Q

Max APU RPM

A

110%

Auto Shut Down At 107%

127
Q

Minimum N2 For Windmilling Starts

A

N2 Greater Than/Equal To 10% 10,000 Feet And Below

N2 Greater Than/Equal To 12% Above 10,000 Feet

128
Q

Starter Assisted Cross-bleed Start Speed Envelope

A

Min 60 PSI
Sea Level To 15,000 Ft 140-300 KIAS
15,000 Ft - 21,000 Ft 200-300 KIAS

129
Q

Which Lights Can Be ON While Stationary

A

Nose Light (NOT Taxi/Recog & NOT L/R Landing)

130
Q

When Can L/R Landing Light Be Selected “ON”

A

Landing & Take Off Roll

131
Q

What is the speed limitation for operating the APU?

A

290 KIAS (Based On Chart

Challenger 605 (1 decks)

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