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BBD700 > Limitations > Flashcards

Limitations Flashcards

1
Q

STRUCTURAL WEIGHT LIMITATIONS

Max Taxi & Ramp Weight………?
Max Takeoff Weight …………….?
Max Landing Weight……………..?
Max Zero Fuel Weight ………….?

A 
Max Taxi & Ramp Weight 
99,750 lbs 
Max Takeoff Weight  
99,500 lbs
Max Landing Weight....
78,600 lbs 
Max Zero Fuel Weight 
56,000 lbs
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2
Q

AUXILIARY POWER UNIT

MaxRPM……………………………………..?
Max EGT During Start ……………….? Operations………………………………….? Operating Altitude……………………..?

A 
Max RPM 
106% 
Max EGT During Start 
675oC TO 1038oC
NORMAL Operations
613oC TO 732oC 
MAX Operating Altitude  45,000 FEET
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3
Q

AUXILIARY POWER UNIT: STARTING Min Temp for Cold-Soaked APU on Ground?
Max Start Attempts per Hour? Altitude: Max Starting…………………………..?
Bleed Air Extraction Limit?
APU GEN………….?

A

Min Temp for Cold-Soaked APU on Ground……………. -40oC
Max Start Attempts per Hour 3
Altitude: Max Starting
37,000 FEET
Bleed Air Extraction Limit……………………….30,000 FEET, APU BLEED EXTRACTION ABOVE 45oC OAT FOR AIR CONDITIONING OPS IS PROHIBITED
APU GEN….40 KVA FOR ALL OPERATIONS & ALTITUDES

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4
Q 
ALTITUDE LIMITS
Max Ops. Altitude.......? 
Max T/O & Landing .......? 
Max with Gear Extended......? 
Max with Slats/Flaps....? 
Min with Spoilers Out......?
A

Max Ops. Altitude……. 51,000 FT Max T/O & Landing 10,000 FT
Max with Gear Extended. 20,000
Max with Slats/Flaps….18,000 FT
Min with Spoilers Out……300 FEET AGL

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5
Q

TEMPERATURE LIMITS
Max Temp T/O and Lndg?
Min Temp T/O…………?
Runway Slope ……………..?

A

Max Temp T/O and Lndg….+50oC AMBIENT @ SL Min Temperature T/O-40oC AMBIENT@SL
Runway Slope +/- 2.0% MAX

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6
Q 
WIND LIMITS
Tailwind.....................? 
Max Tailwind for Start....? 
Max Tailwind HUD/CAT II ......? 
T/O Xwind Exceeds 20 Knots ..?
A

Tailwind ………………………10 KTS
Max Tailwind for Start 20 KTS
Max Tailwind HUD/CAT II 11 KTS
T/O Xwind Exceeds 20 Knots …….66% N1 MAX BELOW 30 KIAS

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7
Q 
ENGINE ITT LIMITS
Start (On Ground) ? 
(In Flight).................? 
Idle ......................... ? 
Takeoff..............  ....? 
Max Continuous .. ?
A

Start (On Ground)………………………. 700
(In Flight)…………………………………….. 850
Idle …………………………………….. ……. 860 Takeoff………………………………………….900*
Max Continuous………………….860 (905 FOR 20 SECONDS) *TAKEOFF THRUST FOR 5 MINUTES WITH ALL ENGINES RUNNING *TAKEOFF THRUST FOR 10 MINUTES IN EVENT OF ENGINE FAILURE

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8
Q

ENGINE RPM LIMITS N1
Takeoff………………………………………?
Max Continuous …………………….. ?
Reverse ………………………………… …?

A

Takeoff…………………………. 102
Max Continuous…………….102 (102.5 FOR 20 SECS)
Reverse ………………………… 70 FOR 30 SECONDS
*STATIC GROUND OPS RANGE OF 66% TO 80% N1 IS PROHIBITED

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9
Q

ENGINE RPM LIMITS N2
Idle ……………………………………… ? Takeoff…………………………………..?
Max Continuous …………………. ?

A

Idle ………………………………… 58
MIN Takeoff………………….. 99.6
Max Continuous…………….98.9 (99.8 FOR 20 SECS)

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10
Q 
ENGINE START/DRY MOTORING
3 Min. On.............................?
3 Min. On..............................?
3 Min. On........................    .? 
Do not engage starter if indicated N2 exceeds \_\_\_%. 
Dry motoring/
cranking ENGINE RUN switches OFF. 
Maximum tailwind for start is \_\_\_ knots.
A

3 Min. On………………15 SEC OFF
3 Min. On………………15 SEC OFF
3 Min. On……………… 15 MIN OFF
Do not engage starter if indicated N2 exceeds 42%.
Dry motoring/cranking ENGINE RUN switches OFF.
Maximum tailwind for start is 20 knots.
EXTERNAL OR EICAS INDICATION OF N1 IS PRESENT, THE ENGINE MUST BE CRANKED FOR 30 SECONDS FOLLOWED IMMEDIATELY BY AUTO START.

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11
Q 
FUEL
L Main Tank .....................? 
R Main Tank......................? 
Center Tank ...........................................?
Aft Tank..........................? 
Total ......         ................?
A

L Main Tank1 15,050 (GRAVITY 13,850) LBS
R Main Tank ………..15,050 (GRAVITY 13,850)
LBS Center Tank . 12,700 (GRAVITY 11,150) LBS
Aft Tank………………..2,300 (GRAVITY N/A) LBS Total……………………..45,100 (GRAVITY 38,850) LBS

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12
Q

FUEL
Min Temp for T/O ……..?
Fuel for Go-Around……?


A

Min Temp for T/O.. +5oC MINIMUM Fuel for Go-Around ………………. 600 LBS PER WING
MAX 10o NOSE UP

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13
Q

FUEL MAX IMBALANCE
Wing Fuel Load GND FLT
20,250 lbs.. ?…………..?

A

FUEL MAX IMBALANCE
Wing Fuel Load GND FLT
20,250 lbs 600…..1100

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14
Q

FUEL DISTRIBUTION
Fuel in the center tank must be considered unusable unless each wing tank is full at departure, and the planned cruise altitude is greater than ________ feet.
Fuel in the aft tank must be considered unusable unless each wing tank contains at least _____ lbs of fuel at departure, and the planned cruise altitude is greater than _____ feet.
If use of the center/aft tank is planned, the tank fuel load is to be no less than ____ lbs to ensure transfer pumps re-prime.

A

Fuel in the center tank must be considered unusable unless each wing tank
is full at departure, and the planned cruise altitude is greater than 30,000 feet.
Fuel in the aft tank must be considered unusable unless each wing tank contains at least 5,500 lbs of fuel at departure, and the planned cruise altitude is greater than 30,000 feet.
If use of the center/aft tank is planned, the tank fuel load is to be no less than 500 lbs to ensure transfer pumps re-prime.

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15
Q 
AIR COND AND PRESS 
Max Diff ............................? 
Max Neg Diff.....................? 
Max During Taxi/Takeoff .....? 
Max at Touchdown............... ? Max Alt in Manual Mode .... .?
A

Max Diff ………………………10.73 PSI Max Neg Diff……….-0.5 PSI
Max During Taxi/Takeoff…0.1 PSI
Max at Touchdown…………1.0 PSI Max Alt in Manual Mode …………………………………. 35,000 FT

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16
Q 
AIR COND AND PRESS
Manual Mode Discharge Temp.............................................?
One pack must be selected off if pack control is in manual mode.
Auxiliary pressurization (AUX PRESS) system operations are PROHIBITED at altitudes greater than \_\_\_\_\_\_ feet.
Use of EMERGENCY DEPRESS switch above \_\_\_\_\_ feet is prohibited.
A 
AIR CONDITIONING AND PRESSURIZATION
Manual Mode Discharge Temp ..........5oC (MIN) 60oC (MAX)
One pack must be selected off if pack control is in manual mode.
Auxiliary pressurization (AUX PRESS) system operations are PROHIBITED at altitudes greater than 41,000 feet.
Use of EMERGENCY DEPRESS switch above 15,000 feet is prohibited.
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17
Q

SPEEDS
vSE ……………………………………..?
VFE 6…………………………………..?
VFE 16………………………………….?
VFE 30…………………………………?
VLO Ret/Ext………….. .. ?

A

SPEEDS
vSE …………………..225KIAS
VFE 6………………. 210 KIAS VFE 16……………………… 210 KIAS VFE 30…………………….. 185 KIAS VLO Ret…………………… 200 KIAS

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18
Q

SPEEDS
vLE ………………………………………?
VTIRE …………………………………..?
Turb Air ………………………………..?
VMCG …………………………………..? VMCA………………………… ?

A

vLE …………………250KIAS
VTIRE …………….183 KNOTS
GROUND SPEED Turb Air …300 KIAS/0.80M VMCG …. 80 KIAS VMCA………………… 86 KIAS

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19
Q

AUTOMATIC FC SYSTEM
Min Alt AP Engagement is…………………………………………….? Min Alt AP Use (Precision App) ……………………………………..? Min Alt AP Use (Non-Precision App) ………………………………? Min Alt AP Use (Non-Precision App with Vertical Path Ref)…..?

A

AUTOMATIC FC SYSTEM
Min Alt AP Engagement is ……………………………400 FT AGL
Min Alt AP Use (Precision App) ………………………. 80 FT AGL
Min Alt AP Use (Non-Precision App)………………400 FT AGL
Min Alt AP Use (Non-Precision App with Vertical Path Ref) ……. ………………………………………………………………….160 FT AGL

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20
Q

AUTOMATIC FC SYSTEM

Max altitude for yaw dampers disengaged is _______ feet.

A

AUTOMATIC FC SYSTEM

Max altitude for yaw dampers disengaged is 41,000 feet.

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21
Q

What is the ground operation limit of the display units with the cockpit temperature in excess of 40°C?

A

Operation for greater than 30 minutes is prohibited

22
Q

What is maximum altitude for flight with the yaw damper disengaged?

A

41,000 feet

23
Q

What is the minimum autopilot use height for a precision approach? Non-precision approach?

A

Category I or II ILS - 50 AGL FAA
80 AGL JAA
Non-precision – 400 feet AGL

24
Q

What is the minimum autopilot use height for a non-precision approach with vertical path reference?

A

160 AGL

25
Q

What is the operational limitation when using FLC?

A

Use of FLC mode with the speed bug above .85M is prohibited

26
Q

When must both stall protection pusher switches be “ON”?

A

For duration of the flight

27
Q

What is the purpose of the master disconnect switch on the control wheel?

A

Disconnect the autopilot
Silence a disconnect aural
Inhibit the stick pusher (non-JAA

28
Q

What is the purpose of the touch control steering switch (TCS)?

A

Momentarily override the autopilot

29
Q

Does the indicator light on the guidance panel (GP) indicate that the associated mode is currently active?

A

No, the pilot must confirm mode status or operation from the flight director annunciator on the PFD

30
Q

How are active / armed flight director and autothrottle modes indicated on the AFCS display?

A

Active displayed in “green”

Armed displayed in “white”

31
Q

How does the pilot manually switch the flight guidance computer (FGC)?

A

On the MFD control panel
MENU button, page 2
Press ENT

32
Q

How will the autopilot engage if no vertical or lateral flight director mode is armed?

A

Basic pitch (PIT) and roll (ROL) modes

33
Q

What will cause manual disengagement of the autopilot?

A 
Pressing the AP pushbutton
Pressing either MASTER DISC pushbutton 
Pressing either TOGA switch
Manual trim activation
Pressing the YD switch on the GP
Physical override of the AP servos (not recommended)
34
Q

What will cause automatic disengagement of the autopilot?

A

Activation of windshear avoidance*
Unusual attitude
Stall warning activation

35
Q

When is use of the FMS as a sole NAV source for instrument approaches prohibited?

A

Prohibited past the FAF unless APP is annunciated on the PFD

36
Q

What is required for an automatic Nav-to-Nav transfer to occur?

A

Lateral mode is captured in LNAV
Pilot has selected the APR button
Aircraft has captured the LOC beam

37
Q

What course is set to capture and track a back course localizer?

A

Front course

38
Q

What must be the active lateral navigation mode for VPTH to be operational?

A

LNAV

39
Q

When is the ILS automatically tuned by the FMS?

A

Within 75 nm flight plan distance and

30 nm direct distance of the airfield

40
Q

When does Dual Coupling of the AFCS occur?

A

Below 1200 feet with

The PFDs displaying localizer data from different navigational sources

41
Q

What are the FD pitch commands for takeoff, SE takeoff and GA ?

A

Takeoff - 17.5 degrees
SE takeoff – 13 degrees
GA – 10 degrees

42
Q

How is the autothrottle GA mode cleared?

A

By selecting the AP on or

Selecting another vertical mode

43
Q

When is the automatic emergency descent mode (EDM) enabled?

A

Aircraft altitude above 25,000 feet

Cabin altitude has exceeded 14,500 feet

44
Q

Once the EDM is activated, what will occur?

A

FD will command a descent to 15,000 feet
FD will command a turn of 90 degrees left
Autothrottles will target airspeed of VMO-10 until 250 knots at 15,000 feet

45
Q

On the ground, what parameters are required to engage the autothrottles?

A

Either engage switch selected
Aircraft speed less than 60 knots
Throttle levers are above 23° TLA

46
Q

When is the autothrottle takeoff HOLD control mode activated?

A

On ground above 60 knots

In flight below 400 feet AGL

47
Q

When will the autothrottles transition to the RETARD mode?

A

Aircraft in landing configuration

Radio altitude of 50 feet AGL

48
Q

Temp below 10C TAT with moisture the brakes has to be wormed up to ….. units before TO

A

4 units

49
Q

After a rejected TO ….. To wait until the final read out of the breaks temp

A

15 min

50
Q

VMO
AB FL 200
BL FL 200

A

Above 340

Below 300

BBD700 (22 decks)

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