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6112A Flashcards

1
Q

Scope of the NATOPS

A

contains flight clearance information, operating procedures and restrictions necessary for flight crews to effectively operate their aircraftno manual can address every situation completely or be a substitute for sound judgement

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2
Q

Takeoff power max

A

4700 hp at temps up to 39.4*C (104*F) at sea level no bleed air

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3
Q

max continuous power

A

4700 hp at 28.3*C (83*F) sea level with both a/c packs on

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4
Q

Overspeed protection

A
  • Np >104.5% the overspeed governor diverts oil from PCU to increase blade angle and control overspeed
  • Np >106% fuel flow is decrease
  • Np >119% the FADEC shuts down the engine
  • Ng >109% the FADEC shuts down the engine
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5
Q

AFCS Basic Operation

A
  • -Used for 4-,3-engine operation during climb, cruise, descent and approach
  • -Capable of intercepts of 90* (75* loc BC) 45*preferred
  • -Autothrottles will not allow speed below 1.2 Vs
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6
Q

Autopilot Limitations

A
  1. T/o and LDG
  2. A/S > Vh
  3. ILS Below 200’ HAT, Below MDA on NPA, over localizer
  4. IPRA below 200’ HAT
  5. At or below 500’ non-app operations
  6. RVSM ALT plus/minus 65’
  7. Weight >164,000 lbs below 1,000’ AGL, config changes or approach operations
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7
Q

3 distinct phases of emergencies

A
  1. Establish and maintain A/C control, flt path clear of terrain, identify and verify nature of malfunction and complete memory items
  2. Complete ACAWS crew action items, engine-out considerations, determine COA (continue, mission abort, return to base/divert, etc.) and brief the plan
  3. Monitoring/managing degraded systems, prepare fro unscheduled LDG if necessary, employ crewmember at ACS`
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8
Q

Immediate actions and stabilization during emergency

A
  • Regardless of altitude PF keep controls and maintain safe flight path until immediate action items are completed- <1000 AGL
  • PM announce nature of malfunction (engine failure) and perform duties as required
  • >1000 AGL PM state precise nature of malfunction (gearbox No. 1 no oil pressure), PF shall verify and verbally confirm malfunction, AC then calls for appropriate checklist/crew action
  • AC should assume role of PM
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9
Q

Takeoff Abort Criteria<70 kts

A
  • Abort if a major condition arises
  • Abort with WARNING-CAUTION ACAWS
  • Abort with any ADVISORY ACAWS associated with a malfunction
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10
Q

Takeoff Abort Criteria>70kts to V1 (Vref)

A
  • Abort if a major condition arises
  • Abort for a MASTER CAUTION/WARNING AURAL and VISUAL ALERT that threatens takeoff
  • Abort for an engine failure, fire or serious directional control problems exists
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11
Q

Takeoff Abort Criteria>V1 (Vref)

A
  • Continue takeoff unless airworthiness of A/C is in jeopardy
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12
Q

Flaps 10

A

220kias

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13
Q

flaps 20

A

210kias

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14
Q

flaps 30

A

200kias

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15
Q

flaps 40

A

190kias

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16
Q

flaps 50

A

183kias

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17
Q

flaps 60

A

165kias

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18
Q

flaps 70

A

155kias

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19
Q

flaps 80

A

150kias

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20
Q

flaps 90

A

145kias

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21
Q

flaps 100

A

145kias

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22
Q

ldg gear extended

A

168kias

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23
Q

ldg gear lights extended

A

250kias

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24
Q

cargo door open and locked, ramp up and locked

A

250kias

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25
Q

cargo door (all positions)

A

250kias

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26
Q

ramp (all positions)

A

250kias

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27
Q

paratroop air deflectors open

A

150kias

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28
Q

paratroop doors open and locked

A

250kias

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29
Q

paratroop doors opening/closing

A

150kias

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30
Q

high-speed drogues

A

185-250kias

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31
Q

low-speed drogues

A

105-120kias

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32
Q

low-speed drogues engaged

A

130kias

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33
Q

severe turbulent airspeed

A

65kias above stall to 180kias

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34
Q

inop windshield nesa below 10,000ft

A

187kias

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35
Q

ldg gear door removed max speed, gear up

A

200kias

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36
Q

ldg gear door removed max speed, gear down

A

168kias

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37
Q

Taxi t/o max normal weight

A

164,000lbs

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38
Q

taxi t/o max alternate weight

A

175,000lbs

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39
Q

landing recommended sink rate 540fpm

A

142,000lbs

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40
Q

landing max normal sink rate 300fpm

A

164,000lbs

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41
Q

landing max alternate sink rate 300fpm

A

175,000lbs

42
Q

sink rate limit with ar podstanks 1/4main tanks

A

tanks 1/4: 7,320lbs…..main tanks: 28,000lbs

43
Q

sink rate limit with aux tanks

44
Q

sink rate limit with ext tanks

A

less than or equal to 500lbs

45
Q

nose gear deflections 20*

46
Q

nose gear deflection 60*

47
Q

max nose wheel tire speed

48
Q

max main wheel tire speed

49
Q

Fuel weight unbalance limits

A
  1. 1,000 pounds between symmetrical pair (main/ext)
  2. 1,500 pounds between wings
  3. One aux tank full and other aux tank empty, provided all other tanks are symmetrical or unbalanced toward the opposite side
  4. # 1/#4 always contain 500-1000lbs more than #2/#3 except when total usable fuel is less than 6000lbs
50
Q

T/O landing fuel management

A
  1. each tank is w/in respective weight limit
  2. 1/4 have 500-1000 more than 2/3
  3. main tanks full except for STTOC, 1/4 greater than or equal to 7060lbs, 2/3 are greater than or equal to 6410lbs when externals have fuel
  4. fuel unbalance within limits
  5. sink rate limits are in accordance with chart
51
Q

Enroute fuel management

A
  1. each tank w/in respective limit
  2. aux/ext contain usable fuel, 1/4 kept at 8310 and 500-1000 more than 2/3
  3. W/O usable fuel in aux/ext, 1/4 stay @ 8310, crossfeed 2/3 down to 1520 then crossfeed 1/4 down to 1520
  4. fuel unbalance within limits
  5. sink rate limits in accordance with sink rate chart if outboards are full
52
Q

eng start limit

A

70 secs on, 60 secs off for 5 cycles then 20 minute cooling cycle needed

53
Q

apu limit

A

start duty cycle: 1 minute on and 4 minutes off no limit to duty cycle MAX cont EGT 680*C If EGT exceeds 710*C for >3 sec reduce APU load’ APU auto shutdown if RPM exceeds 110

54
Q

Fuel tank limits 1/4

55
Q

fuel tank limits 2/3

56
Q

fuel tank limits aux

57
Q

fuel tank limits ext

58
Q

fuel tank limits fuselage tank

59
Q

Engine Failure Below Refusal Speed

A

A. Aborted Takeoff procedures……Perform (PF)

60
Q

Engine Failure After Refusal Speed

A

A. Takeoff……….Continue (PF) B. Directional Control……..Maintain (PF)-Maintain directional control and wings level with rudder and ailerons. At rotation speed: C. Aircraft attitude….Rotate to target pitch (PF)WARNING: Rotating at significantly less than 3 degrees per second or rotating to a pitch attitude significantly below the target may delay liftoff and result in not clearing obstacles.

61
Q

Aborted Takeoff

A

A. Abort……………….Announce (PF) B. Power levers……GND IDLE (PF) C. Brakes and nose wheel steering…………As required (PF)

62
Q

Engine Fire Shutdown

A

A. Fire Handle…………..Pull (PM)B. Agent………Discharge (if required) (PM)C. ENGINE START switch………..STOP (PM)

63
Q

APU Fire (Ground/In Flight)

A

A. APU Fire Handle………….Pull (P/CP/PM) B. Agent…………….Discharge (if required) (P/CP/PM)

64
Q

Fire/Smoke/Fumes Elimination

A

A. Crew/Passengers……………..Notify (PF/PM)B. Oxygen………………..Emergency, 100%, ON (ALL)

65
Q

Rapid Decompression

A

A. Oxygen……………………..Normal, 100%, ON (ALL)

66
Q

Four Engine Flameout

A

A. Aircraft attitude…..Adjust to maintain 15-28% NG (PF) B. Power levers (all)………………FLT IDLE (PF) C. CROSS FEED switches………………….CLSD (PM/CM) D. #2 and #3 ENGINE START switches………STOP, START, Release (PM) E. #1 and #4 ENGINE START switches………..STOP, START, Release (PM)

67
Q

Hose Rapid Trail

A

(-109 Reel) A. RAPID TRAIL………………….Announce (CM) B. MASTER POWER LSK………………OFF (CM/PM) (-110 Reel) A. RAPID TRAIL…………Announce (CM)

68
Q

Broken Hose

A

A. Broken Hose/Breakaway…..Announce (as required) (CM/PM) B. HYDRAULIC POWER LSK…………..OFF (CM/PM) C. MASTER POWER LSK………….OFF (CM/PM)

69
Q

Hydraulic System Pressure LO/LOSS/LEAK

A

A. ENGINE PUMPS switches (affected system)………….OFF (PM) B. SUCTION BOOST PUMPS switch (affected system)……….OFF (PM)

70
Q

WINDSHEAR/GCAS/TAWS PULL UP Alert Recovery

A

A. TAKEOFF power…………..set (PF) B. Aircraft attitude………….wings level, nose up (PF) C. Radar altitude, airspeed, and sink rate (as appropriate……………………Call out (PM)

71
Q

Ground Evacuation

A

A. Parking Brake……Set (P) B. Tower………………Notify (CP) C. Pressurization………….EMER DEPRESS (CP) D. Exits……………………..Open (as required) (CM) E. FIRE Handles for all engines and APU…………..Pull (CP) F. Crew/Passengers………….Notify to evacuate the aircraft (CP)

72
Q

Ground evacuation alarm – abandoned aircraft

A

one long sustained ring

73
Q

prepare to bailout alarm bailout alarm

A

3 short rings one long sustained ring

74
Q

ditching/crash imminent brace for impact

A

6 short rings one long sustained ring

75
Q

how many overhead escape hatches

A

3 forward, center and aft

76
Q

primary ground exit

A

crew entrance door

77
Q

primary air exit

A

cargo door/ramp

78
Q

how many fire extinguishers

79
Q

of first aid kits

80
Q

of hand axes

81
Q

of emergency exit lights

82
Q

of life vest stowage

83
Q

of escape ropes

84
Q

size of liferafts

A

20 person 30 person max/liferaft we carry four in the wings and one in the cargo compartment

85
Q

how many walk-around O2 bottles

A

4, 2 up front one by the manual shutoff in the cargo compartment and the 4th by the ramp/door

86
Q

What are the factors for an abort?

A
  1. airspeed 2. seriousness of malfunction/degraded condition some warnings/cautions are inhibited from 70-140KIAS and below 400’ AGL
87
Q

Engine fire shutdown

A

WARNING=== applies if smoke or flames occur WARNING=== agent should only be discharged if condition persists after the fire handle was pulled or if any other indication or malfunction is suspected that requires the fire ext agent

88
Q

Engine shutdown ACAWS

A

WARNINGS: -START VLV OPEN -ENG FIRE -MGT HI CAUTIONS: -ENG FLAMEOUT -FADEC A & B FAIL -GBOX NO OIL PRESSURE -PRESS HI / PRESS LO -HOT START -NP LO -OIL HOT -OIL LOW -PROP 1 CNTL LOST -PROP NO 119% PROTECT ADVISORIES: -ENG NO LIGHTOFF -ENG STAGNATED START

89
Q

What caution is advised with UTIL SYS PRESS HI (C) or BSTR SYS PRESS HI (C) or for EXCESSIVE HYD SYSTEM PRESSURE?

A

DON’T shut down an engine! You will lose your pressure relief

90
Q

If bleed air is available an airstart can be accomplished at an airspeed less than ___KIAS (Ng

A

250 KIAS <29% Ng

91
Q

If bleed air is not available, Ng needs to be?

A

15% < Ng < 29%

92
Q

Altitudes for an airstart with what fuel?

A

25,000’ JP-5/JP-8 Jet A 22,500’ JP-4

93
Q

What must the MGT be less than for start?

94
Q

What would make you not try a restart?

A

Eng vibration, fire or fluid leak

95
Q

Purpose of the engine system?

A

monitor operation of engines, complete operations of engine and assist. Primary purpose is to supply power to the four propellers

96
Q

3 major assemblies of the engine

A
  1. power section 2. torquemeter 3. propeller gearbox
97
Q

what does the torquemeter do?

A

it transmits power from the power section to the PGB

98
Q

what does the PGB do?

A

transfers shaft horsepower to the Prop and powers power to the GMAD

99
Q

what does the power section do?

A

provides power to the PGB with the 14 stage compressor, 2 stage gas generator turbine and 2 stage free power turbine

100
Q

GMAD provides drive pads for:

A

-PCU -overspeed governor -pgb oil pump and scavenge pump -ac generator -hydraulic pump -prop high pressure oil pump

101
Q

Power section accessory gearbox provides drive pads for?

A

-Fuel pump metering unit (FPMU) -Permanent magnetic alternator (PMA) -oil pressure and scavenge pumps -air turbine starter

102
Q

engine oil tank specs

A

20 gal reservoir 12 gals liquid and 8 gals air with 0.66 gal reserve for aux feathering

KC-130J (12 decks)

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