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T-45 Intermediate > Limits > Flashcards

Limits Flashcards

1
Q

Maximum Altitude

A

41,000 MSL

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2
Q

Icing Limits

A

Prolonged flight into icing conditions prohibited.

When airframe icing is visible, intentional stalls or use of full flaps is not authorized.

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3
Q

Throttle at Idle For:

A
  • abrupt (0.5s or less from neutral to full back stick) pulls to full backstick
  • abrupt full lateral stick inputs at full backstick.
  • airspeeds less than 85KIAS at altitudes above 15,000 MSL
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4
Q

Slow throttle movements

A

required for airspeeds 85 to 150 KIAS above 35,000 MSL

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5
Q

Engine must be stabilized

A

at Idle for at least 30s prior to shutdown, except for an emergency.

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6
Q

may result in sub-idle condition leading to flameout:

A

sustained engine operation at less than 70% N2 above 30,000 MSL

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7
Q

Manual Fuel control limits

A

N2 less than 90% over 20,000 MSL

N2 less than 95% at or below 20,000 MSL

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8
Q

Throttle position for start

A

Start prohibited with throttle above ground Idle detent

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9
Q

Max time for engine light-off

A

within 15s of moving throttle to idle.

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10
Q

Minimum battery voltage for start

A

24V

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11
Q

Sequential start attempt limitations

A

3 successive starts. 30 minute cool down period before another attempt.

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12
Q

idle increase with airflow knob in OFF position:

A

approximately 2%

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13
Q

maximum shift in Idle RPM between post-start and engine shutdown checks:

A

2%, corrected for standard day conditions.

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14
Q

GTS start with external power:

A

is prohibited

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15
Q

minimum interval between GTS start attempts/GTS start limitations:

A

3 minutes. ( 3 minute delay does not apply in emergencies)

after 3 successive start attempts, minimum 30 minute delay

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16
Q

Additional GTS start attempts after an unsuccessful GTS start attempt:

A

prohibited until the GTS exhaust duct and combusted inspected, residual fuel removed.

RAT doors inspected for discoloration and warpage.

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17
Q

GTS starts:

A

not reliable over 15,000 MSL

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18
Q

Freeze point for F-24, JET A, and F-24 + 100 (F-27)

A

-40C ( - 40F)

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19
Q

To Prevent fuel freezing

A

do not allow indicated OAT to dwell at or below freeze point of fuel in use.

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20
Q

fuel additives (FSII, CI/LI)

A

must be injected at the fuel source to be used without restriction.

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21
Q

FSII / CI/LI

A

Fuel System Icing Inhibitor,

Corrosion inhibitor / lubricity improver

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22
Q

the addition of aerosol FSII

A

is prohibited

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23
Q

MAX AoA for emergency flap configuration
(flaps half/full, slats up)

(Flaps extended by EMER FLAPS in DOWN position)

A

AoA for pedal shaker / warning tone.

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24
Q

Sideslip limitations

A

minimize sideslip with gear in transition or extended above 150KIAS in order to prevent damage to gear doors and NLG strut door.

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25
Q

Airspeed limit:

landing gear, transition/extended

A

max 200 kias

26
Q

Airspeed limit:

flaps/slats, transition / extended

A

max 200 KIAS

27
Q

Airspeed limit:

arresting hook, transition / extended

A

max 450 KIAS

28
Q

windspeed limit:

canopy, stationary and towing with canopy full open.

A

prevailing wind MAX 32 knots

29
Q

Canopy, locked in intermediate position limitation:

A

permitted only for ingress and egress, NO taxiing.

30
Q

windspeed limit,

taxi with canopy full open

A

MAX 20 knots

31
Q

max groundspeed on deck, tire limitation

A

MAX 176 knots

32
Q

max groundspeed on deck, NWS limitation

A

MAX 176 Knots

33
Q

fuel level limitation for hot refueling

A

less than or equal to 2,800 LB if PRECHECK unsuccessful.

34
Q

Do not use large lateral inputs at:

A

less than 8 units AoA for all configurations / store loadings

35
Q

Roll limitations,
Cruise configuration,
0-260 KIAS

A
  • 1 to 1.25 G : max bank angle change, 360 deg
    1. 25 to 4 G : max bank angle change is 180 deg OR 360 with half lateral stick / half rudder pedal inputs

4 G to G limit: max angle of bank change of 180 degrees.

36
Q

Roll limitations,
Cruise configuration,
260 KIAS to 0.8 Mach

A
  • 0.2 to 1.25 G : max bank angle change is 360 degrees
    1. 25 to 4 G : max bank angle change is 180 deg OR 360 with half lateral stick / half rudder pedal inputs

4 G to G limit: max angle of bank change of 180 degrees.

37
Q

Roll limitations,
Cruise configuration,
airspeeds greater than 0.8 mach, to airspeed limit

A

from 0.75 to 1.25 G : max bank angle change is 360 deg

from 1.25 to g limit: max bank angle change is 180 deg

38
Q

Max AoB with gear and/or flaps down

A

90 degrees AoB

39
Q

max 90 degree crosswind component,

single aircraft, dry runway

A

20 knots

40
Q

max 90 degree crosswind component,

single aircraft, wet runway

A

15 knots

41
Q

max 90 degree crosswind component,

section takeoff

A

10 knots

42
Q

max 90 degree crosswind component,

banner tow

A

10 knots

43
Q

max 90 degree crosswind component,

NWS OFF / Failed

A

15 knots

44
Q

Prohibited maneuvers

A
  1. ) intentional spins / tailslides
  2. ) rolling cross-controll maneuvers of more than 60 degrees bank angle change
  3. ) Intentional departures except for
    • erect rolling departure with full aft stick/full lateral stick
    • erect rudder-induced departure entered with full aft stick/full rudder
    • nose high departures (70 and 110 degrees)
  4. ) sustained zero or negative g flight for more than 30 s
  5. ) less than 30 seconds between negative g or zero g maneuvers
  6. ) rolls at less than:
    • negative 1.0 G at less than 260 KIAS
    • Negative 0.2 G at or greater than 260 KIAS, but less than 0.8 Mach
  7. ) lateral / directional inputs below 3 units AoA
  8. ) intentional departures with greater than 1,000 ft-lb asymmetry
  9. ) operations with EMER FLAPS selected, when normal HYD1 power is available, is restricted to 30 seconds with engine RPM less than or equal to 90%. Except in actual emergency, use of EMER FLAPS is restricted to FCF profiles.
  10. ) intentional accelerated stalls with landing gear extended while carrying stores.
45
Q

Weight Limitation,

Field Takeoff

A

14,500 lbs

46
Q

Weight Limitation,

Catapult

A

14,200

47
Q

Weight Limitation,

field landing

A

13,360

48
Q

Weight Limitation,

FCLP

A

13,360

49
Q

Weight Limitation,

Carrier Landing

A

13,360

50
Q

normal acceleration limits;

gear in transition, and/or extended with flaps or full

A
  1. 0 to 2.0G for Symmetrical loading

1. 0 to 1.5G for Unsymmetrical loading

51
Q

symmetric acceleration limit,
below 5,000 MSL
weight 13,233 or less

A

max + 6.5 G

52
Q

symmetric acceleration limit,
above 5,000 MSL
weight 13,233 or less

A

max +7.33G

53
Q

symmetric acceleration limit,
airspeed 0.8 mach or above
weight 13,233 or less

A

min -1.0G

54
Q

symmetric acceleration limit,
airspeed below 0.8 Mach
weight below 13,233

A

min -3.0

55
Q

unsymmetric acceleration limit,
below 5,000 MSL
weight 13,233 or less

A

max 5.0G

56
Q

unsymmetric acceleration limit,
above 5,000 MSL
weight 13,233 or less

A

max 5.86G

57
Q

unsymmetric acceleration limit,
airspeed 0.8 mach or above
weight 13,233 or less

A

Min 1.0 G

58
Q

unsymmetric acceleration limit,
airspeed between 260kts 0.8 mach
weight 13,233 or less

A

Min -0.2G

59
Q

unsymmetric acceleration limit,
airspeed below 260kts
weight 13,233 or less

A

Min-1.0G

60
Q

speed brakes may not fully extend above:

A

340 KIAS

61
Q

Speed brakes will blow back above:

A

380 KIAS

T-45 Intermediate (12 decks)

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