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TPC Upgrade > CH. 4 > Flashcards

CH. 4 Flashcards

1
Q

Maximum Normal Taxi and Takeoff Weight

A

164,000 pounds

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2
Q

Maximum Alternate Taxi and Takeoff Weight

A

175,000 pounds

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3
Q

Recommended Landing Weight

A

142,000 pounds

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4
Q

Maximum Normal Landing Weight

A

164,000 pounds

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5
Q

Maximum Alternate Landing Weight

A

175,000 pounds

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6
Q

Due to reduced performance margins, the use of maximum effort speeds during landing when the aircraft is limited to ___ fpm may result in an airframe overstress condition.

A

300 fpm

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7
Q

Where should the aux tanks and external tanks be prior to landing?

A

Aux tank = no restriction
External = ~empty (<= 500 pounds)

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8
Q

Tank Limits
-Outboards
-Inboards
-Total Main
-Aux
-External
-Total without fuselage
-Fuselage
-Total with fuselage

A

-Outboards = 8310
-Inboards = 7650
-Total Main = 31920
-Aux = 5810
-External = 8900
-Total without fuselage = 61,340
-Fuselage = 24,390
-Total with fuselage = 85,730

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9
Q

What are the three categories of fuel management?

A
  1. Primary
  2. Alternate Enroute
  3. Secondary
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10
Q

Explain primary fuel management

A
  • No. 1 and No. 4 always contain 500-1000# more fuel per tank than No. 2 and No. 3
    -No less than 7060# in No. 1 and No. 4 and no less than 6410# in No. 2 and No. 3 when externals contain usable fuel
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11
Q

Explain alternate enroute fuel management

A

Used to maximize weight in outboard tanks during long transit legs, potentially extending airframe service life

-When external/aux contains usable fuel, No. 1/4 are kept at max and contain 500-1000# more than No. 2/3
-Once external/aux empty, use No. 2/3 down to 1520, then use 1/4 down to 1520
-Once all tanks at 1520#, go tank-to engine

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12
Q

Explain secondary fuel management

A

Any fuel management that fails to meet primary or alternate enroute

This will occur when there is usable fuel in the external tanks and the main tanks are partly filled to less than 26,940#

An extreme deviation is operation with No. 1 and No. 4 empty

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13
Q

What are the G limits for area A (Primary Fuel Management with externals and pods)

A

Up to Vh
-1 to 3 symmetrical
0 to 2.33 rolling

Vh to Vd
0 to 2.5 symmetrical
0 to 2 rolling

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14
Q

What are the G limits for area B (Primary Fuel Management with externals and pods)

A

Up to Vh
0 to 2.5 symmetrical
0 to 2 rolling

Vh to Vd
Same

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15
Q

What are the extra requirements to be 540 sink?

A

Gross Weight <= 142,000 pounds
Fuel in 1 or 4 <= 7,320
Fuel in mains <= 28,000

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16
Q

What gross weight range must you be in order to still make 540 sink for a main tank fuel of:

23K
24K
25K
26K
27K
28K

A

23K = Less than 142K gross weight
24K = 115K-142K gross weight
25K = 122K-142K gross weight
26K = 128-142K gross weight
27K = 135K-142K gross weight
28K = 142K gross weight exactly

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17
Q

NOTE: If more than 2.5 degrees aileron tab deflection is required to trim unbalanced fuel at speeds >200 KIAS, reduce Vh to ___ KIAS less than shown in Figures 4.1-1 and 4.1-2

A

5 KIAS less than advertised

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18
Q

If severe turbulence cannot be avoided, flight should be in the range of ___ KIAS above power-off stall speed for the operating gross weight, not to exceed ___ KIAS

A

65 KIAS above power-off stall speed not to exceed 180 KIAS

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19
Q

List the flap speeds in reverse order

A

100 = 145
90 = 145
80 = 150
70 = 155
60 = 165
50 = 183
40 = 190
30 = 200
20 = 210
10 = 220

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20
Q

List the flap speed for

-60
-80

A

60 = 165
80 = 150

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21
Q

List the flap speed for

-70

A

70 = 155

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22
Q

CAUTION: Avoid abrupt or full rudder deflection with flaps lever positioned ___ or greater (high rudder boost) and airspeed ___ KIAS or greater

A

15%
200 KIAS

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23
Q

Landing Gear Speed
Landing Lights Speed

A

Gear = 168
Lights = 250

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24
Q

Cargo door and Ramp speed (all positions and motions including locked)

A

250

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25
Q

Air deflector speed

A

150

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26
Q

Paratroop doors open and locked

A

250

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27
Q

Paratroop doors opening/closing

A

150

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28
Q

High speed drogues

A

185-250

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29
Q

Low speed drogues

A

105-120
130 engaged

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30
Q

Severe turbulent air speed limit

A

180 KIAS

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31
Q

Inoperative windshield anti-icing below 10,000 feet

A

187 KIAS

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32
Q

Max speed with gear doors removed

A

200 KIAS

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33
Q

CAUTION: Since CG shifts with changes in aircraft attitude, if fuel is carried in the fuselage tank, the external tanks should be empty when the fuselage contains less than _____ pounds, or the aircraft is restricted to level flight until external tanks are empty

A

20,000 pounds

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34
Q

Can you turn with the brakes locked on the inside of the turn?

A

No

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35
Q

What are the taxi speed limits for
20 degrees
60 degrees

A

20 = 20 KTS
60 = 5 KTS

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36
Q

What are the limits when taxiing at gross weights above 164,000 pounds?

A
  1. Smooth surfaces
  2. 10 KTS
  3. Shortest distance
  4. Min braking
  5. Only light braking while turning
  6. 20 degrees nosewheel steering
  7. Avoid abrupt or hard uneven application of brakes
37
Q

What is the max nose gear speed and main landing gear speed

A

Nose = 139 KGS
Main = 174 KGS

38
Q

What are the three categories of airfields?

A
  1. High Strength
  2. Marginal Strength
  3. Substandard
39
Q

For normal operations, tire pressure for a nominal tire deflection of ____ percent is recommended as shown by the high strength airfield data in Figure 4.6-2

A

35 percent

40
Q

Minimum soil strength for operation on a Marginal Strength Airfield

A

CBR of 3 (Particular consideration should be given when not 540, or with CBR less than 6)

41
Q

The number of passes on a marginal strength airfield is based on the recommended tire pressures corresponding to ____ percent tire deflection

A

39 percent

42
Q

What are the 8 additional considerations when operating on a marginal strength airfield or substandard airfield?

A

1 . Inflate/Deflate tires to recommended psi for marginal strength
2. Empty externals
3. 10 KGS max taxi
4. Minimize braking if porpoising
5. Minimize nose gear loads by using elevator on takeoff/landing and loading aircraft to mid or aft center of gravity
6. Minimize reverse thrust to prevent FOD
7. Shut off flight station and cargo compartment AC when on unpaved surface to prevent clogging of heat exchanger
8. Limit gross weight to 164K

43
Q

Gross weight and fuel limits for substandard airfields are those corresponding to a ____ fpm sink rate

A

540

44
Q

Explain the max passenger load for extended overwater flights

A

No more than 80 persons including crewmembers for extended over-water flights more than 50 NM from nearest shore line.

Extended over-water ops with mixed pax/cargo loads are restricted to 35 pax per unobstructed overhead exit

45
Q

What is the G limit with any flap extension

A

2 g symmetrical
1.5 g unsymmetrical

46
Q

Prohibited Maneuvers
(Spin Stall Stall)
(7 push slip)
(long roll swap)

A
  1. Aerobatics and Spins
  2. Practice stalls with power above 1,000 HP
  3. Practice asymmetric power stalls
  4. Intentional zero or negative G maneuvers lasting longer than 7 seconds
  5. Sustained airspeed below stick pusher speed
  6. Intentionally maneuvering the aircraft into a sideslip for a LEFT/RIGHT RUDDER alert
  7. Abrupt longitudinal control inputs at high speeds (faster than 1.0 g per second load factor increase or decrease)
  8. Rapid roll reversals (roll rate should be zero momentarily before applying full aileron in the opposite direction)
  9. At airspeeds above 150 KIAS, moderate to large rudder input held until sideslip peaks followed by opposite rudder (past neutral) or a series of large alternating rudder inputs tending to produce successively larger sideslip angles
47
Q

Air Start Altitude limit

A

25,000 feet
22,500 with JP-4

48
Q

Static propeller feathering limit

A

2 cycles

(Then the propeller gearbox must be drained or the engine started)

49
Q

When do you count a static propeller cycle

A

Each time the aux feather pump is used to drive the propeller from feather to reverse to feather

50
Q

Regular feathering limit

A

4 commands

(A command is counted each time the FIRE handle is pulled or the PROPELLER CONTROL SWITCH is placed to FEATHER)

51
Q

Total auxiliary feather pump operating time limit

A

Shall not exceed 80 seconds

52
Q

MGT limit for

-Prior to start
-START
-Max Reverse
-Take-off
-Flight

A

-Prior to start = <=175
-START = <807
-Max Reverse = <833
-Take-off = <=852
-Flight = <833

53
Q

When is an overtemp inspection required based on MGT?

A

-During start, below 65% NG, 807 for 2 seconds is permissible, otherwise an overtemp inspection is required

-If MGT exceeds 852 on take-off, an overtemp inspection is required

54
Q

What is the normal EPSI?

A

40-90 psi (40 to <90 for ground ops)

When oil temp is in normal range and EPSI is holding at or above 90, perform engine shutdown. MX is required.

55
Q

What is the normal GPSI?

A

> 10 Feathered LSGI
110-210 LSGI
170-210 all other times

56
Q

What is the normal oil temp?

A

60-85

Must be above -40C/F for start unless oil has been changed to cold weather oil

Engine power is limited to idle with oil temp less than 0C, and 1000 HP when engine oil temp is less than 45C during ground ops

45C is technically allowed for takeoff

If temp exceeds 93, shut down engine. MX required. If temp is 86-93 for >5 minutes, shutdown is recommended and oil overtemp inspection is required.

57
Q

Prop Aux Pump Limits

30 seconds = ___ cool down
1 minute = ___ cool down
2 minutes = ___ cool down
3 minutes = ___ cool down

A

30 seconds = 5 min cool down
1 minute = 10 min cool down
2 minutes = 20 min cool down
3 minutes = 30 min cool down

58
Q

Engine Starter Duty Cycle Limits

A

70 on
60 off
5 cycles

Then 20 minute cooling

59
Q

What is the Takeoff Crosswind and Tailwind limitation?

A

If wind is not from 315 to 045 degrees relative, and crosswind is greater than 15 but less than 35 knots, the limit it 2500 HP until indicated speed is greater than 35 knots

60
Q

What are the windmilling propellor limitations?

<7 NG FIRE HANDLE IN / FEATHERED
>7 NG FIRE HANDLE IN / FEATHERED
FIRE HANDLE IN / NOT FEATHERED

FIRE HANDLE PULLED / FEATHERED

A

<7 NG FIRE HANDLE IN / FEATHERED = 3 min

> 7 NG FIRE HANDLE IN / FEATHERED = 20 min

FIRE HANDLE IN / NOT FEATHERED = 5 min

FIRE HANDLE PULLED / FEATHERED = 6 hours
(run for 20 min at FLIGHT IDLE)

61
Q

Can you use the APU for bleed air in flight?

A

No, only the ac generator

62
Q

What is the APU starter duty cycle?

A

90 seconds on, 5 minutes off for three cycles, then a wait of 60 minutes (inspect starter after last cycle abort)

63
Q

APU Numbers:

-Door operation
-Start light to on speed
-Normal RPM
-Max RPM
-EGT
-Bleed air pressure
-Bleed air pressure check 30-15 psi
-Voltage
-Load

A

-Door operation = 9-18 seconds
-Start light to on speed = 35 seconds
-Normal RPM = 98-105 percent
-Max RPM = 110 percent
-EGT = 260-680C, 710C max
-Bleed air pressure = 40-50 psi
-Bleed air pressure check 30-15 psi = not less than 22 seconds
-Voltage = 108-117V
-Load = 0-100%

64
Q

When will you get an ACAWS for APU temp?

A

Exceeding 710C for 3 seconds

65
Q

What RPM will the APU automatically shut down?

A

110 percent

66
Q

Pump pressures

-Boost
-Transfer
-Fuselage Tank Transfer

A

-Boost = 15-24 psi
-Transfer = 28-40 psi
-Fuselage Tank Transfer = 28-46 psi

(Boost pump pressures are no flow. Pressures below are acceptable with flow as long as no flow meets limits)

67
Q

Fuel unbalance limits

-Between symmetrical tanks
-Between left and right wing
-Aux exception to left and right wing

A

-Between symmetrical tanks = 1000 lbs

-Between left and right wing = 1500 pounds (except for aux exception)

-Aux exception to left and right wing = One aux full and the other empty, provided all other tanks are symmetrically fueled or unbalanced toward the opposite side within the above limits

68
Q

Fuel temps should not be lower than ___ degrees above the freeze point. What instrument reading should we consider equal to fuel temp?

A

6F (3.3C)

TAT

69
Q

What is the one time limit for using emergency fuel?

A

6 hours

70
Q

What is the worst case scenario of percent range lost due to boil-off from aviation gasoline?

A

20 percent (when fuel temp is 125F and you are climbing to 35,000 feet)

71
Q

What are the 7 times you cannot have the autopilot engaged?

A
  1. Takeoff and Landing
  2. Above Vh
  3. Below 200 HAT (precision) or MDA (non-precision)
  4. IPRA below 200 HAT
  5. At or below 500’ AGL (when not on an approach)
  6. In RVSM unless ALT HOLD can hold +-65 feet
  7. Gross weights above 164K and any of the following:
    a. Below 1,000’ AGL
    b. Configuration changes
    c. Approach
72
Q

Can you use the autopilot with any engine(s) out?

A

Yes, if manual symmetric power changes are made

(Cannot use autothrottles)

73
Q

What approach instrumentation can HF transmissions interfere with?

A

VOR/ILS approaches

74
Q

What are the limits on comms when using secure voice?

A

Nonsecure voice, including interphone, cannot be used at the same time. Crypto must be back in P and PLAIN positions prior to using nonsecure or interphone systems

75
Q

What are the restrictions associated with using a soft panel in flight?

A

If a soft panel is activated in flight because of a hard panel failure or fault, do not attempt to deactivate the soft panel until the aircraft is back on the ground in a parked configuration.

76
Q

Is the CNI-MU LZ function a primary source of navigation data?

A

No. Using it as such is prohibited.

77
Q

What are the airdrop speed restrictions?

A

Above 150 KIAS or with flaps up is prohibited because of the possibility of damage to the aircraft and injury to personnel

78
Q

Tolerance for airspeed indication difference between pilot and co-pilot

A

+- 6 KCAS

79
Q

Static reading of altimeter at field elevation

A

+- 50 feet field elevation

(Standby altimeter does not internally compensate for temperature; therefore, these tolerances only apply for the standby altimeter if the flight station temperature is between 60-85F)

80
Q

Max difference between pilot, co-pilot, and standby altimeter at:

10K
20K
30K

A

10K = 120 feet
20K = 180 feet
30K = 265 feet

Cabin altimeter should be +-500 feet of actual field pressure altitude

81
Q

HUD/PFD and standby compass heading tolerance

A

+-5 degrees

82
Q

Pilot and Copilot HUD/PFD heading tolerence

A

+-2 degrees

83
Q

Engine Instrument Fluctuation Limits:
(Ground operation, below flight idle)

NG
MGT
Fuel Flow

A

NG = +- 1% (not oscillating or quivering rapidly)

MGT = +- 10C

Fuel Flow = +- 10 pph

84
Q

Minimum for one brake application with normal brakes and anti skid OFF is _____ psi

A

2,250 psi

85
Q

What are the normal oxygen regulator readings?

A

270-340 psi breathing
270-455 no flow

(walk around bottle = 375 +- 75 psi)

86
Q

Hydraulic Accumulator Preload:

Utility
Booster
Normal Brakes
Emergency Brakes
Aerial Refueling Hydraulic Accumulator

A

Utility = 1500 (+-100)
Booster = 1500 (+-100)
Normal Brakes = 1500 (+-100)
Emergency Brakes = 1000 (+-100)
Aerial Refueling Hydraulic Accumulator = 1350 (+-50)

87
Q

Differential Pressure Limits:

Outflow valve differential control
Safety valve
Negative pressure relief
Negative pressure limit

A

Outflow valve differential control = 14.3 +- 0.2 in Hg
Safety valve = 15.0 +- 0.3 in Hg (do not exceed 16.0 in Hg)
Negative pressure relief = -0.76 in Hg
Negative pressure limit = Do not exceed -1.6 in Hg

88
Q

Fuel Suppressor Preload:

SPR Fuel Suppressor Precharge
Aerial Refueling Fuel Surge Suppressor Precharge

A

SPR Fuel Suppressor Precharge = 40 (+-5) psi
Aerial Refueling Fuel Surge Suppressor Precharge = 90 (+-5) psi

89
Q

Flap Indicator Limits

UP
50
DN

A

UP = 0 +-1
50 = 50+-8
DN = 100+-7

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