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UH60M Master Subject > 9's - C7 > Flashcards

9's - C7 Flashcards

1
Q

CHIP MAIN MDL SUMP,

CHIP L OR R ACC MDL,

CHIP TAIL XMSN, TAIL XMSN OIL HOT,

CHIP INT XMSN or INT XMSN OIL HOT

Caution Appears

A
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2
Q

Engine Compressor Stall

Indications

A

An engine compressor stall is normally recognized by a noticeable bang or popping noise and possible helicopter yaw. These responses are normally accompanied by the rapid increase in TGT and fluctuations in NG, Q, and NP reading for the affected engine.

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3
Q

CHIP ENG 1 OR 2,

ENG 1 OR 2 OIL PRESS ,

ENG 1 OR 2 OIL HOT

CAUTION APPEARS

A
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4
Q

Main Transmission Failure

⟹ Warning and Note ⟸

A
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5
Q

CHIP L INPUT MDL

or

CHIP R INPUT MDL

A
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6
Q

HYD PUMP 1 FAIL

or

HYD PUMP 2 FAIL

NO BACKUP PUMP

A
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7
Q

CONV 1 FAIL

or

CONV 2 FAIL

Cautions appear

A

No action required ➠

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8
Q

Single Engine Failure

A
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9
Q

LOCKOUT

EP

A
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10
Q

Flight Control / Main-rotor system malfunctions

Warning

A
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11
Q

APU Oil Hot caution appears

A

⟹ BACK ME UP ⟸

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12
Q

FUEL 1 PRESS LOW or FUEL 2 PRESS LOW Caution Appears.

Situation non-critical

A

⟹ BACK ME UP ⟸

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13
Q

Increasing NR

A
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14
Q

Engine Compressor Stall

A
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15
Q

T/R SERVO 1 FAIL Caution Appears

and

BACK UP PUMP ON Advisory Does Not Appear or T/R SERVO 2 ON Advisory Does Not Appear.

A
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16
Q

Smoke and Fume Elimination

A

⟹ BACK ME UP ⟸

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17
Q

Single EGI Failure

Indications

A

⟹ EP is BACK ME UP ⟸

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18
Q

Uncommanded Nose Down/Up Pitch Attitude Change

(2/2) Nose up

A
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19
Q

ROTOR BRAKE ON

Advisory Appears in flight

A
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20
Q

STAB UNLOCKED

Caution Appears

A
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21
Q

AFCS FAIL

Caution Appears

A

⟹ BACK ME UP ⟸

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22
Q

ENG 1 OIL BYPASS

OR

ENG 2 OIL BYPASS

CAUTION APPEARS.

A
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23
Q

Single EGI Failure

A

⟹ BACK ME UP ⟸

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24
Q

Dual EGI Failure

A
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25
Q

STABILATOR MALFUNCTION

AUTO MODE FAILURE

A
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26
Q

Loss of Control at Low Airspeed/Hover or T/R QUAD FAIL Caution Appears

(Left Rotation)

A
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27
Q

FLT DIR FAIL,

FD COUPLE FAIL

Cautions Appear

A
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28
Q

RSVR 2 LOW Caution Appears

A

⟹ BACK ME UP ⟸

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29
Q

SAS OFF

Caution Appears

A

⟹ BACK ME UP ⟸

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30
Q

AVCS Malfunction

A
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31
Q

FUEL 1 PRESS LOW or FUEL 2 PRESS LOW Caution Appears.

Critical situation

A
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32
Q

Ditching

Power on

A

⟹ BACK ME UP ⟸

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33
Q

Loss of Tail Rotor Thrust in Cruise Flight

A
34
Q

Main Transmission Failure

A
35
Q

Electrical Fire In Flight

A

Prior to shutting off all electrical power, the pilot must consider the equipment that is essential to a particular flight environment which will be affected, e.g., flight instruments, flight controls, etc. If a landing cannot be made as soon as possible, the af- fected circuit may be isolated by selectively turning off electrical equipment and/or pulling circuit breakers.

36
Q

Ditching

Power OFF

A
37
Q

EMER ENG SHUTDOWN

A
38
Q

STABILATOR MALFUNCTION

AUTO MODE FAILURE

If automatic control is not regained after first steps of EP

A

⟹ BACK ME UP ⟸

39
Q

APU Compartment Fire

A
40
Q

NP INCREASING/DECREASING (OSCILLATION).

A

BACK ME UP

or

41
Q

Lightning Strike

A
42
Q

Pitch Boost Servo Hardover

A

⟹ BACK ME UP ⟸

43
Q

T/R QUAD FAIL Caution Appears in Cruise Flight.

WARNING

A
44
Q

Pedal Bind/Restriction or Drive With No Accompanying Caution

A
45
Q

GEN 1 FAIL

or

GEN 2 FAIL

Cautions appear

A

⟹ BACK ME UP ⟸

46
Q

MAIN XMSN PRESS Caution Appears/

MAIN XMSN OIL HOT Caution Appears

A
47
Q

Loss of Control at Low Airspeed/Hover or T/R QUAD FAIL Caution Appears

(Left Rotation)

⟹WARNING ⟸

A
48
Q

Dual Engine Failure

A
49
Q

AVCS Malfunction

Indications

A
50
Q

HYD PUMP 1 FAIL and HYD PUMP 2 FAIL

Cautions Appear

A
51
Q

CONV 1 FAIL and CONV 2 FAIL

A

⟹ BACK ME UP ⟸

52
Q

Flight Control / Main-rotor system malfunctions

A
53
Q

RSVR 2 LOW and

HYD PUMP 2 Cautions appear

With BACKUP PUMP ON Advisory

A
54
Q

BOOST SERVO OFF Caution Appears

A
55
Q

LOCKOUT definition

A
56
Q

Integrated Avionics Systems Malfunctions

A
57
Q

Trim Actuator Jammed

A

⟹ BACK ME UP ⟸

LAND AS SOON AS PRACTICABLE

58
Q

Fuel 1 BYPASS

or

Fuel 2 BYPASS

cautions appear

A

⟹ BACK ME UP ⟸

59
Q

STABILATOR MALFUNCTION

AUTO MODE FAILURE

WARNING

A
60
Q

SAS Failure With no Failure/Advisory

A

⟹ BACK ME UP ⟸

Indication: Moderate rotor tip path oscillations

61
Q

GEN 1 FAIL and GEN 2 FAIL

(1 & 2 CONV and AC REF BUS DEGRAD cautions appear)

A

⟹ BACK ME UP? ⟸

only one underline step

62
Q

Loss of Tail Rotor Thrust or T/R QUAD FAIL Caution Appears with Loss of Control at Low Airspeed/Hover

(Right Rotation).

A
63
Q

Engine Hi-speed shaft failure

A
64
Q

Engine Fire In Flight

A
65
Q

Coupled Flight Director Malfunction

A

⟹ BACK ME UP ⟸

66
Q

Decreasing NR

A
67
Q

RSVR 1 LOW and

HYD PUMP 1 Cautions appear

With BACKUP PUMP ON Advisory

A
68
Q

LOCKOUT

Warning and Caution

A
69
Q

HYD PUMP 2 FAIL Caution Appears

A

⟹ BACK ME UP ⟸

70
Q

Collective Boost Servo Hardover/Power Piston Failure

A

Increase in control forces, as much as 150 pounds - can be eliminated by shutting off boost servo.

71
Q

Dual EGI Failure

Indications

A
72
Q

PRI SERVO 1 FAIL

or

PRI SERVO 2 FAIL

Cautions Appear

A
73
Q

FUEL 1 PRESS LOW

and

FUEL 2 PRESS LOW

Cautions Appear

A
74
Q

EMER APU START

A
75
Q

STAB DEGRADED Advisory

A

⟹ BACK ME UP ⟸

The STAB DEGRADED advisory indicates that the stabilator control has reverted to a condition of reduced functionality in either speed or control. Full stabilator range of motion may not be available. Exercise caution when operating at high speed or low power descents which may require the stabilator to go beyond its available range.

76
Q

Engine/Fuselage Fire On Ground

A
77
Q

Fuel 1 BYPASS

and

Fuel 2 BYPASS

cautions appear

A
78
Q

T/R QUAD FAIL Caution Appears in Cruise Flight.

A
79
Q

HYD PUMP 1 FAIL Caution Appears

A

⟹ BACK ME UP ⟸

80
Q

Uncommanded Nose Down/Up Pitch Attitude Change

(1/2) Nose down

A
81
Q

Emergency Landing in Wooded Areas

Power OFF

A
82
Q

Fuel 1 or 2 Low

A

UH60M Master Subject (2 decks)

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