LIMITS Flashcards

1
Q

If a limit is exceed to where “XXX” is indicated:

A

The crew shall land as soon as practicable.

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2
Q

Except for emergencies, a ___ delay is required between start attempts anytime a start is aborted.

A

60 second

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3
Q

For crossbleed starts the receiving engine shall be at or above ___ prior to advancing the PCL to idle.

A

24% Ng

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4
Q

TGT start limit

A

851 Celsius until idle speed is attained

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5
Q

Engine operation with ____ engaged is prohibited.

A

Gust lock

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6
Q

TGT Limit

EDECU MRP

A
0-810 continuous green
810-851 30 minutes yellow
851-878 10 minutes red (as required for max power and limiter checks only)
878-903 2.5 minutes red
903-949 12 seconds red
949 maximum
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7
Q

Np

A
<96% avoid red
96-105 continuous green (yellow >101)
105-117 20 seconds yellow
117-120 12 seconds yellow
120 maximum red

*during engagement extended operations in the 20-40 and 60-75 ranges may cause engine damage.

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8
Q

Nr

A
<96% avoid red
96-101 continuous green
101-120 precautionary yellow
120 max red 
>120 123% maximum for FCF only red
127 overspeed latch red
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9
Q

Dual engine torque <80kias

A

0-120 continuous green
120-144 10 seconds yellow
144 max red

Dual engine torque applies anytime both engines are above 65% torque

*Engine torques over 150 are displayed as red XXX.

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10
Q

Dual engine torque

>80 kias

A

0-106 continuous green
106-127 10 seconds yellow
127 max red

Dual engine torque applies anytime both engines are above 65% torque

*Engine torques over 150 are displayed as red XXX

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11
Q

Single engine torque

A

0-135 continuous green
135-144 10 seconds yellow
144 max red

*Engine torques over 150 are displayed as red XXX

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12
Q

Ng

A

0-102.2 continuous green
102.2-106 2.5 minutes yellow
106-107 12 seconds red
107 max red

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13
Q

XMSN Temp

A

-50-105 continuous green
105-120 precautionary yellow
120 max red

*prolonged hovering in hot weather 86F (30C) and high gross weight may cause temperatures to rise in the yellow precautionary range. Operation in the precautionary range for less than 30 mins during any one flight under these conditions is acceptable.

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14
Q

XSMN Pressure

A
20psi minimum red
20-30 idle and transient yellow
30-65 (45-60 in lvl flt)continuous green
65-130 precautionary yellow
130 max red
  • during steady state level pitch attitudes (level flight) the xsmn oil pressure should be 45-60psi. The following conditions do not constitute an emergency situation but may be indicative of a degraded lubrication system. Any discrepancy shall be documented on a MAF.
    1: steady pressure outside the 45-60 range but within the normal limits 30-65.
    2: fluctuations not to exceed a range of 10psi within the normal limits of 30-65.

During transient pitch or steady state nose high attitudes (autos, downwind hovering, rearward flight, slope up landings) xsmn oil pressure fluctuations (including momentary fluctuations below 30psi and transient drops below 20psi for up to 1 second) are acceptable. Operating with pressure fluctuations below 30psi shall be limited to 30 minutes.

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15
Q

Engine Oil Temp

A

-50-135 normal green
135-150 30minutes yellow
150 max red

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16
Q

Eng oil press

A
22 min red
22-26 precautionary yellow
26-100 continuous green
100-120 precautionary yellow
120 max red

*normal idle is 22-55psi

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17
Q

Min fuel on landing

A

600 lbs

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18
Q

Engine Start/motor

A
START
             STRTR ENGD      STRTR DISNGD
<16c     First cycle            60s
             Second cycle.      60s
             Third cycle.          60s
             Fourth cycle.        30m
16-52c First cycle.           60s
             Second cycle.      30m

ENGINE MOTOR (IGN OFF)
Any temp
Two minutes. 2min
Two minutes. 5min

  • a start cycle is defined as starter initiation, acceleration and dropout.
  • times for motoring are cumulative within a five minute period.
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19
Q

APU Limitations (not temps)

A
Not intended for routine flight use. Acceptable in flight use includes:
Emergency procedures
Single engine training
Practice autos
Powering ECS during extreme temp ops
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20
Q

Transmission Limitations (think MAFs)

A

The transmission is limited by Nr, torque, xsmn oil pressure and temp.

If xsmn oil pressure or temperature are in the precautionary range the helicopter shall not be scheduled for additional flights until mx action is performed.

21
Q

Rotor engagement/disengagement

A

Max winds are 45kts from any direction

22
Q

Vne

A

180kias

23
Q

Sideward/rearward

A

35kts

24
Q

Autorotation

A

100kias

With FLIR installed failure to maintain balanced flight below 90kts in descents over 1000fpm will result in inaccurate and erratic air speed indications

25
Q

Boost off

A

140 kias

26
Q

Two sas inop in IMC

A

125 kias

27
Q

Either pri servo press caution

A

125 kias

28
Q

Searchlight in fixed other than stowed

A

160kias

29
Q

Searchlight in transition

A

100 kias

30
Q

Dome at or above trail (10’ cable extended, 6’ below aircraft)

Dome below trail

A

70kias
45 aob

70kias
15 aob

Dome 6’ below aircraft 10’ of cable out

31
Q

Cabin door open/close

A

60kias

With cabin door open uncoordinated flight should be avoided.

32
Q

Maneuvering with rescue hoist loads

A

Rate of descent limited to 1000fpm

33
Q

Hovering limits

A

Avoid prolonged rearward flight and downwind hovering to prevent exhaust accum in helicopter and heat damage to an open cabin door.

Pedal turns at a rate in excess of 30degrees/sec

Dipping sonar ops at alts other than 70’
*if at other than 70’ when dome entering/exiting water equipment may be damaged by electrostatic discharge:

Do not tow transducer in the water above 8kgs with array folded and 4kgs unfolded.

  • exceeding 8/4kgs May cause TA cable separation
  • towing is cable contacting the funnel. Airspeed May be higher than 8/4 if not contacting the funnel.
34
Q

AOB limits

A

Normal ops 45 deg

Ops above 10k DA. 30deg

Either pri servo press caution. 30deg

Boost off flight. 30deg

35
Q

Max operating DA

A

13k

36
Q

Prohibited maneuvers

A

Aerobatic flight
*an intentional maneuver involving an abrupt change in a/c attitude, intentionally performed spins, or other maneuvers requiring pitch/dive angles greater than 45deg, bank angles greater than 60deg, or accel greater than 2Gs. A maneuver that conforms to the model NATOPS manual (break, autorotation) is not considered aerobatic flight.

Practice full autorotation landings

Intentional approaches into or inducement of retreating blade stall.

37
Q

Rotor break

A

Max application is 76% Nr

Routine stops between 30-50% Nr at 180psi.

38
Q

Fold/spread limits

A

Max wind is 45kts from any direction for main rotors, stab and tail rotor

10min cooking period between a complete fold and spread evolution.
(Defined as a complete spread followed immediately by a fold or vice versa)

39
Q

Landing limits
Fpm
Speeds
Slopes

A

720 fpm for gross weight <19,500

480 fpm for gross weight >19,500

360 fpm for sloped terrain

Max touchdown speed shall not exceed 75kgs with tailwheel locked and 20kgs with TW unlocked.

Max ground taxi is 40kgs with tail gear shimmy damper and 20kgs without shimmy damper.

Slope landing Limits
6deg nose down
9deg nose up
12deg cross slope
*a low frequency oscillation may occur when landing nose down on a slope with cyclic near aft stop.

Downwind landings should be avoided.

40
Q

Max operating weights

A

23,500lbs total

23,500lbs for aviation ships

22,500lbs for air capable/amphibious assault aviation ships

41
Q

Internal load weight limits

A

300lbs/ft^2

42
Q

Cargo hook and rescue hoist max weight

A

6000lbs cargo hook

600lbs rescue hoist

43
Q

Cg limits

A

7.5 in left and 8.0 in right at max gross weight

44
Q

Min equip for night flight overwater

A

LAWS

Altitude Hold

45
Q

Min equip for flight into known icing

A

Helicopters equipped with operable anti ice and blade deice equip are permitted flight into known forecast or known trace/light icing conditions. All installed equipment (engine/rotor/windshield) shall be operational prior to flight. Helicopters not equipped with operable blade deice equipment are prohibited from flight into forecast or know icing conditions (ambient temp of 5c or below in visible moisture).

*flight into forecast or known moderate/severe icing conditions is prohibited.

46
Q

Advanced helicopter emer egress lighting system

Individual heli emer egr ltg sys

A

Except in emergencies adheels/iheels shall be operational for all overwater flights requiring pax/non aircrew in the cabin.

47
Q

Temperature limits

A
  • 40f to 140f

- 40c to 60c

48
Q

Backup hydraulic pump

*Rotors Static

A

OAT OP TIME. COOLDOWN
33-38c. 24min. 72min

39-60c. 16min. 48min

49
Q

APU op limit

A

To prevent APU overheating, operation at ambient temps above 43c with engine and rotor operating is limited to 30mins.
With engine and rotor not operating APU may be operated continuously up to 51c.