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P-3 > Limits > Flashcards

Limits Flashcards

1
Q

Ground starter px and temp limits

140psi?
110psi?

A

480F

625F

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2
Q

Engine limitations

  • limit power during transients should not exceed…?
  • how many minute limit during climb?
  • when will red overtorque light illuminate? (Note)
  • when does flopover occur (Caution)
A
  • 4600shp for 3 secs on the gauge
  • 5 minutes
  • above 4600shp
  • 5300shp
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3
Q

Hp Max, mil, and normal

A

4600shp

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4
Q

APU Tachometer limits

  • Ground
  • Flight
A

98-102%

98-103%

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5
Q

Engine tachometer limits

A

99-101% normal

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6
Q

Engine Oil Temp

  • Max: 5 minutes in flight range and 30 minutes in ground range
  • Normal range
  • permitted under extremely cold conditions
  • minimum for start low or normal rpm (note)
  • min allowable range during run up below 1000shp (note)
  • what and rising for takeoff? (note)
A 
100C
60-90C
50-60C
-54C and -40C if MIL-L23699 is used 
0-40C
40C
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7
Q

TIT Temp limits

  • Max allowable over temp
  • Max allowable
  • military power
  • Max cruise
  • warning light comes in at? (note)
A 
1175C for 5 seconds 
1077C for 5 mins
1049C for 30 mins 
1010C 
1080C plus or minus 2C
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8
Q

EGT Limits

  • Max peak
  • Max peak (10 secs)
  • Max continuous
A

732C
710C
649C

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9
Q

Oil PX power section

  • normal range
  • max allowable
  • Max during warmup (note)
A

50-60psi
60psi
100psi

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10
Q

Hyd System 1 and 2 normal pressure range

A

2960-3200psi

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11
Q

HYD Brake PX min

A

1900psi min for normal flight

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12
Q

Oil PX range for gear section

- Max allowable (except during warmup)

A

150-250psi

250psi

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13
Q

Start TIT range

A

750-830 degrees C

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14
Q

Start Oil Px (9) for RGB & P/S

A

Positive oil px by 35% rpm

(9) Max allowable fluctuation at 100%rpm provided px remains within limits is + or - 5psi for P/S and + or - 20 for RGB

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15
Q

Start oil temp minimum

A
  • 40C
    (6) : if L7808 is used -54C is the lower limit ; if L23699 oil is used -40C is the lower limit; when ambient tem below 0C, ref starting engines paragraph 18.3.2
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16
Q

Low rpm (2)(7) TIT range

A

410-730C (12)
(12): Max TIT in low rpm shall be limited to 730 degrees C regardless of power lever position, accessory loading, or use of diffuser bleed air to ensure adequate cooling airflow to the turbine.

(2) use of power between GND Start and MAX Reverse in low rpm can cause engine rpm to decay. Contributing causes to higher ambient temp, field elevation, airspeed, accessory load, end bleed are effects on the power available at low rpm. If rpm begins to decay, advance the power lever. If rpm decay continues, shut down the engine
(7) acceleration time from start of rotation to low rpm should not exceed 60secs.

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17
Q

Low rpm RPM range

A

71.0-73.8%

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18
Q

Low rpm Max oil px RGB

A

250psi, except start and warmup: 50 psi

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19
Q

Low rpm oil px P/S

A

100psi Start and Warmup only, then 50-60psi

(4) if px is below 50psi at low rpm, condition is acceptable provided px is within limits at 100%rpm

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20
Q

Low rpm oil temp range

A

90C (5) Max
-40C (6) Min
Range: 60 to 90C
(5): 100C is Max allowed for 30mins in beta range and 5mins in alpha range then 90C is max

(6): if L7808 is used -54C is the lower limit ; if L23699 oil is used -40C is the lower limit; when ambient tem below 0C, ref starting engines paragraph 18.3.2

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21
Q

Low rpm Indicated HP

A

Minimum until oil temp is above 0C

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22
Q

Normal RPM (start position) TIT range

A

445-645C

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23
Q

Normal RPM (start position) RPM range

A

96.3-99.1

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24
Q

Normal RPM (start position) oil px RGB

A

250psi except start and warmup 150
(3): operation below 150psi when rpm is below 100% is permitted. If RGB px is between 130-150psi at 100% rpm, record and continue. Maintenance action shall be accomplished prior to next flight.

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25
Q

Normal RPM (start position) oil px P/S

A

100psi start and warmup only, then 60-50

(4): if px is below 50psi at low rpm, condition is acceptable provided px is within limits at 100%rpm

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26
Q

Normal RPM (start position) Oil PX P/S

A

100psi Start and Warmup only, then 50-60psi

(4) if px is below 50psi at low rpm, condition is acceptable provided px is within limits at 100%rpm

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27
Q

Note

A

TIT and rpm values in ground operation are based on 0 airspeed, no diffuser bleed, no accessory loading, and ambient air temp range from -54 to 55C

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28
Q

Normal RPM (start position) Indicated HP

A

1,000hp Max at oil temp 0 to 40C

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29
Q

Maximum Reverse 0 degrees TIT

A

580-790C

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30
Q

Maximum Reverse 0 degrees RPM

A

96.7 to 104.9%

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31
Q

Maximum Reverse 0 degrees Oil Px RGB

A

250psi except start and warmup 150(3)
(3): operation below 150psi when rpm is below 100% is permitted. If RGB px is between 130-150psi at 100% rpm, record and continue. Maintenance action shall be accomplished prior to next flight.

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32
Q

Maximum Reverse 0 degrees RPM Oil Px P/S

A

100psi start and warmup only, then 60-50

(4): if px is below 50psi at low rpm, condition is acceptable provided px is within limits at 100%rpm

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33
Q

Maximum Reverse 0 degrees Oil Temp

A

90C (5) Max
40C Min
Range: 60 to 90C
(5): 100C is Max allowed for 30mins in beta range and 5mins in alpha range then 90C is max

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34
Q

Normal RPM (start position) Oil Temp

A

90C (5) Max
-40C (6) Min
Range: 60 to 90C
(5): 100C is Max allowed for 30mins in beta range and 5mins in alpha range then 90C is max

(6): if L7808 is used -54C is the lower limit ; if L23699 oil is used -40C is the lower limit; when ambient tem below 0C, ref starting engines paragraph 18.3.2

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35
Q

Maximum Reverse 0 degrees Indicated HP

A

1,000hp Max at oil temp 0 to 40C

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36
Q

Flight Idle 34 degrees TIT

A

430 to 705C

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37
Q

Flight Idle 34 degrees RPM

A

94.5 to 98.4%

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38
Q

Flight Idle 34 degrees Oil Px RGB

A

250psi except start and warmup 150
(3): operation below 150psi when rpm is below 100% is permitted. If RGB px is between 130-150psi at 100% rpm, record and continue. Maintenance action shall be accomplished prior to next flight.

39
Q

Flight Idle 34 degrees Oil Px P/S

A

100psi start and warmup only, then 60-50

(4): if px is below 50psi at low rpm, condition is acceptable provided px is within limits at 100%rpm

40
Q

Flight Idle 34 degrees Oil Temp

A

90(5) Max
Normal range: 60 to 90C
0C Min

(5): 100C is Max allowed for 30mins in beta range and 5mins in alpha range then 90C is max

41
Q

Flight Idle 34 degrees Indicated HP

A

1,000hp Max at oil temp 0 to 40C

42
Q

Maximum 90 degrees TIT

A

1077C (5 mins Max)

43
Q

Maximum 90 degrees RPM

A

99 to 101(10)%

(10): Takeoff rpm limits: allowable momentary overshoot/undershoot with power lever advancement is 96 to 106%. An overshoot exceeding 106% but immediately returning to within limits must be corrected prior to the next flight. Rpm should be stabilized within 10 secs of initial overshoot

44
Q

Maximum 90 degrees Oil Px RGB

A

150(3) to 250psi

(3): operation below 150psi when rpm is below 100% is permitted. If RGB px is between 130-150psi at 100% rpm, record and continue. Maintenance action shall be accomplished prior to next flight.

45
Q

Maximum 90 degrees Oil Px P/S

A

50-60psi

46
Q

Maximum 90 degrees Oil Px Oil Temp

A

90C (5) Max
40C (8) Min and increasing then 60 (8)
Normal Range: 60 to 90C
(5): 100C is Max allowed for 30mins in beta range and 5mins in alpha range then 90C is max
(8): Operation with oil temp from 50-60C is permitted under extremely cold conditions provided all oil limits are maintained. When oil temp reaches 40C and RGB px shows no fluctuation, Max power may be applied

47
Q

Maximum 90 degrees Oil Px Indicated HP

A

4,600 to 5,300 (engine limiting 3 secs)

48
Q

Military TIT

A

1049C (30 mins)

49
Q

Military RPM

A

101%

50
Q

Military Oil Px RGB

A 
250psi Max (1)
(1): the maximum time allowed at 0 or negative g conditions is 10 secs. Fluctuating oil px is allowed during and following 0 or negative g conditions however a shutdown is required if: 
A. Oil px flux continue longer than 15 secs after returning to positive g flight 
B. Oil px remains at 0 longer than during a momentary transient condition 
C. After 1 min, an air start may be attempted
51
Q

Military Oil Px P/S

A

60psi Max (1)

(1): the maximum time allowed at 0 or negative g conditions is 10 secs. Fluctuating oil px is allowed during and following 0 or negative g conditions however a shutdown is required if:
A. Oil px flux continue longer than 15 secs after returning to positive g flight
B. Oil px remains at 0 longer than during a momentary transient condition
C. After 1 min, an air start may be attempted

52
Q

Military oil temp

A

90C (5) Max
40C (8) Min and increasing then 60 (8)
Normal Range: 60 to 90C
(5): 100C is Max allowed for 30mins in beta range and 5mins in alpha range then 90C is max
(8): Operation with oil temp from 50-60C is permitted under extremely cold conditions provided all oil limits are maintained. When oil temp reaches 40C and RGB px shows no fluctuation, Max power may be applied

53
Q

Military indicated HP

A

4,600SHP Max

4,600 continuous operation
During air start minimum until oil is above 0C
1,000 maximum at oil temp of 0 to 40C

54
Q

Over temp during power change description

A

TIT remains in the 1083 to 1175C range for more than 5 secs or exceeds 1175C

55
Q

Over temp during power change: Ground Operation action required…

A

Reduce power. Shut down, record and call for Mx. An over temp inspection is required

56
Q

Over temp during power change: During Takeoff action required…

A

Reduce power until TIT is 1077C or below. Record and call for Mx prior to next flight.

57
Q

Over temp during power change: In flight action required…

A

Reduce power until TIT is 1010C or below. Record and call for mx prior to next flight.

58
Q

APU Limits EGT (GTCP 95-10)

  • Max Peak
  • Max Peak (10 secs)
  • Max continuous
A

732C
710C (10 secs)
649C

59
Q

APU limits

- Alt / as

A
  • 20,000ft Max
  • 225kts Max
    (can start engine at field elevations up to 6,000ft and temps of -54 to 54C
60
Q

Engine starter operation limits

A

Pull out at 64% rpm

61
Q

Flaps Max Speeds

  • Manuever
  • Takeoff and Approach
  • Land
A
  • 275kts
  • 190kts
  • 170kts
62
Q

Landing gear

  • Flight with landing gear extended and main cabin door open
  • Flight with landing gear extended above 1G and landing gear retraction speed
  • landing lights extended
  • over wing exit
  • APU door open
A
  • 300kts
  • 190kts
  • 260kts
  • 170kts
  • 225kts
63
Q

IRDS turret

  • extended
  • extending and retracting
A
  • 405kts

- 350kts

64
Q

Fuel dump airspeed range

A

140-300kts

65
Q

Air starts

- min airspeed

A
  • 170kts Or 210kts (if range critical)
66
Q

Max airspeed

A

345kts and reduce 6kts per 1000ft

67
Q

Flight Restrions: Max Airspeed with Gross Wt less than 125,000lbs

  • SL to 15K
  • 15K to 20K
  • 20k to 25k
  • 25k and up
A

300Kts

68
Q

Flight Restrions: Max Airspeed with Gross Wt between 125,000lbs and 135,000lbs

  • SL to 15K
  • 15K to 20K
  • 20k to 25k
  • 25k and up
A
  • 225kts
  • 235kts
  • 245kts
  • 255kts
69
Q

Flight Restrions: Max Airspeed with Gross Wt between 135,000lbs and 139,760lbs

  • SL to 15K
  • 15K to 20K
  • 20k to 25k
  • 25k and up
A

215kts

70
Q

Flight restrictions: Symmetric flight gross weight less than 125,000lbs

  • Min
  • Max
A
  1. 0G’s

2. 5G’s

71
Q

Flight restrictions: Symmetric flight with Gross Wt between 125,000lbs and 135,000lbs

  • Min
  • Max
A
  1. 0G’s

2. 0G’s

72
Q

Flight restrictions: Symmetric flight with Gross Wt between 135,000lbs and 139,760lbs

  • Min
  • Max
A
  1. 0G’s

2. 0G’s

73
Q

Flight Restrictions: Roll Manuever with Gross Wt less than 125,000lbs

  • Min
  • Max
A
  1. 0G’s

2. 0G’s

74
Q

Flight Restrictions: Roll Manuever with Gross Wt between 125,000lbs and 135,000lbs

  • Min
  • Max
A
  1. 0G’s

1. 5G’s

75
Q

Flight Restrictions: Roll Manuever with Gross Wt between 135,000lbs and 139,760lbs

  • Min
  • Max
A
  1. 0G’s

1. 5G’s

76
Q

Flight restrictions notes

1: speed restrictions for all gross weights
2: Exceedsnce of restriction limits
3: for aircraft with AFC-784 (outer wing assembly) or standalone center wing repair

A

1: may be exceeded for 1.0G weapons release at air speeds not exceeding 300kts then restricted airspeed re established prior to maneuvering
2: required no additional inspection. If abode restrictions exceeded, make log book entry with type, magnitude and number of occurrences
3: airspeed limited to 300kts, symmetrical flight limits 0 to 2.5G and roll Manuever limits 1.0 to 2.0G at all gross wts

77
Q

Minimum altitude on station: aircraft with operable radalt and raws

  • Day/VMC
  • Night/IMC
A
  • 200ft AGL

- 300ft AGL

78
Q

Minimum altitude on station: aircraft without operable radalt and raws but with updated baro altimeter setting

  • Day/VMC
  • Night/IMC
A
  • 300ft

- 500ft

79
Q

Minimum altitude on station: aircraft with operable radalt or updated baro alt setting

  • Day/VMC
  • Night/IMC
A
  • 500ft

- 1000ft

80
Q

What three primary attitude sources do we have?

A

INS 1, 2 and standby gyro

81
Q

Minimum attitude sources for flight: VMC

A

Any two or three primary attitude sources

82
Q

Minimum attitude Sources for Flight: IMC/cross country

A

All three primary attitude sources, or any two of three primary attitude sources and standby attitude indicator

83
Q

Minimum attitude Sources for Flight: Outside NAVAID coverage

A

Two inertials (both NAV mode) and standby gyro

84
Q

Minimum attitude Sources for Flight: note

A

On aircraft equipped with EFDS, an operable standby attitude indicator (peanut Gyro) is required for flights outside NAVAID coverage and for flights when instrument conditions are anticipated

85
Q

Zero fuel weight definition

A

The aircraft gross weight without usable fuel

Caution: If non-standard fuel management results in the calculated 0 fuel weight exceeding the maximums ZFW limit, the aircraft design load factor is 2.1 g

86
Q

P-3C Max ZFW Limit: Clean Wing

  • with foam
  • without foam
A

80,400lbs

82,400lbs

87
Q

Lateral imbalance maximum differential: For Takeoff

  • Tanks one and four
  • Tanks two and three
A

1400 pounds

5025 pounds

88
Q

Lateral imbalance maximum differential: In Flight

  • Tanks one and four
  • Tanks two and three
A

4,389lbs

No restriction

89
Q

Lateral imbalance maximum differential: For Landing

  • Tanks one and four
  • Tanks two and three
A

4,389

No Restriction

90
Q

Fuel Temp Caution

A

Do not allow Indicated OAT in flight to dwell at or below the freezing point of fuel type Because airframe and engine fuel filters may become blocked if you’ll is chilled below it’s specified freeze point

91
Q

Fuel dumping limitations Warning

A

Feel dumping is prohibited with the wing flaps extended to be on the takeoff/approach position

92
Q

Weight Limitations

  • operations > 135,000 to 139,760 pounds
  • operations > 135,000 pounds
  • Landing at gross weights > 103,880 pounds
  • Landing at gross weights > 114,000 pounds
A
  • May be undertaken only when authorized by the commanding officer and due consideration should be given to other taxiway, runway and aircraft conditions
  • Will result in increased airframe fatigue
  • Shall be made at a minimum rate of descent and shall be documented. Overweight inspection after 10 landings
  • Should be conducted only in an emergency
93
Q

Weight Limits Max

  • Recommended takeoff
  • overload takeoff
  • landing
A

135,000 pounds
139,760 pounds
114,000 pounds

94
Q

Cargo loading limit

A

Floor panel loading is restricted to 60 pounds max per square foot. Cargo should not be stood in any electronics racks

P-3 (14 decks)

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