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Aircraft > C-27J general > Flashcards

C-27J general Flashcards

1
Q

Land as soon as possible:

A

Emergency conditions are urgent and require an immediate landing at the nearest suitable airfield, considering also other factors such as weather conditions and aircraft weight.

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2
Q

Land as soon as practical:

A

Emergency conditions are less urgent. Aircrews use their best judgement to determine if the flight may be safely continued to an airfield where more adequate facilities are available.

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3
Q

Emergency Signal: Abandon Airplane

A

Abandon Airplane - one long sustained blast

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4
Q

Emergency Signal: Bailout

A

Bailout, Prepare - three short blasts

Bailout - One long sustained blast

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5
Q

Emergency Signal: Ditching or Crash Landing

A

Ditching or crash landing imminent - six short blasts

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6
Q

Emergency Signal: Brace For Impact

A

Brace For Impact - one long sustained blast

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7
Q

ACAWS

A

Advisory, Caution, and Warning System (ACAWS)

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8
Q

How many ACAWS alert levels?

A

Four: Special Alerts, Warnings, Cautions, Advisories

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9
Q

Special Alerts

A

Alert the crew of a flight-critical condition that must be corrected to preclude loss of or damage to the aircraft. Most special alerts require an immediate crew response and may have priority over Warning, Caution, and Advisory messages.

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10
Q

Warnings

A

Alert the crew for emergency operation or aircraft system conditions that require immediate corrective or compensatory crew action to prevent personal injury or loss of life. ACAWS warnings are displayed in RED and at the top of the ESA display.

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11
Q

Cautions

A

Alert the crew for abnormal operational or aircraft system conditions that require corrective or compensatory crew action to prevent damage to airplane. ACAWS cautions are displayed in YELLOW and are listed after warnings on the ESA display.

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12
Q

Advisories

A

Alert the crew for operational or aircraft system conditions that may require crew action. ACAWS Advisories are displayed in white and are listed after cautions on the ESA display.

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13
Q

Meaning of term “FAIL”

A

FAIL is used to indicate when the communication from equipment to 1553 data bus is lost. In this case, the equipment functionality is completely lost.

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14
Q

Meaning of term “FAULT”

A

FAULT is used when the equipment BIT detects an anomaly. In this case, the equipment functions could be unreliable.

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15
Q

Aural Characteristics of Warning

A

Sweeping Tone, Continuous until cancelled or cause corrected, press either MASTER WARNING switch light

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16
Q

Aural Characteristics of Caution

A

Two sets of complex tone, repeats at 7 sec interval until cancelled or cause corrected, press either MASTER CAUTION switch light

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17
Q

Aural Characteristics of Advisory

A

Complex “ding, ding” tone, duration 0.84 sec, cancellation automatic after one occurence

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18
Q

Checklist Interrupted

A

If interrupted, the checklist shall be reviewed in its entirety and resumed from the point of interruption. Confirm checklist completion before proceeding to any other checklist.

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19
Q

ENGINE FIRE (Bold Face) EP

A

Engine FIRE Handle (affected engine) - PULL

Engine FIRE Handle (affected engine) - ROTATE LEFT

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20
Q

APU FIRE (Bold Face) EP

A

APU FIRE Handle - PULL

APU FIRE Handle - ROTATE

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21
Q

ELECTRICAL FIRE (Bold Face) EP

A

OXYGEN - ON, 100%

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22
Q

CARGO and/or LAVATORY FIRE/SMOKE/FUMES ELIMINATION (Bold Face) EP

A

OXYGEN - ON, 100%

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23
Q

RAPID DECOMPRESSION

A

OXYGEN - ON, 100%

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24
Q

MAX Airspeed / AWR

A

Max Airspeed is 260 KCAS (.55 mach) AWR is 235 kcas

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25
Q

MIN Airspeed

A

Min Airspeed is 87 KCAS (engine operating limit, 1.2 Vstall with autopilot engaged)

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26
Q

MAX Effort Touchdown

A

Max Effort Touchdown is 1.05 Vstall

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27
Q

X-WIND Takeoff up to 15 knots

A

X-Wind >15 knots = MAX HP 4705

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28
Q

X-WIND Takeoff 16 - 25 knots

A

X-Wind 16-25 knots = MAX HP 2500

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29
Q

MAX Tailwind per AWR

A

Max Tailwind = 10 knots per AWR

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30
Q

MAX X-WIND Component

A

Max Crosswind Component = 25 knots

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31
Q

Tire Limit Speed

A

Tire Limit Speed = 182 knots

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32
Q

High Speed Landing Flight Idle to Ground Idle

A

High Speed Landing = 145 Knots

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33
Q

FLAPS Max Speed: 1 (25%)

A

FLAPS Max Speed: 1 (25%) = 180 KCAS

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34
Q

FLAPS Max Speed: 2 (50%)

A

FLAPS Max Speed: 2 (50%) = 175 KCAS

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35
Q

FLAPS Max Speed: 3 (75%)

A

FLAPS Max Speed: 3 (75%) = 172 KCAS

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36
Q

FLAPS Max Speed: Full (100%)

A

FLAPS Max Speed: Full (100%) = 165 kcas

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37
Q

Landing Gear Max Extend Speed

A

Landing Gear Max Extend Speed = 200 kcas

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38
Q

Landing Gear Max Operating Speed

A

Landing Gear Max Operating Speed = 155 kcas

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39
Q

RAMP, DOOR, and Paratroop Door Max Airspeed

A

Max = 180 kcas

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40
Q

RAMP, DOOR, and Paratroop Door Min Airspeed

A

Min = 105 kcas or 1.15 Vstall

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41
Q

Max Takeoff Weight (MTOW)

A

MTOW = 67, 241 lbs normal and tactical

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42
Q

Max Landing Weight (MLW) - Emergency

A

MLW - Emer = 67, 241 lbs (with 360 vvi limit)

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43
Q

Max Landing Weight (MLW) - Normal

A

MLW - Norm = 60, 627 lbs (with 600 vvi limit)

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44
Q

Max Zero Fuel Weight

A

Max Zero Fuel Weight = 58,422 lbs normal, 57,320 lbs tactical

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45
Q

Max Fuel Load

A

Max Fuel Load = 21,458 lbs

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46
Q

Emergency Fuel

A

EMER Fuel = 1500 lbs ( 750 each main )

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47
Q

Fuel In-flight asymmetry

A

Max 1,300 lbs between mains, Aux no limit

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48
Q

Fuel asymmetry - Takeoff and Landing

A

Max Takeoff or Landing Split = 750 lbs mains, 2,000 lbs Aux

49
Q

Fuel asymmetry - Landing X-Wind

A

X-Wind >5 knots = 400 lbs mains, 900 lbs Aux

50
Q

APU Starting EGT Limit

A

APU Starting EGT Limit = 927 EGT or 718 EGT for 3 seconds

51
Q

ENGINE Starting MGT Limit

A

ENG Start EGT Limit = 807 MGT

52
Q

ENGINE After Starting MGT Limit

A

ENGINE After Starting MGT Limit = 833 MGT

53
Q

ENGINE Operating MGT Limit

A

ENG Operating MGT = 852 MGT

54
Q

TAKEOFF Horsepower

A

T/O HP = 4705

55
Q

TAKEOFF Power Time Limit

A

T/O PWR Time = 5 min

56
Q

Load Factor with gear and flaps extended

A

Load with gear and flaps (any setting) = 0 - -2g

57
Q

APU Starting EGT Limit

A

APU Starting EGT Limit = 927 EGT or 718 EGT for 3 seconds

58
Q

ENGINE Starting MGT Limit

A

ENG Start EGT Limit = 807 MGT

59
Q

Engine Power, Ground Ops

A

Ground Idle with oil temp less than 0 deg, and to 1000 HP with oil temp <45 deg

60
Q

Engine Start “Sing Song”

A
  1. “Box and Clock”
  2. “NG” within 10 seconds
  3. “E-Psi” within 15 seconds
  4. “Fuel Flow / MGT” rise, move right hand from start switch to fire handle at 29% NG
  5. “NP”
  6. “G-PSI” within 15 seconds
  7. “MGT XXX” Peak Note ( 807 Max )
  8. “B and BETA”
  9. “Stable Start” ( 72 NP in LSGI )
61
Q

TAKEOFF Horsepower

A

T/O HP = 4705

62
Q

TAKEOFF Power Time Limit

A

T/O PWR Time = 5 min

63
Q

Load Factor with gear and flaps extended

A

Load with gear and flaps (any setting) = 0 - -2g

64
Q

Engine Start Considerations - MGT

A

Before start, check temp below 175 MGT

65
Q

Engine Start Considerations - NG

A

NG Zero for re-start attempts

66
Q

Engine Power, Ground Ops

A

Ground Idle with oil temp less than 0 deg, and to 1000 HP with oil temp <45 deg

67
Q

Cargo Compartment Dimensions - Length

A

Compartment Length = 337 in (28 ft)

68
Q

C-27J Length

A

Length = 74.4 ft

69
Q

C-27J Height

A

Height = 34.6

70
Q

C-27J Wing Span

A

Wing Span = 94.1 ft

71
Q

C-27J Tailplane Span

A

Tailplane Span = 40.6 ft

72
Q

HALO/HAHO no supplemental oxygen (AWR)

A

Up to 38 HALO/HAHO not using supplemental oxygen + four crewmembers

73
Q

Cargo Compartment Dimensions - Width

A

Compartment Width = 96 in

74
Q

Cargo Compartment Dimensions - Length

A

Compartment Length = 337 in (28 ft)

75
Q

Seating (AWR)

A

Seating per AWR = up to 38 + four crewmembers

76
Q

Static Line Troops (AWR)

A

Up to 26 pre-rigged static line + four crewmembers

77
Q

Static Line (in-flight rigged) per AWR

A

Up to 22 in-flight rigged + four crewmembers

78
Q

HALO/HAHO with supplemental oxygen (AWR)

A

Up to 20 HALO/HAHO on supplemental oxygen + four crewmembers

79
Q

HALO/HAHO no supplemental oxygen (AWR)

A

Up to 38 HALO/HAHO not using supplemental oxygen + four crewmembers

80
Q

Static Ground Run Wind Limits per AWR 0 - 25kts

A

0 - 25 kts front , 0 - 20 kts side, 0 - 15 tail = 4705 hp

81
Q

Static Ground Run Wind Limits per AWR 26 - 35kts

A

26 - 35 kts front, 21 - 35 kts side, 16 - 35 tail = <2500 hp

82
Q

Static Ground Run Wind Limits per AWR 36 - 45kts

A

36 - 45 kts all around = <1250 hp

83
Q

Autopilot restriction per AWR (after takeoff or GA)

A

After takeoff or GA, the autopilot must not be engaged below 1,000 agl

84
Q

Auto-throttle restrictions per AWR

A

Auto-throttle is prohibited during approach phase in icing conditions or below 200’ agl at all times

85
Q

Vmo per AWR (maximum operating speed)

A

Vmo = 235

86
Q

Maximum Load Factor (g-max) per AWR

A

+2.5 Gs

87
Q

Paratroop Door Bundle type and weight

A

Standard A-7A / A-21 bundles, max 500 lbs/bundle

88
Q

Static Ground Run Wind Limits per AWR 26 - 35kts

A

26 - 35 kts = <2500 hp

89
Q

Static Ground Run Wind Limits per AWR 36 - 45kts

A

36 - 45 kts = <1250 hp

90
Q

Medevac Max Litters

A

Up to 27 litter patients plus 6 ambulatory patients

91
Q

How many 463L 88’ x 108” pallets?

A

Up to 3 463L pallets will fit in the cargo compartment

92
Q

How many 463L 88” x 54” half pallets?

A

Up to 5 463L half pallets

93
Q

Number and weight of standard A-22 containers

A

Max 6 gravity airdrop containers, max weight 2.328 lbs/container (rigged)

94
Q

Paratroop Door Bundle type and weight

A

Standard A-7A / A-21 bundles, max 500 lbs/bundle

95
Q

Propulsion System

A

Two Rolls Royce/Allison AE2100D2 turboprops

96
Q

Propellers

A

Dowty R391 six-blade, coarse seeking counter-weight with variable pitch props

97
Q

APU Provides?

A

APU provides bleed air for engine start, A/C, Elec power

98
Q

How many fuel tanks?

A

Four (two aux two main)

99
Q

Total aircraft fuel quantity?

A

Total quantity of up to 3,256 gallons - 21,458 lbs

100
Q

Aux fuel tank capacity?

A

aux tanks capacity 740 gal each, 1,480 gal (total)

101
Q

Fuel Pumps total / each tank

A

8, each of the four tanks has two electrically-driven fuel pumps

102
Q

AC Power (main generators)

A

Two engine driven electrical generator, 115/200 VAC

103
Q

DC 28 VDC supply?

A

Transformer Rectifier Units TRU 1 & TRU 2

104
Q

Hydromechanical Overspeed Governor provides:

A

104% NP (prop rpm) protection

105
Q

First indication of potential BETA MODE LOCKED situation:

A

Absence of both green B’s in the HP dial below 8’ radalt

106
Q

ACAWS logic for takeoff inhibits selected ACAWS messages when all (3) of the following occur:

A
  1. Power lever angles are > 40 deg
  2. Airspeed is between 70 - 140 kcas
  3. Altitude is </= 400 agl
107
Q

BIU Backup mode serves what purpose?

A

In the event that both mission computers are disabled BIU backup mode provides functions necessary to fly the aircraft and make a safe landing.

108
Q

When power levers are fwd of FLT IDLE the FADEC maintains propeller speed at:

A

100% 1020 rpm

109
Q

What altitude is associated with BETA lockout mode?

A

8’ agl, above BETA is locked (entering ground mode/max reverse not permitted)

110
Q

Ground Range on the Power Levers is divided into two ranges:

A

BETA and Reverse

111
Q

Power Levers have two distinct ranges:

A

Ground and Flight

112
Q

When will a green “B” display in the center of the HP dial?

A

When the propeller blade angle is less than 23 deg and BETA lockout is unlocked (ground mode) but greater than 10.5 deg

113
Q

When will the BETA label below the HP display and the BETA 1 and BETA 2 lights illuminate?

A

Propeller is in the BETA range (blade angle less than 10.5 deg)

114
Q

PCU stands for:

A

Pitch Control Unit

114
Q

To prevent the lower cowl from exceeding its temperature limit reverse power is limited for a maximum of:

A

Two min

115
Q

During ground operations if the APU EGT exceeds ??? the APU will shut down automatically.

A

927 C

116
Q

Normal APU EGT temperature limits?

A

718°C for 3 seconds or 788°C for .5 seconds

117
Q

Pressing the entrance pushbutton on the cargo lighting panel located on the left side of the crew entrance door will illuminate the two white dome lights in the front compartment and the white dome light located above the entrance door in the cargo compartment for:

A

Two minutes

118
Q

Do not select auto nav until both CNI – MUs show correct present position and both FOMs are:

A

Three or less

Aircraft (7 decks)

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