GENERAL OPERATING LIMITATIONS Flashcards

1
Q

MAXIMUM OPERATING PRESSURE ALTITUDE

A

41,000 FEET

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2
Q

MAXIMUM TAKEOFF/LANDING PRESSURE ALTITUDE

A

10,000 FEET

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3
Q

RUNWAY SLOPE

A

+/- 2%

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4
Q

MAX TAKEOFF/LANDING TAILWIND COMPONENT

A

15 KNOTS

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5
Q

MAX GEAR RETRACTION SPEED

A

235 KNOTS

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6
Q

MAX GEAR EXTENSION SPEED

A

270 KNOTS/ .82 MACH

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7
Q

MAX GEAR OPERATING/EXTENDED SPEED

A

320/ .82 MACH

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8
Q

RECOMMENDED SEVERE TURBULENCE PENETRATION SPEED

A

CRUISE - TURB N1 Setting from CRUISE Page
CLIMB and DESCENT - 280 knots/.76 Mach
(If below 15,000ft and Aircraft gross weight is less than MLW, the A/C can be slowed to 250kts in the clean configuration)

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9
Q

QFE ALTIMETRY

A

Pilots are prohibited from operating with a QFE ALT setting selected

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10
Q

RECOMMENDED CROSSWIND COMPONENT GUIDELINES

Runway Condition Code 6, DRY

A

Takeoff Crosswind Component (knots)
-Blended Winglet/Split Scimitar Winglet - 34/33

Landing Crosswind Component (knots)
-Blended Winglet/Split Scimitar Winglet - 40/37

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11
Q

RECOMMENDED CROSSWIND COMPONENT GUIDELINES
(Runway Condition Code 5, “GOOD”)
(Wet, Damp, Frost/ 1/8” or Less of Water, Slush, Dry/Wet Snow)

A

Takeoff Crosswind Component (knots)
-Blended Winglet/Split Scimitar - 25/25

Landing Crosswind Component (knots)
-Blended Winglet/Split Scimitar - 40/37

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12
Q

PRESSURIZATION DIFFERENTIAL

A

MAXIMUM CABIN PRESSURE - 9.10 PSI

MAX CABIN for T/O & LDG - 0.125 PSI

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13
Q

OPERATING DIFFERENTIAL PRESSURE

A

ABOVE 37,000 - 8.35 +/- PSI
28,000 - 37,000 - 7.8 +/- PSI
BELOW 28,000 - 7.45 +/- PSI

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14
Q

ICING CONDITIONS ON GROUND AND T/O

A

OAT 10° or Below and…
Visible moisture in any form is present (i.e. clouds, fog with 1sm visibility or less, rain, snow sleet, or ice crystals) or…
While operating on ramps taxiways, or runways where snow, standing water, or slush may be ingested into engines or freeze on the engines, nacelles, or probes.

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15
Q

ICING CONDITIONS EXIST IN FLIGHT

A

OAT 10° or Below and…
Visible moisture in any form is present (i.e. clouds, fog with 1sm visibility or less, rain, snow sleet, or ice crystals)

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16
Q

AUTOPILOT MIN ENGAGEMENT HEIGHT

A

400 FT AGL

17
Q

AUTOLAND - MAX WINDS

A
  • HEADWIND - 25kts
  • CROSSWIND - 15kts
  • TAILWIND - 10kts (Flaps 30/40)
18
Q

MIN ALTITUDE FOR USE OF AUTOPILOT ON APPROACH

A

ILS/GLS (No AUTOLAND) - 50ft AGL
Non-precision - 50ft Below MDA/DA
Auto landings - Touchdown

19
Q

AUTOFLIGHT PARAMETERS

A
  • DO NOT use on Overweight Landings
  • DO NOT use A/P and A/T if the RA is INOP
  • AUTOLAND with FO is not authorized
  • *Do not use LVL CHG on Final Approach below 1000 ft AFE**
20
Q

BATTERY VOLTAGE FOR APU START

A

23 VOLTS

21
Q

SINGLE ENGINE GENERATOR LOAD MAXIMUM

A

Ground Operations - 75 kVa - 215 amps
700/800/900/900ER - 90kVa - 215 amps (air)
737MAX - 75kVa - 215 amps (air)

22
Q

ENGINE OIL TEMP

A
  • MIN for Starting (Max) - -40°
  • MIN for Takeoff (Max) - 31°
  • Maximum - 155°
  • Max Continuous - 140°
  • Max Allowable - 155° (NG- 45mins; MAX - 15mins)
23
Q

NORMAL ENGINE STARTER DUTY CYCLE

A
  • Multiple cycles permitted
    • NG - 2 minutes
    • MAX - 3 minutes
  • A minimum of 10 seconds is needed between start attempts
24
Q

REDUCED THRUST TAKEOFFS

A

NOT PERMITTED WHEN:

- Anti-skid is INOP
- Runways are contaminated with standing water, ice, slush, or snow.
25
Q

APU ALTITUDES

A
  • BLEED and ELECTRICAL - 10,000FT
  • BLEED - 17,000FT
  • ELECTRICAL LOAD - 41,000FT
26
Q

APU STARTER DUTY CYCLE

A

GROUND/IN-FLIGHT OPS

-15minute cooling is required after 3rd start attempt

27
Q

APU BLEED VALVE MUST BE CLOSED…

A
  • Ground air is connected and isolation valve is open
  • Engine 1 Bleed valve is open
  • ISOL valve is open and Engine 2 Bleed valve is open
28
Q

FLAP EXTENSION ALTITUDE

A

20,000 feet

29
Q

TIRE GROUNDSPEED

A

700/800/900/900ER - 195 Knots

MAX - 204 Knots