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P3C > Limits > Flashcards

Limits Flashcards

1
Q

BEFORE START TEMPERATURE

A

GROUND-200 DEGREES C

PRIME-100 DEGREES C

AIR-150 DEGREES C

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2
Q

START TIT

A

750-830 DEGREES C

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3
Q

LOW RPM TIT

A

410-730 DEGREES C

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4
Q

NORMAL RPM TIT

A

445-645 DEGREES C

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5
Q

MAX REVERSE TIT

A

580-790 DEGREES C

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6
Q

FLIGHT IDLE TIT

A

430-705 DEGREES C

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7
Q

MAX TIT

A

1077 DEGREES C (5 MIN)

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8
Q

MILITARY POWER TIT

A

1049 DEGREES C (30 MIN)

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9
Q

MAX CRUISE TIT

A

1010 DEGREES C

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10
Q

LOW RPM RPM %

A

71.0-73.8%

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11
Q

NORMAL RPM RPM %

A

96.3-99.1%

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12
Q

MAX REVERSE RPM

A

96.7-104.9%

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13
Q

FLIGHT IDLE RPM

A

94.5-98.4%

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14
Q

MAX RPM

A

99-101%

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15
Q

MILITARY, NORMAL AND MAX CRUISE RPM

A

99-101%

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16
Q

START OIL PX

A

POSITIVE PRESSURE BY 35%

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17
Q

LOW RPM OIL PX

A

RGB-250 EXCEPT START AND WARMUP IS 50

P/S-100 START AND WARMUP ONLY, THEN 60 50 (4)

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18
Q

NORMAL, MAX REVERSE AND FLIGHT IDLE OIL PX

A

RGB-250 EXCEPT START AND WARMUP, 150(3)

P/S- 100 START AND WARMUP ONLY, THEN 60 50(4)

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19
Q

MAX POWER OIL PX

A

RGB-150-250

P/S-50-60

20
Q

MILITARY, NORMAL AND MAX CRUISE OIL PX

A

RGB-150-250

P/S-50-60

21
Q

START OIL TEMPERATURE

A

-40 DEGREES C

22
Q

LOW AND NORMAL RPM OIL TEMP

A

90, 60-90, -40

23
Q

MAX REVERSE OIL TEMP

A
  1. 60-90, 40
24
Q

FLIGHT IDLE OIL TEMP

A

90, 60-90, 0

25
Q

MAX POWER oil temp

A

90, 60-90, 40 AND INCREASING THEN TO 60

26
Q

MILITARY, NORMAL, MAX CRUISE OIL TEMP

A

90, 60-90, 40 AND INCREASING, THEN TO 60

27
Q

INDICATED HORSEPOWER LOW RPM

A

MINIMUM UNTIL OIL TEMP IS ABOVE 0 DEGREES C

28
Q

NORMAL RPM, MAX REVERSE, AND FLIGHT IDLE INDICATED HORSEPOWER

A

1000 MAXIMUM AT OIL TEMP 0-40 DEGREES C

29
Q

MAX POWER INDICATED HORSEPOWER

A

4,600

5300 ENGINE LIMITING TO 3 SECONDS

30
Q

MILITARY, NORMAL, AND MAX CRUISE INDICATED HORSEPOWER

A

4,600
4600 CONTINUOUS OPERATION
DURING AIRSTART, MINIMUM UNTIL OIL TEMP IS ABOVE 0 DEGREES C
1000 MAXIMUM AT OIL TEMP OF 0-40 DEGREES C

31
Q

APU LIMITS

A

649 DEGREES C MAX CONTINUOUS
710 DEGREES C MAX PEAK (10 SECS)
732 DEGREES MAXIMUM PEAK
RPM- GROUND 98 TO 102%
AIR-98-103%

32
Q

FLAPS AIRSPEED LIMITATIONS

A

MANUEVER-275 KIAS
APPROACH-190 KIAS
LAND-170 KIAS

33
Q

LANDING GEAR AIRSPEED LIMITATIONS

A

EXTENDED-300 KIAS
RETRACTION-190KIAS

34
Q

LANDING LIGHTS EXTENDED AIRSPEED LIMIT

A

260 KIAS

35
Q

BOMB BAY DOORS AIRSPEED LIMIT

A

LIMIT DIVE SPEED

36
Q

OVERWING EXIT AIRSPEED LIMIT

A

170 KIAS

37
Q

MAIN CABIN DOOR OPEN AIRSPEED LIMIT

A

300 KIAS

38
Q

APU DOOR OPEN AIRSPEED LIMIT

A

225 KIAS

39
Q

FUEL DUMP AIRSPEED LIMIT

A

140-300 KIAS

40
Q

AIRSTARTS AIRSPEED

A

MAX-345 KIAS (-6KTS FOR EVERY 1000FT OF ALTITUDE
MIN-170 KIAS
MIN IS RANGES IS CRITICAL-210 KIAS

41
Q

AIRPLANE WEIGHT LIMITS

A

MAX TAKEOFF-139,760 LBS
RECOMMENDED TO-135,000LBS
MAX LANDING WEIGHT-103,880 LBS
MAX LANDING IN CASE OF EMERGENCY -114,000 LBS

42
Q

MINIMUM ALTITUDE ON STATION WITH OPERABLE RADALT AND RAWS

A

DAY-200FT AGL
NIGHT/IMC-300FT AGL

43
Q

MINIMUM OPERATING ALTITUDE W/O RADAR OR RAWS, W/ UPDATED BARO

A

DAY-300FT AGL
NIGHT/IMC-500FT AGL

44
Q

MIN OPERATING ALTITUDE W/O OPERABLE RADALT,W/O UPDATED BARO

A

DAY-500FT AGL
NIGHT/IMC-1000FT AGL

45
Q

MINIMUM ATTITUDE SOURCES

A

PRIMARY SOURCES-INS-1, INS-2, AND STANDBY GYRO
VMC-ANY TWO OF THE THREE PRIMARY ATTITUDE SOURCES
IMC/CROSS COUNTRY-ALL THREE PRIMARY SOURCES, OR ANY TWO OF THE THREE AND STANDBY ATTITUDE INDICATOR
OUTSIDE NAVAID COVERAGE-TWO INERTIALS (BOTH IN NAV MODE) AND STANDBY GYRO

46
Q

LATERAL IMBALANCE

A

TANKS 1 AND 4- TAKEOFF 1400 IN FLIGHT AND LANDING 4389
TANKS 2 AND 3- TAKEOFF 5025

P3C (10 decks)

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