Limitations Flashcards

1
Q

Single Point Usable Fuel

A

14150 Total

L/R 7075

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2
Q

Gravity Usable Fuel

A

13000 Total

6500 L/R

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3
Q

Min fuel for GA

A

500 lbs per side

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4
Q

Fuel Transfer Limitations

A

Power and gravity shut off valves OFF for takeout

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5
Q

Single Point fueling

A

55 psig

-8 psig

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6
Q

Approved fuels

A

Jet A
Jet A1
JP 5
JP 8

Jet B & JP 4 approved up to 16000ft

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7
Q

Landing gear altitude

A

Not extend above 18000ft

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8
Q

Spoilers

A
  • Not extended in flight at airspeeds below approach speed +8 knots.
  • Not extended in flight below 500AGL
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9
Q

Flaps

A

Not too be used above 18000ft.

Flaps 10 - 210kts
Flaps 20 - 210kts
Flaps 30 - 175kts

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10
Q

Electrical (Generators/Batteries)

A

Continuous:
2 or 3 Generators - 400A
1 Generator on Ground - 400A
1 Generator in Flight - 500A

Transient:
5 minutes - limit 600A

Prohibited to takeoff in Battery Temps are below -20°c.

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11
Q

Compass

A

Left and Right windshield must be temporarily off while the standby compass is being read.

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12
Q

Standby Instrument

A

Localizer deviation is prohibited during back course approaches.

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13
Q

GPS T-transition Speed

A

210kts out less

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14
Q

VNAV

A
  • VFLC is prohibited during climb when airspeed is displayed as Mach.
  • VNAV for VMDA approaches is prohibited between final approach fix and MAP.
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15
Q

Autopilot Engagement Heights

A

Climb, Enroute, Descent - 700 AGL
Precision with GP 3.5 or less - 80 AGL
Precision with GP 3.5 to 4.5 - 160 AGL
Visual and non-precision - 200 AGL

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16
Q

Pressurization

A

Max Diff on ground - -0.1 psid
Max Diff on landing - 1 psid
Max positive diff - 9.4 psid
Max negative diff - -0.5 psid

17
Q

Oxygen masks

A

Crew and Pax Oxygen Masks not approved above 40000ft.

Prolonged operation of Pax masks above 25000ft is not recommended.

18
Q

Air Conditioning

A

Do not select air source to TRIM AIR ONLY in the ground.

Pack must be operating when electrical power is on for more than 30 minutes and OAT is greater than 40°c.

19
Q

Maneuvering Load Limits

A

Flaps Up +2.6G -1.0G

Flaps Extended +2.0G -0.0G

20
Q

Max altitude

A

45000ft

21
Q

Takeoff and Landing Limitations

A

Max takeoff and landing altitude 10000ft.

Max tailwind component - 10kts

Max runway slopes +/- 2°

22
Q

Tire Speed

A

182kts

23
Q
Other Airspeeds:
Vra
Vlo retract
Vlo extend
Vle
Vfe
A
Vra - 265/.75M
Vlo retract - 200kts
Vlo extend - 250kts
Vle - 250kts
Vfe 10, 20, 30 - 210, 210, 175
24
Q

Max Operating Speeds
Vmo
Mmo

A

Vmo (up to 8000) - 300kts
Vmo (8001 to 29475) - 320kts
Mmo (above 29475) - 0.83M

25
Q

Wing Anti-ice

A

On ground below 5°c + visible moisture

In flight below 10°c + visible moisture except when SAT is below -40°c.

Must be in when ICE DETECTED CAS is on or in icing and below 210kts.

26
Q

Engine Anti-ice

A

On ground below 10°c + visible moisture

In flight below 10°c + visible moisture

Must be on when ICE DETECTED CAS is on or in icing conditions.

27
Q

Stabilized Approach Criteria

A

ABCD 1PF

  • Airspeed Vref -0 to +10
  • Briefed
  • Configured
  • 1 Dot lateral and vertical CDI deflection
  • 1000ft/minute or less VSI
  • On Profile
  • No Flags
28
Q

Icing limits

A

Do not hold on icing with flaps extended.

When side window icing is observed - wing and engine Anti-ice must be on, leave icing ASAP.

29
Q

Dimensions

A

Wingspan
300 - 63’ 10”
350 - 69’

Length - 68’ 8”

Height - 20’

Minimum pavement for 180° turn - 58’
Wingtip clearance for 180° turn 300 - 95’ 5”, 350 - 101’

30
Q
Weights
Ramp
Takeoff
Zero Fuel
Landing
Flight
A
Max Ramp - 40750
Max Takeoff - 40600
Max ZeroFuel - 28200
Max Landing - 34150
Flight - 24800
31
Q

Crosswind

A

Max takeoff - 28kts

Max landing - 24kts

32
Q

APU RPM / EGT

A

Max RPM - 108%

Max EGT - 973°c starting, 718°c normal

33
Q

APU and altitude

A

APU operation - 37000ft
APU generator - 30000ft
Bleed air for engine start - 20000ft
Bleed air for ECS - 20000ft

Do not use APU to start L engine on ground above 9000ft.

APU ops during de-icing prohibited.

34
Q

Thrust reversers

A
  • on paved surfaces only
  • not in flight
  • not for backing up
  • not for touch and go’s
  • reverse thrust above idle prohibited below 40kts
35
Q

APU starting

A

On ground-
3 attempts with 1 minute cooling, after 3rd attempt 20 minutes cooking.
2 more attempts may be made then no further attempts for 40 minutes.

In flight-
Below 285kts, 1 attempt.

36
Q

Engine start limits

A

3 consecutive start cycles may be made followed by 15 minutes cooling before more start attempts.

Engines must be motored for 30 seconds after aborted start.

Engine can be motored for 5 minutes followed by 15 minutes cooling.

37
Q

Engine Type

A

HTF 7350 / AS907-2-1A

7323lbs thrust

Flat rated ISA +15 TO
Flat rated ISA +20 APR

38
Q

Engine Oil Temps

A

Normal range 27 - 138°C

-40°C minimum for Engine Start.
(Below -30°c minimum, oil temp limit is 15°c provided fuel system icing inhibitor is used)

Oil temp of minimum 5°c to operate engines above ground idle.

Oil temp between 5°c - 14°c, engines may be operated up to but not including CLB.

27°C is a Green Indication.

39
Q

Fuel Temps

A

Fuel system icing inhibitor must be used when fuel is below -20°c for takeoff.

Takeoff with bulk fuel temp above 50°c is prohibited.

With wing bulk fuel 45°c and above:

  • min fuel for takeoff is 2800lbs
  • less than 1000lbs per side, do not operate engines for more than 30 minutes.

Fuel Temps:
Jet A - -30°c
Jet A1 - -35°c
Jet B - -40°c