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EFSIXTEEN > TR Flash Cards > Flashcards

TR Flash Cards

1
Q

Engine Warning Light

A 
RPM sub Idle (<55%)
Overtemp, Flameout, Stagnation
2 Seconds after FTIT exceeds 1000˚ C
Alternator Failure
May occur if RPM or FTIT indicators fail
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2
Q

SEC Operation

A

Unrestricted throttle movement between 15k-40k ft when subsonic
80-100% MIL thrust

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3
Q

Fire and Overheat Loops

A

Fire: Engine compartment
Overheat: Engine compartment, MLG wheel wells, ECS bay, EPU bay (EWEE)
Overheat loop happens 100˚ below fire loops

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4
Q

Fuel system (C model)

A 
Internal wing: 550 +/- 100
Forward: 3150 +/- 100
Aft: 2810 +/- 100
Reservoir: 480 +/- 30
Centerline: 1890 +/- 100
Wing Tank: 2420 +/- 100
Fuel Low Caution: Fwd res <400, Aft res <250
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5
Q

FLCS: Power Sources

A

FLCS PMG, MAIN GEN, STBY GEN, EPU GEN, EPU PMG, Batt, FLCS batteries

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6
Q

FLCS: AoA/g limiter

A

G-based until 15.8 AoA, blended AoA & G 15.8-25.8 AoA

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7
Q

FLCS: Roll Rate Limiter

A

Prevents roll-coupled departures by limiting roll rate

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8
Q

FLCS: Yaw axis limiter

A

Overrides rudder inputs above 26˚AoA

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9
Q

FLCS: Yaw rate limiter

A

Provides anti-spin controls at >35 AoA and < -5 AoA

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10
Q

FLCS: Gains

A

Cruise Gains, T/O & Lnd Gains, STBY Gains

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11
Q

Hydraulics: System A

A

Flight Controls
Speed Brakes
FFP (Fuel Flow Proportioner)

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12
Q

Hydraulics: System B

A 
Flight Controls
Gun
Gun Purge Door
AR Door
LG
Brakes
NWS
JFS accumulator
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13
Q

Hydraulics: HYD/OIL Light

A

A or B Hydraulic <1000 psi
Oil PX < 10 psi for >30 seconds

Goes out above 1000 psi HYD and 20 psi OIL

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14
Q

EPU: When does it come on

A

Dual GEN Failure and Dual Hydraulic Failure (with WOW)

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15
Q

EPU: What does it back up

A

System A Hydraulics

Emergency AC & DC buses

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16
Q

EPU: How do you avoid using Hydrazine

A

Set 75-80% RPM minimum

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17
Q

EPU: Hydrazine limit

A

10 min run time when operating only on Hydrazine.

Assuming normal flight control movement

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18
Q

Landing Gear:

A

B System
NLG extended and retracted with HYD PX
MLG extended by free-fall, retracted with HYD PX
Alt. Gear (NLG) is pneumatic PX bottle

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19
Q

Landing Gear: Warning light/horn

A

All gear not down and locked when…
<190 knots
<10K’
>250 fpm VVI

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20
Q

Brakes: A or B HYD system

A

B

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21
Q

Brakes: How long do you have Accumulator braking

A

75 seconds

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22
Q

Brakes: When does CH 1 braking work

A

Only when LDG gear handle is down

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23
Q

Brakes: When does CH 2 work

A

LDG gear handle up or down

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24
Q

Brakes: When does Anti-skid light come on and what does it mean

A

Above 5 knots

Braking effectiveness is reduced by 25-50%

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25
Q

Brakes: What does Anti-skid light flashing mean?

A

Total electrical failure of at least one brake

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26
Q

What are the speed brake limits

A

60˚ full

43˚ with RMLG down and locked

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27
Q

Describe lights at startup

A

Batt on, 2, 1, 0
Power test, 4, 1, 3, 0 (adds FLCS PMG and FLCS channels)
Main Power, 2, 1, 0

Eyebrow: HYD/OIL, ENGINE
Caution: SEC, ELEC SYS, FLT CONT SYS

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28
Q

How long do you motor the JFS

A

1 minute

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29
Q

What are the JFS limitations

A

Run for 4 minutes
Cool for 5
1 minute in between start attempts

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30
Q

What does a flashing JFS run light mean?

A 
1/sec = non-critical failure, continue
2/sec = critical failure, don’t continue
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31
Q

When is the JFS recharged

A

40-60 seconds after 12% RPM

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32
Q

When does HYD and Fuel PX increase

A

15% RPM

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33
Q

When does the SEC light go out?

A

18%

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34
Q

When should engine light off occur

A

20 seconds after IDLE

RPM leads FTIT

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35
Q

When does the HYD/OIL light go out?

A

Not before 25% RPM

36
Q

When does the FLCS PMG light turn off?

A

40% RPM

37
Q

When the does the JFS turn off?

A

50% RPM

38
Q

When do the STBY GEN & ENGINE lights go off?

A

55% RPM

39
Q

What do you check when the STBY GEN comes online

A

SEAT NOT ARMED & 3 Green gear lights

40
Q

What does failure of the EPU check indicate?

A

Failure of the bleed valve, which could over speed the EPU in flight.

41
Q

Fuel: What are the tolerances between individual tanks and the totalizer?

A

+/- 300 internal, 300 external, 600 internal and external

42
Q

Describe the anti-ice test?

A

IDLE with switch on for 1 minute
Turn off switch
FTIT should decease 10˚ within 15 seconds
If not, abort jet

43
Q

What are the altimeter tolerances

A

With 75’ of known elevation and each other between ELECT and PNEU (270 in the air)
HUD Alt and Steam Alt within 75’

44
Q

Describe Takeoff parameters

A

5-15 seconds for RPM and FTIT to stabilize
MIL: nozzle 30% or less
Oil PX increases at least 15 psi
AB: nozzle opens within 5 seconds of selecting AB
NWS: off when rudder is effective (70 knots)

45
Q

What is the A/S for an 11˚ AoA approach?

A

C Model: 142 + 4/1000#

D Model: 134 + 4/1000#

46
Q

Describe an oil scavenge

A

75-78% RPM for 5-10 seconds
IDLE for 1-2 seconds
OFF

47
Q

Tire limitations

A

225 kts for MLG

217 kts for NLG

48
Q

Negative G flight limitations

A

AB: 10 secs
Mil: 30 secs
Max Fuel Flow is 25,000 pph with one empty reservoir

49
Q

JFS in flight limitations

A

<400 KIAS
<20,000 ft
3 min max run time if engine operating above 60%, otherwise unlimited

50
Q

Cable limits

A

150 Normal

160 Emergency

51
Q

Canopy Limit

A

70 kts

Above 30 kts open canopy only as far as required

52
Q

LDG Gear limits

A

300kts/0.65M

4g symmetric, 2g asymmetric, 2g while extending/retracting

53
Q

AR door limits

A 
Opening/closing = 400/0.85 Mach
Opened = 400/0.95 Mach
54
Q

Severe turbulence A/S

A

500kts

55
Q

T-Storm penetration A/S

A

300kts or optimum cruise, whichever is lower

56
Q

Max A/S

A

800 kts <30,000’ MSL

2.05 Mach >30K

57
Q

What is holding A/S

A

Max endurance

58
Q

What is penetration A/S?

A

300 kts
70% min RPM
Speed brakes as required

59
Q

What is a hot start?

A

FTIT over 680˚

If FTIT is over 500, motor JFS until below 200˚

60
Q

Personal Go/No-Go on Takeoff

A

<100kts abort for anything
100kts to T/O = AWOS (AB fail, WARN, overheat, SEC)
T/O to Gear in the well = HEFE (HYD/OIL, Engine Fail, Engine Fire, ENGINE)
Above 100, take tire failure airborne
Above 120, hot brakes

61
Q

AB malfunction

A

Loss of thrust
Nozzle closing
AB failure to light within 5 seconds
Stalls accompanied by loud bangs

62
Q

FTIT limit for operating in SEC with a nozzle stuck open or missing?

A

If operating >850˚, engine can fail in 5 minutes

63
Q

What do you do if you lose your canopy?

A

180 kts Max
Lower your seat
Extend ALT flaps
Duck behind glareshield

64
Q

What do you do if you experience a low altitude engine failure?

A

> 350kts, 3G pull to 30˚, lead level off by 50kts
< 350kts and >2000’ AGL, use a constant altitude deceleration

< 5000’ AGL, may not have time to restart engine

65
Q

What are your initial actions for an oil system malfunction?

A

Max AB
Jett Stores
EPU on
Set throttle @ 80%

66
Q

What do you do if you get a SEC light above 40K’?

A

Minimize throttle movements

67
Q

What do you do if you get a SEC light @ 1.05 MACH

A

Don’t retard throttle from MIL until below the MACH

68
Q

SEC light below 15K’ and below 70% RPM

A

Slowly advance throttle to >70%

69
Q

Airstart parameters: Spooldown

A

250 in PRI
275 in SEC

Need 12% RPM for ignition and fuel flow

70
Q

Airstart Parameters: JFS Assisted

A

<400KIAS & <20K’

170 in PRI
200 in SEC

+5kts/1000#

71
Q

Overhead SFO Altitudes

A

High Key: 7K’ AGL + 500/1000#
Low Key: 3K’ AGL + 250/1000#
Base Key: 2K’ AGL

72
Q

Overhead SFO A/S

A

200kts + 5/1000# Gear Up
190kts + 5/1000# Gear Down
180kts + 5/1000# Minimum

73
Q

Overhead SFO Bank Angle and Dive Angle

A

55˚ gear down
50˚ gear up

10˚ Straight
15˚ In Turn

74
Q

SFO Low Key point

A

Abeam rollout point, 3/4 NM from planned touchdown.

75
Q

Minimum SFO EPU fuel

A

25% (20% JFS assisted)

76
Q

Straight-In SFO: When do you lower the gear

A

Aim point is 11˚- 17˚ NL

77
Q

Straight-In SFO: Minimum Weather

A

3000’ AGL

3nm vis

78
Q

Straight in SFO: Altitudes and Distances

A

7000’ AGL @ 8nm

4000 AGL @ 4nm

79
Q

Straight In SFO: Minimum EPU Fuel

A

45% (40% JFS Assisted)

80
Q

What do you need to fly CAT D mins

A

Straight-In
165 KIA or less on the approach
260 KTAS or less on MAP
No CAT E available

81
Q

Formation penetration restrictions

A

2 Aircraft limit when WX is below overhead minimums

82
Q

Lead change altitude requirements

A

500 AGL over land
1000 AGL over water
1500 AGL at night
1500 AGL in IMC unless on radar downwind.

83
Q

Reserve Fuel requirement

A

10% of flight time up to 45 min max
OR
20 min

(Whichever is greater)

84
Q

VFR WX requirements

A

> /= 1500/3
Class A: N/A
Class B: 3 SM and clear of clouds
Class C&D: 3SM, 1000’ Above, 500’ Below, 2000’ Horizontal
Class E&G: Below 10K’ (Same as C&D)
Class E&G: Above 10K’: 5SM, 1000’ Above, 1000’ Below, 1SM Horiz

85
Q

Minimum climb gradient if not stated.

A

200 ft/NM

86
Q

Minimum altitudes on airways

Minimum altitudes off airways

A

MEA or MOCA

OROCA or ORTCA

1000’ Clearance within 5NM, 2000’ in mountainous terrain.

87
Q

MSA vs ESA

A

MSA: 1000’ clearance within 25nm
ESA: 1000’ clearance within 100nm (2000’ in mountainous)

EFSIXTEEN (5 decks)

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