Limitations Flashcards

1
Q

NR Limits

A

. 110 Maximum (>110 red)

106-110 Transient operation (yellow)

     106 High rotor warning annunciated

95-105 Normal operation (green)

  0-94 Transient operation (red)
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2
Q

Engine Oil Pressure (PSI)

A

. 120 Maximum (>120 red w/box)

23-120 Normal operation (green)

     23 Minimum <23 red
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3
Q

Hydraulic Pressure (PSI)

A

. >3410 Transient – permitted for 5 sec(yellow)
(≥5 sec red w/box)

3310-3400 Transient – permitted for 5 min (yellow)
(≥5 min red w/box)

2750-3300 Normal operation (green)

          1260 Minimum (<1260 red w/box)

         2600 Minimum for APU start

          1650 Accumulator Pre-charge
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4
Q

Air Turbine Starter (ATS) Limits

A

NOTE: 60 seconds between cycles.

Engine Starts At Ambient Temperatures of 61° F (16° C) and Below. (2–3–2–30) 
 • 2 consecutive start cycles;
 • 3 minute rest; 
 • 2 consecutive start cycles; 
 • 30 minute rest. 

Engine Starts At Ambient Temperatures
Above 61° F (16° C). (2–30)
• 2 consecutive start cycles;
• 30 minute rest

Dual engine starts — Prohibited.

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5
Q

TGT Limiter

A

Single Engine: 903 ±12 (891-915)° (SEC)

Dual Engine: 879 ±12 (867-891)° (MRP)

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6
Q

ENG Np (%) Digital Readouts

A

. 121 Maximum (>121 red w/box)

      115 Engine overspeed annunciated

106-121 Transient operation, 12 sec (yellow, w/box at 115)

0-105 Normal operation (green)
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7
Q

ENG1 Ng (%) Digital Readouts

A

. 106.0 Maximum (>106.0 red)

  1. 1-106.0 Transient 12 sec (yellow)
  2. 1-105.0 Normal operation (green)
        63.0 Minimum engine out warning annunciationed
                   (<63.0 red w/box).
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8
Q

Torque (%) Digital Readouts with NR <50%

A

. 30 Maximum (>30 red)

0-30 Normal operation (green)

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9
Q

Torque (%) Digital Readouts with NR <90%

A

. 70 Maximum (>70 red)

0-70 Normal operation (green)

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10
Q

Torque (%) Digital Readouts – DE

A

. 115 Maximum (>115 red)

101-115 Transient 6 sec (yellow)

0-100 Normal operation (green)
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11
Q

Torque (%) Digital Readouts – SE

A

. 125 Maximum (>125 red)

123-125 Transient 6 sec (yellow)

111-122 Single Engine Contingency 2.5 min (yellow)

     110 SE maximum continuous power (green)

  0-110 Normal operation (green)
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12
Q

CAUTION: Prolonged APU Operations (NR)

A

Avoid prolonged operation at 94% - 96% NR with the APU running.

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13
Q

APU Operating Limitations (Starts)

A

APU operation is prohibited during normal flight.

(30 - 2 - 20 - 3)
After a fault/aborted start wait 30 seconds
After 2 consecutive start attempts, wait 20 minutes.
No more than 3 start attempts are permitted in one hour.

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14
Q

CAUTION: XMSN Temp

A

Do not operate the APU for more than 5 minutes at a XMSN TEMP of 120 - 130°C.

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15
Q

Extended APU Ground Operations

A

During prolonged ground operations (>30 min), if the temperatures exceed 130°C, shutdown and cool the transmission fluid for 30 minutes prior to resuming APU ground operations.

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16
Q

Maximum Airspeed for Autorotation

A

145 Knots

17
Q

Airspeed Limits With One Engine Inoperative

A

The greater of:

  1. 67% of VNE
  2. The airspeed for minimum power from MAX END/MAX R/C lines
18
Q

Maximum Airspeeds During Manual Stabilator

Operations.

A

Airspeed restrictions are displayed on the:

  • FLT
  • FLT SET
  • SYS pages
19
Q

Maximum Rearward/Sideward Airspeed

A

45 KTA

20
Q

Maximum Airspeed for Searchlight Extension

A
  • Extend/ retract/rotate <90 knots

* Operation not attempted - extended

21
Q

Maximum Airspeed for Stores Jettison

A
  1. Maximum airspeed for stores jettison is 130 KTAS
  2. Hover to 45 KTAS (minimize side slip, if possible)
  3. 45 to 130 KTAS (ball centered, if possible)
22
Q

Maneuvering Limits

A

-10 Limit: ±30° in pitch, ±60° in roll

AWR 2006D-A02 : ±60° in pitch, ±120° in roll

23
Q

Excessive Tail Rotor Scissors Loads

A

(早)Avoid aggressive directional and lateral control inputs greater than 1 inch/second when conducting combat maneuvers requiring a left turn. This is to prevent excessive tail rotor scissors loads.

24
Q

Excessive Tail Rotor Loads

A

(遅)Avoid large pedal step inputs in arresting right hovering/low speed yawing turns greater than 60°/second. This is to prevent excessive tail rotor drive system loads.

25
Q

Flight with Canopy Enclosure Open

A

Flight with the canopy open is prohibited, except for smoke/fume elimination.

26
Q

Landing Limits

A

Pitch attitude change from a hover greater than:

  • 7° up
  • 12° down
  • 10° roll attitude
  • Data is not available beyond above 17,650.
27
Q

Flight into Turbulence

A

Prohibited:

  • Extreme — known or forecast
  • Severe — known
28
Q

Flight In Icing Conditions

A
  • MODERATE icing — Prohibited (Intentional flight)
  • KNOW or FORECAST TRACE or LIGHT icing conditions are authorized and not a hazard unless encountered for an extended period (over one hour).
29
Q

Use of Force Trim

A

Force trim will not be selected off except in a FAULTED or PARTIAL FAILED mode.