Brainscape's Knowledge GenomeTM

Browse over 1 million classes created by top students, professors, publishers, and experts.


See full index

T-1 Flashcards > T-1 Systems/Trans GK > Flashcards

T-1 Systems/Trans GK Flashcards

1
Q

Red Colored Annunciator

A

Immediate Action, Danger

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

Yellow Colored Annunciator

A

Aircrew Action, not as serious

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

White Colored Annunciator

A

System Advisory

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

Green Colored Annunciator

A

System advisory - Widget working normally

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

Aural Tones sound for:

A

BEAR

B - Boldface situations
E - Exceeding flight envelope
A - Aircraft Configuration
R - Reminders (i.e.: cruise altitude)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q
A

Very Slow

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q
A

Slow

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q
A

On Speed

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q
A

Fast

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q
A

Very Fast

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

Engine Bypass Ratio

A

2:1

66% Bypass: 33% Core

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

What systems make up the Fire Protection System

A
  • Overheat / Fire Detection System
  • Fire Extinguishing Systems
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

Functions of the engine flow divider valve

A
  • Separate fuel flow to engine into primary and secondary flows

1-23 Dash-1

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

Engine Driven Accessories

A

BASE

B - Bleed Air
A - Accessory Gearbox
S - Engine Synchronization System
E - Engine Vibration Indicators

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

ITT is measured in the engine nacelle by:

A
  • 6x Thermo Couplers
  • 2x T1 Probes
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

Cost/benefit of the bleed air system

A

Good:

  • Air clean (no fuel, oil, or exhaust fumes)
  • Hot
  • Under pressure
  • Large quantity available

Bad:

-Degrades engine performance

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
17
Q

Fuel capacity of fuselage tanks

A

2462 lbs total

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
18
Q

Fuel capacity of wing tanks

A

2781 lbs total

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
19
Q

Boost Pump functions

A
  • Engine start
  • Cross feed fuel
  • Primary Jet Pump backup
  • Motive flow for transfer jet pumps
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
20
Q

Explain Fuel Cross Feed

A
  • Fuel flows from one wing to both engines
  • Fuel flows only from whichever wing is selected by the Cross Feed controls
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
21
Q

How much extra fuel can the T-1 take if pressure fueled ?

A

~215 lbs

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
22
Q

Icing inhibitor required

A

0.04% - 0.15%

5-11 Dash-1

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
23
Q

How many fuel tanks are in the T-1?

A

6x total:

  1. Left wing
  2. Right wing
  3. Left Mid
  4. Right Mid
  5. Aft Fuselage
  6. Aft Cabin
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
24
Q

How many fuel probes are in the T-1?

A

12x total:

  • 4x in left wing
  • 4x in right wing
  • 2x in left mid
  • 1x Aft fuselage
  • 1x Aft cabin
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
25
Q

Allowed fuel types

A

Jet A

Jet A-1

Jet B

JP-4

JP-5

JP-8

JP-8 +100

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
26
Q

Fuel Temperature Limitations

A

-40°C - +50°C

5-11 Dash-1

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
27
Q

At what pressure does the fuel filter bypass valve open?

A

2.3 +/- 0.2 psi

1-51 Daash-1

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
28
Q

When does wing overpressurization occur?

A

3.5 +/- 0.5 psi

1-49, 1-51 Dash-1

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
29
Q

Items on the Left Hand Load Bus

A

NO RAISE

N – Nonessentials (L)
O – Overhead Panel
R – Radio Masters (L)
A - AHRS
I – Inverter 1
S – Standby Bus
E – Emergency Bus

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
30
Q

Items on Right Hand Load Bus

A

IRON G

I - Inverter 2
R - Radio Masters (R)
O - Overhead Panel
N - Nonessentials (R)

G - Galley Bus (R Main)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
31
Q

Items on the Standby Bus

A

CRUISE

C – Copilot Instrument Lights
R – RTU 1
U – UHF
I – ITT (L)
S – Stby Attitude/Altimeter
E – EFC Eng Start

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
32
Q

Items on the Emergency Bus

A

SLEEVES

S – Selected Left Hand Inst
L – Landing Gear Lts
E – Engine Fire/Cabin Smoke
E – Emergency Pitch Trim
V – VHF (NAV 1)
E – Emergency Lights
S – Standby Bus

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
33
Q

Purpose of the GCU

A

GORE

G – Ground Fault Protection
O – Overvoltage Protection
R – Reverse current Protection
E – Equalize gen outputs

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
34
Q

What is powered by the AC current system

A

PG FOG

P – Pitch trim indicator
G – GPWS

F – Flap ind & Flap assym
O – Oil Px ind (R&L)
G – GRE (Ground Recording Equip)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
35
Q

When does the boost pump automatically engage?

A

EFFC

E – Engine Start
F – Fuel Feed Chamber less than full
F – Fuel Pressure Low
C – Cross Feed

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
36
Q

When does the Ignition System automatically activate?

A

SEE

S – Stick Shaker (Stall)
E – Engine Anti-Ice
E – Engine Start

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
37
Q

What is contained in the Accessory Box?

A

SHOPPN

S – Starter Generator
H – HMU
O – Oil Pump
P – Hydraulic Pump
P – Engine Driven Fuel Pump
N – N2 Sensors

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
38
Q

What is the nose gear strut extension?

A

Approx 3.5 inches for nominal CG

2-5 Dash-1

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
39
Q

Hot Start possible causes

A
  • Incorrect starting procedure
  • Bleed air system(s) left on
  • Early starter dropout
  • No %N1 RPM during start (possibly frozen due to ice in the inlet)
  • Leaking pneumatic line
  • Faulty HMU or misadjusted HMU linkage
  • Faulty igniter, power supply or igniters

1-29 Dash-1

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
40
Q

False or Hung Start possible causes

A
  • Incorrect starting procedure
  • EFC not out of reversion
  • Bleed air system(s) left on
  • Faulty HMU
  • Misadjusted HMU linkage or HMU regulating valve stuck
  • Flow divider valve malfunction or leak

1-29, Dash-1

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
41
Q

Engine Fails to Start

posible causes

A
  • Incorrect starting procedure
  • Faulty igniter system power supply or igniters
  • Faulty HMU
  • Misadjusted HMU linkage or HMU regulating valve stuck
  • Faulty fuel supply system or contamination
  • Flow divider valve malfunction or blockage

1-29 Dash-1

42
Q

Engine Fails To Accelerate From Idle

(after a normal start)

possible causes

A
  • EFC is not ON and out of reversion
  • HMU or flow divider valve leaks or restrictions
  • Faulty fuel supply system to engine or blockage

1-29 Dash-1

43
Q

Normal engine start criteria

A
  • Light-off occurs within 10 seconds after advancing the throttle to IDLE
  • The engine accelerates normally to idle RPM
  • ITT does not exceed the start temperature limitations during the acceleration to stabilized idle RPM
  • Oil pressure is at least 40 psi

1-29 Dash-1

44
Q

Land As Soon As Practicle

A
  • Emergency conditions are less urgent and although the mission is to be terminated,
  • The degree of the emergency is such that an immediate landing at the nearest adequate airfield may not be necessary.
45
Q

Land As Soon As Possible

A
  • An emergency will be declared. A landing should be accomplished at the nearest suitable airfield considering
  • The severity of the emergency
  • Weather conditions
  • Field facilities
  • Aambient lighting
  • Aircraft gross weight
  • and Command guidance
46
Q

Dash-1 Section II

What’s the deal with Asterisk (*) items?

A

They do not need to be accomplished on subsequent flights by the same crew, flying the same aircraft, on the same day

47
Q

Where can you find weight and balance information on the T-1?

A

Dash-1 Section V

1 Dash-1

48
Q

Before Exterior Inspection

How long should the knife valve be open?

A

¼ inch minimum

49
Q

Before Exterior Inspection

Should you test the AHRS battery multiple times?

A

No

50
Q

Before Exterior Inspection

What is the fuel reading tolerance after being pressure refueled?

A

+/-50 lbs

51
Q

Exterior Inspection

When is NWS lost?

A

When the mechanical disconnect pin is disconnected

52
Q

Interior Inspection

What altitude do you set the Cabin Pressure Controller?

A
  • The higher of 1,000 feet above cruise altitude or,
  • 500 feet above field elevation
53
Q

Interior Inspection

How low can the pneumatic pressure gage read?

A

Down to 1305 at 0° F

54
Q

Interior Inspection

How many door locking pins are there in the entrance door?

A

8x

55
Q

Before Starting Engines

If a GPU is not available, what power sources should be turned on?

A

Battery and Standby Battery

56
Q

Before Starting Engines

When checking the indicator lights, which lights will not illuminate?

A
  • Red LDG Gear unlock indicator light
  • GRND COMM
  • Yellow ENG START (both)
  • White starter DISENGAGE button
  • ELT ON annunciator
57
Q

Before Starting Engines

When performing a battery start, which step of the checklist do you not complete before completing the Starting Engines Checklist?

A
  1. Fuel crossfeed
58
Q

Before Starting Engines

After how many seconds of continuous pitch or roll trim engagement does the trim warning horn sound?

A

5 seconds

59
Q

Starting Engines

At what ambient temperature is an external power unit required for engine start?

A

Below 5° F (-15° C)

60
Q

Starting Engines

What are reasons to abort a start?

A

B A W N I Y C A I R O

B - Boost pump light does not light up
A - No Automatic Starter Dropout by 45% N2
W - White Starter Disengage button does not light up
N - No turbine rotation
I - ITT rises with no increase in %N2
Y - Yellow Start button does not light up

C - Throttle placed in CUTOFF
A - Anything Abnormal
I - No rise in ITT after bumping throttle to 8%
R - No N1 Rotation after throttle are in idle
O - No Oil Px indication

61
Q

Starting Engines

Abort start procedures after throttles have been brought to IDLE

A

THROTTLE - CUTOFF
IGNITION SWITCH - OFF
STARTER - MOTOR FOR 15 SECONDS
STARTER DISENGAGE BUTTON - PRESS

62
Q

Starting Engines
Abort start procedure if starter dropout doesn’t happen by 45%N2

A

STARTER DISENGAGE BUTTON - PRESS
If the yellow start button and white disengage button do not extinguish:
THROTTLES - CUTOFF
BATTERY - OFF
MASTER GEN (BOTH) - EMER

63
Q

Starting Engines

During a generator assisted start, the operating engine must be at ___ to avoid damaging the generator.

A

IDLE

64
Q

Starting Engines
Under what conditions must you have the Engine anti-ice turned on for taxi and takeoff?

A

OAT/SAT of 5° C or colder

65
Q

Before Taxi
Is the AOA test accurate in the air or with flaps extended

A

NOPE

66
Q

Before Taxi
Horizontal Stabilizer operation light

A
  • 12 positions
  • Each position powered for 0.6 seconds
67
Q

Taxi

If a malfunction in the anti-skid system occurs w/ an associated loss of brakes, what should happen to recover control?

A

ANTI-SKID - OFF
BRAKES - AS REQUIRED
If braking is not restored:
EMER BRAKE - AS REQUIRED

68
Q

Taxi

How long will do you have to wait for normal braking after testing the anti-skid system?

A

Approx. 4 seconds

69
Q

Before Takeoff
Why do we not use engine crossfeed on takeoff, final approach, or landing?

A

To prevent dual engine flame out

70
Q

Before Takeoff
When can you operate wing anti ice on the ground?

A
  • Preflight testing
  • Landing rollout
71
Q

Before Takeoff
Crew Briefing Basics:

A

N E R A N A (kind of like Nirvana)
N - Normal takeoff
E - Emergency takeoff
R - Emergency Return
A - ATC cleared departure procedures
N - Noise abatement
A - Altimeter setting

(Dash-1, 2-22)

72
Q

Takeoff
Static takeoff procedure:

A
  1. Line up, hold brakes
  2. Set power approx. 80%
  3. Check engine (and flight) instruments
  4. Release brakes and advance power to target N1
  5. Set TRT prior to 60 KIAS
  6. Both hands on control wheel at S1
  7. Rotate 13-15 at Vrot
73
Q

Takeoff
Wake turbulence considerations

A
  • 2 minutes (min) behind large AC or helos
  • 3 minutes (min) behind Boeing 757 or heavy jet AC
  • With consistent 5 knot crosswind, you can reduce the interval
  • Remain above and upwind of the flightpath of the preceding AC
74
Q

After Takeoff

What elevation does the performance data expect you to bring your gear up by?

A

50 feet AGL

75
Q

After Takeoff
Dual Engine Climbout Speed:

A

Vco + 10

76
Q

Cruise

What kind of temperature drop will reduce the Px in the O2 tank?

A

100° F (20% reduction)

77
Q

Maximum range descent:

A

Idle power
Clean
0.70 IMN/ 230 KIAS (AB/BL 35,900’)

78
Q

Enroute Descent:

A

Idle power
Speed Brakes - Out
0.70 IMN/ 250 KIAS (AB/BL 32,300’)

79
Q

Penetration Descent:

A

Only used under 20,000’
Throttles - Idle/As Required
Speed Brakes - As Necessary (to descend & decelerate)
Airspeed - 180 KIAS
Pitch - Approx. 3° NL
Level off & reduce drag - Approx 1,000’ above desired altitude

80
Q

Rapid Descent:

A

Throttles - Idle
Speed Brakes - Extended
0.78 IMN/ 330 KIAS (AB/BL 24,800’)

81
Q

Descent Crew Briefing Minimums:

A

Destination
Weather
How the approach will be flown

82
Q

Do you use the radio altimeter for decision heights?

A

Nope, used to indicate absolute altitude only

83
Q

Descent
How do we set the cabin pressure?

A
  • 500’ above landing field Px altitude
  • Rate control commensurate w/ AC rate of discent
84
Q

Radar downwind airspeed:

A

200 KIAS

85
Q

Low Altitude Approach airspeed:

A

180 KIAS

86
Q

Circling Approach airspeed:

A

Vapp + 10 KIAS prior to final

87
Q

Use of 30° flaps after encountering icing is permitted only when:

A

-Icing encountered was for less than 10 min & it was warmer than -8° C
or
-A RAT of +10° C or warmer is observed during the descent, approach, or landing

88
Q

What is the lowest altitude you can roll flaps to 30°?

A

250 AGL

89
Q

Go around flap retraction speed:

A

Vref + 20 KIAS

90
Q

Can you use aux cool with one engine running?

A

No

Dash-1, 2-35

91
Q

Maximum Zero Fuel Weight:

A

13,000 lbs

92
Q

Cabin Floor Loading limit:

A

100 lb/sq ft

93
Q

Prohibited Maneuvers:

A
  • Bank angle in excess of 60°
  • Pitch attitude in excess of 30°
  • Spins
  • Takeoff & Landing on unprepared surfaces
94
Q

Acceleration Limitations:

A

Flaps up: -1.0 to +3.2 G’s
Flaps out: 0 to +2.0 G’s

95
Q

Maximum rate of descent at touchdown:

A

600 feet per minute

96
Q

Taxi compatible arresting cables:

A

5 knots max
-BAK 9
-BAK 12
-BAK 13
(looks like they pop up from the RWY)

97
Q

Quantity of Fuel Icing Inhibitor Required:

A

0.04 - 0.15%

98
Q

GPU Limitations:

A

28 - 28.5 VDC
1,000-1,500 Amps

99
Q

Maximum airfield Px altitude TO/LDG

A

10,000’

100
Q

Ambient temperature range for TO/LDG

A

-40° C to ISA +35° C

101
Q

Ambient temperature range for cruise

A

-65° C to ISA +35° C

T-1 Flashcards (13 decks)

Brainscape helps you reach your goals faster, through stronger study habits.
© 2024 Bold Learning Solutions. Terms and Conditions