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B717 Limitations > Aircraft Limitations > Flashcards

Aircraft Limitations Flashcards

1
Q

Types of 717 operations allowed at HAL:

A

Day/Night VFR, IFR, Icing Conditions and CAT I approaches.

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2
Q

Types of 717 operations NOT allowed at HAL::

A

CAT II & III approaches and Backing the airplane.

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3
Q

Are reduced thrust takeoffs permitted on wet runways using wet runway takeoff performance?

A

Yes.

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4
Q

Reduced thrust takeoffs are NOT permitted on runways…

A

contaminated with standing water, slush, loose snow, compacted snow or wet ice OR in a situation requiring increased crew workload (inoperative engine gauges or anti-skid or nonstandard takeoff).

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5
Q

Minimum Crew

A

Two pilots

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6
Q

Slide girt bars must be inserted into floor fittings at forward entry and forward service door from…

A

prior to departure from loading ramp and until arrival at un-loading ramp.

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7
Q

The Emergency Light System must be armed for all flight operations?

A

Yes.

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8
Q

Wing Landing light motors should be allowed to cool…

A

1.5 minutes after initial extension or retraction and 3.5 minutes for each subsequent extension or retraction.

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9
Q

Wing landing light lamps should not be “ON” in still ambient air for periods longer than ______ to prevent heat buildup.

A

10 minutes.

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10
Q

Maximum Weights:

Taxi, Takeoff, Landing and Zero Fuel.

A

Taxi: 115,000 or (119,000)
Takeoff: 114,000 or (118,000)
Landing: 110,000 or (110,000)
Zero Fuel: 100,500 or (100,500)

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11
Q

Maneuvering Limit Load Factors:
Flaps/Slats retracted?
Flaps/Slats extended?
Flaps retracted/Slats extended?

A

Flaps/Slats retracted +2.5 to -1.0 G
Flaps/Slats extended +2.0 to 0.0 G
Flaps retracted/Slats extended +2.0 to 0.0 G

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12
Q

What is the maximum takeoff/landing runway slope?

A

+1.7% to -2.0%

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13
Q

Airspeed Limits
Vmo from sea-level to 26,000?
Vmo for 26,000 and above?

A

sea-level to 26,000: 340 KIAS

26,000 and above: .82 MACH

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14
Q

The Engine Takeoff Crosswind/Tailwind Limit is?

A

Crosswind: 40 knots
Tailwind: 10 knots

Above these limits only taxi and ground handing is allowed, with N1 limited to 50%.

Demonstrated crosswind takeoff and landing has been at 38 knots.

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15
Q

Maximum Altitude:

A

37,000 feet

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16
Q

Can you operate windshield anti-ice or anti-fog on a cracked windshield?

A

NO.

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17
Q

If windshield heat is INOP, do not exceed ____ airspeed below _______ feet.

A

315 knots below 10,000 feet

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18
Q

If Captain’s, Center or First Officer’s windshield is cracked, what are your airspeed limits below 10,000 feet? Outer pane? Inner pane?

A

Below 10,000 feet with a cracked windshield:
Outer glass pane: stay below 315 KIAS.
Inner glass pane: stay below 235 KIAS

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19
Q

Cabin Pressurization Limits:
Max cabin differential pressure is?
Max emergency relief pressure is?
If operating in MANUAL mode, takeoff and land?

A

Max cabin differential pressure: 7.86 psi
Max emergency relief pressure: 8.27 psi
(begins to open at 8.06)
In MANUAL, takeoff/land UNPRESSURIZED!

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20
Q

If air conditioning is used during takeoff, the FLOW switch must be in ______?

A

NORM.

do NOT want to be in high otherwise, its robbing your power

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21
Q

717 Autoland Operations:

A

NOT Approved for HAL 717.

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22
Q

Autopilot Limits

During takeoff, do NOT engage AP below ___?

Do NOT conduct and auto coupled ILS approach if _______________ alert illuminates for longer than ______ seconds.

For Precison and NP approached the AP must be disengaged no lower than minimums minus ______ feet.

A

Do NOT engage AP below “200 ft” on takeoff.
HALs limit is more restrictive at 500 ft.

Do NOT conduct and auto coupled ILS approach if “STAB OUT OF TRIM” alert illuminates for longer than “3” seconds.

For Precison and NP approached the AP must be disengaged no lower than minimums minus “50 ft”.

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23
Q

The Maximum airspeed with a malfunctioning or INOP Mach Trim Compensator (MTC) is ____?

A

“.78 Mach” max speed with MTC not working

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24
Q

Range Calculations, Fuel management and engine out terrain clearance must not be predicated on __________?

A

FMS.

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25
Q

Reduce RNP value by _____ when using FMS NAV as a GPS approach.

A

0.3 (doesn’t need to be displayed on the flight deck).

26
Q

The amber Vmin foot on the PFD airspeed tape must NOT be used for setting any approach or landing target speeds?

A

True.

27
Q

During an ILS approach, with an INOP GLIDESLOPE, FMS PROF Mode, the Vertical Deviation Indication must not be used for descent after the FAF.

A

True.

28
Q

FMS PROF mode, must NOT be used in descent /approach below MDA or DA.

A

True.

29
Q

The FMS computed V1, Vr and V2 speeds must be verified to AFM derived data unless on a _____ runway with a _____ ______ ______.

A

Dry Runway and Balanced Field Length.

30
Q

Windshear Guidance:

Use of FD or Coupled Windshear Guidance with OEI is ____________.

A

PROHIBITED.

31
Q

The airplane MUST be stationary during IRS ground alignment?

A

True.

32
Q

Maximum Altitude for starting APU.

A

37,000 feet

33
Q

APU Starter Motor Duty Cycles:

A

3 start attempts, then 30 minute wait.

34
Q

APU Air MUST be ______ for takeoff and inflight operations.

A

OFF.

35
Q

Power Plant Limits:

See chart

A

Mostly red lines, with one Amber line. Takeoff power is 5 minutes, with an engine failure or GA it can be 10 minutes.

36
Q

Normal Oil Pressure:

A

45 psi and greater.

37
Q

Oil Pressures less than ______ are undesirable and should be tolerated only for completion of the flight, preferably at reduced power settings.

A

35 psi.

38
Q

If the maximum Starting temperature is exceeded, engine should be _______ and ________.

A

shut down, inspected.

39
Q

Prior to takeoff, engine anti-ice should be turned ______ if icing conditions exist or is anticipated.

A

ON.

40
Q

Use of N1 mode for takeoff is _________.

A

PROHIBITED.

41
Q

With U/L or REV displayed on the primary engine display, ______ ____ _________.

A

Do NOT Takeoff.

42
Q

Engine Starter Duty Cycle Limits:

A

3 (3 minute) attempts with a 15 second in between, then 15 minutes.
3m on, 15s off, 3m on, 15s off, 3m on, 15min off.

43
Q

Inflight movement of the reverse thrust levers or use of inflight reverse thrust is _________.

A

PROHIBITED.

44
Q

Do _____ use Asymmetric Reverse Thrust for __________ _____________.

A

NOT, directional control.

45
Q

HAL is _____ _________ for power back operations.

A

NOT Approved.

46
Q 
Flap Speeds
Slats Extend:
Flaps 0-10:
Flaps 10.1 to 20:
Flaps 25:
Flaps 40:
A 
*Slats Extend:        280/.57
Flaps 0-10:             280/.57
Flaps 10.1 to 20:     240/.57
Flaps 25:                220/.57
Flaps 40:                200/.57
*(Slats MUST be extended for Takeoff)
47
Q 
Gear Speeds
Landing Gear Retraction:
 (Retraction with an HYD issue:) 
Landing Gear Extension:
Landing Gear Extended:
Emergency Gear Extension:
A

Landing Gear Retraction: 250 knots (maybe 220 with limitation on full system)
Landing Gear Extension: 300 knots/.70
Landing Gear Extended: 300 knots/.70
Emergency Gear Extension: 230 knots.

48
Q

Tire Speed

The maximum tire speed is ________ knots.

A

195.

49
Q

Takeoff with flap setting of less than ____ degrees is _________.

A

5 degrees, PROHIBITED.

50
Q

Rudder Power

The Rudder Hydraulic Power MUST be ON for takeoff.

A

True.

51
Q

Manual Rudder Control
Do NOT attempt an approach or missed approach at a speed less than _____ KIAS (until landing assured) when _____ _____ _____ alert is displayed.

A

144 KIAS

RUDDER PWR OFF

52
Q

Speed Brakes
Speed brakes must not be used with flaps extended beyond ________ degrees.

Do NOT move spoiler/speedbrake lever to ground spoiler position __ _____.

A

20 degrees. (20 and 40 Flaps)

in flight.

53
Q

Fuel Pump Circuit breakers:

A

DO NOT RESET.

54
Q

Fuel Density limited to ______ to ______ per gallon.

A

6.3 to 7.1

55
Q

Max/Min Fuel Temperature:

A

Max: 54 degree C.
Min: JetA -40.
JetB -47.

56
Q

Fuel
With main tanks NOT full, treat center fuel weight at cargo in zero fuel weight calculations.

Use ________ tank fuel first.

A

True.

Center Tank (may use only down to ballast level if required).

57
Q

Max Fuel Imbalance:

A

1500 pounds.

58
Q

Hydraulic Pump Circuit Breakers:

A

DO NOT RESET

59
Q

Gear Load Limits
Landing at Max landing weight 110,000):
Landing at Max takeoff weight 114,000):

A

Landing at Max landing weight: 600 fpm

Landing at Max takeoff weight: 360 fpm

60
Q

Brake Pressure

Brake pressure for parking is ________ psi to ensure at least ________ hours of parking time.

A

2000 psi, 8 hours.

61
Q

Do NOT set Parking Brake if _______ _______ alert is displayed.

Do NOT takeoff is any brake temperature exceeds _____ degrees C unless other data is available.

A

BRAKE OVERHEAT

170 degrees

B717 Limitations (1 decks)

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