Brainscape's Knowledge GenomeTM

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


See full index

UH-60 A+/L Ch. 5 w/Change 9 > UH-60 Ch. 5 EPs Change 9 > Flashcards

UH-60 Ch. 5 EPs Change 9 Flashcards

Memorization of EPs

1
Q

Maximum wind

velocity for rotor start or stop from any direction.

A

45 knots

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

MAIN TRANSMISSION MODULE LIMITATIONS
Oil pressure should remain steady and should be in the__ to__ psi range for the UH-60A, and__ to__ psi range for the UH-60L, to ensure that when fluctuations occur, they remain in the acceptable range. If oil pressure is not steady during steady state forward flight or in a level hover or if oil pressure is steady but under __ psi, make an entry on DA Form 2408-13-1. Sudden pressure drops (more than. ___ psi) without fluctuations require an entry on DA Form 2408-13-1.

A

MAIN TRANSMISSION MODULE LIMITATIONS
Oil pressure should remain steady and should be in the 45 to 55 psi range for the UH60A, and 45 to 60 psi range for the UH-60L, to ensure that when fluctuations occur, they remain in the acceptable range. If oil pressure is not steady during steady state forward flight or in a level hover or if oil pressure is steady but under 45 psi, make an entry on DA Form 2408-13-1. Sudden pressure drops (more than. 10 psi) without fluctuations require an entry on DA Form 2408-13-1.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q 
Engine % RPM 1-2 (Np)
\_\_ Sec. Transient\_\_\_\_\_\_\_\_\_\_
Transient\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_
Continuous\_\_\_\_\_\_\_\_\_\_\_\_\_\_
Transient\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_
Avoid Operations in the \_\_ - \_\_ and \_\_ - \_\_ 
range except during start and shutdown.
A 
Engine % RPM 1-2 (Np)
12 Sec. Transient: 105% - 107%
Transient: 101% - 105%
Continuous: 95% - 101%
Transient:  91% - 95%
Avoid Operations in the 20% - 40% and 60 - 90% 
range except during start and shutdown.
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

Engine Ng
__ Sec. Transient_________
__ Min Limit_____________
Continuous_____________

A

Engine Ng
12 Sec. Transient: 102% - 105%
30 Min Limit: 99% - 102%
Continuous: 05 - 99%

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

Engine Oil Temperature (A+/L)
__ Min Limit____________
Continuous____________

A

Engine Oil Temperature (A+/L)
30 Min Limit: 135°C − 150°C
Continuous: -50°C - 135°C

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q 
Turbine Gas Temperature
\_\_ Sec. Transient\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_
\_\_ Min. Limit (Contingency Power)\_\_\_\_\_\_\_\_\_\_
Start Abort Limit \_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_
\_\_ Min Limit \_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_
\_\_ Min Limit \_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_
Normal \_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_
A 
Turbine Gas Temperature
12 Sec Transient: 903°C - 949°C
2.5 Min Limit (Contingency Power): 878°C - 903°C
Start Abort Limit: 851°C
10-Min Limit: 851°C - 878°C
30-Min Limit: 810°C - 851°C
Normal: 0 - 810°C
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

Transmission Oil Temp (A+)
Precautionary__________
Continuous____________

A

Transmission Oil Temp (A+)
Precautionary: 105°C - 120°C
Continuous: -50°C - 105°C

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

Transmission Oil Temp (L)
Precautionary__________
Continuous____________

A

Transmission Oil Temp (L)
Precautionary: 105°C - 140°C
Continuous: -50°C - 105°C

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

Transmission Oil Pressure (A+/L)
Precautionary__________
Continuous____________
Idle and Transient_______

A

Transmission Oil Pressure (A+/L)
Precautionary: 60 - 130 PSI
Continuous: 30 - 60 PSI
Idle and Transient: 20 - 30 PSI

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q 
Main Rotor % RPM R
         Power On
Transient\_\_\_\_\_\_\_\_\_\_\_\_\_
Continuous\_\_\_\_\_\_\_\_\_\_\_
Transient\_\_\_\_\_\_\_\_\_\_\_\_\_

Power Off (Autorotation)
Maximum_____________
Transient_____________
Normal_______________

A 
Main Rotor % RPM R
         Power On
Transient: 101% - 107%
Continuous: 95% - 101%
Transient: 91% - 95%

Power Off (Autorotation)
Maximum: 110%
Transient: 105% - 110%
Normal: 90% - 105%

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

Fuel Quantity
Normal_____________
Precautionary________

A

Fuel Quantity
Normal: 200 - 1500 lbs
Precautionary: 0 - 200 lbs

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q 
Engine Oil Pressure (A+/L)
\_\_ Min. Limit\_\_\_\_\_\_\_\_\_\_\_\_
Normal Operation\_\_\_\_\_\_\_\_
Idle\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_
*\_\_\_ PSI minimum @ 90% Ng and above
A 
Engine Oil Pressure (A+/L)
5 Min. Limit: 100 - 120 PSI
Normal Operation: 26 - 100 PSI
Idle: 22 - 26 PSI
*35 PSI minimum @ 90% Ng and above
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q 
Engine % Torque (A+)
         \_\_ - Sec Transient
Dual- Engine\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_
Single- Engine\_\_\_\_\_\_\_\_\_\_\_\_\_
          Continuous 
Single-Engine Only\_\_\_\_\_\_\_\_\_\_
Dual-Engine\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_
A 
Engine % Torque (A+)
         10 - Sec Transient
Single- Engine: 110% - 135% 
Dual- Engine: 100% - 125%
          Continuous 
Single-Engine Only: 0 - 110%
Dual-Engine: 0 - 100%
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q 
Engine % Torque (L)
        \_\_-Sec Transient
Dual-Engine
Above \_\_ KIAS\_\_\_\_\_\_\_\_\_\_\_\_\_
\_\_\_ KIAS and below\_\_\_\_\_\_\_\_\_
Single-Engine\_\_\_\_\_\_\_\_\_\_\_\_\_\_
             Continuous
Dual-Engine
Above \_\_ KIAS\_\_\_\_\_\_\_\_\_\_\_\_\_
\_\_ KIAS and below\_\_\_\_\_\_\_\_\_\_
Single-Engine\_\_\_\_\_\_\_\_\_\_\_\_\_\_
A 
Engine % Torque (L)
        10-Sec Transient
Dual-Engine
Above 80 KIAS: 100% - 144%
80 KIAS and below: 120% - 144%
Single-Engine: 135% - 144%
             Continuous
Dual-Engine
Above 80 KIAS: 0 - 100%
80 KIAS and below: 0 - 120%
Single-Engine: 0 - 135%
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

Engine Starter Limits
At ambient temperatures of __°C and below,
__ consecutive start cycles may be made, followed by a __-minute rest period, followed by two additional consecutive start cycles. A __-minute rest period is then required before any additional starts. At ambient temperatures above __ up to __°C, __ consecutive start cycles may be made. A __-minute rest period is then required before any additional start cycles.

A

At ambient temperatures of 15°C and below, two consecutive start cycles may be made, followed by a
3-minute rest period, followed by two additional
consecutive start cycles. A 30-minute rest period is then required before any additional starts. At ambient temperatures above 15° up to 52°C, two consecutive start cycles may be made. A 30-minute rest period is then required before any additional start cycles.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

Pneumatic Source Inlet Limits
The minimum ground-air source (pneumatic) required
to start the helicopter engines is __ psig and __ ppm at
___°C. The maximum ground-air source to be applied
to the helicopter is __ psig at ___°C

A

Pneumatic Source Inlet Limits
The minimum ground-air source (pneumatic) required
to start the helicopter engines is 40 psig and 30 ppm at
149°C (300°F). The maximum ground-air source to be appliedto the helicopter is 50 psig at 249°C

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

ENGINE OVERSPEED CHECK LIMITATIONS.
Engine overspeed check in flight is _________. Engine
overspeed checks, on the ground, are authorized ___________________________ only.

A

ENGINE OVERSPEED CHECK LIMITATIONS.
Engine overspeed check in flight is prohibited. Engine
overspeed checks, on the ground, are authorized by
designated maintenance personnel only.

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

ENGINE START LIMITS
Crossbleed starts shall not be attempted unless the ______________ or ________________ advisory does not appear, and operating engine must be at __% Ng SPEED or above and rotor speed at ___% RPM R.

A

ENGINE START LIMITS
Crossbleed starts shall not be attempted unless the #1
ENG ANTI-ICE ON or #2 ENG ANTI-ICE ON advisory does not appear, and operating engine must be at 90% Ng SPEED or above and rotor speed at 100% RPM R.

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

STOWAGE PROVISIONS.
Maximum capacity for each storage compartment is
___ pounds.

A

STOWAGE PROVISIONS.
Maximum capacity for each storage compartment is
125 pounds.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
20
Q

CARGO HOOK WEIGHT LIMITATION
UH-60A cargo hook: _____ lbs
UH-60L cargo hook: _____ lbs

A

CARGO HOOK WEIGHT LIMITATION
UH-60A cargo hook: 8,000 lbs
UH-60L cargo hook: 9,000 lbs

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
21
Q

WEIGHT LIMITATIONS
Maximum weight is further limited by cargo floor
maximum capacity of ___ pounds per square foot.

A

WEIGHT LIMITATIONS
Maximum weight is further limited by cargo floor
maximum capacity of 300 pounds per square foot.

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

WEIGHT LIMITATIONS
Ground operations with seven-lug wheels are limited
to gross weights less than ______ pounds.

A

WEIGHT LIMITATIONS
Ground operations with seven-lug wheels are limited
to gross weights less than 20,500 pounds.

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

RESCUE HOIST WEIGHT LIMITATIONS.
The maximum weight that may be suspended from the
rescue hoist is ___ pounds.

A

RESCUE HOIST WEIGHT LIMITATIONS.
The maximum weight that may be suspended from the
rescue hoist is 600 pounds.

24
Q

AIRSPEED OPERATING LIMITS.
Maximum airspeed for one engine inoperative is ___
KIAS.

A

AIRSPEED OPERATING LIMITS.
Maximum airspeed for one engine inoperative is 130
KIAS.

25
Q

AIRSPEED OPERATING LIMITS.
Maximum airspeed for autorotation at a gross weight
of 16,825 pounds or less is ____ KIAS.

Maximum airspeed for autorotation at a gross weight
of greater than 16,825 pounds is ____ KIAS.

A

AIRSPEED OPERATING LIMITS.
Maximum airspeed for autorotation at a gross weight
of 16,825 pounds or less is 150 KIAS.

Maximum airspeed for autorotation at a gross weight
of greater than 16,825 pounds is 130 KIAS.

26
Q

AIRSPEED OPERATING LIMITS.

Sideward/rearward flight into the wind, when combined with windspeed, shall not exceed __ knots.

A

AIRSPEED OPERATING LIMITS.

Sideward/rearward flight into the wind, when combined with windspeed, shall not exceed 45 knots.

27
Q

SAS inoperative airspeed limits

(1) One SAS inoperative - ___ KIAS.
(2) Two SAS inoperative - ___ KIAS.
(3) Two SAS inoperative in IMC - ___ KIAS.

A

SAS inoperative airspeed limits

(1) One SAS inoperative - 170 KIAS.
(2) Two SAS inoperative - 150 KIAS.
(3) Two SAS inoperative in IMC - 140 KIAS.

28
Q

Hydraulic system inoperative limits
(1) One hydraulic system inoperative - ___ KIAS.
(2) Two hydraulic systems inoperative - ___ KIAS.
(3) Two hydraulic systems inoperative in IMC - ___
KIAS.

A

Hydraulic system inoperative limits
(1) One hydraulic system inoperative - 170 KIAS.
(2) Two hydraulic systems inoperative - 150 KIAS.
(3) Two hydraulic systems inoperative in IMC - 140
KIAS.

29
Q

Maximum Airspeed for: Extending KIAS Extended KIAS
Landing Light ___ KIAS ___ KIAS
Search Light ___ KIAS ___ KIAS

A

Maximum Airspeed for: Extending KIAS Extended KIAS
Landing Light 130 KIAS 180 KIAS
Search Light 100 KIAS 180 KIAS

30
Q

FLIGHT WITH CABIN DOOR(S)/WINDOW(S) OPEN.
(1) Cabin doors may be fully open up to ___ KIAS with soundproofing installed aft of station 379.
(2) Cabin doors may be fully open up to ___ KIAS with soundproofing removed aft of station 379 or with
soundproofing secured properly.

A

FLIGHT WITH CABIN DOOR(S)/WINDOW(S) OPEN.
(1) Cabin doors may be fully open up to 100 KIAS with soundproofing installed aft of station 379.
(2) Cabin doors may be fully open up to 145 KIAS with soundproofing removed aft of station 379 or with
soundproofing secured properly.

31
Q

FLIGHT WITH CABIN DOOR(S)/WINDOW(S) OPEN.
Gunner’s or BAM window(s) may be fully open up
to ___ KIAS.

A

FLIGHT WITH CABIN DOOR(S)/WINDOW(S) OPEN.
Gunner’s or BAM window(s) may be fully open up
to 170 KIAS.

32
Q

FLIGHT WITH CABIN DOOR(S)/WINDOW(S) OPEN.
Cockpit doors sliding windows will not be ______ or
______ during flight except during hover.

A

FLIGHT WITH CABIN DOOR(S)/WINDOW(S) OPEN.
Cockpit doors sliding windows will not be opened or
closed during flight except during hover.

33
Q

FLIGHT WITH CABIN DOOR(S)/WINDOW(S) OPEN.

Flight with cockpit door(s) removed is _________.

A

FLIGHT WITH CABIN DOOR(S)/WINDOW(S) OPEN.

Flight with cockpit door(s) removed is prohibited.

34
Q

AIRSPEED LIMITATIONS FOLLOWING FAILURE OF THE AUTOMATIC STABILATOR CONTROL SYSTEM.
Manual control available:
The stabilator shall be set full down at speeds __ KIAS and below.
The stabilator shall be set at 0° at speeds above __ KIAS.
Autorotation airspeed shall be limited to ___ KIAS at all gross weights.

A

AIRSPEED LIMITATIONS FOLLOWING FAILURE OF THE AUTOMATIC STABILATOR CONTROL SYSTEM.
Manual control available:
The stabilator shall be set full down at speeds 40 KIAS and below.
The stabilator shall be set at 0° at speeds above 40 KIAS.
Autorotation airspeed shall be limited to 120 KIAS at all gross weights.

35
Q

AIRSPEED LIMITATIONS FOLLOWING FAILURE OF THE AUTOMATIC STABILATOR CONTROL SYSTEM.
Manual control NOT available.
The placard airspeed limits shall be observed as not-to-exceed speed (powered flight and autorotation), except in no case shall the autorotation limit exceed ___ KIAS.

A

AIRSPEED LIMITATIONS FOLLOWING FAILURE OF THE AUTOMATIC STABILATOR CONTROL SYSTEM.
Manual control NOT available.
The placard airspeed limits shall be observed as not-to-exceed speed (powered flight and autorotation), except in no case shall the autorotation limit exceed 120 KIAS.

36
Q

PROHIBITED MANEUVERS
Hovering turns greater than __° per second are
prohibited. Intentional maneuvers beyond attitudes of
____° in pitch or over ___° in roll are prohibited.

A

PROHIBITED MANEUVERS
Hovering turns greater than 30° per second are
prohibited. Intentional maneuvers beyond attitudes of
+/-30° in pitch or over 60° in roll are prohibited.

37
Q

PROHIBITED MANEUVERS

Simultaneous moving of both_____________________ to ____ or ___ (throttle chop) in flight is prohibited.

A

PROHIBITED MANEUVERS

Simultaneous moving of both ENG POWER CONT levers to IDLE or OFF (throttle chop) in flight is prohibited.

38
Q

PROHIBITED MANEUVERS

________ ground taxi is prohibited.

A

PROHIBITED MANEUVERS

Rearward ground taxi is prohibited.

39
Q

RESTRICTED MANEUVERS
Manual Operation of the Stabilator. Manual operation of the stabilator in flight is _________, except as required by formal training and _______________ requirements or as alternate stabilator control in case the AUTO mode malfunctions.

A

RESTRICTED MANEUVERS
Manual Operation of the Stabilator. Manual operation of the stabilator in flight is prohibited, except as required by formal training and maintenance test flight requirements or as alternate stabilator control in case the AUTO mode malfunctions.

40
Q

RESTRICTED MANEUVERS
Prolonged rearward flight and downwind hovering are to be avoided to prevent accumulation of ____________ in the helicopter and __________ to windows ________________.

A

RESTRICTED MANEUVERS
Prolonged rearward flight and downwind hovering are to be avoided to prevent accumulation of exhaust fumes in the helicopter and heat damage to windows on open cargo doors.

41
Q

Maneuvering Limitations

NOTE: Maneuvers entered from a ______________ may result in transient droop of __% RPM R or greater.

A

Maneuvering Limitations

NOTE: Maneuvers entered from a low power setting may result in transient droop of 5% RPM R or greater.

42
Q

Maneuvering Limitations
High-Speed Yaw Maneuver Limitation.
Above __ KIAS avoid ___________________ to prevent excess tail rotor system loading.

A

Maneuvering Limitations
High-Speed Yaw Maneuver Limitation.
Above 80 KIAS avoid abrupt, full pedal inputs to prevent excess tail rotor system loading.
excess tail rotor system loading.

43
Q

Maneuvering Limitations: Sling Loads
Maneuvering limitations with a sling load are limited to a maximum of __° angle of bank in forward flight. Side flight is limited by __________ and is decreased as _____________.
Rearward flight with sling load is limited to __ knots.

A

Maneuvering Limitations: Sling Loads
Maneuvering limitations with a sling load are limited to a maximum of 30° angle of bank in forward flight. Side flight is limited by bank angle and is decreased as airspeed increases.
Rearward flight with sling load is limited to 35 knots.

44
Q

Maneuvering Limitations

Bank Angle Limitation. Bank angles shall be limited to __° when a PRI SERVO PRESS caution appears.

A

Maneuvering Limitations

Bank Angle Limitation. Bank angles shall be limited to 30° when a PRI SERVO PRESS caution appears.

45
Q

LANDING GEAR LIMITATIONS.
Do not exceed a touchdown sink rate (feet per minute) of:
Gross Weight Level Terrain Slopes
Up to 16,825 lbs ___ fpm ___ fpm
Above 16,825 lbs ___ fpm ___ fpm

A

LANDING GEAR LIMITATIONS.
Do not exceed a touchdown sink rate (feet per minute) of:
Gross Weight Level Terrain Slopes
Up to 16,825 lbs 540 fpm 360 fpm
Above 16,825 lbs 300 fpm 180 fpm

46
Q

LANDING SPEED LIMITATIONS.
Maximum forward touchdown speed is limited to __
knots ground speed on level terrain.

A

LANDING SPEED LIMITATIONS.
Maximum forward touchdown speed is limited to 60
knots ground speed on level terrain.

47
Q

SLOPE LANDING LIMITATIONS
__° nose-up, right wheel up or left wheel upslope.
The slope limitations shall be further reduced by __° for
every __ knots of wind

A

SLOPE LANDING LIMITATIONS
15° nose-up, right wheel up or left wheel upslope.
The slope limitations shall be further reduced by 2° for
every 5 knots of wind.

48
Q

SLOPE LANDING LIMITATIONS
__° nose downslope. Landing in downslope conditions
with tail winds greater than __ knots shall not be conducted.

A

SLOPE LANDING LIMITATIONS
6° nose downslope. Landing in downslope conditions
with tail winds greater than 15 knots shall not be conducted.

49
Q

SLOPE LANDING LIMITATIONS
The main gearbox may be operated up to __ minutes
at a time with pressure fluctuations when the helicopter is known to be at a ________________.

A

SLOPE LANDING LIMITATIONS
The main gearbox may be operated up to 30 minutes
at a time with pressure fluctuations when the helicopter is known to be at a nose-up attitude.

50
Q 
ENVIRONMENTAL RESTRICTIONS
Helicopters with the following equipment installed,
operational, and turned on are permitted to fly into \_\_\_\_\_ or \_\_\_\_\_ icing conditions.
(1) \_\_\_\_\_\_\_\_\_\_\_\_\_\_\_.
(2) \_\_\_\_\_\_\_\_\_\_.
(3) \_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_.
(4) \_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_.
(5) \_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_.
A

ENVIRONMENTAL RESTRICTIONS
Helicopters with the following equipment installed,
operational, and turned on are permitted to fly into trace or light icing conditions.
(1) Windshield Anti-ice.
(2) Pitot Heat.
(3) Engine Anti-ice.
(4) Engine Inlet Anti-ice Modulating Valve.
(5) Insulated Ambient Air Sensing Tube.

51
Q

ENVIRONMENTAL RESTRICTIONS
For flight into moderate icing conditions, ________________________________________ must be installed, operational, and turned on.
Flight into heavy orsevere icing is __________.

A

ENVIRONMENTAL RESTRICTIONS
For flight into moderate icing conditions, all equipment in paragraph 5.28 b. and blade deice kit must be installed, operational, and turned on.
Flight into heavy or severe icing is prohibited.

52
Q

BACKUP HYDRAULIC PUMP HOT WEATHER LIMITATIONS with the rotor system ______.
FAT °C Operating Time Cool Down Time
__° - __° _______ _______
__° - __° _______ _______
__° - __° _______ _______

A

BACKUP HYDRAULIC PUMP HOT WEATHER LIMITATIONS with the rotor system static.
FAT °C Operating Time Cool Down Time
-54° - 32° Unlimited –
33° - 38° 24 minutes 72 minutes
39° - 52° 16 minutes 48 minutes

53
Q

APU OPERATING LIMITATIONS.
To prevent APU overheating, APU operation at ambient
temperature of __°C and above with engine and rotor operating is limited to __ minutes. With engine and rotor not operating, the APU may be operated ___________
up to an ambient temperature of __°C.

A

APU OPERATING LIMITATIONS.
To prevent APU overheating, APU operation at ambient
temperature of 43°C and above with engine and rotor operating is limited to 30 minutes. With engine and rotor not operating, the APU may be operated continuously
up to an ambient temperature of 51°C.

54
Q

WINDSHIELD ANTI-ICE LIMITATIONS.
Windshield anti-ice check shall not be done when FAT
is over __°C.

A

WINDSHIELD ANTI-ICE LIMITATIONS.
Windshield anti-ice check shall not be done when FAT
is over 27°C.

55
Q

TURBULENCE AND THUNDERSTORM OPERATION.
Intentional flight into ______ turbulence is prohibited.
Intentional flight into ____________ is prohibited.
Intentional flight into turbulence with a sling load
attached and an inoperative _______________________ is prohibited.

A

TURBULENCE AND THUNDERSTORM OPERATION.
Intentional flight into severe turbulence is prohibited.
Intentional flight into thunderstorms is prohibited.
Intentional flight into turbulence with a sling load
attached and an inoperative collective pitch control friction is prohibited.

56
Q

GUST LOCK LIMITATIONS
(1) Dual-engine operation with gust lock engaged is
__________.
(2) Single-engine operation with gust lock engaged will
be performed by authorized pilot(s) at _____ only.
(3) Gust lock shall not be __________ with engine running.

A

GUST LOCK LIMITATIONS
(1) Dual-engine operation with gust lock engaged is
prohibited.
(2) Single-engine operation with gust lock engaged will
be performed by authorized pilot(s) at IDLE only.
(3) Gust lock shall not be disengaged with engine running.

UH-60 A+/L Ch. 5 w/Change 9 (1 decks)

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