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U-28 GK > CAPs/Ops Limits > Flashcards

CAPs/Ops Limits Flashcards

1
Q

(PILOT) ENGINE FIRE IN FLIGHT

A
  1. ECS EMER SHUT OFF - PULL
  2. Pilot Oxygen Masks - ON/100%
  3. Passenger Oxygen Selector - ON
  4. Crew Oxygen Masks - ON/100%
  5. Engine - CONFIRM FIRE EXISTS
    If fire exists:
  6. FUEL EMER SHUTOFF - PULL
  7. Condition Lever - CUT-OFF/FEATHER
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2
Q

(PILOT) ENGINE FAILURE IN FLIGHT

A
  1. Engine - CONFIRM FAILED
  2. PCL - IDLE
  3. Condition Lever - CUT-OFF/FEATHER
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3
Q

(PILOT) ENGINE FAILURE AFTER ROTATION

A
  1. AOA - CENTERED
  2. Flaps - 15*
    If below turn back altitude, land straight-ahead, turning only to avoid obstacles. If above turn back altitude, smoothly initiate a 45* bank turn toward the landing site and maintain AOA CENTERED.
  3. Engine - CONFIRM FAILED
    If the engine has failed:
  4. Condition Lever - CUT-OFF/FEATHER
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4
Q

(PILOT) COCKPIT/CABIN FIRE, SMOKE OR FUMES AND SMOKE EVACUATION

A
  1. Pilot Oxygen Masks - ON/100%
  2. Passenger Oxygen Selector - ON
  3. Crew Oxygen Masks - ON/100%
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5
Q

(OTHER CREW) ENGINE FIRE IN FLIGHT

A
  1. Pilot Oxygen Masks - ON/100%
  2. Passenger Oxygen Selector - ON
  3. Crew Oxygen Masks - ON/100%
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6
Q

(OTHER CREW) COCKPIT/CABIN FIRE, SMOKE OR FUMES AND SMOKE EVACUATION

A
  1. Pilot Oxygen Masks - ON/100%
  2. Passenger Oxygen Selector - ON
  3. Crew Oxygen Masks - ON/100%
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7
Q

Operating Condition

A

67B/67P

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8
Q

TORQUE (PSI)
TAKEOFF (5 min limit)

A

44.34

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9
Q

TORQUE (PSI)
MAX CONT. CLIMB or MAX CRUISE

A

36.95/44.34 (1)

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10
Q

TORQUE (PSI)
MIN IDLE

A
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11
Q

TORQUE (PSI)
STARTING

A
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12
Q

TORQUE (PSI)
TRANSIENT (20 sec limit)

A

61

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13
Q

TORQUE (PSI)
MAX. REVERSE

A

34.25

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14
Q

MAX ITT (*C)
TAKEOFF (5 min limit)

A

800/850

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15
Q

MAX ITT (*C)
MAX CONT. CLIMB or MAX CRUISE

A

760/820

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16
Q

MAX ITT (*C)
MIN IDLE

A

750 (2)

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17
Q

MAX ITT (*C)
STARTING

A

1000 (5 sec limit)

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18
Q

MAX ITT (*C)
TRANSIENT (20 sec limit)

A

870

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19
Q

MAX ITT (*C)
MAX. REVERSE

A

760

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20
Q

%NG
TAKEOFF (5 min limit)

A
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21
Q

%NG
MAX CONT. CLIMB or MAX CRUISE

A

104

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22
Q

%NG
MIN IDLE

A

50.7 Gnd Idle
64 Flt Idle

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23
Q

%NG
STARTING

A
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24
Q

%NG
TRANSIENT (20 sec limit)

A
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25
Q

%NG
MAX. REVERSE

A
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26
Q

Np (RPM) (4)
TAKEOFF (5 min limit)

A

1700

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27
Q

Np (RPM) (4)
MAX CONT. CLIMB or MAX CRUISE

A

1700

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28
Q

Np (RPM) (4)
MIN IDLE

A
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29
Q

Np (RPM) (4)
STARTING

A
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30
Q

Np (RPM) (4)
TRANSIENT (20 sec limit)

A

1870

31
Q

Np (RPM) (4)
MAX. REVERSE

A

1650

32
Q

OIL PRESS (PSI)
TAKEOFF (5 min limit)

A

90 TO 135

33
Q

OIL PRESS (PSI)
MAX CONT. CLIMB or MAX CRUISE

A

90 TO 135

34
Q

OIL PRESS (PSI)
MIN IDLE

A

60 MIN

35
Q

OIL PRESS (PSI)
STARTING

A

200 MAX

36
Q

OIL PRESS (PSI)
TRANSIENT (20 sec limit)

A

40 TO 200

37
Q

OIL PRESS (PSI)
MAX. REVERSE

A

90 TO 135

38
Q

OIL TEMP (*C)
TAKEOFF (5 min limit)

A

10 TO 110

39
Q

OIL TEMP (*C)
MAX CONT. CLIMB or MAX CRUISE

A

10 TO 105

40
Q

OIL TEMP (*C)
MIN IDLE

A

-40 TO 110

41
Q

OIL TEMP (*C)
STARTING

A

-40 MIN

42
Q

OIL TEMP (*C)
TRANSIENT (20 sec limit)

A

110 MAX (3)

43
Q

OIL TEMP (*C)
MAX. REVERSE

A

10 TO 105

44
Q

67P MAX CRUISE limited to _____ PSI.

A

36.95

45
Q

Applies over a speed range of _____ to _____ Ng RPM.

A

50.7%, 61.4%

46
Q

Oil temperature is limited to _____ minutes at _____C to _____C.

A

10, 105, 110

47
Q

During steady state operation, operation from _____RPM up to _____ RPM is permitted to allow for governing accuracy.

A

1670, 1730

48
Q

Stabilized operation of propeller on the ground between _____ and _____ RPM is not permitted.

A

350, 950

49
Q

67P Gen 2 limited to _____ on the ground.

A

200A

50
Q

Max Fuel Imbalance For Takeoff: _____

A

3 LCD Segments

51
Q

Max landing weight: _____ lbs. Max zero fuel weight: _____ lbs /_____ lbs (Trainer/EQ-EQ+)

A

9921, 9039, 9240

52
Q

(Trainer) Max ramp weight: _____ lbs. Max T/O weight: _____ lbs.

A

10495, 10450

53
Q

(EQ/EQ+) Max ramp weight: _____ lbs. Max taxi weight: _____ lbs. Max T/O weight: _____ lbs.

A

11400, 10979, 10935

54
Q

Above 10450 lbs, no _____ maneuvers, bank angle is limited to _____ maximum, make _____ transitions from climb or descent.

A

abrupt, 30*, slow

55
Q

If landing above max landing weight, max touchdown descent rate is limited to _____ FPM.

A

300

56
Q

MAX FLAP EXTENDED SPEED (V,FE) < or = 15*

A

163 KIAS

57
Q

MAX FLAP EXTENDED SPEED (V,FE) > 15*

A

130 KIAS

58
Q

GEAR EXTEND/RETRACT SPEED (V,LO)

A

177 KIAS

59
Q

GEAR EXTENDED SPEED (V,LE)

A

236 KIAS

60
Q

MAX OPERATING SPEED (V,MO)

A

236 KIAS (Trainer)
216 KIAS (EQ/EQ+)

61
Q

ICING LIMITATIONS
In pusher ice mode with gross weight < or = _____/_____/_____ lbs:

A

9921, 10450, 10935

62
Q

ICING LIMITATIONS
MAXIMUM FLAP EXTENSION

A

15* with de-ice boots
0* without de-ice boots

63
Q

ICING LIMITATIONS
MIN CLIMB SPEED, 0* FLAPS

A

130/135/145 KIAS

64
Q

ICING LIMITATIONS
MIN APPROACH SPEED, 15* FLAPS

A

108/111/114 KIAS

65
Q

ICING LIMITATIONS
MIN APPROACH SPEED, 0* FLAPS

A

134/140/145 KIAS

66
Q

XW LIMIT
FLAPS 0*

A

30 KTS

67
Q

XW LIMITS
FLAPS 15*

A

25 KTS

68
Q

XW LIMITS
FLAPS 30*

A

20 KTS

69
Q

XW LIMITS
FLAPS 40*

A

15 KTS

70
Q

GENERATOR 1 RATING

A

28 V, 400 A

71
Q

GENERATOR 2 RATING 67B/67P

A

28 V, 115 A / 28 V, 300 A

72
Q

BATTERY RATING

A

24 V, 42 Ah

73
Q

Engine automatic starting cycle shall be limited to the following intervals:

A
  1. Sequence, 60 seconds OFF
  2. Sequence, 60 seconds OFF
  3. Sequence, 30 minutes OFF

U-28 GK (13 decks)

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