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C-27J general Flashcards

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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
MIN Airspeed
Min Airspeed is 87 KCAS (engine operating limit, 1.2 Vstall with autopilot engaged)
26
MAX Effort Touchdown
Max Effort Touchdown is 1.05 Vstall
27
X-WIND Takeoff up to 15 knots
X-Wind >15 knots = MAX HP 4705
28
X-WIND Takeoff 16 - 25 knots
X-Wind 16-25 knots = MAX HP 2500
29
MAX Tailwind per AWR
Max Tailwind = 10 knots per AWR
30
MAX X-WIND Component
Max Crosswind Component = 25 knots
31
Tire Limit Speed
Tire Limit Speed = 182 knots
32
High Speed Landing Flight Idle to Ground Idle
High Speed Landing = 145 Knots
33
FLAPS Max Speed: 1 (25%)
FLAPS Max Speed: 1 (25%) = 180 KCAS
34
FLAPS Max Speed: 2 (50%)
FLAPS Max Speed: 2 (50%) = 175 KCAS
35
FLAPS Max Speed: 3 (75%)
FLAPS Max Speed: 3 (75%) = 172 KCAS
36
FLAPS Max Speed: Full (100%)
FLAPS Max Speed: Full (100%) = 165 kcas
37
Landing Gear Max Extend Speed
Landing Gear Max Extend Speed = 200 kcas
38
Landing Gear Max Operating Speed
Landing Gear Max Operating Speed = 155 kcas
39
RAMP, DOOR, and Paratroop Door Max Airspeed
Max = 180 kcas
40
RAMP, DOOR, and Paratroop Door Min Airspeed
Min = 105 kcas or 1.15 Vstall
41
Max Takeoff Weight (MTOW)
MTOW = 67, 241 lbs normal and tactical
42
Max Landing Weight (MLW) - Emergency
MLW - Emer = 67, 241 lbs (with 360 vvi limit)
43
Max Landing Weight (MLW) - Normal
MLW - Norm = 60, 627 lbs (with 600 vvi limit)
44
Max Zero Fuel Weight
Max Zero Fuel Weight = 58,422 lbs normal, 57,320 lbs tactical
45
Max Fuel Load
Max Fuel Load = 21,458 lbs
46
Emergency Fuel
EMER Fuel = 1500 lbs ( 750 each main )
47
Fuel In-flight asymmetry
Max 1,300 lbs between mains, Aux no limit
48
Fuel asymmetry - Takeoff and Landing
Max Takeoff or Landing Split = 750 lbs mains, 2,000 lbs Aux
49
Fuel asymmetry - Landing X-Wind
X-Wind >5 knots = 400 lbs mains, 900 lbs Aux
50
APU Starting EGT Limit
APU Starting EGT Limit = 927 EGT or 718 EGT for 3 seconds
51
ENGINE Starting MGT Limit
ENG Start EGT Limit = 807 MGT
52
ENGINE After Starting MGT Limit
ENGINE After Starting MGT Limit = 833 MGT
53
ENGINE Operating MGT Limit
ENG Operating MGT = 852 MGT
54
TAKEOFF Horsepower
T/O HP = 4705
55
TAKEOFF Power Time Limit
T/O PWR Time = 5 min
56
Load Factor with gear and flaps extended
Load with gear and flaps (any setting) = 0 - -2g
57
APU Starting EGT Limit
APU Starting EGT Limit = 927 EGT or 718 EGT for 3 seconds
58
ENGINE Starting MGT Limit
ENG Start EGT Limit = 807 MGT
59
Engine Power, Ground Ops
Ground Idle with oil temp less than 0 deg, and to 1000 HP with oil temp <45 deg
60
Engine Start "Sing Song"
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
TAKEOFF Horsepower
T/O HP = 4705
62
TAKEOFF Power Time Limit
T/O PWR Time = 5 min
63
Load Factor with gear and flaps extended
Load with gear and flaps (any setting) = 0 - -2g
64
Engine Start Considerations - MGT
Before start, check temp below 175 MGT
65
Engine Start Considerations - NG
NG Zero for re-start attempts
66
Engine Power, Ground Ops
Ground Idle with oil temp less than 0 deg, and to 1000 HP with oil temp <45 deg
67
Cargo Compartment Dimensions - Length
Compartment Length = 337 in (28 ft)
68
C-27J Length
Length = 74.4 ft
69
C-27J Height
Height = 34.6
70
C-27J Wing Span
Wing Span = 94.1 ft
71
C-27J Tailplane Span
Tailplane Span = 40.6 ft
72
HALO/HAHO no supplemental oxygen (AWR)
Up to 38 HALO/HAHO not using supplemental oxygen + four crewmembers
73
Cargo Compartment Dimensions - Width
Compartment Width = 96 in
74
Cargo Compartment Dimensions - Length
Compartment Length = 337 in (28 ft)
75
Seating (AWR)
Seating per AWR = up to 38 + four crewmembers
76
Static Line Troops (AWR)
Up to 26 pre-rigged static line + four crewmembers
77
Static Line (in-flight rigged) per AWR
Up to 22 in-flight rigged + four crewmembers
78
HALO/HAHO with supplemental oxygen (AWR)
Up to 20 HALO/HAHO on supplemental oxygen + four crewmembers
79
HALO/HAHO no supplemental oxygen (AWR)
Up to 38 HALO/HAHO not using supplemental oxygen + four crewmembers
80
Static Ground Run Wind Limits per AWR 0 - 25kts
0 - 25 kts front , 0 - 20 kts side, 0 - 15 tail = 4705 hp
81
Static Ground Run Wind Limits per AWR 26 - 35kts
26 - 35 kts front, 21 - 35 kts side, 16 - 35 tail = <2500 hp
82
Static Ground Run Wind Limits per AWR 36 - 45kts
36 - 45 kts all around = <1250 hp
83
Autopilot restriction per AWR (after takeoff or GA)
After takeoff or GA, the autopilot must not be engaged below 1,000 agl
84
Auto-throttle restrictions per AWR
Auto-throttle is prohibited during approach phase in icing conditions or below 200' agl at all times
85
Vmo per AWR (maximum operating speed)
Vmo = 235
86
Maximum Load Factor (g-max) per AWR
+2.5 Gs
87
Paratroop Door Bundle type and weight
Standard A-7A / A-21 bundles, max 500 lbs/bundle
88
Static Ground Run Wind Limits per AWR 26 - 35kts
26 - 35 kts = <2500 hp
89
Static Ground Run Wind Limits per AWR 36 - 45kts
36 - 45 kts = <1250 hp
90
Medevac Max Litters
Up to 27 litter patients plus 6 ambulatory patients
91
How many 463L 88' x 108" pallets?
Up to 3 463L pallets will fit in the cargo compartment
92
How many 463L 88" x 54" half pallets?
Up to 5 463L half pallets
93
Number and weight of standard A-22 containers
Max 6 gravity airdrop containers, max weight 2.328 lbs/container (rigged)
94
Paratroop Door Bundle type and weight
Standard A-7A / A-21 bundles, max 500 lbs/bundle
95
Propulsion System
Two Rolls Royce/Allison AE2100D2 turboprops
96
Propellers
Dowty R391 six-blade, coarse seeking counter-weight with variable pitch props
97
APU Provides?
APU provides bleed air for engine start, A/C, Elec power
98
How many fuel tanks?
Four (two aux two main)
99
Total aircraft fuel quantity?
Total quantity of up to 3,256 gallons - 21,458 lbs
100
Aux fuel tank capacity?
aux tanks capacity 740 gal each, 1,480 gal (total)
101
Fuel Pumps total / each tank
8, each of the four tanks has two electrically-driven fuel pumps
102
AC Power (main generators)
Two engine driven electrical generator, 115/200 VAC
103
DC 28 VDC supply?
Transformer Rectifier Units TRU 1 & TRU 2
104
Hydromechanical Overspeed Governor provides:
104% NP (prop rpm) protection
105
First indication of potential BETA MODE LOCKED situation:
Absence of both green B's in the HP dial below 8' radalt
106
ACAWS logic for takeoff inhibits selected ACAWS messages when all (3) of the following occur:
1. Power lever angles are > 40 deg 2. Airspeed is between 70 - 140 kcas 3. Altitude is
107
BIU Backup mode serves what purpose?
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
When power levers are fwd of FLT IDLE the FADEC maintains propeller speed at:
100% 1020 rpm
109
What altitude is associated with BETA lockout mode?
8' agl, above BETA is locked (entering ground mode/max reverse not permitted)
110
Ground Range on the Power Levers is divided into two ranges:
BETA and Reverse
111
Power Levers have two distinct ranges:
Ground and Flight
112
When will a green "B" display in the center of the HP dial?
When the propeller blade angle is less than 23 deg and BETA lockout is unlocked (ground mode) but greater than 10.5 deg
113
When will the BETA label below the HP display and the BETA 1 and BETA 2 lights illuminate?
Propeller is in the BETA range (blade angle less than 10.5 deg)
114
PCU stands for:
Pitch Control Unit
114
To prevent the lower cowl from exceeding its temperature limit reverse power is limited for a maximum of:
Two min
115
During ground operations if the APU EGT exceeds ??? the APU will shut down automatically.
927 C
116
Normal APU EGT temperature limits?
718°C for 3 seconds or 788°C for .5 seconds
117
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:
Two minutes
118
Do not select auto nav until both CNI – MUs show correct present position and both FOMs are:
Three or less

Aircraft (7 decks)

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