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Checkride > FT4290 GK > Flashcards

FT4290 GK Flashcards

1
Q

Reasons to Abort the start

A
  1. ITT exceed 1000C
    2.ITT 871-1000    C >5sec
    3.Normal N1 increase halted
  2. No ITT rise within in Sec of FF
    5.Bat Bus Annunciator
  3. PCL is moved or ST READY goes out
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2
Q

When is a motoring run procedure required

A

If fuel is introduced

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3
Q

red BAT BUS

A

BAT BUS inop or BAT BUS CWS circuit breaker

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4
Q

red GEN BUS

A

GEN BUS inop or GEN BUS CWS circuit breaker

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5
Q

red PMU FAIL

A

PMU Failure

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6
Q

red GEN

A

Gen inop

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7
Q

red CKPT PX

A

cockpit over pressurization, Px exceed 3.9-4.0psi

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8
Q

Red CANOPY

A

Canopy unlocked/unsafe

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9
Q

Red FUEL PX

A

Fuel pressure in motive flow line <10psi

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10
Q

red OIL PX

A

Oil PX is….
Below 15 psi
15-40 psi for 5 sec at IDLE
below 40 PSI above IDLE

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11
Q

red OBOGS FAIL

A

OBIGS sys malf

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12
Q

red CHIP

A

CHIP detector indicates oil contamination

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13
Q

amber CKPT ALT

A

CKPT px alt above 19,000 ft

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14
Q

amber DUCT TEMP

A

environmental duct or defog duct above 300*F

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15
Q

amber HYDR FL LO

A

HYD res fluid level below 1 QT

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16
Q

amber BUS TIE

A

Bus tie inop or open

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17
Q

amber FUEL BAL

A

fuel imbalance exceed 30lbs for 2 min
Fuel probe/EDM fail

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18
Q

amber EHYD PX LO

A

emergency accumulator @ or below 2400 +/-150 psi

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19
Q

amber OBOGS TEMP

A

OBOGS above 200*F

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20
Q

amber TAD FAIL

A

Trim aid device fail

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21
Q

amber L/R FUEL LO

A

Wing tank below 110lbs usable fuel

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22
Q

amber PMU STATUS

A

PMU detected in flight fault, or WOW

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23
Q

amber OIL PX

A

Oil PX is…
15-40PSI at IDLE
40-90PSI above IDLE

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24
Q

Land as soon as possible definition

A

an emergency shall be declared and a landing accomplished at the nearest suitable landing area considering severity, wx, field facilities, ambient lighting and command guidance

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25
Q

Land as soon a practical definition

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 may not be necessary

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26
Q

Suitable landing area definition

A

hard surface runway, taxiway, or over/underrun

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27
Q

BATT BUS fail effect on configuration

A

Use emer gear extension
AOA, GEAR/FLAP indication inop

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28
Q

GEN BUS fail effect on configuration

A

ASI,TAS,VSI,Altimeter, SMU, TAD VHF nav inop, AOA pitot heat inop

fly formation approach/GPS approach, normal gear/flap extension

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29
Q

HYDRAULIC FAIL effect on configuration

A

-Normal gear/flaps inop below 1800 psi
-EHYD PX LO or HYDR FL LO could be small leak to not trigger fuse, day VMC consider lowering gear

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30
Q

AOA computer fail on TP Stalls

A

-stick shaker malfunctions do not mean problem with AOA indicator
-Fly known pitch and power

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31
Q

Oil tank capacity

A

10 quarts

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32
Q

Normal oil level on Dipstick

A

Between “add” and “max hot”

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33
Q

When to check oil level

A

w/in 30 min of engine shutdown, 15-20 min most accurate

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34
Q

White numbers on voltmeter

A

22.0-29.5 VDC

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35
Q

Np limit with counter weights

A

106%

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36
Q

Vo

A

227 KIAS 150 KIAS rudder

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37
Q

Vo definition

A

operating maneuvering speed is speed above which full deflection or abrupt movement in 1 axis will exceed structural limits

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38
Q

0 G limit

A

5 Sec +/-.25 is considered 0 G

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39
Q

Neg G limit

A

60 sec

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40
Q

Defog limits for t/o or ldg

A

do not use

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41
Q

max decent rate when mains 185 +/-5 psi

A

3.7 Gs 600 FPM

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42
Q

max decent rate when mains 225 +/- 5 psi

A

5.1 Gs 780 FPM

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43
Q

Barrier limits

A

-taxi as slow as possible so all gear avoids contact with support doughnuts
-avoid taxi over net barriers if possible
-do not engage raised web barrier

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44
Q

Icing maneuver limits

A

30* AOB 0-2 Gs

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45
Q

Hydro limits on gauge

A

Green 2880-3120
white 1800-2880 or 3120-3500

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46
Q

Best glide speed VVI clean

A

125 KIAS 1350-1500 FPM

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47
Q

Best glide speed VVI Dirty

A

120 KIAS 1500 FPM

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48
Q

Best glide speed VVI Dirty flaps LDG

A

95 KIAS 1850 FPM

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49
Q

Best glide speed VVI prop windmilling clean

A

110 KIAS 2350 FPM

50
Q

When does stick shaker activate?

A

Min 5 Kts below stall or 5-10

51
Q

When does buffet occur?

A

3 Knots before, turning buffet occurs much before stall

52
Q

Roll of tendency >60% Torque

A

Torque roll off often occurs before reaching aft stick

53
Q

Configuration effect on stall

A

-Flaps aggravate roll of tendency
-Speed brake and fuel imbalance negligible effect

54
Q

Parts of a Spin

A

Post stall gyration
Incipient Spin
Steady State Spin

55
Q

OCF Definition

A

Aircraft does not respond immediately and in a normal sense of flight controlls.

56
Q

Post Stall Gyration

A

Motions of acft about 1 or more axis immediately following the stall but prior to incipient spin

57
Q

Spiral definition

A

Rolling and/or yawing motion of acft, but not steady state as A/S increasing thru 160 KIAS

58
Q

Why no spins below 10,000 msl

A

high stress on propeller during the spin on the prop rpm below 80%

59
Q

Erect spin AOA
Airspeed
Time
Alt Loss

A

AOA= 18 Units
Airspeed 120-135 KIAS
2-3 Sec per turn
400-500’ lost per turn

60
Q

Alt lost during efect spin recovery

A

1500-2000’

61
Q

RCR Numbers

A

Dry=23
Wet=12
Icy=5

62
Q

Max braking speed def

A

Max speed which acft can come to a stop without exceeding energy limits of brakes

63
Q

Brake energy limit

A

3.96 Mil ft/lbs

64
Q

Assumptions of abort speed

A

3 seconds to recognize, 3 seconds to move throttle to idle and brakes.
Speed may increase 20 Knots

65
Q

Max Range vs Max Endure

A

Max Range: speed that gives max range per lb of fuel
Max Endure: speed for min fuel flow in level flight

66
Q

Long Range Cruise Definition

A

Speed above max range speed which yields 99% of max range

67
Q

Landing Distance Assumptions

A
  1. 3* approach to 50 ft obstacle
  2. 2 sec delay from touchdown to braking
  3. max braking once firmly on ground
  4. idle power and threshold speed determined by chart at 50’
  5. braking for dry asphalt/concrete 23 RCR
68
Q

Taxi Spacing restrictions

A

maintain min of 75 feet while staggered 150 ft in line
300 ft icy

69
Q

When do you have to wear g suit

A

when anticipating 2 or more Gs

70
Q

When to wear helmet visor

A

Anytime the canopy is down

71
Q

When to wear gloves

A

Engine start to engine shutdown
should be worn during exterior inspection

72
Q

Joker Definition

A

Fuel qty above bingo which separations, bug out, or event termination should begin and proceed w/ remainder of mission

73
Q

Bingo Definition

A

Fuel qty that allows acft to return to base of intended landing or alternate using preplanned recovery fuel

74
Q

Normal recovery

A

fuel at initial or FAF, 200 lbs

75
Q

When to declare min/emer fuel

A

once it becomes apparent fuel remain at touchdown will be less

76
Q

When to use ldg flaps

A

full stop landings when hvy weight flaps up LDG dist >= 80% of actual field length

77
Q

Low approach definition

A

do not allow acft to touch down when cleared low approach

78
Q

restricted low approach definition

A

do not descend below 500 AGL or alt given by controller

79
Q

WX clearance during OCF

A

Clear of clouds w/ horizion min 7000’ above
must complete recovery by 3,000’ above

80
Q

Min Altitude aero

A

6000’ AGL

81
Q

Min Altitude OCF

A

13,500’ MSL

82
Q

MEA for students

A

5000’ AGL

83
Q

Min non local VFR point to point

A

3000’ AGL

84
Q

Min altitude to complete slip for training

A

300’ AGL

85
Q

Dual only Maneuvers

A
  • Rolling T/O
  • Stalls
  • Slow Flight
  • Stability Demo
  • Contact Recoveries
  • Intentional Spins
  • Straight in approaches
  • low-closed patterns
  • UA Operations
86
Q

When to accomplish GPS approach

A

Day VMC

87
Q

GPS database limits

A

Do not use GPS as prime nav source w/expired database

88
Q

FDE rules for GPS

A

Aircrew will check FDE before using GPS as a primary source of IFR navigation

89
Q

RNAV SID/STAR Rules

A

Do not fly SID/STAR with RNAV in title

90
Q

NTA Max acft in pattern

A

4 total

91
Q

NTA Overhead vs rectangular

A

Do not fly overhead w/ civilian traffic in pattern

92
Q

NTA Max airspeed

A

200 KIAS within 3 NM 1500 AGL

93
Q

High Surface Wind restriction

A

-no overland flight exceeding 35 kts
-OG/CC approval for surface winds exceed 25 Kts

94
Q

Solo flying recommendations for engine malfunction

A

fly PEL

95
Q

Solo flying recommendations for engine failure

A

serious consideration should be given to ejection

96
Q

Tire Wear Criteria

A

Red Cord= do not accept
3 cord for out and back
2 cord for cross country

97
Q

When to install ejection pin

A

Clear of runway prior to turning on parallel taxiway

98
Q

Contact MOAs

A

1,2,6,7,9,10

99
Q

Instrument MOAS

A

3,4,5,9,10

100
Q

Formation MOAs

A

3,4,5,Pecos,8 High/Low,Burr,9,10 h/l

101
Q

Pattern priorities

A
  1. Emergencies
  2. Min Fuel
  3. Formation
  4. Radar Entry
  5. Established in Pattern
  6. VFR Entries
102
Q

Pattern Comm Priorities

A
  1. SOF/Deconfliction/Emergency
  2. Clearances/ Cancellation/ Acknowledgements
  3. Gear Down Calls
  4. Position Reports
  5. Requests
103
Q

When to not break

A
  1. Traffic on high/closed, low closed, inside downwind
  2. Acft on straight in btwn 5NM and 2NM
  3. Acft between high and low key
  4. Acft orbiting high key
104
Q

When no to request closed

A
  1. Traffic between 2 mile and break
  2. acft between 5NM and 2NM on straight in
  3. Between initial and halfway between high and low key
105
Q

MOA altitudes based on altimeter settings

A

28.92-29.41 high cap 21,000’
29.42-29.91 high cap 21,500’

106
Q

Expected MOA recovery altitude
High
Low

A

14,000
6,000

107
Q

Taxi Right of way
1. Exit rwy vs. Taxi G
2. Taxi G vs. Parking Ramp

A
  1. Taxi G
  2. Parking Ramp
108
Q

Number of Aircraft allowed on Taxi A

A

No more than 6 T-38 or combination if 4 T-6/1 holding between the runways

109
Q

What to do if unable VMC MOA?

A

Advise ATC when unable to 3SM and clear of clouds. Standard IFR separation will be provided until pilot advises 3SM and clear of clouds

110
Q

Reduced Same Runway Separation

A

3000’ alternate sides of the runway

111
Q

When does Reduced Same Runway Separation not apply?

A
  1. Between trainer and non-trainer aircraft
  2. Situation cleared for option
  3. Between departure following arrival acft
  4. Wet runway
  5. SOF determines safety is jeopardized
112
Q

Unrestricted Patterns

A

Full use of MOA+HONCHO, crosswinds in solo limits. HONCHO controls

113
Q

Solo Patterns

A

3100 MSL/5 SM Crosswind in limits

114
Q

Dual status

A

3100’ MSL/ 3SM

115
Q

Restricted Patterns Wx and entry

A

2600 MSL/3SM
Enter via init T/O, pattern straight in, closed/crosswind from center

116
Q

Simultaneous Instruments WX

A

2100/3

117
Q

Alternating Instrument WX

A

WX >= suitable IAP mins

118
Q

Wx Recall

A

Discontinue profile
Max endure top of the block
Await sequencing
Fly 250 KIAS

119
Q

OG recall

A

Same as Wx recall except fly normal speeds

120
Q

Insufficient Radar Separation
Dual or better

A
  1. Climb 2600’ turn west
  2. Contact RSU
  3. Do not cross pattern ground tracks until 2600’
  4. Enter VFR entry
121
Q

Insufficient Radar Separation
Restricted Patterns

A
  1. Maintain 2100’ turn corner outside down/crosswind
  2. Contact RSU
  3. Enter pattern, west 360 to avoid traffic
122
Q

Controlled Ejection
Steps/location

A
  1. Ref controlled ejection
  2. 7700
  3. DLF 043/4DME 3100’
  4. Eject using controlled ejection

Checkride (2 decks)

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